Started by upstream project "<a href='/csi/job/ESP_bPreBuilt/' class='jenkins-table__link model-link model-link--float'>ESP_bPreBuilt</a>" build number <a href='/csi/job/ESP_bPreBuilt/76' class='jenkins-table__link model-link model-link--float'>76</a>
originally caused by:
 Started by user <a href='/csi/user/galbramc' class='jenkins-table__link model-link model-link--float'>galbramc</a>
Running as <a href='/csi/user/galbramc' class='jenkins-table__link model-link model-link--float'>galbramc</a>
[EnvInject] - Loading node environment variables.
Building remotely on <a href='/csi/computer/viggen' class='jenkins-table__link model-link model-link--float'>viggen</a> in workspace /Users/jenkins/workspace/ESP_bPreBuilt
[WS-CLEANUP] Deleting project workspace...
[WS-CLEANUP] Deferred wipeout is used...
[WS-CLEANUP] Done
Checking out a fresh workspace because there's no workspace at /Users/jenkins/workspace/ESP_bPreBuilt
Cleaning local Directory .
Checking out svn+ssh://acdl.mit.edu/home/svnroot/OpenCSM/trunk/Jenkins at revision '2024-07-26T18:41:35.498 -0400' --quiet
Using sole credentials 3614a4cf-01de-4393-97de-73734b7dd5a2 in realm ‘svn+ssh://acdl.mit.edu’
Using sole credentials 3614a4cf-01de-4393-97de-73734b7dd5a2 in realm ‘svn+ssh://acdl.mit.edu’
At revision 2518

Checking out a fresh workspace because /Users/jenkins/workspace/ESP_bPreBuilt/JenkinsESP doesn't exist
Cleaning local Directory JenkinsESP
Checking out svn+ssh://acdl.mit.edu/home/svnroot/JenkinsESP at revision '2024-07-26T18:41:35.498 -0400' --quiet
Using sole credentials 3614a4cf-01de-4393-97de-73734b7dd5a2 in realm ‘svn+ssh://acdl.mit.edu’
Using sole credentials 3614a4cf-01de-4393-97de-73734b7dd5a2 in realm ‘svn+ssh://acdl.mit.edu’
At revision 881

Checking out a fresh workspace because /Users/jenkins/workspace/ESP_bPreBuilt/CAPS/training/2023 doesn't exist
Cleaning local Directory CAPS/training/2023
Checking out svn+ssh://acdl.mit.edu/home/svnroot/CAPS/training/2023 at revision '2024-07-26T18:41:35.498 -0400' --quiet
Using sole credentials 3614a4cf-01de-4393-97de-73734b7dd5a2 in realm ‘svn+ssh://acdl.mit.edu’
Using sole credentials 3614a4cf-01de-4393-97de-73734b7dd5a2 in realm ‘svn+ssh://acdl.mit.edu’
At revision 4250

No changes for svn+ssh://acdl.mit.edu/home/svnroot/OpenCSM/trunk/Jenkins since the previous build
No changes for svn+ssh://acdl.mit.edu/home/svnroot/JenkinsESP since the previous build
No changes for svn+ssh://acdl.mit.edu/home/svnroot/CAPS/training/2023 since the previous build
[GitCheckoutListener] SCM 'hudson.scm.SubversionSCM' is not of type GitSCM
Run condition [Execution node ] enabling prebuild for step [Execute shell]
Run condition [Execution node ] enabling prebuild for step [Execute shell]
Run condition [Execution node ] enabling prebuild for step [Execute Windows batch command]
[Execution node] check if [viggen] is in [[macys, macys_VM, master, reynolds, reynolds-centOS7, reynolds-centOS8, reynolds-rhel7, reynolds-ubuntu16, reynolds-ubuntu18, reynolds-ubuntu20]]
Run condition [Execution node ] preventing perform for step [Execute shell]
[Execution node] check if [viggen] is in [[viggen]]
Run condition [Execution node ] enabling perform for step [Execute shell]
[ESP_bPreBuilt] $ /bin/bash -ex /var/folders/l7/7s0m18td3fxg_w_dxpkj1d600000gp/T/jenkins1838911454339454321.sh
+ arch -arch arm64 /bin/bash -ex /Users/jenkins/workspace/ESP_bPreBuilt/JenkinsESP/ESP_PreBuilt.sh
+ source /Users/jenkins/workspace/ESP_bPreBuilt/JenkinsESP/ESP_Env.sh
++ export OCCTREF=7.8
++ OCCTREF=7.8
++ AFLR_VERSION=11.5.15
++ SU2_VERSION=8.0.0
++ TETGEN_VERSION=1.6.0
++ VSP_VERSION=3.38.0
++ export PYTHON_VERSION=3.11.9
++ PYTHON_VERSION=3.11.9
++ export MPLBACKEND=agg
++ MPLBACKEND=agg
++ export EFCOMP=gfortran
++ EFCOMP=gfortran
++ [[ viggen == \r\e\y\n\o\l\d\s ]]
++ [[ '' == *\.\i\f\o\r\t ]]
++ '[' -f /opt/intel/oneapi/setvars.sh ']'
++ source /opt/intel/oneapi/setvars.sh
++ '[' -f /Users/jenkins/.bashrc ']'
++ export CAPS_OUTLEVEL=0
++ CAPS_OUTLEVEL=0
++ export ESP_UDC_PATH=/Users/jenkins/workspace/ESP_bPreBuilt/OpenCSM/trunk/personalUdc
++ ESP_UDC_PATH=/Users/jenkins/workspace/ESP_bPreBuilt/OpenCSM/trunk/personalUdc
++ [[ '' == \D\A\R\W\I\N\6\4\.\g\c\c ]]
++ export ESP_BLOC=/Users/jenkins/workspace/ESP_bPreBuilt/ESP/
++ ESP_BLOC=/Users/jenkins/workspace/ESP_bPreBuilt/ESP/
++ export ESP_ROOT=/Users/jenkins/workspace/ESP_bPreBuilt/ESP/
++ ESP_ROOT=/Users/jenkins/workspace/ESP_bPreBuilt/ESP/
++ export JULIA_DEPOT_PATH=/Users/jenkins/workspace/ESP_bPreBuilt/ESP//julia
++ JULIA_DEPOT_PATH=/Users/jenkins/workspace/ESP_bPreBuilt/ESP//julia
++ export AWAVE=awavemod.f
++ AWAVE=awavemod.f
++ export RLM_CONNECT_TIMEOUT=350
++ RLM_CONNECT_TIMEOUT=350
++ [[ 7.8 != '' ]]
++ [[ '' != '' ]]
++ [[ viggen == *\r\e\y\n\o\l\d\s* ]]
++ [[ viggen == *\m\a\c\y\s* ]]
++ [[ viggen == *\v\i\g\g\e\n* ]]
++ export EMPnumProc=2
++ EMPnumProc=2
++ export OMP_NUM_THREADS=2
++ OMP_NUM_THREADS=2
++ source /Users/jenkins/.bash_profile
++++ /opt/homebrew/bin/brew shellenv
+++ eval 'export HOMEBREW_PREFIX="/opt/homebrew";
export HOMEBREW_CELLAR="/opt/homebrew/Cellar";
export HOMEBREW_REPOSITORY="/opt/homebrew";
export PATH="/opt/homebrew/bin:/opt/homebrew/sbin${PATH+:$PATH}";
[ -z "${MANPATH-}" ] || export MANPATH=":${MANPATH#:}";
export INFOPATH="/opt/homebrew/share/info:${INFOPATH:-}";'
++++ export HOMEBREW_PREFIX=/opt/homebrew
++++ HOMEBREW_PREFIX=/opt/homebrew
++++ export HOMEBREW_CELLAR=/opt/homebrew/Cellar
++++ HOMEBREW_CELLAR=/opt/homebrew/Cellar
++++ export HOMEBREW_REPOSITORY=/opt/homebrew
++++ HOMEBREW_REPOSITORY=/opt/homebrew
++++ export PATH=/opt/homebrew/bin:/opt/homebrew/sbin:/opt/intel/oneapi/dev-utilities/2021.5.0/bin:/usr/bin:/bin:/usr/sbin:/sbin
++++ PATH=/opt/homebrew/bin:/opt/homebrew/sbin:/opt/intel/oneapi/dev-utilities/2021.5.0/bin:/usr/bin:/bin:/usr/sbin:/sbin
++++ '[' -z '' ']'
++++ export INFOPATH=/opt/homebrew/share/info:
++++ INFOPATH=/opt/homebrew/share/info:
+++ [[ -r /opt/homebrew/etc/profile.d/bash_completion.sh ]]
+++ . /opt/homebrew/etc/profile.d/bash_completion.sh
++++ '[' -z '3.2.57(1)-release' -o -z '' -o -n '' ']'
++++ return
+++ export NETCDF_PATH=/opt/homebrew
+++ NETCDF_PATH=/opt/homebrew
++ [[ viggen == *\m\a\c\y\s* ]]
++ export PATH=/opt/homebrew/bin:/opt/homebrew/sbin:/opt/intel/oneapi/dev-utilities/2021.5.0/bin:/usr/bin:/bin:/usr/sbin:/sbin:/opt/homebrew/bin/
++ PATH=/opt/homebrew/bin:/opt/homebrew/sbin:/opt/intel/oneapi/dev-utilities/2021.5.0/bin:/usr/bin:/bin:/usr/sbin:/sbin:/opt/homebrew/bin/
++ [[ viggen == \m\a\c\y\s ]]
++ export CASARCH=.
++ CASARCH=.
++ '[' '!' -z '' ']'
+++ ls -d '/Users/jenkins/util/ESP/OpenCASCADE-.?'
ls: /Users/jenkins/util/ESP/OpenCASCADE-.?: No such file or directory
++ export CASROOT=
++ CASROOT=
++ export UDUNITS2_XML_PATH=/Users/jenkins/workspace/ESP_bPreBuilt/ESP/udunits/udunits2.xml
++ UDUNITS2_XML_PATH=/Users/jenkins/workspace/ESP_bPreBuilt/ESP/udunits/udunits2.xml
++ export ESP_EXTERN_LIBS=/Users/jenkins/util/ESP/ExternLibs
++ ESP_EXTERN_LIBS=/Users/jenkins/util/ESP/ExternLibs
++ export DYLD_LIBRARY_PATH=/Users/jenkins/workspace/ESP_bPreBuilt/ESP//lib:/lib:/opt/intel/oneapi/tbb/2021.5.0/env/../lib:/opt/intel/oneapi/mkl/2022.0.0/lib
++ DYLD_LIBRARY_PATH=/Users/jenkins/workspace/ESP_bPreBuilt/ESP//lib:/lib:/opt/intel/oneapi/tbb/2021.5.0/env/../lib:/opt/intel/oneapi/mkl/2022.0.0/lib
++ export AFLR=/Users/jenkins/util/AFLR/aflr_lib_11.5.15
++ AFLR=/Users/jenkins/util/AFLR/aflr_lib_11.5.15
++ [[ viggen == *\m\a\c\y\s* ]]
++ export AFLR_ARCH=MacOSX-arm64
++ AFLR_ARCH=MacOSX-arm64
++ export ASTROS_ROOT=/Users/jenkins/util/astros/Astros/Darwin-64bit
++ ASTROS_ROOT=/Users/jenkins/util/astros/Astros/Darwin-64bit
++ export PATH=/Users/jenkins/util/astros/Astros/Darwin-64bit:/opt/homebrew/bin:/opt/homebrew/sbin:/opt/intel/oneapi/dev-utilities/2021.5.0/bin:/usr/bin:/bin:/usr/sbin:/sbin:/opt/homebrew/bin/
++ PATH=/Users/jenkins/util/astros/Astros/Darwin-64bit:/opt/homebrew/bin:/opt/homebrew/sbin:/opt/intel/oneapi/dev-utilities/2021.5.0/bin:/usr/bin:/bin:/usr/sbin:/sbin:/opt/homebrew/bin/
++ export CART3D=/Users/jenkins/util/cart3d/cart3d_v1.5.9_OSX64_ICC--22.11.16
++ CART3D=/Users/jenkins/util/cart3d/cart3d_v1.5.9_OSX64_ICC--22.11.16
++ export CART3D_ARCH=OSX64_ICC
++ CART3D_ARCH=OSX64_ICC
++ export PATH=/Users/jenkins/util/cart3d/cart3d_v1.5.9_OSX64_ICC--22.11.16/bin/OSX64_ICC/:/Users/jenkins/util/astros/Astros/Darwin-64bit:/opt/homebrew/bin:/opt/homebrew/sbin:/opt/intel/oneapi/dev-utilities/2021.5.0/bin:/usr/bin:/bin:/usr/sbin:/sbin:/opt/homebrew/bin/
++ PATH=/Users/jenkins/util/cart3d/cart3d_v1.5.9_OSX64_ICC--22.11.16/bin/OSX64_ICC/:/Users/jenkins/util/astros/Astros/Darwin-64bit:/opt/homebrew/bin:/opt/homebrew/sbin:/opt/intel/oneapi/dev-utilities/2021.5.0/bin:/usr/bin:/bin:/usr/sbin:/sbin:/opt/homebrew/bin/
++ export PATH=/Users/jenkins/util/cart3d/cart3d_v1.5.9_OSX64_ICC--22.11.16/bin:/Users/jenkins/util/cart3d/cart3d_v1.5.9_OSX64_ICC--22.11.16/bin/OSX64_ICC/:/Users/jenkins/util/astros/Astros/Darwin-64bit:/opt/homebrew/bin:/opt/homebrew/sbin:/opt/intel/oneapi/dev-utilities/2021.5.0/bin:/usr/bin:/bin:/usr/sbin:/sbin:/opt/homebrew/bin/
++ PATH=/Users/jenkins/util/cart3d/cart3d_v1.5.9_OSX64_ICC--22.11.16/bin:/Users/jenkins/util/cart3d/cart3d_v1.5.9_OSX64_ICC--22.11.16/bin/OSX64_ICC/:/Users/jenkins/util/astros/Astros/Darwin-64bit:/opt/homebrew/bin:/opt/homebrew/sbin:/opt/intel/oneapi/dev-utilities/2021.5.0/bin:/usr/bin:/bin:/usr/sbin:/sbin:/opt/homebrew/bin/
++ export PATH=/Users/jenkins/util/delaundo/delaundo/src:/Users/jenkins/util/cart3d/cart3d_v1.5.9_OSX64_ICC--22.11.16/bin:/Users/jenkins/util/cart3d/cart3d_v1.5.9_OSX64_ICC--22.11.16/bin/OSX64_ICC/:/Users/jenkins/util/astros/Astros/Darwin-64bit:/opt/homebrew/bin:/opt/homebrew/sbin:/opt/intel/oneapi/dev-utilities/2021.5.0/bin:/usr/bin:/bin:/usr/sbin:/sbin:/opt/homebrew/bin/
++ PATH=/Users/jenkins/util/delaundo/delaundo/src:/Users/jenkins/util/cart3d/cart3d_v1.5.9_OSX64_ICC--22.11.16/bin:/Users/jenkins/util/cart3d/cart3d_v1.5.9_OSX64_ICC--22.11.16/bin/OSX64_ICC/:/Users/jenkins/util/astros/Astros/Darwin-64bit:/opt/homebrew/bin:/opt/homebrew/sbin:/opt/intel/oneapi/dev-utilities/2021.5.0/bin:/usr/bin:/bin:/usr/sbin:/sbin:/opt/homebrew/bin/
++ export VSP3_ROOT=/Users/jenkins/util/OpenVSP/OpenVSP-3.38.0-MacOS
++ VSP3_ROOT=/Users/jenkins/util/OpenVSP/OpenVSP-3.38.0-MacOS
++ export PATH=/Users/jenkins/util/refine/build_parallel/install/bin:/Users/jenkins/util/delaundo/delaundo/src:/Users/jenkins/util/cart3d/cart3d_v1.5.9_OSX64_ICC--22.11.16/bin:/Users/jenkins/util/cart3d/cart3d_v1.5.9_OSX64_ICC--22.11.16/bin/OSX64_ICC/:/Users/jenkins/util/astros/Astros/Darwin-64bit:/opt/homebrew/bin:/opt/homebrew/sbin:/opt/intel/oneapi/dev-utilities/2021.5.0/bin:/usr/bin:/bin:/usr/sbin:/sbin:/opt/homebrew/bin/
++ PATH=/Users/jenkins/util/refine/build_parallel/install/bin:/Users/jenkins/util/delaundo/delaundo/src:/Users/jenkins/util/cart3d/cart3d_v1.5.9_OSX64_ICC--22.11.16/bin:/Users/jenkins/util/cart3d/cart3d_v1.5.9_OSX64_ICC--22.11.16/bin/OSX64_ICC/:/Users/jenkins/util/astros/Astros/Darwin-64bit:/opt/homebrew/bin:/opt/homebrew/sbin:/opt/intel/oneapi/dev-utilities/2021.5.0/bin:/usr/bin:/bin:/usr/sbin:/sbin:/opt/homebrew/bin/
++ [[ viggen == \m\a\c\y\s ]]
++ [[ viggen == \v\i\g\g\e\n ]]
++ export SEACAS=/Users/jenkins/util/sandialabs/seacas
++ SEACAS=/Users/jenkins/util/sandialabs/seacas
++ [[ viggen == \v\i\g\g\e\n ]]
++ export NETCDFINC=/opt/homebrew/include
++ NETCDFINC=/opt/homebrew/include
++ export SU2_HOME=/Users/jenkins/util/SU2/SU2-v8.0.0
++ SU2_HOME=/Users/jenkins/util/SU2/SU2-v8.0.0
++ export SU2_RUN=/Users/jenkins/util/SU2/SU2-v8.0.0/bin
++ SU2_RUN=/Users/jenkins/util/SU2/SU2-v8.0.0/bin
++ export PATH=/Users/jenkins/util/refine/build_parallel/install/bin:/Users/jenkins/util/delaundo/delaundo/src:/Users/jenkins/util/cart3d/cart3d_v1.5.9_OSX64_ICC--22.11.16/bin:/Users/jenkins/util/cart3d/cart3d_v1.5.9_OSX64_ICC--22.11.16/bin/OSX64_ICC/:/Users/jenkins/util/astros/Astros/Darwin-64bit:/opt/homebrew/bin:/opt/homebrew/sbin:/opt/intel/oneapi/dev-utilities/2021.5.0/bin:/usr/bin:/bin:/usr/sbin:/sbin:/opt/homebrew/bin/:/Users/jenkins/util/SU2/SU2-v8.0.0/bin
++ PATH=/Users/jenkins/util/refine/build_parallel/install/bin:/Users/jenkins/util/delaundo/delaundo/src:/Users/jenkins/util/cart3d/cart3d_v1.5.9_OSX64_ICC--22.11.16/bin:/Users/jenkins/util/cart3d/cart3d_v1.5.9_OSX64_ICC--22.11.16/bin/OSX64_ICC/:/Users/jenkins/util/astros/Astros/Darwin-64bit:/opt/homebrew/bin:/opt/homebrew/sbin:/opt/intel/oneapi/dev-utilities/2021.5.0/bin:/usr/bin:/bin:/usr/sbin:/sbin:/opt/homebrew/bin/:/Users/jenkins/util/SU2/SU2-v8.0.0/bin
++ export PYTHONPATH=:/Users/jenkins/util/SU2/SU2-v8.0.0/bin
++ PYTHONPATH=:/Users/jenkins/util/SU2/SU2-v8.0.0/bin
++ export TETGEN=/Users/jenkins/util/tetgen/tetgen1.6.0
++ TETGEN=/Users/jenkins/util/tetgen/tetgen1.6.0
++ export PATH=/Users/jenkins/util/tsfoil:/Users/jenkins/util/refine/build_parallel/install/bin:/Users/jenkins/util/delaundo/delaundo/src:/Users/jenkins/util/cart3d/cart3d_v1.5.9_OSX64_ICC--22.11.16/bin:/Users/jenkins/util/cart3d/cart3d_v1.5.9_OSX64_ICC--22.11.16/bin/OSX64_ICC/:/Users/jenkins/util/astros/Astros/Darwin-64bit:/opt/homebrew/bin:/opt/homebrew/sbin:/opt/intel/oneapi/dev-utilities/2021.5.0/bin:/usr/bin:/bin:/usr/sbin:/sbin:/opt/homebrew/bin/:/Users/jenkins/util/SU2/SU2-v8.0.0/bin
++ PATH=/Users/jenkins/util/tsfoil:/Users/jenkins/util/refine/build_parallel/install/bin:/Users/jenkins/util/delaundo/delaundo/src:/Users/jenkins/util/cart3d/cart3d_v1.5.9_OSX64_ICC--22.11.16/bin:/Users/jenkins/util/cart3d/cart3d_v1.5.9_OSX64_ICC--22.11.16/bin/OSX64_ICC/:/Users/jenkins/util/astros/Astros/Darwin-64bit:/opt/homebrew/bin:/opt/homebrew/sbin:/opt/intel/oneapi/dev-utilities/2021.5.0/bin:/usr/bin:/bin:/usr/sbin:/sbin:/opt/homebrew/bin/:/Users/jenkins/util/SU2/SU2-v8.0.0/bin
++ '[' -d /Users/jenkins/util/cart3d/cart3d_v1.5.9_OSX64_ICC--22.11.16 ']'
+++ perl -I/Users/jenkins/util/cart3d/cart3d_v1.5.9_OSX64_ICC--22.11.16/lib/perl/lib/perl5 -Mlocal::lib=/Users/jenkins/util/cart3d/cart3d_v1.5.9_OSX64_ICC--22.11.16/lib/perl
++ eval 'PATH="/Users/jenkins/util/cart3d/cart3d_v1.5.9_OSX64_ICC--22.11.16/lib/perl/bin${PATH:+:${PATH}}"; export PATH;
PERL5LIB="/Users/jenkins/util/cart3d/cart3d_v1.5.9_OSX64_ICC--22.11.16/lib/perl/lib/perl5${PERL5LIB:+:${PERL5LIB}}"; export PERL5LIB;
PERL_LOCAL_LIB_ROOT="/Users/jenkins/util/cart3d/cart3d_v1.5.9_OSX64_ICC--22.11.16/lib/perl${PERL_LOCAL_LIB_ROOT:+:${PERL_LOCAL_LIB_ROOT}}"; export PERL_LOCAL_LIB_ROOT;
PERL_MB_OPT="--install_base \"/Users/jenkins/util/cart3d/cart3d_v1.5.9_OSX64_ICC--22.11.16/lib/perl\""; export PERL_MB_OPT;
PERL_MM_OPT="INSTALL_BASE=/Users/jenkins/util/cart3d/cart3d_v1.5.9_OSX64_ICC--22.11.16/lib/perl"; export PERL_MM_OPT;'
+++ PATH=/Users/jenkins/util/cart3d/cart3d_v1.5.9_OSX64_ICC--22.11.16/lib/perl/bin:/Users/jenkins/util/tsfoil:/Users/jenkins/util/refine/build_parallel/install/bin:/Users/jenkins/util/delaundo/delaundo/src:/Users/jenkins/util/cart3d/cart3d_v1.5.9_OSX64_ICC--22.11.16/bin:/Users/jenkins/util/cart3d/cart3d_v1.5.9_OSX64_ICC--22.11.16/bin/OSX64_ICC/:/Users/jenkins/util/astros/Astros/Darwin-64bit:/opt/homebrew/bin:/opt/homebrew/sbin:/opt/intel/oneapi/dev-utilities/2021.5.0/bin:/usr/bin:/bin:/usr/sbin:/sbin:/opt/homebrew/bin/:/Users/jenkins/util/SU2/SU2-v8.0.0/bin
+++ export PATH
+++ PERL5LIB=/Users/jenkins/util/cart3d/cart3d_v1.5.9_OSX64_ICC--22.11.16/lib/perl/lib/perl5
+++ export PERL5LIB
+++ PERL_LOCAL_LIB_ROOT=/Users/jenkins/util/cart3d/cart3d_v1.5.9_OSX64_ICC--22.11.16/lib/perl
+++ export PERL_LOCAL_LIB_ROOT
+++ PERL_MB_OPT='--install_base "/Users/jenkins/util/cart3d/cart3d_v1.5.9_OSX64_ICC--22.11.16/lib/perl"'
+++ export PERL_MB_OPT
+++ PERL_MM_OPT=INSTALL_BASE=/Users/jenkins/util/cart3d/cart3d_v1.5.9_OSX64_ICC--22.11.16/lib/perl
+++ export PERL_MM_OPT
++ export PATH=/Users/jenkins/workspace/ESP_bPreBuilt/ESP//bin:/Users/jenkins/util/cart3d/cart3d_v1.5.9_OSX64_ICC--22.11.16/lib/perl/bin:/Users/jenkins/util/tsfoil:/Users/jenkins/util/refine/build_parallel/install/bin:/Users/jenkins/util/delaundo/delaundo/src:/Users/jenkins/util/cart3d/cart3d_v1.5.9_OSX64_ICC--22.11.16/bin:/Users/jenkins/util/cart3d/cart3d_v1.5.9_OSX64_ICC--22.11.16/bin/OSX64_ICC/:/Users/jenkins/util/astros/Astros/Darwin-64bit:/opt/homebrew/bin:/opt/homebrew/sbin:/opt/intel/oneapi/dev-utilities/2021.5.0/bin:/usr/bin:/bin:/usr/sbin:/sbin:/opt/homebrew/bin/:/Users/jenkins/util/SU2/SU2-v8.0.0/bin
++ PATH=/Users/jenkins/workspace/ESP_bPreBuilt/ESP//bin:/Users/jenkins/util/cart3d/cart3d_v1.5.9_OSX64_ICC--22.11.16/lib/perl/bin:/Users/jenkins/util/tsfoil:/Users/jenkins/util/refine/build_parallel/install/bin:/Users/jenkins/util/delaundo/delaundo/src:/Users/jenkins/util/cart3d/cart3d_v1.5.9_OSX64_ICC--22.11.16/bin:/Users/jenkins/util/cart3d/cart3d_v1.5.9_OSX64_ICC--22.11.16/bin/OSX64_ICC/:/Users/jenkins/util/astros/Astros/Darwin-64bit:/opt/homebrew/bin:/opt/homebrew/sbin:/opt/intel/oneapi/dev-utilities/2021.5.0/bin:/usr/bin:/bin:/usr/sbin:/sbin:/opt/homebrew/bin/:/Users/jenkins/util/SU2/SU2-v8.0.0/bin
++ export PATH=/Users/jenkins/workspace/ESP_bPreBuilt/ESP//test:/Users/jenkins/workspace/ESP_bPreBuilt/ESP//bin:/Users/jenkins/util/cart3d/cart3d_v1.5.9_OSX64_ICC--22.11.16/lib/perl/bin:/Users/jenkins/util/tsfoil:/Users/jenkins/util/refine/build_parallel/install/bin:/Users/jenkins/util/delaundo/delaundo/src:/Users/jenkins/util/cart3d/cart3d_v1.5.9_OSX64_ICC--22.11.16/bin:/Users/jenkins/util/cart3d/cart3d_v1.5.9_OSX64_ICC--22.11.16/bin/OSX64_ICC/:/Users/jenkins/util/astros/Astros/Darwin-64bit:/opt/homebrew/bin:/opt/homebrew/sbin:/opt/intel/oneapi/dev-utilities/2021.5.0/bin:/usr/bin:/bin:/usr/sbin:/sbin:/opt/homebrew/bin/:/Users/jenkins/util/SU2/SU2-v8.0.0/bin
++ PATH=/Users/jenkins/workspace/ESP_bPreBuilt/ESP//test:/Users/jenkins/workspace/ESP_bPreBuilt/ESP//bin:/Users/jenkins/util/cart3d/cart3d_v1.5.9_OSX64_ICC--22.11.16/lib/perl/bin:/Users/jenkins/util/tsfoil:/Users/jenkins/util/refine/build_parallel/install/bin:/Users/jenkins/util/delaundo/delaundo/src:/Users/jenkins/util/cart3d/cart3d_v1.5.9_OSX64_ICC--22.11.16/bin:/Users/jenkins/util/cart3d/cart3d_v1.5.9_OSX64_ICC--22.11.16/bin/OSX64_ICC/:/Users/jenkins/util/astros/Astros/Darwin-64bit:/opt/homebrew/bin:/opt/homebrew/sbin:/opt/intel/oneapi/dev-utilities/2021.5.0/bin:/usr/bin:/bin:/usr/sbin:/sbin:/opt/homebrew/bin/:/Users/jenkins/util/SU2/SU2-v8.0.0/bin
++ export PYTHONPATH=/Users/jenkins/workspace/ESP_bPreBuilt/EGADS/trunk/pyEGADS::/Users/jenkins/util/SU2/SU2-v8.0.0/bin
++ PYTHONPATH=/Users/jenkins/workspace/ESP_bPreBuilt/EGADS/trunk/pyEGADS::/Users/jenkins/util/SU2/SU2-v8.0.0/bin
++ export PYTHONPATH=/Users/jenkins/workspace/ESP_bPreBuilt/OpenCSM/trunk/pyOCSM:/Users/jenkins/workspace/ESP_bPreBuilt/EGADS/trunk/pyEGADS::/Users/jenkins/util/SU2/SU2-v8.0.0/bin
++ PYTHONPATH=/Users/jenkins/workspace/ESP_bPreBuilt/OpenCSM/trunk/pyOCSM:/Users/jenkins/workspace/ESP_bPreBuilt/EGADS/trunk/pyEGADS::/Users/jenkins/util/SU2/SU2-v8.0.0/bin
++ export PYTHONPATH=/Users/jenkins/workspace/ESP_bPreBuilt/CAPS/pyCAPS:/Users/jenkins/workspace/ESP_bPreBuilt/OpenCSM/trunk/pyOCSM:/Users/jenkins/workspace/ESP_bPreBuilt/EGADS/trunk/pyEGADS::/Users/jenkins/util/SU2/SU2-v8.0.0/bin
++ PYTHONPATH=/Users/jenkins/workspace/ESP_bPreBuilt/CAPS/pyCAPS:/Users/jenkins/workspace/ESP_bPreBuilt/OpenCSM/trunk/pyOCSM:/Users/jenkins/workspace/ESP_bPreBuilt/EGADS/trunk/pyEGADS::/Users/jenkins/util/SU2/SU2-v8.0.0/bin
++ [[ viggen == \m\a\c\y\s* ]]
++ [[ viggen == \v\i\g\g\e\n ]]
++ mkdir -p /Users/jenkins/workspace/ESP_bPreBuilt/ESP//bin
++ rm -f /Users/jenkins/workspace/ESP_bPreBuilt/ESP//bin/python
++ rm -f /Users/jenkins/workspace/ESP_bPreBuilt/ESP//bin/python-config
++ rm -f /Users/jenkins/workspace/ESP_bPreBuilt/ESP//bin/virtualenv
++ rm -f '/Users/jenkins/workspace/ESP_bPreBuilt/ESP//bin/analyze-*'
++ rm -f '/Users/jenkins/workspace/ESP_bPreBuilt/ESP//bin/intercept-*'
++ [[ viggen == \m\a\c\y\s ]]
++ [[ viggen == \v\i\g\g\e\n ]]
++ ln -s /Users/jenkins/util/ESP/Python/ESP_Python-3.11.9/bin/python3 /Users/jenkins/workspace/ESP_bPreBuilt/ESP//bin/python
++ ln -s /Users/jenkins/util/ESP/Python/ESP_Python-3.11.9/bin/python3-config /Users/jenkins/workspace/ESP_bPreBuilt/ESP//bin/python-config
++ ln -s /Users/jenkins/util/ESP/Python/ESP_Python-3.11.9/bin/virtualenv /Users/jenkins/workspace/ESP_bPreBuilt/ESP//bin/virtualenv
+++ ls /Users/jenkins/util/ESP/Python/ESP_Python-3.11.9/bin/analyze-build /Users/jenkins/util/ESP/Python/ESP_Python-3.11.9/bin/analyze-c++ /Users/jenkins/util/ESP/Python/ESP_Python-3.11.9/bin/analyze-cc /Users/jenkins/util/ESP/Python/ESP_Python-3.11.9/bin/intercept-build /Users/jenkins/util/ESP/Python/ESP_Python-3.11.9/bin/intercept-c++ /Users/jenkins/util/ESP/Python/ESP_Python-3.11.9/bin/intercept-cc
++ for i in '`ls /Users/jenkins/util/ESP/Python/ESP_Python-${PYTHON_VERSION}/bin/analyze-* /Users/jenkins/util/ESP/Python/ESP_Python-${PYTHON_VERSION}/bin/intercept-*`'
+++ basename /Users/jenkins/util/ESP/Python/ESP_Python-3.11.9/bin/analyze-build
+++ basename /Users/jenkins/util/ESP/Python/ESP_Python-3.11.9/bin/analyze-build
++ ln -s /Users/jenkins/util/ESP/Python/ESP_Python-3.11.9/bin/analyze-build /Users/jenkins/workspace/ESP_bPreBuilt/ESP//bin/analyze-build
++ for i in '`ls /Users/jenkins/util/ESP/Python/ESP_Python-${PYTHON_VERSION}/bin/analyze-* /Users/jenkins/util/ESP/Python/ESP_Python-${PYTHON_VERSION}/bin/intercept-*`'
+++ basename /Users/jenkins/util/ESP/Python/ESP_Python-3.11.9/bin/analyze-c++
+++ basename /Users/jenkins/util/ESP/Python/ESP_Python-3.11.9/bin/analyze-c++
++ ln -s /Users/jenkins/util/ESP/Python/ESP_Python-3.11.9/bin/analyze-c++ /Users/jenkins/workspace/ESP_bPreBuilt/ESP//bin/analyze-c++
++ for i in '`ls /Users/jenkins/util/ESP/Python/ESP_Python-${PYTHON_VERSION}/bin/analyze-* /Users/jenkins/util/ESP/Python/ESP_Python-${PYTHON_VERSION}/bin/intercept-*`'
+++ basename /Users/jenkins/util/ESP/Python/ESP_Python-3.11.9/bin/analyze-cc
+++ basename /Users/jenkins/util/ESP/Python/ESP_Python-3.11.9/bin/analyze-cc
++ ln -s /Users/jenkins/util/ESP/Python/ESP_Python-3.11.9/bin/analyze-cc /Users/jenkins/workspace/ESP_bPreBuilt/ESP//bin/analyze-cc
++ for i in '`ls /Users/jenkins/util/ESP/Python/ESP_Python-${PYTHON_VERSION}/bin/analyze-* /Users/jenkins/util/ESP/Python/ESP_Python-${PYTHON_VERSION}/bin/intercept-*`'
+++ basename /Users/jenkins/util/ESP/Python/ESP_Python-3.11.9/bin/intercept-build
+++ basename /Users/jenkins/util/ESP/Python/ESP_Python-3.11.9/bin/intercept-build
++ ln -s /Users/jenkins/util/ESP/Python/ESP_Python-3.11.9/bin/intercept-build /Users/jenkins/workspace/ESP_bPreBuilt/ESP//bin/intercept-build
++ for i in '`ls /Users/jenkins/util/ESP/Python/ESP_Python-${PYTHON_VERSION}/bin/analyze-* /Users/jenkins/util/ESP/Python/ESP_Python-${PYTHON_VERSION}/bin/intercept-*`'
+++ basename /Users/jenkins/util/ESP/Python/ESP_Python-3.11.9/bin/intercept-c++
+++ basename /Users/jenkins/util/ESP/Python/ESP_Python-3.11.9/bin/intercept-c++
++ ln -s /Users/jenkins/util/ESP/Python/ESP_Python-3.11.9/bin/intercept-c++ /Users/jenkins/workspace/ESP_bPreBuilt/ESP//bin/intercept-c++
++ for i in '`ls /Users/jenkins/util/ESP/Python/ESP_Python-${PYTHON_VERSION}/bin/analyze-* /Users/jenkins/util/ESP/Python/ESP_Python-${PYTHON_VERSION}/bin/intercept-*`'
+++ basename /Users/jenkins/util/ESP/Python/ESP_Python-3.11.9/bin/intercept-cc
+++ basename /Users/jenkins/util/ESP/Python/ESP_Python-3.11.9/bin/intercept-cc
++ ln -s /Users/jenkins/util/ESP/Python/ESP_Python-3.11.9/bin/intercept-cc /Users/jenkins/workspace/ESP_bPreBuilt/ESP//bin/intercept-cc
+++ python-config --includes
++ export 'PYTHONINC=. -I/Users/jenkins/util/ESP/Python/ESP_Python-3.11.9/include/python3.11 -I/Users/jenkins/util/ESP/Python/ESP_Python-3.11.9/include/python3.11'
++ PYTHONINC='. -I/Users/jenkins/util/ESP/Python/ESP_Python-3.11.9/include/python3.11 -I/Users/jenkins/util/ESP/Python/ESP_Python-3.11.9/include/python3.11'
+++ python-config --help
++ [[ Usage: /Users/jenkins/workspace/ESP_bPreBuilt/ESP//bin/python-config [--prefix|--exec-prefix|--includes|--libs|--cflags|--ldflags|--extension-suffix|--help|--abiflags|--configdir|--embed] == *\e\m\b\e\d* ]]
+++ python-config --ldflags --embed
++ export 'PYTHONLIB=-L/Users/jenkins/util/ESP/Python/ESP_Python-3.11.9/lib -lpython3.11 -ldl -framework CoreFoundation'
++ PYTHONLIB='-L/Users/jenkins/util/ESP/Python/ESP_Python-3.11.9/lib -lpython3.11 -ldl -framework CoreFoundation'
++ [[ viggen == \m\a\c\y\s ]]
++ [[ viggen == \v\i\g\g\e\n ]]
++ export 'PYTHONLIB=-L/Users/jenkins/util/ESP/Python/ESP_Python-3.11.9/lib -lpython3.11 -ldl -framework CoreFoundation -Wl,-w'
++ PYTHONLIB='-L/Users/jenkins/util/ESP/Python/ESP_Python-3.11.9/lib -lpython3.11 -ldl -framework CoreFoundation -Wl,-w'
++ export PYTHONUNBUFFERED=true
++ PYTHONUNBUFFERED=true
++ export PYTHONFAULTHANDLER=true
++ PYTHONFAULTHANDLER=true
++ python --version
Python 3.11.9
++ [[ '' == \D\A\R\W\I\N\6\4\.\g\c\c ]]
++ export CSMDATA=/Users/jenkins/workspace/ESP_bPreBuilt/OpenCSM/trunk/data
++ CSMDATA=/Users/jenkins/workspace/ESP_bPreBuilt/OpenCSM/trunk/data
+ unset PYTHONINC
+ unset PYTHONLIB
+ unset ESP_BLOC
+ unset ESP_ROOT
+ unset ESP_ARCH
+ unset AWAVE
++ uname -s
+ [[ Darwin == *\D\a\r\w\i\n* ]]
+ DESKTOP=/Users/jenkins/Desktop
+ OSI=macos
++ uname -m
+ ARCH=arm64
+ wget --tries=3 <a href='https://acdl.mit.edu/ESP/archive/ESP126-macos-arm64.tgz'>https://acdl.mit.edu/ESP/archive/ESP126-macos-arm64.tgz</a>
--2024-07-26 18:41:49--  <a href='https://acdl.mit.edu/ESP/archive/ESP126-macos-arm64.tgz'>https://acdl.mit.edu/ESP/archive/ESP126-macos-arm64.tgz</a>
Resolving acdl.mit.edu (acdl.mit.edu)... 18.18.33.14
Connecting to acdl.mit.edu (acdl.mit.edu)|18.18.33.14|:443... connected.
HTTP request sent, awaiting response... 200 OK
Length: 522032067 (498M) [application/x-gzip]
Saving to: ‘ESP126-macos-arm64.tgz’

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  6850K .......... .......... .......... .......... ..........  1% 11.3M 21s
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  7500K .......... .......... .......... .......... ..........  1% 39.4M 23s
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  7900K .......... .......... .......... .......... ..........  1% 13.9M 24s
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  8000K .......... .......... .......... .......... ..........  1% 16.0M 24s
  8050K .......... .......... .......... .......... ..........  1% 10.5M 24s
  8100K .......... .......... .......... .......... ..........  1% 13.8M 24s
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105550K .......... .......... .......... .......... .......... 20% 33.0M 27s
105600K .......... .......... .......... .......... .......... 20% 12.3M 27s
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119000K .......... .......... .......... .......... .......... 23% 10.2M 27s
119050K .......... .......... .......... .......... .......... 23% 11.9M 27s
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119200K .......... .......... .......... .......... .......... 23% 7.86M 27s
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119300K .......... .......... .......... .......... .......... 23% 26.3M 27s
119350K .......... .......... .......... .......... .......... 23% 24.6M 27s
119400K .......... .......... .......... .......... .......... 23% 17.6M 27s
119450K .......... .......... .......... .......... .......... 23% 26.3M 27s
119500K .......... .......... .......... .......... .......... 23% 33.1M 27s
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119600K .......... .......... .......... .......... .......... 23% 19.8M 27s
119650K .......... .......... .......... .......... .......... 23% 18.9M 27s
119700K .......... .......... .......... .......... .......... 23% 17.2M 27s
119750K .......... .......... .......... .......... .......... 23% 10.8M 27s
119800K .......... .......... .......... .......... .......... 23% 46.8M 27s
119850K .......... .......... .......... .......... .......... 23% 9.40M 27s
119900K .......... .......... .......... .......... .......... 23% 11.0M 27s
119950K .......... .......... .......... .......... .......... 23% 8.08M 27s
120000K .......... .......... .......... .......... .......... 23% 11.0M 27s
120050K .......... .......... .......... .......... .......... 23% 12.3M 27s
120100K .......... .......... .......... .......... .......... 23% 8.06M 27s
120150K .......... .......... .......... .......... .......... 23% 6.45M 27s
120200K .......... .......... .......... .......... .......... 23% 4.28M 27s
120250K .......... .......... .......... .......... .......... 23% 4.09M 27s
120300K .......... .......... .......... .......... .......... 23% 11.6M 27s
120350K .......... .......... .......... .......... .......... 23% 10.5M 27s
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120450K .......... .......... .......... .......... .......... 23% 9.56M 27s
120500K .......... .......... .......... .......... .......... 23% 10.9M 27s
120550K .......... .......... .......... .......... .......... 23% 14.1M 27s
120600K .......... .......... .......... .......... .......... 23% 8.00M 27s
120650K .......... .......... .......... .......... .......... 23% 12.2M 27s
120700K .......... .......... .......... .......... .......... 23% 27.1M 27s
120750K .......... .......... .......... .......... .......... 23% 32.0M 27s
120800K .......... .......... .......... .......... .......... 23% 14.9M 27s
120850K .......... .......... .......... .......... .......... 23% 79.7M 27s
120900K .......... .......... .......... .......... .......... 23% 25.8M 27s
120950K .......... .......... .......... .......... .......... 23% 29.1M 27s
121000K .......... .......... .......... .......... .......... 23% 17.8M 27s
121050K .......... .......... .......... .......... .......... 23% 41.8M 27s
121100K .......... .......... .......... .......... .......... 23% 19.0M 27s
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121200K .......... .......... .......... .......... .......... 23% 15.6M 27s
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121300K .......... .......... .......... .......... .......... 23% 19.7M 27s
121350K .......... .......... .......... .......... .......... 23% 15.6M 27s
121400K .......... .......... .......... .......... .......... 23% 20.2M 27s
121450K .......... .......... .......... .......... .......... 23% 13.4M 27s
121500K .......... .......... .......... .......... .......... 23% 18.3M 27s
121550K .......... .......... .......... .......... .......... 23% 12.5M 27s
121600K .......... .......... .......... .......... .......... 23% 10.2M 27s
121650K .......... .......... .......... .......... .......... 23% 93.9M 27s
121700K .......... .......... .......... .......... .......... 23% 32.2M 27s
121750K .......... .......... .......... .......... .......... 23% 17.5M 27s
121800K .......... .......... .......... .......... .......... 23% 46.6M 27s
121850K .......... .......... .......... .......... .......... 23% 13.0M 27s
121900K .......... .......... .......... .......... .......... 23% 18.0M 27s
121950K .......... .......... .......... .......... .......... 23% 14.6M 27s
122000K .......... .......... .......... .......... .......... 23% 3.96M 27s
122050K .......... .......... .......... .......... .......... 23% 12.5M 27s
122100K .......... .......... .......... .......... .......... 23% 9.64M 27s
122150K .......... .......... .......... .......... .......... 23% 10.0M 27s
122200K .......... .......... .......... .......... .......... 23% 8.35M 27s
122250K .......... .......... .......... .......... .......... 23% 29.5M 27s
122300K .......... .......... .......... .......... .......... 23% 29.0M 27s
122350K .......... .......... .......... .......... .......... 24% 28.6M 27s
122400K .......... .......... .......... .......... .......... 24% 27.3M 27s
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122500K .......... .......... .......... .......... .......... 24% 31.2M 27s
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122600K .......... .......... .......... .......... .......... 24% 26.9M 27s
122650K .......... .......... .......... .......... .......... 24% 21.1M 27s
122700K .......... .......... .......... .......... .......... 24% 21.0M 27s
122750K .......... .......... .......... .......... .......... 24% 13.2M 27s
122800K .......... .......... .......... .......... .......... 24% 13.1M 27s
122850K .......... .......... .......... .......... .......... 24% 10.0M 27s
122900K .......... .......... .......... .......... .......... 24% 12.7M 27s
122950K .......... .......... .......... .......... .......... 24% 11.5M 27s
123000K .......... .......... .......... .......... .......... 24% 11.9M 27s
123050K .......... .......... .......... .......... .......... 24% 9.01M 27s
123100K .......... .......... .......... .......... .......... 24% 7.48M 27s
123150K .......... .......... .......... .......... .......... 24% 5.29M 27s
123200K .......... .......... .......... .......... .......... 24% 9.08M 27s
123250K .......... .......... .......... .......... .......... 24% 9.97M 27s
123300K .......... .......... .......... .......... .......... 24% 7.02M 27s
123350K .......... .......... .......... .......... .......... 24% 9.69M 27s
123400K .......... .......... .......... .......... .......... 24% 14.5M 27s
123450K .......... .......... .......... .......... .......... 24% 12.2M 27s
123500K .......... .......... .......... .......... .......... 24% 13.2M 27s
123550K .......... .......... .......... .......... .......... 24% 11.1M 27s
123600K .......... .......... .......... .......... .......... 24% 9.01M 27s
123650K .......... .......... .......... .......... .......... 24% 10.1M 27s
123700K .......... .......... .......... .......... .......... 24% 9.31M 27s
123750K .......... .......... .......... .......... .......... 24% 9.82M 27s
123800K .......... .......... .......... .......... .......... 24% 10.7M 27s
123850K .......... .......... .......... .......... .......... 24% 8.63M 27s
123900K .......... .......... .......... .......... .......... 24% 11.0M 27s
123950K .......... .......... .......... .......... .......... 24% 9.51M 27s
124000K .......... .......... .......... .......... .......... 24% 28.0M 27s
124050K .......... .......... .......... .......... .......... 24% 17.2M 27s
124100K .......... .......... .......... .......... .......... 24% 23.6M 27s
124150K .......... .......... .......... .......... .......... 24% 16.3M 27s
124200K .......... .......... .......... .......... .......... 24% 14.4M 27s
124250K .......... .......... .......... .......... .......... 24% 21.0M 27s
124300K .......... .......... .......... .......... .......... 24% 15.1M 27s
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124400K .......... .......... .......... .......... .......... 24% 10.0M 27s
124450K .......... .......... .......... .......... .......... 24% 15.1M 27s
124500K .......... .......... .......... .......... .......... 24% 10.5M 27s
124550K .......... .......... .......... .......... .......... 24% 12.5M 27s
124600K .......... .......... .......... .......... .......... 24% 9.51M 27s
124650K .......... .......... .......... .......... .......... 24% 8.24M 27s
124700K .......... .......... .......... .......... .......... 24% 8.01M 27s
124750K .......... .......... .......... .......... .......... 24% 8.22M 27s
124800K .......... .......... .......... .......... .......... 24% 8.27M 27s
124850K .......... .......... .......... .......... .......... 24% 6.43M 27s
124900K .......... .......... .......... .......... .......... 24% 8.54M 27s
124950K .......... .......... .......... .......... .......... 24% 9.62M 27s
125000K .......... .......... .......... .......... .......... 24% 47.8M 27s
125050K .......... .......... .......... .......... .......... 24% 38.9M 27s
125100K .......... .......... .......... .......... .......... 24% 17.2M 27s
125150K .......... .......... .......... .......... .......... 24% 17.1M 27s
125200K .......... .......... .......... .......... .......... 24% 16.2M 27s
125250K .......... .......... .......... .......... .......... 24% 15.8M 27s
125300K .......... .......... .......... .......... .......... 24% 12.6M 27s
125350K .......... .......... .......... .......... .......... 24% 12.2M 27s
125400K .......... .......... .......... .......... .......... 24% 11.8M 27s
125450K .......... .......... .......... .......... .......... 24% 12.8M 27s
125500K .......... .......... .......... .......... .......... 24% 13.2M 27s
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125600K .......... .......... .......... .......... .......... 24% 17.2M 27s
125650K .......... .......... .......... .......... .......... 24% 34.2M 27s
125700K .......... .......... .......... .......... .......... 24% 41.1M 27s
125750K .......... .......... .......... .......... .......... 24% 21.6M 27s
125800K .......... .......... .......... .......... .......... 24% 75.0M 27s
125850K .......... .......... .......... .......... .......... 24% 27.7M 27s
125900K .......... .......... .......... .......... .......... 24% 75.7M 27s
125950K .......... .......... .......... .......... .......... 24% 26.1M 27s
126000K .......... .......... .......... .......... .......... 24% 22.6M 27s
126050K .......... .......... .......... .......... .......... 24% 44.7M 27s
126100K .......... .......... .......... .......... .......... 24% 20.9M 27s
126150K .......... .......... .......... .......... .......... 24% 17.1M 27s
126200K .......... .......... .......... .......... .......... 24% 11.9M 27s
126250K .......... .......... .......... .......... .......... 24% 32.0M 27s
126300K .......... .......... .......... .......... .......... 24% 16.6M 27s
126350K .......... .......... .......... .......... .......... 24% 13.1M 27s
126400K .......... .......... .......... .......... .......... 24% 14.5M 27s
126450K .......... .......... .......... .......... .......... 24% 15.8M 27s
126500K .......... .......... .......... .......... .......... 24% 15.2M 27s
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126600K .......... .......... .......... .......... .......... 24% 8.83M 27s
126650K .......... .......... .......... .......... .......... 24% 14.1M 27s
126700K .......... .......... .......... .......... .......... 24% 8.55M 27s
126750K .......... .......... .......... .......... .......... 24% 17.5M 27s
126800K .......... .......... .......... .......... .......... 24% 13.4M 27s
126850K .......... .......... .......... .......... .......... 24% 11.8M 27s
126900K .......... .......... .......... .......... .......... 24% 16.2M 27s
126950K .......... .......... .......... .......... .......... 24% 63.3M 27s
127000K .......... .......... .......... .......... .......... 24% 21.2M 27s
127050K .......... .......... .......... .......... .......... 24% 56.6M 27s
127100K .......... .......... .......... .......... .......... 24% 19.3M 27s
127150K .......... .......... .......... .......... .......... 24% 52.6M 27s
127200K .......... .......... .......... .......... .......... 24% 15.7M 27s
127250K .......... .......... .......... .......... .......... 24% 21.9M 27s
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127350K .......... .......... .......... .......... .......... 24% 14.6M 27s
127400K .......... .......... .......... .......... .......... 25% 12.3M 27s
127450K .......... .......... .......... .......... .......... 25% 13.5M 27s
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127550K .......... .......... .......... .......... .......... 25% 8.71M 27s
127600K .......... .......... .......... .......... .......... 25% 17.8M 27s
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127700K .......... .......... .......... .......... .......... 25% 6.63M 27s
127750K .......... .......... .......... .......... .......... 25% 9.43M 27s
127800K .......... .......... .......... .......... .......... 25% 10.8M 27s
127850K .......... .......... .......... .......... .......... 25% 9.94M 27s
127900K .......... .......... .......... .......... .......... 25% 10.6M 27s
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128000K .......... .......... .......... .......... .......... 25% 10.0M 27s
128050K .......... .......... .......... .......... .......... 25% 15.2M 27s
128100K .......... .......... .......... .......... .......... 25% 27.1M 27s
128150K .......... .......... .......... .......... .......... 25% 16.2M 27s
128200K .......... .......... .......... .......... .......... 25% 49.3M 27s
128250K .......... .......... .......... .......... .......... 25% 35.0M 27s
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128400K .......... .......... .......... .......... .......... 25% 17.1M 27s
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128500K .......... .......... .......... .......... .......... 25% 13.4M 27s
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128650K .......... .......... .......... .......... .......... 25% 13.6M 27s
128700K .......... .......... .......... .......... .......... 25% 8.65M 27s
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128800K .......... .......... .......... .......... .......... 25% 9.05M 27s
128850K .......... .......... .......... .......... .......... 25% 7.15M 27s
128900K .......... .......... .......... .......... .......... 25% 12.1M 27s
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129000K .......... .......... .......... .......... .......... 25% 9.80M 27s
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129100K .......... .......... .......... .......... .......... 25% 7.76M 27s
129150K .......... .......... .......... .......... .......... 25% 8.58M 27s
129200K .......... .......... .......... .......... .......... 25% 6.93M 27s
129250K .......... .......... .......... .......... .......... 25% 8.07M 27s
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129350K .......... .......... .......... .......... .......... 25% 8.09M 27s
129400K .......... .......... .......... .......... .......... 25% 8.86M 27s
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129500K .......... .......... .......... .......... .......... 25% 7.74M 27s
129550K .......... .......... .......... .......... .......... 25% 9.09M 27s
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129650K .......... .......... .......... .......... .......... 25% 24.9M 27s
129700K .......... .......... .......... .......... .......... 25% 26.9M 27s
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129800K .......... .......... .......... .......... .......... 25% 16.5M 27s
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129900K .......... .......... .......... .......... .......... 25% 34.3M 27s
129950K .......... .......... .......... .......... .......... 25% 16.6M 27s
130000K .......... .......... .......... .......... .......... 25% 14.4M 27s
130050K .......... .......... .......... .......... .......... 25% 14.8M 27s
130100K .......... .......... .......... .......... .......... 25% 17.7M 27s
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130200K .......... .......... .......... .......... .......... 25% 14.7M 27s
130250K .......... .......... .......... .......... .......... 25% 13.6M 27s
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130350K .......... .......... .......... .......... .......... 25% 12.3M 27s
130400K .......... .......... .......... .......... .......... 25% 12.1M 27s
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130500K .......... .......... .......... .......... .......... 25% 12.8M 27s
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130600K .......... .......... .......... .......... .......... 25% 17.5M 27s
130650K .......... .......... .......... .......... .......... 25% 72.2M 27s
130700K .......... .......... .......... .......... .......... 25% 27.4M 27s
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130800K .......... .......... .......... .......... .......... 25% 75.9M 26s
130850K .......... .......... .......... .......... .......... 25% 19.3M 26s
130900K .......... .......... .......... .......... .......... 25% 72.7M 26s
130950K .......... .......... .......... .......... .......... 25% 34.0M 26s
131000K .......... .......... .......... .......... .......... 25% 27.4M 26s
131050K .......... .......... .......... .......... .......... 25% 23.1M 26s
131100K .......... .......... .......... .......... .......... 25% 14.4M 26s
131150K .......... .......... .......... .......... .......... 25% 51.5M 26s
131200K .......... .......... .......... .......... .......... 25% 19.8M 26s
131250K .......... .......... .......... .......... .......... 25% 22.2M 26s
131300K .......... .......... .......... .......... .......... 25% 26.7M 26s
131350K .......... .......... .......... .......... .......... 25% 19.9M 26s
131400K .......... .......... .......... .......... .......... 25% 20.9M 26s
131450K .......... .......... .......... .......... .......... 25% 16.4M 26s
131500K .......... .......... .......... .......... .......... 25% 21.8M 26s
131550K .......... .......... .......... .......... .......... 25% 21.0M 26s
131600K .......... .......... .......... .......... .......... 25% 14.5M 26s
131650K .......... .......... .......... .......... .......... 25% 16.1M 26s
131700K .......... .......... .......... .......... .......... 25% 8.75M 26s
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131800K .......... .......... .......... .......... .......... 25% 12.1M 26s
131850K .......... .......... .......... .......... .......... 25% 7.67M 26s
131900K .......... .......... .......... .......... .......... 25% 9.04M 26s
131950K .......... .......... .......... .......... .......... 25% 7.88M 26s
132000K .......... .......... .......... .......... .......... 25% 8.86M 26s
132050K .......... .......... .......... .......... .......... 25% 8.84M 26s
132100K .......... .......... .......... .......... .......... 25% 7.75M 26s
132150K .......... .......... .......... .......... .......... 25% 14.0M 26s
132200K .......... .......... .......... .......... .......... 25% 20.0M 26s
132250K .......... .......... .......... .......... .......... 25% 20.0M 26s
132300K .......... .......... .......... .......... .......... 25% 17.8M 26s
132350K .......... .......... .......... .......... .......... 25% 15.0M 26s
132400K .......... .......... .......... .......... .......... 25% 16.5M 26s
132450K .......... .......... .......... .......... .......... 25% 11.1M 26s
132500K .......... .......... .......... .......... .......... 26% 10.2M 26s
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132600K .......... .......... .......... .......... .......... 26% 10.2M 26s
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132700K .......... .......... .......... .......... .......... 26% 11.0M 26s
132750K .......... .......... .......... .......... .......... 26% 14.5M 26s
132800K .......... .......... .......... .......... .......... 26% 29.8M 26s
132850K .......... .......... .......... .......... .......... 26% 23.2M 26s
132900K .......... .......... .......... .......... .......... 26% 21.8M 26s
132950K .......... .......... .......... .......... .......... 26% 55.9M 26s
133000K .......... .......... .......... .......... .......... 26% 28.7M 26s
133050K .......... .......... .......... .......... .......... 26% 28.9M 26s
133100K .......... .......... .......... .......... .......... 26% 25.2M 26s
133150K .......... .......... .......... .......... .......... 26% 26.5M 26s
133200K .......... .......... .......... .......... .......... 26% 28.9M 26s
133250K .......... .......... .......... .......... .......... 26% 28.1M 26s
133300K .......... .......... .......... .......... .......... 26% 24.5M 26s
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133400K .......... .......... .......... .......... .......... 26% 29.9M 26s
133450K .......... .......... .......... .......... .......... 26% 21.5M 26s
133500K .......... .......... .......... .......... .......... 26% 22.5M 26s
133550K .......... .......... .......... .......... .......... 26% 24.9M 26s
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133650K .......... .......... .......... .......... .......... 26% 17.7M 26s
133700K .......... .......... .......... .......... .......... 26% 17.1M 26s
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133800K .......... .......... .......... .......... .......... 26% 20.8M 26s
133850K .......... .......... .......... .......... .......... 26% 11.8M 26s
133900K .......... .......... .......... .......... .......... 26% 14.5M 26s
133950K .......... .......... .......... .......... .......... 26% 8.22M 26s
134000K .......... .......... .......... .......... .......... 26% 19.8M 26s
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161500K .......... .......... .......... .......... .......... 31% 58.6M 25s
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162150K .......... .......... .......... .......... .......... 31% 29.2M 25s
162200K .......... .......... .......... .......... .......... 31% 23.7M 25s
162250K .......... .......... .......... .......... .......... 31% 27.0M 25s
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162800K .......... .......... .......... .......... .......... 31% 83.2M 25s
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176350K .......... .......... .......... .......... .......... 34% 5.95M 24s
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190450K .......... .......... .......... .......... .......... 37% 8.48M 23s
190500K .......... .......... .......... .......... .......... 37% 11.5M 23s
190550K .......... .......... .......... .......... .......... 37% 8.44M 23s
190600K .......... .......... .......... .......... .......... 37% 8.53M 23s
190650K .......... .......... .......... .......... .......... 37% 5.73M 23s
190700K .......... .......... .......... .......... .......... 37% 6.66M 23s
190750K .......... .......... .......... .......... .......... 37% 7.74M 23s
190800K .......... .......... .......... .......... .......... 37% 8.45M 23s
190850K .......... .......... .......... .......... .......... 37% 5.67M 23s
190900K .......... .......... .......... .......... .......... 37% 15.0M 23s
190950K .......... .......... .......... .......... .......... 37% 10.2M 23s
191000K .......... .......... .......... .......... .......... 37% 12.3M 23s
191050K .......... .......... .......... .......... .......... 37% 10.2M 23s
191100K .......... .......... .......... .......... .......... 37% 10.6M 23s
191150K .......... .......... .......... .......... .......... 37% 10.7M 23s
191200K .......... .......... .......... .......... .......... 37% 8.12M 23s
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191300K .......... .......... .......... .......... .......... 37% 11.0M 23s
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191400K .......... .......... .......... .......... .......... 37% 9.27M 23s
191450K .......... .......... .......... .......... .......... 37% 8.41M 23s
191500K .......... .......... .......... .......... .......... 37% 9.36M 23s
191550K .......... .......... .......... .......... .......... 37% 12.3M 23s
191600K .......... .......... .......... .......... .......... 37% 18.1M 23s
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191700K .......... .......... .......... .......... .......... 37% 27.4M 23s
191750K .......... .......... .......... .......... .......... 37% 19.9M 23s
191800K .......... .......... .......... .......... .......... 37% 56.4M 23s
191850K .......... .......... .......... .......... .......... 37% 20.5M 22s
191900K .......... .......... .......... .......... .......... 37% 23.0M 22s
191950K .......... .......... .......... .......... .......... 37% 15.0M 22s
192000K .......... .......... .......... .......... .......... 37% 16.3M 22s
192050K .......... .......... .......... .......... .......... 37% 18.7M 22s
192100K .......... .......... .......... .......... .......... 37% 12.6M 22s
192150K .......... .......... .......... .......... .......... 37% 13.5M 22s
192200K .......... .......... .......... .......... .......... 37% 12.3M 22s
192250K .......... .......... .......... .......... .......... 37% 11.8M 22s
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192500K .......... .......... .......... .......... .......... 37% 20.8M 22s
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192700K .......... .......... .......... .......... .......... 37% 10.2M 22s
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192800K .......... .......... .......... .......... .......... 37% 14.5M 22s
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192900K .......... .......... .......... .......... .......... 37% 17.0M 22s
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193000K .......... .......... .......... .......... .......... 37% 13.8M 22s
193050K .......... .......... .......... .......... .......... 37% 10.5M 22s
193100K .......... .......... .......... .......... .......... 37% 9.76M 22s
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193200K .......... .......... .......... .......... .......... 37% 7.93M 22s
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193300K .......... .......... .......... .......... .......... 37% 13.6M 22s
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193400K .......... .......... .......... .......... .......... 37% 11.4M 22s
193450K .......... .......... .......... .......... .......... 37% 7.01M 22s
193500K .......... .......... .......... .......... .......... 37% 8.11M 22s
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193600K .......... .......... .......... .......... .......... 37% 5.36M 22s
193650K .......... .......... .......... .......... .......... 37% 5.00M 22s
193700K .......... .......... .......... .......... .......... 38% 4.81M 22s
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193800K .......... .......... .......... .......... .......... 38% 12.3M 22s
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193900K .......... .......... .......... .......... .......... 38% 12.0M 22s
193950K .......... .......... .......... .......... .......... 38% 10.3M 22s
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194050K .......... .......... .......... .......... .......... 38% 10.9M 22s
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194200K .......... .......... .......... .......... .......... 38% 8.43M 22s
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194300K .......... .......... .......... .......... .......... 38% 6.57M 22s
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194400K .......... .......... .......... .......... .......... 38% 14.7M 22s
194450K .......... .......... .......... .......... .......... 38% 64.5M 22s
194500K .......... .......... .......... .......... .......... 38% 23.8M 22s
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194600K .......... .......... .......... .......... .......... 38% 11.7M 22s
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194750K .......... .......... .......... .......... .......... 38% 14.7M 22s
194800K .......... .......... .......... .......... .......... 38% 18.4M 22s
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194900K .......... .......... .......... .......... .......... 38% 13.9M 22s
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195000K .......... .......... .......... .......... .......... 38% 8.30M 22s
195050K .......... .......... .......... .......... .......... 38% 8.96M 22s
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195150K .......... .......... .......... .......... .......... 38% 13.5M 22s
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195300K .......... .......... .......... .......... .......... 38% 12.6M 22s
195350K .......... .......... .......... .......... .......... 38% 8.96M 22s
195400K .......... .......... .......... .......... .......... 38% 11.3M 22s
195450K .......... .......... .......... .......... .......... 38% 5.85M 22s
195500K .......... .......... .......... .......... .......... 38% 77.4M 22s
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195600K .......... .......... .......... .......... .......... 38% 11.0M 22s
195650K .......... .......... .......... .......... .......... 38% 35.3M 22s
195700K .......... .......... .......... .......... .......... 38% 16.2M 22s
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195800K .......... .......... .......... .......... .......... 38% 13.1M 22s
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195900K .......... .......... .......... .......... .......... 38% 16.0M 22s
195950K .......... .......... .......... .......... .......... 38% 11.0M 22s
196000K .......... .......... .......... .......... .......... 38% 15.7M 22s
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196150K .......... .......... .......... .......... .......... 38% 13.9M 22s
196200K .......... .......... .......... .......... .......... 38% 30.4M 22s
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196300K .......... .......... .......... .......... .......... 38% 37.9M 22s
196350K .......... .......... .......... .......... .......... 38% 15.0M 22s
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196550K .......... .......... .......... .......... .......... 38% 71.7M 22s
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196700K .......... .......... .......... .......... .......... 38% 18.7M 22s
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196800K .......... .......... .......... .......... .......... 38% 19.8M 22s
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196950K .......... .......... .......... .......... .......... 38% 13.9M 22s
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197050K .......... .......... .......... .......... .......... 38% 10.9M 22s
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197150K .......... .......... .......... .......... .......... 38% 10.7M 22s
197200K .......... .......... .......... .......... .......... 38% 8.89M 22s
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197300K .......... .......... .......... .......... .......... 38% 7.68M 22s
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197400K .......... .......... .......... .......... .......... 38% 12.8M 22s
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197500K .......... .......... .......... .......... .......... 38% 12.6M 22s
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197600K .......... .......... .......... .......... .......... 38% 10.1M 22s
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197700K .......... .......... .......... .......... .......... 38% 11.6M 22s
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197800K .......... .......... .......... .......... .......... 38% 10.8M 22s
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197900K .......... .......... .......... .......... .......... 38% 12.2M 22s
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198000K .......... .......... .......... .......... .......... 38% 10.2M 22s
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198200K .......... .......... .......... .......... .......... 38% 91.4M 22s
198250K .......... .......... .......... .......... .......... 38% 5.06M 22s
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198500K .......... .......... .......... .......... .......... 38% 7.32M 22s
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198600K .......... .......... .......... .......... .......... 38% 17.8M 22s
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198700K .......... .......... .......... .......... .......... 38% 13.5M 22s
198750K .......... .......... .......... .......... .......... 38% 23.7M 22s
198800K .......... .......... .......... .......... .......... 39% 33.7M 22s
198850K .......... .......... .......... .......... .......... 39% 16.3M 22s
198900K .......... .......... .......... .......... .......... 39% 18.7M 22s
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199000K .......... .......... .......... .......... .......... 39% 13.7M 22s
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199100K .......... .......... .......... .......... .......... 39% 13.5M 22s
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199200K .......... .......... .......... .......... .......... 39% 14.2M 22s
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199300K .......... .......... .......... .......... .......... 39% 9.29M 22s
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199400K .......... .......... .......... .......... .......... 39% 27.9M 22s
199450K .......... .......... .......... .......... .......... 39% 28.5M 22s
199500K .......... .......... .......... .......... .......... 39% 83.2M 22s
199550K .......... .......... .......... .......... .......... 39% 17.2M 22s
199600K .......... .......... .......... .......... .......... 39% 28.0M 22s
199650K .......... .......... .......... .......... .......... 39% 23.1M 22s
199700K .......... .......... .......... .......... .......... 39% 23.1M 22s
199750K .......... .......... .......... .......... .......... 39% 95.6M 22s
199800K .......... .......... .......... .......... .......... 39% 23.0M 22s
199850K .......... .......... .......... .......... .......... 39% 15.6M 22s
199900K .......... .......... .......... .......... .......... 39% 85.7M 22s
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200000K .......... .......... .......... .......... .......... 39% 64.8M 22s
200050K .......... .......... .......... .......... .......... 39% 20.9M 22s
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200300K .......... .......... .......... .......... .......... 39% 21.2M 22s
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200400K .......... .......... .......... .......... .......... 39% 22.3M 22s
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200550K .......... .......... .......... .......... .......... 39% 12.5M 22s
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200800K .......... .......... .......... .......... .......... 39% 9.70M 22s
200850K .......... .......... .......... .......... .......... 39% 20.3M 22s
200900K .......... .......... .......... .......... .......... 39% 10.5M 22s
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201000K .......... .......... .......... .......... .......... 39% 10.3M 22s
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201100K .......... .......... .......... .......... .......... 39% 7.48M 22s
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201200K .......... .......... .......... .......... .......... 39% 8.39M 22s
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201300K .......... .......... .......... .......... .......... 39% 30.7M 22s
201350K .......... .......... .......... .......... .......... 39% 17.9M 22s
201400K .......... .......... .......... .......... .......... 39% 16.3M 22s
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201550K .......... .......... .......... .......... .......... 39% 19.7M 22s
201600K .......... .......... .......... .......... .......... 39% 11.7M 22s
201650K .......... .......... .......... .......... .......... 39% 19.0M 22s
201700K .......... .......... .......... .......... .......... 39% 9.54M 22s
201750K .......... .......... .......... .......... .......... 39% 16.9M 22s
201800K .......... .......... .......... .......... .......... 39% 12.9M 22s
201850K .......... .......... .......... .......... .......... 39% 12.2M 22s
201900K .......... .......... .......... .......... .......... 39% 12.2M 22s
201950K .......... .......... .......... .......... .......... 39% 12.2M 22s
202000K .......... .......... .......... .......... .......... 39% 15.1M 22s
202050K .......... .......... .......... .......... .......... 39% 19.6M 22s
202100K .......... .......... .......... .......... .......... 39% 15.6M 22s
202150K .......... .......... .......... .......... .......... 39% 17.2M 22s
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202800K .......... .......... .......... .......... .......... 39% 18.9M 22s
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203000K .......... .......... .......... .......... .......... 39% 8.86M 22s
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203100K .......... .......... .......... .......... .......... 39% 11.0M 22s
203150K .......... .......... .......... .......... .......... 39% 14.5M 22s
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203250K .......... .......... .......... .......... .......... 39% 11.6M 22s
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203550K .......... .......... .......... .......... .......... 39% 11.8M 22s
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203700K .......... .......... .......... .......... .......... 39% 11.6M 22s
203750K .......... .......... .......... .......... .......... 39% 35.3M 22s
203800K .......... .......... .......... .......... .......... 39% 72.6M 22s
203850K .......... .......... .......... .......... .......... 39% 17.4M 22s
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204000K .......... .......... .......... .......... .......... 40% 11.3M 22s
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204100K .......... .......... .......... .......... .......... 40% 9.93M 22s
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204200K .......... .......... .......... .......... .......... 40% 9.76M 22s
204250K .......... .......... .......... .......... .......... 40% 12.7M 22s
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204350K .......... .......... .......... .......... .......... 40% 16.8M 22s
204400K .......... .......... .......... .......... .......... 40% 29.0M 22s
204450K .......... .......... .......... .......... .......... 40% 18.5M 22s
204500K .......... .......... .......... .......... .......... 40% 28.1M 22s
204550K .......... .......... .......... .......... .......... 40% 45.7M 22s
204600K .......... .......... .......... .......... .......... 40% 22.9M 22s
204650K .......... .......... .......... .......... .......... 40% 15.8M 22s
204700K .......... .......... .......... .......... .......... 40% 48.1M 22s
204750K .......... .......... .......... .......... .......... 40% 21.2M 22s
204800K .......... .......... .......... .......... .......... 40% 18.5M 22s
204850K .......... .......... .......... .......... .......... 40% 15.2M 22s
204900K .......... .......... .......... .......... .......... 40% 20.7M 22s
204950K .......... .......... .......... .......... .......... 40% 16.4M 22s
205000K .......... .......... .......... .......... .......... 40% 18.1M 22s
205050K .......... .......... .......... .......... .......... 40% 17.3M 22s
205100K .......... .......... .......... .......... .......... 40% 13.0M 22s
205150K .......... .......... .......... .......... .......... 40% 19.8M 22s
205200K .......... .......... .......... .......... .......... 40% 15.6M 22s
205250K .......... .......... .......... .......... .......... 40% 18.9M 22s
205300K .......... .......... .......... .......... .......... 40% 18.0M 22s
205350K .......... .......... .......... .......... .......... 40% 15.9M 22s
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205450K .......... .......... .......... .......... .......... 40% 8.24M 22s
205500K .......... .......... .......... .......... .......... 40% 9.99M 22s
205550K .......... .......... .......... .......... .......... 40% 6.62M 22s
205600K .......... .......... .......... .......... .......... 40% 8.19M 22s
205650K .......... .......... .......... .......... .......... 40% 8.07M 22s
205700K .......... .......... .......... .......... .......... 40% 7.32M 22s
205750K .......... .......... .......... .......... .......... 40% 7.73M 22s
205800K .......... .......... .......... .......... .......... 40% 7.27M 22s
205850K .......... .......... .......... .......... .......... 40% 2.86M 22s
205900K .......... .......... .......... .......... .......... 40% 2.61M 22s
205950K .......... .......... .......... .......... .......... 40% 3.22M 22s
206000K .......... .......... .......... .......... .......... 40% 17.2M 22s
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206100K .......... .......... .......... .......... .......... 40% 13.4M 22s
206150K .......... .......... .......... .......... .......... 40% 71.0M 22s
206200K .......... .......... .......... .......... .......... 40% 19.2M 22s
206250K .......... .......... .......... .......... .......... 40% 52.1M 22s
206300K .......... .......... .......... .......... .......... 40% 22.5M 22s
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206400K .......... .......... .......... .......... .......... 40% 19.8M 22s
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206500K .......... .......... .......... .......... .......... 40% 26.8M 22s
206550K .......... .......... .......... .......... .......... 40% 18.9M 22s
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206700K .......... .......... .......... .......... .......... 40% 14.1M 22s
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206800K .......... .......... .......... .......... .......... 40% 14.5M 22s
206850K .......... .......... .......... .......... .......... 40% 12.2M 22s
206900K .......... .......... .......... .......... .......... 40% 10.3M 22s
206950K .......... .......... .......... .......... .......... 40% 8.63M 22s
207000K .......... .......... .......... .......... .......... 40% 7.67M 22s
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207100K .......... .......... .......... .......... .......... 40% 5.57M 22s
207150K .......... .......... .......... .......... .......... 40% 5.26M 22s
207200K .......... .......... .......... .......... .......... 40% 4.45M 22s
207250K .......... .......... .......... .......... .......... 40% 6.87M 22s
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207400K .......... .......... .......... .......... .......... 40% 12.2M 22s
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207500K .......... .......... .......... .......... .......... 40% 14.5M 22s
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207600K .......... .......... .......... .......... .......... 40% 10.2M 22s
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207700K .......... .......... .......... .......... .......... 40% 12.6M 22s
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207800K .......... .......... .......... .......... .......... 40% 13.2M 22s
207850K .......... .......... .......... .......... .......... 40% 9.38M 22s
207900K .......... .......... .......... .......... .......... 40% 11.3M 22s
207950K .......... .......... .......... .......... .......... 40% 39.2M 22s
208000K .......... .......... .......... .......... .......... 40% 19.7M 22s
208050K .......... .......... .......... .......... .......... 40% 26.8M 22s
208100K .......... .......... .......... .......... .......... 40% 14.6M 22s
208150K .......... .......... .......... .......... .......... 40% 17.8M 22s
208200K .......... .......... .......... .......... .......... 40% 19.8M 22s
208250K .......... .......... .......... .......... .......... 40% 19.8M 22s
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208350K .......... .......... .......... .......... .......... 40% 12.8M 22s
208400K .......... .......... .......... .......... .......... 40% 17.9M 22s
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208500K .......... .......... .......... .......... .......... 40% 14.4M 22s
208550K .......... .......... .......... .......... .......... 40% 12.2M 22s
208600K .......... .......... .......... .......... .......... 40% 7.85M 22s
208650K .......... .......... .......... .......... .......... 40% 12.1M 22s
208700K .......... .......... .......... .......... .......... 40% 11.4M 22s
208750K .......... .......... .......... .......... .......... 40% 10.2M 22s
208800K .......... .......... .......... .......... .......... 40% 9.47M 22s
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208900K .......... .......... .......... .......... .......... 40% 8.84M 22s
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209000K .......... .......... .......... .......... .......... 41% 12.6M 22s
209050K .......... .......... .......... .......... .......... 41% 74.3M 21s
209100K .......... .......... .......... .......... .......... 41% 22.6M 21s
209150K .......... .......... .......... .......... .......... 41% 24.6M 21s
209200K .......... .......... .......... .......... .......... 41% 13.4M 21s
209250K .......... .......... .......... .......... .......... 41% 16.8M 21s
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209450K .......... .......... .......... .......... .......... 41% 11.0M 21s
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209600K .......... .......... .......... .......... .......... 41% 7.33M 21s
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209800K .......... .......... .......... .......... .......... 41% 11.6M 21s
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210000K .......... .......... .......... .......... .......... 41% 9.23M 21s
210050K .......... .......... .......... .......... .......... 41% 7.48M 21s
210100K .......... .......... .......... .......... .......... 41% 8.43M 21s
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210200K .......... .......... .......... .......... .......... 41% 12.4M 21s
210250K .......... .......... .......... .......... .......... 41% 18.0M 21s
210300K .......... .......... .......... .......... .......... 41% 79.5M 21s
210350K .......... .......... .......... .......... .......... 41% 30.0M 21s
210400K .......... .......... .......... .......... .......... 41% 18.3M 21s
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210500K .......... .......... .......... .......... .......... 41% 15.9M 21s
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210600K .......... .......... .......... .......... .......... 41% 18.0M 21s
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210700K .......... .......... .......... .......... .......... 41% 13.0M 21s
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210800K .......... .......... .......... .......... .......... 41% 12.6M 21s
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211000K .......... .......... .......... .......... .......... 41% 6.93M 21s
211050K .......... .......... .......... .......... .......... 41% 78.4M 21s
211100K .......... .......... .......... .......... .......... 41% 11.6M 21s
211150K .......... .......... .......... .......... .......... 41% 15.2M 21s
211200K .......... .......... .......... .......... .......... 41% 11.8M 21s
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211300K .......... .......... .......... .......... .......... 41% 11.0M 21s
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211400K .......... .......... .......... .......... .......... 41% 15.2M 21s
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211500K .......... .......... .......... .......... .......... 41% 9.67M 21s
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211600K .......... .......... .......... .......... .......... 41% 7.07M 21s
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211700K .......... .......... .......... .......... .......... 41% 9.73M 21s
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211800K .......... .......... .......... .......... .......... 41% 14.5M 21s
211850K .......... .......... .......... .......... .......... 41% 12.9M 21s
211900K .......... .......... .......... .......... .......... 41% 9.92M 21s
211950K .......... .......... .......... .......... .......... 41% 10.5M 21s
212000K .......... .......... .......... .......... .......... 41% 11.8M 21s
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212200K .......... .......... .......... .......... .......... 41% 8.80M 21s
212250K .......... .......... .......... .......... .......... 41% 7.78M 21s
212300K .......... .......... .......... .......... .......... 41% 13.9M 21s
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212400K .......... .......... .......... .......... .......... 41% 10.4M 21s
212450K .......... .......... .......... .......... .......... 41% 7.31M 21s
212500K .......... .......... .......... .......... .......... 41% 15.1M 21s
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212600K .......... .......... .......... .......... .......... 41% 7.20M 21s
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212900K .......... .......... .......... .......... .......... 41% 7.08M 21s
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213000K .......... .......... .......... .......... .......... 41% 10.2M 21s
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213100K .......... .......... .......... .......... .......... 41% 8.22M 21s
213150K .......... .......... .......... .......... .......... 41% 9.99M 21s
213200K .......... .......... .......... .......... .......... 41% 8.41M 21s
213250K .......... .......... .......... .......... .......... 41% 8.00M 21s
213300K .......... .......... .......... .......... .......... 41% 7.65M 21s
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213400K .......... .......... .......... .......... .......... 41% 7.77M 21s
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213500K .......... .......... .......... .......... .......... 41% 11.4M 21s
213550K .......... .......... .......... .......... .......... 41% 6.99M 21s
213600K .......... .......... .......... .......... .......... 41% 10.9M 21s
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213700K .......... .......... .......... .......... .......... 41% 7.30M 21s
213750K .......... .......... .......... .......... .......... 41% 9.29M 21s
213800K .......... .......... .......... .......... .......... 41% 12.4M 21s
213850K .......... .......... .......... .......... .......... 41% 8.27M 21s
213900K .......... .......... .......... .......... .......... 41% 8.02M 21s
213950K .......... .......... .......... .......... .......... 41% 5.76M 21s
214000K .......... .......... .......... .......... .......... 41% 8.66M 21s
214050K .......... .......... .......... .......... .......... 41% 9.97M 21s
214100K .......... .......... .......... .......... .......... 42% 5.57M 21s
214150K .......... .......... .......... .......... .......... 42% 4.18M 21s
214200K .......... .......... .......... .......... .......... 42% 4.53M 21s
214250K .......... .......... .......... .......... .......... 42% 4.78M 21s
214300K .......... .......... .......... .......... .......... 42% 3.99M 21s
214350K .......... .......... .......... .......... .......... 42% 3.19M 21s
214400K .......... .......... .......... .......... .......... 42% 2.85M 21s
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214500K .......... .......... .......... .......... .......... 42% 17.6M 21s
214550K .......... .......... .......... .......... .......... 42% 29.9M 21s
214600K .......... .......... .......... .......... .......... 42% 18.0M 21s
214650K .......... .......... .......... .......... .......... 42% 38.2M 21s
214700K .......... .......... .......... .......... .......... 42% 17.7M 21s
214750K .......... .......... .......... .......... .......... 42% 19.7M 21s
214800K .......... .......... .......... .......... .......... 42% 11.2M 21s
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214900K .......... .......... .......... .......... .......... 42% 17.9M 21s
214950K .......... .......... .......... .......... .......... 42% 9.53M 21s
215000K .......... .......... .......... .......... .......... 42% 12.2M 21s
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215100K .......... .......... .......... .......... .......... 42% 13.6M 21s
215150K .......... .......... .......... .......... .......... 42% 9.30M 21s
215200K .......... .......... .......... .......... .......... 42% 12.8M 21s
215250K .......... .......... .......... .......... .......... 42% 13.9M 21s
215300K .......... .......... .......... .......... .......... 42% 9.07M 21s
215350K .......... .......... .......... .......... .......... 42% 75.8M 21s
215400K .......... .......... .......... .......... .......... 42% 21.5M 21s
215450K .......... .......... .......... .......... .......... 42% 19.3M 21s
215500K .......... .......... .......... .......... .......... 42% 19.1M 21s
215550K .......... .......... .......... .......... .......... 42% 29.7M 21s
215600K .......... .......... .......... .......... .......... 42% 20.8M 21s
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215700K .......... .......... .......... .......... .......... 42% 13.9M 21s
215750K .......... .......... .......... .......... .......... 42% 20.7M 21s
215800K .......... .......... .......... .......... .......... 42% 21.0M 21s
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215900K .......... .......... .......... .......... .......... 42% 20.7M 21s
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216000K .......... .......... .......... .......... .......... 42% 19.1M 21s
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216100K .......... .......... .......... .......... .......... 42% 14.5M 21s
216150K .......... .......... .......... .......... .......... 42% 15.6M 21s
216200K .......... .......... .......... .......... .......... 42% 12.0M 21s
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216300K .......... .......... .......... .......... .......... 42% 8.22M 21s
216350K .......... .......... .......... .......... .......... 42% 12.1M 21s
216400K .......... .......... .......... .......... .......... 42% 11.9M 21s
216450K .......... .......... .......... .......... .......... 42% 8.62M 21s
216500K .......... .......... .......... .......... .......... 42% 10.4M 21s
216550K .......... .......... .......... .......... .......... 42% 13.5M 21s
216600K .......... .......... .......... .......... .......... 42% 8.88M 21s
216650K .......... .......... .......... .......... .......... 42% 9.07M 21s
216700K .......... .......... .......... .......... .......... 42% 8.28M 21s
216750K .......... .......... .......... .......... .......... 42% 6.03M 21s
216800K .......... .......... .......... .......... .......... 42% 6.93M 21s
216850K .......... .......... .......... .......... .......... 42% 5.04M 21s
216900K .......... .......... .......... .......... .......... 42% 5.82M 21s
216950K .......... .......... .......... .......... .......... 42% 8.78M 21s
217000K .......... .......... .......... .......... .......... 42% 13.1M 21s
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217100K .......... .......... .......... .......... .......... 42% 12.2M 21s
217150K .......... .......... .......... .......... .......... 42% 14.5M 21s
217200K .......... .......... .......... .......... .......... 42% 10.2M 21s
217250K .......... .......... .......... .......... .......... 42% 12.3M 21s
217300K .......... .......... .......... .......... .......... 42% 14.6M 21s
217350K .......... .......... .......... .......... .......... 42% 13.1M 21s
217400K .......... .......... .......... .......... .......... 42% 11.8M 21s
217450K .......... .......... .......... .......... .......... 42% 27.7M 21s
217500K .......... .......... .......... .......... .......... 42% 35.6M 21s
217550K .......... .......... .......... .......... .......... 42% 11.2M 21s
217600K .......... .......... .......... .......... .......... 42% 70.9M 21s
217650K .......... .......... .......... .......... .......... 42% 27.1M 21s
217700K .......... .......... .......... .......... .......... 42% 18.0M 21s
217750K .......... .......... .......... .......... .......... 42% 25.0M 21s
217800K .......... .......... .......... .......... .......... 42% 22.2M 21s
217850K .......... .......... .......... .......... .......... 42% 15.1M 21s
217900K .......... .......... .......... .......... .......... 42% 17.9M 21s
217950K .......... .......... .......... .......... .......... 42% 12.2M 21s
218000K .......... .......... .......... .......... .......... 42% 10.6M 21s
218050K .......... .......... .......... .......... .......... 42% 13.1M 21s
218100K .......... .......... .......... .......... .......... 42% 10.7M 21s
218150K .......... .......... .......... .......... .......... 42% 13.2M 21s
218200K .......... .......... .......... .......... .......... 42% 7.14M 21s
218250K .......... .......... .......... .......... .......... 42% 10.8M 21s
218300K .......... .......... .......... .......... .......... 42% 10.8M 21s
218350K .......... .......... .......... .......... .......... 42% 7.60M 21s
218400K .......... .......... .......... .......... .......... 42% 7.31M 21s
218450K .......... .......... .......... .......... .......... 42% 6.98M 21s
218500K .......... .......... .......... .......... .......... 42% 7.19M 21s
218550K .......... .......... .......... .......... .......... 42% 6.34M 21s
218600K .......... .......... .......... .......... .......... 42% 4.90M 21s
218650K .......... .......... .......... .......... .......... 42% 6.52M 21s
218700K .......... .......... .......... .......... .......... 42% 17.6M 21s
218750K .......... .......... .......... .......... .......... 42% 26.4M 21s
218800K .......... .......... .......... .......... .......... 42% 19.2M 21s
218850K .......... .......... .......... .......... .......... 42% 16.7M 21s
218900K .......... .......... .......... .......... .......... 42% 27.4M 21s
218950K .......... .......... .......... .......... .......... 42% 21.6M 21s
219000K .......... .......... .......... .......... .......... 42% 16.7M 21s
219050K .......... .......... .......... .......... .......... 42% 8.79M 21s
219100K .......... .......... .......... .......... .......... 42% 12.5M 21s
219150K .......... .......... .......... .......... .......... 42% 12.6M 21s
219200K .......... .......... .......... .......... .......... 43% 10.2M 21s
219250K .......... .......... .......... .......... .......... 43% 9.50M 21s
219300K .......... .......... .......... .......... .......... 43% 7.11M 21s
219350K .......... .......... .......... .......... .......... 43% 5.08M 21s
219400K .......... .......... .......... .......... .......... 43% 5.67M 21s
219450K .......... .......... .......... .......... .......... 43% 3.16M 21s
219500K .......... .......... .......... .......... .......... 43% 8.65M 21s
219550K .......... .......... .......... .......... .......... 43% 10.5M 21s
219600K .......... .......... .......... .......... .......... 43% 9.46M 21s
219650K .......... .......... .......... .......... .......... 43% 8.24M 21s
219700K .......... .......... .......... .......... .......... 43% 8.83M 21s
219750K .......... .......... .......... .......... .......... 43% 10.2M 21s
219800K .......... .......... .......... .......... .......... 43% 13.5M 21s
219850K .......... .......... .......... .......... .......... 43% 17.3M 21s
219900K .......... .......... .......... .......... .......... 43% 27.2M 21s
219950K .......... .......... .......... .......... .......... 43% 18.7M 21s
220000K .......... .......... .......... .......... .......... 43% 16.9M 21s
220050K .......... .......... .......... .......... .......... 43% 62.0M 21s
220100K .......... .......... .......... .......... .......... 43% 22.0M 21s
220150K .......... .......... .......... .......... .......... 43% 23.6M 21s
220200K .......... .......... .......... .......... .......... 43% 20.1M 21s
220250K .......... .......... .......... .......... .......... 43% 18.4M 21s
220300K .......... .......... .......... .......... .......... 43% 24.0M 21s
220350K .......... .......... .......... .......... .......... 43% 15.3M 21s
220400K .......... .......... .......... .......... .......... 43% 12.9M 21s
220450K .......... .......... .......... .......... .......... 43% 19.5M 21s
220500K .......... .......... .......... .......... .......... 43% 13.8M 21s
220550K .......... .......... .......... .......... .......... 43% 19.0M 21s
220600K .......... .......... .......... .......... .......... 43% 16.6M 21s
220650K .......... .......... .......... .......... .......... 43% 16.1M 21s
220700K .......... .......... .......... .......... .......... 43% 4.03M 21s
220750K .......... .......... .......... .......... .......... 43% 11.5M 21s
220800K .......... .......... .......... .......... .......... 43% 18.0M 21s
220850K .......... .......... .......... .......... .......... 43% 16.6M 21s
220900K .......... .......... .......... .......... .......... 43% 11.8M 21s
220950K .......... .......... .......... .......... .......... 43% 11.6M 21s
221000K .......... .......... .......... .......... .......... 43% 23.5M 21s
221050K .......... .......... .......... .......... .......... 43% 18.3M 21s
221100K .......... .......... .......... .......... .......... 43% 17.4M 21s
221150K .......... .......... .......... .......... .......... 43% 18.2M 21s
221200K .......... .......... .......... .......... .......... 43% 20.0M 21s
221250K .......... .......... .......... .......... .......... 43% 34.8M 21s
221300K .......... .......... .......... .......... .......... 43% 22.4M 21s
221350K .......... .......... .......... .......... .......... 43% 19.5M 21s
221400K .......... .......... .......... .......... .......... 43% 24.5M 21s
221450K .......... .......... .......... .......... .......... 43% 20.1M 21s
221500K .......... .......... .......... .......... .......... 43% 17.3M 21s
221550K .......... .......... .......... .......... .......... 43% 15.8M 21s
221600K .......... .......... .......... .......... .......... 43% 16.0M 21s
221650K .......... .......... .......... .......... .......... 43% 15.7M 21s
221700K .......... .......... .......... .......... .......... 43% 9.23M 21s
221750K .......... .......... .......... .......... .......... 43% 10.6M 21s
221800K .......... .......... .......... .......... .......... 43% 11.2M 21s
221850K .......... .......... .......... .......... .......... 43% 10.1M 21s
221900K .......... .......... .......... .......... .......... 43% 10.3M 21s
221950K .......... .......... .......... .......... .......... 43% 6.95M 21s
222000K .......... .......... .......... .......... .......... 43% 7.32M 21s
222050K .......... .......... .......... .......... .......... 43% 8.40M 21s
222100K .......... .......... .......... .......... .......... 43% 10.2M 21s
222150K .......... .......... .......... .......... .......... 43% 11.1M 21s
222200K .......... .......... .......... .......... .......... 43% 11.5M 21s
222250K .......... .......... .......... .......... .......... 43% 11.3M 21s
222300K .......... .......... .......... .......... .......... 43% 10.6M 21s
222350K .......... .......... .......... .......... .......... 43% 10.4M 21s
222400K .......... .......... .......... .......... .......... 43% 13.8M 21s
222450K .......... .......... .......... .......... .......... 43% 12.0M 21s
222500K .......... .......... .......... .......... .......... 43% 11.1M 21s
222550K .......... .......... .......... .......... .......... 43% 9.94M 21s
222600K .......... .......... .......... .......... .......... 43% 8.15M 21s
222650K .......... .......... .......... .......... .......... 43% 7.20M 21s
222700K .......... .......... .......... .......... .......... 43% 6.09M 21s
222750K .......... .......... .......... .......... .......... 43% 8.31M 21s
222800K .......... .......... .......... .......... .......... 43% 6.78M 21s
222850K .......... .......... .......... .......... .......... 43% 5.36M 21s
222900K .......... .......... .......... .......... .......... 43% 7.96M 21s
222950K .......... .......... .......... .......... .......... 43% 12.4M 21s
223000K .......... .......... .......... .......... .......... 43% 10.8M 21s
223050K .......... .......... .......... .......... .......... 43% 14.6M 21s
223100K .......... .......... .......... .......... .......... 43% 8.89M 21s
223150K .......... .......... .......... .......... .......... 43% 11.2M 21s
223200K .......... .......... .......... .......... .......... 43% 8.49M 21s
223250K .......... .......... .......... .......... .......... 43% 14.8M 21s
223300K .......... .......... .......... .......... .......... 43% 8.46M 21s
223350K .......... .......... .......... .......... .......... 43% 8.15M 21s
223400K .......... .......... .......... .......... .......... 43% 6.14M 21s
223450K .......... .......... .......... .......... .......... 43% 8.42M 21s
223500K .......... .......... .......... .......... .......... 43% 8.90M 21s
223550K .......... .......... .......... .......... .......... 43% 7.18M 21s
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223650K .......... .......... .......... .......... .......... 43% 6.67M 21s
223700K .......... .......... .......... .......... .......... 43% 5.43M 21s
223750K .......... .......... .......... .......... .......... 43% 6.47M 21s
223800K .......... .......... .......... .......... .......... 43% 7.76M 21s
223850K .......... .......... .......... .......... .......... 43% 9.89M 21s
223900K .......... .......... .......... .......... .......... 43% 11.4M 21s
223950K .......... .......... .......... .......... .......... 43% 10.2M 21s
224000K .......... .......... .......... .......... .......... 43% 9.30M 21s
224050K .......... .......... .......... .......... .......... 43% 6.90M 21s
224100K .......... .......... .......... .......... .......... 43% 6.75M 21s
224150K .......... .......... .......... .......... .......... 43% 9.03M 21s
224200K .......... .......... .......... .......... .......... 43% 15.2M 21s
224250K .......... .......... .......... .......... .......... 43% 8.55M 21s
224300K .......... .......... .......... .......... .......... 44% 9.78M 21s
224350K .......... .......... .......... .......... .......... 44% 8.22M 21s
224400K .......... .......... .......... .......... .......... 44% 9.21M 21s
224450K .......... .......... .......... .......... .......... 44% 7.02M 21s
224500K .......... .......... .......... .......... .......... 44% 8.30M 21s
224550K .......... .......... .......... .......... .......... 44% 7.34M 21s
224600K .......... .......... .......... .......... .......... 44% 7.93M 21s
224650K .......... .......... .......... .......... .......... 44% 18.4M 21s
224700K .......... .......... .......... .......... .......... 44% 13.0M 21s
224750K .......... .......... .......... .......... .......... 44% 58.3M 21s
224800K .......... .......... .......... .......... .......... 44% 20.8M 21s
224850K .......... .......... .......... .......... .......... 44% 13.0M 21s
224900K .......... .......... .......... .......... .......... 44% 10.4M 21s
224950K .......... .......... .......... .......... .......... 44% 10.8M 21s
225000K .......... .......... .......... .......... .......... 44% 13.1M 21s
225050K .......... .......... .......... .......... .......... 44% 10.6M 21s
225100K .......... .......... .......... .......... .......... 44% 11.2M 21s
225150K .......... .......... .......... .......... .......... 44% 10.2M 21s
225200K .......... .......... .......... .......... .......... 44% 9.31M 21s
225250K .......... .......... .......... .......... .......... 44% 9.70M 21s
225300K .......... .......... .......... .......... .......... 44% 10.8M 21s
225350K .......... .......... .......... .......... .......... 44% 8.94M 21s
225400K .......... .......... .......... .......... .......... 44% 18.9M 21s
225450K .......... .......... .......... .......... .......... 44% 17.3M 21s
225500K .......... .......... .......... .......... .......... 44% 15.9M 21s
225550K .......... .......... .......... .......... .......... 44% 10.1M 21s
225600K .......... .......... .......... .......... .......... 44% 7.91M 21s
225650K .......... .......... .......... .......... .......... 44% 9.75M 21s
225700K .......... .......... .......... .......... .......... 44% 7.23M 21s
225750K .......... .......... .......... .......... .......... 44% 8.40M 21s
225800K .......... .......... .......... .......... .......... 44% 9.89M 21s
225850K .......... .......... .......... .......... .......... 44% 6.24M 21s
225900K .......... .......... .......... .......... .......... 44% 8.49M 21s
225950K .......... .......... .......... .......... .......... 44% 5.75M 21s
226000K .......... .......... .......... .......... .......... 44% 17.1M 21s
226050K .......... .......... .......... .......... .......... 44% 26.1M 21s
226100K .......... .......... .......... .......... .......... 44% 31.6M 21s
226150K .......... .......... .......... .......... .......... 44% 12.6M 21s
226200K .......... .......... .......... .......... .......... 44% 73.3M 21s
226250K .......... .......... .......... .......... .......... 44% 86.1M 21s
226300K .......... .......... .......... .......... .......... 44% 63.6M 21s
226350K .......... .......... .......... .......... .......... 44% 62.0M 21s
226400K .......... .......... .......... .......... .......... 44% 23.5M 21s
226450K .......... .......... .......... .......... .......... 44% 14.0M 21s
226500K .......... .......... .......... .......... .......... 44% 19.1M 21s
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226650K .......... .......... .......... .......... .......... 44% 13.9M 21s
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227000K .......... .......... .......... .......... .......... 44% 5.69M 21s
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227100K .......... .......... .......... .......... .......... 44% 7.90M 21s
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227650K .......... .......... .......... .......... .......... 44% 16.6M 21s
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227800K .......... .......... .......... .......... .......... 44% 31.0M 21s
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228000K .......... .......... .......... .......... .......... 44% 17.2M 21s
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228100K .......... .......... .......... .......... .......... 44% 12.6M 21s
228150K .......... .......... .......... .......... .......... 44% 18.9M 21s
228200K .......... .......... .......... .......... .......... 44% 14.6M 21s
228250K .......... .......... .......... .......... .......... 44% 14.0M 21s
228300K .......... .......... .......... .......... .......... 44% 14.6M 21s
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228400K .......... .......... .......... .......... .......... 44% 16.7M 21s
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228600K .......... .......... .......... .......... .......... 44% 9.24M 21s
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228700K .......... .......... .......... .......... .......... 44% 11.5M 21s
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228800K .......... .......... .......... .......... .......... 44% 11.9M 21s
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228900K .......... .......... .......... .......... .......... 44% 16.2M 21s
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229000K .......... .......... .......... .......... .......... 44% 9.85M 21s
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229100K .......... .......... .......... .......... .......... 44% 10.7M 21s
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229200K .......... .......... .......... .......... .......... 44% 8.58M 21s
229250K .......... .......... .......... .......... .......... 44% 9.68M 21s
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229500K .......... .......... .......... .......... .......... 45% 12.1M 21s
229550K .......... .......... .......... .......... .......... 45% 6.55M 21s
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229650K .......... .......... .......... .......... .......... 45% 5.02M 21s
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230000K .......... .......... .......... .......... .......... 45% 11.0M 21s
230050K .......... .......... .......... .......... .......... 45% 11.7M 21s
230100K .......... .......... .......... .......... .......... 45% 8.19M 21s
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230200K .......... .......... .......... .......... .......... 45% 10.5M 21s
230250K .......... .......... .......... .......... .......... 45% 10.4M 21s
230300K .......... .......... .......... .......... .......... 45% 11.5M 21s
230350K .......... .......... .......... .......... .......... 45% 11.3M 21s
230400K .......... .......... .......... .......... .......... 45% 11.6M 21s
230450K .......... .......... .......... .......... .......... 45% 8.29M 21s
230500K .......... .......... .......... .......... .......... 45% 12.7M 21s
230550K .......... .......... .......... .......... .......... 45% 12.3M 21s
230600K .......... .......... .......... .......... .......... 45% 12.8M 21s
230650K .......... .......... .......... .......... .......... 45% 11.5M 21s
230700K .......... .......... .......... .......... .......... 45% 7.81M 21s
230750K .......... .......... .......... .......... .......... 45% 8.11M 21s
230800K .......... .......... .......... .......... .......... 45% 7.73M 21s
230850K .......... .......... .......... .......... .......... 45% 5.99M 21s
230900K .......... .......... .......... .......... .......... 45% 7.10M 21s
230950K .......... .......... .......... .......... .......... 45% 5.70M 21s
231000K .......... .......... .......... .......... .......... 45% 6.24M 21s
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231100K .......... .......... .......... .......... .......... 45% 6.23M 21s
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231200K .......... .......... .......... .......... .......... 45% 4.85M 21s
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231300K .......... .......... .......... .......... .......... 45% 8.16M 21s
231350K .......... .......... .......... .......... .......... 45% 6.89M 21s
231400K .......... .......... .......... .......... .......... 45% 7.06M 21s
231450K .......... .......... .......... .......... .......... 45% 6.12M 21s
231500K .......... .......... .......... .......... .......... 45% 6.48M 21s
231550K .......... .......... .......... .......... .......... 45% 7.30M 21s
231600K .......... .......... .......... .......... .......... 45% 5.01M 21s
231650K .......... .......... .......... .......... .......... 45% 6.08M 21s
231700K .......... .......... .......... .......... .......... 45% 14.9M 21s
231750K .......... .......... .......... .......... .......... 45% 11.4M 21s
231800K .......... .......... .......... .......... .......... 45% 10.2M 21s
231850K .......... .......... .......... .......... .......... 45% 7.73M 21s
231900K .......... .......... .......... .......... .......... 45% 11.4M 21s
231950K .......... .......... .......... .......... .......... 45% 9.48M 21s
232000K .......... .......... .......... .......... .......... 45% 12.3M 21s
232050K .......... .......... .......... .......... .......... 45% 9.55M 21s
232100K .......... .......... .......... .......... .......... 45% 7.70M 21s
232150K .......... .......... .......... .......... .......... 45% 10.7M 21s
232200K .......... .......... .......... .......... .......... 45% 8.35M 21s
232250K .......... .......... .......... .......... .......... 45% 7.64M 21s
232300K .......... .......... .......... .......... .......... 45% 8.63M 21s
232350K .......... .......... .......... .......... .......... 45% 7.15M 21s
232400K .......... .......... .......... .......... .......... 45% 12.1M 21s
232450K .......... .......... .......... .......... .......... 45% 9.26M 21s
232500K .......... .......... .......... .......... .......... 45% 10.9M 21s
232550K .......... .......... .......... .......... .......... 45% 9.95M 21s
232600K .......... .......... .......... .......... .......... 45% 6.75M 21s
232650K .......... .......... .......... .......... .......... 45% 11.8M 21s
232700K .......... .......... .......... .......... .......... 45% 6.76M 21s
232750K .......... .......... .......... .......... .......... 45% 9.46M 21s
232800K .......... .......... .......... .......... .......... 45% 7.93M 21s
232850K .......... .......... .......... .......... .......... 45% 6.11M 21s
232900K .......... .......... .......... .......... .......... 45% 8.67M 21s
232950K .......... .......... .......... .......... .......... 45% 6.32M 21s
233000K .......... .......... .......... .......... .......... 45% 9.47M 21s
233050K .......... .......... .......... .......... .......... 45% 15.8M 21s
233100K .......... .......... .......... .......... .......... 45% 28.5M 20s
233150K .......... .......... .......... .......... .......... 45% 19.5M 20s
233200K .......... .......... .......... .......... .......... 45% 18.7M 20s
233250K .......... .......... .......... .......... .......... 45% 30.6M 20s
233300K .......... .......... .......... .......... .......... 45% 19.2M 20s
233350K .......... .......... .......... .......... .......... 45% 14.0M 20s
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275250K .......... .......... .......... .......... .......... 54% 36.4M 18s
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275700K .......... .......... .......... .......... .......... 54% 12.6M 18s
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289100K .......... .......... .......... .......... .......... 56% 15.8M 17s
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318200K .......... .......... .......... .......... .......... 62% 7.30M 15s
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318300K .......... .......... .......... .......... .......... 62% 9.84M 15s
318350K .......... .......... .......... .......... .......... 62% 18.4M 15s
318400K .......... .......... .......... .......... .......... 62% 33.3M 15s
318450K .......... .......... .......... .......... .......... 62% 17.5M 15s
318500K .......... .......... .......... .......... .......... 62% 13.5M 15s
318550K .......... .......... .......... .......... .......... 62% 61.0M 15s
318600K .......... .......... .......... .......... .......... 62% 13.9M 15s
318650K .......... .......... .......... .......... .......... 62% 24.1M 15s
318700K .......... .......... .......... .......... .......... 62% 9.60M 15s
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318800K .......... .......... .......... .......... .......... 62% 13.6M 15s
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318900K .......... .......... .......... .......... .......... 62% 15.9M 15s
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319000K .......... .......... .......... .......... .......... 62% 13.2M 15s
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319100K .......... .......... .......... .......... .......... 62% 9.66M 15s
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319200K .......... .......... .......... .......... .......... 62% 11.9M 15s
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319300K .......... .......... .......... .......... .......... 62% 30.7M 15s
319350K .......... .......... .......... .......... .......... 62% 30.3M 15s
319400K .......... .......... .......... .......... .......... 62% 28.8M 15s
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319600K .......... .......... .......... .......... .......... 62% 21.2M 15s
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319700K .......... .......... .......... .......... .......... 62% 13.9M 15s
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319800K .......... .......... .......... .......... .......... 62% 40.8M 15s
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321500K .......... .......... .......... .......... .......... 63% 18.0M 15s
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322000K .......... .......... .......... .......... .......... 63% 12.7M 15s
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323000K .......... .......... .......... .......... .......... 63% 24.0M 15s
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323100K .......... .......... .......... .......... .......... 63% 10.2M 15s
323150K .......... .......... .......... .......... .......... 63% 60.7M 15s
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323250K .......... .......... .......... .......... .......... 63% 15.1M 15s
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332200K .......... .......... .......... .......... .......... 65% 24.5M 14s
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332300K .......... .......... .......... .......... .......... 65% 43.3M 14s
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332400K .......... .......... .......... .......... .......... 65% 62.5M 14s
332450K .......... .......... .......... .......... .......... 65% 20.6M 14s
332500K .......... .......... .......... .......... .......... 65% 25.4M 14s
332550K .......... .......... .......... .......... .......... 65% 21.1M 14s
332600K .......... .......... .......... .......... .......... 65% 12.6M 14s
332650K .......... .......... .......... .......... .......... 65% 17.9M 14s
332700K .......... .......... .......... .......... .......... 65% 13.9M 14s
332750K .......... .......... .......... .......... .......... 65% 11.5M 14s
332800K .......... .......... .......... .......... .......... 65% 16.3M 14s
332850K .......... .......... .......... .......... .......... 65% 13.0M 14s
332900K .......... .......... .......... .......... .......... 65% 10.2M 14s
332950K .......... .......... .......... .......... .......... 65% 14.0M 14s
333000K .......... .......... .......... .......... .......... 65% 14.5M 14s
333050K .......... .......... .......... .......... .......... 65% 14.0M 14s
333100K .......... .......... .......... .......... .......... 65% 14.0M 14s
333150K .......... .......... .......... .......... .......... 65% 13.9M 14s
333200K .......... .......... .......... .......... .......... 65% 11.5M 14s
333250K .......... .......... .......... .......... .......... 65% 14.1M 14s
333300K .......... .......... .......... .......... .......... 65% 9.65M 14s
333350K .......... .......... .......... .......... .......... 65% 13.4M 14s
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333550K .......... .......... .......... .......... .......... 65% 17.1M 14s
333600K .......... .......... .......... .......... .......... 65% 13.5M 14s
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333700K .......... .......... .......... .......... .......... 65% 10.7M 14s
333750K .......... .......... .......... .......... .......... 65% 15.7M 14s
333800K .......... .......... .......... .......... .......... 65% 17.1M 14s
333850K .......... .......... .......... .......... .......... 65% 32.1M 14s
333900K .......... .......... .......... .......... .......... 65% 41.6M 14s
333950K .......... .......... .......... .......... .......... 65% 11.9M 14s
334000K .......... .......... .......... .......... .......... 65% 63.7M 14s
334050K .......... .......... .......... .......... .......... 65%  102M 14s
334100K .......... .......... .......... .......... .......... 65% 83.6M 14s
334150K .......... .......... .......... .......... .......... 65% 40.0M 14s
334200K .......... .......... .......... .......... .......... 65% 24.5M 14s
334250K .......... .......... .......... .......... .......... 65% 29.2M 14s
334300K .......... .......... .......... .......... .......... 65% 30.9M 14s
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334400K .......... .......... .......... .......... .......... 65% 23.4M 14s
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334500K .......... .......... .......... .......... .......... 65% 20.9M 14s
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334650K .......... .......... .......... .......... .......... 65% 21.9M 14s
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334800K .......... .......... .......... .......... .......... 65% 21.4M 14s
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334900K .......... .......... .......... .......... .......... 65% 15.7M 14s
334950K .......... .......... .......... .......... .......... 65% 9.06M 14s
335000K .......... .......... .......... .......... .......... 65% 20.2M 14s
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335100K .......... .......... .......... .......... .......... 65% 67.7M 14s
335150K .......... .......... .......... .......... .......... 65% 79.7M 14s
335200K .......... .......... .......... .......... .......... 65% 45.8M 14s
335250K .......... .......... .......... .......... .......... 65% 24.4M 14s
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335400K .......... .......... .......... .......... .......... 65% 14.6M 14s
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335500K .......... .......... .......... .......... .......... 65% 12.7M 14s
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335700K .......... .......... .......... .......... .......... 65% 10.7M 14s
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335900K .......... .......... .......... .......... .......... 65% 15.1M 14s
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336000K .......... .......... .......... .......... .......... 65% 13.1M 14s
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336100K .......... .......... .......... .......... .......... 65% 13.7M 14s
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336250K .......... .......... .......... .......... .......... 65% 10.1M 14s
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336450K .......... .......... .......... .......... .......... 66% 16.5M 14s
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336550K .......... .......... .......... .......... .......... 66% 12.5M 14s
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336650K .......... .......... .......... .......... .......... 66% 10.8M 14s
336700K .......... .......... .......... .......... .......... 66% 11.1M 14s
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336900K .......... .......... .......... .......... .......... 66% 7.07M 14s
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337000K .......... .......... .......... .......... .......... 66% 11.6M 14s
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337100K .......... .......... .......... .......... .......... 66% 15.0M 14s
337150K .......... .......... .......... .......... .......... 66% 9.29M 14s
337200K .......... .......... .......... .......... .......... 66% 13.1M 14s
337250K .......... .......... .......... .......... .......... 66% 9.76M 14s
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337350K .......... .......... .......... .......... .......... 66% 7.60M 14s
337400K .......... .......... .......... .......... .......... 66% 10.4M 14s
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337500K .......... .......... .......... .......... .......... 66% 9.89M 14s
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337700K .......... .......... .......... .......... .......... 66% 8.51M 13s
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337900K .......... .......... .......... .......... .......... 66% 31.6M 13s
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338000K .......... .......... .......... .......... .......... 66% 13.5M 13s
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338100K .......... .......... .......... .......... .......... 66% 12.6M 13s
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339250K .......... .......... .......... .......... .......... 66% 12.8M 13s
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341000K .......... .......... .......... .......... .......... 66% 14.6M 13s
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341400K .......... .......... .......... .......... .......... 66% 31.0M 13s
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341500K .......... .......... .......... .......... .......... 66% 25.5M 13s
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341600K .......... .......... .......... .......... .......... 67% 18.7M 13s
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341700K .......... .......... .......... .......... .......... 67% 14.9M 13s
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341800K .......... .......... .......... .......... .......... 67% 19.8M 13s
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342000K .......... .......... .......... .......... .......... 67% 14.1M 13s
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342150K .......... .......... .......... .......... .......... 67% 19.0M 13s
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342250K .......... .......... .......... .......... .......... 67% 11.9M 13s
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342400K .......... .......... .......... .......... .......... 67% 31.0M 13s
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342500K .......... .......... .......... .......... .......... 67% 15.1M 13s
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342900K .......... .......... .......... .......... .......... 67% 16.8M 13s
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343000K .......... .......... .......... .......... .......... 67% 18.7M 13s
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343100K .......... .......... .......... .......... .......... 67% 13.1M 13s
343150K .......... .......... .......... .......... .......... 67% 14.6M 13s
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343250K .......... .......... .......... .......... .......... 67% 17.3M 13s
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343400K .......... .......... .......... .......... .......... 67% 14.3M 13s
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343500K .......... .......... .......... .......... .......... 67% 13.9M 13s
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343600K .......... .......... .......... .......... .......... 67% 10.1M 13s
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343700K .......... .......... .......... .......... .......... 67% 9.49M 13s
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343800K .......... .......... .......... .......... .......... 67% 17.2M 13s
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343900K .......... .......... .......... .......... .......... 67% 14.4M 13s
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344000K .......... .......... .......... .......... .......... 67% 14.5M 13s
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344100K .......... .......... .......... .......... .......... 67% 11.8M 13s
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344250K .......... .......... .......... .......... .......... 67% 10.8M 13s
344300K .......... .......... .......... .......... .......... 67% 19.0M 13s
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344500K .......... .......... .......... .......... .......... 67% 33.7M 13s
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344600K .......... .......... .......... .......... .......... 67% 29.5M 13s
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344700K .......... .......... .......... .......... .......... 67% 16.7M 13s
344750K .......... .......... .......... .......... .......... 67% 74.8M 13s
344800K .......... .......... .......... .......... .......... 67% 15.7M 13s
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344900K .......... .......... .......... .......... .......... 67% 25.2M 13s
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345000K .......... .......... .......... .......... .......... 67% 29.2M 13s
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345100K .......... .......... .......... .......... .......... 67% 21.8M 13s
345150K .......... .......... .......... .......... .......... 67% 32.4M 13s
345200K .......... .......... .......... .......... .......... 67% 17.8M 13s
345250K .......... .......... .......... .......... .......... 67% 33.9M 13s
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345400K .......... .......... .......... .......... .......... 67% 31.3M 13s
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345500K .......... .......... .......... .......... .......... 67% 27.4M 13s
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345600K .......... .......... .......... .......... .......... 67% 15.8M 13s
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345700K .......... .......... .......... .......... .......... 67% 13.2M 13s
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345800K .......... .......... .......... .......... .......... 67% 15.6M 13s
345850K .......... .......... .......... .......... .......... 67% 9.59M 13s
345900K .......... .......... .......... .......... .......... 67% 17.0M 13s
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346000K .......... .......... .......... .......... .......... 67% 17.0M 13s
346050K .......... .......... .......... .......... .......... 67% 11.8M 13s
346100K .......... .......... .......... .......... .......... 67% 11.1M 13s
346150K .......... .......... .......... .......... .......... 67% 9.96M 13s
346200K .......... .......... .......... .......... .......... 67% 10.2M 13s
346250K .......... .......... .......... .......... .......... 67% 17.7M 13s
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346350K .......... .......... .......... .......... .......... 67% 8.37M 13s
346400K .......... .......... .......... .......... .......... 67% 9.09M 13s
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346500K .......... .......... .......... .......... .......... 67% 13.0M 13s
346550K .......... .......... .......... .......... .......... 67% 10.0M 13s
346600K .......... .......... .......... .......... .......... 67% 7.33M 13s
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360000K .......... .......... .......... .......... .......... 70% 24.3M 11s
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360300K .......... .......... .......... .......... .......... 70% 22.9M 11s
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360500K .......... .......... .......... .......... .......... 70% 22.9M 11s
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360650K .......... .......... .......... .......... .......... 70% 37.4M 11s
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360750K .......... .......... .......... .......... .......... 70% 27.7M 11s
360800K .......... .......... .......... .......... .......... 70% 35.5M 11s
360850K .......... .......... .......... .......... .......... 70% 12.1M 11s
360900K .......... .......... .......... .......... .......... 70% 21.5M 11s
360950K .......... .......... .......... .......... .......... 70%  102M 11s
361000K .......... .......... .......... .......... .......... 70% 35.0M 11s
361050K .......... .......... .......... .......... .......... 70% 25.9M 11s
361100K .......... .......... .......... .......... .......... 70% 86.1M 11s
361150K .......... .......... .......... .......... .......... 70% 27.0M 11s
361200K .......... .......... .......... .......... .......... 70% 14.3M 11s
361250K .......... .......... .......... .......... .......... 70% 46.0M 11s
361300K .......... .......... .......... .......... .......... 70% 27.6M 11s
361350K .......... .......... .......... .......... .......... 70% 20.9M 11s
361400K .......... .......... .......... .......... .......... 70% 35.2M 11s
361450K .......... .......... .......... .......... .......... 70% 19.6M 11s
361500K .......... .......... .......... .......... .......... 70% 29.3M 11s
361550K .......... .......... .......... .......... .......... 70% 19.7M 11s
361600K .......... .......... .......... .......... .......... 70% 22.3M 11s
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361700K .......... .......... .......... .......... .......... 70% 20.3M 11s
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361800K .......... .......... .......... .......... .......... 70% 18.1M 11s
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361900K .......... .......... .......... .......... .......... 70% 22.1M 11s
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362000K .......... .......... .......... .......... .......... 71% 20.0M 11s
362050K .......... .......... .......... .......... .......... 71% 29.2M 11s
362100K .......... .......... .......... .......... .......... 71% 12.3M 11s
362150K .......... .......... .......... .......... .......... 71% 26.8M 11s
362200K .......... .......... .......... .......... .......... 71% 78.0M 11s
362250K .......... .......... .......... .......... .......... 71% 15.0M 11s
362300K .......... .......... .......... .......... .......... 71% 89.8M 11s
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362400K .......... .......... .......... .......... .......... 71% 79.3M 11s
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362500K .......... .......... .......... .......... .......... 71% 27.4M 11s
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362800K .......... .......... .......... .......... .......... 71% 34.1M 11s
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363000K .......... .......... .......... .......... .......... 71% 22.1M 11s
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363250K .......... .......... .......... .......... .......... 71% 23.8M 11s
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363850K .......... .......... .......... .......... .......... 71% 30.8M 11s
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364000K .......... .......... .......... .......... .......... 71% 26.9M 11s
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365000K .......... .......... .......... .......... .......... 71% 18.2M 11s
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365100K .......... .......... .......... .......... .......... 71% 27.2M 11s
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365250K .......... .......... .......... .......... .......... 71% 21.1M 11s
365300K .......... .......... .......... .......... .......... 71% 18.8M 11s
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365600K .......... .......... .......... .......... .......... 71% 18.9M 11s
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365700K .......... .......... .......... .......... .......... 71% 14.9M 11s
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365900K .......... .......... .......... .......... .......... 71% 24.9M 11s
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366000K .......... .......... .......... .......... .......... 71% 11.7M 11s
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366100K .......... .......... .......... .......... .......... 71% 76.3M 11s
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366250K .......... .......... .......... .......... .......... 71% 48.3M 11s
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367250K .......... .......... .......... .......... .......... 72% 60.1M 11s
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367500K .......... .......... .......... .......... .......... 72% 94.6M 11s
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368000K .......... .......... .......... .......... .......... 72% 26.8M 11s
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368100K .......... .......... .......... .......... .......... 72% 31.2M 11s
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368250K .......... .......... .......... .......... .......... 72% 37.6M 11s
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369000K .......... .......... .......... .......... .......... 72% 25.1M 11s
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369100K .......... .......... .......... .......... .......... 72% 19.2M 11s
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370000K .......... .......... .......... .......... .......... 72% 18.4M 11s
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370500K .......... .......... .......... .......... .......... 72% 19.6M 10s
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371000K .......... .......... .......... .......... .......... 72% 21.9M 10s
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371100K .......... .......... .......... .......... .......... 72% 17.7M 10s
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371400K .......... .......... .......... .......... .......... 72% 94.1M 10s
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371500K .......... .......... .......... .......... .......... 72% 28.1M 10s
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371600K .......... .......... .......... .......... .......... 72% 27.8M 10s
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371900K .......... .......... .......... .......... .......... 72% 38.9M 10s
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372000K .......... .......... .......... .......... .......... 72% 37.6M 10s
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372150K .......... .......... .......... .......... .......... 73% 22.8M 10s
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372250K .......... .......... .......... .......... .......... 73% 25.1M 10s
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372500K .......... .......... .......... .......... .......... 73%  102M 10s
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372800K .......... .......... .......... .......... .......... 73% 67.2M 10s
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373000K .......... .......... .......... .......... .......... 73% 26.9M 10s
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373100K .......... .......... .......... .......... .......... 73% 22.1M 10s
373150K .......... .......... .......... .......... .......... 73% 25.6M 10s
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373250K .......... .......... .......... .......... .......... 73% 25.2M 10s
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374000K .......... .......... .......... .......... .......... 73% 37.0M 10s
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374100K .......... .......... .......... .......... .......... 73% 33.8M 10s
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374250K .......... .......... .......... .......... .......... 73% 31.7M 10s
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374950K .......... .......... .......... .......... .......... 73% 31.4M 10s
375000K .......... .......... .......... .......... .......... 73% 21.1M 10s
375050K .......... .......... .......... .......... .......... 73% 91.6M 10s
375100K .......... .......... .......... .......... .......... 73% 19.6M 10s
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375200K .......... .......... .......... .......... .......... 73% 22.7M 10s
375250K .......... .......... .......... .......... .......... 73% 75.0M 10s
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389100K .......... .......... .......... .......... .......... 76% 28.2M 9s
389150K .......... .......... .......... .......... .......... 76% 32.1M 9s
389200K .......... .......... .......... .......... .......... 76% 69.0M 9s
389250K .......... .......... .......... .......... .......... 76% 34.3M 9s
389300K .......... .......... .......... .......... .......... 76% 35.8M 9s
389350K .......... .......... .......... .......... .......... 76% 62.3M 9s
389400K .......... .......... .......... .......... .......... 76% 25.4M 9s
389450K .......... .......... .......... .......... .......... 76% 33.6M 9s
389500K .......... .......... .......... .......... .......... 76% 72.8M 9s
389550K .......... .......... .......... .......... .......... 76% 39.1M 9s
389600K .......... .......... .......... .......... .......... 76% 52.8M 9s
389650K .......... .......... .......... .......... .......... 76% 46.3M 9s
389700K .......... .......... .......... .......... .......... 76% 37.3M 9s
389750K .......... .......... .......... .......... .......... 76% 46.3M 9s
389800K .......... .......... .......... .......... .......... 76% 74.9M 9s
389850K .......... .......... .......... .......... .......... 76% 37.5M 9s
389900K .......... .......... .......... .......... .......... 76% 61.5M 9s
389950K .......... .......... .......... .......... .......... 76% 46.0M 9s
390000K .......... .......... .......... .......... .......... 76% 19.2M 9s
390050K .......... .......... .......... .......... .......... 76% 79.7M 9s
390100K .......... .......... .......... .......... .......... 76%  101M 9s
390150K .......... .......... .......... .......... .......... 76% 99.6M 9s
390200K .......... .......... .......... .......... .......... 76% 51.2M 9s
390250K .......... .......... .......... .......... .......... 76% 38.3M 9s
390300K .......... .......... .......... .......... .......... 76% 42.0M 9s
390350K .......... .......... .......... .......... .......... 76% 31.7M 9s
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390450K .......... .......... .......... .......... .......... 76% 29.1M 9s
390500K .......... .......... .......... .......... .......... 76% 37.4M 9s
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390600K .......... .......... .......... .......... .......... 76% 36.8M 9s
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390700K .......... .......... .......... .......... .......... 76% 22.7M 9s
390750K .......... .......... .......... .......... .......... 76% 45.0M 9s
390800K .......... .......... .......... .......... .......... 76% 39.7M 9s
390850K .......... .......... .......... .......... .......... 76% 22.2M 9s
390900K .......... .......... .......... .......... .......... 76% 39.4M 9s
390950K .......... .......... .......... .......... .......... 76% 25.7M 9s
391000K .......... .......... .......... .......... .......... 76% 38.9M 9s
391050K .......... .......... .......... .......... .......... 76% 41.6M 9s
391100K .......... .......... .......... .......... .......... 76% 25.2M 9s
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391200K .......... .......... .......... .......... .......... 76% 34.1M 9s
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391350K .......... .......... .......... .......... .......... 76% 31.3M 9s
391400K .......... .......... .......... .......... .......... 76%  144M 9s
391450K .......... .......... .......... .......... .......... 76% 27.1M 9s
391500K .......... .......... .......... .......... .......... 76% 13.0M 9s
391550K .......... .......... .......... .......... .......... 76%  148M 9s
391600K .......... .......... .......... .......... .......... 76% 35.9M 9s
391650K .......... .......... .......... .......... .......... 76%  113M 9s
391700K .......... .......... .......... .......... .......... 76% 47.6M 9s
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391800K .......... .......... .......... .......... .......... 76% 40.6M 9s
391850K .......... .......... .......... .......... .......... 76% 57.2M 9s
391900K .......... .......... .......... .......... .......... 76% 40.3M 9s
391950K .......... .......... .......... .......... .......... 76% 24.1M 9s
392000K .......... .......... .......... .......... .......... 76% 32.0M 9s
392050K .......... .......... .......... .......... .......... 76% 26.9M 9s
392100K .......... .......... .......... .......... .......... 76% 34.0M 9s
392150K .......... .......... .......... .......... .......... 76% 21.9M 9s
392200K .......... .......... .......... .......... .......... 76% 22.7M 9s
392250K .......... .......... .......... .......... .......... 76% 21.7M 9s
392300K .......... .......... .......... .......... .......... 76% 37.0M 9s
392350K .......... .......... .......... .......... .......... 76% 21.2M 9s
392400K .......... .......... .......... .......... .......... 76% 26.8M 9s
392450K .......... .......... .......... .......... .......... 76% 19.3M 9s
392500K .......... .......... .......... .......... .......... 77% 23.0M 9s
392550K .......... .......... .......... .......... .......... 77% 33.8M 9s
392600K .......... .......... .......... .......... .......... 77% 20.3M 9s
392650K .......... .......... .......... .......... .......... 77% 21.6M 9s
392700K .......... .......... .......... .......... .......... 77% 18.2M 9s
392750K .......... .......... .......... .......... .......... 77% 29.4M 9s
392800K .......... .......... .......... .......... .......... 77% 41.3M 9s
392850K .......... .......... .......... .......... .......... 77% 27.2M 9s
392900K .......... .......... .......... .......... .......... 77% 37.8M 9s
392950K .......... .......... .......... .......... .......... 77% 36.2M 9s
393000K .......... .......... .......... .......... .......... 77% 15.5M 9s
393050K .......... .......... .......... .......... .......... 77% 16.0M 9s
393100K .......... .......... .......... .......... .......... 77%  107M 9s
393150K .......... .......... .......... .......... .......... 77%  118M 9s
393200K .......... .......... .......... .......... .......... 77% 39.3M 9s
393250K .......... .......... .......... .......... .......... 77% 61.7M 9s
393300K .......... .......... .......... .......... .......... 77% 87.7M 9s
393350K .......... .......... .......... .......... .......... 77% 21.3M 9s
393400K .......... .......... .......... .......... .......... 77%  108M 9s
393450K .......... .......... .......... .......... .......... 77% 29.5M 9s
393500K .......... .......... .......... .......... .......... 77% 37.6M 9s
393550K .......... .......... .......... .......... .......... 77% 31.2M 8s
393600K .......... .......... .......... .......... .......... 77% 26.8M 8s
393650K .......... .......... .......... .......... .......... 77% 5.79M 8s
393700K .......... .......... .......... .......... .......... 77% 18.9M 8s
393750K .......... .......... .......... .......... .......... 77% 47.5M 8s
393800K .......... .......... .......... .......... .......... 77% 32.4M 8s
393850K .......... .......... .......... .......... .......... 77% 31.3M 8s
393900K .......... .......... .......... .......... .......... 77% 28.3M 8s
393950K .......... .......... .......... .......... .......... 77% 41.1M 8s
394000K .......... .......... .......... .......... .......... 77% 24.0M 8s
394050K .......... .......... .......... .......... .......... 77% 27.0M 8s
394100K .......... .......... .......... .......... .......... 77% 34.3M 8s
394150K .......... .......... .......... .......... .......... 77% 22.1M 8s
394200K .......... .......... .......... .......... .......... 77% 31.6M 8s
394250K .......... .......... .......... .......... .......... 77% 29.6M 8s
394300K .......... .......... .......... .......... .......... 77%  101M 8s
394350K .......... .......... .......... .......... .......... 77% 11.6M 8s
394400K .......... .......... .......... .......... .......... 77% 51.8M 8s
394450K .......... .......... .......... .......... .......... 77%  144M 8s
394500K .......... .......... .......... .......... .......... 77% 26.7M 8s
394550K .......... .......... .......... .......... .......... 77%  176M 8s
394600K .......... .......... .......... .......... .......... 77% 22.8M 8s
394650K .......... .......... .......... .......... .......... 77%  166M 8s
394700K .......... .......... .......... .......... .......... 77% 61.9M 8s
394750K .......... .......... .......... .......... .......... 77% 53.5M 8s
394800K .......... .......... .......... .......... .......... 77% 40.4M 8s
394850K .......... .......... .......... .......... .......... 77% 49.2M 8s
394900K .......... .......... .......... .......... .......... 77% 31.3M 8s
394950K .......... .......... .......... .......... .......... 77% 34.2M 8s
395000K .......... .......... .......... .......... .......... 77% 31.2M 8s
395050K .......... .......... .......... .......... .......... 77% 44.9M 8s
395100K .......... .......... .......... .......... .......... 77% 27.5M 8s
395150K .......... .......... .......... .......... .......... 77% 31.7M 8s
395200K .......... .......... .......... .......... .......... 77% 41.9M 8s
395250K .......... .......... .......... .......... .......... 77% 26.5M 8s
395300K .......... .......... .......... .......... .......... 77% 41.5M 8s
395350K .......... .......... .......... .......... .......... 77% 25.4M 8s
395400K .......... .......... .......... .......... .......... 77% 37.0M 8s
395450K .......... .......... .......... .......... .......... 77% 28.9M 8s
395500K .......... .......... .......... .......... .......... 77% 41.7M 8s
395550K .......... .......... .......... .......... .......... 77% 34.3M 8s
395600K .......... .......... .......... .......... .......... 77% 34.4M 8s
395650K .......... .......... .......... .......... .......... 77% 31.3M 8s
395700K .......... .......... .......... .......... .......... 77% 38.5M 8s
395750K .......... .......... .......... .......... .......... 77% 26.3M 8s
395800K .......... .......... .......... .......... .......... 77% 37.0M 8s
395850K .......... .......... .......... .......... .......... 77% 29.0M 8s
395900K .......... .......... .......... .......... .......... 77% 41.5M 8s
395950K .......... .......... .......... .......... .......... 77% 34.2M 8s
396000K .......... .......... .......... .......... .......... 77% 15.9M 8s
396050K .......... .......... .......... .......... .......... 77% 22.6M 8s
396100K .......... .......... .......... .......... .......... 77% 11.7M 8s
396150K .......... .......... .......... .......... .......... 77%  152M 8s
396200K .......... .......... .......... .......... .......... 77% 25.0M 8s
396250K .......... .......... .......... .......... .......... 77% 52.9M 8s
396300K .......... .......... .......... .......... .......... 77% 96.9M 8s
396350K .......... .......... .......... .......... .......... 77% 28.8M 8s
396400K .......... .......... .......... .......... .......... 77% 35.5M 8s
396450K .......... .......... .......... .......... .......... 77% 39.3M 8s
396500K .......... .......... .......... .......... .......... 77% 27.1M 8s
396550K .......... .......... .......... .......... .......... 77% 38.8M 8s
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396650K .......... .......... .......... .......... .......... 77% 38.7M 8s
396700K .......... .......... .......... .......... .......... 77% 23.2M 8s
396750K .......... .......... .......... .......... .......... 77% 52.5M 8s
396800K .......... .......... .......... .......... .......... 77% 26.2M 8s
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396900K .......... .......... .......... .......... .......... 77% 29.3M 8s
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397000K .......... .......... .......... .......... .......... 77% 31.2M 8s
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397100K .......... .......... .......... .......... .......... 77% 26.8M 8s
397150K .......... .......... .......... .......... .......... 77% 38.2M 8s
397200K .......... .......... .......... .......... .......... 77% 28.5M 8s
397250K .......... .......... .......... .......... .......... 77% 28.4M 8s
397300K .......... .......... .......... .......... .......... 77% 35.9M 8s
397350K .......... .......... .......... .......... .......... 77% 22.8M 8s
397400K .......... .......... .......... .......... .......... 77% 27.7M 8s
397450K .......... .......... .......... .......... .......... 77% 26.0M 8s
397500K .......... .......... .......... .......... .......... 77%  152M 8s
397550K .......... .......... .......... .......... .......... 77% 7.94M 8s
397600K .......... .......... .......... .......... .......... 78%  132M 8s
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397800K .......... .......... .......... .......... .......... 78% 24.9M 8s
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397900K .......... .......... .......... .......... .......... 78% 29.0M 8s
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398000K .......... .......... .......... .......... .......... 78% 22.2M 8s
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398100K .......... .......... .......... .......... .......... 78% 16.0M 8s
398150K .......... .......... .......... .......... .......... 78% 22.2M 8s
398200K .......... .......... .......... .......... .......... 78% 14.3M 8s
398250K .......... .......... .......... .......... .......... 78% 25.7M 8s
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398400K .......... .......... .......... .......... .......... 78% 21.9M 8s
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398500K .......... .......... .......... .......... .......... 78% 15.9M 8s
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398600K .......... .......... .......... .......... .......... 78% 14.2M 8s
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398700K .......... .......... .......... .......... .......... 78% 11.0M 8s
398750K .......... .......... .......... .......... .......... 78% 76.1M 8s
398800K .......... .......... .......... .......... .......... 78% 30.3M 8s
398850K .......... .......... .......... .......... .......... 78% 30.1M 8s
398900K .......... .......... .......... .......... .......... 78% 21.9M 8s
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399000K .......... .......... .......... .......... .......... 78% 26.6M 8s
399050K .......... .......... .......... .......... .......... 78% 18.8M 8s
399100K .......... .......... .......... .......... .......... 78% 16.8M 8s
399150K .......... .......... .......... .......... .......... 78% 15.2M 8s
399200K .......... .......... .......... .......... .......... 78% 20.4M 8s
399250K .......... .......... .......... .......... .......... 78% 22.0M 8s
399300K .......... .......... .......... .......... .......... 78% 19.0M 8s
399350K .......... .......... .......... .......... .......... 78% 18.8M 8s
399400K .......... .......... .......... .......... .......... 78% 20.4M 8s
399450K .......... .......... .......... .......... .......... 78% 13.3M 8s
399500K .......... .......... .......... .......... .......... 78% 19.9M 8s
399550K .......... .......... .......... .......... .......... 78% 13.2M 8s
399600K .......... .......... .......... .......... .......... 78% 21.3M 8s
399650K .......... .......... .......... .......... .......... 78% 9.45M 8s
399700K .......... .......... .......... .......... .......... 78% 53.2M 8s
399750K .......... .......... .......... .......... .......... 78% 30.5M 8s
399800K .......... .......... .......... .......... .......... 78% 55.7M 8s
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399900K .......... .......... .......... .......... .......... 78% 25.0M 8s
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400000K .......... .......... .......... .......... .......... 78% 34.1M 8s
400050K .......... .......... .......... .......... .......... 78% 20.8M 8s
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400250K .......... .......... .......... .......... .......... 78% 29.4M 8s
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400700K .......... .......... .......... .......... .......... 78% 22.0M 8s
400750K .......... .......... .......... .......... .......... 78% 44.8M 8s
400800K .......... .......... .......... .......... .......... 78% 13.7M 8s
400850K .......... .......... .......... .......... .......... 78% 66.6M 8s
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400950K .......... .......... .......... .......... .......... 78% 47.1M 8s
401000K .......... .......... .......... .......... .......... 78% 37.6M 8s
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401300K .......... .......... .......... .......... .......... 78% 16.9M 8s
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401400K .......... .......... .......... .......... .......... 78% 19.7M 8s
401450K .......... .......... .......... .......... .......... 78% 13.7M 8s
401500K .......... .......... .......... .......... .......... 78% 22.3M 8s
401550K .......... .......... .......... .......... .......... 78% 24.8M 8s
401600K .......... .......... .......... .......... .......... 78% 17.9M 8s
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401700K .......... .......... .......... .......... .......... 78% 8.73M 8s
401750K .......... .......... .......... .......... .......... 78% 22.4M 8s
401800K .......... .......... .......... .......... .......... 78% 68.2M 8s
401850K .......... .......... .......... .......... .......... 78% 14.3M 8s
401900K .......... .......... .......... .......... .......... 78% 26.8M 8s
401950K .......... .......... .......... .......... .......... 78% 15.9M 8s
402000K .......... .......... .......... .......... .......... 78% 17.6M 8s
402050K .......... .......... .......... .......... .......... 78% 27.4M 8s
402100K .......... .......... .......... .......... .......... 78% 14.5M 8s
402150K .......... .......... .......... .......... .......... 78% 20.0M 8s
402200K .......... .......... .......... .......... .......... 78% 15.7M 8s
402250K .......... .......... .......... .......... .......... 78% 18.2M 8s
402300K .......... .......... .......... .......... .......... 78% 22.1M 8s
402350K .......... .......... .......... .......... .......... 78% 16.7M 8s
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402500K .......... .......... .......... .......... .......... 78% 20.0M 8s
402550K .......... .......... .......... .......... .......... 78% 13.6M 8s
402600K .......... .......... .......... .......... .......... 78% 12.7M 8s
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402750K .......... .......... .......... .......... .......... 79% 62.7M 8s
402800K .......... .......... .......... .......... .......... 79% 23.5M 8s
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402900K .......... .......... .......... .......... .......... 79% 20.9M 8s
402950K .......... .......... .......... .......... .......... 79% 18.2M 8s
403000K .......... .......... .......... .......... .......... 79% 20.7M 8s
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403150K .......... .......... .......... .......... .......... 79% 16.5M 8s
403200K .......... .......... .......... .......... .......... 79% 19.8M 8s
403250K .......... .......... .......... .......... .......... 79% 19.3M 8s
403300K .......... .......... .......... .......... .......... 79% 22.6M 8s
403350K .......... .......... .......... .......... .......... 79% 16.6M 8s
403400K .......... .......... .......... .......... .......... 79% 23.3M 8s
403450K .......... .......... .......... .......... .......... 79% 20.0M 8s
403500K .......... .......... .......... .......... .......... 79% 32.1M 8s
403550K .......... .......... .......... .......... .......... 79% 10.7M 8s
403600K .......... .......... .......... .......... .......... 79% 35.3M 8s
403650K .......... .......... .......... .......... .......... 79%  175M 8s
403700K .......... .......... .......... .......... .......... 79% 32.6M 8s
403750K .......... .......... .......... .......... .......... 79% 29.8M 8s
403800K .......... .......... .......... .......... .......... 79% 37.2M 8s
403850K .......... .......... .......... .......... .......... 79% 37.2M 8s
403900K .......... .......... .......... .......... .......... 79% 19.9M 8s
403950K .......... .......... .......... .......... .......... 79% 18.9M 8s
404000K .......... .......... .......... .......... .......... 79% 17.1M 8s
404050K .......... .......... .......... .......... .......... 79% 24.0M 8s
404100K .......... .......... .......... .......... .......... 79% 12.2M 8s
404150K .......... .......... .......... .......... .......... 79% 18.9M 8s
404200K .......... .......... .......... .......... .......... 79% 11.7M 8s
404250K .......... .......... .......... .......... .......... 79% 17.4M 8s
404300K .......... .......... .......... .......... .......... 79% 19.0M 8s
404350K .......... .......... .......... .......... .......... 79% 16.4M 8s
404400K .......... .......... .......... .......... .......... 79% 14.1M 8s
404450K .......... .......... .......... .......... .......... 79% 18.3M 8s
404500K .......... .......... .......... .......... .......... 79% 26.3M 8s
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404700K .......... .......... .......... .......... .......... 79% 12.9M 8s
404750K .......... .......... .......... .......... .......... 79% 42.8M 8s
404800K .......... .......... .......... .......... .......... 79% 53.3M 8s
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404900K .......... .......... .......... .......... .......... 79% 26.5M 8s
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405000K .......... .......... .......... .......... .......... 79% 23.4M 8s
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405100K .......... .......... .......... .......... .......... 79% 23.6M 8s
405150K .......... .......... .......... .......... .......... 79% 22.1M 8s
405200K .......... .......... .......... .......... .......... 79% 20.2M 8s
405250K .......... .......... .......... .......... .......... 79% 22.9M 8s
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405400K .......... .......... .......... .......... .......... 79% 18.0M 8s
405450K .......... .......... .......... .......... .......... 79% 14.0M 8s
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405550K .......... .......... .......... .......... .......... 79% 32.3M 8s
405600K .......... .......... .......... .......... .......... 79% 24.5M 8s
405650K .......... .......... .......... .......... .......... 79% 8.84M 8s
405700K .......... .......... .......... .......... .......... 79% 69.7M 8s
405750K .......... .......... .......... .......... .......... 79% 33.4M 8s
405800K .......... .......... .......... .......... .......... 79% 85.2M 8s
405850K .......... .......... .......... .......... .......... 79% 42.5M 8s
405900K .......... .......... .......... .......... .......... 79% 34.9M 8s
405950K .......... .......... .......... .......... .......... 79% 39.8M 7s
406000K .......... .......... .......... .......... .......... 79% 36.4M 7s
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406100K .......... .......... .......... .......... .......... 79% 26.6M 7s
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406250K .......... .......... .......... .......... .......... 79% 28.8M 7s
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406900K .......... .......... .......... .......... .......... 79% 21.6M 7s
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407000K .......... .......... .......... .......... .......... 79% 16.3M 7s
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407100K .......... .......... .......... .......... .......... 79% 27.5M 7s
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407200K .......... .......... .......... .......... .......... 79% 42.5M 7s
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407300K .......... .......... .......... .......... .......... 79% 31.7M 7s
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407400K .......... .......... .......... .......... .......... 79% 22.6M 7s
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407700K .......... .......... .......... .......... .......... 79% 18.0M 7s
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407800K .......... .......... .......... .......... .......... 80% 20.8M 7s
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407900K .......... .......... .......... .......... .......... 80% 23.4M 7s
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408000K .......... .......... .......... .......... .......... 80% 18.9M 7s
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408200K .......... .......... .......... .......... .......... 80% 37.1M 7s
408250K .......... .......... .......... .......... .......... 80% 63.2M 7s
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409100K .......... .......... .......... .......... .......... 80% 11.8M 7s
409150K .......... .......... .......... .......... .......... 80% 74.1M 7s
409200K .......... .......... .......... .......... .......... 80% 32.4M 7s
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410000K .......... .......... .......... .......... .......... 80% 11.9M 7s
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410100K .......... .......... .......... .......... .......... 80% 9.99M 7s
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410200K .......... .......... .......... .......... .......... 80% 8.75M 7s
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410300K .......... .......... .......... .......... .......... 80% 11.2M 7s
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410400K .......... .......... .......... .......... .......... 80% 12.9M 7s
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410500K .......... .......... .......... .......... .......... 80% 22.6M 7s
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410600K .......... .......... .......... .......... .......... 80% 24.0M 7s
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410800K .......... .......... .......... .......... .......... 80% 25.3M 7s
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411000K .......... .......... .......... .......... .......... 80% 30.0M 7s
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411100K .......... .......... .......... .......... .......... 80% 25.8M 7s
411150K .......... .......... .......... .......... .......... 80% 29.8M 7s
411200K .......... .......... .......... .......... .......... 80% 31.0M 7s
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411300K .......... .......... .......... .......... .......... 80% 32.1M 7s
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411400K .......... .......... .......... .......... .......... 80% 36.0M 7s
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411500K .......... .......... .......... .......... .......... 80% 26.3M 7s
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411600K .......... .......... .......... .......... .......... 80% 28.6M 7s
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411700K .......... .......... .......... .......... .......... 80% 31.2M 7s
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411800K .......... .......... .......... .......... .......... 80% 31.3M 7s
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411900K .......... .......... .......... .......... .......... 80% 36.0M 7s
411950K .......... .......... .......... .......... .......... 80%  109M 7s
412000K .......... .......... .......... .......... .......... 80% 29.8M 7s
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412100K .......... .......... .......... .......... .......... 80%  112M 7s
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412200K .......... .......... .......... .......... .......... 80% 54.5M 7s
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412300K .......... .......... .......... .......... .......... 80% 55.5M 7s
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412400K .......... .......... .......... .......... .......... 80% 39.4M 7s
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412500K .......... .......... .......... .......... .......... 80% 64.7M 7s
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412600K .......... .......... .......... .......... .......... 80% 37.2M 7s
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412700K .......... .......... .......... .......... .......... 80% 38.1M 7s
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412900K .......... .......... .......... .......... .......... 81% 50.2M 7s
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413000K .......... .......... .......... .......... .......... 81% 35.6M 7s
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413100K .......... .......... .......... .......... .......... 81% 44.1M 7s
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413200K .......... .......... .......... .......... .......... 81% 37.9M 7s
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413300K .......... .......... .......... .......... .......... 81% 44.5M 7s
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413400K .......... .......... .......... .......... .......... 81% 40.0M 7s
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413500K .......... .......... .......... .......... .......... 81% 36.3M 7s
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413600K .......... .......... .......... .......... .......... 81% 39.4M 7s
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413700K .......... .......... .......... .......... .......... 81% 37.0M 7s
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413800K .......... .......... .......... .......... .......... 81% 51.0M 7s
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413900K .......... .......... .......... .......... .......... 81% 91.3M 7s
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414000K .......... .......... .......... .......... .......... 81% 47.3M 7s
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414100K .......... .......... .......... .......... .......... 81%  133M 7s
414150K .......... .......... .......... .......... .......... 81% 47.4M 7s
414200K .......... .......... .......... .......... .......... 81% 54.1M 7s
414250K .......... .......... .......... .......... .......... 81%  191M 7s
414300K .......... .......... .......... .......... .......... 81%  108M 7s
414350K .......... .......... .......... .......... .......... 81% 22.9M 7s
414400K .......... .......... .......... .......... .......... 81% 54.0M 7s
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414500K .......... .......... .......... .......... .......... 81% 38.2M 7s
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414600K .......... .......... .......... .......... .......... 81% 28.7M 7s
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414700K .......... .......... .......... .......... .......... 81% 22.1M 7s
414750K .......... .......... .......... .......... .......... 81% 27.1M 7s
414800K .......... .......... .......... .......... .......... 81% 46.6M 7s
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414900K .......... .......... .......... .......... .......... 81% 43.1M 7s
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415000K .......... .......... .......... .......... .......... 81% 23.2M 7s
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415100K .......... .......... .......... .......... .......... 81% 29.0M 7s
415150K .......... .......... .......... .......... .......... 81% 34.3M 7s
415200K .......... .......... .......... .......... .......... 81% 25.8M 7s
415250K .......... .......... .......... .......... .......... 81% 35.4M 7s
415300K .......... .......... .......... .......... .......... 81% 37.0M 7s
415350K .......... .......... .......... .......... .......... 81% 27.1M 7s
415400K .......... .......... .......... .......... .......... 81% 23.3M 7s
415450K .......... .......... .......... .......... .......... 81% 41.4M 7s
415500K .......... .......... .......... .......... .......... 81% 23.0M 7s
415550K .......... .......... .......... .......... .......... 81% 41.1M 7s
415600K .......... .......... .......... .......... .......... 81% 75.8M 7s
415650K .......... .......... .......... .......... .......... 81% 34.6M 7s
415700K .......... .......... .......... .......... .......... 81% 10.6M 7s
415750K .......... .......... .......... .......... .......... 81%  155M 7s
415800K .......... .......... .......... .......... .......... 81%  163M 7s
415850K .......... .......... .......... .......... .......... 81% 52.3M 7s
415900K .......... .......... .......... .......... .......... 81% 44.7M 7s
415950K .......... .......... .......... .......... .......... 81% 19.4M 7s
416000K .......... .......... .......... .......... .......... 81% 95.2M 7s
416050K .......... .......... .......... .......... .......... 81%  125M 7s
416100K .......... .......... .......... .......... .......... 81% 21.6M 7s
416150K .......... .......... .......... .......... .......... 81% 41.7M 7s
416200K .......... .......... .......... .......... .......... 81% 22.0M 7s
416250K .......... .......... .......... .......... .......... 81% 27.3M 7s
416300K .......... .......... .......... .......... .......... 81% 29.2M 7s
416350K .......... .......... .......... .......... .......... 81% 24.8M 7s
416400K .......... .......... .......... .......... .......... 81% 23.9M 7s
416450K .......... .......... .......... .......... .......... 81% 22.9M 7s
416500K .......... .......... .......... .......... .......... 81% 21.4M 7s
416550K .......... .......... .......... .......... .......... 81% 22.1M 7s
416600K .......... .......... .......... .......... .......... 81% 22.0M 7s
416650K .......... .......... .......... .......... .......... 81% 23.6M 7s
416700K .......... .......... .......... .......... .......... 81% 26.7M 7s
416750K .......... .......... .......... .......... .......... 81% 28.9M 7s
416800K .......... .......... .......... .......... .......... 81% 23.1M 7s
416850K .......... .......... .......... .......... .......... 81% 23.8M 7s
416900K .......... .......... .......... .......... .......... 81% 21.5M 7s
416950K .......... .......... .......... .......... .......... 81% 34.1M 7s
417000K .......... .......... .......... .......... .......... 81% 17.6M 7s
417050K .......... .......... .......... .......... .......... 81% 10.3M 7s
417100K .......... .......... .......... .......... .......... 81%  106M 7s
417150K .......... .......... .......... .......... .......... 81% 30.8M 7s
417200K .......... .......... .......... .......... .......... 81% 30.7M 7s
417250K .......... .......... .......... .......... .......... 81% 49.7M 7s
417300K .......... .......... .......... .......... .......... 81% 24.3M 7s
417350K .......... .......... .......... .......... .......... 81% 26.4M 7s
417400K .......... .......... .......... .......... .......... 81% 27.1M 7s
417450K .......... .......... .......... .......... .......... 81% 24.2M 7s
417500K .......... .......... .......... .......... .......... 81% 21.8M 7s
417550K .......... .......... .......... .......... .......... 81% 24.6M 7s
417600K .......... .......... .......... .......... .......... 81% 25.0M 7s
417650K .......... .......... .......... .......... .......... 81% 30.3M 7s
417700K .......... .......... .......... .......... .......... 81% 19.5M 7s
417750K .......... .......... .......... .......... .......... 81% 20.7M 7s
417800K .......... .......... .......... .......... .......... 81% 19.7M 7s
417850K .......... .......... .......... .......... .......... 81% 20.8M 7s
417900K .......... .......... .......... .......... .......... 81% 20.5M 7s
417950K .......... .......... .......... .......... .......... 81% 18.9M 7s
418000K .......... .......... .......... .......... .......... 82% 20.4M 7s
418050K .......... .......... .......... .......... .......... 82% 32.5M 7s
418100K .......... .......... .......... .......... .......... 82% 14.8M 7s
418150K .......... .......... .......... .......... .......... 82% 30.0M 7s
418200K .......... .......... .......... .......... .......... 82% 23.0M 7s
418250K .......... .......... .......... .......... .......... 82% 10.4M 7s
418300K .......... .......... .......... .......... .......... 82% 44.5M 7s
418350K .......... .......... .......... .......... .......... 82% 66.8M 7s
418400K .......... .......... .......... .......... .......... 82% 16.9M 7s
418450K .......... .......... .......... .......... .......... 82% 19.9M 7s
418500K .......... .......... .......... .......... .......... 82% 23.5M 6s
418550K .......... .......... .......... .......... .......... 82% 17.2M 6s
418600K .......... .......... .......... .......... .......... 82% 14.1M 6s
418650K .......... .......... .......... .......... .......... 82% 19.0M 6s
418700K .......... .......... .......... .......... .......... 82% 11.9M 6s
418750K .......... .......... .......... .......... .......... 82% 18.6M 6s
418800K .......... .......... .......... .......... .......... 82% 18.1M 6s
418850K .......... .......... .......... .......... .......... 82% 12.8M 6s
418900K .......... .......... .......... .......... .......... 82% 16.7M 6s
418950K .......... .......... .......... .......... .......... 82% 13.4M 6s
419000K .......... .......... .......... .......... .......... 82% 17.2M 6s
419050K .......... .......... .......... .......... .......... 82% 21.4M 6s
419100K .......... .......... .......... .......... .......... 82% 7.55M 6s
419150K .......... .......... .......... .......... .......... 82% 86.4M 6s
419200K .......... .......... .......... .......... .......... 82% 17.8M 6s
419250K .......... .......... .......... .......... .......... 82% 5.04M 6s
419300K .......... .......... .......... .......... .......... 82% 97.1M 6s
419350K .......... .......... .......... .......... .......... 82%  104M 6s
419400K .......... .......... .......... .......... .......... 82%  126M 6s
419450K .......... .......... .......... .......... .......... 82% 21.2M 6s
419500K .......... .......... .......... .......... .......... 82% 25.1M 6s
419550K .......... .......... .......... .......... .......... 82% 23.2M 6s
419600K .......... .......... .......... .......... .......... 82% 26.5M 6s
419650K .......... .......... .......... .......... .......... 82% 24.8M 6s
419700K .......... .......... .......... .......... .......... 82% 15.6M 6s
419750K .......... .......... .......... .......... .......... 82% 21.7M 6s
419800K .......... .......... .......... .......... .......... 82% 22.1M 6s
419850K .......... .......... .......... .......... .......... 82% 27.0M 6s
419900K .......... .......... .......... .......... .......... 82% 25.3M 6s
419950K .......... .......... .......... .......... .......... 82% 24.3M 6s
420000K .......... .......... .......... .......... .......... 82% 37.6M 6s
420050K .......... .......... .......... .......... .......... 82% 35.0M 6s
420100K .......... .......... .......... .......... .......... 82% 15.9M 6s
420150K .......... .......... .......... .......... .......... 82%  364M 6s
420200K .......... .......... .......... .......... .......... 82% 19.2M 6s
420250K .......... .......... .......... .......... .......... 82%  444M 6s
420300K .......... .......... .......... .......... .......... 82%  248M 6s
420350K .......... .......... .......... .......... .......... 82% 27.9M 6s
420400K .......... .......... .......... .......... .......... 82% 33.0M 6s
420450K .......... .......... .......... .......... .......... 82% 29.4M 6s
420500K .......... .......... .......... .......... .......... 82% 34.9M 6s
420550K .......... .......... .......... .......... .......... 82% 42.3M 6s
420600K .......... .......... .......... .......... .......... 82% 22.2M 6s
420650K .......... .......... .......... .......... .......... 82% 35.1M 6s
420700K .......... .......... .......... .......... .......... 82% 25.7M 6s
420750K .......... .......... .......... .......... .......... 82% 31.6M 6s
420800K .......... .......... .......... .......... .......... 82% 35.0M 6s
420850K .......... .......... .......... .......... .......... 82% 31.6M 6s
420900K .......... .......... .......... .......... .......... 82% 29.7M 6s
420950K .......... .......... .......... .......... .......... 82% 29.2M 6s
421000K .......... .......... .......... .......... .......... 82% 43.1M 6s
421050K .......... .......... .......... .......... .......... 82% 31.2M 6s
421100K .......... .......... .......... .......... .......... 82% 29.7M 6s
421150K .......... .......... .......... .......... .......... 82% 28.6M 6s
421200K .......... .......... .......... .......... .......... 82% 29.4M 6s
421250K .......... .......... .......... .......... .......... 82% 31.5M 6s
421300K .......... .......... .......... .......... .......... 82% 34.7M 6s
421350K .......... .......... .......... .......... .......... 82% 37.5M 6s
421400K .......... .......... .......... .......... .......... 82% 35.2M 6s
421450K .......... .......... .......... .......... .......... 82% 27.0M 6s
421500K .......... .......... .......... .......... .......... 82% 42.0M 6s
421550K .......... .......... .......... .......... .......... 82% 29.5M 6s
421600K .......... .......... .......... .......... .......... 82% 29.5M 6s
421650K .......... .......... .......... .......... .......... 82% 17.7M 6s
421700K .......... .......... .......... .......... .......... 82%  351M 6s
421750K .......... .......... .......... .......... .......... 82% 22.5M 6s
421800K .......... .......... .......... .......... .......... 82% 27.8M 6s
421850K .......... .......... .......... .......... .......... 82% 70.4M 6s
421900K .......... .......... .......... .......... .......... 82% 52.4M 6s
421950K .......... .......... .......... .......... .......... 82% 57.0M 6s
422000K .......... .......... .......... .......... .......... 82% 37.8M 6s
422050K .......... .......... .......... .......... .......... 82% 29.0M 6s
422100K .......... .......... .......... .......... .......... 82% 41.3M 6s
422150K .......... .......... .......... .......... .......... 82% 42.7M 6s
422200K .......... .......... .......... .......... .......... 82% 31.6M 6s
422250K .......... .......... .......... .......... .......... 82% 37.1M 6s
422300K .......... .......... .......... .......... .......... 82% 34.9M 6s
422350K .......... .......... .......... .......... .......... 82% 25.4M 6s
422400K .......... .......... .......... .......... .......... 82% 47.1M 6s
422450K .......... .......... .......... .......... .......... 82% 28.9M 6s
422500K .......... .......... .......... .......... .......... 82% 37.9M 6s
422550K .......... .......... .......... .......... .......... 82% 42.5M 6s
422600K .......... .......... .......... .......... .......... 82% 31.4M 6s
422650K .......... .......... .......... .......... .......... 82% 40.9M 6s
422700K .......... .......... .......... .......... .......... 82% 31.7M 6s
422750K .......... .......... .......... .......... .......... 82% 29.2M 6s
422800K .......... .......... .......... .......... .......... 82% 45.8M 6s
422850K .......... .......... .......... .......... .......... 82% 32.2M 6s
422900K .......... .......... .......... .......... .......... 82% 41.5M 6s
422950K .......... .......... .......... .......... .......... 82% 31.1M 6s
423000K .......... .......... .......... .......... .......... 82% 22.8M 6s
423050K .......... .......... .......... .......... .......... 82% 46.5M 6s
423100K .......... .......... .......... .......... .......... 83% 42.6M 6s
423150K .......... .......... .......... .......... .......... 83% 25.8M 6s
423200K .......... .......... .......... .......... .......... 83% 42.4M 6s
423250K .......... .......... .......... .......... .......... 83% 34.7M 6s
423300K .......... .......... .......... .......... .......... 83% 55.6M 6s
423350K .......... .......... .......... .......... .......... 83% 34.7M 6s
423400K .......... .......... .......... .......... .......... 83% 41.9M 6s
423450K .......... .......... .......... .......... .......... 83% 27.6M 6s
423500K .......... .......... .......... .......... .......... 83% 18.0M 6s
423550K .......... .......... .......... .......... .......... 83% 37.0M 6s
423600K .......... .......... .......... .......... .......... 83%  138M 6s
423650K .......... .......... .......... .......... .......... 83% 34.5M 6s
423700K .......... .......... .......... .......... .......... 83%  155M 6s
423750K .......... .......... .......... .......... .......... 83% 27.6M 6s
423800K .......... .......... .......... .......... .......... 83% 81.7M 6s
423850K .......... .......... .......... .......... .......... 83% 43.8M 6s
423900K .......... .......... .......... .......... .......... 83% 35.5M 6s
423950K .......... .......... .......... .......... .......... 83% 30.2M 6s
424000K .......... .......... .......... .......... .......... 83% 38.3M 6s
424050K .......... .......... .......... .......... .......... 83% 44.7M 6s
424100K .......... .......... .......... .......... .......... 83% 32.5M 6s
424150K .......... .......... .......... .......... .......... 83% 34.1M 6s
424200K .......... .......... .......... .......... .......... 83% 33.7M 6s
424250K .......... .......... .......... .......... .......... 83% 41.6M 6s
424300K .......... .......... .......... .......... .......... 83% 46.7M 6s
424350K .......... .......... .......... .......... .......... 83% 27.0M 6s
424400K .......... .......... .......... .......... .......... 83% 53.4M 6s
424450K .......... .......... .......... .......... .......... 83% 38.2M 6s
424500K .......... .......... .......... .......... .......... 83% 34.7M 6s
424550K .......... .......... .......... .......... .......... 83% 47.2M 6s
424600K .......... .......... .......... .......... .......... 83% 28.7M 6s
424650K .......... .......... .......... .......... .......... 83% 42.6M 6s
424700K .......... .......... .......... .......... .......... 83% 42.4M 6s
424750K .......... .......... .......... .......... .......... 83% 34.2M 6s
424800K .......... .......... .......... .......... .......... 83% 48.0M 6s
424850K .......... .......... .......... .......... .......... 83% 26.8M 6s
424900K .......... .......... .......... .......... .......... 83% 46.6M 6s
424950K .......... .......... .......... .......... .......... 83% 27.0M 6s
425000K .......... .......... .......... .......... .......... 83% 48.6M 6s
425050K .......... .......... .......... .......... .......... 83% 37.3M 6s
425100K .......... .......... .......... .......... .......... 83% 25.6M 6s
425150K .......... .......... .......... .......... .......... 83% 27.4M 6s
425200K .......... .......... .......... .......... .......... 83% 11.6M 6s
425250K .......... .......... .......... .......... .......... 83%  161M 6s
425300K .......... .......... .......... .......... .......... 83% 79.3M 6s
425350K .......... .......... .......... .......... .......... 83% 23.6M 6s
425400K .......... .......... .......... .......... .......... 83% 32.8M 6s
425450K .......... .......... .......... .......... .......... 83% 28.0M 6s
425500K .......... .......... .......... .......... .......... 83% 25.8M 6s
425550K .......... .......... .......... .......... .......... 83% 30.9M 6s
425600K .......... .......... .......... .......... .......... 83% 26.8M 6s
425650K .......... .......... .......... .......... .......... 83% 21.7M 6s
425700K .......... .......... .......... .......... .......... 83% 19.2M 6s
425750K .......... .......... .......... .......... .......... 83% 20.0M 6s
425800K .......... .......... .......... .......... .......... 83% 34.0M 6s
425850K .......... .......... .......... .......... .......... 83% 21.1M 6s
425900K .......... .......... .......... .......... .......... 83% 31.6M 6s
425950K .......... .......... .......... .......... .......... 83% 23.5M 6s
426000K .......... .......... .......... .......... .......... 83% 24.0M 6s
426050K .......... .......... .......... .......... .......... 83% 24.4M 6s
426100K .......... .......... .......... .......... .......... 83% 20.9M 6s
426150K .......... .......... .......... .......... .......... 83% 43.0M 6s
426200K .......... .......... .......... .......... .......... 83% 22.4M 6s
426250K .......... .......... .......... .......... .......... 83% 22.6M 6s
426300K .......... .......... .......... .......... .......... 83% 32.6M 6s
426350K .......... .......... .......... .......... .......... 83% 31.9M 6s
426400K .......... .......... .......... .......... .......... 83% 30.9M 6s
426450K .......... .......... .......... .......... .......... 83% 92.0M 6s
426500K .......... .......... .......... .......... .......... 83% 33.4M 6s
426550K .......... .......... .......... .......... .......... 83% 54.3M 6s
426600K .......... .......... .......... .......... .......... 83% 17.6M 6s
426650K .......... .......... .......... .......... .......... 83% 69.0M 6s
426700K .......... .......... .......... .......... .......... 83% 65.7M 6s
426750K .......... .......... .......... .......... .......... 83% 92.0M 6s
426800K .......... .......... .......... .......... .......... 83% 54.4M 6s
426850K .......... .......... .......... .......... .......... 83% 36.7M 6s
426900K .......... .......... .......... .......... .......... 83% 45.2M 6s
426950K .......... .......... .......... .......... .......... 83% 28.4M 6s
427000K .......... .......... .......... .......... .......... 83% 43.8M 6s
427050K .......... .......... .......... .......... .......... 83% 41.3M 6s
427100K .......... .......... .......... .......... .......... 83% 27.5M 6s
427150K .......... .......... .......... .......... .......... 83% 35.1M 6s
427200K .......... .......... .......... .......... .......... 83% 25.5M 6s
427250K .......... .......... .......... .......... .......... 83% 37.1M 6s
427300K .......... .......... .......... .......... .......... 83% 28.1M 6s
427350K .......... .......... .......... .......... .......... 83% 31.3M 6s
427400K .......... .......... .......... .......... .......... 83% 41.6M 6s
427450K .......... .......... .......... .......... .......... 83% 23.6M 6s
427500K .......... .......... .......... .......... .......... 83% 44.7M 6s
427550K .......... .......... .......... .......... .......... 83% 35.5M 6s
427600K .......... .......... .......... .......... .......... 83% 32.9M 6s
427650K .......... .......... .......... .......... .......... 83% 29.8M 6s
427700K .......... .......... .......... .......... .......... 83% 32.8M 6s
427750K .......... .......... .......... .......... .......... 83% 28.0M 6s
427800K .......... .......... .......... .......... .......... 83% 39.6M 6s
427850K .......... .......... .......... .......... .......... 83% 33.0M 6s
427900K .......... .......... .......... .......... .......... 83% 22.8M 6s
427950K .......... .......... .......... .......... .......... 83% 34.0M 6s
428000K .......... .......... .......... .......... .......... 83% 27.5M 6s
428050K .......... .......... .......... .......... .......... 83%  110M 6s
428100K .......... .......... .......... .......... .......... 83% 30.7M 6s
428150K .......... .......... .......... .......... .......... 83% 26.6M 6s
428200K .......... .......... .......... .......... .......... 84% 18.4M 6s
428250K .......... .......... .......... .......... .......... 84% 30.4M 6s
428300K .......... .......... .......... .......... .......... 84%  131M 6s
428350K .......... .......... .......... .......... .......... 84% 34.9M 6s
428400K .......... .......... .......... .......... .......... 84%  125M 6s
428450K .......... .......... .......... .......... .......... 84%  123M 6s
428500K .......... .......... .......... .......... .......... 84% 46.8M 6s
428550K .......... .......... .......... .......... .......... 84% 23.3M 6s
428600K .......... .......... .......... .......... .......... 84% 44.6M 6s
428650K .......... .......... .......... .......... .......... 84%  106M 6s
428700K .......... .......... .......... .......... .......... 84% 28.6M 6s
428750K .......... .......... .......... .......... .......... 84% 34.7M 6s
428800K .......... .......... .......... .......... .......... 84% 33.6M 6s
428850K .......... .......... .......... .......... .......... 84% 34.2M 6s
428900K .......... .......... .......... .......... .......... 84% 34.1M 6s
428950K .......... .......... .......... .......... .......... 84% 36.9M 6s
429000K .......... .......... .......... .......... .......... 84% 34.3M 6s
429050K .......... .......... .......... .......... .......... 84% 37.7M 6s
429100K .......... .......... .......... .......... .......... 84% 25.0M 6s
429150K .......... .......... .......... .......... .......... 84% 42.8M 6s
429200K .......... .......... .......... .......... .......... 84% 24.4M 6s
429250K .......... .......... .......... .......... .......... 84% 38.6M 6s
429300K .......... .......... .......... .......... .......... 84% 24.2M 6s
429350K .......... .......... .......... .......... .......... 84% 35.5M 6s
429400K .......... .......... .......... .......... .......... 84% 27.3M 6s
429450K .......... .......... .......... .......... .......... 84% 35.4M 6s
429500K .......... .......... .......... .......... .......... 84% 38.0M 6s
429550K .......... .......... .......... .......... .......... 84% 34.9M 6s
429600K .......... .......... .......... .......... .......... 84% 23.5M 6s
429650K .......... .......... .......... .......... .......... 84% 37.7M 6s
429700K .......... .......... .......... .......... .......... 84% 31.6M 6s
429750K .......... .......... .......... .......... .......... 84% 32.5M 6s
429800K .......... .......... .......... .......... .......... 84% 27.0M 6s
429850K .......... .......... .......... .......... .......... 84% 25.2M 6s
429900K .......... .......... .......... .......... .......... 84% 23.4M 6s
429950K .......... .......... .......... .......... .......... 84% 14.1M 6s
430000K .......... .......... .......... .......... .......... 84% 42.3M 6s
430050K .......... .......... .......... .......... .......... 84%  122M 6s
430100K .......... .......... .......... .......... .......... 84%  104M 6s
430150K .......... .......... .......... .......... .......... 84% 25.6M 6s
430200K .......... .......... .......... .......... .......... 84% 96.3M 6s
430250K .......... .......... .......... .......... .......... 84%  114M 6s
430300K .......... .......... .......... .......... .......... 84% 28.7M 6s
430350K .......... .......... .......... .......... .......... 84%  115M 6s
430400K .......... .......... .......... .......... .......... 84% 39.8M 6s
430450K .......... .......... .......... .......... .......... 84% 43.6M 6s
430500K .......... .......... .......... .......... .......... 84% 36.1M 6s
430550K .......... .......... .......... .......... .......... 84% 50.7M 6s
430600K .......... .......... .......... .......... .......... 84% 27.4M 6s
430650K .......... .......... .......... .......... .......... 84% 54.1M 6s
430700K .......... .......... .......... .......... .......... 84% 35.7M 6s
430750K .......... .......... .......... .......... .......... 84% 44.2M 6s
430800K .......... .......... .......... .......... .......... 84% 27.1M 6s
430850K .......... .......... .......... .......... .......... 84% 35.6M 6s
430900K .......... .......... .......... .......... .......... 84% 38.7M 6s
430950K .......... .......... .......... .......... .......... 84% 41.9M 6s
431000K .......... .......... .......... .......... .......... 84% 23.4M 6s
431050K .......... .......... .......... .......... .......... 84% 35.2M 6s
431100K .......... .......... .......... .......... .......... 84% 35.2M 6s
431150K .......... .......... .......... .......... .......... 84% 45.1M 6s
431200K .......... .......... .......... .......... .......... 84% 29.5M 6s
431250K .......... .......... .......... .......... .......... 84% 44.1M 5s
431300K .......... .......... .......... .......... .......... 84% 49.4M 5s
431350K .......... .......... .......... .......... .......... 84% 37.3M 5s
431400K .......... .......... .......... .......... .......... 84% 37.6M 5s
431450K .......... .......... .......... .......... .......... 84% 29.2M 5s
431500K .......... .......... .......... .......... .......... 84% 46.2M 5s
431550K .......... .......... .......... .......... .......... 84% 46.5M 5s
431600K .......... .......... .......... .......... .......... 84% 33.5M 5s
431650K .......... .......... .......... .......... .......... 84% 49.6M 5s
431700K .......... .......... .......... .......... .......... 84% 35.8M 5s
431750K .......... .......... .......... .......... .......... 84% 52.4M 5s
431800K .......... .......... .......... .......... .......... 84% 12.2M 5s
431850K .......... .......... .......... .......... .......... 84%  168M 5s
431900K .......... .......... .......... .......... .......... 84% 33.0M 5s
431950K .......... .......... .......... .......... .......... 84%  147M 5s
432000K .......... .......... .......... .......... .......... 84% 35.0M 5s
432050K .......... .......... .......... .......... .......... 84%  192M 5s
432100K .......... .......... .......... .......... .......... 84% 76.3M 5s
432150K .......... .......... .......... .......... .......... 84% 26.1M 5s
432200K .......... .......... .......... .......... .......... 84% 59.8M 5s
432250K .......... .......... .......... .......... .......... 84%  202M 5s
432300K .......... .......... .......... .......... .......... 84% 46.9M 5s
432350K .......... .......... .......... .......... .......... 84% 32.4M 5s
432400K .......... .......... .......... .......... .......... 84% 41.7M 5s
432450K .......... .......... .......... .......... .......... 84% 38.0M 5s
432500K .......... .......... .......... .......... .......... 84% 47.8M 5s
432550K .......... .......... .......... .......... .......... 84% 41.5M 5s
432600K .......... .......... .......... .......... .......... 84% 35.0M 5s
432650K .......... .......... .......... .......... .......... 84% 54.1M 5s
432700K .......... .......... .......... .......... .......... 84% 34.9M 5s
432750K .......... .......... .......... .......... .......... 84% 46.7M 5s
432800K .......... .......... .......... .......... .......... 84% 53.5M 5s
432850K .......... .......... .......... .......... .......... 84% 41.8M 5s
432900K .......... .......... .......... .......... .......... 84% 34.6M 5s
432950K .......... .......... .......... .......... .......... 84% 41.9M 5s
433000K .......... .......... .......... .......... .......... 84% 47.4M 5s
433050K .......... .......... .......... .......... .......... 84% 47.6M 5s
433100K .......... .......... .......... .......... .......... 84% 41.9M 5s
433150K .......... .......... .......... .......... .......... 84% 45.8M 5s
433200K .......... .......... .......... .......... .......... 84% 32.3M 5s
433250K .......... .......... .......... .......... .......... 84% 46.4M 5s
433300K .......... .......... .......... .......... .......... 85% 40.9M 5s
433350K .......... .......... .......... .......... .......... 85% 13.3M 5s
433400K .......... .......... .......... .......... .......... 85%  509M 5s
433450K .......... .......... .......... .......... .......... 85% 83.3M 5s
433500K .......... .......... .......... .......... .......... 85% 29.3M 5s
433550K .......... .......... .......... .......... .......... 85% 37.9M 5s
433600K .......... .......... .......... .......... .......... 85% 34.4M 5s
433650K .......... .......... .......... .......... .......... 85% 29.2M 5s
433700K .......... .......... .......... .......... .......... 85% 17.4M 5s
433750K .......... .......... .......... .......... .......... 85% 19.8M 5s
433800K .......... .......... .......... .......... .......... 85% 13.3M 5s
433850K .......... .......... .......... .......... .......... 85% 17.7M 5s
433900K .......... .......... .......... .......... .......... 85% 15.3M 5s
433950K .......... .......... .......... .......... .......... 85% 29.8M 5s
434000K .......... .......... .......... .......... .......... 85% 23.8M 5s
434050K .......... .......... .......... .......... .......... 85% 18.2M 5s
434100K .......... .......... .......... .......... .......... 85% 16.4M 5s
434150K .......... .......... .......... .......... .......... 85% 23.2M 5s
434200K .......... .......... .......... .......... .......... 85% 16.2M 5s
434250K .......... .......... .......... .......... .......... 85% 18.9M 5s
434300K .......... .......... .......... .......... .......... 85% 16.6M 5s
434350K .......... .......... .......... .......... .......... 85% 16.2M 5s
434400K .......... .......... .......... .......... .......... 85% 19.4M 5s
434450K .......... .......... .......... .......... .......... 85% 14.9M 5s
434500K .......... .......... .......... .......... .......... 85% 14.3M 5s
434550K .......... .......... .......... .......... .......... 85% 18.9M 5s
434600K .......... .......... .......... .......... .......... 85% 20.0M 5s
434650K .......... .......... .......... .......... .......... 85% 22.0M 5s
434700K .......... .......... .......... .......... .......... 85% 52.8M 5s
434750K .......... .......... .......... .......... .......... 85% 12.3M 5s
434800K .......... .......... .......... .......... .......... 85%  137M 5s
434850K .......... .......... .......... .......... .......... 85% 20.8M 5s
434900K .......... .......... .......... .......... .......... 85%  130M 5s
434950K .......... .......... .......... .......... .......... 85% 29.8M 5s
435000K .......... .......... .......... .......... .......... 85% 39.6M 5s
435050K .......... .......... .......... .......... .......... 85% 31.2M 5s
435100K .......... .......... .......... .......... .......... 85% 21.7M 5s
435150K .......... .......... .......... .......... .......... 85% 33.9M 5s
435200K .......... .......... .......... .......... .......... 85% 22.3M 5s
435250K .......... .......... .......... .......... .......... 85% 35.2M 5s
435300K .......... .......... .......... .......... .......... 85% 22.6M 5s
435350K .......... .......... .......... .......... .......... 85% 31.6M 5s
435400K .......... .......... .......... .......... .......... 85% 22.4M 5s
435450K .......... .......... .......... .......... .......... 85% 20.7M 5s
435500K .......... .......... .......... .......... .......... 85% 42.2M 5s
435550K .......... .......... .......... .......... .......... 85% 26.9M 5s
435600K .......... .......... .......... .......... .......... 85% 20.9M 5s
435650K .......... .......... .......... .......... .......... 85% 34.3M 5s
435700K .......... .......... .......... .......... .......... 85% 20.4M 5s
435750K .......... .......... .......... .......... .......... 85% 40.1M 5s
435800K .......... .......... .......... .......... .......... 85% 22.4M 5s
435850K .......... .......... .......... .......... .......... 85% 34.1M 5s
435900K .......... .......... .......... .......... .......... 85% 27.0M 5s
435950K .......... .......... .......... .......... .......... 85% 92.1M 5s
436000K .......... .......... .......... .......... .......... 85% 44.8M 5s
436050K .......... .......... .......... .......... .......... 85% 93.4M 5s
436100K .......... .......... .......... .......... .......... 85% 37.4M 5s
436150K .......... .......... .......... .......... .......... 85%  104M 5s
436200K .......... .......... .......... .......... .......... 85% 29.7M 5s
436250K .......... .......... .......... .......... .......... 85% 91.8M 5s
436300K .......... .......... .......... .......... .......... 85% 21.1M 5s
436350K .......... .......... .......... .......... .......... 85% 31.8M 5s
436400K .......... .......... .......... .......... .......... 85%  119M 5s
436450K .......... .......... .......... .......... .......... 85% 36.9M 5s
436500K .......... .......... .......... .......... .......... 85%  109M 5s
436550K .......... .......... .......... .......... .......... 85% 67.1M 5s
436600K .......... .......... .......... .......... .......... 85% 83.6M 5s
436650K .......... .......... .......... .......... .......... 85% 37.6M 5s
436700K .......... .......... .......... .......... .......... 85% 37.4M 5s
436750K .......... .......... .......... .......... .......... 85% 38.0M 5s
436800K .......... .......... .......... .......... .......... 85% 39.9M 5s
436850K .......... .......... .......... .......... .......... 85% 24.2M 5s
436900K .......... .......... .......... .......... .......... 85% 35.6M 5s
436950K .......... .......... .......... .......... .......... 85% 38.0M 5s
437000K .......... .......... .......... .......... .......... 85% 36.4M 5s
437050K .......... .......... .......... .......... .......... 85% 24.2M 5s
437100K .......... .......... .......... .......... .......... 85% 36.7M 5s
437150K .......... .......... .......... .......... .......... 85% 37.3M 5s
437200K .......... .......... .......... .......... .......... 85% 23.7M 5s
437250K .......... .......... .......... .......... .......... 85% 36.6M 5s
437300K .......... .......... .......... .......... .......... 85% 37.0M 5s
437350K .......... .......... .......... .......... .......... 85% 34.5M 5s
437400K .......... .......... .......... .......... .......... 85% 31.3M 5s
437450K .......... .......... .......... .......... .......... 85% 37.5M 5s
437500K .......... .......... .......... .......... .......... 85% 41.7M 5s
437550K .......... .......... .......... .......... .......... 85% 46.9M 5s
437600K .......... .......... .......... .......... .......... 85% 31.0M 5s
437650K .......... .......... .......... .......... .......... 85% 43.6M 5s
437700K .......... .......... .......... .......... .......... 85% 25.1M 5s
437750K .......... .......... .......... .......... .......... 85% 36.2M 5s
437800K .......... .......... .......... .......... .......... 85% 37.7M 5s
437850K .......... .......... .......... .......... .......... 85% 52.1M 5s
437900K .......... .......... .......... .......... .......... 85% 35.6M 5s
437950K .......... .......... .......... .......... .......... 85% 15.0M 5s
438000K .......... .......... .......... .......... .......... 85% 51.5M 5s
438050K .......... .......... .......... .......... .......... 85%  114M 5s
438100K .......... .......... .......... .......... .......... 85% 73.0M 5s
438150K .......... .......... .......... .......... .......... 85% 46.9M 5s
438200K .......... .......... .......... .......... .......... 85% 93.5M 5s
438250K .......... .......... .......... .......... .......... 85% 48.4M 5s
438300K .......... .......... .......... .......... .......... 85% 63.1M 5s
438350K .......... .......... .......... .......... .......... 85% 60.4M 5s
438400K .......... .......... .......... .......... .......... 86% 32.0M 5s
438450K .......... .......... .......... .......... .......... 86% 28.1M 5s
438500K .......... .......... .......... .......... .......... 86% 26.9M 5s
438550K .......... .......... .......... .......... .......... 86% 29.9M 5s
438600K .......... .......... .......... .......... .......... 86% 23.3M 5s
438650K .......... .......... .......... .......... .......... 86% 35.9M 5s
438700K .......... .......... .......... .......... .......... 86% 24.7M 5s
438750K .......... .......... .......... .......... .......... 86% 28.8M 5s
438800K .......... .......... .......... .......... .......... 86% 34.5M 5s
438850K .......... .......... .......... .......... .......... 86% 23.9M 5s
438900K .......... .......... .......... .......... .......... 86% 26.8M 5s
438950K .......... .......... .......... .......... .......... 86% 23.6M 5s
439000K .......... .......... .......... .......... .......... 86% 34.6M 5s
439050K .......... .......... .......... .......... .......... 86% 31.5M 5s
439100K .......... .......... .......... .......... .......... 86% 21.7M 5s
439150K .......... .......... .......... .......... .......... 86% 35.7M 5s
439200K .......... .......... .......... .......... .......... 86% 18.6M 5s
439250K .......... .......... .......... .......... .......... 86% 29.1M 5s
439300K .......... .......... .......... .......... .......... 86% 39.8M 5s
439350K .......... .......... .......... .......... .......... 86% 22.6M 5s
439400K .......... .......... .......... .......... .......... 86% 34.4M 5s
439450K .......... .......... .......... .......... .......... 86% 30.2M 5s
439500K .......... .......... .......... .......... .......... 86%  132M 5s
439550K .......... .......... .......... .......... .......... 86% 13.4M 5s
439600K .......... .......... .......... .......... .......... 86% 95.4M 5s
439650K .......... .......... .......... .......... .......... 86% 54.5M 5s
439700K .......... .......... .......... .......... .......... 86% 57.0M 5s
439750K .......... .......... .......... .......... .......... 86% 42.8M 5s
439800K .......... .......... .......... .......... .......... 86% 22.2M 5s
439850K .......... .......... .......... .......... .......... 86% 94.8M 5s
439900K .......... .......... .......... .......... .......... 86% 62.8M 5s
439950K .......... .......... .......... .......... .......... 86% 41.0M 5s
440000K .......... .......... .......... .......... .......... 86% 29.0M 5s
440050K .......... .......... .......... .......... .......... 86% 37.3M 5s
440100K .......... .......... .......... .......... .......... 86% 22.6M 5s
440150K .......... .......... .......... .......... .......... 86% 38.6M 5s
440200K .......... .......... .......... .......... .......... 86% 33.0M 5s
440250K .......... .......... .......... .......... .......... 86% 26.9M 5s
440300K .......... .......... .......... .......... .......... 86% 38.8M 5s
440350K .......... .......... .......... .......... .......... 86% 20.7M 5s
440400K .......... .......... .......... .......... .......... 86% 39.3M 5s
440450K .......... .......... .......... .......... .......... 86% 36.4M 5s
440500K .......... .......... .......... .......... .......... 86% 27.0M 5s
440550K .......... .......... .......... .......... .......... 86% 37.8M 5s
440600K .......... .......... .......... .......... .......... 86% 23.8M 5s
440650K .......... .......... .......... .......... .......... 86% 27.1M 5s
440700K .......... .......... .......... .......... .......... 86% 34.1M 5s
440750K .......... .......... .......... .......... .......... 86% 39.9M 5s
440800K .......... .......... .......... .......... .......... 86% 31.3M 5s
440850K .......... .......... .......... .......... .......... 86% 22.0M 5s
440900K .......... .......... .......... .......... .......... 86% 43.4M 5s
440950K .......... .......... .......... .......... .......... 86% 20.7M 5s
441000K .......... .......... .......... .......... .......... 86% 24.3M 5s
441050K .......... .......... .......... .......... .......... 86% 90.9M 5s
441100K .......... .......... .......... .......... .......... 86% 20.5M 5s
441150K .......... .......... .......... .......... .......... 86% 18.9M 5s
441200K .......... .......... .......... .......... .......... 86% 32.4M 5s
441250K .......... .......... .......... .......... .......... 86%  110M 5s
441300K .......... .......... .......... .......... .......... 86% 17.1M 5s
441350K .......... .......... .......... .......... .......... 86% 33.7M 5s
441400K .......... .......... .......... .......... .......... 86% 33.9M 5s
441450K .......... .......... .......... .......... .......... 86% 18.4M 5s
441500K .......... .......... .......... .......... .......... 86% 27.1M 5s
441550K .......... .......... .......... .......... .......... 86% 16.6M 5s
441600K .......... .......... .......... .......... .......... 86% 20.4M 5s
441650K .......... .......... .......... .......... .......... 86% 16.3M 5s
441700K .......... .......... .......... .......... .......... 86% 19.3M 5s
441750K .......... .......... .......... .......... .......... 86% 19.8M 5s
441800K .......... .......... .......... .......... .......... 86% 18.5M 5s
441850K .......... .......... .......... .......... .......... 86% 14.1M 5s
441900K .......... .......... .......... .......... .......... 86% 21.0M 5s
441950K .......... .......... .......... .......... .......... 86% 19.3M 5s
442000K .......... .......... .......... .......... .......... 86% 22.3M 5s
442050K .......... .......... .......... .......... .......... 86% 20.0M 5s
442100K .......... .......... .......... .......... .......... 86% 14.0M 5s
442150K .......... .......... .......... .......... .......... 86% 12.5M 5s
442200K .......... .......... .......... .......... .......... 86% 47.1M 5s
442250K .......... .......... .......... .......... .......... 86% 76.4M 5s
442300K .......... .......... .......... .......... .......... 86% 60.7M 5s
442350K .......... .......... .......... .......... .......... 86% 33.7M 5s
442400K .......... .......... .......... .......... .......... 86% 64.9M 5s
442450K .......... .......... .......... .......... .......... 86% 26.7M 5s
442500K .......... .......... .......... .......... .......... 86% 31.3M 5s
442550K .......... .......... .......... .......... .......... 86% 29.2M 5s
442600K .......... .......... .......... .......... .......... 86% 27.2M 5s
442650K .......... .......... .......... .......... .......... 86% 23.5M 5s
442700K .......... .......... .......... .......... .......... 86% 25.2M 5s
442750K .......... .......... .......... .......... .......... 86% 31.2M 5s
442800K .......... .......... .......... .......... .......... 86% 31.5M 5s
442850K .......... .......... .......... .......... .......... 86% 18.6M 5s
442900K .......... .......... .......... .......... .......... 86% 36.2M 5s
442950K .......... .......... .......... .......... .......... 86% 21.2M 5s
443000K .......... .......... .......... .......... .......... 86% 24.8M 5s
443050K .......... .......... .......... .......... .......... 86% 33.8M 5s
443100K .......... .......... .......... .......... .......... 86% 23.7M 5s
443150K .......... .......... .......... .......... .......... 86% 22.7M 5s
443200K .......... .......... .......... .......... .......... 86% 23.6M 5s
443250K .......... .......... .......... .......... .......... 86% 37.5M 5s
443300K .......... .......... .......... .......... .......... 86% 23.8M 5s
443350K .......... .......... .......... .......... .......... 86% 21.7M 5s
443400K .......... .......... .......... .......... .......... 86% 33.3M 5s
443450K .......... .......... .......... .......... .......... 86% 22.7M 5s
443500K .......... .......... .......... .......... .......... 87% 15.6M 5s
443550K .......... .......... .......... .......... .......... 87% 98.8M 5s
443600K .......... .......... .......... .......... .......... 87% 41.7M 5s
443650K .......... .......... .......... .......... .......... 87% 30.3M 5s
443700K .......... .......... .......... .......... .......... 87% 32.7M 5s
443750K .......... .......... .......... .......... .......... 87% 68.2M 5s
443800K .......... .......... .......... .......... .......... 87% 46.9M 5s
443850K .......... .......... .......... .......... .......... 87% 51.9M 5s
443900K .......... .......... .......... .......... .......... 87% 37.4M 5s
443950K .......... .......... .......... .......... .......... 87% 27.0M 5s
444000K .......... .......... .......... .......... .......... 87% 34.9M 5s
444050K .......... .......... .......... .......... .......... 87% 44.2M 5s
444100K .......... .......... .......... .......... .......... 87% 20.6M 5s
444150K .......... .......... .......... .......... .......... 87% 27.6M 5s
444200K .......... .......... .......... .......... .......... 87% 34.3M 5s
444250K .......... .......... .......... .......... .......... 87% 21.7M 5s
444300K .......... .......... .......... .......... .......... 87% 37.7M 5s
444350K .......... .......... .......... .......... .......... 87% 22.8M 5s
444400K .......... .......... .......... .......... .......... 87% 23.5M 5s
444450K .......... .......... .......... .......... .......... 87% 34.5M 5s
444500K .......... .......... .......... .......... .......... 87% 24.1M 4s
444550K .......... .......... .......... .......... .......... 87% 42.2M 4s
444600K .......... .......... .......... .......... .......... 87% 22.7M 4s
444650K .......... .......... .......... .......... .......... 87% 21.2M 4s
444700K .......... .......... .......... .......... .......... 87% 23.5M 4s
444750K .......... .......... .......... .......... .......... 87% 38.1M 4s
444800K .......... .......... .......... .......... .......... 87% 20.8M 4s
444850K .......... .......... .......... .......... .......... 87% 29.0M 4s
444900K .......... .......... .......... .......... .......... 87% 62.6M 4s
444950K .......... .......... .......... .......... .......... 87% 21.2M 4s
445000K .......... .......... .......... .......... .......... 87% 35.8M 4s
445050K .......... .......... .......... .......... .......... 87% 14.0M 4s
445100K .......... .......... .......... .......... .......... 87% 73.4M 4s
445150K .......... .......... .......... .......... .......... 87% 79.8M 4s
445200K .......... .......... .......... .......... .......... 87% 39.6M 4s
445250K .......... .......... .......... .......... .......... 87% 39.1M 4s
445300K .......... .......... .......... .......... .......... 87% 70.7M 4s
445350K .......... .......... .......... .......... .......... 87% 25.0M 4s
445400K .......... .......... .......... .......... .......... 87% 37.6M 4s
445450K .......... .......... .......... .......... .......... 87% 22.2M 4s
445500K .......... .......... .......... .......... .......... 87% 22.0M 4s
445550K .......... .......... .......... .......... .......... 87% 43.1M 4s
445600K .......... .......... .......... .......... .......... 87% 22.0M 4s
445650K .......... .......... .......... .......... .......... 87% 21.3M 4s
445700K .......... .......... .......... .......... .......... 87% 21.9M 4s
445750K .......... .......... .......... .......... .......... 87% 24.3M 4s
445800K .......... .......... .......... .......... .......... 87% 37.3M 4s
445850K .......... .......... .......... .......... .......... 87% 20.8M 4s
445900K .......... .......... .......... .......... .......... 87% 21.5M 4s
445950K .......... .......... .......... .......... .......... 87% 20.8M 4s
446000K .......... .......... .......... .......... .......... 87% 42.4M 4s
446050K .......... .......... .......... .......... .......... 87% 23.1M 4s
446100K .......... .......... .......... .......... .......... 87% 26.9M 4s
446150K .......... .......... .......... .......... .......... 87% 27.0M 4s
446200K .......... .......... .......... .......... .......... 87% 26.2M 4s
446250K .......... .......... .......... .......... .......... 87% 47.3M 4s
446300K .......... .......... .......... .......... .......... 87% 11.3M 4s
446350K .......... .......... .......... .......... .......... 87% 24.1M 4s
446400K .......... .......... .......... .......... .......... 87%  119M 4s
446450K .......... .......... .......... .......... .......... 87% 32.0M 4s
446500K .......... .......... .......... .......... .......... 87%  115M 4s
446550K .......... .......... .......... .......... .......... 87%  131M 4s
446600K .......... .......... .......... .......... .......... 87% 46.3M 4s
446650K .......... .......... .......... .......... .......... 87% 15.5M 4s
446700K .......... .......... .......... .......... .......... 87%  122M 4s
446750K .......... .......... .......... .......... .......... 87%  121M 4s
446800K .......... .......... .......... .......... .......... 87% 8.70M 4s
446850K .......... .......... .......... .......... .......... 87% 38.8M 4s
446900K .......... .......... .......... .......... .......... 87% 25.3M 4s
446950K .......... .......... .......... .......... .......... 87% 29.1M 4s
447000K .......... .......... .......... .......... .......... 87% 37.6M 4s
447050K .......... .......... .......... .......... .......... 87% 34.4M 4s
447100K .......... .......... .......... .......... .......... 87% 21.9M 4s
447150K .......... .......... .......... .......... .......... 87% 36.3M 4s
447200K .......... .......... .......... .......... .......... 87% 24.3M 4s
447250K .......... .......... .......... .......... .......... 87% 41.8M 4s
447300K .......... .......... .......... .......... .......... 87% 25.7M 4s
447350K .......... .......... .......... .......... .......... 87% 36.8M 4s
447400K .......... .......... .......... .......... .......... 87% 26.9M 4s
447450K .......... .......... .......... .......... .......... 87% 33.0M 4s
447500K .......... .......... .......... .......... .......... 87% 32.0M 4s
447550K .......... .......... .......... .......... .......... 87% 24.5M 4s
447600K .......... .......... .......... .......... .......... 87% 33.0M 4s
447650K .......... .......... .......... .......... .......... 87% 36.5M 4s
447700K .......... .......... .......... .......... .......... 87% 26.5M 4s
447750K .......... .......... .......... .......... .......... 87% 27.9M 4s
447800K .......... .......... .......... .......... .......... 87% 80.6M 4s
447850K .......... .......... .......... .......... .......... 87% 13.0M 4s
447900K .......... .......... .......... .......... .......... 87%  161M 4s
447950K .......... .......... .......... .......... .......... 87% 29.9M 4s
448000K .......... .......... .......... .......... .......... 87%  180M 4s
448050K .......... .......... .......... .......... .......... 87% 19.5M 4s
448100K .......... .......... .......... .......... .......... 87% 24.6M 4s
448150K .......... .......... .......... .......... .......... 87% 50.3M 4s
448200K .......... .......... .......... .......... .......... 87% 27.7M 4s
448250K .......... .......... .......... .......... .......... 87% 27.0M 4s
448300K .......... .......... .......... .......... .......... 87% 25.1M 4s
448350K .......... .......... .......... .......... .......... 87% 20.6M 4s
448400K .......... .......... .......... .......... .......... 87% 21.0M 4s
448450K .......... .......... .......... .......... .......... 87% 21.3M 4s
448500K .......... .......... .......... .......... .......... 87% 35.8M 4s
448550K .......... .......... .......... .......... .......... 87% 24.0M 4s
448600K .......... .......... .......... .......... .......... 88% 21.9M 4s
448650K .......... .......... .......... .......... .......... 88% 45.0M 4s
448700K .......... .......... .......... .......... .......... 88% 13.5M 4s
448750K .......... .......... .......... .......... .......... 88% 19.8M 4s
448800K .......... .......... .......... .......... .......... 88% 37.9M 4s
448850K .......... .......... .......... .......... .......... 88% 15.5M 4s
448900K .......... .......... .......... .......... .......... 88% 37.5M 4s
448950K .......... .......... .......... .......... .......... 88% 11.5M 4s
449000K .......... .......... .......... .......... .......... 88% 23.7M 4s
449050K .......... .......... .......... .......... .......... 88% 13.0M 4s
449100K .......... .......... .......... .......... .......... 88% 37.0M 4s
449150K .......... .......... .......... .......... .......... 88%  121M 4s
449200K .......... .......... .......... .......... .......... 88% 44.1M 4s
449250K .......... .......... .......... .......... .......... 88% 42.7M 4s
449300K .......... .......... .......... .......... .......... 88% 36.8M 4s
449350K .......... .......... .......... .......... .......... 88% 96.7M 4s
449400K .......... .......... .......... .......... .......... 88% 36.8M 4s
449450K .......... .......... .......... .......... .......... 88% 32.5M 4s
449500K .......... .......... .......... .......... .......... 88% 31.7M 4s
449550K .......... .......... .......... .......... .......... 88% 38.4M 4s
449600K .......... .......... .......... .......... .......... 88% 38.1M 4s
449650K .......... .......... .......... .......... .......... 88% 30.2M 4s
449700K .......... .......... .......... .......... .......... 88% 29.3M 4s
449750K .......... .......... .......... .......... .......... 88% 12.7M 4s
449800K .......... .......... .......... .......... .......... 88% 36.4M 4s
449850K .......... .......... .......... .......... .......... 88% 35.4M 4s
449900K .......... .......... .......... .......... .......... 88% 23.8M 4s
449950K .......... .......... .......... .......... .......... 88% 36.9M 4s
450000K .......... .......... .......... .......... .......... 88% 23.9M 4s
450050K .......... .......... .......... .......... .......... 88% 42.4M 4s
450100K .......... .......... .......... .......... .......... 88% 24.8M 4s
450150K .......... .......... .......... .......... .......... 88% 42.3M 4s
450200K .......... .......... .......... .......... .......... 88% 35.9M 4s
450250K .......... .......... .......... .......... .......... 88% 28.5M 4s
450300K .......... .......... .......... .......... .......... 88% 38.7M 4s
450350K .......... .......... .......... .......... .......... 88% 25.1M 4s
450400K .......... .......... .......... .......... .......... 88% 29.6M 4s
450450K .......... .......... .......... .......... .......... 88% 8.48M 4s
450500K .......... .......... .......... .......... .......... 88% 16.8M 4s
450550K .......... .......... .......... .......... .......... 88%  107M 4s
450600K .......... .......... .......... .......... .......... 88% 30.5M 4s
450650K .......... .......... .......... .......... .......... 88% 19.3M 4s
450700K .......... .......... .......... .......... .......... 88% 13.1M 4s
450750K .......... .......... .......... .......... .......... 88% 14.9M 4s
450800K .......... .......... .......... .......... .......... 88% 12.2M 4s
450850K .......... .......... .......... .......... .......... 88% 11.0M 4s
450900K .......... .......... .......... .......... .......... 88% 14.1M 4s
450950K .......... .......... .......... .......... .......... 88% 13.6M 4s
451000K .......... .......... .......... .......... .......... 88% 13.5M 4s
451050K .......... .......... .......... .......... .......... 88% 12.8M 4s
451100K .......... .......... .......... .......... .......... 88% 5.26M 4s
451150K .......... .......... .......... .......... .......... 88% 83.3M 4s
451200K .......... .......... .......... .......... .......... 88% 17.3M 4s
451250K .......... .......... .......... .......... .......... 88% 10.4M 4s
451300K .......... .......... .......... .......... .......... 88% 10.5M 4s
451350K .......... .......... .......... .......... .......... 88% 8.60M 4s
451400K .......... .......... .......... .......... .......... 88% 9.49M 4s
451450K .......... .......... .......... .......... .......... 88% 7.15M 4s
451500K .......... .......... .......... .......... .......... 88% 9.83M 4s
451550K .......... .......... .......... .......... .......... 88% 7.07M 4s
451600K .......... .......... .......... .......... .......... 88% 6.08M 4s
451650K .......... .......... .......... .......... .......... 88% 79.1M 4s
451700K .......... .......... .......... .......... .......... 88% 12.0M 4s
451750K .......... .......... .......... .......... .......... 88% 70.6M 4s
451800K .......... .......... .......... .......... .......... 88% 25.2M 4s
451850K .......... .......... .......... .......... .......... 88% 22.1M 4s
451900K .......... .......... .......... .......... .......... 88% 20.0M 4s
451950K .......... .......... .......... .......... .......... 88% 16.5M 4s
452000K .......... .......... .......... .......... .......... 88% 18.1M 4s
452050K .......... .......... .......... .......... .......... 88% 16.5M 4s
452100K .......... .......... .......... .......... .......... 88% 13.9M 4s
452150K .......... .......... .......... .......... .......... 88% 19.8M 4s
452200K .......... .......... .......... .......... .......... 88% 11.8M 4s
452250K .......... .......... .......... .......... .......... 88% 17.7M 4s
452300K .......... .......... .......... .......... .......... 88% 14.9M 4s
452350K .......... .......... .......... .......... .......... 88% 13.1M 4s
452400K .......... .......... .......... .......... .......... 88% 22.3M 4s
452450K .......... .......... .......... .......... .......... 88% 18.2M 4s
452500K .......... .......... .......... .......... .......... 88% 15.0M 4s
452550K .......... .......... .......... .......... .......... 88% 81.0M 4s
452600K .......... .......... .......... .......... .......... 88% 27.0M 4s
452650K .......... .......... .......... .......... .......... 88% 32.7M 4s
452700K .......... .......... .......... .......... .......... 88% 22.2M 4s
452750K .......... .......... .......... .......... .......... 88% 26.9M 4s
452800K .......... .......... .......... .......... .......... 88% 23.3M 4s
452850K .......... .......... .......... .......... .......... 88% 28.9M 4s
452900K .......... .......... .......... .......... .......... 88% 21.0M 4s
452950K .......... .......... .......... .......... .......... 88% 19.2M 4s
453000K .......... .......... .......... .......... .......... 88% 35.8M 4s
453050K .......... .......... .......... .......... .......... 88% 22.9M 4s
453100K .......... .......... .......... .......... .......... 88% 20.9M 4s
453150K .......... .......... .......... .......... .......... 88% 32.3M 4s
453200K .......... .......... .......... .......... .......... 88% 16.2M 4s
453250K .......... .......... .......... .......... .......... 88% 30.4M 4s
453300K .......... .......... .......... .......... .......... 88% 20.4M 4s
453350K .......... .......... .......... .......... .......... 88% 19.9M 4s
453400K .......... .......... .......... .......... .......... 88% 32.2M 4s
453450K .......... .......... .......... .......... .......... 88% 20.6M 4s
453500K .......... .......... .......... .......... .......... 88% 27.1M 4s
453550K .......... .......... .......... .......... .......... 88% 32.6M 4s
453600K .......... .......... .......... .......... .......... 88% 21.0M 4s
453650K .......... .......... .......... .......... .......... 88% 76.9M 4s
453700K .......... .......... .......... .......... .......... 89% 26.3M 4s
453750K .......... .......... .......... .......... .......... 89% 21.3M 4s
453800K .......... .......... .......... .......... .......... 89% 83.6M 4s
453850K .......... .......... .......... .......... .......... 89% 18.2M 4s
453900K .......... .......... .......... .......... .......... 89% 84.5M 4s
453950K .......... .......... .......... .......... .......... 89% 72.0M 4s
454000K .......... .......... .......... .......... .......... 89% 61.3M 4s
454050K .......... .......... .......... .......... .......... 89% 84.2M 4s
454100K .......... .......... .......... .......... .......... 89% 58.8M 4s
454150K .......... .......... .......... .......... .......... 89% 30.9M 4s
454200K .......... .......... .......... .......... .......... 89% 34.4M 4s
454250K .......... .......... .......... .......... .......... 89% 40.9M 4s
454300K .......... .......... .......... .......... .......... 89% 46.2M 4s
454350K .......... .......... .......... .......... .......... 89% 23.9M 4s
454400K .......... .......... .......... .......... .......... 89% 38.0M 4s
454450K .......... .......... .......... .......... .......... 89% 24.3M 4s
454500K .......... .......... .......... .......... .......... 89% 26.8M 4s
454550K .......... .......... .......... .......... .......... 89% 39.8M 4s
454600K .......... .......... .......... .......... .......... 89% 22.5M 4s
454650K .......... .......... .......... .......... .......... 89% 34.9M 4s
454700K .......... .......... .......... .......... .......... 89% 23.3M 4s
454750K .......... .......... .......... .......... .......... 89% 35.2M 4s
454800K .......... .......... .......... .......... .......... 89% 21.7M 4s
454850K .......... .......... .......... .......... .......... 89% 20.7M 4s
454900K .......... .......... .......... .......... .......... 89% 31.6M 4s
454950K .......... .......... .......... .......... .......... 89% 23.9M 4s
455000K .......... .......... .......... .......... .......... 89% 24.5M 4s
455050K .......... .......... .......... .......... .......... 89% 13.1M 4s
455100K .......... .......... .......... .......... .......... 89% 41.6M 4s
455150K .......... .......... .......... .......... .......... 89% 21.3M 4s
455200K .......... .......... .......... .......... .......... 89% 19.2M 4s
455250K .......... .......... .......... .......... .......... 89% 26.6M 4s
455300K .......... .......... .......... .......... .......... 89% 25.3M 4s
455350K .......... .......... .......... .......... .......... 89% 13.9M 4s
455400K .......... .......... .......... .......... .......... 89% 30.4M 4s
455450K .......... .......... .......... .......... .......... 89% 15.7M 4s
455500K .......... .......... .......... .......... .......... 89% 34.6M 4s
455550K .......... .......... .......... .......... .......... 89% 19.2M 4s
455600K .......... .......... .......... .......... .......... 89% 18.5M 4s
455650K .......... .......... .......... .......... .......... 89% 17.8M 4s
455700K .......... .......... .......... .......... .......... 89% 19.9M 4s
455750K .......... .......... .......... .......... .......... 89% 16.9M 4s
455800K .......... .......... .......... .......... .......... 89% 17.2M 4s
455850K .......... .......... .......... .......... .......... 89% 9.72M 4s
455900K .......... .......... .......... .......... .......... 89% 17.6M 4s
455950K .......... .......... .......... .......... .......... 89% 70.1M 4s
456000K .......... .......... .......... .......... .......... 89% 38.4M 4s
456050K .......... .......... .......... .......... .......... 89% 29.0M 4s
456100K .......... .......... .......... .......... .......... 89% 23.7M 4s
456150K .......... .......... .......... .......... .......... 89% 23.4M 4s
456200K .......... .......... .......... .......... .......... 89% 18.3M 4s
456250K .......... .......... .......... .......... .......... 89% 19.8M 4s
456300K .......... .......... .......... .......... .......... 89% 19.8M 4s
456350K .......... .......... .......... .......... .......... 89% 19.7M 4s
456400K .......... .......... .......... .......... .......... 89% 22.2M 4s
456450K .......... .......... .......... .......... .......... 89% 19.9M 4s
456500K .......... .......... .......... .......... .......... 89% 27.0M 4s
456550K .......... .......... .......... .......... .......... 89% 20.9M 4s
456600K .......... .......... .......... .......... .......... 89% 13.7M 4s
456650K .......... .......... .......... .......... .......... 89% 20.3M 4s
456700K .......... .......... .......... .......... .......... 89% 33.9M 4s
456750K .......... .......... .......... .......... .......... 89% 34.5M 4s
456800K .......... .......... .......... .......... .......... 89% 32.6M 4s
456850K .......... .......... .......... .......... .......... 89% 15.1M 4s
456900K .......... .......... .......... .......... .......... 89% 77.9M 4s
456950K .......... .......... .......... .......... .......... 89%  158M 4s
457000K .......... .......... .......... .......... .......... 89% 26.2M 4s
457050K .......... .......... .......... .......... .......... 89%  180M 4s
457100K .......... .......... .......... .......... .......... 89% 32.7M 4s
457150K .......... .......... .......... .......... .......... 89% 45.0M 4s
457200K .......... .......... .......... .......... .......... 89% 44.1M 4s
457250K .......... .......... .......... .......... .......... 89% 31.4M 4s
457300K .......... .......... .......... .......... .......... 89% 35.3M 4s
457350K .......... .......... .......... .......... .......... 89% 25.3M 4s
457400K .......... .......... .......... .......... .......... 89% 43.2M 4s
457450K .......... .......... .......... .......... .......... 89% 22.8M 4s
457500K .......... .......... .......... .......... .......... 89% 39.9M 4s
457550K .......... .......... .......... .......... .......... 89% 24.2M 4s
457600K .......... .......... .......... .......... .......... 89% 19.7M 4s
457650K .......... .......... .......... .......... .......... 89% 35.2M 4s
457700K .......... .......... .......... .......... .......... 89% 19.7M 4s
457750K .......... .......... .......... .......... .......... 89% 31.3M 4s
457800K .......... .......... .......... .......... .......... 89% 20.3M 4s
457850K .......... .......... .......... .......... .......... 89% 23.4M 4s
457900K .......... .......... .......... .......... .......... 89% 31.7M 4s
457950K .......... .......... .......... .......... .......... 89% 19.3M 4s
458000K .......... .......... .......... .......... .......... 89% 19.4M 4s
458050K .......... .......... .......... .......... .......... 89% 32.2M 4s
458100K .......... .......... .......... .......... .......... 89% 29.5M 4s
458150K .......... .......... .......... .......... .......... 89% 79.7M 4s
458200K .......... .......... .......... .......... .......... 89% 9.45M 4s
458250K .......... .......... .......... .......... .......... 89% 79.7M 4s
458300K .......... .......... .......... .......... .......... 89% 82.9M 4s
458350K .......... .......... .......... .......... .......... 89% 56.7M 4s
458400K .......... .......... .......... .......... .......... 89% 79.5M 3s
458450K .......... .......... .......... .......... .......... 89% 37.7M 3s
458500K .......... .......... .......... .......... .......... 89% 47.0M 3s
458550K .......... .......... .......... .......... .......... 89% 42.2M 3s
458600K .......... .......... .......... .......... .......... 89% 27.8M 3s
458650K .......... .......... .......... .......... .......... 89% 34.7M 3s
458700K .......... .......... .......... .......... .......... 89% 30.6M 3s
458750K .......... .......... .......... .......... .......... 89% 46.2M 3s
458800K .......... .......... .......... .......... .......... 90% 32.3M 3s
458850K .......... .......... .......... .......... .......... 90% 23.7M 3s
458900K .......... .......... .......... .......... .......... 90% 33.1M 3s
458950K .......... .......... .......... .......... .......... 90% 21.6M 3s
459000K .......... .......... .......... .......... .......... 90% 38.4M 3s
459050K .......... .......... .......... .......... .......... 90% 35.0M 3s
459100K .......... .......... .......... .......... .......... 90% 21.0M 3s
459150K .......... .......... .......... .......... .......... 90% 34.9M 3s
459200K .......... .......... .......... .......... .......... 90% 30.8M 3s
459250K .......... .......... .......... .......... .......... 90% 18.3M 3s
459300K .......... .......... .......... .......... .......... 90% 32.5M 3s
459350K .......... .......... .......... .......... .......... 90% 31.1M 3s
459400K .......... .......... .......... .......... .......... 90% 20.7M 3s
459450K .......... .......... .......... .......... .......... 90% 52.2M 3s
459500K .......... .......... .......... .......... .......... 90% 48.1M 3s
459550K .......... .......... .......... .......... .......... 90% 65.0M 3s
459600K .......... .......... .......... .......... .......... 90% 44.2M 3s
459650K .......... .......... .......... .......... .......... 90% 60.5M 3s
459700K .......... .......... .......... .......... .......... 90% 78.1M 3s
459750K .......... .......... .......... .......... .......... 90%  100M 3s
459800K .......... .......... .......... .......... .......... 90% 15.1M 3s
459850K .......... .......... .......... .......... .......... 90% 77.1M 3s
459900K .......... .......... .......... .......... .......... 90% 95.4M 3s
459950K .......... .......... .......... .......... .......... 90% 82.3M 3s
460000K .......... .......... .......... .......... .......... 90% 96.9M 3s
460050K .......... .......... .......... .......... .......... 90% 34.7M 3s
460100K .......... .......... .......... .......... .......... 90% 62.0M 3s
460150K .......... .......... .......... .......... .......... 90% 89.4M 3s
460200K .......... .......... .......... .......... .......... 90% 49.1M 3s
460250K .......... .......... .......... .......... .......... 90%  102M 3s
460300K .......... .......... .......... .......... .......... 90% 85.7M 3s
460350K .......... .......... .......... .......... .......... 90% 39.8M 3s
460400K .......... .......... .......... .......... .......... 90% 46.5M 3s
460450K .......... .......... .......... .......... .......... 90% 45.4M 3s
460500K .......... .......... .......... .......... .......... 90% 41.8M 3s
460550K .......... .......... .......... .......... .......... 90% 33.9M 3s
460600K .......... .......... .......... .......... .......... 90% 41.6M 3s
460650K .......... .......... .......... .......... .......... 90% 52.3M 3s
460700K .......... .......... .......... .......... .......... 90% 34.6M 3s
460750K .......... .......... .......... .......... .......... 90% 49.7M 3s
460800K .......... .......... .......... .......... .......... 90% 42.1M 3s
460850K .......... .......... .......... .......... .......... 90% 35.9M 3s
460900K .......... .......... .......... .......... .......... 90% 37.4M 3s
460950K .......... .......... .......... .......... .......... 90% 34.2M 3s
461000K .......... .......... .......... .......... .......... 90% 49.9M 3s
461050K .......... .......... .......... .......... .......... 90% 51.5M 3s
461100K .......... .......... .......... .......... .......... 90% 46.4M 3s
461150K .......... .......... .......... .......... .......... 90% 43.8M 3s
461200K .......... .......... .......... .......... .......... 90% 35.0M 3s
461250K .......... .......... .......... .......... .......... 90% 41.7M 3s
461300K .......... .......... .......... .......... .......... 90% 46.7M 3s
461350K .......... .......... .......... .......... .......... 90% 39.2M 3s
461400K .......... .......... .......... .......... .......... 90% 46.0M 3s
461450K .......... .......... .......... .......... .......... 90% 49.8M 3s
461500K .......... .......... .......... .......... .......... 90% 41.3M 3s
461550K .......... .......... .......... .......... .......... 90% 42.8M 3s
461600K .......... .......... .......... .......... .......... 90% 36.6M 3s
461650K .......... .......... .......... .......... .......... 90% 46.8M 3s
461700K .......... .......... .......... .......... .......... 90% 60.2M 3s
461750K .......... .......... .......... .......... .......... 90% 43.2M 3s
461800K .......... .......... .......... .......... .......... 90% 50.7M 3s
461850K .......... .......... .......... .......... .......... 90% 77.8M 3s
461900K .......... .......... .......... .......... .......... 90% 13.5M 3s
461950K .......... .......... .......... .......... .......... 90%  144M 3s
462000K .......... .......... .......... .......... .......... 90%  198M 3s
462050K .......... .......... .......... .......... .......... 90% 46.7M 3s
462100K .......... .......... .......... .......... .......... 90%  176M 3s
462150K .......... .......... .......... .......... .......... 90% 21.0M 3s
462200K .......... .......... .......... .......... .......... 90%  170M 3s
462250K .......... .......... .......... .......... .......... 90%  193M 3s
462300K .......... .......... .......... .......... .......... 90% 32.9M 3s
462350K .......... .......... .......... .......... .......... 90%  166M 3s
462400K .......... .......... .......... .......... .......... 90%  201M 3s
462450K .......... .......... .......... .......... .......... 90%  144M 3s
462500K .......... .......... .......... .......... .......... 90% 71.0M 3s
462550K .......... .......... .......... .......... .......... 90% 36.7M 3s
462600K .......... .......... .......... .......... .......... 90% 41.7M 3s
462650K .......... .......... .......... .......... .......... 90% 34.1M 3s
462700K .......... .......... .......... .......... .......... 90% 41.8M 3s
462750K .......... .......... .......... .......... .......... 90% 41.6M 3s
462800K .......... .......... .......... .......... .......... 90% 41.1M 3s
462850K .......... .......... .......... .......... .......... 90% 30.2M 3s
462900K .......... .......... .......... .......... .......... 90% 46.6M 3s
462950K .......... .......... .......... .......... .......... 90% 31.8M 3s
463000K .......... .......... .......... .......... .......... 90% 34.0M 3s
463050K .......... .......... .......... .......... .......... 90% 45.0M 3s
463100K .......... .......... .......... .......... .......... 90% 38.1M 3s
463150K .......... .......... .......... .......... .......... 90% 25.3M 3s
463200K .......... .......... .......... .......... .......... 90% 42.8M 3s
463250K .......... .......... .......... .......... .......... 90% 39.9M 3s
463300K .......... .......... .......... .......... .......... 90% 45.3M 3s
463350K .......... .......... .......... .......... .......... 90% 25.7M 3s
463400K .......... .......... .......... .......... .......... 90% 40.0M 3s
463450K .......... .......... .......... .......... .......... 90% 38.9M 3s
463500K .......... .......... .......... .......... .......... 90% 26.4M 3s
463550K .......... .......... .......... .......... .......... 90% 43.5M 3s
463600K .......... .......... .......... .......... .......... 90% 45.5M 3s
463650K .......... .......... .......... .......... .......... 90% 39.5M 3s
463700K .......... .......... .......... .......... .......... 90% 29.1M 3s
463750K .......... .......... .......... .......... .......... 90% 41.7M 3s
463800K .......... .......... .......... .......... .......... 90% 43.3M 3s
463850K .......... .......... .......... .......... .......... 90% 36.8M 3s
463900K .......... .......... .......... .......... .......... 91%  162M 3s
463950K .......... .......... .......... .......... .......... 91% 34.8M 3s
464000K .......... .......... .......... .......... .......... 91% 18.0M 3s
464050K .......... .......... .......... .......... .......... 91% 66.0M 3s
464100K .......... .......... .......... .......... .......... 91%  142M 3s
464150K .......... .......... .......... .......... .......... 91%  158M 3s
464200K .......... .......... .......... .......... .......... 91% 58.5M 3s
464250K .......... .......... .......... .......... .......... 91%  117M 3s
464300K .......... .......... .......... .......... .......... 91% 25.7M 3s
464350K .......... .......... .......... .......... .......... 91%  135M 3s
464400K .......... .......... .......... .......... .......... 91%  140M 3s
464450K .......... .......... .......... .......... .......... 91%  147M 3s
464500K .......... .......... .......... .......... .......... 91%  152M 3s
464550K .......... .......... .......... .......... .......... 91% 44.9M 3s
464600K .......... .......... .......... .......... .......... 91% 44.2M 3s
464650K .......... .......... .......... .......... .......... 91% 63.2M 3s
464700K .......... .......... .......... .......... .......... 91% 41.4M 3s
464750K .......... .......... .......... .......... .......... 91% 53.8M 3s
464800K .......... .......... .......... .......... .......... 91% 47.5M 3s
464850K .......... .......... .......... .......... .......... 91% 43.0M 3s
464900K .......... .......... .......... .......... .......... 91% 53.6M 3s
464950K .......... .......... .......... .......... .......... 91% 53.1M 3s
465000K .......... .......... .......... .......... .......... 91% 47.4M 3s
465050K .......... .......... .......... .......... .......... 91% 42.3M 3s
465100K .......... .......... .......... .......... .......... 91% 54.0M 3s
465150K .......... .......... .......... .......... .......... 91% 54.4M 3s
465200K .......... .......... .......... .......... .......... 91% 40.7M 3s
465250K .......... .......... .......... .......... .......... 91% 48.4M 3s
465300K .......... .......... .......... .......... .......... 91% 52.8M 3s
465350K .......... .......... .......... .......... .......... 91% 38.3M 3s
465400K .......... .......... .......... .......... .......... 91% 53.8M 3s
465450K .......... .......... .......... .......... .......... 91% 41.9M 3s
465500K .......... .......... .......... .......... .......... 91% 54.3M 3s
465550K .......... .......... .......... .......... .......... 91% 53.1M 3s
465600K .......... .......... .......... .......... .......... 91% 46.1M 3s
465650K .......... .......... .......... .......... .......... 91% 54.1M 3s
465700K .......... .......... .......... .......... .......... 91% 43.1M 3s
465750K .......... .......... .......... .......... .......... 91% 42.0M 3s
465800K .......... .......... .......... .......... .......... 91% 47.8M 3s
465850K .......... .......... .......... .......... .......... 91% 53.1M 3s
465900K .......... .......... .......... .......... .......... 91% 54.4M 3s
465950K .......... .......... .......... .......... .......... 91% 47.8M 3s
466000K .......... .......... .......... .......... .......... 91% 48.0M 3s
466050K .......... .......... .......... .......... .......... 91% 47.4M 3s
466100K .......... .......... .......... .......... .......... 91% 42.3M 3s
466150K .......... .......... .......... .......... .......... 91% 15.0M 3s
466200K .......... .......... .......... .......... .......... 91% 91.8M 3s
466250K .......... .......... .......... .......... .......... 91% 47.3M 3s
466300K .......... .......... .......... .......... .......... 91% 75.9M 3s
466350K .......... .......... .......... .......... .......... 91% 39.1M 3s
466400K .......... .......... .......... .......... .......... 91% 15.0M 3s
466450K .......... .......... .......... .......... .......... 91%  421M 3s
466500K .......... .......... .......... .......... .......... 91% 59.2M 3s
466550K .......... .......... .......... .......... .......... 91% 18.9M 3s
466600K .......... .......... .......... .......... .......... 91%  404M 3s
466650K .......... .......... .......... .......... .......... 91%  404M 3s
466700K .......... .......... .......... .......... .......... 91%  428M 3s
466750K .......... .......... .......... .......... .......... 91%  514M 3s
466800K .......... .......... .......... .......... .......... 91% 43.8M 3s
466850K .......... .......... .......... .......... .......... 91% 64.9M 3s
466900K .......... .......... .......... .......... .......... 91% 28.1M 3s
466950K .......... .......... .......... .......... .......... 91%  373M 3s
467000K .......... .......... .......... .......... .......... 91%  234M 3s
467050K .......... .......... .......... .......... .......... 91%  414M 3s
467100K .......... .......... .......... .......... .......... 91% 42.9M 3s
467150K .......... .......... .......... .......... .......... 91% 88.5M 3s
467200K .......... .......... .......... .......... .......... 91%  208M 3s
467250K .......... .......... .......... .......... .......... 91% 54.6M 3s
467300K .......... .......... .......... .......... .......... 91% 38.0M 3s
467350K .......... .......... .......... .......... .......... 91% 47.4M 3s
467400K .......... .......... .......... .......... .......... 91% 47.3M 3s
467450K .......... .......... .......... .......... .......... 91% 41.8M 3s
467500K .......... .......... .......... .......... .......... 91% 42.1M 3s
467550K .......... .......... .......... .......... .......... 91% 47.5M 3s
467600K .......... .......... .......... .......... .......... 91% 37.9M 3s
467650K .......... .......... .......... .......... .......... 91% 38.0M 3s
467700K .......... .......... .......... .......... .......... 91% 53.7M 3s
467750K .......... .......... .......... .......... .......... 91% 42.7M 3s
467800K .......... .......... .......... .......... .......... 91% 46.5M 3s
467850K .......... .......... .......... .......... .......... 91% 47.5M 3s
467900K .......... .......... .......... .......... .......... 91% 56.8M 3s
467950K .......... .......... .......... .......... .......... 91% 37.7M 3s
468000K .......... .......... .......... .......... .......... 91% 54.3M 3s
468050K .......... .......... .......... .......... .......... 91% 42.8M 3s
468100K .......... .......... .......... .......... .......... 91% 47.3M 3s
468150K .......... .......... .......... .......... .......... 91% 42.7M 3s
468200K .......... .......... .......... .......... .......... 91% 53.2M 3s
468250K .......... .......... .......... .......... .......... 91% 48.5M 3s
468300K .......... .......... .......... .......... .......... 91% 52.1M 3s
468350K .......... .......... .......... .......... .......... 91% 42.2M 3s
468400K .......... .......... .......... .......... .......... 91% 30.2M 3s
468450K .......... .......... .......... .......... .......... 91% 42.6M 3s
468500K .......... .......... .......... .......... .......... 91% 52.8M 3s
468550K .......... .......... .......... .......... .......... 91% 43.5M 3s
468600K .......... .......... .......... .......... .......... 91% 34.5M 3s
468650K .......... .......... .......... .......... .......... 91% 41.8M 3s
468700K .......... .......... .......... .......... .......... 91% 53.1M 3s
468750K .......... .......... .......... .......... .......... 91% 25.8M 3s
468800K .......... .......... .......... .......... .......... 91% 37.7M 3s
468850K .......... .......... .......... .......... .......... 91% 77.8M 3s
468900K .......... .......... .......... .......... .......... 91% 14.6M 3s
468950K .......... .......... .......... .......... .......... 91% 95.9M 3s
469000K .......... .......... .......... .......... .......... 92% 43.2M 3s
469050K .......... .......... .......... .......... .......... 92% 77.5M 3s
469100K .......... .......... .......... .......... .......... 92%  282M 3s
469150K .......... .......... .......... .......... .......... 92% 30.2M 3s
469200K .......... .......... .......... .......... .......... 92% 52.4M 3s
469250K .......... .......... .......... .......... .......... 92% 65.7M 3s
469300K .......... .......... .......... .......... .......... 92% 37.6M 3s
469350K .......... .......... .......... .......... .......... 92% 46.5M 3s
469400K .......... .......... .......... .......... .......... 92% 35.6M 3s
469450K .......... .......... .......... .......... .......... 92% 38.0M 3s
469500K .......... .......... .......... .......... .......... 92% 45.7M 3s
469550K .......... .......... .......... .......... .......... 92% 31.9M 3s
469600K .......... .......... .......... .......... .......... 92% 29.1M 3s
469650K .......... .......... .......... .......... .......... 92% 35.3M 3s
469700K .......... .......... .......... .......... .......... 92% 38.0M 3s
469750K .......... .......... .......... .......... .......... 92% 41.2M 3s
469800K .......... .......... .......... .......... .......... 92% 43.6M 3s
469850K .......... .......... .......... .......... .......... 92% 31.8M 3s
469900K .......... .......... .......... .......... .......... 92% 47.7M 3s
469950K .......... .......... .......... .......... .......... 92% 37.9M 3s
470000K .......... .......... .......... .......... .......... 92% 38.5M 3s
470050K .......... .......... .......... .......... .......... 92% 34.9M 3s
470100K .......... .......... .......... .......... .......... 92% 42.1M 3s
470150K .......... .......... .......... .......... .......... 92% 41.9M 3s
470200K .......... .......... .......... .......... .......... 92% 25.5M 3s
470250K .......... .......... .......... .......... .......... 92% 46.8M 3s
470300K .......... .......... .......... .......... .......... 92% 47.4M 3s
470350K .......... .......... .......... .......... .......... 92% 42.4M 3s
470400K .......... .......... .......... .......... .......... 92% 27.9M 3s
470450K .......... .......... .......... .......... .......... 92% 46.2M 3s
470500K .......... .......... .......... .......... .......... 92% 33.9M 3s
470550K .......... .......... .......... .......... .......... 92% 45.7M 3s
470600K .......... .......... .......... .......... .......... 92% 30.4M 3s
470650K .......... .......... .......... .......... .......... 92% 33.2M 3s
470700K .......... .......... .......... .......... .......... 92% 13.2M 3s
470750K .......... .......... .......... .......... .......... 92%  170M 3s
470800K .......... .......... .......... .......... .......... 92% 61.0M 3s
470850K .......... .......... .......... .......... .......... 92% 34.3M 3s
470900K .......... .......... .......... .......... .......... 92% 83.3M 3s
470950K .......... .......... .......... .......... .......... 92% 33.1M 3s
471000K .......... .......... .......... .......... .......... 92% 51.1M 3s
471050K .......... .......... .......... .......... .......... 92% 65.9M 3s
471100K .......... .......... .......... .......... .......... 92% 39.6M 3s
471150K .......... .......... .......... .......... .......... 92% 41.0M 3s
471200K .......... .......... .......... .......... .......... 92% 25.6M 3s
471250K .......... .......... .......... .......... .......... 92% 42.0M 3s
471300K .......... .......... .......... .......... .......... 92% 38.6M 3s
471350K .......... .......... .......... .......... .......... 92% 25.8M 3s
471400K .......... .......... .......... .......... .......... 92% 38.8M 3s
471450K .......... .......... .......... .......... .......... 92% 38.9M 3s
471500K .......... .......... .......... .......... .......... 92% 24.7M 3s
471550K .......... .......... .......... .......... .......... 92% 39.2M 3s
471600K .......... .......... .......... .......... .......... 92% 36.5M 3s
471650K .......... .......... .......... .......... .......... 92% 27.8M 3s
471700K .......... .......... .......... .......... .......... 92% 38.9M 3s
471750K .......... .......... .......... .......... .......... 92% 42.6M 3s
471800K .......... .......... .......... .......... .......... 92% 38.8M 3s
471850K .......... .......... .......... .......... .......... 92% 25.6M 3s
471900K .......... .......... .......... .......... .......... 92% 39.0M 3s
471950K .......... .......... .......... .......... .......... 92% 31.2M 3s
472000K .......... .......... .......... .......... .......... 92% 37.9M 3s
472050K .......... .......... .......... .......... .......... 92% 33.4M 3s
472100K .......... .......... .......... .......... .......... 92% 32.0M 3s
472150K .......... .......... .......... .......... .......... 92% 41.5M 3s
472200K .......... .......... .......... .......... .......... 92% 23.3M 3s
472250K .......... .......... .......... .......... .......... 92% 39.7M 3s
472300K .......... .......... .......... .......... .......... 92% 88.1M 3s
472350K .......... .......... .......... .......... .......... 92% 28.9M 2s
472400K .......... .......... .......... .......... .......... 92% 37.1M 2s
472450K .......... .......... .......... .......... .......... 92% 12.0M 2s
472500K .......... .......... .......... .......... .......... 92%  128M 2s
472550K .......... .......... .......... .......... .......... 92%  129M 2s
472600K .......... .......... .......... .......... .......... 92% 39.9M 2s
472650K .......... .......... .......... .......... .......... 92% 33.6M 2s
472700K .......... .......... .......... .......... .......... 92%  117M 2s
472750K .......... .......... .......... .......... .......... 92% 41.2M 2s
472800K .......... .......... .......... .......... .......... 92% 52.6M 2s
472850K .......... .......... .......... .......... .......... 92% 42.9M 2s
472900K .......... .......... .......... .......... .......... 92% 50.9M 2s
472950K .......... .......... .......... .......... .......... 92% 66.2M 2s
473000K .......... .......... .......... .......... .......... 92% 36.0M 2s
473050K .......... .......... .......... .......... .......... 92% 35.7M 2s
473100K .......... .......... .......... .......... .......... 92% 34.5M 2s
473150K .......... .......... .......... .......... .......... 92% 34.4M 2s
473200K .......... .......... .......... .......... .......... 92% 31.6M 2s
473250K .......... .......... .......... .......... .......... 92% 37.7M 2s
473300K .......... .......... .......... .......... .......... 92% 9.43M 2s
473350K .......... .......... .......... .......... .......... 92% 40.6M 2s
473400K .......... .......... .......... .......... .......... 92% 42.0M 2s
473450K .......... .......... .......... .......... .......... 92% 27.1M 2s
473500K .......... .......... .......... .......... .......... 92% 46.2M 2s
473550K .......... .......... .......... .......... .......... 92% 36.6M 2s
473600K .......... .......... .......... .......... .......... 92% 26.9M 2s
473650K .......... .......... .......... .......... .......... 92% 37.6M 2s
473700K .......... .......... .......... .......... .......... 92% 23.5M 2s
473750K .......... .......... .......... .......... .......... 92% 51.0M 2s
473800K .......... .......... .......... .......... .......... 92% 42.8M 2s
473850K .......... .......... .......... .......... .......... 92% 32.2M 2s
473900K .......... .......... .......... .......... .......... 92% 41.1M 2s
473950K .......... .......... .......... .......... .......... 92% 24.8M 2s
474000K .......... .......... .......... .......... .......... 92% 38.2M 2s
474050K .......... .......... .......... .......... .......... 92% 29.2M 2s
474100K .......... .......... .......... .......... .......... 93% 52.4M 2s
474150K .......... .......... .......... .......... .......... 93% 34.9M 2s
474200K .......... .......... .......... .......... .......... 93% 48.3M 2s
474250K .......... .......... .......... .......... .......... 93% 37.9M 2s
474300K .......... .......... .......... .......... .......... 93% 15.5M 2s
474350K .......... .......... .......... .......... .......... 93%  157M 2s
474400K .......... .......... .......... .......... .......... 93%  242M 2s
474450K .......... .......... .......... .......... .......... 93% 12.1M 2s
474500K .......... .......... .......... .......... .......... 93%  448M 2s
474550K .......... .......... .......... .......... .......... 93%  452M 2s
474600K .......... .......... .......... .......... .......... 93% 27.1M 2s
474650K .......... .......... .......... .......... .......... 93% 83.9M 2s
474700K .......... .......... .......... .......... .......... 93% 40.1M 2s
474750K .......... .......... .......... .......... .......... 93% 53.2M 2s
474800K .......... .......... .......... .......... .......... 93% 48.4M 2s
474850K .......... .......... .......... .......... .......... 93% 34.1M 2s
474900K .......... .......... .......... .......... .......... 93% 47.4M 2s
474950K .......... .......... .......... .......... .......... 93% 27.2M 2s
475000K .......... .......... .......... .......... .......... 93% 42.8M 2s
475050K .......... .......... .......... .......... .......... 93% 38.3M 2s
475100K .......... .......... .......... .......... .......... 93% 35.0M 2s
475150K .......... .......... .......... .......... .......... 93% 53.4M 2s
475200K .......... .......... .......... .......... .......... 93% 34.8M 2s
475250K .......... .......... .......... .......... .......... 93% 39.3M 2s
475300K .......... .......... .......... .......... .......... 93% 37.4M 2s
475350K .......... .......... .......... .......... .......... 93% 38.7M 2s
475400K .......... .......... .......... .......... .......... 93% 40.9M 2s
475450K .......... .......... .......... .......... .......... 93% 23.8M 2s
475500K .......... .......... .......... .......... .......... 93% 47.9M 2s
475550K .......... .......... .......... .......... .......... 93% 36.7M 2s
475600K .......... .......... .......... .......... .......... 93% 24.9M 2s
475650K .......... .......... .......... .......... .......... 93% 43.9M 2s
475700K .......... .......... .......... .......... .......... 93% 32.9M 2s
475750K .......... .......... .......... .......... .......... 93% 30.2M 2s
475800K .......... .......... .......... .......... .......... 93% 22.0M 2s
475850K .......... .......... .......... .......... .......... 93% 27.2M 2s
475900K .......... .......... .......... .......... .......... 93% 42.4M 2s
475950K .......... .......... .......... .......... .......... 93% 46.8M 2s
476000K .......... .......... .......... .......... .......... 93% 93.9M 2s
476050K .......... .......... .......... .......... .......... 93% 20.2M 2s
476100K .......... .......... .......... .......... .......... 93% 95.4M 2s
476150K .......... .......... .......... .......... .......... 93% 75.7M 2s
476200K .......... .......... .......... .......... .......... 93%  356M 2s
476250K .......... .......... .......... .......... .......... 93% 53.7M 2s
476300K .......... .......... .......... .......... .......... 93% 57.0M 2s
476350K .......... .......... .......... .......... .......... 93% 42.9M 2s
476400K .......... .......... .......... .......... .......... 93%  483M 2s
476450K .......... .......... .......... .......... .......... 93% 72.7M 2s
476500K .......... .......... .......... .......... .......... 93% 53.7M 2s
476550K .......... .......... .......... .......... .......... 93% 54.1M 2s
476600K .......... .......... .......... .......... .......... 93% 34.4M 2s
476650K .......... .......... .......... .......... .......... 93% 46.9M 2s
476700K .......... .......... .......... .......... .......... 93% 35.1M 2s
476750K .......... .......... .......... .......... .......... 93% 53.2M 2s
476800K .......... .......... .......... .......... .......... 93% 54.3M 2s
476850K .......... .......... .......... .......... .......... 93% 45.8M 2s
476900K .......... .......... .......... .......... .......... 93% 38.0M 2s
476950K .......... .......... .......... .......... .......... 93% 42.9M 2s
477000K .......... .......... .......... .......... .......... 93% 54.6M 2s
477050K .......... .......... .......... .......... .......... 93% 42.1M 2s
477100K .......... .......... .......... .......... .......... 93% 38.1M 2s
477150K .......... .......... .......... .......... .......... 93% 47.6M 2s
477200K .......... .......... .......... .......... .......... 93% 41.7M 2s
477250K .......... .......... .......... .......... .......... 93% 56.0M 2s
477300K .......... .......... .......... .......... .......... 93% 42.3M 2s
477350K .......... .......... .......... .......... .......... 93% 47.7M 2s
477400K .......... .......... .......... .......... .......... 93% 42.1M 2s
477450K .......... .......... .......... .......... .......... 93% 38.2M 2s
477500K .......... .......... .......... .......... .......... 93% 47.4M 2s
477550K .......... .......... .......... .......... .......... 93% 48.1M 2s
477600K .......... .......... .......... .......... .......... 93% 47.9M 2s
477650K .......... .......... .......... .......... .......... 93% 54.7M 2s
477700K .......... .......... .......... .......... .......... 93% 29.3M 2s
477750K .......... .......... .......... .......... .......... 93% 54.1M 2s
477800K .......... .......... .......... .......... .......... 93% 54.6M 2s
477850K .......... .......... .......... .......... .......... 93% 31.9M 2s
477900K .......... .......... .......... .......... .......... 93% 46.3M 2s
477950K .......... .......... .......... .......... .......... 93% 49.3M 2s
478000K .......... .......... .......... .......... .......... 93% 53.4M 2s
478050K .......... .......... .......... .......... .......... 93% 42.1M 2s
478100K .......... .......... .......... .......... .......... 93% 29.4M 2s
478150K .......... .......... .......... .......... .......... 93% 14.1M 2s
478200K .......... .......... .......... .......... .......... 93%  503M 2s
478250K .......... .......... .......... .......... .......... 93% 81.5M 2s
478300K .......... .......... .......... .......... .......... 93% 68.1M 2s
478350K .......... .......... .......... .......... .......... 93% 45.7M 2s
478400K .......... .......... .......... .......... .......... 93% 43.5M 2s
478450K .......... .......... .......... .......... .......... 93%  397M 2s
478500K .......... .......... .......... .......... .......... 93% 54.4M 2s
478550K .......... .......... .......... .......... .......... 93% 47.6M 2s
478600K .......... .......... .......... .......... .......... 93% 29.5M 2s
478650K .......... .......... .......... .......... .......... 93% 46.7M 2s
478700K .......... .......... .......... .......... .......... 93% 42.6M 2s
478750K .......... .......... .......... .......... .......... 93% 48.3M 2s
478800K .......... .......... .......... .......... .......... 93% 38.5M 2s
478850K .......... .......... .......... .......... .......... 93% 41.7M 2s
478900K .......... .......... .......... .......... .......... 93% 35.3M 2s
478950K .......... .......... .......... .......... .......... 93% 42.3M 2s
479000K .......... .......... .......... .......... .......... 93% 51.9M 2s
479050K .......... .......... .......... .......... .......... 93% 39.2M 2s
479100K .......... .......... .......... .......... .......... 93% 29.2M 2s
479150K .......... .......... .......... .......... .......... 93% 41.3M 2s
479200K .......... .......... .......... .......... .......... 94% 42.5M 2s
479250K .......... .......... .......... .......... .......... 94% 42.3M 2s
479300K .......... .......... .......... .......... .......... 94% 37.8M 2s
479350K .......... .......... .......... .......... .......... 94% 41.2M 2s
479400K .......... .......... .......... .......... .......... 94% 56.1M 2s
479450K .......... .......... .......... .......... .......... 94% 35.0M 2s
479500K .......... .......... .......... .......... .......... 94% 42.0M 2s
479550K .......... .......... .......... .......... .......... 94% 46.4M 2s
479600K .......... .......... .......... .......... .......... 94% 39.1M 2s
479650K .......... .......... .......... .......... .......... 94% 53.6M 2s
479700K .......... .......... .......... .......... .......... 94% 35.2M 2s
479750K .......... .......... .......... .......... .......... 94% 52.7M 2s
479800K .......... .......... .......... .......... .......... 94% 55.2M 2s
479850K .......... .......... .......... .......... .......... 94% 31.3M 2s
479900K .......... .......... .......... .......... .......... 94% 47.7M 2s
479950K .......... .......... .......... .......... .......... 94% 41.7M 2s
480000K .......... .......... .......... .......... .......... 94% 48.1M 2s
480050K .......... .......... .......... .......... .......... 94% 29.4M 2s
480100K .......... .......... .......... .......... .......... 94%  117M 2s
480150K .......... .......... .......... .......... .......... 94% 12.5M 2s
480200K .......... .......... .......... .......... .......... 94%  440M 2s
480250K .......... .......... .......... .......... .......... 94% 88.5M 2s
480300K .......... .......... .......... .......... .......... 94%  465M 2s
480350K .......... .......... .......... .......... .......... 94% 25.7M 2s
480400K .......... .......... .......... .......... .......... 94%  114M 2s
480450K .......... .......... .......... .......... .......... 94% 38.2M 2s
480500K .......... .......... .......... .......... .......... 94% 35.2M 2s
480550K .......... .......... .......... .......... .......... 94%  191M 2s
480600K .......... .......... .......... .......... .......... 94% 29.1M 2s
480650K .......... .......... .......... .......... .......... 94% 38.0M 2s
480700K .......... .......... .......... .......... .......... 94% 29.5M 2s
480750K .......... .......... .......... .......... .......... 94% 46.7M 2s
480800K .......... .......... .......... .......... .......... 94% 34.7M 2s
480850K .......... .......... .......... .......... .......... 94% 34.6M 2s
480900K .......... .......... .......... .......... .......... 94% 29.2M 2s
480950K .......... .......... .......... .......... .......... 94% 42.3M 2s
481000K .......... .......... .......... .......... .......... 94% 38.1M 2s
481050K .......... .......... .......... .......... .......... 94% 31.7M 2s
481100K .......... .......... .......... .......... .......... 94% 29.3M 2s
481150K .......... .......... .......... .......... .......... 94% 34.8M 2s
481200K .......... .......... .......... .......... .......... 94% 34.2M 2s
481250K .......... .......... .......... .......... .......... 94% 37.1M 2s
481300K .......... .......... .......... .......... .......... 94% 41.4M 2s
481350K .......... .......... .......... .......... .......... 94% 25.4M 2s
481400K .......... .......... .......... .......... .......... 94% 46.5M 2s
481450K .......... .......... .......... .......... .......... 94% 27.6M 2s
481500K .......... .......... .......... .......... .......... 94% 37.4M 2s
481550K .......... .......... .......... .......... .......... 94% 34.8M 2s
481600K .......... .......... .......... .......... .......... 94% 29.3M 2s
481650K .......... .......... .......... .......... .......... 94% 32.0M 2s
481700K .......... .......... .......... .......... .......... 94% 34.2M 2s
481750K .......... .......... .......... .......... .......... 94% 35.2M 2s
481800K .......... .......... .......... .......... .......... 94% 63.6M 2s
481850K .......... .......... .......... .......... .......... 94% 31.8M 2s
481900K .......... .......... .......... .......... .......... 94% 63.0M 2s
481950K .......... .......... .......... .......... .......... 94% 11.7M 2s
482000K .......... .......... .......... .......... .......... 94%  574M 2s
482050K .......... .......... .......... .......... .......... 94%  444M 2s
482100K .......... .......... .......... .......... .......... 94% 20.3M 2s
482150K .......... .......... .......... .......... .......... 94%  555M 2s
482200K .......... .......... .......... .......... .......... 94% 27.6M 2s
482250K .......... .......... .......... .......... .......... 94% 29.5M 2s
482300K .......... .......... .......... .......... .......... 94% 39.2M 2s
482350K .......... .......... .......... .......... .......... 94% 25.1M 2s
482400K .......... .......... .......... .......... .......... 94% 22.4M 2s
482450K .......... .......... .......... .......... .......... 94% 22.1M 2s
482500K .......... .......... .......... .......... .......... 94% 20.3M 2s
482550K .......... .......... .......... .......... .......... 94% 23.1M 2s
482600K .......... .......... .......... .......... .......... 94% 23.3M 2s
482650K .......... .......... .......... .......... .......... 94% 27.8M 2s
482700K .......... .......... .......... .......... .......... 94% 20.5M 2s
482750K .......... .......... .......... .......... .......... 94% 23.4M 2s
482800K .......... .......... .......... .......... .......... 94% 31.4M 2s
482850K .......... .......... .......... .......... .......... 94% 22.2M 2s
482900K .......... .......... .......... .......... .......... 94% 23.6M 2s
482950K .......... .......... .......... .......... .......... 94% 27.1M 2s
483000K .......... .......... .......... .......... .......... 94% 23.9M 2s
483050K .......... .......... .......... .......... .......... 94% 27.2M 2s
483100K .......... .......... .......... .......... .......... 94% 25.4M 2s
483150K .......... .......... .......... .......... .......... 94% 20.9M 2s
483200K .......... .......... .......... .......... .......... 94% 62.8M 2s
483250K .......... .......... .......... .......... .......... 94% 13.3M 2s
483300K .......... .......... .......... .......... .......... 94%  113M 2s
483350K .......... .......... .......... .......... .......... 94%  116M 2s
483400K .......... .......... .......... .......... .......... 94% 20.7M 2s
483450K .......... .......... .......... .......... .......... 94% 37.4M 2s
483500K .......... .......... .......... .......... .......... 94% 49.9M 2s
483550K .......... .......... .......... .......... .......... 94% 45.4M 2s
483600K .......... .......... .......... .......... .......... 94% 24.9M 2s
483650K .......... .......... .......... .......... .......... 94% 44.4M 2s
483700K .......... .......... .......... .......... .......... 94% 22.4M 2s
483750K .......... .......... .......... .......... .......... 94% 39.4M 2s
483800K .......... .......... .......... .......... .......... 94% 39.7M 2s
483850K .......... .......... .......... .......... .......... 94% 22.3M 2s
483900K .......... .......... .......... .......... .......... 94% 37.0M 2s
483950K .......... .......... .......... .......... .......... 94% 32.1M 2s
484000K .......... .......... .......... .......... .......... 94% 28.7M 2s
484050K .......... .......... .......... .......... .......... 94% 31.2M 2s
484100K .......... .......... .......... .......... .......... 94% 30.2M 2s
484150K .......... .......... .......... .......... .......... 94% 31.7M 2s
484200K .......... .......... .......... .......... .......... 94% 31.3M 2s
484250K .......... .......... .......... .......... .......... 94% 37.1M 2s
484300K .......... .......... .......... .......... .......... 95% 34.2M 2s
484350K .......... .......... .......... .......... .......... 95% 23.6M 2s
484400K .......... .......... .......... .......... .......... 95% 47.7M 2s
484450K .......... .......... .......... .......... .......... 95% 33.9M 2s
484500K .......... .......... .......... .......... .......... 95% 23.5M 2s
484550K .......... .......... .......... .......... .......... 95% 44.3M 2s
484600K .......... .......... .......... .......... .......... 95% 37.3M 2s
484650K .......... .......... .......... .......... .......... 95% 26.7M 2s
484700K .......... .......... .......... .......... .......... 95% 29.6M 2s
484750K .......... .......... .......... .......... .......... 95% 27.4M 2s
484800K .......... .......... .......... .......... .......... 95% 59.0M 2s
484850K .......... .......... .......... .......... .......... 95% 11.0M 2s
484900K .......... .......... .......... .......... .......... 95%  128M 2s
484950K .......... .......... .......... .......... .......... 95%  124M 2s
485000K .......... .......... .......... .......... .......... 95% 19.8M 2s
485050K .......... .......... .......... .......... .......... 95%  131M 2s
485100K .......... .......... .......... .......... .......... 95% 23.9M 2s
485150K .......... .......... .......... .......... .......... 95% 32.1M 2s
485200K .......... .......... .......... .......... .......... 95% 42.2M 2s
485250K .......... .......... .......... .......... .......... 95% 26.6M 2s
485300K .......... .......... .......... .......... .......... 95% 35.9M 2s
485350K .......... .......... .......... .......... .......... 95% 22.7M 2s
485400K .......... .......... .......... .......... .......... 95% 38.4M 2s
485450K .......... .......... .......... .......... .......... 95% 21.0M 2s
485500K .......... .......... .......... .......... .......... 95% 38.4M 2s
485550K .......... .......... .......... .......... .......... 95% 22.2M 2s
485600K .......... .......... .......... .......... .......... 95% 23.8M 2s
485650K .......... .......... .......... .......... .......... 95% 33.4M 2s
485700K .......... .......... .......... .......... .......... 95% 23.0M 2s
485750K .......... .......... .......... .......... .......... 95% 23.7M 2s
485800K .......... .......... .......... .......... .......... 95% 41.0M 2s
485850K .......... .......... .......... .......... .......... 95% 22.4M 2s
485900K .......... .......... .......... .......... .......... 95% 34.7M 2s
485950K .......... .......... .......... .......... .......... 95% 23.9M 2s
486000K .......... .......... .......... .......... .......... 95% 34.1M 2s
486050K .......... .......... .......... .......... .......... 95% 34.9M 2s
486100K .......... .......... .......... .......... .......... 95% 25.0M 2s
486150K .......... .......... .......... .......... .......... 95% 25.5M 2s
486200K .......... .......... .......... .......... .......... 95% 31.0M 2s
486250K .......... .......... .......... .......... .......... 95% 24.8M 2s
486300K .......... .......... .......... .......... .......... 95% 92.5M 2s
486350K .......... .......... .......... .......... .......... 95% 11.2M 2s
486400K .......... .......... .......... .......... .......... 95%  132M 2s
486450K .......... .......... .......... .......... .......... 95%  115M 2s
486500K .......... .......... .......... .......... .......... 95%  144M 2s
486550K .......... .......... .......... .......... .......... 95%  122M 2s
486600K .......... .......... .......... .......... .......... 95% 43.4M 2s
486650K .......... .......... .......... .......... .......... 95%  120M 2s
486700K .......... .......... .......... .......... .......... 95%  102M 2s
486750K .......... .......... .......... .......... .......... 95% 54.9M 2s
486800K .......... .......... .......... .......... .......... 95% 54.4M 2s
486850K .......... .......... .......... .......... .......... 95% 44.0M 2s
486900K .......... .......... .......... .......... .......... 95% 40.8M 1s
486950K .......... .......... .......... .......... .......... 95% 40.2M 1s
487000K .......... .......... .......... .......... .......... 95% 62.7M 1s
487050K .......... .......... .......... .......... .......... 95% 56.7M 1s
487100K .......... .......... .......... .......... .......... 95% 32.8M 1s
487150K .......... .......... .......... .......... .......... 95% 46.5M 1s
487200K .......... .......... .......... .......... .......... 95% 47.1M 1s
487250K .......... .......... .......... .......... .......... 95% 54.7M 1s
487300K .......... .......... .......... .......... .......... 95% 48.0M 1s
487350K .......... .......... .......... .......... .......... 95% 47.9M 1s
487400K .......... .......... .......... .......... .......... 95% 46.3M 1s
487450K .......... .......... .......... .......... .......... 95% 45.8M 1s
487500K .......... .......... .......... .......... .......... 95% 47.2M 1s
487550K .......... .......... .......... .......... .......... 95% 57.5M 1s
487600K .......... .......... .......... .......... .......... 95% 41.2M 1s
487650K .......... .......... .......... .......... .......... 95% 48.2M 1s
487700K .......... .......... .......... .......... .......... 95% 47.3M 1s
487750K .......... .......... .......... .......... .......... 95% 44.3M 1s
487800K .......... .......... .......... .......... .......... 95% 45.7M 1s
487850K .......... .......... .......... .......... .......... 95% 55.5M 1s
487900K .......... .......... .......... .......... .......... 95% 63.1M 1s
487950K .......... .......... .......... .......... .......... 95% 47.3M 1s
488000K .......... .......... .......... .......... .......... 95% 53.9M 1s
488050K .......... .......... .......... .......... .......... 95% 53.8M 1s
488100K .......... .......... .......... .......... .......... 95% 53.4M 1s
488150K .......... .......... .......... .......... .......... 95% 48.6M 1s
488200K .......... .......... .......... .......... .......... 95% 52.2M 1s
488250K .......... .......... .......... .......... .......... 95% 48.8M 1s
488300K .......... .......... .......... .......... .......... 95% 62.4M 1s
488350K .......... .......... .......... .......... .......... 95% 48.9M 1s
488400K .......... .......... .......... .......... .......... 95% 61.7M 1s
488450K .......... .......... .......... .......... .......... 95% 42.9M 1s
488500K .......... .......... .......... .......... .......... 95% 48.2M 1s
488550K .......... .......... .......... .......... .......... 95% 17.3M 1s
488600K .......... .......... .......... .......... .......... 95%  332M 1s
488650K .......... .......... .......... .......... .......... 95%  309M 1s
488700K .......... .......... .......... .......... .......... 95% 40.0M 1s
488750K .......... .......... .......... .......... .......... 95% 44.5M 1s
488800K .......... .......... .......... .......... .......... 95%  161M 1s
488850K .......... .......... .......... .......... .......... 95% 25.0M 1s
488900K .......... .......... .......... .......... .......... 95%  168M 1s
488950K .......... .......... .......... .......... .......... 95%  154M 1s
489000K .......... .......... .......... .......... .......... 95%  182M 1s
489050K .......... .......... .......... .......... .......... 95% 79.5M 1s
489100K .......... .......... .......... .......... .......... 95% 59.2M 1s
489150K .......... .......... .......... .......... .......... 95% 58.1M 1s
489200K .......... .......... .......... .......... .......... 95% 45.0M 1s
489250K .......... .......... .......... .......... .......... 95% 47.5M 1s
489300K .......... .......... .......... .......... .......... 95% 53.0M 1s
489350K .......... .......... .......... .......... .......... 95% 42.7M 1s
489400K .......... .......... .......... .......... .......... 96% 62.8M 1s
489450K .......... .......... .......... .......... .......... 96% 51.1M 1s
489500K .......... .......... .......... .......... .......... 96% 48.6M 1s
489550K .......... .......... .......... .......... .......... 96% 54.9M 1s
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489650K .......... .......... .......... .......... .......... 96% 48.7M 1s
489700K .......... .......... .......... .......... .......... 96% 54.1M 1s
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489800K .......... .......... .......... .......... .......... 96% 54.1M 1s
489850K .......... .......... .......... .......... .......... 96% 47.5M 1s
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489950K .......... .......... .......... .......... .......... 96% 41.9M 1s
490000K .......... .......... .......... .......... .......... 96% 53.1M 1s
490050K .......... .......... .......... .......... .......... 96% 47.7M 1s
490100K .......... .......... .......... .......... .......... 96% 47.1M 1s
490150K .......... .......... .......... .......... .......... 96% 54.1M 1s
490200K .......... .......... .......... .......... .......... 96% 49.0M 1s
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490300K .......... .......... .......... .......... .......... 96% 54.5M 1s
490350K .......... .......... .......... .......... .......... 96% 45.7M 1s
490400K .......... .......... .......... .......... .......... 96% 48.1M 1s
490450K .......... .......... .......... .......... .......... 96% 53.6M 1s
490500K .......... .......... .......... .......... .......... 96% 48.1M 1s
490550K .......... .......... .......... .......... .......... 96% 54.7M 1s
490600K .......... .......... .......... .......... .......... 96% 63.2M 1s
490650K .......... .......... .......... .......... .......... 96% 47.2M 1s
490700K .......... .......... .......... .......... .......... 96% 48.3M 1s
490750K .......... .......... .......... .......... .......... 96% 45.9M 1s
490800K .......... .......... .......... .......... .......... 96% 47.9M 1s
490850K .......... .......... .......... .......... .......... 96% 91.6M 1s
490900K .......... .......... .......... .......... .......... 96% 63.0M 1s
490950K .......... .......... .......... .......... .......... 96% 53.5M 1s
491000K .......... .......... .......... .......... .......... 96% 17.2M 1s
491050K .......... .......... .......... .......... .......... 96% 69.0M 1s
491100K .......... .......... .......... .......... .......... 96%  381M 1s
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491200K .......... .......... .......... .......... .......... 96% 27.8M 1s
491250K .......... .......... .......... .......... .......... 96%  543M 1s
491300K .......... .......... .......... .......... .......... 96% 46.0M 1s
491350K .......... .......... .......... .......... .......... 96%  461M 1s
491400K .......... .......... .......... .......... .......... 96% 30.6M 1s
491450K .......... .......... .......... .......... .......... 96% 65.7M 1s
491500K .......... .......... .......... .......... .......... 96% 41.5M 1s
491550K .......... .......... .......... .......... .......... 96%  509M 1s
491600K .......... .......... .......... .......... .......... 96% 73.3M 1s
491650K .......... .......... .......... .......... .......... 96% 61.0M 1s
491700K .......... .......... .......... .......... .......... 96% 29.7M 1s
491750K .......... .......... .......... .......... .......... 96% 53.7M 1s
491800K .......... .......... .......... .......... .......... 96% 54.0M 1s
491850K .......... .......... .......... .......... .......... 96% 47.4M 1s
491900K .......... .......... .......... .......... .......... 96% 47.7M 1s
491950K .......... .......... .......... .......... .......... 96% 35.0M 1s
492000K .......... .......... .......... .......... .......... 96% 52.2M 1s
492050K .......... .......... .......... .......... .......... 96% 38.7M 1s
492100K .......... .......... .......... .......... .......... 96% 34.7M 1s
492150K .......... .......... .......... .......... .......... 96% 42.2M 1s
492200K .......... .......... .......... .......... .......... 96% 46.0M 1s
492250K .......... .......... .......... .......... .......... 96% 39.0M 1s
492300K .......... .......... .......... .......... .......... 96% 54.4M 1s
492350K .......... .......... .......... .......... .......... 96% 39.2M 1s
492400K .......... .......... .......... .......... .......... 96% 38.7M 1s
492450K .......... .......... .......... .......... .......... 96% 28.6M 1s
492500K .......... .......... .......... .......... .......... 96% 47.6M 1s
492550K .......... .......... .......... .......... .......... 96% 51.9M 1s
492600K .......... .......... .......... .......... .......... 96% 38.7M 1s
492650K .......... .......... .......... .......... .......... 96% 48.2M 1s
492700K .......... .......... .......... .......... .......... 96% 34.2M 1s
492750K .......... .......... .......... .......... .......... 96% 53.3M 1s
492800K .......... .......... .......... .......... .......... 96% 32.1M 1s
492850K .......... .......... .......... .......... .......... 96% 61.2M 1s
492900K .......... .......... .......... .......... .......... 96% 60.7M 1s
492950K .......... .......... .......... .......... .......... 96% 32.3M 1s
493000K .......... .......... .......... .......... .......... 96% 47.3M 1s
493050K .......... .......... .......... .......... .......... 96% 55.0M 1s
493100K .......... .......... .......... .......... .......... 96% 34.2M 1s
493150K .......... .......... .......... .......... .......... 96% 38.6M 1s
493200K .......... .......... .......... .......... .......... 96% 12.1M 1s
493250K .......... .......... .......... .......... .......... 96%  164M 1s
493300K .......... .......... .......... .......... .......... 96%  168M 1s
493350K .......... .......... .......... .......... .......... 96% 34.1M 1s
493400K .......... .......... .......... .......... .......... 96% 25.8M 1s
493450K .......... .......... .......... .......... .......... 96%  177M 1s
493500K .......... .......... .......... .......... .......... 96%  192M 1s
493550K .......... .......... .......... .......... .......... 96%  187M 1s
493600K .......... .......... .......... .......... .......... 96% 28.1M 1s
493650K .......... .......... .......... .......... .......... 96%  206M 1s
493700K .......... .......... .......... .......... .......... 96%  162M 1s
493750K .......... .......... .......... .......... .......... 96% 39.8M 1s
493800K .......... .......... .......... .......... .......... 96% 36.8M 1s
493850K .......... .......... .......... .......... .......... 96% 37.0M 1s
493900K .......... .......... .......... .......... .......... 96% 28.8M 1s
493950K .......... .......... .......... .......... .......... 96% 34.1M 1s
494000K .......... .......... .......... .......... .......... 96% 26.2M 1s
494050K .......... .......... .......... .......... .......... 96% 38.3M 1s
494100K .......... .......... .......... .......... .......... 96% 24.7M 1s
494150K .......... .......... .......... .......... .......... 96% 37.9M 1s
494200K .......... .......... .......... .......... .......... 96% 28.4M 1s
494250K .......... .......... .......... .......... .......... 96% 34.6M 1s
494300K .......... .......... .......... .......... .......... 96% 36.9M 1s
494350K .......... .......... .......... .......... .......... 96% 29.0M 1s
494400K .......... .......... .......... .......... .......... 96% 31.1M 1s
494450K .......... .......... .......... .......... .......... 96% 36.5M 1s
494500K .......... .......... .......... .......... .......... 97% 25.8M 1s
494550K .......... .......... .......... .......... .......... 97% 38.7M 1s
494600K .......... .......... .......... .......... .......... 97% 23.2M 1s
494650K .......... .......... .......... .......... .......... 97% 35.3M 1s
494700K .......... .......... .......... .......... .......... 97% 24.8M 1s
494750K .......... .......... .......... .......... .......... 97% 39.0M 1s
494800K .......... .......... .......... .......... .......... 97% 32.1M 1s
494850K .......... .......... .......... .......... .......... 97% 14.9M 1s
494900K .......... .......... .......... .......... .......... 97% 21.1M 1s
494950K .......... .......... .......... .......... .......... 97% 16.0M 1s
495000K .......... .......... .......... .......... .......... 97%  166M 1s
495050K .......... .......... .......... .......... .......... 97% 21.5M 1s
495100K .......... .......... .......... .......... .......... 97% 33.8M 1s
495150K .......... .......... .......... .......... .......... 97% 23.2M 1s
495200K .......... .......... .......... .......... .......... 97% 28.1M 1s
495250K .......... .......... .......... .......... .......... 97% 22.8M 1s
495300K .......... .......... .......... .......... .......... 97% 28.2M 1s
495350K .......... .......... .......... .......... .......... 97% 18.5M 1s
495400K .......... .......... .......... .......... .......... 97% 26.9M 1s
495450K .......... .......... .......... .......... .......... 97% 20.0M 1s
495500K .......... .......... .......... .......... .......... 97% 26.5M 1s
495550K .......... .......... .......... .......... .......... 97% 21.5M 1s
495600K .......... .......... .......... .......... .......... 97% 21.3M 1s
495650K .......... .......... .......... .......... .......... 97% 23.4M 1s
495700K .......... .......... .......... .......... .......... 97% 24.5M 1s
495750K .......... .......... .......... .......... .......... 97% 19.4M 1s
495800K .......... .......... .......... .......... .......... 97% 18.9M 1s
495850K .......... .......... .......... .......... .......... 97% 15.1M 1s
495900K .......... .......... .......... .......... .......... 97% 27.9M 1s
495950K .......... .......... .......... .......... .......... 97% 20.7M 1s
496000K .......... .......... .......... .......... .......... 97% 15.4M 1s
496050K .......... .......... .......... .......... .......... 97% 37.3M 1s
496100K .......... .......... .......... .......... .......... 97%  112M 1s
496150K .......... .......... .......... .......... .......... 97% 17.6M 1s
496200K .......... .......... .......... .......... .......... 97% 97.9M 1s
496250K .......... .......... .......... .......... .......... 97% 20.3M 1s
496300K .......... .......... .......... .......... .......... 97% 49.2M 1s
496350K .......... .......... .......... .......... .......... 97% 23.9M 1s
496400K .......... .......... .......... .......... .......... 97% 30.2M 1s
496450K .......... .......... .......... .......... .......... 97% 24.5M 1s
496500K .......... .......... .......... .......... .......... 97% 25.8M 1s
496550K .......... .......... .......... .......... .......... 97% 37.7M 1s
496600K .......... .......... .......... .......... .......... 97% 24.7M 1s
496650K .......... .......... .......... .......... .......... 97% 34.9M 1s
496700K .......... .......... .......... .......... .......... 97% 26.5M 1s
496750K .......... .......... .......... .......... .......... 97% 30.3M 1s
496800K .......... .......... .......... .......... .......... 97% 26.8M 1s
496850K .......... .......... .......... .......... .......... 97% 23.0M 1s
496900K .......... .......... .......... .......... .......... 97% 27.2M 1s
496950K .......... .......... .......... .......... .......... 97% 22.6M 1s
497000K .......... .......... .......... .......... .......... 97% 24.0M 1s
497050K .......... .......... .......... .......... .......... 97% 31.8M 1s
497100K .......... .......... .......... .......... .......... 97% 24.2M 1s
497150K .......... .......... .......... .......... .......... 97% 20.6M 1s
497200K .......... .......... .......... .......... .......... 97% 23.7M 1s
497250K .......... .......... .......... .......... .......... 97% 36.7M 1s
497300K .......... .......... .......... .......... .......... 97% 33.9M 1s
497350K .......... .......... .......... .......... .......... 97% 9.10M 1s
497400K .......... .......... .......... .......... .......... 97%  132M 1s
497450K .......... .......... .......... .......... .......... 97% 38.8M 1s
497500K .......... .......... .......... .......... .......... 97% 26.2M 1s
497550K .......... .......... .......... .......... .......... 97% 66.3M 1s
497600K .......... .......... .......... .......... .......... 97% 39.6M 1s
497650K .......... .......... .......... .......... .......... 97% 30.9M 1s
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497800K .......... .......... .......... .......... .......... 97% 29.1M 1s
497850K .......... .......... .......... .......... .......... 97% 24.2M 1s
497900K .......... .......... .......... .......... .......... 97% 29.2M 1s
497950K .......... .......... .......... .......... .......... 97% 27.1M 1s
498000K .......... .......... .......... .......... .......... 97% 30.0M 1s
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498100K .......... .......... .......... .......... .......... 97% 26.1M 1s
498150K .......... .......... .......... .......... .......... 97% 38.2M 1s
498200K .......... .......... .......... .......... .......... 97% 22.5M 1s
498250K .......... .......... .......... .......... .......... 97% 30.2M 1s
498300K .......... .......... .......... .......... .......... 97% 20.9M 1s
498350K .......... .......... .......... .......... .......... 97% 20.8M 1s
498400K .......... .......... .......... .......... .......... 97% 31.8M 1s
498450K .......... .......... .......... .......... .......... 97% 20.0M 1s
498500K .......... .......... .......... .......... .......... 97% 35.0M 1s
498550K .......... .......... .......... .......... .......... 97% 29.1M 1s
498600K .......... .......... .......... .......... .......... 97% 21.1M 1s
498650K .......... .......... .......... .......... .......... 97% 11.2M 1s
498700K .......... .......... .......... .......... .......... 97% 80.6M 1s
498750K .......... .......... .......... .......... .......... 97% 91.4M 1s
498800K .......... .......... .......... .......... .......... 97%  110M 1s
498850K .......... .......... .......... .......... .......... 97% 93.4M 1s
498900K .......... .......... .......... .......... .......... 97% 15.6M 1s
498950K .......... .......... .......... .......... .......... 97%  101M 1s
499000K .......... .......... .......... .......... .......... 97%  112M 1s
499050K .......... .......... .......... .......... .......... 97%  118M 1s
499100K .......... .......... .......... .......... .......... 97% 92.5M 1s
499150K .......... .......... .......... .......... .......... 97% 53.1M 1s
499200K .......... .......... .......... .......... .......... 97% 38.2M 1s
499250K .......... .......... .......... .......... .......... 97% 24.5M 1s
499300K .......... .......... .......... .......... .......... 97% 31.2M 1s
499350K .......... .......... .......... .......... .......... 97% 33.6M 1s
499400K .......... .......... .......... .......... .......... 97% 22.5M 1s
499450K .......... .......... .......... .......... .......... 97% 37.4M 1s
499500K .......... .......... .......... .......... .......... 97% 41.2M 1s
499550K .......... .......... .......... .......... .......... 97% 26.8M 1s
499600K .......... .......... .......... .......... .......... 98% 36.9M 1s
499650K .......... .......... .......... .......... .......... 98% 25.2M 1s
499700K .......... .......... .......... .......... .......... 98% 33.9M 1s
499750K .......... .......... .......... .......... .......... 98% 36.8M 1s
499800K .......... .......... .......... .......... .......... 98% 24.0M 1s
499850K .......... .......... .......... .......... .......... 98% 29.8M 1s
499900K .......... .......... .......... .......... .......... 98% 41.1M 1s
499950K .......... .......... .......... .......... .......... 98% 26.2M 1s
500000K .......... .......... .......... .......... .......... 98% 37.2M 1s
500050K .......... .......... .......... .......... .......... 98% 33.7M 1s
500100K .......... .......... .......... .......... .......... 98% 32.4M 1s
500150K .......... .......... .......... .......... .......... 98% 21.9M 1s
500200K .......... .......... .......... .......... .......... 98% 93.7M 1s
500250K .......... .......... .......... .......... .......... 98% 29.3M 1s
500300K .......... .......... .......... .......... .......... 98% 23.7M 1s
500350K .......... .......... .......... .......... .......... 98% 17.2M 1s
500400K .......... .......... .......... .......... .......... 98% 41.5M 1s
500450K .......... .......... .......... .......... .......... 98% 93.4M 1s
500500K .......... .......... .......... .......... .......... 98% 64.7M 1s
500550K .......... .......... .......... .......... .......... 98% 24.7M 1s
500600K .......... .......... .......... .......... .......... 98% 88.9M 1s
500650K .......... .......... .......... .......... .......... 98% 26.8M 1s
500700K .......... .......... .......... .......... .......... 98% 50.0M 1s
500750K .......... .......... .......... .......... .......... 98% 29.0M 1s
500800K .......... .......... .......... .......... .......... 98% 37.8M 1s
500850K .......... .......... .......... .......... .......... 98% 21.2M 1s
500900K .......... .......... .......... .......... .......... 98% 23.3M 1s
500950K .......... .......... .......... .......... .......... 98% 35.3M 1s
501000K .......... .......... .......... .......... .......... 98% 22.2M 1s
501050K .......... .......... .......... .......... .......... 98% 37.1M 1s
501100K .......... .......... .......... .......... .......... 98% 21.1M 1s
501150K .......... .......... .......... .......... .......... 98% 31.0M 1s
501200K .......... .......... .......... .......... .......... 98% 27.9M 1s
501250K .......... .......... .......... .......... .......... 98% 25.3M 1s
501300K .......... .......... .......... .......... .......... 98% 32.7M 1s
501350K .......... .......... .......... .......... .......... 98% 22.3M 1s
501400K .......... .......... .......... .......... .......... 98% 37.2M 1s
501450K .......... .......... .......... .......... .......... 98% 20.2M 1s
501500K .......... .......... .......... .......... .......... 98% 22.9M 1s
501550K .......... .......... .......... .......... .......... 98% 33.1M 1s
501600K .......... .......... .......... .......... .......... 98% 20.3M 1s
501650K .......... .......... .......... .......... .......... 98% 31.9M 1s
501700K .......... .......... .......... .......... .......... 98% 67.3M 1s
501750K .......... .......... .......... .......... .......... 98% 8.20M 1s
501800K .......... .......... .......... .......... .......... 98% 70.8M 1s
501850K .......... .......... .......... .......... .......... 98% 63.4M 1s
501900K .......... .......... .......... .......... .......... 98% 48.2M 1s
501950K .......... .......... .......... .......... .......... 98% 19.9M 1s
502000K .......... .......... .......... .......... .......... 98%  126M 0s
502050K .......... .......... .......... .......... .......... 98% 5.62M 0s
502100K .......... .......... .......... .......... .......... 98% 92.3M 0s
502150K .......... .......... .......... .......... .......... 98%  125M 0s
502200K .......... .......... .......... .......... .......... 98% 24.1M 0s
502250K .......... .......... .......... .......... .......... 98% 26.5M 0s
502300K .......... .......... .......... .......... .......... 98% 52.6M 0s
502350K .......... .......... .......... .......... .......... 98% 33.8M 0s
502400K .......... .......... .......... .......... .......... 98% 30.3M 0s
502450K .......... .......... .......... .......... .......... 98% 30.1M 0s
502500K .......... .......... .......... .......... .......... 98% 30.5M 0s
502550K .......... .......... .......... .......... .......... 98% 43.4M 0s
502600K .......... .......... .......... .......... .......... 98% 22.0M 0s
502650K .......... .......... .......... .......... .......... 98% 41.5M 0s
502700K .......... .......... .......... .......... .......... 98% 31.6M 0s
502750K .......... .......... .......... .......... .......... 98% 24.2M 0s
502800K .......... .......... .......... .......... .......... 98% 39.4M 0s
502850K .......... .......... .......... .......... .......... 98% 32.3M 0s
502900K .......... .......... .......... .......... .......... 98% 25.8M 0s
502950K .......... .......... .......... .......... .......... 98% 35.4M 0s
503000K .......... .......... .......... .......... .......... 98% 71.6M 0s
503050K .......... .......... .......... .......... .......... 98% 28.6M 0s
503100K .......... .......... .......... .......... .......... 98% 17.5M 0s
503150K .......... .......... .......... .......... .......... 98% 54.6M 0s
503200K .......... .......... .......... .......... .......... 98%  128M 0s
503250K .......... .......... .......... .......... .......... 98% 37.6M 0s
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503700K .......... .......... .......... .......... .......... 98% 24.1M 0s
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505000K .......... .......... .......... .......... .......... 99% 60.7M 0s
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505100K .......... .......... .......... .......... .......... 99%  126M 0s
505150K .......... .......... .......... .......... .......... 99% 47.0M 0s
505200K .......... .......... .......... .......... .......... 99% 42.3M 0s
505250K .......... .......... .......... .......... .......... 99% 47.3M 0s
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509150K .......... .......... .......... .......... .......... 99% 47.7M 0s
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509750K .......... .......... .......... .......... ......    100% 39.9M=33s

2024-07-26 18:42:22 (15.3 MB/s) - ‘ESP126-macos-arm64.tgz’ saved [522032067/522032067]

+ tar -xf ESP126-macos-arm64.tgz
+ cd ESP126
+ rm -rf /Users/jenkins/workspace/ESP_bPreBuilt/ESP126/EngSketchPad/data/Slugs
++ uname -a
+ [[ Darwin VIGGEN.MIT.EDU 23.5.0 Darwin Kernel Version 23.5.0: Wed May  1 20:16:51 PDT 2024; root:xnu-10063.121.3~5/RELEASE_ARM64_T8103 arm64 == *\D\a\r\w\i\n* ]]
+ ./setup.command
Custom icon assigned to '/Users/jenkins/Desktop/ESP126.command' based on '/Users/jenkins/workspace/ESP_bPreBuilt/ESP126/EngSketchPad/ESP/esp_logo.png'.
Custom icon assigned to '/Users/jenkins/Desktop/runESP126.command' based on '/Users/jenkins/workspace/ESP_bPreBuilt/ESP126/EngSketchPad/ESP/esp_logo.png'.
Patching '/Users/jenkins/workspace/ESP_bPreBuilt/ESP126/Python-3.11.9/bin/idle3.11'
Patching '/Users/jenkins/workspace/ESP_bPreBuilt/ESP126/Python-3.11.9/bin/pyftsubset'
Patching '/Users/jenkins/workspace/ESP_bPreBuilt/ESP126/Python-3.11.9/bin/test_op4'
Patching '/Users/jenkins/workspace/ESP_bPreBuilt/ESP126/Python-3.11.9/bin/ttx'
Patching '/Users/jenkins/workspace/ESP_bPreBuilt/ESP126/Python-3.11.9/bin/wingproj'
Patching '/Users/jenkins/workspace/ESP_bPreBuilt/ESP126/Python-3.11.9/bin/test_op2'
Patching '/Users/jenkins/workspace/ESP_bPreBuilt/ESP126/Python-3.11.9/bin/pip3'
Patching '/Users/jenkins/workspace/ESP_bPreBuilt/ESP126/Python-3.11.9/bin/test_bdf'
Patching '/Users/jenkins/workspace/ESP_bPreBuilt/ESP126/Python-3.11.9/bin/imageio_remove_bin'
Patching '/Users/jenkins/workspace/ESP_bPreBuilt/ESP126/Python-3.11.9/bin/undill'
Patching '/Users/jenkins/workspace/ESP_bPreBuilt/ESP126/Python-3.11.9/bin/bdf'
Patching '/Users/jenkins/workspace/ESP_bPreBuilt/ESP126/Python-3.11.9/bin/run_om_test'
Patching '/Users/jenkins/workspace/ESP_bPreBuilt/ESP126/Python-3.11.9/bin/f90nml'
Patching '/Users/jenkins/workspace/ESP_bPreBuilt/ESP126/Python-3.11.9/bin/webview'
Patching '/Users/jenkins/workspace/ESP_bPreBuilt/ESP126/Python-3.11.9/bin/fonttools'
Patching '/Users/jenkins/workspace/ESP_bPreBuilt/ESP126/Python-3.11.9/bin/openmdao'
Patching '/Users/jenkins/workspace/ESP_bPreBuilt/ESP126/Python-3.11.9/bin/pyNastranGUI'
Patching '/Users/jenkins/workspace/ESP_bPreBuilt/ESP126/Python-3.11.9/bin/f2py'
Patching '/Users/jenkins/workspace/ESP_bPreBuilt/ESP126/Python-3.11.9/bin/pydoc3.11'
Patching '/Users/jenkins/workspace/ESP_bPreBuilt/ESP126/Python-3.11.9/bin/2to3-3.11'
Patching '/Users/jenkins/workspace/ESP_bPreBuilt/ESP126/Python-3.11.9/bin/imageio_download_bin'
Patching '/Users/jenkins/workspace/ESP_bPreBuilt/ESP126/Python-3.11.9/bin/pip3.11'
Patching '/Users/jenkins/workspace/ESP_bPreBuilt/ESP126/Python-3.11.9/bin/test_pynastrangui'
Patching '/Users/jenkins/workspace/ESP_bPreBuilt/ESP126/Python-3.11.9/bin/numba'
Patching '/Users/jenkins/workspace/ESP_bPreBuilt/ESP126/Python-3.11.9/bin/normalizer'
Patching '/Users/jenkins/workspace/ESP_bPreBuilt/ESP126/Python-3.11.9/bin/virtualenv'
Patching '/Users/jenkins/workspace/ESP_bPreBuilt/ESP126/Python-3.11.9/bin/reset_notebook'
Patching '/Users/jenkins/workspace/ESP_bPreBuilt/ESP126/Python-3.11.9/bin/abaqus_to_nastran'
Patching '/Users/jenkins/workspace/ESP_bPreBuilt/ESP126/Python-3.11.9/bin/get_gprof'
Patching '/Users/jenkins/workspace/ESP_bPreBuilt/ESP126/Python-3.11.9/bin/format_converter'
Patching '/Users/jenkins/workspace/ESP_bPreBuilt/ESP126/Python-3.11.9/bin/pyftmerge'
Patching '/Users/jenkins/workspace/ESP_bPreBuilt/ESP126/Python-3.11.9/bin/python3.11-config'
Patching '/Users/jenkins/workspace/ESP_bPreBuilt/ESP126/Python-3.11.9/bin/f06'
Patching '/Users/jenkins/workspace/ESP_bPreBuilt/ESP126/Python-3.11.9/bin/get_objgraph'
Patching '/Users/jenkins/workspace/ESP_bPreBuilt/ESP126/Python-3.11.9/lib/python3.11/config-3.11-darwin/Makefile'
Patching '/Users/jenkins/workspace/ESP_bPreBuilt/ESP126/Python-3.11.9/lib/python3.11/config-3.11-darwin/python-config.py'
Patching '/Users/jenkins/workspace/ESP_bPreBuilt/ESP126/Python-3.11.9/lib/pkgconfig/python-3.11-embed.pc'
Patching '/Users/jenkins/workspace/ESP_bPreBuilt/ESP126/Python-3.11.9/lib/pkgconfig/python-3.11.pc'
Patching '/Users/jenkins/workspace/ESP_bPreBuilt/ESP126/Python-3.11.9/lib/python3.11/_sysconfigdata__darwin_darwin.py'
Patching '/Users/jenkins/workspace/ESP_bPreBuilt/ESP126/Python-3.11.9/lib/python3.11/site-packages/mpi4py/mpi.cfg'
Patching 'lib/cmake/libevent/LibeventTargets-shared-release.cmake'
Patching 'lib/cmake/libevent/LibeventTargets-shared.cmake'
Patching 'lib/pkgconfig/libevent.pc'
Patching 'lib/pkgconfig/libevent_core.pc'
Patching 'lib/pkgconfig/libevent_extra.pc'
Patching 'lib/pkgconfig/libevent_openssl.pc'
Patching 'lib/pkgconfig/libevent_pthreads.pc'
Patching 'bin/mpirun_esp'
Patching 'bin/ompi_info'
Patching 'bin/pmix_info'
Patching 'bin/prte_info'
Patching 'lib/libmpi.40.dylib'
Patching 'lib/libopen-pal.80.dylib'
Patching 'lib/libpmix.2.dylib'
Patching 'lib/libprrte.3.dylib'
Patching 'lib/openmpi/mca_io_romio341.so'
Patching 'lib/prte/prte_mca_schizo_ompi.so'
Patching 'include/pmix/src/include/pmix_config.h'
Patching 'lib/pkgconfig/ompi-c.pc'
Patching 'lib/pkgconfig/ompi-cxx.pc'
Patching 'lib/pkgconfig/ompi-fort.pc'
Patching 'lib/pkgconfig/ompi.pc'
Patching 'lib/pkgconfig/pmix.pc'
Patching 'share/openmpi/mpic++-wrapper-data.txt'
Patching 'share/openmpi/mpicc-wrapper-data.txt'
Patching 'share/openmpi/mpifort-wrapper-data.txt'
Patching 'share/pmix/pmixcc-wrapper-data.txt'
+ rm -rf /Users/jenkins/Desktop/ESP126.command /Users/jenkins/Desktop/runESP126.command
+ source /Users/jenkins/workspace/ESP_bPreBuilt/ESP126/EngSketchPad/ESPenv.sh
++ export ESP_ARCH=DARWIN_ARM64
++ ESP_ARCH=DARWIN_ARM64
++ export ESP_ROOT=/Users/jenkins/workspace/ESP_bPreBuilt/ESP126/EngSketchPad
++ ESP_ROOT=/Users/jenkins/workspace/ESP_bPreBuilt/ESP126/EngSketchPad
++ export CASROOT=/Users/jenkins/workspace/ESP_bPreBuilt/ESP126/OpenCASCADE-7.8.1
++ CASROOT=/Users/jenkins/workspace/ESP_bPreBuilt/ESP126/OpenCASCADE-7.8.1
++ export CASARCH=.
++ CASARCH=.
++ export CASREV=7.8
++ CASREV=7.8
++ '[' -z /Users/jenkins/workspace/ESP_bPreBuilt/ESP//test:/Users/jenkins/workspace/ESP_bPreBuilt/ESP//bin:/Users/jenkins/util/cart3d/cart3d_v1.5.9_OSX64_ICC--22.11.16/lib/perl/bin:/Users/jenkins/util/tsfoil:/Users/jenkins/util/refine/build_parallel/install/bin:/Users/jenkins/util/delaundo/delaundo/src:/Users/jenkins/util/cart3d/cart3d_v1.5.9_OSX64_ICC--22.11.16/bin:/Users/jenkins/util/cart3d/cart3d_v1.5.9_OSX64_ICC--22.11.16/bin/OSX64_ICC/:/Users/jenkins/util/astros/Astros/Darwin-64bit:/opt/homebrew/bin:/opt/homebrew/sbin:/opt/intel/oneapi/dev-utilities/2021.5.0/bin:/usr/bin:/bin:/usr/sbin:/sbin:/opt/homebrew/bin/:/Users/jenkins/util/SU2/SU2-v8.0.0/bin ']'
++ export PATH=.:/Users/jenkins/workspace/ESP_bPreBuilt/ESP126/EngSketchPad/bin:/Users/jenkins/workspace/ESP_bPreBuilt/ESP126/Python-3.11.9/bin:/Users/jenkins/workspace/ESP_bPreBuilt/ESP//test:/Users/jenkins/workspace/ESP_bPreBuilt/ESP//bin:/Users/jenkins/util/cart3d/cart3d_v1.5.9_OSX64_ICC--22.11.16/lib/perl/bin:/Users/jenkins/util/tsfoil:/Users/jenkins/util/refine/build_parallel/install/bin:/Users/jenkins/util/delaundo/delaundo/src:/Users/jenkins/util/cart3d/cart3d_v1.5.9_OSX64_ICC--22.11.16/bin:/Users/jenkins/util/cart3d/cart3d_v1.5.9_OSX64_ICC--22.11.16/bin/OSX64_ICC/:/Users/jenkins/util/astros/Astros/Darwin-64bit:/opt/homebrew/bin:/opt/homebrew/sbin:/opt/intel/oneapi/dev-utilities/2021.5.0/bin:/usr/bin:/bin:/usr/sbin:/sbin:/opt/homebrew/bin/:/Users/jenkins/util/SU2/SU2-v8.0.0/bin
++ PATH=.:/Users/jenkins/workspace/ESP_bPreBuilt/ESP126/EngSketchPad/bin:/Users/jenkins/workspace/ESP_bPreBuilt/ESP126/Python-3.11.9/bin:/Users/jenkins/workspace/ESP_bPreBuilt/ESP//test:/Users/jenkins/workspace/ESP_bPreBuilt/ESP//bin:/Users/jenkins/util/cart3d/cart3d_v1.5.9_OSX64_ICC--22.11.16/lib/perl/bin:/Users/jenkins/util/tsfoil:/Users/jenkins/util/refine/build_parallel/install/bin:/Users/jenkins/util/delaundo/delaundo/src:/Users/jenkins/util/cart3d/cart3d_v1.5.9_OSX64_ICC--22.11.16/bin:/Users/jenkins/util/cart3d/cart3d_v1.5.9_OSX64_ICC--22.11.16/bin/OSX64_ICC/:/Users/jenkins/util/astros/Astros/Darwin-64bit:/opt/homebrew/bin:/opt/homebrew/sbin:/opt/intel/oneapi/dev-utilities/2021.5.0/bin:/usr/bin:/bin:/usr/sbin:/sbin:/opt/homebrew/bin/:/Users/jenkins/util/SU2/SU2-v8.0.0/bin
++ export PYTHONINC=/Users/jenkins/workspace/ESP_bPreBuilt/ESP126/Python-3.11.9/include/python3.11
++ PYTHONINC=/Users/jenkins/workspace/ESP_bPreBuilt/ESP126/Python-3.11.9/include/python3.11
++ export 'PYTHONLIB=-L/Users/jenkins/workspace/ESP_bPreBuilt/ESP126/Python-3.11.9/lib -lpython3.11'
++ PYTHONLIB='-L/Users/jenkins/workspace/ESP_bPreBuilt/ESP126/Python-3.11.9/lib -lpython3.11'
++ '[' -z /Users/jenkins/workspace/ESP_bPreBuilt/CAPS/pyCAPS:/Users/jenkins/workspace/ESP_bPreBuilt/OpenCSM/trunk/pyOCSM:/Users/jenkins/workspace/ESP_bPreBuilt/EGADS/trunk/pyEGADS::/Users/jenkins/util/SU2/SU2-v8.0.0/bin ']'
++ export PYTHONPATH=/Users/jenkins/workspace/ESP_bPreBuilt/ESP126/EngSketchPad/lib:/Users/jenkins/workspace/ESP_bPreBuilt/ESP126/EngSketchPad/pyESP:/Users/jenkins/workspace/ESP_bPreBuilt/ESP126/Python-3.11.9/lib/python3.11/site-packages:/Users/jenkins/workspace/ESP_bPreBuilt/CAPS/pyCAPS:/Users/jenkins/workspace/ESP_bPreBuilt/OpenCSM/trunk/pyOCSM:/Users/jenkins/workspace/ESP_bPreBuilt/EGADS/trunk/pyEGADS::/Users/jenkins/util/SU2/SU2-v8.0.0/bin
++ PYTHONPATH=/Users/jenkins/workspace/ESP_bPreBuilt/ESP126/EngSketchPad/lib:/Users/jenkins/workspace/ESP_bPreBuilt/ESP126/EngSketchPad/pyESP:/Users/jenkins/workspace/ESP_bPreBuilt/ESP126/Python-3.11.9/lib/python3.11/site-packages:/Users/jenkins/workspace/ESP_bPreBuilt/CAPS/pyCAPS:/Users/jenkins/workspace/ESP_bPreBuilt/OpenCSM/trunk/pyOCSM:/Users/jenkins/workspace/ESP_bPreBuilt/EGADS/trunk/pyEGADS::/Users/jenkins/util/SU2/SU2-v8.0.0/bin
++ export UDUNITS2_XML_PATH=/Users/jenkins/workspace/ESP_bPreBuilt/ESP126/EngSketchPad/src/CAPS/udunits/udunits2.xml
++ UDUNITS2_XML_PATH=/Users/jenkins/workspace/ESP_bPreBuilt/ESP126/EngSketchPad/src/CAPS/udunits/udunits2.xml
++ export CAPS_GLYPH=/Users/jenkins/workspace/ESP_bPreBuilt/ESP126/EngSketchPad/src/CAPS/aim/pointwise/glyph
++ CAPS_GLYPH=/Users/jenkins/workspace/ESP_bPreBuilt/ESP126/EngSketchPad/src/CAPS/aim/pointwise/glyph
++ export 'SLUGS_START=open -a /Applications/Safari.app /Users/jenkins/workspace/ESP_bPreBuilt/ESP126/EngSketchPad/SLUGS/Slugs.html'
++ SLUGS_START='open -a /Applications/Safari.app /Users/jenkins/workspace/ESP_bPreBuilt/ESP126/EngSketchPad/SLUGS/Slugs.html'
++ export 'ESP_START=open -a /Applications/Safari.app;sleep 1;open -a /Applications/Safari.app /Users/jenkins/workspace/ESP_bPreBuilt/ESP126/EngSketchPad/ESP/ESP-localhost7681.html'
++ ESP_START='open -a /Applications/Safari.app;sleep 1;open -a /Applications/Safari.app /Users/jenkins/workspace/ESP_bPreBuilt/ESP126/EngSketchPad/ESP/ESP-localhost7681.html'
++ export 'WV_START=open -a /Applications/Safari.app /Users/jenkins/workspace/ESP_bPreBuilt/ESP126/EngSketchPad/wvClient/wv.html'
++ WV_START='open -a /Applications/Safari.app /Users/jenkins/workspace/ESP_bPreBuilt/ESP126/EngSketchPad/wvClient/wv.html'
+ which python
/Users/jenkins/workspace/ESP_bPreBuilt/ESP126/Python-3.11.9/bin/python
+ python --version
Python 3.11.9
+ export CSMDATA=/Users/jenkins/workspace/ESP_bPreBuilt/ESP126/EngSketchPad/data
+ CSMDATA=/Users/jenkins/workspace/ESP_bPreBuilt/ESP126/EngSketchPad/data
+ cd /Users/jenkins/workspace/ESP_bPreBuilt/ESP126/EngSketchPad/bin
++ uname -a
+ [[ Darwin VIGGEN.MIT.EDU 23.5.0 Darwin Kernel Version 23.5.0: Wed May  1 20:16:51 PDT 2024; root:xnu-10063.121.3~5/RELEASE_ARM64_T8103 arm64 == *\D\a\r\w\i\n* ]]
+ sed -i '' '/.*capsExamples.*/d' /Users/jenkins/workspace/ESP_bPreBuilt/Verification.sh
+ bash -ex /Users/jenkins/workspace/ESP_bPreBuilt/Verification.sh
+ expectSuccess 01 /Users/jenkins/workspace/ESP_bPreBuilt/ESP126/EngSketchPad/data/basic/expressions
+ ./serveESP -batch -verify -outLevel 0 /Users/jenkins/workspace/ESP_bPreBuilt/ESP126/EngSketchPad/data/basic/expressions
WARNING:: cannot open "/Users/jenkins/workspace/ESP_bPreBuilt/ESP126/EngSketchPad/data/basic/verify_7.8.1/expressions.vfy", so verification is being skipped
ERROR:: problem evaluating argument 2 (slice(e3,0,999)) for Branch 152 (set)
ERROR:: problem evaluating argument 2 (slice(e3,14,999)) for Branch 158 (set)
ERROR:: problem evaluating argument 2 (slice(e3,4,-1)) for Branch 164 (set)
==&gt; serveESP completed successfully with no verification data

real	0m5.616s
user	0m0.140s
sys	0m0.041s
+ set +x

=============================================
ESP verification case 01 passed (as expected)
=============================================

+ expectSuccess 02 /Users/jenkins/workspace/ESP_bPreBuilt/ESP126/EngSketchPad/data/basic/demo2
+ ./serveESP -batch -verify -outLevel 0 /Users/jenkins/workspace/ESP_bPreBuilt/ESP126/EngSketchPad/data/basic/demo2
WARNING:: cannot open "/Users/jenkins/workspace/ESP_bPreBuilt/ESP126/EngSketchPad/data/basic/verify_7.8.1/demo2.vfy", so verification is being skipped
==&gt; serveESP completed successfully with no verification data

real	0m0.195s
user	0m0.222s
sys	0m0.026s
+ set +x

=============================================
ESP verification case 02 passed (as expected)
=============================================

+ expectSuccess 03 /Users/jenkins/workspace/ESP_bPreBuilt/ESP126/EngSketchPad/data/legacy/tutorial1_whole
+ ./serveESP -batch -verify -outLevel 0 /Users/jenkins/workspace/ESP_bPreBuilt/ESP126/EngSketchPad/data/legacy/tutorial1_whole
WARNING:: cannot open "/Users/jenkins/workspace/ESP_bPreBuilt/ESP126/EngSketchPad/data/legacy/verify_7.8.1/tutorial1_whole.vfy", so verification is being skipped
==&gt; serveESP completed successfully with no verification data

real	0m1.214s
user	0m1.870s
sys	0m0.567s
+ set +x

=============================================
ESP verification case 03 passed (as expected)
=============================================

+ expectSuccess 04 /Users/jenkins/workspace/ESP_bPreBuilt/ESP126/EngSketchPad/data/basic/design2
+ ./serveESP -batch -verify -outLevel 0 /Users/jenkins/workspace/ESP_bPreBuilt/ESP126/EngSketchPad/data/basic/design2
WARNING:: cannot open "/Users/jenkins/workspace/ESP_bPreBuilt/ESP126/EngSketchPad/data/basic/verify_7.8.1/design2.vfy", so verification is being skipped
==&gt; serveESP completed successfully with no verification data

real	0m0.280s
user	0m0.322s
sys	0m0.028s
+ set +x

=============================================
ESP verification case 04 passed (as expected)
=============================================

+ expectSuccess 05 /Users/jenkins/workspace/ESP_bPreBuilt/ESP126/EngSketchPad/data/basic/design3
+ ./serveESP -batch -verify -outLevel 0 /Users/jenkins/workspace/ESP_bPreBuilt/ESP126/EngSketchPad/data/basic/design3
WARNING:: cannot open "/Users/jenkins/workspace/ESP_bPreBuilt/ESP126/EngSketchPad/data/basic/verify_7.8.1/design3.vfy", so verification is being skipped
==&gt; serveESP completed successfully with no verification data

real	0m0.296s
user	0m0.415s
sys	0m0.035s
+ set +x

=============================================
ESP verification case 05 passed (as expected)
=============================================

+ expectSuccess 06 /Users/jenkins/workspace/ESP_bPreBuilt/ESP126/EngSketchPad/data/legacy/tutorial2
+ ./serveESP -batch -verify -outLevel 0 /Users/jenkins/workspace/ESP_bPreBuilt/ESP126/EngSketchPad/data/legacy/tutorial2
WARNING:: cannot open "/Users/jenkins/workspace/ESP_bPreBuilt/ESP126/EngSketchPad/data/legacy/verify_7.8.1/tutorial2.vfy", so verification is being skipped
==&gt; serveESP completed successfully with no verification data

real	0m0.288s
user	0m0.424s
sys	0m0.015s
+ set +x

=============================================
ESP verification case 06 passed (as expected)
=============================================

+ expectSuccess 07 /Users/jenkins/workspace/ESP_bPreBuilt/ESP126/EngSketchPad/data/legacy/tutorial3
+ ./serveESP -batch -verify -outLevel 0 /Users/jenkins/workspace/ESP_bPreBuilt/ESP126/EngSketchPad/data/legacy/tutorial3
WARNING:: cannot open "/Users/jenkins/workspace/ESP_bPreBuilt/ESP126/EngSketchPad/data/legacy/verify_7.8.1/tutorial3.vfy", so verification is being skipped
==&gt; serveESP completed successfully with no verification data

real	0m2.143s
user	0m3.450s
sys	0m0.312s
+ set +x

=============================================
ESP verification case 07 passed (as expected)
=============================================

+ expectSuccess 08 /Users/jenkins/workspace/ESP_bPreBuilt/ESP126/EngSketchPad/data/CAPS/myPlane
+ ./serveESP -batch -verify -outLevel 0 /Users/jenkins/workspace/ESP_bPreBuilt/ESP126/EngSketchPad/data/CAPS/myPlane
WARNING:: cannot open "/Users/jenkins/workspace/ESP_bPreBuilt/ESP126/EngSketchPad/data/CAPS/verify_7.8.1/myPlane.vfy", so verification is being skipped
==&gt; serveESP completed successfully with 12 warnings and no verification data

real	0m14.378s
user	0m26.406s
sys	0m1.095s
+ set +x

=============================================
ESP verification case 08 passed (as expected)
=============================================

+ expectSuccess 09 /Users/jenkins/workspace/ESP_bPreBuilt/ESP126/EngSketchPad/data/bottle
+ ./serveESP -batch -verify -outLevel 0 /Users/jenkins/workspace/ESP_bPreBuilt/ESP126/EngSketchPad/data/bottle
WARNING:: cannot open "/Users/jenkins/workspace/ESP_bPreBuilt/ESP126/EngSketchPad/data/verify_7.8.1/bottle.vfy", so verification is being skipped
==&gt; serveESP completed successfully with no verification data

real	0m0.327s
user	0m0.389s
sys	0m0.012s
+ set +x

=============================================
ESP verification case 09 passed (as expected)
=============================================

+ expectSuccess 10 /Users/jenkins/workspace/ESP_bPreBuilt/ESP126/EngSketchPad/data/basic/wingMultiModel
+ ./serveESP -batch -verify -outLevel 0 /Users/jenkins/workspace/ESP_bPreBuilt/ESP126/EngSketchPad/data/basic/wingMultiModel
WARNING:: cannot open "/Users/jenkins/workspace/ESP_bPreBuilt/ESP126/EngSketchPad/data/basic/verify_7.8.1/wingMultiModel.vfy", so verification is being skipped
==&gt; serveESP completed successfully with 4 warnings and no verification data

real	0m13.874s
user	0m47.654s
sys	0m16.089s
+ set +x

=============================================
ESP verification case 10 passed (as expected)
=============================================

+ expectSuccess 11 /Users/jenkins/workspace/ESP_bPreBuilt/ESP126/EngSketchPad/data/basic/bullet
+ ./serveESP -batch -verify -outLevel 0 /Users/jenkins/workspace/ESP_bPreBuilt/ESP126/EngSketchPad/data/basic/bullet
WARNING:: cannot open "/Users/jenkins/workspace/ESP_bPreBuilt/ESP126/EngSketchPad/data/basic/verify_7.8.1/bullet.vfy", so verification is being skipped
WARNING:: 8 _hist and/or __trace__ attributes removed
WARNING:: 8 _hist and/or __trace__ attributes removed
WARNING:: could not find mapping for iedge=10
WARNING:: could not find mapping for iedge=14
WARNING:: could not find mapping for iedge=7
WARNING:: could not find mapping for iedge=11
==&gt; serveESP completed successfully with 4 warnings and no verification data

real	0m0.384s
user	0m0.260s
sys	0m0.023s
+ set +x

=============================================
ESP verification case 11 passed (as expected)
=============================================

+ expectSuccess 12 /Users/jenkins/workspace/ESP_bPreBuilt/ESP126/EngSketchPad/data/basic/connect5
+ ./serveESP -batch -verify -outLevel 0 /Users/jenkins/workspace/ESP_bPreBuilt/ESP126/EngSketchPad/data/basic/connect5
WARNING:: cannot open "/Users/jenkins/workspace/ESP_bPreBuilt/ESP126/EngSketchPad/data/basic/verify_7.8.1/connect5.vfy", so verification is being skipped
==&gt; serveESP completed successfully with no verification data

real	0m0.330s
user	0m0.523s
sys	0m0.006s
+ set +x

=============================================
ESP verification case 12 passed (as expected)
=============================================

+ expectSuccess 13 /Users/jenkins/workspace/ESP_bPreBuilt/ESP126/EngSketchPad/data/basic/group2
+ ./serveESP -batch -verify -outLevel 0 /Users/jenkins/workspace/ESP_bPreBuilt/ESP126/EngSketchPad/data/basic/group2
WARNING:: cannot open "/Users/jenkins/workspace/ESP_bPreBuilt/ESP126/EngSketchPad/data/basic/verify_7.8.1/group2.vfy", so verification is being skipped
==&gt; serveESP completed successfully with no verification data

real	0m0.123s
user	0m0.139s
sys	0m0.006s
+ set +x

=============================================
ESP verification case 13 passed (as expected)
=============================================

+ expectSuccess 14 /Users/jenkins/workspace/ESP_bPreBuilt/ESP126/EngSketchPad/data/basic/csm3
+ ./serveESP -batch -verify -outLevel 0 /Users/jenkins/workspace/ESP_bPreBuilt/ESP126/EngSketchPad/data/basic/csm3
WARNING:: cannot open "/Users/jenkins/workspace/ESP_bPreBuilt/ESP126/EngSketchPad/data/basic/verify_7.8.1/csm3.vfy", so verification is being skipped
nnode=8
nedge=12
nface=6
nnode=8
nedge=12
nface=6
nnode=16
nedge=24
nface=10
nnode=8
nedge=12
nface=6
==&gt; serveESP completed successfully with no verification data

real	0m0.438s
user	0m0.354s
sys	0m0.011s
+ set +x

=============================================
ESP verification case 14 passed (as expected)
=============================================

+ cd /Users/jenkins/workspace/ESP_bPreBuilt/ESP126/EngSketchPad/pyESP/testEGADS
+ make test
python --version
Python 3.11.9
python -u -m unittest discover
......................................................   PCurve Map: 48 (alloc 48)!
   Surface Map: 12 (alloc 24)!
   Curve Map: 28 (alloc 28)!
 Writing PCurves...
 Writing Curves...
 Writing Surfaces...
 Writing 16 Nodes...
 Writing 28 Edges...
 Writing 12 Loops...
 Writing 12 Faces...
 Writing 1 Shells...
 EGADS Info: 0 Objects, 0 Reference in Use (of 972) at Close!
...................
----------------------------------------------------------------------
Ran 73 tests in 1.120s

OK
+ cd /Users/jenkins/workspace/ESP_bPreBuilt/ESP126/EngSketchPad/pyESP/testOCSM
+ source /Users/jenkins/workspace/ESP_bPreBuilt/JenkinsESP/test_pyOCSM.sh
++ set -x
++ python -u test_pyOCSM.py -skipHelp

real	0m3.628s
user	0m5.229s
sys	0m0.077s
++ set +x
=================================================
test_pyOCSM.py passed (as expected)
=================================================
+ cd /Users/jenkins/workspace/ESP_bPreBuilt/ESP126/EngSketchPad/pyESP/testCAPS
+ make test
python --version
Python 3.11.9
python -u -m unittest discover
..Mapping Csys attributes ................
	Number of unique Csys attributes = 2
	Name = leftWingSkin, index = 1
	Name = riteWingSkin, index = 2

Getting FEA coordinate systems.......
	Number of coordinate systems - 2
	Coordinate system name - leftWingSkin
	Coordinate system name - riteWingSkin
Mapping capsConstraint attributes ................
	Number of unique capsConstraint attributes = 0
Mapping capsLoad attributes ................
	Number of unique capsLoad attributes = 0
Mapping capsBound attributes ................
	Number of unique capsBound attributes = 1
	Name = Upper_Left, index = 1
Mapping capsConnect attributes ................
	Number of unique capsConnect attributes = 0
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 2
	Name = Wing1, index = 1
	Name = Wing2, index = 2
Setting FEA Data
	Mesh for body = 0
	Number of nodal coordinates = 143
	Number of elements = 282
	Elemental Nodes = 0
	Elemental Rods  = 0
	Elemental Tria3 = 282
	Elemental Quad4 = 0
Setting FEA Data
	Mesh for body = 1
	Number of nodal coordinates = 155
	Number of elements = 306
	Elemental Nodes = 0
	Elemental Rods  = 0
	Elemental Tria3 = 306
	Elemental Quad4 = 0
Combining multiple FEA meshes!
	Combined Number of nodal coordinates = 298
	Combined Number of elements = 588
	Combined Elemental Nodes = 0
	Combined Elemental Rods  = 0
	Combined Elemental Tria3 = 588
	Combined Elemental Quad4 = 0

Getting FEA materials.......
	Number of materials - 2
	Material name - madeupium
	Material name - unobtainium
	Done getting FEA materials

Getting FEA properties.......
	Number of properties - 2
	Property name - Wing1
	Property name - Wing2
	Done getting FEA properties
Updating mesh element types based on properties input
... EGADS Info: 0 Objects, 0 Reference in Use (of 0) at Close!
..Writing D3 Javascript library -  d3.v3.min.js
........... EGADS Info: 0 Objects, 0 Reference in Use (of 0) at Close!
. EGADS Info: 0 Objects, 0 Reference in Use (of 0) at Close!
. EGADS Info: 0 Objects, 0 Reference in Use (of 0) at Close!
 EGADS Info: 0 Objects, 0 Reference in Use (of 0) at Close!
.No analysis directory provided - defaulting to altName
Mapping Csys attributes ................
	Number of unique Csys attributes = 2
	Name = leftWingSkin, index = 1
	Name = riteWingSkin, index = 2

Getting FEA coordinate systems.......
	Number of coordinate systems - 2
	Coordinate system name - leftWingSkin
	Coordinate system name - riteWingSkin
Mapping capsConstraint attributes ................
	Number of unique capsConstraint attributes = 0
Mapping capsLoad attributes ................
	Number of unique capsLoad attributes = 0
Mapping capsBound attributes ................
	Number of unique capsBound attributes = 1
	Name = Upper_Left, index = 1
Mapping capsConnect attributes ................
	Number of unique capsConnect attributes = 0
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 2
	Name = Wing1, index = 1
	Name = Wing2, index = 2
Setting FEA Data
	Mesh for body = 0
	Number of nodal coordinates = 209
	Number of elements = 414
	Elemental Nodes = 0
	Elemental Rods  = 0
	Elemental Tria3 = 414
	Elemental Quad4 = 0
Setting FEA Data
	Mesh for body = 1
	Number of nodal coordinates = 186
	Number of elements = 368
	Elemental Nodes = 0
	Elemental Rods  = 0
	Elemental Tria3 = 368
	Elemental Quad4 = 0
Combining multiple FEA meshes!
	Combined Number of nodal coordinates = 395
	Combined Number of elements = 782
	Combined Elemental Nodes = 0
	Combined Elemental Rods  = 0
	Combined Elemental Tria3 = 782
	Combined Elemental Quad4 = 0

Getting FEA materials.......
	Number of materials - 2
	Material name - madeupium
	Material name - unobtainium
	Done getting FEA materials

Getting FEA properties.......
	Number of properties - 2
	Property name - Wing1
	Property name - Wing2
	Done getting FEA properties
Updating mesh element types based on properties input
..........--&gt; Opening DESPMTR file "unitGeom.param"
    updating CFGPMTR series                          [ 1, 1] =  8412.000000
    updating CFGPMTR series2                         [ 1, 1] =    20.000000
    updating CFGPMTR VIEW:CFD                        [ 1, 1] =     1.000000
    updating CFGPMTR nrow                            [ 1, 1] =     3.000000
    updating CFGPMTR ncol                            [ 1, 1] =     2.000000
    updating DESPMTR area                            [ 1, 1] =    40.000000
    updating DESPMTR aspect                          [ 1, 1] =     5.000000
    updating DESPMTR taper                           [ 1, 1] =     0.500000
    updating DESPMTR twist                           [ 1, 1] =    15.000000
    updating DESPMTR wing:lesweep                    [ 1, 1] =    30.000000
    updating DESPMTR wing:dihedral                   [ 1, 1] =     1.000000
    updating DESPMTR wing:chord:root                 [ 1, 1] =     1.560000
    updating DESPMTR htail                           [ 1, 1] =     1.000000
    updating DESPMTR htail:chord                     [ 1, 1] =     2.000000
    updating DESPMTR vtail:chord                     [ 1, 1] =     3.000000
    updating DESPMTR vtail                           [ 1, 1] =     4.000000
    updating DESPMTR sphereR                         [ 1, 1] =    80.000000
    updating DESPMTR v@1:d_name                      [ 1, 1] =     1.000000
    updating DESPMTR despMat                         [ 1, 1] =    11.000000
    updating DESPMTR despMat                         [ 1, 2] =    12.000000
    updating DESPMTR despMat                         [ 2, 1] =    13.000000
    updating DESPMTR despMat                         [ 2, 2] =    14.000000
    updating DESPMTR despMat                         [ 3, 1] =    15.000000
    updating DESPMTR despMat                         [ 3, 2] =    16.000000
    updating DESPMTR despCol                         [ 1, 1] =    11.000000
    updating DESPMTR despCol                         [ 2, 1] =    13.000000
    updating DESPMTR despCol                         [ 3, 1] =    15.000000
    updating DESPMTR despRow                         [ 1, 1] =    11.000000
    updating DESPMTR despRow                         [ 1, 2] =    12.000000
    updating DESPMTR despRow                         [ 1, 3] =    13.000000
ERROR:: DESPMTR file "unitGeom.param" not found
 CAPS Error: ocsmSaveDespmtrs = -201 (caps_readParameters)!
 EGADS Info: 0 Objects, 0 Reference in Use (of 0) at Close!
.. EGADS Error: No Attribute -&gt; __numRemaining__ (EG_attributeDel)!
 EGADS Error: No Attribute -&gt; __numRemaining__ (EG_attributeDel)!
 EGADS Error: No Attribute -&gt; _body (EG_attributeDel)!
 EGADS Error: No Attribute -&gt; _nface (EG_attributeDel)!
 EGADS Error: No Attribute -&gt; __trace__ (EG_attributeDel)!
 EGADS Error: No Attribute -&gt; _body (EG_attributeDel)!
 EGADS Error: No Attribute -&gt; _nface (EG_attributeDel)!
 EGADS Error: No Attribute -&gt; __trace__ (EG_attributeDel)!
 EGADS Error: No Attribute -&gt; _body (EG_attributeDel)!
 EGADS Error: No Attribute -&gt; _nface (EG_attributeDel)!
 EGADS Error: No Attribute -&gt; __trace__ (EG_attributeDel)!
 EGADS Error: No Attribute -&gt; _body (EG_attributeDel)!
 EGADS Error: No Attribute -&gt; _nface (EG_attributeDel)!
 EGADS Error: No Attribute -&gt; __trace__ (EG_attributeDel)!
. EGADS Info: 0 Objects, 0 Reference in Use (of 0) at Close!
.. EGADS Info: 0 Objects, 0 Reference in Use (of 0) at Close!
 CAPS Info: Hit last success -- going live!
 CAPS Info: Hit last success -- going live!
 CAPS Info: Hit last success -- going live!
 CAPS Info: Hit last success -- going live!
 CAPS Info: Hit last success -- going live!
 CAPS Info: Hit last success -- going live!
 CAPS Info: Hit last success -- going live!
 CAPS Info: Hit last success -- going live!
 CAPS Info: Hit last success -- going live!
 CAPS Info: Hit last success -- going live!
 CAPS Info: Hit last success -- going live!
 CAPS Info: Hit last success -- going live!
 CAPS Info: Hit last success -- going live!
 CAPS Info: Hit last success -- going live!
 CAPS Info: Hit last success -- going live!
 CAPS Info: Hit last success -- going live!
 CAPS Info: Hit last success -- going live!
 CAPS Info: Hit last success -- going live!
 CAPS Info: Hit last success -- going live!
. EGADS Info: 0 Objects, 0 Reference in Use (of 0) at Close!
 CAPS Info: Hit last success -- going live!
 CAPS Info: Hit last success -- going live!
 CAPS Info: Hit last success -- going live!
 CAPS Info: Hit last success -- going live!
 CAPS Info: Hit last success -- going live!
 CAPS Info: Hit last success -- going live!
 CAPS Info: Hit last success -- going live!
 CAPS Info: Hit last success -- going live!
 CAPS Info: Hit last success -- going live!
 CAPS Info: Hit last success -- going live!
 CAPS Info: Hit last success -- going live!
 CAPS Info: Hit last success -- going live!
. EGADS Info: 0 Objects, 0 Reference in Use (of 0) at Close!
 CAPS Info: Hit last success -- going live!
 CAPS Info: Hit last success -- going live!
 CAPS Info: Hit last success -- going live!
 CAPS Info: Hit last success -- going live!
 CAPS Info: Hit last success -- going live!
 CAPS Info: Hit last success -- going live!
 CAPS Info: Hit last success -- going live!
 CAPS Info: Hit last success -- going live!
 CAPS Info: Hit last success -- going live!
 CAPS Info: Hit last success -- going live!
 CAPS Info: Hit last success -- going live!
 CAPS Info: Hit last success -- going live!
..Linked Parameter Beta to analysis su2 input Beta
Linked Parameter Alpha to analysis su2 input Alpha
No linkable data found for Altitude
No linkable data found for Strings
No linkable data found for Strings2
Linked Parameter Beta to analysis su2 input Beta
Linked Parameter Alpha to analysis su2 input Alpha
............ EGADS Info: 0 Objects, 0 Reference in Use (of 0) at Close!
. EGADS Info: 0 Objects, 0 Reference in Use (of 0) at Close!
. EGADS Info: 0 Objects, 0 Reference in Use (of 0) at Close!
.. EGADS Info: 0 Objects, 0 Reference in Use (of 0) at Close!
 EGADS Info: 0 Objects, 0 Reference in Use (of 0) at Close!
 EGADS Info: 0 Objects, 0 Reference in Use (of 0) at Close!
. EGADS Info: 0 Objects, 0 Reference in Use (of 0) at Close!
. EGADS Info: 0 Objects, 0 Reference in Use (of 0) at Close!
 EGADS Info: 0 Objects, 0 Reference in Use (of 0) at Close!
 EGADS Info: 0 Objects, 0 Reference in Use (of 0) at Close!
 EGADS Info: 0 Objects, 0 Reference in Use (of 0) at Close!
. EGADS Info: 0 Objects, 0 Reference in Use (of 0) at Close!
. CAPS Info: Hit last success -- going live!
... EGADS Info: 0 Objects, 0 Reference in Use (of 0) at Close!
. EGADS Info: 0 Objects, 0 Reference in Use (of 0) at Close!
. EGADS Info: 0 Objects, 0 Reference in Use (of 0) at Close!
.. EGADS Info: 0 Objects, 0 Reference in Use (of 0) at Close!
.. EGADS Info: 0 Objects, 0 Reference in Use (of 0) at Close!
. EGADS Info: 0 Objects, 0 Reference in Use (of 0) at Close!
. EGADS Info: 0 Objects, 0 Reference in Use (of 0) at Close!
.. EGADS Info: 0 Objects, 0 Reference in Use (of 0) at Close!
. EGADS Info: 0 Objects, 0 Reference in Use (of 0) at Close!
. EGADS Info: 0 Objects, 0 Reference in Use (of 0) at Close!
.. EGADS Info: 0 Objects, 0 Reference in Use (of 0) at Close!
. EGADS Info: 0 Objects, 0 Reference in Use (of 0) at Close!
. EGADS Info: 0 Objects, 0 Reference in Use (of 0) at Close!
. EGADS Error: No Attribute -&gt; __numRemaining__ (EG_attributeDel)!
 EGADS Error: No Attribute -&gt; _body (EG_attributeDel)!
 EGADS Error: No Attribute -&gt; _nface (EG_attributeDel)!
 EGADS Error: No Attribute -&gt; __trace__ (EG_attributeDel)!
 EGADS Error: No Attribute -&gt; _body (EG_attributeDel)!
 EGADS Error: No Attribute -&gt; _nface (EG_attributeDel)!
 EGADS Error: No Attribute -&gt; __trace__ (EG_attributeDel)!
 EGADS Error: No Attribute -&gt; _body (EG_attributeDel)!
 EGADS Error: No Attribute -&gt; _nface (EG_attributeDel)!
 EGADS Error: No Attribute -&gt; __trace__ (EG_attributeDel)!
 EGADS Error: No Attribute -&gt; _body (EG_attributeDel)!
 EGADS Error: No Attribute -&gt; _nface (EG_attributeDel)!
 EGADS Error: No Attribute -&gt; __trace__ (EG_attributeDel)!
 EGADS Error: No Attribute -&gt; __numRemaining__ (EG_attributeDel)!
. EGADS Info: 0 Objects, 0 Reference in Use (of 0) at Close!
.--&gt; Opening DESPMTR file "unitGeom.param"
    updating CFGPMTR series                          [ 1, 1] =  8412.000000
    updating CFGPMTR series2                         [ 1, 1] =    20.000000
    updating CFGPMTR VIEW:CFD                        [ 1, 1] =     1.000000
    updating CFGPMTR nrow                            [ 1, 1] =     3.000000
    updating CFGPMTR ncol                            [ 1, 1] =     2.000000
    updating DESPMTR area                            [ 1, 1] =    40.000000
    updating DESPMTR aspect                          [ 1, 1] =     5.000000
    updating DESPMTR taper                           [ 1, 1] =     0.500000
    updating DESPMTR twist                           [ 1, 1] =    15.000000
    updating DESPMTR wing:lesweep                    [ 1, 1] =    30.000000
    updating DESPMTR wing:dihedral                   [ 1, 1] =     1.000000
    updating DESPMTR wing:chord:root                 [ 1, 1] =     1.560000
    updating DESPMTR htail                           [ 1, 1] =     1.000000
    updating DESPMTR htail:chord                     [ 1, 1] =     2.000000
    updating DESPMTR vtail:chord                     [ 1, 1] =     3.000000
    updating DESPMTR vtail                           [ 1, 1] =     4.000000
    updating DESPMTR sphereR                         [ 1, 1] =    80.000000
    updating DESPMTR v@1:d_name                      [ 1, 1] =     1.000000
    updating DESPMTR despMat                         [ 1, 1] =    11.000000
    updating DESPMTR despMat                         [ 1, 2] =    12.000000
    updating DESPMTR despMat                         [ 2, 1] =    13.000000
    updating DESPMTR despMat                         [ 2, 2] =    14.000000
    updating DESPMTR despMat                         [ 3, 1] =    15.000000
    updating DESPMTR despMat                         [ 3, 2] =    16.000000
    updating DESPMTR despCol                         [ 1, 1] =    11.000000
    updating DESPMTR despCol                         [ 2, 1] =    13.000000
    updating DESPMTR despCol                         [ 3, 1] =    15.000000
    updating DESPMTR despRow                         [ 1, 1] =    11.000000
    updating DESPMTR despRow                         [ 1, 2] =    12.000000
    updating DESPMTR despRow                         [ 1, 3] =    13.000000
ERROR:: DESPMTR file "unitGeom.param" not found
 CAPS Error: ocsmSaveDespmtrs = -201 (caps_readParameters)!
 EGADS Info: 0 Objects, 0 Reference in Use (of 0) at Close!
. EGADS Info: 0 Objects, 0 Reference in Use (of 0) at Close!
. EGADS Info: 0 Objects, 0 Reference in Use (of 0) at Close!
................ EGADS Info: 0 Objects, 0 Reference in Use (of 0) at Close!

----------------------------------------------------------------------
Ran 100 tests in 9.921s

OK
WARNING: 'capsProblem.loadCAPS' is deprecated. Please use 'Problem.__init__'!
WARNING: 'capsGeometry.__init__' is deprecated. Please use 'Problem.__init__'!
WARNING: 'capsProblem.loadAIM' is deprecated. Please use 'Problem.analysis.create'!
WARNING: 'capsAnalysis.__init__' is deprecated. Please use 'Problem.analysis.create'!
WARNING: 'capsAnalysis.setAnalysisVal' is deprecated. Please use 'Analysis.input["varname"].value'!
WARNING: 'capsGeometry.setGeometryVal' is deprecated. Please use 'Problem.geometry.despmtr["varname"].value'!
WARNING: 'capsAnalysis.getAnalysisOutVal' is deprecated. Please use 'Analysis.output["varname"].value'!
WARNING: 'capsProblem.__init__' is deprecated. Please use 'Problem.__init__'!
+ cd /Users/jenkins/workspace/ESP_bPreBuilt/ESP126/EngSketchPad/src/CAPS/aim/unitTest/pyCAPS/
+ make test
python --version
Python 3.11.9
python -u -m unittest discover --verbose
test_journal (test_aflr2.TestAFLR2.test_journal) ... Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 5
	Name = 2DSlice, index = 1
	Name = TunnelWall, index = 2
	Name = OutFlow, index = 3
	Name = InFlow, index = 4
	Name = Airfoil, index = 5
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 4
	Name = TunnelWall, index = 1
	Name = OutFlow, index = 2
	Name = InFlow, index = 3
	Name = Airfoil, index = 4
Getting 2D mesh for body 1 (of 1)
 
AFLR2    : ---------------------------------------
AFLR2    : AFLR2 LIBRARY
AFLR2    : ADVANCING-FRONT/LOCAL-RECONNECTION
AFLR2    : TRIA/QUAD GRID GENERATOR
AFLR2    : Version Number 9.18.1
AFLR2    : Version Date   06/11/24 @ 05:52PM
AFLR2    : Compile OS     Darwin 23.5.0 arm64
AFLR2    : Compile Date   06/11/24 @ 05:52PM
AFLR2    : Copyright 1994-2021, D.L. Marcum
AFLR2    : ---------------------------------------
 
AFLR2 IC : INPUT DATA CHECK
 
AFLR2 IC : Nodes, Faces      =      2244         0
 
AFLR2    : CPU Time          =     0.000   seconds
 
AFLR2 EG : EDGE GRID RE-GENERATION
 
AFLR2 EG : Nodes, Edges      =      2244      2244
 
AFLR2    : CPU Time          =     0.000   seconds
 
AFLR2 IG : INITIAL GRID GENERATION
 
AFLR2 IG : Nodes, Faces      =         0         2
AFLR2 IG : Nodes, Faces      =       450       902
AFLR2 IG : Nodes, Faces      =       900      1802
AFLR2 IG : Nodes, Faces      =      1145      2292
AFLR2 IG : Nodes, Faces      =      1260      2522
AFLR2 IG : Nodes, Faces      =      1350      2702
AFLR2 IG : Nodes, Faces      =      1360      2722
AFLR2 IG : Nodes, Faces      =      1460      2922
AFLR2 IG : Nodes, Faces      =      1560      3122
AFLR2 IG : Nodes, Faces      =      1660      3322
AFLR2 IG : Nodes, Faces      =      1760      3522
AFLR2 IG : Nodes, Faces      =      1800      3602
AFLR2 IG : Nodes, Faces      =      1860      3722
AFLR2 IG : Nodes, Faces      =      1960      3922
AFLR2 IG : Nodes, Faces      =      2060      4122
AFLR2 IG : Nodes, Faces      =      2085      4172
AFLR2 IG : Nodes, Faces      =      2244      4490
AFLR2 IG : Nodes, Faces      =      2248      4490
AFLR2 IG : Nodes, Faces      =      2244      2244
 
AFLR2    : CPU Time          =     0.014   seconds
 
AFLR2 GG : FIELD GRID GENERATION
 
AFLR2 GG : Nodes, Faces      =      2244      2244
AFLR2 GG : Nodes, Faces      =      4285      6326
AFLR2 GG : Nodes, Faces      =      6135     10026
AFLR2 GG : Nodes, Faces      =      7878     13512
AFLR2 GG : Nodes, Faces      =      9485     16726
AFLR2 GG : Nodes, Faces      =     10981     19718
AFLR2 GG : Nodes, Faces      =     12372     22500
AFLR2 GG : Nodes, Faces      =     13686     25128
AFLR2 GG : Nodes, Faces      =     14908     27572
AFLR2 GG : Nodes, Faces      =     16063     29882
AFLR2 GG : Nodes, Faces      =     17170     32096
AFLR2 GG : Nodes, Faces      =     18222     34200
AFLR2 GG : Nodes, Faces      =     19208     36172
AFLR2 GG : Nodes, Faces      =     20165     38086
AFLR2 GG : Nodes, Faces      =     21087     39930
AFLR2 GG : Nodes, Faces      =     21975     41706
AFLR2 GG : Nodes, Faces      =     22803     43362
AFLR2 GG : Nodes, Faces      =     23582     44920
AFLR2 GG : Nodes, Faces      =     24330     46416
AFLR2 GG : Nodes, Faces      =     25041     47838
AFLR2 GG : Nodes, Faces      =     25723     49202
AFLR2 GG : Nodes, Faces      =     26365     50486
AFLR2 GG : Nodes, Faces      =     26993     51742
AFLR2 GG : Nodes, Faces      =     27556     52868
AFLR2 GG : Nodes, Faces      =     28054     53864
AFLR2 GG : Nodes, Faces      =     28487     54730
AFLR2 GG : Nodes, Faces      =     28847     55450
AFLR2 GG : Nodes, Faces      =     29118     55992
AFLR2 GG : Nodes, Faces      =     29355     56466
AFLR2 GG : Nodes, Faces      =     29553     56862
AFLR2 GG : Nodes, Faces      =     29735     57226
AFLR2 GG : Nodes, Faces      =     29878     57512
AFLR2 GG : Nodes, Faces      =     29969     57694
AFLR2 GG : Nodes, Faces      =     30009     57774
AFLR2 GG : Nodes, Faces      =     30018     57792
AFLR2 GG : Nodes, Faces      =     30019     57794
 
AFLR2    : CPU Time          =     0.037   seconds
 
AFLR2 QI : QUALITY IMPROVEMENT
 
AFLR2 QI : Nodes, Faces      =     30019     57794
 
AFLR2    : CPU Time          =     0.003   seconds
 
AFLR2    : DONE

Writing AFLR3 file ....
Finished writing AFLR3 file

Number of nodes = 30019
Number of elements = 60038
Number of tris = 57794
Number of quad = 0
Getting 2D mesh for body 1 (of 1)
 
AFLR2 IC : INPUT DATA CHECK
 
AFLR2 IC : Nodes, Faces      =      2224         0
 
AFLR2    : CPU Time          =     0.000   seconds
 
AFLR2 EG : EDGE GRID RE-GENERATION
 
AFLR2 EG : Nodes, Edges      =      2224      2224
 
AFLR2    : CPU Time          =     0.000   seconds
 
AFLR2 IG : INITIAL GRID GENERATION
 
AFLR2 IG : Nodes, Faces      =         0         2
AFLR2 IG : Nodes, Faces      =       446       894
AFLR2 IG : Nodes, Faces      =       892      1786
AFLR2 IG : Nodes, Faces      =       918      1838
AFLR2 IG : Nodes, Faces      =      1033      2068
AFLR2 IG : Nodes, Faces      =      1133      2268
AFLR2 IG : Nodes, Faces      =      1233      2468
AFLR2 IG : Nodes, Faces      =      1333      2668
AFLR2 IG : Nodes, Faces      =      1338      2678
AFLR2 IG : Nodes, Faces      =      1433      2868
AFLR2 IG : Nodes, Faces      =      1533      3068
AFLR2 IG : Nodes, Faces      =      1633      3268
AFLR2 IG : Nodes, Faces      =      1733      3468
AFLR2 IG : Nodes, Faces      =      1784      3570
AFLR2 IG : Nodes, Faces      =      1833      3668
AFLR2 IG : Nodes, Faces      =      1858      3718
AFLR2 IG : Nodes, Faces      =      2224      4450
AFLR2 IG : Nodes, Faces      =      2228      4450
AFLR2 IG : Nodes, Faces      =      2224      2224
 
AFLR2    : CPU Time          =     0.014   seconds
 
AFLR2 GG : FIELD GRID GENERATION
 
AFLR2 GG : Nodes, Faces      =      2224      2224
AFLR2 GG : Nodes, Faces      =      4120      6016
AFLR2 GG : Nodes, Faces      =      5820      9416
AFLR2 GG : Nodes, Faces      =      7322     12420
AFLR2 GG : Nodes, Faces      =      8613     15002
AFLR2 GG : Nodes, Faces      =      9793     17362
AFLR2 GG : Nodes, Faces      =     10847     19470
AFLR2 GG : Nodes, Faces      =     11828     21432
AFLR2 GG : Nodes, Faces      =     12749     23274
AFLR2 GG : Nodes, Faces      =     13580     24936
AFLR2 GG : Nodes, Faces      =     14355     26486
AFLR2 GG : Nodes, Faces      =     15088     27952
AFLR2 GG : Nodes, Faces      =     15774     29324
AFLR2 GG : Nodes, Faces      =     16420     30616
AFLR2 GG : Nodes, Faces      =     17013     31802
AFLR2 GG : Nodes, Faces      =     17571     32918
AFLR2 GG : Nodes, Faces      =     18089     33954
AFLR2 GG : Nodes, Faces      =     18573     34922
AFLR2 GG : Nodes, Faces      =     19005     35786
AFLR2 GG : Nodes, Faces      =     19413     36602
AFLR2 GG : Nodes, Faces      =     19779     37334
AFLR2 GG : Nodes, Faces      =     20116     38008
AFLR2 GG : Nodes, Faces      =     20443     38662
AFLR2 GG : Nodes, Faces      =     20756     39288
AFLR2 GG : Nodes, Faces      =     21054     39884
AFLR2 GG : Nodes, Faces      =     21344     40464
AFLR2 GG : Nodes, Faces      =     21621     41018
AFLR2 GG : Nodes, Faces      =     21885     41546
AFLR2 GG : Nodes, Faces      =     22137     42050
AFLR2 GG : Nodes, Faces      =     22387     42550
AFLR2 GG : Nodes, Faces      =     22603     42982
AFLR2 GG : Nodes, Faces      =     22772     43320
AFLR2 GG : Nodes, Faces      =     22912     43600
AFLR2 GG : Nodes, Faces      =     23039     43854
AFLR2 GG : Nodes, Faces      =     23142     44060
AFLR2 GG : Nodes, Faces      =     23205     44186
AFLR2 GG : Nodes, Faces      =     23240     44256
AFLR2 GG : Nodes, Faces      =     23257     44290
AFLR2 GG : Nodes, Faces      =     23269     44314
AFLR2 GG : Nodes, Faces      =     23273     44322
 
AFLR2    : CPU Time          =     0.035   seconds
 
AFLR2 QI : QUALITY IMPROVEMENT
 
AFLR2 QI : Nodes, Faces      =     23273     44322
 
AFLR2    : CPU Time          =     0.003   seconds
 
AFLR2    : DONE

Writing AFLR3 file ....
Finished writing AFLR3 file

Number of nodes = 23273
Number of elements = 46546
Number of tris = 44322
Number of quad = 0
 EGADS Info: 0 Objects, 0 Reference in Use (of 0) at Close!
 CAPS Info: Hit last success -- going live!
 CAPS Info: Hit last success -- going live!
 CAPS Info: Hit last success -- going live!
 CAPS Info: Hit last success -- going live!
 CAPS Info: Hit last success -- going live!
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 5
	Name = 2DSlice, index = 1
	Name = TunnelWall, index = 2
	Name = OutFlow, index = 3
	Name = InFlow, index = 4
	Name = Airfoil, index = 5
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 4
	Name = TunnelWall, index = 1
	Name = OutFlow, index = 2
	Name = InFlow, index = 3
	Name = Airfoil, index = 4
Getting 2D mesh for body 1 (of 1)
 
AFLR2    : ---------------------------------------
AFLR2    : AFLR2 LIBRARY
AFLR2    : ADVANCING-FRONT/LOCAL-RECONNECTION
AFLR2    : TRIA/QUAD GRID GENERATOR
AFLR2    : Version Number 9.18.1
AFLR2    : Version Date   06/11/24 @ 05:52PM
AFLR2    : Compile OS     Darwin 23.5.0 arm64
AFLR2    : Compile Date   06/11/24 @ 05:52PM
AFLR2    : Copyright 1994-2021, D.L. Marcum
AFLR2    : ---------------------------------------
 
AFLR2 IC : INPUT DATA CHECK
 
AFLR2 IC : Nodes, Faces      =      2244         0
 
AFLR2    : CPU Time          =     0.000   seconds
 
AFLR2 EG : EDGE GRID RE-GENERATION
 
AFLR2 EG : Nodes, Edges      =      2244      2244
 
AFLR2    : CPU Time          =     0.000   seconds
 
AFLR2 IG : INITIAL GRID GENERATION
 
AFLR2 IG : Nodes, Faces      =         0         2
AFLR2 IG : Nodes, Faces      =       450       902
AFLR2 IG : Nodes, Faces      =       900      1802
AFLR2 IG : Nodes, Faces      =      1145      2292
AFLR2 IG : Nodes, Faces      =      1260      2522
AFLR2 IG : Nodes, Faces      =      1350      2702
AFLR2 IG : Nodes, Faces      =      1360      2722
AFLR2 IG : Nodes, Faces      =      1460      2922
AFLR2 IG : Nodes, Faces      =      1560      3122
AFLR2 IG : Nodes, Faces      =      1660      3322
AFLR2 IG : Nodes, Faces      =      1760      3522
AFLR2 IG : Nodes, Faces      =      1800      3602
AFLR2 IG : Nodes, Faces      =      1860      3722
AFLR2 IG : Nodes, Faces      =      1960      3922
AFLR2 IG : Nodes, Faces      =      2060      4122
AFLR2 IG : Nodes, Faces      =      2085      4172
AFLR2 IG : Nodes, Faces      =      2244      4490
AFLR2 IG : Nodes, Faces      =      2248      4490
AFLR2 IG : Nodes, Faces      =      2244      2244
 
AFLR2    : CPU Time          =     0.014   seconds
 
AFLR2 GG : FIELD GRID GENERATION
 
AFLR2 GG : Nodes, Faces      =      2244      2244
AFLR2 GG : Nodes, Faces      =      4285      6326
AFLR2 GG : Nodes, Faces      =      6135     10026
AFLR2 GG : Nodes, Faces      =      7878     13512
AFLR2 GG : Nodes, Faces      =      9485     16726
AFLR2 GG : Nodes, Faces      =     10981     19718
AFLR2 GG : Nodes, Faces      =     12372     22500
AFLR2 GG : Nodes, Faces      =     13686     25128
AFLR2 GG : Nodes, Faces      =     14908     27572
AFLR2 GG : Nodes, Faces      =     16063     29882
AFLR2 GG : Nodes, Faces      =     17170     32096
AFLR2 GG : Nodes, Faces      =     18222     34200
AFLR2 GG : Nodes, Faces      =     19208     36172
AFLR2 GG : Nodes, Faces      =     20165     38086
AFLR2 GG : Nodes, Faces      =     21087     39930
AFLR2 GG : Nodes, Faces      =     21975     41706
AFLR2 GG : Nodes, Faces      =     22803     43362
AFLR2 GG : Nodes, Faces      =     23582     44920
AFLR2 GG : Nodes, Faces      =     24330     46416
AFLR2 GG : Nodes, Faces      =     25041     47838
AFLR2 GG : Nodes, Faces      =     25723     49202
AFLR2 GG : Nodes, Faces      =     26365     50486
AFLR2 GG : Nodes, Faces      =     26993     51742
AFLR2 GG : Nodes, Faces      =     27556     52868
AFLR2 GG : Nodes, Faces      =     28054     53864
AFLR2 GG : Nodes, Faces      =     28487     54730
AFLR2 GG : Nodes, Faces      =     28847     55450
AFLR2 GG : Nodes, Faces      =     29118     55992
AFLR2 GG : Nodes, Faces      =     29355     56466
AFLR2 GG : Nodes, Faces      =     29553     56862
AFLR2 GG : Nodes, Faces      =     29735     57226
AFLR2 GG : Nodes, Faces      =     29878     57512
AFLR2 GG : Nodes, Faces      =     29969     57694
AFLR2 GG : Nodes, Faces      =     30009     57774
AFLR2 GG : Nodes, Faces      =     30018     57792
AFLR2 GG : Nodes, Faces      =     30019     57794
 
AFLR2    : CPU Time          =     0.037   seconds
 
AFLR2 QI : QUALITY IMPROVEMENT
 
AFLR2 QI : Nodes, Faces      =     30019     57794
 
AFLR2    : CPU Time          =     0.003   seconds
 
AFLR2    : DONE

Writing AFLR3 file ....
Finished writing AFLR3 file

Number of nodes = 30019
Number of elements = 60038
Number of tris = 57794
Number of quad = 0
 CAPS Info: Hit last success -- going live!
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 5
	Name = 2DSlice, index = 1
	Name = TunnelWall, index = 2
	Name = OutFlow, index = 3
	Name = InFlow, index = 4
	Name = Airfoil, index = 5
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 4
	Name = TunnelWall, index = 1
	Name = OutFlow, index = 2
	Name = InFlow, index = 3
	Name = Airfoil, index = 4
 CAPS Info: Hit last success -- going live!
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 5
	Name = 2DSlice, index = 1
	Name = TunnelWall, index = 2
	Name = OutFlow, index = 3
	Name = InFlow, index = 4
	Name = Airfoil, index = 5
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 4
	Name = TunnelWall, index = 1
	Name = OutFlow, index = 2
	Name = InFlow, index = 3
	Name = Airfoil, index = 4
 CAPS Info: Hit last success -- going live!
 CAPS Info: Hit last success -- going live!
 CAPS Info: Hit last success -- going live!
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 5
	Name = 2DSlice, index = 1
	Name = TunnelWall, index = 2
	Name = OutFlow, index = 3
	Name = InFlow, index = 4
	Name = Airfoil, index = 5
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 4
	Name = TunnelWall, index = 1
	Name = OutFlow, index = 2
	Name = InFlow, index = 3
	Name = Airfoil, index = 4
Getting 2D mesh for body 1 (of 1)
 
AFLR2    : ---------------------------------------
AFLR2    : AFLR2 LIBRARY
AFLR2    : ADVANCING-FRONT/LOCAL-RECONNECTION
AFLR2    : TRIA/QUAD GRID GENERATOR
AFLR2    : Version Number 9.18.1
AFLR2    : Version Date   06/11/24 @ 05:52PM
AFLR2    : Compile OS     Darwin 23.5.0 arm64
AFLR2    : Compile Date   06/11/24 @ 05:52PM
AFLR2    : Copyright 1994-2021, D.L. Marcum
AFLR2    : ---------------------------------------
 
AFLR2 IC : INPUT DATA CHECK
 
AFLR2 IC : Nodes, Faces      =      2224         0
 
AFLR2    : CPU Time          =     0.000   seconds
 
AFLR2 EG : EDGE GRID RE-GENERATION
 
AFLR2 EG : Nodes, Edges      =      2224      2224
 
AFLR2    : CPU Time          =     0.000   seconds
 
AFLR2 IG : INITIAL GRID GENERATION
 
AFLR2 IG : Nodes, Faces      =         0         2
AFLR2 IG : Nodes, Faces      =       446       894
AFLR2 IG : Nodes, Faces      =       892      1786
AFLR2 IG : Nodes, Faces      =       918      1838
AFLR2 IG : Nodes, Faces      =      1033      2068
AFLR2 IG : Nodes, Faces      =      1133      2268
AFLR2 IG : Nodes, Faces      =      1233      2468
AFLR2 IG : Nodes, Faces      =      1333      2668
AFLR2 IG : Nodes, Faces      =      1338      2678
AFLR2 IG : Nodes, Faces      =      1433      2868
AFLR2 IG : Nodes, Faces      =      1533      3068
AFLR2 IG : Nodes, Faces      =      1633      3268
AFLR2 IG : Nodes, Faces      =      1733      3468
AFLR2 IG : Nodes, Faces      =      1784      3570
AFLR2 IG : Nodes, Faces      =      1833      3668
AFLR2 IG : Nodes, Faces      =      1858      3718
AFLR2 IG : Nodes, Faces      =      2224      4450
AFLR2 IG : Nodes, Faces      =      2228      4450
AFLR2 IG : Nodes, Faces      =      2224      2224
 
AFLR2    : CPU Time          =     0.014   seconds
 
AFLR2 GG : FIELD GRID GENERATION
 
AFLR2 GG : Nodes, Faces      =      2224      2224
AFLR2 GG : Nodes, Faces      =      4120      6016
AFLR2 GG : Nodes, Faces      =      5820      9416
AFLR2 GG : Nodes, Faces      =      7322     12420
AFLR2 GG : Nodes, Faces      =      8613     15002
AFLR2 GG : Nodes, Faces      =      9793     17362
AFLR2 GG : Nodes, Faces      =     10847     19470
AFLR2 GG : Nodes, Faces      =     11828     21432
AFLR2 GG : Nodes, Faces      =     12749     23274
AFLR2 GG : Nodes, Faces      =     13580     24936
AFLR2 GG : Nodes, Faces      =     14355     26486
AFLR2 GG : Nodes, Faces      =     15088     27952
AFLR2 GG : Nodes, Faces      =     15774     29324
AFLR2 GG : Nodes, Faces      =     16420     30616
AFLR2 GG : Nodes, Faces      =     17013     31802
AFLR2 GG : Nodes, Faces      =     17571     32918
AFLR2 GG : Nodes, Faces      =     18089     33954
AFLR2 GG : Nodes, Faces      =     18573     34922
AFLR2 GG : Nodes, Faces      =     19005     35786
AFLR2 GG : Nodes, Faces      =     19413     36602
AFLR2 GG : Nodes, Faces      =     19779     37334
AFLR2 GG : Nodes, Faces      =     20116     38008
AFLR2 GG : Nodes, Faces      =     20443     38662
AFLR2 GG : Nodes, Faces      =     20756     39288
AFLR2 GG : Nodes, Faces      =     21054     39884
AFLR2 GG : Nodes, Faces      =     21344     40464
AFLR2 GG : Nodes, Faces      =     21621     41018
AFLR2 GG : Nodes, Faces      =     21885     41546
AFLR2 GG : Nodes, Faces      =     22137     42050
AFLR2 GG : Nodes, Faces      =     22387     42550
AFLR2 GG : Nodes, Faces      =     22603     42982
AFLR2 GG : Nodes, Faces      =     22772     43320
AFLR2 GG : Nodes, Faces      =     22912     43600
AFLR2 GG : Nodes, Faces      =     23039     43854
AFLR2 GG : Nodes, Faces      =     23142     44060
AFLR2 GG : Nodes, Faces      =     23205     44186
AFLR2 GG : Nodes, Faces      =     23240     44256
AFLR2 GG : Nodes, Faces      =     23257     44290
AFLR2 GG : Nodes, Faces      =     23269     44314
AFLR2 GG : Nodes, Faces      =     23273     44322
 
AFLR2    : CPU Time          =     0.035   seconds
 
AFLR2 QI : QUALITY IMPROVEMENT
 
AFLR2 QI : Nodes, Faces      =     23273     44322
 
AFLR2    : CPU Time          =     0.003   seconds
 
AFLR2    : DONE

Writing AFLR3 file ....
Finished writing AFLR3 file

Number of nodes = 23273
Number of elements = 46546
Number of tris = 44322
Number of quad = 0
 CAPS Info: Hit last success -- going live!
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 5
	Name = 2DSlice, index = 1
	Name = TunnelWall, index = 2
	Name = OutFlow, index = 3
	Name = InFlow, index = 4
	Name = Airfoil, index = 5
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 4
	Name = TunnelWall, index = 1
	Name = OutFlow, index = 2
	Name = InFlow, index = 3
	Name = Airfoil, index = 4
ok
test_phase (test_aflr2.TestAFLR2.test_phase) ... Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 5
	Name = 2DSlice, index = 1
	Name = TunnelWall, index = 2
	Name = OutFlow, index = 3
	Name = InFlow, index = 4
	Name = Airfoil, index = 5
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 4
	Name = TunnelWall, index = 1
	Name = OutFlow, index = 2
	Name = InFlow, index = 3
	Name = Airfoil, index = 4
Getting 2D mesh for body 1 (of 1)
 
AFLR2    : ---------------------------------------
AFLR2    : AFLR2 LIBRARY
AFLR2    : ADVANCING-FRONT/LOCAL-RECONNECTION
AFLR2    : TRIA/QUAD GRID GENERATOR
AFLR2    : Version Number 9.18.1
AFLR2    : Version Date   06/11/24 @ 05:52PM
AFLR2    : Compile OS     Darwin 23.5.0 arm64
AFLR2    : Compile Date   06/11/24 @ 05:52PM
AFLR2    : Copyright 1994-2021, D.L. Marcum
AFLR2    : ---------------------------------------
 
AFLR2 IC : INPUT DATA CHECK
 
AFLR2 IC : Nodes, Faces      =      2244         0
 
AFLR2    : CPU Time          =     0.000   seconds
 
AFLR2 EG : EDGE GRID RE-GENERATION
 
AFLR2 EG : Nodes, Edges      =      2244      2244
 
AFLR2    : CPU Time          =     0.000   seconds
 
AFLR2 IG : INITIAL GRID GENERATION
 
AFLR2 IG : Nodes, Faces      =         0         2
AFLR2 IG : Nodes, Faces      =       450       902
AFLR2 IG : Nodes, Faces      =       900      1802
AFLR2 IG : Nodes, Faces      =      1145      2292
AFLR2 IG : Nodes, Faces      =      1260      2522
AFLR2 IG : Nodes, Faces      =      1350      2702
AFLR2 IG : Nodes, Faces      =      1360      2722
AFLR2 IG : Nodes, Faces      =      1460      2922
AFLR2 IG : Nodes, Faces      =      1560      3122
AFLR2 IG : Nodes, Faces      =      1660      3322
AFLR2 IG : Nodes, Faces      =      1760      3522
AFLR2 IG : Nodes, Faces      =      1800      3602
AFLR2 IG : Nodes, Faces      =      1860      3722
AFLR2 IG : Nodes, Faces      =      1960      3922
AFLR2 IG : Nodes, Faces      =      2060      4122
AFLR2 IG : Nodes, Faces      =      2085      4172
AFLR2 IG : Nodes, Faces      =      2244      4490
AFLR2 IG : Nodes, Faces      =      2248      4490
AFLR2 IG : Nodes, Faces      =      2244      2244
 
AFLR2    : CPU Time          =     0.014   seconds
 
AFLR2 GG : FIELD GRID GENERATION
 
AFLR2 GG : Nodes, Faces      =      2244      2244
AFLR2 GG : Nodes, Faces      =      4285      6326
AFLR2 GG : Nodes, Faces      =      6135     10026
AFLR2 GG : Nodes, Faces      =      7878     13512
AFLR2 GG : Nodes, Faces      =      9485     16726
AFLR2 GG : Nodes, Faces      =     10981     19718
AFLR2 GG : Nodes, Faces      =     12372     22500
AFLR2 GG : Nodes, Faces      =     13686     25128
AFLR2 GG : Nodes, Faces      =     14908     27572
AFLR2 GG : Nodes, Faces      =     16063     29882
AFLR2 GG : Nodes, Faces      =     17170     32096
AFLR2 GG : Nodes, Faces      =     18222     34200
AFLR2 GG : Nodes, Faces      =     19208     36172
AFLR2 GG : Nodes, Faces      =     20165     38086
AFLR2 GG : Nodes, Faces      =     21087     39930
AFLR2 GG : Nodes, Faces      =     21975     41706
AFLR2 GG : Nodes, Faces      =     22803     43362
AFLR2 GG : Nodes, Faces      =     23582     44920
AFLR2 GG : Nodes, Faces      =     24330     46416
AFLR2 GG : Nodes, Faces      =     25041     47838
AFLR2 GG : Nodes, Faces      =     25723     49202
AFLR2 GG : Nodes, Faces      =     26365     50486
AFLR2 GG : Nodes, Faces      =     26993     51742
AFLR2 GG : Nodes, Faces      =     27556     52868
AFLR2 GG : Nodes, Faces      =     28054     53864
AFLR2 GG : Nodes, Faces      =     28487     54730
AFLR2 GG : Nodes, Faces      =     28847     55450
AFLR2 GG : Nodes, Faces      =     29118     55992
AFLR2 GG : Nodes, Faces      =     29355     56466
AFLR2 GG : Nodes, Faces      =     29553     56862
AFLR2 GG : Nodes, Faces      =     29735     57226
AFLR2 GG : Nodes, Faces      =     29878     57512
AFLR2 GG : Nodes, Faces      =     29969     57694
AFLR2 GG : Nodes, Faces      =     30009     57774
AFLR2 GG : Nodes, Faces      =     30018     57792
AFLR2 GG : Nodes, Faces      =     30019     57794
 
AFLR2    : CPU Time          =     0.037   seconds
 
AFLR2 QI : QUALITY IMPROVEMENT
 
AFLR2 QI : Nodes, Faces      =     30019     57794
 
AFLR2    : CPU Time          =     0.003   seconds
 
AFLR2    : DONE

Writing AFLR3 file ....
Finished writing AFLR3 file

Number of nodes = 30019
Number of elements = 60038
Number of tris = 57794
Number of quad = 0
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 5
	Name = 2DSlice, index = 1
	Name = TunnelWall, index = 2
	Name = OutFlow, index = 3
	Name = InFlow, index = 4
	Name = Airfoil, index = 5
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 4
	Name = TunnelWall, index = 1
	Name = OutFlow, index = 2
	Name = InFlow, index = 3
	Name = Airfoil, index = 4
Getting 2D mesh for body 1 (of 1)
 
AFLR2    : ---------------------------------------
AFLR2    : AFLR2 LIBRARY
AFLR2    : ADVANCING-FRONT/LOCAL-RECONNECTION
AFLR2    : TRIA/QUAD GRID GENERATOR
AFLR2    : Version Number 9.18.1
AFLR2    : Version Date   06/11/24 @ 05:52PM
AFLR2    : Compile OS     Darwin 23.5.0 arm64
AFLR2    : Compile Date   06/11/24 @ 05:52PM
AFLR2    : Copyright 1994-2021, D.L. Marcum
AFLR2    : ---------------------------------------
 
AFLR2 IC : INPUT DATA CHECK
 
AFLR2 IC : Nodes, Faces      =        48         0
 
AFLR2    : CPU Time          =     0.000   seconds
 
AFLR2 EG : EDGE GRID RE-GENERATION
 
AFLR2 EG : Nodes, Edges      =        48        48
 
AFLR2    : CPU Time          =     0.000   seconds
 
AFLR2 IG : INITIAL GRID GENERATION
 
AFLR2 IG : Nodes, Faces      =         0         2
AFLR2 IG : Nodes, Faces      =        10        22
AFLR2 IG : Nodes, Faces      =        20        42
AFLR2 IG : Nodes, Faces      =        30        62
AFLR2 IG : Nodes, Faces      =        40        82
AFLR2 IG : Nodes, Faces      =        45        92
AFLR2 IG : Nodes, Faces      =        46        94
AFLR2 IG : Nodes, Faces      =        48        98
AFLR2 IG : Nodes, Faces      =        52        98
AFLR2 IG : Nodes, Faces      =        48        48
 
AFLR2    : CPU Time          =     0.000   seconds
 
AFLR2 GG : FIELD GRID GENERATION
 
AFLR2 GG : Nodes, Faces      =        48        48
AFLR2 GG : Nodes, Faces      =        88       128
AFLR2 GG : Nodes, Faces      =       109       170
AFLR2 GG : Nodes, Faces      =       124       200
AFLR2 GG : Nodes, Faces      =       136       224
AFLR2 GG : Nodes, Faces      =       148       248
AFLR2 GG : Nodes, Faces      =       160       272
AFLR2 GG : Nodes, Faces      =       172       296
AFLR2 GG : Nodes, Faces      =       182       316
AFLR2 GG : Nodes, Faces      =       188       328
AFLR2 GG : Nodes, Faces      =       190       332
 
AFLR2    : CPU Time          =     0.000   seconds
 
AFLR2 QI : QUALITY IMPROVEMENT
 
AFLR2 QI : Nodes, Faces      =       190       332
 
AFLR2    : CPU Time          =     0.000   seconds
 
AFLR2    : DONE

Writing AFLR3 file ....
Finished writing AFLR3 file

Number of nodes = 190
Number of elements = 380
Number of tris = 332
Number of quad = 0
ok
test_reenter (test_aflr2.TestAFLR2.test_reenter) ... Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 5
	Name = 2DSlice, index = 1
	Name = TunnelWall, index = 2
	Name = OutFlow, index = 3
	Name = InFlow, index = 4
	Name = Airfoil, index = 5
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 4
	Name = TunnelWall, index = 1
	Name = OutFlow, index = 2
	Name = InFlow, index = 3
	Name = Airfoil, index = 4

Getting mesh sizing parameters
	Mesh sizing name - 2DSlice
	Mesh sizing name - Airfoil
	Mesh sizing name - InFlow
	Mesh sizing name - OutFlow
	Mesh sizing name - TunnelWall
	Done getting mesh sizing parameters
Getting 2D mesh for body 1 (of 1)
 
AFLR2    : ---------------------------------------
AFLR2    : AFLR2 LIBRARY
AFLR2    : ADVANCING-FRONT/LOCAL-RECONNECTION
AFLR2    : TRIA/QUAD GRID GENERATOR
AFLR2    : Version Number 9.18.1
AFLR2    : Version Date   06/11/24 @ 05:52PM
AFLR2    : Compile OS     Darwin 23.5.0 arm64
AFLR2    : Compile Date   06/11/24 @ 05:52PM
AFLR2    : Copyright 1994-2021, D.L. Marcum
AFLR2    : ---------------------------------------
 
AFLR2 IC : INPUT DATA CHECK
 
AFLR2 IC : Nodes, Faces      =       344         0
 
AFLR2    : CPU Time          =     0.000   seconds
 
AFLR2 EG : EDGE GRID RE-GENERATION
 
AFLR2 EG : Nodes, Edges      =       344       344
 
AFLR2    : CPU Time          =     0.000   seconds
 
AFLR2 IG : INITIAL GRID GENERATION
 
AFLR2 IG : Nodes, Faces      =         0         2
AFLR2 IG : Nodes, Faces      =        70       142
AFLR2 IG : Nodes, Faces      =       140       282
AFLR2 IG : Nodes, Faces      =       210       422
AFLR2 IG : Nodes, Faces      =       280       562
AFLR2 IG : Nodes, Faces      =       339       680
AFLR2 IG : Nodes, Faces      =       340       682
AFLR2 IG : Nodes, Faces      =       344       690
AFLR2 IG : Nodes, Faces      =       348       690
AFLR2 IG : Nodes, Faces      =       344       344
 
AFLR2    : CPU Time          =     0.000   seconds
 
AFLR2 GG : FIELD GRID GENERATION
 
AFLR2 GG : Nodes, Faces      =       344       344
AFLR2 GG : Nodes, Faces      =       679      1014
AFLR2 GG : Nodes, Faces      =      1006      1668
AFLR2 GG : Nodes, Faces      =      1321      2298
AFLR2 GG : Nodes, Faces      =      1604      2864
AFLR2 GG : Nodes, Faces      =      1886      3428
AFLR2 GG : Nodes, Faces      =      2155      3966
AFLR2 GG : Nodes, Faces      =      2409      4474
AFLR2 GG : Nodes, Faces      =      2649      4954
AFLR2 GG : Nodes, Faces      =      2867      5390
AFLR2 GG : Nodes, Faces      =      3063      5782
AFLR2 GG : Nodes, Faces      =      3243      6142
AFLR2 GG : Nodes, Faces      =      3400      6456
AFLR2 GG : Nodes, Faces      =      3540      6736
AFLR2 GG : Nodes, Faces      =      3665      6986
AFLR2 GG : Nodes, Faces      =      3786      7228
AFLR2 GG : Nodes, Faces      =      3900      7456
AFLR2 GG : Nodes, Faces      =      4010      7676
AFLR2 GG : Nodes, Faces      =      4114      7884
AFLR2 GG : Nodes, Faces      =      4209      8074
AFLR2 GG : Nodes, Faces      =      4292      8240
AFLR2 GG : Nodes, Faces      =      4368      8392
AFLR2 GG : Nodes, Faces      =      4439      8534
AFLR2 GG : Nodes, Faces      =      4503      8662
AFLR2 GG : Nodes, Faces      =      4560      8776
AFLR2 GG : Nodes, Faces      =      4611      8878
AFLR2 GG : Nodes, Faces      =      4650      8956
AFLR2 GG : Nodes, Faces      =      4677      9010
AFLR2 GG : Nodes, Faces      =      4695      9046
AFLR2 GG : Nodes, Faces      =      4705      9066
 
AFLR2    : CPU Time          =     0.004   seconds
 
AFLR2 QI : QUALITY IMPROVEMENT
 
AFLR2 QI : Nodes, Faces      =      4705      9066
 
AFLR2    : CPU Time          =     0.001   seconds
 
AFLR2    : DONE

Writing AFLR3 file ....
Finished writing AFLR3 file

Number of nodes = 4705
Number of elements = 9410
Number of tris = 9066
Number of quad = 0

Writing Binary VTK file ....
Finished writing Binary VTK file


Writing vtk file ....

Writing vtk general file ....
Finished writing vtk file

libMeshb expects 2D meshes in the x-y plane... attempting to rotate mesh!Swapping z and y coordinates!
Writing FAST file ....
Finished writing FAST file


Writing SU2 file ....
SU2 expects 2D meshes in the x-y plane... attempting to rotate mesh!
Swapping z and y coordinates!
Finished writing SU2 file


Writing Binary STL file ....
Finished writing Binary STL file


Writing ASCII STL file ....
Finished writing ASCII STL file


Writing Tecplot file ....
Finished writing Tecplot file


Getting mesh sizing parameters
	Mesh sizing name - 2DSlice
	Mesh sizing name - Airfoil
	Mesh sizing name - InFlow
	Mesh sizing name - OutFlow
	Mesh sizing name - TunnelWall
	Done getting mesh sizing parameters
Getting 2D mesh for body 1 (of 1)
 
AFLR2 IC : INPUT DATA CHECK
 
AFLR2 IC : Nodes, Faces      =       344         0
 
AFLR2    : CPU Time          =     0.000   seconds
 
AFLR2 EG : EDGE GRID RE-GENERATION
 
AFLR2 EG : Nodes, Edges      =       344       344
 
AFLR2    : CPU Time          =     0.000   seconds
 
AFLR2 IG : INITIAL GRID GENERATION
 
AFLR2 IG : Nodes, Faces      =         0         2
AFLR2 IG : Nodes, Faces      =        70       142
AFLR2 IG : Nodes, Faces      =       140       282
AFLR2 IG : Nodes, Faces      =       210       422
AFLR2 IG : Nodes, Faces      =       280       562
AFLR2 IG : Nodes, Faces      =       339       680
AFLR2 IG : Nodes, Faces      =       340       682
AFLR2 IG : Nodes, Faces      =       344       690
AFLR2 IG : Nodes, Faces      =       348       690
AFLR2 IG : Nodes, Faces      =       344       344
 
AFLR2    : CPU Time          =     0.000   seconds
 
AFLR2 GG : FIELD GRID GENERATION
 
AFLR2 GGp: Nodes, Faces      =       344       344
AFLR2 GGp: Nodes, Faces      =       682      1020
AFLR2 GGp: Nodes, Faces      =      1010      1676
AFLR2 GGp: Nodes, Faces      =      1316      2288
AFLR2 GGp: Nodes, Faces      =      1592      2840
AFLR2 GGp: Nodes, Faces      =      1855      3366
AFLR2 GGp: Nodes, Faces      =      2106      3868
AFLR2 GGp: Nodes, Faces      =      2341      4338
AFLR2 GGp: Nodes, Faces      =      2551      4758
AFLR2 GGp: Nodes, Faces      =      2741      5138
AFLR2 GGp: Nodes, Faces      =      2917      5490
AFLR2 GGp: Nodes, Faces      =      3082      5820
AFLR2 GGp: Nodes, Faces      =      3240      6136
AFLR2 GGp: Nodes, Faces      =      3379      6414
AFLR2 GGp: Nodes, Faces      =      3513      6682
AFLR2 GGp: Nodes, Faces      =      3642      6940
AFLR2 GGp: Nodes, Faces      =      3748      7152
AFLR2 GGp: Nodes, Faces      =      3846      7348
AFLR2 GGp: Nodes, Faces      =      3931      7518
AFLR2 GGp: Nodes, Faces      =      3999      7654
AFLR2 GGp: Nodes, Faces      =      4044      7744
AFLR2 GGp: Nodes, Faces      =      4058      7772
 
AFLR2    : CPU Time          =     0.006   seconds
 
AFLR2 QI : QUALITY IMPROVEMENT
 
AFLR2 QI : Nodes, Faces      =      4058      7772
AFLR2 QI : Nodes, Faces      =      4057       364
AFLR2 QI : Nodes, Faces      =      4057      3703
AFLR2 QI : Nodes, Faces      =      4057      7770
AFLR2 QI : Nodes, Faces      =      4056       344
AFLR2 QI : Nodes, Faces      =      4056      3712
AFLR2 QI : Nodes, Faces      =      4056      7768
AFLR2 QI : Nodes, Faces      =      4055       348
AFLR2 QI : Nodes, Faces      =      4055      3709
AFLR2 QI : Nodes, Faces      =      4055      7766
AFLR2 QI : Nodes, Faces      =      4055       392
AFLR2 QI : Nodes, Faces      =      4055      3687
AFLR2 QI : Nodes, Faces      =      4055      7766
AFLR2 QI : Nodes, Faces      =      4055       386
AFLR2 QI : Nodes, Faces      =      4055      3690
AFLR2 QI : Nodes, Faces      =      4055       386
AFLR2 QI : Nodes, Faces      =      4055      3690
 
AFLR2    : CPU Time          =     0.003   seconds
 
AFLR2    : DONE

Writing AFLR3 file ....
Finished writing AFLR3 file

Number of nodes = 4055
Number of elements = 4420
Number of tris = 386
Number of quad = 3690

Writing Binary VTK file ....
Finished writing Binary VTK file


Writing vtk file ....

Writing vtk general file ....
Finished writing vtk file

libMeshb expects 2D meshes in the x-y plane... attempting to rotate mesh!Swapping z and y coordinates!
Writing SU2 file ....
SU2 expects 2D meshes in the x-y plane... attempting to rotate mesh!
Swapping z and y coordinates!
Finished writing SU2 file


Writing Binary STL file ....
Finished writing Binary STL file


Writing ASCII STL file ....
Finished writing ASCII STL file


Writing Tecplot file ....
Finished writing Tecplot file

ok
test_setInput (test_aflr2.TestAFLR2.test_setInput) ... Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 5
	Name = 2DSlice, index = 1
	Name = TunnelWall, index = 2
	Name = OutFlow, index = 3
	Name = InFlow, index = 4
	Name = Airfoil, index = 5
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 4
	Name = TunnelWall, index = 1
	Name = OutFlow, index = 2
	Name = InFlow, index = 3
	Name = Airfoil, index = 4

Getting mesh sizing parameters
	Mesh sizing name - 2DSlice
	Mesh sizing name - Airfoil
	Mesh sizing name - InFlow
	Mesh sizing name - OutFlow
	Mesh sizing name - TunnelWall
	Done getting mesh sizing parameters
Getting 2D mesh for body 1 (of 1)
 
AFLR2    : ---------------------------------------
AFLR2    : AFLR2 LIBRARY
AFLR2    : ADVANCING-FRONT/LOCAL-RECONNECTION
AFLR2    : TRIA/QUAD GRID GENERATOR
AFLR2    : Version Number 9.18.1
AFLR2    : Version Date   06/11/24 @ 05:52PM
AFLR2    : Compile OS     Darwin 23.5.0 arm64
AFLR2    : Compile Date   06/11/24 @ 05:52PM
AFLR2    : Copyright 1994-2021, D.L. Marcum
AFLR2    : ---------------------------------------
 
AFLR2 IC : INPUT DATA CHECK
 
AFLR2 IC : Nodes, Faces      =       344         0
 
AFLR2    : CPU Time          =     0.000   seconds
 
AFLR2 EG : EDGE GRID RE-GENERATION
 
AFLR2 EG : Nodes, Edges      =       344       344
 
AFLR2    : CPU Time          =     0.000   seconds
 
AFLR2 IG : INITIAL GRID GENERATION
 
AFLR2 IG : Nodes, Faces      =         0         2
AFLR2 IG : Nodes, Faces      =        70       142
AFLR2 IG : Nodes, Faces      =       140       282
AFLR2 IG : Nodes, Faces      =       210       422
AFLR2 IG : Nodes, Faces      =       280       562
AFLR2 IG : Nodes, Faces      =       339       680
AFLR2 IG : Nodes, Faces      =       340       682
AFLR2 IG : Nodes, Faces      =       344       690
AFLR2 IG : Nodes, Faces      =       348       690
AFLR2 IG : Nodes, Faces      =       344       344
 
AFLR2    : CPU Time          =     0.000   seconds
 
AFLR2 GG : FIELD GRID GENERATION
 
AFLR2 GGp: Nodes, Faces      =       344       344
AFLR2 GGp: Nodes, Faces      =       682      1020
AFLR2 GGp: Nodes, Faces      =      1010      1676
AFLR2 GGp: Nodes, Faces      =      1316      2288
AFLR2 GGp: Nodes, Faces      =      1592      2840
AFLR2 GGp: Nodes, Faces      =      1855      3366
AFLR2 GGp: Nodes, Faces      =      2106      3868
AFLR2 GGp: Nodes, Faces      =      2341      4338
AFLR2 GGp: Nodes, Faces      =      2551      4758
AFLR2 GGp: Nodes, Faces      =      2741      5138
AFLR2 GGp: Nodes, Faces      =      2917      5490
AFLR2 GGp: Nodes, Faces      =      3082      5820
AFLR2 GGp: Nodes, Faces      =      3240      6136
AFLR2 GGp: Nodes, Faces      =      3379      6414
AFLR2 GGp: Nodes, Faces      =      3513      6682
AFLR2 GGp: Nodes, Faces      =      3642      6940
AFLR2 GGp: Nodes, Faces      =      3748      7152
AFLR2 GGp: Nodes, Faces      =      3846      7348
AFLR2 GGp: Nodes, Faces      =      3931      7518
AFLR2 GGp: Nodes, Faces      =      3999      7654
AFLR2 GGp: Nodes, Faces      =      4044      7744
AFLR2 GGp: Nodes, Faces      =      4058      7772
 
AFLR2    : CPU Time          =     0.006   seconds
 
AFLR2 QI : QUALITY IMPROVEMENT
 
AFLR2 QI : Nodes, Faces      =      4058      7772
AFLR2 QI : Nodes, Faces      =      4057       364
AFLR2 QI : Nodes, Faces      =      4057      3703
AFLR2 QI : Nodes, Faces      =      4057      7770
AFLR2 QI : Nodes, Faces      =      4056       344
AFLR2 QI : Nodes, Faces      =      4056      3712
AFLR2 QI : Nodes, Faces      =      4056      7768
AFLR2 QI : Nodes, Faces      =      4055       348
AFLR2 QI : Nodes, Faces      =      4055      3709
AFLR2 QI : Nodes, Faces      =      4055      7766
AFLR2 QI : Nodes, Faces      =      4055       392
AFLR2 QI : Nodes, Faces      =      4055      3687
AFLR2 QI : Nodes, Faces      =      4055      7766
AFLR2 QI : Nodes, Faces      =      4055       386
AFLR2 QI : Nodes, Faces      =      4055      3690
AFLR2 QI : Nodes, Faces      =      4055       386
AFLR2 QI : Nodes, Faces      =      4055      3690
 
AFLR2    : CPU Time          =     0.003   seconds
 
AFLR2    : DONE

Writing AFLR3 file ....
Finished writing AFLR3 file

Number of nodes = 4055
Number of elements = 4420
Number of tris = 386
Number of quad = 3690

Writing Tecplot file ....
Finished writing Tecplot file

ok
test_Multiple_Mesh (test_aflr3.TestAFLR3.test_Multiple_Mesh) ... ERROR:: BAD STATUS = -276 from matsol (called from solveSketchOrig:63376)
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 7
	Name = box, index = 1
	Name = cylinder, index = 2
	Name = cone, index = 3
	Name = torus, index = 4
	Name = sphere, index = 5
	Name = boxhole, index = 6
	Name = bullet, index = 7
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 1
	Name = box, index = 1
AFLR4    : Proximity BG Surface Grid Generation Skipped
AFLR4    : No Modifications Required
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 1
	Name = box, index = 1
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 7
	Name = box, index = 1
	Name = cylinder, index = 2
	Name = cone, index = 3
	Name = torus, index = 4
	Name = sphere, index = 5
	Name = boxhole, index = 6
	Name = bullet, index = 7
Getting volume mesh for body 1 (of 7)
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = box, index = 1
 
AFLR2    : ---------------------------------------
AFLR2    : AFLR2 LIBRARY
AFLR2    : ADVANCING-FRONT/LOCAL-RECONNECTION
AFLR2    : TRIA/QUAD GRID GENERATOR
AFLR2    : Version Number 9.18.1
AFLR2    : Version Date   06/11/24 @ 05:52PM
AFLR2    : Compile OS     Darwin 23.5.0 arm64
AFLR2    : Compile Date   06/11/24 @ 05:52PM
AFLR2    : Copyright 1994-2021, D.L. Marcum
AFLR2    : ---------------------------------------
 
AFLR4    : ---------------------------------------
AFLR4    : AFLR4 LIBRARY
AFLR4    : ADVANCING-FRONT/LOCAL-RECONNECTION
AFLR4    : TRIA/QUAD SURFACE GRID GENERATOR
AFLR4    : Version Number 11.5.15
AFLR4    : Version Date   07/19/24 @ 07:04PM
AFLR4    : Compile OS     Darwin 23.5.0 arm64
AFLR4    : Compile Date   07/19/24 @ 07:06PM
AFLR4    : Copyright 1994-2021, D.L. Marcum
AFLR4    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.8.1
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.8.1
EGADS    : ---------------------------------------
Volume mesh for body 1 (of 7):
	Number of nodes          = 1198
	Number of elements       = 6307
	Number of triangles      = 1332
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 4975
	Number of pyramids       = 0
	Number of prisms         = 0
	Number of hexahedrals    = 0
Getting volume mesh for body 2 (of 7)
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = cylinder, index = 1

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.8.1
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.8.1
EGADS    : ---------------------------------------
Volume mesh for body 2 (of 7):
	Number of nodes          = 6226
	Number of elements       = 34532
	Number of triangles      = 4438
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 30094
	Number of pyramids       = 0
	Number of prisms         = 0
	Number of hexahedrals    = 0
Getting volume mesh for body 3 (of 7)
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = cone, index = 1

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.8.1
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.8.1
EGADS    : ---------------------------------------
Volume mesh for body 3 (of 7):
	Number of nodes          = 13688
	Number of elements       = 76798
	Number of triangles      = 8142
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 68656
	Number of pyramids       = 0
	Number of prisms         = 0
	Number of hexahedrals    = 0
Getting volume mesh for body 4 (of 7)
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = torus, index = 1

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.8.1
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.8.1
EGADS    : ---------------------------------------
Volume mesh for body 4 (of 7):
	Number of nodes          = 41861
	Number of elements       = 237846
	Number of triangles      = 19888
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 217958
	Number of pyramids       = 0
	Number of prisms         = 0
	Number of hexahedrals    = 0
Getting volume mesh for body 5 (of 7)
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = sphere, index = 1

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.8.1
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.8.1
EGADS    : ---------------------------------------
Volume mesh for body 5 (of 7):
	Number of nodes          = 4339
	Number of elements       = 24073
	Number of triangles      = 3010
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 21063
	Number of pyramids       = 0
	Number of prisms         = 0
	Number of hexahedrals    = 0
Getting volume mesh for body 6 (of 7)
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = boxhole, index = 1

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.8.1
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.8.1
EGADS    : ---------------------------------------
Volume mesh for body 6 (of 7):
	Number of nodes          = 11025
	Number of elements       = 60915
	Number of triangles      = 8632
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 52283
	Number of pyramids       = 0
	Number of prisms         = 0
	Number of hexahedrals    = 0
Getting volume mesh for body 7 (of 7)
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = bullet, index = 1

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.8.1
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.8.1
EGADS    : ---------------------------------------
Volume mesh for body 7 (of 7):
	Number of nodes          = 10398
	Number of elements       = 58234
	Number of triangles      = 6366
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 51868
	Number of pyramids       = 0
	Number of prisms         = 0
	Number of hexahedrals    = 0

Writing Tecplot file ....
Finished writing Tecplot file


Writing Tecplot file ....
Finished writing Tecplot file


Writing Tecplot file ....
Finished writing Tecplot file


Writing Tecplot file ....
Finished writing Tecplot file


Writing Tecplot file ....
Finished writing Tecplot file


Writing Tecplot file ....
Finished writing Tecplot file


Writing Tecplot file ....
Finished writing Tecplot file

AFLR4    : Proximity BG Surface Grid Generation Skipped
AFLR4    : No Modifications Required
Getting volume mesh for body 1 (of 7)

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.8.1
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.8.1
EGADS    : ---------------------------------------
Getting volume mesh for body 2 (of 7)

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.8.1
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.8.1
EGADS    : ---------------------------------------
Getting volume mesh for body 3 (of 7)

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.8.1
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.8.1
EGADS    : ---------------------------------------
Getting volume mesh for body 4 (of 7)

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.8.1
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.8.1
EGADS    : ---------------------------------------
Getting volume mesh for body 5 (of 7)

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.8.1
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.8.1
EGADS    : ---------------------------------------
Getting volume mesh for body 6 (of 7)

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.8.1
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.8.1
EGADS    : ---------------------------------------
Getting volume mesh for body 7 (of 7)

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.8.1
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.8.1
EGADS    : ---------------------------------------
Volume mesh:
	Number of nodes          = 88735
	Number of elements       = 498705
	Number of triangles      = 51808
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 446897
	Number of pyramids       = 0
	Number of prisms         = 0
	Number of hexahedrals    = 0

Writing Tecplot file ....
Finished writing Tecplot file

ok
test_all (test_aflr3.TestAFLR3.test_all) ... ERROR:: BAD STATUS = -276 from matsol (called from solveSketchOrig:63376)
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 8
	Name = box, index = 1
	Name = cylinder, index = 2
	Name = cone, index = 3
	Name = torus, index = 4
	Name = sphere, index = 5
	Name = boxhole, index = 6
	Name = bullet, index = 7
	Name = farfield, index = 8
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 1
	Name = box, index = 1
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 1
	Name = box, index = 1
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 8
	Name = box, index = 1
	Name = cylinder, index = 2
	Name = cone, index = 3
	Name = torus, index = 4
	Name = sphere, index = 5
	Name = boxhole, index = 6
	Name = bullet, index = 7
	Name = farfield, index = 8
Getting volume mesh
 
AFLR2    : ---------------------------------------
AFLR2    : AFLR2 LIBRARY
AFLR2    : ADVANCING-FRONT/LOCAL-RECONNECTION
AFLR2    : TRIA/QUAD GRID GENERATOR
AFLR2    : Version Number 9.18.1
AFLR2    : Version Date   06/11/24 @ 05:52PM
AFLR2    : Compile OS     Darwin 23.5.0 arm64
AFLR2    : Compile Date   06/11/24 @ 05:52PM
AFLR2    : Copyright 1994-2021, D.L. Marcum
AFLR2    : ---------------------------------------
 
AFLR4    : ---------------------------------------
AFLR4    : AFLR4 LIBRARY
AFLR4    : ADVANCING-FRONT/LOCAL-RECONNECTION
AFLR4    : TRIA/QUAD SURFACE GRID GENERATOR
AFLR4    : Version Number 11.5.15
AFLR4    : Version Date   07/19/24 @ 07:04PM
AFLR4    : Compile OS     Darwin 23.5.0 arm64
AFLR4    : Compile Date   07/19/24 @ 07:06PM
AFLR4    : Copyright 1994-2021, D.L. Marcum
AFLR4    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.8.1
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.8.1
EGADS    : ---------------------------------------
Volume mesh:
	Number of nodes          = 17445
	Number of elements       = 99279
	Number of triangles      = 8296
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 90983
	Number of pyramids       = 0
	Number of prisms         = 0
	Number of hexahedrals    = 0

Writing Tecplot file ....
Finished writing Tecplot file

ok
test_box (test_aflr3.TestAFLR3.test_box) ... Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 2
	Name = box, index = 1
	Name = farfield, index = 2
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 1
	Name = box, index = 1
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 1
	Name = box, index = 1
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 2
	Name = box, index = 1
	Name = farfield, index = 2
Getting volume mesh

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.8.1
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.8.1
EGADS    : ---------------------------------------
Volume mesh:
	Number of nodes          = 2585
	Number of elements       = 13784
	Number of triangles      = 2758
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 11026
	Number of pyramids       = 0
	Number of prisms         = 0
	Number of hexahedrals    = 0

Writing Tecplot file ....
Finished writing Tecplot file

ok
test_boxhole (test_aflr3.TestAFLR3.test_boxhole) ... Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 2
	Name = boxhole, index = 1
	Name = farfield, index = 2
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 0
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 0
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 2
	Name = boxhole, index = 1
	Name = farfield, index = 2
Getting volume mesh

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.8.1
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.8.1
EGADS    : ---------------------------------------
Volume mesh:
	Number of nodes          = 3615
	Number of elements       = 19589
	Number of triangles      = 3392
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 16197
	Number of pyramids       = 0
	Number of prisms         = 0
	Number of hexahedrals    = 0

Writing Tecplot file ....
Finished writing Tecplot file

ok
test_bullet (test_aflr3.TestAFLR3.test_bullet) ... Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 2
	Name = bullet, index = 1
	Name = farfield, index = 2
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 0
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 0
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 2
	Name = bullet, index = 1
	Name = farfield, index = 2
Getting volume mesh

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.8.1
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.8.1
EGADS    : ---------------------------------------
Volume mesh:
	Number of nodes          = 5438
	Number of elements       = 30214
	Number of triangles      = 3654
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 26560
	Number of pyramids       = 0
	Number of prisms         = 0
	Number of hexahedrals    = 0

Writing Tecplot file ....
Finished writing Tecplot file

ok
test_cone (test_aflr3.TestAFLR3.test_cone) ... Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 2
	Name = cone, index = 1
	Name = farfield, index = 2
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 0
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 0
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 2
	Name = cone, index = 1
	Name = farfield, index = 2
Getting volume mesh

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.8.1
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.8.1
EGADS    : ---------------------------------------
Volume mesh:
	Number of nodes          = 4697
	Number of elements       = 26013
	Number of triangles      = 3324
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 22689
	Number of pyramids       = 0
	Number of prisms         = 0
	Number of hexahedrals    = 0

Writing Tecplot file ....
Finished writing Tecplot file

ok
test_cylinder (test_aflr3.TestAFLR3.test_cylinder) ... Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 2
	Name = cylinder, index = 1
	Name = farfield, index = 2
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 0
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 0
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 2
	Name = cylinder, index = 1
	Name = farfield, index = 2
Getting volume mesh

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.8.1
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.8.1
EGADS    : ---------------------------------------
Volume mesh:
	Number of nodes          = 5467
	Number of elements       = 30346
	Number of triangles      = 3754
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 26592
	Number of pyramids       = 0
	Number of prisms         = 0
	Number of hexahedrals    = 0

Writing Tecplot file ....
Finished writing Tecplot file

ok
test_faceMatch (test_aflr3.TestAFLR3.test_faceMatch) ... Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = wall, index = 1
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 0
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 0
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = wall, index = 1
Getting volume mesh

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.8.1
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.8.1
EGADS    : ---------------------------------------
Volume mesh:
	Number of nodes          = 2273
	Number of elements       = 12220
	Number of triangles      = 2222
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 9998
	Number of pyramids       = 0
	Number of prisms         = 0
	Number of hexahedrals    = 0

Writing Tecplot file ....
Finished writing Tecplot file

Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 0
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 0
Getting volume mesh for body 1 (of 2)

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.8.1
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.8.1
EGADS    : ---------------------------------------
Getting volume mesh for body 2 (of 2)

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.8.1
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.8.1
EGADS    : ---------------------------------------
Volume mesh:
	Number of nodes          = 2405
	Number of elements       = 12664
	Number of triangles      = 2666
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 9998
	Number of pyramids       = 0
	Number of prisms         = 0
	Number of hexahedrals    = 0

Writing Tecplot file ....
Finished writing Tecplot file

Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 0
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 0
Getting volume mesh for body 1 (of 2)
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = wall, index = 1

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.8.1
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.8.1
EGADS    : ---------------------------------------
Volume mesh for body 1 (of 2):
	Number of nodes          = 1212
	Number of elements       = 6382
	Number of triangles      = 1334
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 5048
	Number of pyramids       = 0
	Number of prisms         = 0
	Number of hexahedrals    = 0
Getting volume mesh for body 2 (of 2)
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = wall, index = 1

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.8.1
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.8.1
EGADS    : ---------------------------------------
Volume mesh for body 2 (of 2):
	Number of nodes          = 1193
	Number of elements       = 6282
	Number of triangles      = 1332
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 4950
	Number of pyramids       = 0
	Number of prisms         = 0
	Number of hexahedrals    = 0

Writing Tecplot file ....
Finished writing Tecplot file


Writing Tecplot file ....
Finished writing Tecplot file

Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = wall, index = 1
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 0
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 0
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = wall, index = 1
Getting volume mesh

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.8.1
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.8.1
EGADS    : ---------------------------------------
Volume mesh:
	Number of nodes          = 3357
	Number of elements       = 18188
	Number of triangles      = 3110
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 15078
	Number of pyramids       = 0
	Number of prisms         = 0
	Number of hexahedrals    = 0

Writing Tecplot file ....
Finished writing Tecplot file

Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 0
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 0
Getting volume mesh for body 1 (of 3)

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.8.1
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.8.1
EGADS    : ---------------------------------------
Getting volume mesh for body 2 (of 3)

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.8.1
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.8.1
EGADS    : ---------------------------------------
Getting volume mesh for body 3 (of 3)

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.8.1
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.8.1
EGADS    : ---------------------------------------
Volume mesh:
	Number of nodes          = 3622
	Number of elements       = 19080
	Number of triangles      = 4002
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 15078
	Number of pyramids       = 0
	Number of prisms         = 0
	Number of hexahedrals    = 0

Writing Tecplot file ....
Finished writing Tecplot file

Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 0
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 0
Getting volume mesh for body 1 (of 3)
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = wall, index = 1

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.8.1
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.8.1
EGADS    : ---------------------------------------
Volume mesh for body 1 (of 3):
	Number of nodes          = 1212
	Number of elements       = 6382
	Number of triangles      = 1334
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 5048
	Number of pyramids       = 0
	Number of prisms         = 0
	Number of hexahedrals    = 0
Getting volume mesh for body 2 (of 3)
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = wall, index = 1

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.8.1
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.8.1
EGADS    : ---------------------------------------
Volume mesh for body 2 (of 3):
	Number of nodes          = 1193
	Number of elements       = 6282
	Number of triangles      = 1332
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 4950
	Number of pyramids       = 0
	Number of prisms         = 0
	Number of hexahedrals    = 0
Getting volume mesh for body 3 (of 3)
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = wall, index = 1

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.8.1
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.8.1
EGADS    : ---------------------------------------
Volume mesh for body 3 (of 3):
	Number of nodes          = 1217
	Number of elements       = 6416
	Number of triangles      = 1336
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 5080
	Number of pyramids       = 0
	Number of prisms         = 0
	Number of hexahedrals    = 0

Writing Tecplot file ....
Finished writing Tecplot file


Writing Tecplot file ....
Finished writing Tecplot file


Writing Tecplot file ....
Finished writing Tecplot file

Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = wall, index = 1
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 0
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 0
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = wall, index = 1
Getting volume mesh

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.8.1
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.8.1
EGADS    : ---------------------------------------
Volume mesh:
	Number of nodes          = 4425
	Number of elements       = 24045
	Number of triangles      = 4000
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 20045
	Number of pyramids       = 0
	Number of prisms         = 0
	Number of hexahedrals    = 0

Writing Tecplot file ....
Finished writing Tecplot file

Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 0
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 0
Getting volume mesh for body 1 (of 4)

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.8.1
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.8.1
EGADS    : ---------------------------------------
Getting volume mesh for body 2 (of 4)

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.8.1
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.8.1
EGADS    : ---------------------------------------
Getting volume mesh for body 3 (of 4)

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.8.1
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.8.1
EGADS    : ---------------------------------------
Getting volume mesh for body 4 (of 4)

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.8.1
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.8.1
EGADS    : ---------------------------------------
Volume mesh:
	Number of nodes          = 4822
	Number of elements       = 25381
	Number of triangles      = 5336
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 20045
	Number of pyramids       = 0
	Number of prisms         = 0
	Number of hexahedrals    = 0

Writing Tecplot file ....
Finished writing Tecplot file

Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 0
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 0
Getting volume mesh for body 1 (of 4)
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = wall, index = 1

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.8.1
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.8.1
EGADS    : ---------------------------------------
Volume mesh for body 1 (of 4):
	Number of nodes          = 1212
	Number of elements       = 6382
	Number of triangles      = 1334
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 5048
	Number of pyramids       = 0
	Number of prisms         = 0
	Number of hexahedrals    = 0
Getting volume mesh for body 2 (of 4)
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = wall, index = 1

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.8.1
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.8.1
EGADS    : ---------------------------------------
Volume mesh for body 2 (of 4):
	Number of nodes          = 1193
	Number of elements       = 6282
	Number of triangles      = 1332
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 4950
	Number of pyramids       = 0
	Number of prisms         = 0
	Number of hexahedrals    = 0
Getting volume mesh for body 3 (of 4)
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = wall, index = 1

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.8.1
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.8.1
EGADS    : ---------------------------------------
Volume mesh for body 3 (of 4):
	Number of nodes          = 1217
	Number of elements       = 6416
	Number of triangles      = 1336
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 5080
	Number of pyramids       = 0
	Number of prisms         = 0
	Number of hexahedrals    = 0
Getting volume mesh for body 4 (of 4)
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = wall, index = 1

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.8.1
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.8.1
EGADS    : ---------------------------------------
Volume mesh for body 4 (of 4):
	Number of nodes          = 1200
	Number of elements       = 6301
	Number of triangles      = 1334
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 4967
	Number of pyramids       = 0
	Number of prisms         = 0
	Number of hexahedrals    = 0

Writing Tecplot file ....
Finished writing Tecplot file


Writing Tecplot file ....
Finished writing Tecplot file


Writing Tecplot file ....
Finished writing Tecplot file


Writing Tecplot file ....
Finished writing Tecplot file

Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = wall, index = 1
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 0
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 0
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = wall, index = 1
Getting volume mesh

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.8.1
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.8.1
EGADS    : ---------------------------------------
Volume mesh:
	Number of nodes          = 5483
	Number of elements       = 29853
	Number of triangles      = 4890
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 24963
	Number of pyramids       = 0
	Number of prisms         = 0
	Number of hexahedrals    = 0

Writing Tecplot file ....
Finished writing Tecplot file

Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 0
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 0
Getting volume mesh for body 1 (of 5)

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.8.1
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.8.1
EGADS    : ---------------------------------------
Getting volume mesh for body 2 (of 5)

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.8.1
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.8.1
EGADS    : ---------------------------------------
Getting volume mesh for body 3 (of 5)

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.8.1
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.8.1
EGADS    : ---------------------------------------
Getting volume mesh for body 4 (of 5)

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.8.1
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.8.1
EGADS    : ---------------------------------------
Getting volume mesh for body 5 (of 5)

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.8.1
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.8.1
EGADS    : ---------------------------------------
Volume mesh:
	Number of nodes          = 6012
	Number of elements       = 31633
	Number of triangles      = 6670
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 24963
	Number of pyramids       = 0
	Number of prisms         = 0
	Number of hexahedrals    = 0

Writing Tecplot file ....
Finished writing Tecplot file

Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 0
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 0
Getting volume mesh for body 1 (of 5)
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = wall, index = 1

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.8.1
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.8.1
EGADS    : ---------------------------------------
Volume mesh for body 1 (of 5):
	Number of nodes          = 1212
	Number of elements       = 6382
	Number of triangles      = 1334
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 5048
	Number of pyramids       = 0
	Number of prisms         = 0
	Number of hexahedrals    = 0
Getting volume mesh for body 2 (of 5)
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = wall, index = 1

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.8.1
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.8.1
EGADS    : ---------------------------------------
Volume mesh for body 2 (of 5):
	Number of nodes          = 1193
	Number of elements       = 6282
	Number of triangles      = 1332
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 4950
	Number of pyramids       = 0
	Number of prisms         = 0
	Number of hexahedrals    = 0
Getting volume mesh for body 3 (of 5)
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = wall, index = 1

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.8.1
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.8.1
EGADS    : ---------------------------------------
Volume mesh for body 3 (of 5):
	Number of nodes          = 1217
	Number of elements       = 6416
	Number of triangles      = 1336
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 5080
	Number of pyramids       = 0
	Number of prisms         = 0
	Number of hexahedrals    = 0
Getting volume mesh for body 4 (of 5)
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = wall, index = 1

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.8.1
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.8.1
EGADS    : ---------------------------------------
Volume mesh for body 4 (of 5):
	Number of nodes          = 1200
	Number of elements       = 6301
	Number of triangles      = 1334
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 4967
	Number of pyramids       = 0
	Number of prisms         = 0
	Number of hexahedrals    = 0
Getting volume mesh for body 5 (of 5)
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = wall, index = 1

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.8.1
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.8.1
EGADS    : ---------------------------------------
Volume mesh for body 5 (of 5):
	Number of nodes          = 1190
	Number of elements       = 6252
	Number of triangles      = 1334
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 4918
	Number of pyramids       = 0
	Number of prisms         = 0
	Number of hexahedrals    = 0

Writing Tecplot file ....
Finished writing Tecplot file


Writing Tecplot file ....
Finished writing Tecplot file


Writing Tecplot file ....
Finished writing Tecplot file


Writing Tecplot file ....
Finished writing Tecplot file


Writing Tecplot file ....
Finished writing Tecplot file

Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = wall, index = 1
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 0
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 0
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = wall, index = 1
Getting volume mesh

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.8.1
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.8.1
EGADS    : ---------------------------------------
Volume mesh:
	Number of nodes          = 6555
	Number of elements       = 35742
	Number of triangles      = 5780
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 29962
	Number of pyramids       = 0
	Number of prisms         = 0
	Number of hexahedrals    = 0

Writing Tecplot file ....
Finished writing Tecplot file

Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 0
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 0
Getting volume mesh for body 1 (of 6)

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.8.1
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.8.1
EGADS    : ---------------------------------------
Getting volume mesh for body 2 (of 6)

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.8.1
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.8.1
EGADS    : ---------------------------------------
Getting volume mesh for body 3 (of 6)

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.8.1
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.8.1
EGADS    : ---------------------------------------
Getting volume mesh for body 4 (of 6)

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.8.1
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.8.1
EGADS    : ---------------------------------------
Getting volume mesh for body 5 (of 6)

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.8.1
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.8.1
EGADS    : ---------------------------------------
Getting volume mesh for body 6 (of 6)

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.8.1
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.8.1
EGADS    : ---------------------------------------
Volume mesh:
	Number of nodes          = 7216
	Number of elements       = 37966
	Number of triangles      = 8004
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 29962
	Number of pyramids       = 0
	Number of prisms         = 0
	Number of hexahedrals    = 0

Writing Tecplot file ....
Finished writing Tecplot file

Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 0
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 0
Getting volume mesh for body 1 (of 6)
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = wall, index = 1

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.8.1
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.8.1
EGADS    : ---------------------------------------
Volume mesh for body 1 (of 6):
	Number of nodes          = 1212
	Number of elements       = 6382
	Number of triangles      = 1334
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 5048
	Number of pyramids       = 0
	Number of prisms         = 0
	Number of hexahedrals    = 0
Getting volume mesh for body 2 (of 6)
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = wall, index = 1

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.8.1
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.8.1
EGADS    : ---------------------------------------
Volume mesh for body 2 (of 6):
	Number of nodes          = 1193
	Number of elements       = 6282
	Number of triangles      = 1332
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 4950
	Number of pyramids       = 0
	Number of prisms         = 0
	Number of hexahedrals    = 0
Getting volume mesh for body 3 (of 6)
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = wall, index = 1

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.8.1
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.8.1
EGADS    : ---------------------------------------
Volume mesh for body 3 (of 6):
	Number of nodes          = 1217
	Number of elements       = 6416
	Number of triangles      = 1336
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 5080
	Number of pyramids       = 0
	Number of prisms         = 0
	Number of hexahedrals    = 0
Getting volume mesh for body 4 (of 6)
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = wall, index = 1

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.8.1
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.8.1
EGADS    : ---------------------------------------
Volume mesh for body 4 (of 6):
	Number of nodes          = 1200
	Number of elements       = 6301
	Number of triangles      = 1334
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 4967
	Number of pyramids       = 0
	Number of prisms         = 0
	Number of hexahedrals    = 0
Getting volume mesh for body 5 (of 6)
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = wall, index = 1

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.8.1
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.8.1
EGADS    : ---------------------------------------
Volume mesh for body 5 (of 6):
	Number of nodes          = 1190
	Number of elements       = 6252
	Number of triangles      = 1334
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 4918
	Number of pyramids       = 0
	Number of prisms         = 0
	Number of hexahedrals    = 0
Getting volume mesh for body 6 (of 6)
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = wall, index = 1

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.8.1
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.8.1
EGADS    : ---------------------------------------
Volume mesh for body 6 (of 6):
	Number of nodes          = 1204
	Number of elements       = 6333
	Number of triangles      = 1334
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 4999
	Number of pyramids       = 0
	Number of prisms         = 0
	Number of hexahedrals    = 0

Writing Tecplot file ....
Finished writing Tecplot file


Writing Tecplot file ....
Finished writing Tecplot file


Writing Tecplot file ....
Finished writing Tecplot file


Writing Tecplot file ....
Finished writing Tecplot file


Writing Tecplot file ....
Finished writing Tecplot file


Writing Tecplot file ....
Finished writing Tecplot file

Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = wall, index = 1
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 0
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 0
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = wall, index = 1
Getting volume mesh

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.8.1
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.8.1
EGADS    : ---------------------------------------
Volume mesh:
	Number of nodes          = 7634
	Number of elements       = 41677
	Number of triangles      = 6670
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 35007
	Number of pyramids       = 0
	Number of prisms         = 0
	Number of hexahedrals    = 0

Writing Tecplot file ....
Finished writing Tecplot file

Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 0
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 0
Getting volume mesh for body 1 (of 7)

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.8.1
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.8.1
EGADS    : ---------------------------------------
Getting volume mesh for body 2 (of 7)

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.8.1
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.8.1
EGADS    : ---------------------------------------
Getting volume mesh for body 3 (of 7)

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.8.1
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.8.1
EGADS    : ---------------------------------------
Getting volume mesh for body 4 (of 7)

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.8.1
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.8.1
EGADS    : ---------------------------------------
Getting volume mesh for body 5 (of 7)

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.8.1
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.8.1
EGADS    : ---------------------------------------
Getting volume mesh for body 6 (of 7)

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.8.1
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.8.1
EGADS    : ---------------------------------------
Getting volume mesh for body 7 (of 7)

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.8.1
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.8.1
EGADS    : ---------------------------------------
Volume mesh:
	Number of nodes          = 8427
	Number of elements       = 44345
	Number of triangles      = 9338
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 35007
	Number of pyramids       = 0
	Number of prisms         = 0
	Number of hexahedrals    = 0

Writing Tecplot file ....
Finished writing Tecplot file

Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 0
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 0
Getting volume mesh for body 1 (of 7)
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = wall, index = 1

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.8.1
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.8.1
EGADS    : ---------------------------------------
Volume mesh for body 1 (of 7):
	Number of nodes          = 1212
	Number of elements       = 6382
	Number of triangles      = 1334
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 5048
	Number of pyramids       = 0
	Number of prisms         = 0
	Number of hexahedrals    = 0
Getting volume mesh for body 2 (of 7)
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = wall, index = 1

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.8.1
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.8.1
EGADS    : ---------------------------------------
Volume mesh for body 2 (of 7):
	Number of nodes          = 1193
	Number of elements       = 6282
	Number of triangles      = 1332
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 4950
	Number of pyramids       = 0
	Number of prisms         = 0
	Number of hexahedrals    = 0
Getting volume mesh for body 3 (of 7)
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = wall, index = 1

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.8.1
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.8.1
EGADS    : ---------------------------------------
Volume mesh for body 3 (of 7):
	Number of nodes          = 1217
	Number of elements       = 6416
	Number of triangles      = 1336
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 5080
	Number of pyramids       = 0
	Number of prisms         = 0
	Number of hexahedrals    = 0
Getting volume mesh for body 4 (of 7)
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = wall, index = 1

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.8.1
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.8.1
EGADS    : ---------------------------------------
Volume mesh for body 4 (of 7):
	Number of nodes          = 1200
	Number of elements       = 6301
	Number of triangles      = 1334
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 4967
	Number of pyramids       = 0
	Number of prisms         = 0
	Number of hexahedrals    = 0
Getting volume mesh for body 5 (of 7)
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = wall, index = 1

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.8.1
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.8.1
EGADS    : ---------------------------------------
Volume mesh for body 5 (of 7):
	Number of nodes          = 1190
	Number of elements       = 6252
	Number of triangles      = 1334
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 4918
	Number of pyramids       = 0
	Number of prisms         = 0
	Number of hexahedrals    = 0
Getting volume mesh for body 6 (of 7)
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = wall, index = 1

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.8.1
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.8.1
EGADS    : ---------------------------------------
Volume mesh for body 6 (of 7):
	Number of nodes          = 1204
	Number of elements       = 6333
	Number of triangles      = 1334
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 4999
	Number of pyramids       = 0
	Number of prisms         = 0
	Number of hexahedrals    = 0
Getting volume mesh for body 7 (of 7)
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = wall, index = 1

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.8.1
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.8.1
EGADS    : ---------------------------------------
Volume mesh for body 7 (of 7):
	Number of nodes          = 1211
	Number of elements       = 6379
	Number of triangles      = 1334
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 5045
	Number of pyramids       = 0
	Number of prisms         = 0
	Number of hexahedrals    = 0

Writing Tecplot file ....
Finished writing Tecplot file


Writing Tecplot file ....
Finished writing Tecplot file


Writing Tecplot file ....
Finished writing Tecplot file


Writing Tecplot file ....
Finished writing Tecplot file


Writing Tecplot file ....
Finished writing Tecplot file


Writing Tecplot file ....
Finished writing Tecplot file


Writing Tecplot file ....
Finished writing Tecplot file

Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = wall, index = 1
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 0
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 0
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = wall, index = 1
Getting volume mesh

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.8.1
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.8.1
EGADS    : ---------------------------------------
Volume mesh:
	Number of nodes          = 19879
	Number of elements       = 110275
	Number of triangles      = 15558
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 94717
	Number of pyramids       = 0
	Number of prisms         = 0
	Number of hexahedrals    = 0

Writing Tecplot file ....
Finished writing Tecplot file

Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 0
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 0
Getting volume mesh for body 1 (of 19)

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.8.1
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.8.1
EGADS    : ---------------------------------------
Getting volume mesh for body 2 (of 19)

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.8.1
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.8.1
EGADS    : ---------------------------------------
Getting volume mesh for body 3 (of 19)

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.8.1
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.8.1
EGADS    : ---------------------------------------
Getting volume mesh for body 4 (of 19)

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.8.1
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.8.1
EGADS    : ---------------------------------------
Getting volume mesh for body 5 (of 19)

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.8.1
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.8.1
EGADS    : ---------------------------------------
Getting volume mesh for body 6 (of 19)

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.8.1
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.8.1
EGADS    : ---------------------------------------
Getting volume mesh for body 7 (of 19)

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.8.1
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.8.1
EGADS    : ---------------------------------------
Getting volume mesh for body 8 (of 19)

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.8.1
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.8.1
EGADS    : ---------------------------------------
Getting volume mesh for body 9 (of 19)

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.8.1
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.8.1
EGADS    : ---------------------------------------
Getting volume mesh for body 10 (of 19)

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.8.1
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.8.1
EGADS    : ---------------------------------------
Getting volume mesh for body 11 (of 19)

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.8.1
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.8.1
EGADS    : ---------------------------------------
Getting volume mesh for body 12 (of 19)

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.8.1
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.8.1
EGADS    : ---------------------------------------
Getting volume mesh for body 13 (of 19)

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.8.1
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.8.1
EGADS    : ---------------------------------------
Getting volume mesh for body 14 (of 19)

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.8.1
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.8.1
EGADS    : ---------------------------------------
Getting volume mesh for body 15 (of 19)

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.8.1
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.8.1
EGADS    : ---------------------------------------
Getting volume mesh for body 16 (of 19)

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.8.1
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.8.1
EGADS    : ---------------------------------------
Getting volume mesh for body 17 (of 19)

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.8.1
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.8.1
EGADS    : ---------------------------------------
Getting volume mesh for body 18 (of 19)

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.8.1
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.8.1
EGADS    : ---------------------------------------
Getting volume mesh for body 19 (of 19)

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.8.1
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.8.1
EGADS    : ---------------------------------------
Volume mesh:
	Number of nodes          = 22822
	Number of elements       = 120055
	Number of triangles      = 25338
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 94717
	Number of pyramids       = 0
	Number of prisms         = 0
	Number of hexahedrals    = 0

Writing Tecplot file ....
Finished writing Tecplot file

Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 0
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 0
Getting volume mesh for body 1 (of 19)
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = wall, index = 1

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.8.1
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.8.1
EGADS    : ---------------------------------------
Volume mesh for body 1 (of 19):
	Number of nodes          = 1212
	Number of elements       = 6382
	Number of triangles      = 1334
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 5048
	Number of pyramids       = 0
	Number of prisms         = 0
	Number of hexahedrals    = 0
Getting volume mesh for body 2 (of 19)
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = wall, index = 1

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.8.1
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.8.1
EGADS    : ---------------------------------------
Volume mesh for body 2 (of 19):
	Number of nodes          = 1193
	Number of elements       = 6282
	Number of triangles      = 1332
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 4950
	Number of pyramids       = 0
	Number of prisms         = 0
	Number of hexahedrals    = 0
Getting volume mesh for body 3 (of 19)
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = wall, index = 1

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.8.1
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.8.1
EGADS    : ---------------------------------------
Volume mesh for body 3 (of 19):
	Number of nodes          = 1217
	Number of elements       = 6416
	Number of triangles      = 1336
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 5080
	Number of pyramids       = 0
	Number of prisms         = 0
	Number of hexahedrals    = 0
Getting volume mesh for body 4 (of 19)
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = wall, index = 1

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.8.1
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.8.1
EGADS    : ---------------------------------------
Volume mesh for body 4 (of 19):
	Number of nodes          = 1200
	Number of elements       = 6301
	Number of triangles      = 1334
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 4967
	Number of pyramids       = 0
	Number of prisms         = 0
	Number of hexahedrals    = 0
Getting volume mesh for body 5 (of 19)
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = wall, index = 1

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.8.1
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.8.1
EGADS    : ---------------------------------------
Volume mesh for body 5 (of 19):
	Number of nodes          = 1190
	Number of elements       = 6252
	Number of triangles      = 1334
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 4918
	Number of pyramids       = 0
	Number of prisms         = 0
	Number of hexahedrals    = 0
Getting volume mesh for body 6 (of 19)
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = wall, index = 1

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.8.1
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.8.1
EGADS    : ---------------------------------------
Volume mesh for body 6 (of 19):
	Number of nodes          = 1204
	Number of elements       = 6333
	Number of triangles      = 1334
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 4999
	Number of pyramids       = 0
	Number of prisms         = 0
	Number of hexahedrals    = 0
Getting volume mesh for body 7 (of 19)
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = wall, index = 1

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.8.1
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.8.1
EGADS    : ---------------------------------------
Volume mesh for body 7 (of 19):
	Number of nodes          = 1211
	Number of elements       = 6379
	Number of triangles      = 1334
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 5045
	Number of pyramids       = 0
	Number of prisms         = 0
	Number of hexahedrals    = 0
Getting volume mesh for body 8 (of 19)
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = wall, index = 1

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.8.1
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.8.1
EGADS    : ---------------------------------------
Volume mesh for body 8 (of 19):
	Number of nodes          = 1220
	Number of elements       = 6413
	Number of triangles      = 1336
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 5077
	Number of pyramids       = 0
	Number of prisms         = 0
	Number of hexahedrals    = 0
Getting volume mesh for body 9 (of 19)
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = wall, index = 1

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.8.1
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.8.1
EGADS    : ---------------------------------------
Volume mesh for body 9 (of 19):
	Number of nodes          = 1214
	Number of elements       = 6396
	Number of triangles      = 1336
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 5060
	Number of pyramids       = 0
	Number of prisms         = 0
	Number of hexahedrals    = 0
Getting volume mesh for body 10 (of 19)
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = wall, index = 1

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.8.1
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.8.1
EGADS    : ---------------------------------------
Volume mesh for body 10 (of 19):
	Number of nodes          = 1192
	Number of elements       = 6262
	Number of triangles      = 1332
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 4930
	Number of pyramids       = 0
	Number of prisms         = 0
	Number of hexahedrals    = 0
Getting volume mesh for body 11 (of 19)
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = wall, index = 1

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.8.1
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.8.1
EGADS    : ---------------------------------------
Volume mesh for body 11 (of 19):
	Number of nodes          = 1201
	Number of elements       = 6326
	Number of triangles      = 1332
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 4994
	Number of pyramids       = 0
	Number of prisms         = 0
	Number of hexahedrals    = 0
Getting volume mesh for body 12 (of 19)
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = wall, index = 1

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.8.1
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.8.1
EGADS    : ---------------------------------------
Volume mesh for body 12 (of 19):
	Number of nodes          = 1206
	Number of elements       = 6356
	Number of triangles      = 1334
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 5022
	Number of pyramids       = 0
	Number of prisms         = 0
	Number of hexahedrals    = 0
Getting volume mesh for body 13 (of 19)
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = wall, index = 1

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.8.1
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.8.1
EGADS    : ---------------------------------------
Volume mesh for body 13 (of 19):
	Number of nodes          = 1187
	Number of elements       = 6236
	Number of triangles      = 1332
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 4904
	Number of pyramids       = 0
	Number of prisms         = 0
	Number of hexahedrals    = 0
Getting volume mesh for body 14 (of 19)
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = wall, index = 1

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.8.1
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.8.1
EGADS    : ---------------------------------------
Volume mesh for body 14 (of 19):
	Number of nodes          = 1197
	Number of elements       = 6293
	Number of triangles      = 1334
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 4959
	Number of pyramids       = 0
	Number of prisms         = 0
	Number of hexahedrals    = 0
Getting volume mesh for body 15 (of 19)
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = wall, index = 1

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.8.1
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.8.1
EGADS    : ---------------------------------------
Volume mesh for body 15 (of 19):
	Number of nodes          = 1180
	Number of elements       = 6202
	Number of triangles      = 1332
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 4870
	Number of pyramids       = 0
	Number of prisms         = 0
	Number of hexahedrals    = 0
Getting volume mesh for body 16 (of 19)
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = wall, index = 1

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.8.1
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.8.1
EGADS    : ---------------------------------------
Volume mesh for body 16 (of 19):
	Number of nodes          = 1197
	Number of elements       = 6289
	Number of triangles      = 1332
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 4957
	Number of pyramids       = 0
	Number of prisms         = 0
	Number of hexahedrals    = 0
Getting volume mesh for body 17 (of 19)
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = wall, index = 1

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.8.1
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.8.1
EGADS    : ---------------------------------------
Volume mesh for body 17 (of 19):
	Number of nodes          = 1208
	Number of elements       = 6351
	Number of triangles      = 1334
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 5017
	Number of pyramids       = 0
	Number of prisms         = 0
	Number of hexahedrals    = 0
Getting volume mesh for body 18 (of 19)
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = wall, index = 1

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.8.1
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.8.1
EGADS    : ---------------------------------------
Volume mesh for body 18 (of 19):
	Number of nodes          = 1193
	Number of elements       = 6277
	Number of triangles      = 1332
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 4945
	Number of pyramids       = 0
	Number of prisms         = 0
	Number of hexahedrals    = 0
Getting volume mesh for body 19 (of 19)
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = wall, index = 1

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.8.1
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.8.1
EGADS    : ---------------------------------------
Volume mesh for body 19 (of 19):
	Number of nodes          = 1200
	Number of elements       = 6309
	Number of triangles      = 1334
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 4975
	Number of pyramids       = 0
	Number of prisms         = 0
	Number of hexahedrals    = 0

Writing Tecplot file ....
Finished writing Tecplot file


Writing Tecplot file ....
Finished writing Tecplot file


Writing Tecplot file ....
Finished writing Tecplot file


Writing Tecplot file ....
Finished writing Tecplot file


Writing Tecplot file ....
Finished writing Tecplot file


Writing Tecplot file ....
Finished writing Tecplot file


Writing Tecplot file ....
Finished writing Tecplot file


Writing Tecplot file ....
Finished writing Tecplot file


Writing Tecplot file ....
Finished writing Tecplot file


Writing Tecplot file ....
Finished writing Tecplot file


Writing Tecplot file ....
Finished writing Tecplot file


Writing Tecplot file ....
Finished writing Tecplot file


Writing Tecplot file ....
Finished writing Tecplot file


Writing Tecplot file ....
Finished writing Tecplot file


Writing Tecplot file ....
Finished writing Tecplot file


Writing Tecplot file ....
Finished writing Tecplot file


Writing Tecplot file ....
Finished writing Tecplot file


Writing Tecplot file ....
Finished writing Tecplot file


Writing Tecplot file ....
Finished writing Tecplot file

ok
test_faceMatch_MultiDomain (test_aflr3.TestAFLR3.test_faceMatch_MultiDomain) ... ../csmData/MultiDomain/example1.csm
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = dummy_att, index = 1
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 0
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 0
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = dummy_att, index = 1
Getting volume mesh

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.8.1
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.8.1
EGADS    : ---------------------------------------
Volume mesh:
	Number of nodes          = 8499
	Number of elements       = 47040
	Number of triangles      = 6258
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 40782
	Number of pyramids       = 0
	Number of prisms         = 0
	Number of hexahedrals    = 0

Writing Tecplot file ....
Finished writing Tecplot file

Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 0
Getting volume mesh for body 1 (of 2)

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.8.1
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.8.1
EGADS    : ---------------------------------------
Getting volume mesh for body 2 (of 2)

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.8.1
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.8.1
EGADS    : ---------------------------------------
Volume mesh:
	Number of nodes          = 8631
	Number of elements       = 47484
	Number of triangles      = 6702
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 40782
	Number of pyramids       = 0
	Number of prisms         = 0
	Number of hexahedrals    = 0

Writing Tecplot file ....
Finished writing Tecplot file

Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 0
Getting volume mesh for body 1 (of 2)
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = dummy_att, index = 1

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.8.1
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.8.1
EGADS    : ---------------------------------------
Volume mesh for body 1 (of 2):
	Number of nodes          = 7444
	Number of elements       = 41254
	Number of triangles      = 5370
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 35884
	Number of pyramids       = 0
	Number of prisms         = 0
	Number of hexahedrals    = 0
Getting volume mesh for body 2 (of 2)
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = dummy_att, index = 1

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.8.1
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.8.1
EGADS    : ---------------------------------------
Volume mesh for body 2 (of 2):
	Number of nodes          = 1187
	Number of elements       = 6230
	Number of triangles      = 1332
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 4898
	Number of pyramids       = 0
	Number of prisms         = 0
	Number of hexahedrals    = 0

Writing Tecplot file ....
Finished writing Tecplot file


Writing Tecplot file ....
Finished writing Tecplot file

../csmData/MultiDomain/example2.csm
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = dummy_att, index = 1
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 0
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 0
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = dummy_att, index = 1
Getting volume mesh

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.8.1
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.8.1
EGADS    : ---------------------------------------
Volume mesh:
	Number of nodes          = 9625
	Number of elements       = 53328
	Number of triangles      = 7146
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 46182
	Number of pyramids       = 0
	Number of prisms         = 0
	Number of hexahedrals    = 0

Writing Tecplot file ....
Finished writing Tecplot file

Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 0
Getting volume mesh for body 1 (of 3)

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.8.1
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.8.1
EGADS    : ---------------------------------------
Getting volume mesh for body 2 (of 3)

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.8.1
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.8.1
EGADS    : ---------------------------------------
Getting volume mesh for body 3 (of 3)

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.8.1
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.8.1
EGADS    : ---------------------------------------
Volume mesh:
	Number of nodes          = 9899
	Number of elements       = 54216
	Number of triangles      = 8034
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 46182
	Number of pyramids       = 0
	Number of prisms         = 0
	Number of hexahedrals    = 0

Writing Tecplot file ....
Finished writing Tecplot file

Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 0
Getting volume mesh for body 1 (of 3)
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = dummy_att, index = 1

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.8.1
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.8.1
EGADS    : ---------------------------------------
Volume mesh for body 1 (of 3):
	Number of nodes          = 7485
	Number of elements       = 41497
	Number of triangles      = 5370
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 36127
	Number of pyramids       = 0
	Number of prisms         = 0
	Number of hexahedrals    = 0
Getting volume mesh for body 2 (of 3)
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = dummy_att, index = 1

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.8.1
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.8.1
EGADS    : ---------------------------------------
Volume mesh for body 2 (of 3):
	Number of nodes          = 1212
	Number of elements       = 6385
	Number of triangles      = 1332
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 5053
	Number of pyramids       = 0
	Number of prisms         = 0
	Number of hexahedrals    = 0
Getting volume mesh for body 3 (of 3)
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = dummy_att, index = 1

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.8.1
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.8.1
EGADS    : ---------------------------------------
Volume mesh for body 3 (of 3):
	Number of nodes          = 1202
	Number of elements       = 6334
	Number of triangles      = 1332
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 5002
	Number of pyramids       = 0
	Number of prisms         = 0
	Number of hexahedrals    = 0

Writing Tecplot file ....
Finished writing Tecplot file


Writing Tecplot file ....
Finished writing Tecplot file


Writing Tecplot file ....
Finished writing Tecplot file

../csmData/MultiDomain/example3.csm
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = dummy_att, index = 1
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 0
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 0
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = dummy_att, index = 1
Getting volume mesh

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.8.1
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.8.1
EGADS    : ---------------------------------------
Volume mesh:
	Number of nodes          = 9302
	Number of elements       = 51451
	Number of triangles      = 6968
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 44483
	Number of pyramids       = 0
	Number of prisms         = 0
	Number of hexahedrals    = 0

Writing Tecplot file ....
Finished writing Tecplot file

Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 0
Getting volume mesh for body 1 (of 3)

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.8.1
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.8.1
EGADS    : ---------------------------------------
Getting volume mesh for body 2 (of 3)

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.8.1
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.8.1
EGADS    : ---------------------------------------
Getting volume mesh for body 3 (of 3)

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.8.1
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.8.1
EGADS    : ---------------------------------------
Volume mesh:
	Number of nodes          = 9522
	Number of elements       = 52179
	Number of triangles      = 7696
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 44483
	Number of pyramids       = 0
	Number of prisms         = 0
	Number of hexahedrals    = 0

Writing Tecplot file ....
Finished writing Tecplot file

Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 0
Getting volume mesh for body 1 (of 3)
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = dummy_att, index = 1

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.8.1
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.8.1
EGADS    : ---------------------------------------
Volume mesh for body 1 (of 3):
	Number of nodes          = 7466
	Number of elements       = 41416
	Number of triangles      = 5368
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 36048
	Number of pyramids       = 0
	Number of prisms         = 0
	Number of hexahedrals    = 0
Getting volume mesh for body 2 (of 3)
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = dummy_att, index = 1

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.8.1
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.8.1
EGADS    : ---------------------------------------
Volume mesh for body 2 (of 3):
	Number of nodes          = 1187
	Number of elements       = 6230
	Number of triangles      = 1332
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 4898
	Number of pyramids       = 0
	Number of prisms         = 0
	Number of hexahedrals    = 0
Getting volume mesh for body 3 (of 3)
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = dummy_att, index = 1

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.8.1
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.8.1
EGADS    : ---------------------------------------
Volume mesh for body 3 (of 3):
	Number of nodes          = 869
	Number of elements       = 4533
	Number of triangles      = 996
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 3537
	Number of pyramids       = 0
	Number of prisms         = 0
	Number of hexahedrals    = 0

Writing Tecplot file ....
Finished writing Tecplot file


Writing Tecplot file ....
Finished writing Tecplot file


Writing Tecplot file ....
Finished writing Tecplot file

../csmData/MultiDomain/example4.csm
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = dummy_att, index = 1
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 0
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 0
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = dummy_att, index = 1
Getting volume mesh

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.8.1
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.8.1
EGADS    : ---------------------------------------
Volume mesh:
	Number of nodes          = 8956
	Number of elements       = 49469
	Number of triangles      = 6784
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 42685
	Number of pyramids       = 0
	Number of prisms         = 0
	Number of hexahedrals    = 0

Writing Tecplot file ....
Finished writing Tecplot file

Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 0
Getting volume mesh for body 1 (of 3)

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.8.1
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.8.1
EGADS    : ---------------------------------------
Getting volume mesh for body 2 (of 3)

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.8.1
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.8.1
EGADS    : ---------------------------------------
Getting volume mesh for body 3 (of 3)

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.8.1
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.8.1
EGADS    : ---------------------------------------
Volume mesh:
	Number of nodes          = 9139
	Number of elements       = 50065
	Number of triangles      = 7380
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 42685
	Number of pyramids       = 0
	Number of prisms         = 0
	Number of hexahedrals    = 0

Writing Tecplot file ....
Finished writing Tecplot file

Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 0
Getting volume mesh for body 1 (of 3)
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = dummy_att, index = 1

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.8.1
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.8.1
EGADS    : ---------------------------------------
Volume mesh for body 1 (of 3):
	Number of nodes          = 7430
	Number of elements       = 41197
	Number of triangles      = 5360
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 35837
	Number of pyramids       = 0
	Number of prisms         = 0
	Number of hexahedrals    = 0
Getting volume mesh for body 2 (of 3)
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = dummy_att, index = 1

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.8.1
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.8.1
EGADS    : ---------------------------------------
Volume mesh for body 2 (of 3):
	Number of nodes          = 1187
	Number of elements       = 6230
	Number of triangles      = 1332
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 4898
	Number of pyramids       = 0
	Number of prisms         = 0
	Number of hexahedrals    = 0
Getting volume mesh for body 3 (of 3)
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = dummy_att, index = 1

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.8.1
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.8.1
EGADS    : ---------------------------------------
Volume mesh for body 3 (of 3):
	Number of nodes          = 522
	Number of elements       = 2638
	Number of triangles      = 688
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 1950
	Number of pyramids       = 0
	Number of prisms         = 0
	Number of hexahedrals    = 0

Writing Tecplot file ....
Finished writing Tecplot file


Writing Tecplot file ....
Finished writing Tecplot file


Writing Tecplot file ....
Finished writing Tecplot file

../csmData/MultiDomain/example6.csm
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = dummy_att, index = 1
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 0
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 0
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = dummy_att, index = 1
Getting volume mesh

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.8.1
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.8.1
EGADS    : ---------------------------------------
Volume mesh:
	Number of nodes          = 8638
	Number of elements       = 47663
	Number of triangles      = 6598
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 41065
	Number of pyramids       = 0
	Number of prisms         = 0
	Number of hexahedrals    = 0

Writing Tecplot file ....
Finished writing Tecplot file

Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 0
Getting volume mesh for body 1 (of 3)

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.8.1
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.8.1
EGADS    : ---------------------------------------
Getting volume mesh for body 2 (of 3)

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.8.1
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.8.1
EGADS    : ---------------------------------------
Getting volume mesh for body 3 (of 3)

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.8.1
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.8.1
EGADS    : ---------------------------------------
Volume mesh:
	Number of nodes          = 8777
	Number of elements       = 48099
	Number of triangles      = 7034
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 41065
	Number of pyramids       = 0
	Number of prisms         = 0
	Number of hexahedrals    = 0

Writing Tecplot file ....
Finished writing Tecplot file

Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 0
Getting volume mesh for body 1 (of 3)
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = dummy_att, index = 1

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.8.1
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.8.1
EGADS    : ---------------------------------------
Volume mesh for body 1 (of 3):
	Number of nodes          = 7402
	Number of elements       = 41032
	Number of triangles      = 5352
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 35680
	Number of pyramids       = 0
	Number of prisms         = 0
	Number of hexahedrals    = 0
Getting volume mesh for body 2 (of 3)
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = dummy_att, index = 1

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.8.1
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.8.1
EGADS    : ---------------------------------------
Volume mesh for body 2 (of 3):
	Number of nodes          = 848
	Number of elements       = 4402
	Number of triangles      = 994
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 3408
	Number of pyramids       = 0
	Number of prisms         = 0
	Number of hexahedrals    = 0
Getting volume mesh for body 3 (of 3)
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = dummy_att, index = 1

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.8.1
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.8.1
EGADS    : ---------------------------------------
Volume mesh for body 3 (of 3):
	Number of nodes          = 527
	Number of elements       = 2665
	Number of triangles      = 688
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 1977
	Number of pyramids       = 0
	Number of prisms         = 0
	Number of hexahedrals    = 0

Writing Tecplot file ....
Finished writing Tecplot file


Writing Tecplot file ....
Finished writing Tecplot file


Writing Tecplot file ....
Finished writing Tecplot file

../csmData/MultiDomain/example7.csm
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = dummy_att, index = 1
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 0
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 0
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = dummy_att, index = 1
Getting volume mesh

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.8.1
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.8.1
EGADS    : ---------------------------------------
Volume mesh:
	Number of nodes          = 9771
	Number of elements       = 54406
	Number of triangles      = 6748
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 47658
	Number of pyramids       = 0
	Number of prisms         = 0
	Number of hexahedrals    = 0

Writing Tecplot file ....
Finished writing Tecplot file

Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 0
Getting volume mesh for body 1 (of 3)

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.8.1
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.8.1
EGADS    : ---------------------------------------
Getting volume mesh for body 2 (of 3)

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.8.1
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.8.1
EGADS    : ---------------------------------------
Getting volume mesh for body 3 (of 3)

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.8.1
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.8.1
EGADS    : ---------------------------------------
Volume mesh:
	Number of nodes          = 10261
	Number of elements       = 56170
	Number of triangles      = 8512
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 47658
	Number of pyramids       = 0
	Number of prisms         = 0
	Number of hexahedrals    = 0

Writing Tecplot file ....
Finished writing Tecplot file

Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 0
Getting volume mesh for body 1 (of 3)
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = dummy_att, index = 1

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.8.1
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.8.1
EGADS    : ---------------------------------------
Volume mesh for body 1 (of 3):
	Number of nodes          = 7355
	Number of elements       = 40784
	Number of triangles      = 5334
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 35450
	Number of pyramids       = 0
	Number of prisms         = 0
	Number of hexahedrals    = 0
Getting volume mesh for body 2 (of 3)
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = dummy_att, index = 1

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.8.1
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.8.1
EGADS    : ---------------------------------------
Volume mesh for body 2 (of 3):
	Number of nodes          = 2663
	Number of elements       = 14238
	Number of triangles      = 2794
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 11444
	Number of pyramids       = 0
	Number of prisms         = 0
	Number of hexahedrals    = 0
Getting volume mesh for body 3 (of 3)
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = dummy_att, index = 1

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.8.1
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.8.1
EGADS    : ---------------------------------------
Volume mesh for body 3 (of 3):
	Number of nodes          = 243
	Number of elements       = 1148
	Number of triangles      = 384
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 764
	Number of pyramids       = 0
	Number of prisms         = 0
	Number of hexahedrals    = 0

Writing Tecplot file ....
Finished writing Tecplot file


Writing Tecplot file ....
Finished writing Tecplot file


Writing Tecplot file ....
Finished writing Tecplot file

../csmData/MultiDomain/example8.csm
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = dummy_att, index = 1
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 0
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 0
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = dummy_att, index = 1
Getting volume mesh

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.8.1
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.8.1
EGADS    : ---------------------------------------
Volume mesh:
	Number of nodes          = 1498
	Number of elements       = 7735
	Number of triangles      = 1986
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 5749
	Number of pyramids       = 0
	Number of prisms         = 0
	Number of hexahedrals    = 0

Writing Tecplot file ....
Finished writing Tecplot file

Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 0
Getting volume mesh for body 1 (of 3)

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.8.1
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.8.1
EGADS    : ---------------------------------------
Getting volume mesh for body 2 (of 3)

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.8.1
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.8.1
EGADS    : ---------------------------------------
Getting volume mesh for body 3 (of 3)

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.8.1
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.8.1
EGADS    : ---------------------------------------
Volume mesh:
	Number of nodes          = 1562
	Number of elements       = 7859
	Number of triangles      = 2110
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 5749
	Number of pyramids       = 0
	Number of prisms         = 0
	Number of hexahedrals    = 0

Writing Tecplot file ....
Finished writing Tecplot file

Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 0
Getting volume mesh for body 1 (of 3)
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = dummy_att, index = 1

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.8.1
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.8.1
EGADS    : ---------------------------------------
Volume mesh for body 1 (of 3):
	Number of nodes          = 1156
	Number of elements       = 6055
	Number of triangles      = 1306
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 4749
	Number of pyramids       = 0
	Number of prisms         = 0
	Number of hexahedrals    = 0
Getting volume mesh for body 2 (of 3)
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = dummy_att, index = 1

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.8.1
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.8.1
EGADS    : ---------------------------------------
Volume mesh for body 2 (of 3):
	Number of nodes          = 362
	Number of elements       = 1644
	Number of triangles      = 720
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 924
	Number of pyramids       = 0
	Number of prisms         = 0
	Number of hexahedrals    = 0
Getting volume mesh for body 3 (of 3)
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = dummy_att, index = 1

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.8.1
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.8.1
EGADS    : ---------------------------------------
Volume mesh for body 3 (of 3):
	Number of nodes          = 44
	Number of elements       = 160
	Number of triangles      = 84
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 76
	Number of pyramids       = 0
	Number of prisms         = 0
	Number of hexahedrals    = 0

Writing Tecplot file ....
Finished writing Tecplot file


Writing Tecplot file ....
Finished writing Tecplot file


Writing Tecplot file ....
Finished writing Tecplot file

../csmData/MultiDomain/example9.csm
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = dummy_att, index = 1
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 0
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 0
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = dummy_att, index = 1
Getting volume mesh

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.8.1
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.8.1
EGADS    : ---------------------------------------
Volume mesh:
	Number of nodes          = 5096
	Number of elements       = 27903
	Number of triangles      = 4076
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 23827
	Number of pyramids       = 0
	Number of prisms         = 0
	Number of hexahedrals    = 0

Writing Tecplot file ....
Finished writing Tecplot file

Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 0
Getting volume mesh for body 1 (of 2)

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.8.1
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.8.1
EGADS    : ---------------------------------------
Getting volume mesh for body 2 (of 2)

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.8.1
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.8.1
EGADS    : ---------------------------------------
Volume mesh:
	Number of nodes          = 5242
	Number of elements       = 28455
	Number of triangles      = 4628
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 23827
	Number of pyramids       = 0
	Number of prisms         = 0
	Number of hexahedrals    = 0

Writing Tecplot file ....
Finished writing Tecplot file

Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 0
Getting volume mesh for body 1 (of 2)
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = dummy_att, index = 1

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.8.1
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.8.1
EGADS    : ---------------------------------------
Volume mesh for body 1 (of 2):
	Number of nodes          = 4905
	Number of elements       = 26939
	Number of triangles      = 4044
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 22895
	Number of pyramids       = 0
	Number of prisms         = 0
	Number of hexahedrals    = 0
Getting volume mesh for body 2 (of 2)
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = dummy_att, index = 1

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.8.1
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.8.1
EGADS    : ---------------------------------------
Volume mesh for body 2 (of 2):
	Number of nodes          = 337
	Number of elements       = 1516
	Number of triangles      = 584
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 932
	Number of pyramids       = 0
	Number of prisms         = 0
	Number of hexahedrals    = 0

Writing Tecplot file ....
Finished writing Tecplot file


Writing Tecplot file ....
Finished writing Tecplot file

../csmData/MultiDomain/multi_prim.csm
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = dummy_att, index = 1
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 0
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 0
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = dummy_att, index = 1
Getting volume mesh

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.8.1
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.8.1
EGADS    : ---------------------------------------
Volume mesh:
	Number of nodes          = 33115
	Number of elements       = 191815
	Number of triangles      = 8476
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 183339
	Number of pyramids       = 0
	Number of prisms         = 0
	Number of hexahedrals    = 0

Writing Tecplot file ....
Finished writing Tecplot file

Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 0
Getting volume mesh for body 1 (of 5)

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.8.1
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.8.1
EGADS    : ---------------------------------------
Getting volume mesh for body 2 (of 5)

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.8.1
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.8.1
EGADS    : ---------------------------------------
Getting volume mesh for body 3 (of 5)

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.8.1
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.8.1
EGADS    : ---------------------------------------
Getting volume mesh for body 4 (of 5)

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.8.1
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.8.1
EGADS    : ---------------------------------------
Getting volume mesh for body 5 (of 5)

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.8.1
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.8.1
EGADS    : ---------------------------------------
Volume mesh:
	Number of nodes          = 36459
	Number of elements       = 205159
	Number of triangles      = 21820
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 183339
	Number of pyramids       = 0
	Number of prisms         = 0
	Number of hexahedrals    = 0

Writing Tecplot file ....
Finished writing Tecplot file

Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 0
Getting volume mesh for body 1 (of 5)
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = dummy_att, index = 1

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.8.1
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.8.1
EGADS    : ---------------------------------------
Volume mesh for body 1 (of 5):
	Number of nodes          = 28820
	Number of elements       = 163772
	Number of triangles      = 15148
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 148624
	Number of pyramids       = 0
	Number of prisms         = 0
	Number of hexahedrals    = 0
Getting volume mesh for body 2 (of 5)
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = dummy_att, index = 1

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.8.1
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.8.1
EGADS    : ---------------------------------------
Volume mesh for body 2 (of 5):
	Number of nodes          = 1416
	Number of elements       = 7524
	Number of triangles      = 1456
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 6068
	Number of pyramids       = 0
	Number of prisms         = 0
	Number of hexahedrals    = 0
Getting volume mesh for body 3 (of 5)
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = dummy_att, index = 1

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.8.1
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.8.1
EGADS    : ---------------------------------------
Volume mesh for body 3 (of 5):
	Number of nodes          = 4240
	Number of elements       = 23511
	Number of triangles      = 2950
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 20561
	Number of pyramids       = 0
	Number of prisms         = 0
	Number of hexahedrals    = 0
Getting volume mesh for body 4 (of 5)
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = dummy_att, index = 1

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.8.1
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.8.1
EGADS    : ---------------------------------------
Volume mesh for body 4 (of 5):
	Number of nodes          = 720
	Number of elements       = 3724
	Number of triangles      = 842
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 2882
	Number of pyramids       = 0
	Number of prisms         = 0
	Number of hexahedrals    = 0
Getting volume mesh for body 5 (of 5)
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = dummy_att, index = 1

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.8.1
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.8.1
EGADS    : ---------------------------------------
Volume mesh for body 5 (of 5):
	Number of nodes          = 1263
	Number of elements       = 6628
	Number of triangles      = 1424
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 5204
	Number of pyramids       = 0
	Number of prisms         = 0
	Number of hexahedrals    = 0

Writing Tecplot file ....
Finished writing Tecplot file


Writing Tecplot file ....
Finished writing Tecplot file


Writing Tecplot file ....
Finished writing Tecplot file


Writing Tecplot file ....
Finished writing Tecplot file


Writing Tecplot file ....
Finished writing Tecplot file

../csmData/MultiDomain/cyl_seam.csm
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = dummy_att, index = 1
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 0
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 0
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = dummy_att, index = 1
Getting volume mesh

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.8.1
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.8.1
EGADS    : ---------------------------------------
Volume mesh:
	Number of nodes          = 16667
	Number of elements       = 94472
	Number of triangles      = 8798
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 85674
	Number of pyramids       = 0
	Number of prisms         = 0
	Number of hexahedrals    = 0

Writing Tecplot file ....
Finished writing Tecplot file

Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 0
Getting volume mesh for body 1 (of 2)

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.8.1
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.8.1
EGADS    : ---------------------------------------
Getting volume mesh for body 2 (of 2)

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.8.1
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.8.1
EGADS    : ---------------------------------------
Volume mesh:
	Number of nodes          = 18591
	Number of elements       = 101848
	Number of triangles      = 16174
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 85674
	Number of pyramids       = 0
	Number of prisms         = 0
	Number of hexahedrals    = 0

Writing Tecplot file ....
Finished writing Tecplot file

Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 0
Getting volume mesh for body 1 (of 2)
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = dummy_att, index = 1

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.8.1
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.8.1
EGADS    : ---------------------------------------
Volume mesh for body 1 (of 2):
	Number of nodes          = 12023
	Number of elements       = 67478
	Number of triangles      = 7138
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 60340
	Number of pyramids       = 0
	Number of prisms         = 0
	Number of hexahedrals    = 0
Getting volume mesh for body 2 (of 2)
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = dummy_att, index = 1

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.8.1
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.8.1
EGADS    : ---------------------------------------
Volume mesh for body 2 (of 2):
	Number of nodes          = 6568
	Number of elements       = 34370
	Number of triangles      = 9036
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 25334
	Number of pyramids       = 0
	Number of prisms         = 0
	Number of hexahedrals    = 0

Writing Tecplot file ....
Finished writing Tecplot file


Writing Tecplot file ....
Finished writing Tecplot file

ok
test_journal (test_aflr3.TestAFLR3.test_journal) ... Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 2
	Name = Farfield, index = 1
	Name = Wing1, index = 2
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 4
	Name = Farfield, index = 1
	Name = riteWing, index = 2
	Name = leftWing, index = 3
	Name = trailingEdge, index = 4
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 4
	Name = Farfield, index = 1
	Name = riteWing, index = 2
	Name = leftWing, index = 3
	Name = trailingEdge, index = 4
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 2
	Name = Farfield, index = 1
	Name = Wing1, index = 2
Getting volume mesh

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.8.1
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.8.1
EGADS    : ---------------------------------------
Volume mesh:
	Number of nodes          = 20469
	Number of elements       = 118417
	Number of triangles      = 5446
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 112971
	Number of pyramids       = 0
	Number of prisms         = 0
	Number of hexahedrals    = 0
Getting volume mesh

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.8.1
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.8.1
EGADS    : ---------------------------------------
Volume mesh:
	Number of nodes          = 19887
	Number of elements       = 115064
	Number of triangles      = 5256
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 109808
	Number of pyramids       = 0
	Number of prisms         = 0
	Number of hexahedrals    = 0
 EGADS Info: 0 Objects, 0 Reference in Use (of 0) at Close!
 CAPS Info: Hit last success -- going live!
 CAPS Info: Hit last success -- going live!
 CAPS Info: Hit last success -- going live!
 CAPS Info: Hit last success -- going live!
 CAPS Info: Hit last success -- going live!
 CAPS Info: Hit last success -- going live!
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 2
	Name = Farfield, index = 1
	Name = Wing1, index = 2
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 4
	Name = Farfield, index = 1
	Name = riteWing, index = 2
	Name = leftWing, index = 3
	Name = trailingEdge, index = 4
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 4
	Name = Farfield, index = 1
	Name = riteWing, index = 2
	Name = leftWing, index = 3
	Name = trailingEdge, index = 4
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 2
	Name = Farfield, index = 1
	Name = Wing1, index = 2
Getting volume mesh

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.8.1
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.8.1
EGADS    : ---------------------------------------
Volume mesh:
	Number of nodes          = 20469
	Number of elements       = 118417
	Number of triangles      = 5446
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 112971
	Number of pyramids       = 0
	Number of prisms         = 0
	Number of hexahedrals    = 0
 CAPS Info: Hit last success -- going live!
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 2
	Name = Farfield, index = 1
	Name = Wing1, index = 2
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 4
	Name = Farfield, index = 1
	Name = riteWing, index = 2
	Name = leftWing, index = 3
	Name = trailingEdge, index = 4
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 4
	Name = Farfield, index = 1
	Name = riteWing, index = 2
	Name = leftWing, index = 3
	Name = trailingEdge, index = 4
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 2
	Name = Farfield, index = 1
	Name = Wing1, index = 2
 CAPS Info: Hit last success -- going live!
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 2
	Name = Farfield, index = 1
	Name = Wing1, index = 2
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 4
	Name = Farfield, index = 1
	Name = riteWing, index = 2
	Name = leftWing, index = 3
	Name = trailingEdge, index = 4
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 4
	Name = Farfield, index = 1
	Name = riteWing, index = 2
	Name = leftWing, index = 3
	Name = trailingEdge, index = 4
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 2
	Name = Farfield, index = 1
	Name = Wing1, index = 2
 CAPS Info: Hit last success -- going live!
 CAPS Info: Hit last success -- going live!
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 2
	Name = Farfield, index = 1
	Name = Wing1, index = 2
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 4
	Name = Farfield, index = 1
	Name = riteWing, index = 2
	Name = leftWing, index = 3
	Name = trailingEdge, index = 4
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 4
	Name = Farfield, index = 1
	Name = riteWing, index = 2
	Name = leftWing, index = 3
	Name = trailingEdge, index = 4
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 2
	Name = Farfield, index = 1
	Name = Wing1, index = 2
Getting volume mesh

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.8.1
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.8.1
EGADS    : ---------------------------------------
Volume mesh:
	Number of nodes          = 19887
	Number of elements       = 115064
	Number of triangles      = 5256
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 109808
	Number of pyramids       = 0
	Number of prisms         = 0
	Number of hexahedrals    = 0
 CAPS Info: Hit last success -- going live!
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 2
	Name = Farfield, index = 1
	Name = Wing1, index = 2
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 4
	Name = Farfield, index = 1
	Name = riteWing, index = 2
	Name = leftWing, index = 3
	Name = trailingEdge, index = 4
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 4
	Name = Farfield, index = 1
	Name = riteWing, index = 2
	Name = leftWing, index = 3
	Name = trailingEdge, index = 4
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 2
	Name = Farfield, index = 1
	Name = Wing1, index = 2
ok
test_phase (test_aflr3.TestAFLR3.test_phase) ... Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 2
	Name = Farfield, index = 1
	Name = Wing1, index = 2
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 4
	Name = Farfield, index = 1
	Name = riteWing, index = 2
	Name = leftWing, index = 3
	Name = trailingEdge, index = 4
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 4
	Name = Farfield, index = 1
	Name = riteWing, index = 2
	Name = leftWing, index = 3
	Name = trailingEdge, index = 4
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 2
	Name = Farfield, index = 1
	Name = Wing1, index = 2
Getting volume mesh

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.8.1
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.8.1
EGADS    : ---------------------------------------
Volume mesh:
	Number of nodes          = 20469
	Number of elements       = 118417
	Number of triangles      = 5446
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 112971
	Number of pyramids       = 0
	Number of prisms         = 0
	Number of hexahedrals    = 0

Writing Tecplot file ....
Finished writing Tecplot file

Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 2
	Name = Farfield, index = 1
	Name = Wing1, index = 2
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 4
	Name = Farfield, index = 1
	Name = riteWing, index = 2
	Name = leftWing, index = 3
	Name = trailingEdge, index = 4
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 4
	Name = Farfield, index = 1
	Name = riteWing, index = 2
	Name = leftWing, index = 3
	Name = trailingEdge, index = 4
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 2
	Name = Farfield, index = 1
	Name = Wing1, index = 2
Getting volume mesh

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.8.1
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.8.1
EGADS    : ---------------------------------------
Volume mesh:
	Number of nodes          = 19887
	Number of elements       = 115064
	Number of triangles      = 5256
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 109808
	Number of pyramids       = 0
	Number of prisms         = 0
	Number of hexahedrals    = 0

Writing Tecplot file ....
Finished writing Tecplot file

ok
test_quad (test_aflr3.TestAFLR3.test_quad) ... Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 2
	Name = Farfield, index = 1
	Name = Wing1, index = 2
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 4
	Name = Farfield, index = 1
	Name = riteWing, index = 2
	Name = leftWing, index = 3
	Name = trailingEdge, index = 4
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 4
	Name = Farfield, index = 1
	Name = riteWing, index = 2
	Name = leftWing, index = 3
	Name = trailingEdge, index = 4
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 2
	Name = Farfield, index = 1
	Name = Wing1, index = 2
Getting volume mesh

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.8.1
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.8.1
EGADS    : ---------------------------------------
Volume mesh:
	Number of nodes          = 28277
	Number of elements       = 127463
	Number of triangles      = 410
	Number of quadrilatarals = 3218
	Number of tetrahedrals   = 116651
	Number of pyramids       = 0
	Number of prisms         = 748
	Number of hexahedrals    = 6436

Writing Binary VTK file ....
Finished writing Binary VTK file


Writing vtk file ....

Writing vtk general file ....
Finished writing vtk file


Writing SU2 file ....
Finished writing SU2 file


Writing Binary STL file ....
Finished writing Binary STL file


Writing ASCII STL file ....
Finished writing ASCII STL file


Writing Tecplot file ....
Finished writing Tecplot file

ok
test_reenter (test_aflr3.TestAFLR3.test_reenter) ... Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 2
	Name = Farfield, index = 1
	Name = Wing1, index = 2
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 4
	Name = Farfield, index = 1
	Name = riteWing, index = 2
	Name = leftWing, index = 3
	Name = trailingEdge, index = 4
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 4
	Name = Farfield, index = 1
	Name = riteWing, index = 2
	Name = leftWing, index = 3
	Name = trailingEdge, index = 4
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 2
	Name = Farfield, index = 1
	Name = Wing1, index = 2
Getting volume mesh

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.8.1
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.8.1
EGADS    : ---------------------------------------
Volume mesh:
	Number of nodes          = 22593
	Number of elements       = 131265
	Number of triangles      = 5542
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 125723
	Number of pyramids       = 0
	Number of prisms         = 0
	Number of hexahedrals    = 0

Writing Binary VTK file ....
Finished writing Binary VTK file


Writing vtk file ....

Writing vtk general file ....
Finished writing vtk file


Writing FAST file ....
Finished writing FAST file


Writing SU2 file ....
Finished writing SU2 file


Writing Binary STL file ....
Finished writing Binary STL file


Writing ASCII STL file ....
Finished writing ASCII STL file


Writing Tecplot file ....
Finished writing Tecplot file

Getting volume mesh

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.8.1
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.8.1
EGADS    : ---------------------------------------
Volume mesh:
	Number of nodes          = 17015
	Number of elements       = 97698
	Number of triangles      = 5384
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 92314
	Number of pyramids       = 0
	Number of prisms         = 0
	Number of hexahedrals    = 0

Writing Binary VTK file ....
Finished writing Binary VTK file


Writing vtk file ....

Writing vtk general file ....
Finished writing vtk file


Writing FAST file ....
Finished writing FAST file


Writing SU2 file ....
Finished writing SU2 file


Writing Binary STL file ....
Finished writing Binary STL file


Writing ASCII STL file ....
Finished writing ASCII STL file


Writing Tecplot file ....
Finished writing Tecplot file

ok
test_setInput (test_aflr3.TestAFLR3.test_setInput) ...  EGADS Info: 0 Objects, 0 Reference in Use (of 0) at Close!
ok
test_sphere (test_aflr3.TestAFLR3.test_sphere) ... Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 2
	Name = sphere, index = 1
	Name = farfield, index = 2
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 0
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 0
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 2
	Name = sphere, index = 1
	Name = farfield, index = 2
Getting volume mesh

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.8.1
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.8.1
EGADS    : ---------------------------------------
Volume mesh:
	Number of nodes          = 4972
	Number of elements       = 27531
	Number of triangles      = 3460
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 24071
	Number of pyramids       = 0
	Number of prisms         = 0
	Number of hexahedrals    = 0

Writing Tecplot file ....
Finished writing Tecplot file

ok
test_torus (test_aflr3.TestAFLR3.test_torus) ... Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 2
	Name = torus, index = 1
	Name = farfield, index = 2
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 0
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 0
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 2
	Name = torus, index = 1
	Name = farfield, index = 2
Getting volume mesh

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.8.1
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.8.1
EGADS    : ---------------------------------------
Volume mesh:
	Number of nodes          = 6395
	Number of elements       = 35692
	Number of triangles      = 4048
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 31644
	Number of pyramids       = 0
	Number of prisms         = 0
	Number of hexahedrals    = 0

Writing Tecplot file ....
Finished writing Tecplot file

ok
test_transp (test_aflr3.TestAFLR3.test_transp) ... Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 4
	Name = Wing1, index = 1
	Name = Wing2, index = 2
	Name = Wake, index = 3
	Name = Farfield, index = 4
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 4
	Name = Wing1, index = 1
	Name = Wing2, index = 2
	Name = Wake, index = 3
	Name = Farfield, index = 4
AFLR4    : Proximity BG Surface Grid Generation Skipped
AFLR4    : No Modifications Required

Writing Tecplot file ....
Finished writing Tecplot file

Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 4
	Name = Wing1, index = 1
	Name = Wing2, index = 2
	Name = Wake, index = 3
	Name = Farfield, index = 4
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 4
	Name = Wing1, index = 1
	Name = Wing2, index = 2
	Name = Wake, index = 3
	Name = Farfield, index = 4

Getting mesh sizing parameters
	Mesh sizing name - Wake
	Done getting mesh sizing parameters
Getting volume mesh

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.8.1
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.8.1
EGADS    : ---------------------------------------
Volume mesh:
	Number of nodes          = 43250
	Number of elements       = 250033
	Number of triangles      = 11826
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 238207
	Number of pyramids       = 0
	Number of prisms         = 0
	Number of hexahedrals    = 0

Writing Tecplot file ....
Finished writing Tecplot file


Getting mesh sizing parameters
	Mesh sizing name - Wake
	Done getting mesh sizing parameters
Getting volume mesh

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.8.1
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.8.1
EGADS    : ---------------------------------------
Volume mesh:
	Number of nodes          = 47245
	Number of elements       = 273764
	Number of triangles      = 11696
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 262068
	Number of pyramids       = 0
	Number of prisms         = 0
	Number of hexahedrals    = 0

Writing Tecplot file ....
Finished writing Tecplot file


Getting mesh sizing parameters
	Mesh sizing name - Wake
	Done getting mesh sizing parameters
Getting volume mesh

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.8.1
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.8.1
EGADS    : ---------------------------------------
Volume mesh:
	Number of nodes          = 43250
	Number of elements       = 249903
	Number of triangles      = 11696
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 238207
	Number of pyramids       = 0
	Number of prisms         = 0
	Number of hexahedrals    = 0

Writing Tecplot file ....
Finished writing Tecplot file

ok
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 2
	Name = Farfield, index = 1
	Name = Wing1, index = 2
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 4
	Name = Farfield, index = 1
	Name = riteWing, index = 2
	Name = leftWing, index = 3
	Name = trailingEdge, index = 4
test_Edge_scaleFactor (test_aflr4.TestAFLR4.test_Edge_scaleFactor) ... Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 2
	Name = Farfield, index = 1
	Name = Wing1, index = 2
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 4
	Name = Farfield, index = 1
	Name = riteWing, index = 2
	Name = leftWing, index = 3
	Name = trailingEdge, index = 4

Getting mesh sizing parameters
	Mesh sizing name - trailingEdge
	Done getting mesh sizing parameters
ok
test_Face_scaleFactor (test_aflr4.TestAFLR4.test_Face_scaleFactor) ... Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 2
	Name = Farfield, index = 1
	Name = Wing1, index = 2
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 4
	Name = Farfield, index = 1
	Name = riteWing, index = 2
	Name = leftWing, index = 3
	Name = trailingEdge, index = 4

Getting mesh sizing parameters
	Mesh sizing name - leftWing
	Done getting mesh sizing parameters
ok
test_all (test_aflr4.TestAFLR4.test_all) ... ERROR:: BAD STATUS = -276 from matsol (called from solveSketchOrig:63376)
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 8
	Name = box, index = 1
	Name = cylinder, index = 2
	Name = cone, index = 3
	Name = torus, index = 4
	Name = sphere, index = 5
	Name = boxhole, index = 6
	Name = bullet, index = 7
	Name = farfield, index = 8
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 1
	Name = box, index = 1
ok
test_box (test_aflr4.TestAFLR4.test_box) ... Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 2
	Name = box, index = 1
	Name = farfield, index = 2
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 1
	Name = box, index = 1
ok
test_boxhole (test_aflr4.TestAFLR4.test_boxhole) ... Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 2
	Name = boxhole, index = 1
	Name = farfield, index = 2
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 0
ok
test_bullet (test_aflr4.TestAFLR4.test_bullet) ... Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 2
	Name = bullet, index = 1
	Name = farfield, index = 2
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 0
ok
test_cone (test_aflr4.TestAFLR4.test_cone) ... Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 2
	Name = cone, index = 1
	Name = farfield, index = 2
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 0
ok
test_cylinder (test_aflr4.TestAFLR4.test_cylinder) ... Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 2
	Name = cylinder, index = 1
	Name = farfield, index = 2
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 0
ok
test_erw (test_aflr4.TestAFLR4.test_erw) ... Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 2
	Name = Farfield, index = 1
	Name = Wing1, index = 2
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 4
	Name = Farfield, index = 1
	Name = riteWing, index = 2
	Name = leftWing, index = 3
	Name = trailingEdge, index = 4

Getting mesh sizing parameters
	Mesh sizing name - leftWing
	Done getting mesh sizing parameters
ok
test_faceMatch (test_aflr4.TestAFLR4.test_faceMatch) ... Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = wall, index = 1
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 0
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 0
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 0
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = wall, index = 1
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 0
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 0
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 0
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = wall, index = 1
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 0
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 0
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 0
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = wall, index = 1
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 0
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 0
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 0
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = wall, index = 1
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 0
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 0
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 0
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = wall, index = 1
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 0
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 0
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 0
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = wall, index = 1
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 0
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 0
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 0
ok
test_faceMatch_MultiDomain (test_aflr4.TestAFLR4.test_faceMatch_MultiDomain) ... ../csmData/MultiDomain/example1.csm
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = dummy_att, index = 1
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 0

Writing Tecplot file ....
Finished writing Tecplot file

Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 0

Writing Tecplot file ....
Finished writing Tecplot file

Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 0

Writing Tecplot file ....
Finished writing Tecplot file


Writing Tecplot file ....
Finished writing Tecplot file

../csmData/MultiDomain/example2.csm
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = dummy_att, index = 1
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 0

Writing Tecplot file ....
Finished writing Tecplot file

Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 0

Writing Tecplot file ....
Finished writing Tecplot file

Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 0

Writing Tecplot file ....
Finished writing Tecplot file


Writing Tecplot file ....
Finished writing Tecplot file


Writing Tecplot file ....
Finished writing Tecplot file

../csmData/MultiDomain/example3.csm
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = dummy_att, index = 1
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 0

Writing Tecplot file ....
Finished writing Tecplot file

Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 0

Writing Tecplot file ....
Finished writing Tecplot file

Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 0

Writing Tecplot file ....
Finished writing Tecplot file


Writing Tecplot file ....
Finished writing Tecplot file


Writing Tecplot file ....
Finished writing Tecplot file

../csmData/MultiDomain/example4.csm
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = dummy_att, index = 1
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 0

Writing Tecplot file ....
Finished writing Tecplot file

Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 0

Writing Tecplot file ....
Finished writing Tecplot file

Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 0

Writing Tecplot file ....
Finished writing Tecplot file


Writing Tecplot file ....
Finished writing Tecplot file


Writing Tecplot file ....
Finished writing Tecplot file

../csmData/MultiDomain/example6.csm
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = dummy_att, index = 1
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 0

Writing Tecplot file ....
Finished writing Tecplot file

Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 0

Writing Tecplot file ....
Finished writing Tecplot file

Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 0

Writing Tecplot file ....
Finished writing Tecplot file


Writing Tecplot file ....
Finished writing Tecplot file


Writing Tecplot file ....
Finished writing Tecplot file

../csmData/MultiDomain/example7.csm
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = dummy_att, index = 1
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 0

Writing Tecplot file ....
Finished writing Tecplot file

Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 0

Writing Tecplot file ....
Finished writing Tecplot file

Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 0

Writing Tecplot file ....
Finished writing Tecplot file


Writing Tecplot file ....
Finished writing Tecplot file


Writing Tecplot file ....
Finished writing Tecplot file

../csmData/MultiDomain/example8.csm
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = dummy_att, index = 1
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 0

Writing Tecplot file ....
Finished writing Tecplot file

Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 0

Writing Tecplot file ....
Finished writing Tecplot file

Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 0

Writing Tecplot file ....
Finished writing Tecplot file


Writing Tecplot file ....
Finished writing Tecplot file


Writing Tecplot file ....
Finished writing Tecplot file

../csmData/MultiDomain/example9.csm
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = dummy_att, index = 1
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 0

Writing Tecplot file ....
Finished writing Tecplot file

Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 0

Writing Tecplot file ....
Finished writing Tecplot file

Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 0

Writing Tecplot file ....
Finished writing Tecplot file


Writing Tecplot file ....
Finished writing Tecplot file

../csmData/MultiDomain/multi_prim.csm
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = dummy_att, index = 1
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 0

Writing Tecplot file ....
Finished writing Tecplot file

Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 0

Writing Tecplot file ....
Finished writing Tecplot file

Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 0

Writing Tecplot file ....
Finished writing Tecplot file


Writing Tecplot file ....
Finished writing Tecplot file


Writing Tecplot file ....
Finished writing Tecplot file


Writing Tecplot file ....
Finished writing Tecplot file


Writing Tecplot file ....
Finished writing Tecplot file

../csmData/MultiDomain/cyl_seam.csm
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = dummy_att, index = 1
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 0

Writing Tecplot file ....
Finished writing Tecplot file

Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 0

Writing Tecplot file ....
Finished writing Tecplot file

Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 0

Writing Tecplot file ....
Finished writing Tecplot file


Writing Tecplot file ....
Finished writing Tecplot file

ok
test_ff_cdfr (test_aflr4.TestAFLR4.test_ff_cdfr) ... Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 2
	Name = Farfield, index = 1
	Name = Wing1, index = 2
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 4
	Name = Farfield, index = 1
	Name = riteWing, index = 2
	Name = leftWing, index = 3
	Name = trailingEdge, index = 4
ok
test_invalid_Mesh_Lenght_Scale (test_aflr4.TestAFLR4.test_invalid_Mesh_Lenght_Scale) ... Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 2
	Name = Farfield, index = 1
	Name = Wing1, index = 2
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 4
	Name = Farfield, index = 1
	Name = riteWing, index = 2
	Name = leftWing, index = 3
	Name = trailingEdge, index = 4
ok
test_journal (test_aflr4.TestAFLR4.test_journal) ... ERROR:: BAD STATUS = -276 from matsol (called from solveSketchOrig:63376)
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 2
	Name = box, index = 1
	Name = farfield, index = 2
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 1
	Name = box, index = 1
 EGADS Info: 0 Objects, 0 Reference in Use (of 0) at Close!
ERROR:: BAD STATUS = -276 from matsol (called from solveSketchOrig:63376)
ERROR:: BAD STATUS = -276 from matsol (called from solveSketchOrig:63376)
 CAPS Info: Hit last success -- going live!
ERROR:: BAD STATUS = -276 from matsol (called from solveSketchOrig:63376)
 CAPS Info: Hit last success -- going live!
ERROR:: BAD STATUS = -276 from matsol (called from solveSketchOrig:63376)
 CAPS Info: Hit last success -- going live!
ERROR:: BAD STATUS = -276 from matsol (called from solveSketchOrig:63376)
 CAPS Info: Hit last success -- going live!
ERROR:: BAD STATUS = -276 from matsol (called from solveSketchOrig:63376)
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 2
	Name = box, index = 1
	Name = farfield, index = 2
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 1
	Name = box, index = 1
ERROR:: BAD STATUS = -276 from matsol (called from solveSketchOrig:63376)
 CAPS Info: Hit last success -- going live!
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 2
	Name = box, index = 1
	Name = farfield, index = 2
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 1
	Name = box, index = 1
ERROR:: BAD STATUS = -276 from matsol (called from solveSketchOrig:63376)
 CAPS Info: Hit last success -- going live!
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 2
	Name = box, index = 1
	Name = farfield, index = 2
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 1
	Name = box, index = 1
ERROR:: BAD STATUS = -276 from matsol (called from solveSketchOrig:63376)
 CAPS Info: Hit last success -- going live!
ERROR:: BAD STATUS = -276 from matsol (called from solveSketchOrig:63376)
 CAPS Info: Hit last success -- going live!
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 2
	Name = box, index = 1
	Name = farfield, index = 2
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 1
	Name = box, index = 1
ERROR:: BAD STATUS = -276 from matsol (called from solveSketchOrig:63376)
 CAPS Info: Hit last success -- going live!
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 2
	Name = box, index = 1
	Name = farfield, index = 2
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 1
	Name = box, index = 1
ERROR:: BAD STATUS = -276 from matsol (called from solveSketchOrig:63376)
ok
test_max_min_scale (test_aflr4.TestAFLR4.test_max_min_scale) ... Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 2
	Name = Farfield, index = 1
	Name = Wing1, index = 2
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 4
	Name = Farfield, index = 1
	Name = riteWing, index = 2
	Name = leftWing, index = 3
	Name = trailingEdge, index = 4
ok
test_phase (test_aflr4.TestAFLR4.test_phase) ... ERROR:: BAD STATUS = -276 from matsol (called from solveSketchOrig:63376)
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 2
	Name = box, index = 1
	Name = farfield, index = 2
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 1
	Name = box, index = 1
ERROR:: BAD STATUS = -276 from matsol (called from solveSketchOrig:63376)
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 2
	Name = box, index = 1
	Name = farfield, index = 2
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 1
	Name = box, index = 1
ok
test_proximity (test_aflr4.TestAFLR4.test_proximity) ... Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 4
	Name = Wing1, index = 1
	Name = Wing2, index = 2
	Name = Wake, index = 3
	Name = Farfield, index = 4
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 4
	Name = Wing1, index = 1
	Name = Wing2, index = 2
	Name = Wake, index = 3
	Name = Farfield, index = 4

Getting mesh sizing parameters
	Mesh sizing name - Wing1
	Mesh sizing name - Wing2
	Done getting mesh sizing parameters
AFLR4    : Proximity BG Surface Grid Generation Skipped
AFLR4    : No Modifications Required
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 4
	Name = Wing1, index = 1
	Name = Wing2, index = 2
	Name = Wake, index = 3
	Name = Farfield, index = 4
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 4
	Name = Wing1, index = 1
	Name = Wing2, index = 2
	Name = Wake, index = 3
	Name = Farfield, index = 4

Getting mesh sizing parameters
	Mesh sizing name - Wing1
	Mesh sizing name - Wing2
	Done getting mesh sizing parameters
ok
test_quad (test_aflr4.TestAFLR4.test_quad) ... Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 2
	Name = Farfield, index = 1
	Name = Wing1, index = 2
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 4
	Name = Farfield, index = 1
	Name = riteWing, index = 2
	Name = leftWing, index = 3
	Name = trailingEdge, index = 4

Writing Binary VTK file ....
Finished writing Binary VTK file


Writing vtk file ....

Writing vtk general file ....
Finished writing vtk file


Writing SU2 file ....
Finished writing SU2 file


Writing Binary STL file ....
Finished writing Binary STL file


Writing ASCII STL file ....
Finished writing ASCII STL file


Writing Tecplot file ....
Finished writing Tecplot file


Writing ugrid file ....
Finished writing ugrid file

ok
test_reenter (test_aflr4.TestAFLR4.test_reenter) ... Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 2
	Name = Farfield, index = 1
	Name = Wing1, index = 2
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 4
	Name = Farfield, index = 1
	Name = riteWing, index = 2
	Name = leftWing, index = 3
	Name = trailingEdge, index = 4

Writing Binary VTK file ....
Finished writing Binary VTK file


Writing vtk file ....

Writing vtk surface file ....

capsGroups found:
  1: Farfield
  2: Wing1
Finished writing vtk file


Writing FAST file ....
Finished writing FAST file


Writing SU2 file ....
Finished writing SU2 file


Writing Binary STL file ....
Finished writing Binary STL file


Writing ASCII STL file ....
Finished writing ASCII STL file


Writing Tecplot file ....
Finished writing Tecplot file


Writing ugrid file ....
Finished writing ugrid file


Writing Binary VTK file ....
Finished writing Binary VTK file


Writing vtk file ....

Writing vtk surface file ....

capsGroups found:
  1: Farfield
  2: Wing1
Finished writing vtk file


Writing FAST file ....
Finished writing FAST file


Writing SU2 file ....
Finished writing SU2 file


Writing Binary STL file ....
Finished writing Binary STL file


Writing ASCII STL file ....
Finished writing ASCII STL file


Writing Tecplot file ....
Finished writing Tecplot file


Writing ugrid file ....
Finished writing ugrid file

ok
test_regions (test_aflr4.TestAFLR4.test_regions) ... Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 2
	Name = box, index = 1
	Name = cut, index = 2
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 0

Writing Binary VTK file ....
Finished writing Binary VTK file


Writing vtk file ....

Writing vtk surface file ....

capsGroups found:
  1: box
  2: cut
Finished writing vtk file


Writing FAST file ....
Finished writing FAST file


Writing SU2 file ....
Finished writing SU2 file


Writing Binary STL file ....
Finished writing Binary STL file


Writing ASCII STL file ....
Finished writing ASCII STL file


Writing Tecplot file ....
Finished writing Tecplot file


Writing ugrid file ....
Finished writing ugrid file

ok
test_setInput (test_aflr4.TestAFLR4.test_setInput) ... ok
test_skin (test_aflr4.TestAFLR4.test_skin) ... Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 5
	Name = Ribs, index = 1
	Name = Skin, index = 2
	Name = Spar1, index = 3
	Name = Rib_Root, index = 4
	Name = Spar2, index = 5
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 2
	Name = LeadingEdge, index = 1
	Name = TrailingEdge, index = 2

Writing Binary VTK file ....
Finished writing Binary VTK file


Writing vtk file ....

Writing vtk surface file ....

capsGroups found:
  1: Ribs
  2: Skin
  3: Spar1
  4: Rib_Root
  5: Spar2
Finished writing vtk file


Writing FAST file ....
Finished writing FAST file


Writing SU2 file ....
Finished writing SU2 file


Writing Binary STL file ....
Finished writing Binary STL file


Writing ASCII STL file ....
Finished writing ASCII STL file


Writing Tecplot file ....
Finished writing Tecplot file


Writing ugrid file ....
Finished writing ugrid file

ok
test_sphere (test_aflr4.TestAFLR4.test_sphere) ... Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 2
	Name = sphere, index = 1
	Name = farfield, index = 2
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 0
ok
test_torus (test_aflr4.TestAFLR4.test_torus) ... Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 2
	Name = torus, index = 1
	Name = farfield, index = 2
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 0
ok
test_Aeroelastic (test_astros.TestAstros.test_Aeroelastic) ... Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 2
	Name = Rib_Root, index = 1
	Name = Skin, index = 2
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 0
Getting surface mesh for body 1 (of 2)
Getting surface mesh for body 2 (of 2)
Body 1 (of 2)
Number of nodes    = 1
Number of elements = 0
Number of triangle elements      = 0
Number of quadrilateral elements = 0
Body 2 (of 2)
Number of nodes    = 46
Number of elements = 44
Number of triangle elements      = 0
Number of quadrilateral elements = 44
----------------------------
Total number of nodes    = 47
Total number of elements = 44
Mapping Csys attributes ................
	Number of unique Csys attributes = 0

Getting FEA coordinate systems.......
	Number of coordinate systems - 0
	No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
	Number of unique capsConstraint attributes = 1
	Name = Rib_Root_Point, index = 1
Mapping capsLoad attributes ................
	Number of unique capsLoad attributes = 0
Mapping capsBound attributes ................
	Number of unique capsBound attributes = 1
	Name = Skin_Top, index = 1
Mapping capsConnect attributes ................
	Number of unique capsConnect attributes = 1
	Name = Rib_Root, index = 1
Mapping capsResponse attributes ................
	Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
	Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 3
	Name = Rib_Root, index = 1
	Name = Skin, index = 2
	Name = Wing, index = 3
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 3
	Name = Rib_Root, index = 1
	Name = Skin, index = 2
	Name = Wing, index = 3
Setting FEA Data
	Mesh for body = 0
	Number of nodal coordinates = 1
	Number of elements = 1
	Elemental Nodes = 1
	Elemental Rods  = 0
	Elemental Tria3 = 0
	Elemental Quad4 = 0
Setting FEA Data
	Mesh for body = 1
	Number of nodal coordinates = 46
	Number of elements = 44
	Elemental Nodes = 0
	Elemental Rods  = 0
	Elemental Tria3 = 0
	Elemental Quad4 = 44
Combining multiple FEA meshes!
	Combined Number of nodal coordinates = 47
	Combined Number of elements = 45
	Combined Elemental Nodes = 1
	Combined Elemental Rods  = 0
	Combined Elemental Tria3 = 0
	Combined Elemental Quad4 = 44
Getting vortex lattice surface data
	VLM surface name - Skin_Top
	Done getting vortex lattice surface data

Getting FEA vortex lattice mesh
	Surface 1: Number of points found for aero-spline = 3
	Surface 2: Number of points found for aero-spline = 6
	(Re-)Combining all aerodynamic surfaces into a 'Wing', 'Canard', and/or  'Fin' single surfaces !
Aero_Reference value is NULL - No aero reference parameters set

Getting FEA materials.......
	Number of materials - 1
	Material name - Unobtainium
	No "materialType" specified for Material tuple Unobtainium, defaulting to "Isotropic"
	Done getting FEA materials

Getting FEA properties.......
	Number of properties - 2
	Property name - Rib_Root
	No "material" specified for Property tuple Rib_Root, defaulting to an index of 1
	Property name - Skin
	No "material" specified for Property tuple Skin, defaulting to an index of 1
	Done getting FEA properties
Updating mesh element types based on properties input

Getting FEA constraints.......
	Number of constraints - 1
	Constraint name - ribConstraint
	No "constraintType" specified for Constraint tuple ribConstraint, defaulting to "ZeroDisplacement"
	Done getting FEA constraints

Getting FEA supports.......
	Number of supports - 1
	Support name - ribSupport
	Done getting FEA supports

Getting FEA connections.......
	Number of connection tuples - 1
	Connection name - Rib_Root
	No "groupName" specified for Connection tuple Rib_Root!
	Looking for automatic connections from the use of capsConnectLink for Rib_Root
	8 automatic connections were made for capsConnect Rib_Root (node id 1)
	Done getting FEA connections
Load tuple is NULL - No loads applied
Optimization Control tuple is NULL - Default optimization control is used

Getting FEA optimization control.......
Done getting FEA Optimization Control
Design_Variable tuple is NULL - No design variables applied
Design_Constraint tuple is NULL - No design constraints applied

Getting FEA analyses.......
	Number of analyses - 1
	Analysis name - Trim1
	Done getting FEA analyses

Writing Astros grid and connectivity file (in free field format) ....
Finished writing Astros grid file

Writing subElement types (if any) - appending mesh file
Writing connection cards - appending mesh file

Writing Astros instruction file....
	Writing aeros card
	Writing analysis cards
	Writing constraint cards--each subcase individually
	Writing support cards
	Writing material cards
	Writing property cards
	Writing aeroelastic cards


Running Astros......
Note: The following floating-point exceptions are signalling: IEEE_UNDERFLOW_FLAG
Done running Astros!
ok
test_Plate (test_astros.TestAstros.test_Plate) ... Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = plate, index = 1
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 0
	Face 1 TFI quading disabled with attribute .qParams
Getting surface mesh for body 1 (of 1)
Body 1 (of 1)
Number of nodes    = 25
Number of elements = 16
Number of triangle elements      = 0
Number of quadrilateral elements = 16
----------------------------
Total number of nodes    = 25
Total number of elements = 16
Mapping Csys attributes ................
	Number of unique Csys attributes = 0

Getting FEA coordinate systems.......
	Number of coordinate systems - 0
	No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
	Number of unique capsConstraint attributes = 1
	Name = plateEdge, index = 1
Mapping capsLoad attributes ................
	Number of unique capsLoad attributes = 1
	Name = plate, index = 1
Mapping capsBound attributes ................
	Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
	Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
	Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
	Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
	Mesh for body = 0
	Number of nodal coordinates = 25
	Number of elements = 16
	Elemental Nodes = 0
	Elemental Rods  = 0
	Elemental Tria3 = 0
	Elemental Quad4 = 16
Aero_Reference value is NULL - No aero reference parameters set

Getting FEA materials.......
	Number of materials - 1
	Material name - Madeupium
	Done getting FEA materials

Getting FEA properties.......
	Number of properties - 1
	Property name - plate
	Done getting FEA properties
Updating mesh element types based on properties input

Getting FEA constraints.......
	Number of constraints - 1
	Constraint name - edgeConstraint
	No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement"
	Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults

Getting FEA loads.......
	Number of loads - 1
	Load name - appliedPressure
	Done getting FEA loads
Optimization Control tuple is NULL - Default optimization control is used

Getting FEA optimization control.......
Done getting FEA Optimization Control
Design_Variable tuple is NULL - No design variables applied
Design_Constraint tuple is NULL - No design constraints applied
Analysis tuple is NULL

Getting FEA analyses.......
	Number of analyses - 1
	Analysis name - Default
	Done getting FEA analyses

Writing Astros grid and connectivity file ....
Finished writing Astros grid file

Writing subElement types (if any) - appending mesh file

Writing Astros instruction file....
	Writing analysis cards
	Writing load ADD cards
	Writing constraint cards--each subcase individually
	Writing load cards
	Writing material cards
	Writing property cards
Note: The following floating-point exceptions are signalling: IEEE_UNDERFLOW_FLAG
Aero_Reference value is NULL - No aero reference parameters set

Getting FEA materials.......
	Number of materials - 1
	Material name - Madeupium
	Done getting FEA materials

Getting FEA properties.......
	Number of properties - 1
	Property name - plate
	Done getting FEA properties
Updating mesh element types based on properties input

Getting FEA constraints.......
	Number of constraints - 1
	Constraint name - edgeConstraint
	No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement"
	Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults

Getting FEA loads.......
	Number of loads - 1
	Load name - appliedPressure
	Done getting FEA loads
Optimization Control tuple is NULL - Default optimization control is used

Getting FEA optimization control.......
Done getting FEA Optimization Control
Design_Variable tuple is NULL - No design variables applied
Design_Constraint tuple is NULL - No design constraints applied
Analysis tuple is NULL

Getting FEA analyses.......
	Number of analyses - 1
	Analysis name - Default
	Done getting FEA analyses

Writing Astros grid and connectivity file (in large field format) ....
Finished writing Astros grid file

Writing subElement types (if any) - appending mesh file

Writing Astros instruction file....
	Writing analysis cards
	Writing load ADD cards
	Writing constraint cards--each subcase individually
	Writing load cards
	Writing material cards
	Writing property cards
Note: The following floating-point exceptions are signalling: IEEE_UNDERFLOW_FLAG
Aero_Reference value is NULL - No aero reference parameters set

Getting FEA materials.......
	Number of materials - 1
	Material name - Madeupium
	Done getting FEA materials

Getting FEA properties.......
	Number of properties - 1
	Property name - plate
	Done getting FEA properties
Updating mesh element types based on properties input

Getting FEA constraints.......
	Number of constraints - 1
	Constraint name - edgeConstraint
	No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement"
	Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults

Getting FEA loads.......
	Number of loads - 1
	Load name - appliedPressure
	Done getting FEA loads
Optimization Control tuple is NULL - Default optimization control is used

Getting FEA optimization control.......
Done getting FEA Optimization Control
Design_Variable tuple is NULL - No design variables applied
Design_Constraint tuple is NULL - No design constraints applied
Analysis tuple is NULL

Getting FEA analyses.......
	Number of analyses - 1
	Analysis name - Default
	Done getting FEA analyses

Writing Astros grid and connectivity file (in free field format) ....
Finished writing Astros grid file

Writing subElement types (if any) - appending mesh file

Writing Astros instruction file....
	Writing analysis cards
	Writing load ADD cards
	Writing constraint cards--each subcase individually
	Writing load cards
	Writing material cards
	Writing property cards
Note: The following floating-point exceptions are signalling: IEEE_UNDERFLOW_FLAG
ok
test_MassProp_Units (test_avl.TestAVL.test_MassProp_Units) ... Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 5
	Name = Wing, index = 1
	Name = hTail, index = 2
	Name = vTail, index = 3
	Name = VTail1, index = 4
	Name = VTail2, index = 5
Getting vortex lattice surface data
	VLM surface name - Wing
	Done getting vortex lattice surface data
Warning: Control RightAileron not found in controls tuple! Only defaults will be used.
Warning: Control RightAileron not found in controls tuple! Only defaults will be used.
Warning: Control LeftAileron not found in controls tuple! Only defaults will be used.
Warning: Control LeftAileron not found in controls tuple! Only defaults will be used.
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 5
	Name = Wing, index = 1
	Name = hTail, index = 2
	Name = vTail, index = 3
	Name = VTail1, index = 4
	Name = VTail2, index = 5
Getting vortex lattice surface data
	VLM surface name - Wing
	Done getting vortex lattice surface data
Warning: Control RightAileron not found in controls tuple! Only defaults will be used.
Warning: Control RightAileron not found in controls tuple! Only defaults will be used.
Warning: Control LeftAileron not found in controls tuple! Only defaults will be used.
Warning: Control LeftAileron not found in controls tuple! Only defaults will be used.
Writing surface - Wing (ID = 0)
	Section 1 of 4 (ID = 3)
	  Control surface 1 of 1 
	Section 2 of 4 (ID = 2)
	  Control surface 1 of 1 
	Section 3 of 4 (ID = 1)
	  Control surface 1 of 1 
	Section 4 of 4 (ID = 0)
	  Control surface 1 of 1 
Writing mass properties file: caps.mass
Parsing MassProp
Note: The following floating-point exceptions are signalling: IEEE_DIVIDE_BY_ZERO
Warning: Control RightAileron not found in controls tuple! Only defaults will be used.
Warning: Control RightAileron not found in controls tuple! Only defaults will be used.
Warning: Control LeftAileron not found in controls tuple! Only defaults will be used.
Warning: Control LeftAileron not found in controls tuple! Only defaults will be used.
Writing mass properties file: caps.mass
Parsing MassProp
Note: The following floating-point exceptions are signalling: IEEE_DIVIDE_BY_ZERO
Warning: Control RightAileron not found in controls tuple! Only defaults will be used.
Warning: Control RightAileron not found in controls tuple! Only defaults will be used.
Warning: Control LeftAileron not found in controls tuple! Only defaults will be used.
Warning: Control LeftAileron not found in controls tuple! Only defaults will be used.
Writing mass properties file: caps.mass
Parsing MassProp
Warning: Control RightAileron not found in controls tuple! Only defaults will be used.
Warning: Control RightAileron not found in controls tuple! Only defaults will be used.
Warning: Control LeftAileron not found in controls tuple! Only defaults will be used.
Warning: Control LeftAileron not found in controls tuple! Only defaults will be used.
Writing mass properties file: caps.mass
Parsing MassProp
Warning: Control RightAileron not found in controls tuple! Only defaults will be used.
Warning: Control RightAileron not found in controls tuple! Only defaults will be used.
Warning: Control LeftAileron not found in controls tuple! Only defaults will be used.
Warning: Control LeftAileron not found in controls tuple! Only defaults will be used.
Writing mass properties file: caps.mass
Parsing MassProp
Warning: Control RightAileron not found in controls tuple! Only defaults will be used.
Warning: Control RightAileron not found in controls tuple! Only defaults will be used.
Warning: Control LeftAileron not found in controls tuple! Only defaults will be used.
Warning: Control LeftAileron not found in controls tuple! Only defaults will be used.
Writing mass properties file: caps.mass
Parsing MassProp
Warning: Control RightAileron not found in controls tuple! Only defaults will be used.
Warning: Control RightAileron not found in controls tuple! Only defaults will be used.
Warning: Control LeftAileron not found in controls tuple! Only defaults will be used.
Warning: Control LeftAileron not found in controls tuple! Only defaults will be used.
Writing mass properties file: caps.mass
Parsing MassProp
Warning: Control RightAileron not found in controls tuple! Only defaults will be used.
Warning: Control RightAileron not found in controls tuple! Only defaults will be used.
Warning: Control LeftAileron not found in controls tuple! Only defaults will be used.
Warning: Control LeftAileron not found in controls tuple! Only defaults will be used.
Writing mass properties file: caps.mass
Parsing MassProp
Warning: Control RightAileron not found in controls tuple! Only defaults will be used.
Warning: Control RightAileron not found in controls tuple! Only defaults will be used.
Warning: Control LeftAileron not found in controls tuple! Only defaults will be used.
Warning: Control LeftAileron not found in controls tuple! Only defaults will be used.
Writing mass properties file: caps.mass
Parsing MassProp
ok
test_MassProp_noUnits (test_avl.TestAVL.test_MassProp_noUnits) ... Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 5
	Name = Wing, index = 1
	Name = hTail, index = 2
	Name = vTail, index = 3
	Name = VTail1, index = 4
	Name = VTail2, index = 5
Getting vortex lattice surface data
	VLM surface name - Wing
	Done getting vortex lattice surface data
Warning: Control RightAileron not found in controls tuple! Only defaults will be used.
Warning: Control RightAileron not found in controls tuple! Only defaults will be used.
Warning: Control LeftAileron not found in controls tuple! Only defaults will be used.
Warning: Control LeftAileron not found in controls tuple! Only defaults will be used.
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 5
	Name = Wing, index = 1
	Name = hTail, index = 2
	Name = vTail, index = 3
	Name = VTail1, index = 4
	Name = VTail2, index = 5
Getting vortex lattice surface data
	VLM surface name - Wing
	Done getting vortex lattice surface data
Warning: Control RightAileron not found in controls tuple! Only defaults will be used.
Warning: Control RightAileron not found in controls tuple! Only defaults will be used.
Warning: Control LeftAileron not found in controls tuple! Only defaults will be used.
Warning: Control LeftAileron not found in controls tuple! Only defaults will be used.
Writing surface - Wing (ID = 0)
	Section 1 of 4 (ID = 3)
	  Control surface 1 of 1 
	Section 2 of 4 (ID = 2)
	  Control surface 1 of 1 
	Section 3 of 4 (ID = 1)
	  Control surface 1 of 1 
	Section 4 of 4 (ID = 0)
	  Control surface 1 of 1 
Writing mass properties file: caps.mass
Parsing MassProp
Note: The following floating-point exceptions are signalling: IEEE_DIVIDE_BY_ZERO
Warning: Control RightAileron not found in controls tuple! Only defaults will be used.
Warning: Control RightAileron not found in controls tuple! Only defaults will be used.
Warning: Control LeftAileron not found in controls tuple! Only defaults will be used.
Warning: Control LeftAileron not found in controls tuple! Only defaults will be used.
Writing mass properties file: caps.mass
Parsing MassProp
Note: The following floating-point exceptions are signalling: IEEE_DIVIDE_BY_ZERO
Warning: Control RightAileron not found in controls tuple! Only defaults will be used.
Warning: Control RightAileron not found in controls tuple! Only defaults will be used.
Warning: Control LeftAileron not found in controls tuple! Only defaults will be used.
Warning: Control LeftAileron not found in controls tuple! Only defaults will be used.
Writing mass properties file: caps.mass
Parsing MassProp
Warning: Control RightAileron not found in controls tuple! Only defaults will be used.
Warning: Control RightAileron not found in controls tuple! Only defaults will be used.
Warning: Control LeftAileron not found in controls tuple! Only defaults will be used.
Warning: Control LeftAileron not found in controls tuple! Only defaults will be used.
Writing mass properties file: caps.mass
Parsing MassProp
Warning: Control RightAileron not found in controls tuple! Only defaults will be used.
Warning: Control RightAileron not found in controls tuple! Only defaults will be used.
Warning: Control LeftAileron not found in controls tuple! Only defaults will be used.
Warning: Control LeftAileron not found in controls tuple! Only defaults will be used.
Writing mass properties file: caps.mass
Parsing MassProp
Warning: Control RightAileron not found in controls tuple! Only defaults will be used.
Warning: Control RightAileron not found in controls tuple! Only defaults will be used.
Warning: Control LeftAileron not found in controls tuple! Only defaults will be used.
Warning: Control LeftAileron not found in controls tuple! Only defaults will be used.
Writing mass properties file: caps.mass
Parsing MassProp
ok
test_alpha_custom_increment (test_avl.TestAVL.test_alpha_custom_increment) ... Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 5
	Name = Wing, index = 1
	Name = hTail, index = 2
	Name = vTail, index = 3
	Name = VTail1, index = 4
	Name = VTail2, index = 5
Getting vortex lattice surface data
	VLM surface name - Wing
	Done getting vortex lattice surface data
Warning: Control RightAileron not found in controls tuple! Only defaults will be used.
Warning: Control RightAileron not found in controls tuple! Only defaults will be used.
Warning: Control LeftAileron not found in controls tuple! Only defaults will be used.
Warning: Control LeftAileron not found in controls tuple! Only defaults will be used.
Writing surface - Wing (ID = 0)
	Section 1 of 4 (ID = 3)
	  Control surface 1 of 1 
	Section 2 of 4 (ID = 2)
	  Control surface 1 of 1 
	Section 3 of 4 (ID = 1)
	  Control surface 1 of 1 
	Section 4 of 4 (ID = 0)
	  Control surface 1 of 1 
Warning: Control RightAileron not found in controls tuple! Only defaults will be used.
Warning: Control RightAileron not found in controls tuple! Only defaults will be used.
Warning: Control LeftAileron not found in controls tuple! Only defaults will be used.
Warning: Control LeftAileron not found in controls tuple! Only defaults will be used.
Warning: Control RightAileron not found in controls tuple! Only defaults will be used.
Warning: Control RightAileron not found in controls tuple! Only defaults will be used.
Warning: Control LeftAileron not found in controls tuple! Only defaults will be used.
Warning: Control LeftAileron not found in controls tuple! Only defaults will be used.
ok
test_geom_change (test_avl.TestAVL.test_geom_change) ... Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 5
	Name = Wing, index = 1
	Name = hTail, index = 2
	Name = vTail, index = 3
	Name = VTail1, index = 4
	Name = VTail2, index = 5
Getting vortex lattice surface data
	VLM surface name - Wing
	Done getting vortex lattice surface data
Warning: Control RightAileron not found in controls tuple! Only defaults will be used.
Warning: Control RightAileron not found in controls tuple! Only defaults will be used.
Warning: Control LeftAileron not found in controls tuple! Only defaults will be used.
Warning: Control LeftAileron not found in controls tuple! Only defaults will be used.
Writing surface - Wing (ID = 0)
	Section 1 of 4 (ID = 3)
	  Control surface 1 of 1 
	Section 2 of 4 (ID = 2)
	  Control surface 1 of 1 
	Section 3 of 4 (ID = 1)
	  Control surface 1 of 1 
	Section 4 of 4 (ID = 0)
	  Control surface 1 of 1 
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 5
	Name = Wing, index = 1
	Name = hTail, index = 2
	Name = vTail, index = 3
	Name = VTail1, index = 4
	Name = VTail2, index = 5
Getting vortex lattice surface data
	VLM surface name - Wing
	Done getting vortex lattice surface data
Warning: Control RightAileron not found in controls tuple! Only defaults will be used.
Warning: Control RightAileron not found in controls tuple! Only defaults will be used.
Warning: Control LeftAileron not found in controls tuple! Only defaults will be used.
Warning: Control LeftAileron not found in controls tuple! Only defaults will be used.
Writing surface - Wing (ID = 0)
	Section 1 of 4 (ID = 3)
	  Control surface 1 of 1 
	Section 2 of 4 (ID = 2)
	  Control surface 1 of 1 
	Section 3 of 4 (ID = 1)
	  Control surface 1 of 1 
	Section 4 of 4 (ID = 0)
	  Control surface 1 of 1 
ok
test_numSpan (test_avl.TestAVL.test_numSpan) ... Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 5
	Name = Wing, index = 1
	Name = hTail, index = 2
	Name = vTail, index = 3
	Name = VTail1, index = 4
	Name = VTail2, index = 5
Getting vortex lattice surface data
	VLM surface name - Wing
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 5
	Name = Wing, index = 1
	Name = hTail, index = 2
	Name = vTail, index = 3
	Name = VTail1, index = 4
	Name = VTail2, index = 5
Getting vortex lattice surface data
	VLM surface name - Wing
ok
test_phase (test_avl.TestAVL.test_phase) ... Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 5
	Name = Wing, index = 1
	Name = hTail, index = 2
	Name = vTail, index = 3
	Name = VTail1, index = 4
	Name = VTail2, index = 5
Getting vortex lattice surface data
	VLM surface name - Wing
	Done getting vortex lattice surface data
Warning: Control RightAileron not found in controls tuple! Only defaults will be used.
Warning: Control RightAileron not found in controls tuple! Only defaults will be used.
Warning: Control LeftAileron not found in controls tuple! Only defaults will be used.
Warning: Control LeftAileron not found in controls tuple! Only defaults will be used.
Writing surface - Wing (ID = 0)
	Section 1 of 4 (ID = 3)
	  Control surface 1 of 1 
	Section 2 of 4 (ID = 2)
	  Control surface 1 of 1 
	Section 3 of 4 (ID = 1)
	  Control surface 1 of 1 
	Section 4 of 4 (ID = 0)
	  Control surface 1 of 1 
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 5
	Name = Wing, index = 1
	Name = hTail, index = 2
	Name = vTail, index = 3
	Name = VTail1, index = 4
	Name = VTail2, index = 5
Getting vortex lattice surface data
	VLM surface name - Wing
	Done getting vortex lattice surface data
Warning: Control RightAileron not found in controls tuple! Only defaults will be used.
Warning: Control RightAileron not found in controls tuple! Only defaults will be used.
Warning: Control LeftAileron not found in controls tuple! Only defaults will be used.
Warning: Control LeftAileron not found in controls tuple! Only defaults will be used.
Warning: Control RightAileron not found in controls tuple! Only defaults will be used.
Warning: Control RightAileron not found in controls tuple! Only defaults will be used.
Warning: Control LeftAileron not found in controls tuple! Only defaults will be used.
Warning: Control LeftAileron not found in controls tuple! Only defaults will be used.
ok
test_wing_Vtail (test_avl.TestAVL.test_wing_Vtail) ... Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 5
	Name = Wing, index = 1
	Name = hTail, index = 2
	Name = vTail, index = 3
	Name = VTail1, index = 4
	Name = VTail2, index = 5
Getting vortex lattice surface data
	VLM surface name - VTail1
	No "groupName" variable provided or no matches found, going to use tuple name
	VLM surface name - VTail2
	No "groupName" variable provided or no matches found, going to use tuple name
	VLM surface name - Wing
	Done getting vortex lattice surface data
Warning: Control RightAileron not found in controls tuple! Only defaults will be used.
Warning: Control RightAileron not found in controls tuple! Only defaults will be used.
Warning: Control LeftAileron not found in controls tuple! Only defaults will be used.
Warning: Control LeftAileron not found in controls tuple! Only defaults will be used.
Writing surface - VTail1 (ID = 0)
	Section 1 of 2 (ID = 1)
	Section 2 of 2 (ID = 0)
Writing surface - VTail2 (ID = 1)
	Section 1 of 2 (ID = 0)
	Section 2 of 2 (ID = 1)
Writing surface - Wing (ID = 2)
	Section 1 of 4 (ID = 3)
	  Control surface 1 of 1 
	Section 2 of 4 (ID = 2)
	  Control surface 1 of 1 
	Section 3 of 4 (ID = 1)
	  Control surface 1 of 1 
	Section 4 of 4 (ID = 0)
	  Control surface 1 of 1 
ok
test_wing_tail (test_avl.TestAVL.test_wing_tail) ... Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 5
	Name = Wing, index = 1
	Name = hTail, index = 2
	Name = vTail, index = 3
	Name = VTail1, index = 4
	Name = VTail2, index = 5
Getting vortex lattice surface data
	VLM surface name - Wing
	VLM surface name - hTail
	VLM surface name - vTail
	No "groupName" variable provided or no matches found, going to use tuple name
	Done getting vortex lattice surface data
Warning: Control RightAileron not found in controls tuple! Only defaults will be used.
Warning: Control RightAileron not found in controls tuple! Only defaults will be used.
Warning: Control LeftAileron not found in controls tuple! Only defaults will be used.
Warning: Control LeftAileron not found in controls tuple! Only defaults will be used.
Warning: Control Elevator not found in controls tuple! Only defaults will be used.
Warning: Control Elevator not found in controls tuple! Only defaults will be used.
Warning: Control Elevator not found in controls tuple! Only defaults will be used.
Warning: Control Rudder not found in controls tuple! Only defaults will be used.
Warning: Control Rudder not found in controls tuple! Only defaults will be used.
Writing surface - Wing (ID = 0)
	Section 1 of 4 (ID = 3)
	  Control surface 1 of 1 
	Section 2 of 4 (ID = 2)
	  Control surface 1 of 1 
	Section 3 of 4 (ID = 1)
	  Control surface 1 of 1 
	Section 4 of 4 (ID = 0)
	  Control surface 1 of 1 
Writing surface - hTail (ID = 1)
	Section 1 of 3 (ID = 2)
	  Control surface 1 of 1 
	Section 2 of 3 (ID = 1)
	  Control surface 1 of 1 
	Section 3 of 3 (ID = 0)
	  Control surface 1 of 1 
Writing surface - vTail (ID = 2)
	Section 1 of 2 (ID = 0)
	  Control surface 1 of 1 
	Section 2 of 2 (ID = 1)
	  Control surface 1 of 1 
ok
test_wing_tail_control (test_avl.TestAVL.test_wing_tail_control) ... Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 5
	Name = Wing, index = 1
	Name = hTail, index = 2
	Name = vTail, index = 3
	Name = VTail1, index = 4
	Name = VTail2, index = 5
Getting vortex lattice control surface data
	VLM control surface name - Elevator
	VLM control surface name - LeftAileron
	VLM control surface name - RightAileron
	VLM control surface name - Rudder
	Done getting vortex lattice control surface data
Getting vortex lattice surface data
	VLM surface name - Wing
	VLM surface name - hTail
	VLM surface name - vTail
	No "groupName" variable provided or no matches found, going to use tuple name
	Done getting vortex lattice surface data
Writing surface - Wing (ID = 0)
	Section 1 of 4 (ID = 3)
	  Control surface 1 of 1 
	Section 2 of 4 (ID = 2)
	  Control surface 1 of 1 
	Section 3 of 4 (ID = 1)
	  Control surface 1 of 1 
	Section 4 of 4 (ID = 0)
	  Control surface 1 of 1 
Writing surface - hTail (ID = 1)
	Section 1 of 3 (ID = 2)
	  Control surface 1 of 1 
	Section 2 of 3 (ID = 1)
	  Control surface 1 of 1 
	Section 3 of 3 (ID = 0)
	  Control surface 1 of 1 
Writing surface - vTail (ID = 2)
	Section 1 of 2 (ID = 0)
	  Control surface 1 of 1 
	Section 2 of 2 (ID = 1)
	  Control surface 1 of 1 
ok
test_TargetCL (test_cart3d.TestCart3D.test_TargetCL) ... Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = Wing1, index = 1
 Body size = 15.356535
 Tessellating body 1 with  MaxEdge = 0.383913  Sag = 0.015357  Angle = 15.000000
 Executing: autoInputs -r 28.284271 -nDiv 9 -maxR 7  -mesh2d &gt; autoInputs.out
 Executing: ./aero.csh &gt; aero.out
ok
test_outputs (test_cart3d.TestCart3D.test_outputs) ... ok
test_reenter (test_cart3d.TestCart3D.test_reenter) ... Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = Wing1, index = 1
Getting CFD functional.......
	Number of design variables - 1
	Objective name - Drag
	Done getting CFD functional
 Body size = 15.356535
 Tessellating body 1 with  MaxEdge = 0.383913  Sag = 0.015357  Angle = 15.000000
 Executing: autoInputs -r 80.000000 -nDiv 5 -maxR 7  &gt; autoInputs.out
 Executing: ./aero.csh &gt; aero.out
 Executing: ./aero.csh &gt; aero.out
 Body size = 15.356535
 Tessellating body 1 with  MaxEdge = 0.307131  Sag = 0.015357  Angle = 15.000000
 Executing: autoInputs -r 80.000000 -nDiv 5 -maxR 7  &gt; autoInputs.out
 Executing: ./aero.csh &gt; aero.out
ok
test_sensitivity_AnalysisIn (test_cart3d.TestCart3D.test_sensitivity_AnalysisIn) ... Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = Wing1, index = 1

Getting CFD design variables.......
	Number of design variables - 1
	Design Variable name - Mach
	Done getting CFD design variables
Getting CFD functional.......
	Number of design variables - 3
	Objective name - C_A
	Objective name - C_N
	Objective name - C_Y
	Done getting CFD functional
 Body size = 15.356535
 Tessellating body 1 with  MaxEdge = 0.383913  Sag = 0.015357  Angle = 15.000000
 Executing: autoInputs -r 80.000000 -nDiv 5 -maxR 7  &gt; autoInputs.out
 o Evaluating Cart3D functionals and/or gradients
   ATTENTION: using static geometry ../inputs/Components.i.tri
   (18:45:37) Running aero.csh on 2 core(s) in M0.5A1B0_DP1
   (18:45:38) aero.csh done
 o case M0.5A1B0_DP1, averaging data over 1 cycle(s)
 o Evaluating Cart3D functionals and/or gradients
   ATTENTION: using static geometry ../inputs/Components.i.tri
   (18:45:39) Running aero.csh on 2 core(s) in M0.5A1B0_DP1
   (18:45:41) aero.csh done
              Max memory allowed:       32 GB
              Flow hexes:               8744
              Estimated cutter memory:  0.000874 GB / DV
              Estimated xsensit memory: 0.016614 GB / DV
              Available threads:        2
              # DVs:                    1
   o Number of simultaneous cutter jobs:   1
   (18:45:41) Linearizing cut-cells
   (18:45:41) ... done
   o Number of simultaneous xsensit jobs:  1
   (18:45:41) Computing gradients
   (18:45:49) ... done
 o case M0.5A1B0_DP1, averaging data over 1 cycle(s)
 o Evaluating Cart3D functionals and/or gradients
   ATTENTION: using static geometry ../inputs/Components.i.tri
   (18:45:50) Running aero.csh on 2 core(s) in M0.5A1B0_DP1
   (18:45:51) aero.csh done
 o case M0.5A1B0_DP1, averaging data over 1 cycle(s)
Getting CFD functional.......
	Number of design variables - 3
	Objective name - C_D
	Objective name - C_L
	Objective name - C_S
	Done getting CFD functional
 o Evaluating Cart3D functionals and/or gradients
   ATTENTION: using static geometry ../inputs/Components.i.tri
   (18:45:51) Running aero.csh on 2 core(s) in M0.5A1B0_DP1
   (18:45:52) aero.csh done
 o case M0.5A1B0_DP1, averaging data over 1 cycle(s)
 o Evaluating Cart3D functionals and/or gradients
   ATTENTION: using static geometry ../inputs/Components.i.tri
   (18:45:53) Running aero.csh on 2 core(s) in M0.5A1B0_DP1
   (18:45:54) aero.csh done
              Max memory allowed:       32 GB
              Flow hexes:               8744
              Estimated cutter memory:  0.000874 GB / DV
              Estimated xsensit memory: 0.016614 GB / DV
              Available threads:        2
              # DVs:                    1
   o Number of simultaneous cutter jobs:   1
   (18:45:55) Linearizing cut-cells
   (18:45:55) ... done
   o Number of simultaneous xsensit jobs:  1
   (18:45:55) Computing gradients
   (18:46:03) ... done
 o case M0.5A1B0_DP1, averaging data over 1 cycle(s)
 o Evaluating Cart3D functionals and/or gradients
   ATTENTION: using static geometry ../inputs/Components.i.tri
   (18:46:03) Running aero.csh on 2 core(s) in M0.5A1B0_DP1
   (18:46:04) aero.csh done
 o case M0.5A1B0_DP1, averaging data over 1 cycle(s)
Getting CFD functional.......
	Number of design variables - 1
	Objective name - C_l
	Done getting CFD functional
 o Evaluating Cart3D functionals and/or gradients
   ATTENTION: using static geometry ../inputs/Components.i.tri
   (18:46:05) Running aero.csh on 2 core(s) in M0.5A1B0_DP1
   (18:46:06) aero.csh done
 o case M0.5A1B0_DP1, averaging data over 1 cycle(s)
 o Evaluating Cart3D functionals and/or gradients
   ATTENTION: using static geometry ../inputs/Components.i.tri
   (18:46:06) Running aero.csh on 2 core(s) in M0.5A1B0_DP1
   (18:46:07) aero.csh done
              Max memory allowed:       32 GB
              Flow hexes:               8744
              Estimated cutter memory:  0.000874 GB / DV
              Estimated xsensit memory: 0.016614 GB / DV
              Available threads:        2
              # DVs:                    1
   o Number of simultaneous cutter jobs:   1
   (18:46:07) Linearizing cut-cells
   (18:46:07) ... done
   o Number of simultaneous xsensit jobs:  1
   (18:46:07) Computing gradients
   (18:46:11) ... done
 o case M0.5A1B0_DP1, averaging data over 1 cycle(s)
 o Evaluating Cart3D functionals and/or gradients
   ATTENTION: using static geometry ../inputs/Components.i.tri
   (18:46:12) Running aero.csh on 2 core(s) in M0.5A1B0_DP1
   (18:46:13) aero.csh done
 o case M0.5A1B0_DP1, averaging data over 1 cycle(s)
Getting CFD functional.......
	Number of design variables - 1
	Objective name - C_m
	Done getting CFD functional
 o Evaluating Cart3D functionals and/or gradients
   ATTENTION: using static geometry ../inputs/Components.i.tri
   (18:46:14) Running aero.csh on 2 core(s) in M0.5A1B0_DP1
   (18:46:15) aero.csh done
 o case M0.5A1B0_DP1, averaging data over 1 cycle(s)
 o Evaluating Cart3D functionals and/or gradients
   ATTENTION: using static geometry ../inputs/Components.i.tri
   (18:46:15) Running aero.csh on 2 core(s) in M0.5A1B0_DP1
   (18:46:16) aero.csh done
              Max memory allowed:       32 GB
              Flow hexes:               8744
              Estimated cutter memory:  0.000874 GB / DV
              Estimated xsensit memory: 0.016614 GB / DV
              Available threads:        2
              # DVs:                    1
   o Number of simultaneous cutter jobs:   1
   (18:46:16) Linearizing cut-cells
   (18:46:16) ... done
   o Number of simultaneous xsensit jobs:  1
   (18:46:16) Computing gradients
   (18:46:20) ... done
 o case M0.5A1B0_DP1, averaging data over 1 cycle(s)
 o Evaluating Cart3D functionals and/or gradients
   ATTENTION: using static geometry ../inputs/Components.i.tri
   (18:46:21) Running aero.csh on 2 core(s) in M0.5A1B0_DP1
   (18:46:22) aero.csh done
 o case M0.5A1B0_DP1, averaging data over 1 cycle(s)
Getting CFD functional.......
	Number of design variables - 1
	Objective name - C_n
	Done getting CFD functional
 o Evaluating Cart3D functionals and/or gradients
   ATTENTION: using static geometry ../inputs/Components.i.tri
   (18:46:23) Running aero.csh on 2 core(s) in M0.5A1B0_DP1
   (18:46:24) aero.csh done
 o case M0.5A1B0_DP1, averaging data over 1 cycle(s)
 o Evaluating Cart3D functionals and/or gradients
   ATTENTION: using static geometry ../inputs/Components.i.tri
   (18:46:24) Running aero.csh on 2 core(s) in M0.5A1B0_DP1
   (18:46:25) aero.csh done
              Max memory allowed:       32 GB
              Flow hexes:               8744
              Estimated cutter memory:  0.000874 GB / DV
              Estimated xsensit memory: 0.016614 GB / DV
              Available threads:        2
              # DVs:                    1
   o Number of simultaneous cutter jobs:   1
   (18:46:25) Linearizing cut-cells
   (18:46:25) ... done
   o Number of simultaneous xsensit jobs:  1
   (18:46:25) Computing gradients
   (18:46:29) ... done
 o case M0.5A1B0_DP1, averaging data over 1 cycle(s)
 o Evaluating Cart3D functionals and/or gradients
   ATTENTION: using static geometry ../inputs/Components.i.tri
   (18:46:30) Running aero.csh on 2 core(s) in M0.5A1B0_DP1
   (18:46:31) aero.csh done
 o case M0.5A1B0_DP1, averaging data over 1 cycle(s)
Getting CFD functional.......
	Number of design variables - 1
	Objective name - C_M_x
	Done getting CFD functional
 o Evaluating Cart3D functionals and/or gradients
   ATTENTION: using static geometry ../inputs/Components.i.tri
   (18:46:31) Running aero.csh on 2 core(s) in M0.5A1B0_DP1
   (18:46:32) aero.csh done
 o case M0.5A1B0_DP1, averaging data over 1 cycle(s)
 o Evaluating Cart3D functionals and/or gradients
   ATTENTION: using static geometry ../inputs/Components.i.tri
   (18:46:33) Running aero.csh on 2 core(s) in M0.5A1B0_DP1
   (18:46:34) aero.csh done
              Max memory allowed:       32 GB
              Flow hexes:               8744
              Estimated cutter memory:  0.000874 GB / DV
              Estimated xsensit memory: 0.016614 GB / DV
              Available threads:        2
              # DVs:                    1
   o Number of simultaneous cutter jobs:   1
   (18:46:34) Linearizing cut-cells
   (18:46:34) ... done
   o Number of simultaneous xsensit jobs:  1
   (18:46:34) Computing gradients
   (18:46:38) ... done
 o case M0.5A1B0_DP1, averaging data over 1 cycle(s)
 o Evaluating Cart3D functionals and/or gradients
   ATTENTION: using static geometry ../inputs/Components.i.tri
   (18:46:38) Running aero.csh on 2 core(s) in M0.5A1B0_DP1
   (18:46:39) aero.csh done
 o case M0.5A1B0_DP1, averaging data over 1 cycle(s)
Getting CFD functional.......
	Number of design variables - 1
	Objective name - C_M_y
	Done getting CFD functional
 o Evaluating Cart3D functionals and/or gradients
   ATTENTION: using static geometry ../inputs/Components.i.tri
   (18:46:40) Running aero.csh on 2 core(s) in M0.5A1B0_DP1
   (18:46:41) aero.csh done
 o case M0.5A1B0_DP1, averaging data over 1 cycle(s)
 o Evaluating Cart3D functionals and/or gradients
   ATTENTION: using static geometry ../inputs/Components.i.tri
   (18:46:42) Running aero.csh on 2 core(s) in M0.5A1B0_DP1
   (18:46:42) aero.csh done
              Max memory allowed:       32 GB
              Flow hexes:               8744
              Estimated cutter memory:  0.000874 GB / DV
              Estimated xsensit memory: 0.016614 GB / DV
              Available threads:        2
              # DVs:                    1
   o Number of simultaneous cutter jobs:   1
   (18:46:42) Linearizing cut-cells
   (18:46:42) ... done
   o Number of simultaneous xsensit jobs:  1
   (18:46:43) Computing gradients
   (18:46:47) ... done
 o case M0.5A1B0_DP1, averaging data over 1 cycle(s)
 o Evaluating Cart3D functionals and/or gradients
   ATTENTION: using static geometry ../inputs/Components.i.tri
   (18:46:47) Running aero.csh on 2 core(s) in M0.5A1B0_DP1
   (18:46:48) aero.csh done
 o case M0.5A1B0_DP1, averaging data over 1 cycle(s)
Getting CFD functional.......
	Number of design variables - 1
	Objective name - C_M_z
	Done getting CFD functional
 o Evaluating Cart3D functionals and/or gradients
   ATTENTION: using static geometry ../inputs/Components.i.tri
   (18:46:49) Running aero.csh on 2 core(s) in M0.5A1B0_DP1
   (18:46:50) aero.csh done
 o case M0.5A1B0_DP1, averaging data over 1 cycle(s)
 o Evaluating Cart3D functionals and/or gradients
   ATTENTION: using static geometry ../inputs/Components.i.tri
   (18:46:50) Running aero.csh on 2 core(s) in M0.5A1B0_DP1
   (18:46:51) aero.csh done
              Max memory allowed:       32 GB
              Flow hexes:               8744
              Estimated cutter memory:  0.000874 GB / DV
              Estimated xsensit memory: 0.016614 GB / DV
              Available threads:        2
              # DVs:                    1
   o Number of simultaneous cutter jobs:   1
   (18:46:51) Linearizing cut-cells
   (18:46:51) ... done
   o Number of simultaneous xsensit jobs:  1
   (18:46:51) Computing gradients
   (18:46:55) ... done
 o case M0.5A1B0_DP1, averaging data over 1 cycle(s)
 o Evaluating Cart3D functionals and/or gradients
   ATTENTION: using static geometry ../inputs/Components.i.tri
   (18:46:56) Running aero.csh on 2 core(s) in M0.5A1B0_DP1
   (18:46:57) aero.csh done
 o case M0.5A1B0_DP1, averaging data over 1 cycle(s)
ok
test_sensitivity_GeometryIn (test_cart3d.TestCart3D.test_sensitivity_GeometryIn) ... Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = Wing1, index = 1

Getting CFD design variables.......
	Number of design variables - 2
	Design Variable name - Mach
	Design Variable name - area
	Done getting CFD design variables
Getting CFD functional.......
	Number of design variables - 3
	Objective name - C_A
	Objective name - C_N
	Objective name - C_Y
	Done getting CFD functional
 Body size = 15.356535
 Tessellating body 1 with  MaxEdge = 0.383913  Sag = 0.015357  Angle = 15.000000
 Executing: autoInputs -r 80.000000 -nDiv 5 -maxR 7  &gt; autoInputs.out
 o Evaluating Cart3D functionals and/or gradients
   ATTENTION: using static geometry ../inputs/Components.i.tri
   (18:46:58) Running aero.csh on 2 core(s) in M0.5A1B0_DP1
   (18:46:59) aero.csh done
 o case M0.5A1B0_DP1, averaging data over 1 cycle(s)
 o Evaluating Cart3D functionals and/or gradients
   ATTENTION: using static geometry ../inputs/Components.i.tri
   (18:47:00) Running aero.csh on 2 core(s) in M0.5A1B0_DP1
   (18:47:01) aero.csh done
              Max memory allowed:       32 GB
              Flow hexes:               8744
              Estimated cutter memory:  0.000874 GB / DV
              Estimated xsensit memory: 0.016614 GB / DV
              Available threads:        2
              # DVs:                    2
   o Number of simultaneous cutter jobs:   2
   (18:47:02) Linearizing cut-cells
   (18:47:04) ... done
   o Number of simultaneous xsensit jobs:  2
   (18:47:04) Computing gradients
              Adjusted OMP_NUM_THREADS to 1 for xsensit
   (18:47:12) ... done
 o case M0.5A1B0_DP1, averaging data over 1 cycle(s)
 o Evaluating Cart3D functionals and/or gradients
   ATTENTION: using static geometry ../inputs/Components.i.tri
   (18:47:12) Running aero.csh on 2 core(s) in M0.5A1B0_DP1
   (18:47:13) aero.csh done
 o case M0.5A1B0_DP1, averaging data over 1 cycle(s)
ok
test_Output_v5 (test_cbaero.TestCBAERO.test_Output_v5) ... Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = Wing1, index = 1
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 3
	Name = riteWing, index = 1
	Name = leftWing, index = 2
	Name = trailingEdge, index = 3

Writing FAST file ....
Finished writing FAST file

Writing CBAero input file - cbaero_CAPS.cbaero
Writing CBAero tagged regions - TaggedRegions
Writing CBAero setup file - cbaero_CAPS.stp
ok
test_Output_v6 (test_cbaero.TestCBAERO.test_Output_v6) ... Writing CBAero input file - cbaero_CAPS.cbaero
Writing CBAero tagged regions - TaggedRegions
Writing CBAero setup file - cbaero_CAPS.stp
ok
test_inputs (test_cbaero.TestCBAERO.test_inputs) ... Writing CBAero input file - cbaero_CAPS.cbaero
Writing CBAero tagged regions - TaggedRegions
Writing CBAero setup file - cbaero_CAPS.stp
ok
test_MultiBody (test_egadsTess.TestEGADS.test_MultiBody) ... Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 4
	Name = Wing1, index = 1
	Name = Wing2, index = 2
	Name = Wake, index = 3
	Name = Farfield, index = 4
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 4
	Name = Wing1, index = 1
	Name = Wing2, index = 2
	Name = Wake, index = 3
	Name = Farfield, index = 4

Getting mesh sizing parameters
	Mesh sizing name - Farfield
	Done getting mesh sizing parameters
ok
test_SingleBody_AnalysisOutVal (test_egadsTess.TestEGADS.test_SingleBody_AnalysisOutVal) ... Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 2
	Name = Farfield, index = 1
	Name = Wing1, index = 2
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 4
	Name = Farfield, index = 1
	Name = riteWing, index = 2
	Name = leftWing, index = 3
	Name = trailingEdge, index = 4

Getting mesh sizing parameters
	Mesh sizing name - Farfield
	Done getting mesh sizing parameters
ok
test_all (test_egadsTess.TestEGADS.test_all) ... ERROR:: BAD STATUS = -276 from matsol (called from solveSketchOrig:63376)
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 9
	Name = box, index = 1
	Name = cylinder, index = 2
	Name = cone, index = 3
	Name = torus, index = 4
	Name = sphere, index = 5
	Name = boxhole, index = 6
	Name = bullet, index = 7
	Name = nodeBody, index = 8
	Name = farfield, index = 9
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 1
	Name = box, index = 1
 1F924CC00 EGADS Info: Face #3 -&gt; Edge #9 (9) Internally in Loop 4 7, sen = -1!
 1F924CC00 EGADS Info: Face #3 -&gt; Edge #9 (9) Internally in Loop 7 4, sen = 1!
 174073000 EGADS Info: Face #5 -&gt; Edge #17 (9) Internally in Loop 7 4, sen = -1!
 174073000 EGADS Info: Face #5 -&gt; Edge #17 (9) Internally in Loop 4 7, sen = 1!
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 9
	Name = box, index = 1
	Name = cylinder, index = 2
	Name = cone, index = 3
	Name = torus, index = 4
	Name = sphere, index = 5
	Name = boxhole, index = 6
	Name = bullet, index = 7
	Name = nodeBody, index = 8
	Name = farfield, index = 9
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 1
	Name = box, index = 1
 1F924CC00 EGADS Info: Face #3 -&gt; Edge #9 (9) Internally in Loop 4 7, sen = -1!
 1F924CC00 EGADS Info: Face #3 -&gt; Edge #9 (9) Internally in Loop 7 4, sen = 1!
 174073000 EGADS Info: Face #5 -&gt; Edge #17 (9) Internally in Loop 7 4, sen = -1!
 174073000 EGADS Info: Face #5 -&gt; Edge #17 (9) Internally in Loop 4 7, sen = 1!
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 9
	Name = box, index = 1
	Name = cylinder, index = 2
	Name = cone, index = 3
	Name = torus, index = 4
	Name = sphere, index = 5
	Name = boxhole, index = 6
	Name = bullet, index = 7
	Name = nodeBody, index = 8
	Name = farfield, index = 9
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 1
	Name = box, index = 1
 1F924CC00 EGADS Info: Face #3 -&gt; Edge #9 (9) Internally in Loop 4 7, sen = -1!
 1F924CC00 EGADS Info: Face #3 -&gt; Edge #9 (9) Internally in Loop 7 4, sen = 1!
 174073000 EGADS Info: Face #5 -&gt; Edge #17 (9) Internally in Loop 7 4, sen = -1!
 174073000 EGADS Info: Face #5 -&gt; Edge #17 (9) Internally in Loop 4 7, sen = 1!
ok
test_box (test_egadsTess.TestEGADS.test_box) ... Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 2
	Name = box, index = 1
	Name = farfield, index = 2
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 1
	Name = box, index = 1
ok
test_boxhole (test_egadsTess.TestEGADS.test_boxhole) ... Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 2
	Name = boxhole, index = 1
	Name = farfield, index = 2
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 0
 174073000 EGADS Info: Face #3 -&gt; Edge #9 (9) Internally in Loop 4 7, sen = -1!
 174073000 EGADS Info: Face #3 -&gt; Edge #9 (9) Internally in Loop 7 4, sen = 1!
 1F924CC00 EGADS Info: Face #5 -&gt; Edge #17 (9) Internally in Loop 7 4, sen = -1!
 1F924CC00 EGADS Info: Face #5 -&gt; Edge #17 (9) Internally in Loop 4 7, sen = 1!
ok
test_bullet (test_egadsTess.TestEGADS.test_bullet) ... Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 2
	Name = bullet, index = 1
	Name = farfield, index = 2
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 0
ok
test_cone (test_egadsTess.TestEGADS.test_cone) ... Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 2
	Name = cone, index = 1
	Name = farfield, index = 2
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 0
ok
test_cylinder (test_egadsTess.TestEGADS.test_cylinder) ... Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 2
	Name = cylinder, index = 1
	Name = farfield, index = 2
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 0
ok
test_invalid_Mesh_Lenght_Scale (test_egadsTess.TestEGADS.test_invalid_Mesh_Lenght_Scale) ... Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 2
	Name = Farfield, index = 1
	Name = Wing1, index = 2
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 4
	Name = Farfield, index = 1
	Name = riteWing, index = 2
	Name = leftWing, index = 3
	Name = trailingEdge, index = 4
ok
test_journal (test_egadsTess.TestEGADS.test_journal) ... ERROR:: BAD STATUS = -276 from matsol (called from solveSketchOrig:63376)
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 2
	Name = box, index = 1
	Name = farfield, index = 2
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 1
	Name = box, index = 1

Getting mesh sizing parameters
	Mesh sizing name - box
	Done getting mesh sizing parameters
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 2
	Name = box, index = 1
	Name = farfield, index = 2
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 1
	Name = box, index = 1

Getting mesh sizing parameters
	Mesh sizing name - box
	Done getting mesh sizing parameters
 EGADS Info: 0 Objects, 0 Reference in Use (of 0) at Close!
ERROR:: BAD STATUS = -276 from matsol (called from solveSketchOrig:63376)
ERROR:: BAD STATUS = -276 from matsol (called from solveSketchOrig:63376)
 CAPS Info: Hit last success -- going live!
ERROR:: BAD STATUS = -276 from matsol (called from solveSketchOrig:63376)
 CAPS Info: Hit last success -- going live!
ERROR:: BAD STATUS = -276 from matsol (called from solveSketchOrig:63376)
 CAPS Info: Hit last success -- going live!
ERROR:: BAD STATUS = -276 from matsol (called from solveSketchOrig:63376)
 CAPS Info: Hit last success -- going live!
ERROR:: BAD STATUS = -276 from matsol (called from solveSketchOrig:63376)
 CAPS Info: Hit last success -- going live!
ERROR:: BAD STATUS = -276 from matsol (called from solveSketchOrig:63376)
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 2
	Name = box, index = 1
	Name = farfield, index = 2
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 1
	Name = box, index = 1

Getting mesh sizing parameters
	Mesh sizing name - box
	Done getting mesh sizing parameters
ERROR:: BAD STATUS = -276 from matsol (called from solveSketchOrig:63376)
 CAPS Info: Hit last success -- going live!
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 2
	Name = box, index = 1
	Name = farfield, index = 2
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 1
	Name = box, index = 1

Getting mesh sizing parameters
	Mesh sizing name - box
	Done getting mesh sizing parameters
ERROR:: BAD STATUS = -276 from matsol (called from solveSketchOrig:63376)
 CAPS Info: Hit last success -- going live!
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 2
	Name = box, index = 1
	Name = farfield, index = 2
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 1
	Name = box, index = 1

Getting mesh sizing parameters
	Mesh sizing name - box
	Done getting mesh sizing parameters
ERROR:: BAD STATUS = -276 from matsol (called from solveSketchOrig:63376)
 CAPS Info: Hit last success -- going live!
ERROR:: BAD STATUS = -276 from matsol (called from solveSketchOrig:63376)
 CAPS Info: Hit last success -- going live!
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 2
	Name = box, index = 1
	Name = farfield, index = 2
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 1
	Name = box, index = 1

Getting mesh sizing parameters
	Mesh sizing name - box
	Done getting mesh sizing parameters
ERROR:: BAD STATUS = -276 from matsol (called from solveSketchOrig:63376)
 CAPS Info: Hit last success -- going live!
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 2
	Name = box, index = 1
	Name = farfield, index = 2
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 1
	Name = box, index = 1

Getting mesh sizing parameters
	Mesh sizing name - box
	Done getting mesh sizing parameters
ERROR:: BAD STATUS = -276 from matsol (called from solveSketchOrig:63376)
 CAPS Info: Hit last success -- going live!
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 2
	Name = box, index = 1
	Name = farfield, index = 2
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 1
	Name = box, index = 1

Getting mesh sizing parameters
	Mesh sizing name - box
	Done getting mesh sizing parameters
ERROR:: BAD STATUS = -276 from matsol (called from solveSketchOrig:63376)
ok
test_nodeBody (test_egadsTess.TestEGADS.test_nodeBody) ... Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 2
	Name = nodeBody, index = 1
	Name = farfield, index = 2
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 0
ok
test_phase (test_egadsTess.TestEGADS.test_phase) ... ERROR:: BAD STATUS = -276 from matsol (called from solveSketchOrig:63376)
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 2
	Name = box, index = 1
	Name = farfield, index = 2
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 1
	Name = box, index = 1

Getting mesh sizing parameters
	Mesh sizing name - box
	Done getting mesh sizing parameters
ERROR:: BAD STATUS = -276 from matsol (called from solveSketchOrig:63376)
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 2
	Name = box, index = 1
	Name = farfield, index = 2
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 1
	Name = box, index = 1

Getting mesh sizing parameters
	Mesh sizing name - box
	Done getting mesh sizing parameters
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 2
	Name = box, index = 1
	Name = farfield, index = 2
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 1
	Name = box, index = 1

Getting mesh sizing parameters
	Mesh sizing name - box
	Done getting mesh sizing parameters
ok
test_reenter (test_egadsTess.TestEGADS.test_reenter) ... Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 2
	Name = Farfield, index = 1
	Name = Wing1, index = 2
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 4
	Name = Farfield, index = 1
	Name = riteWing, index = 2
	Name = leftWing, index = 3
	Name = trailingEdge, index = 4

Getting mesh sizing parameters
	Mesh sizing name - Farfield
	Done getting mesh sizing parameters

Writing Binary VTK file ....
Finished writing Binary VTK file


Writing vtk file ....

Writing vtk surface file ....

capsGroups found:
  1: Farfield
  2: Wing1
Finished writing vtk file


Writing FAST file ....
Finished writing FAST file


Writing SU2 file ....
Finished writing SU2 file


Writing Binary STL file ....
Finished writing Binary STL file


Writing ASCII STL file ....
Finished writing ASCII STL file


Writing Tecplot file ....
Finished writing Tecplot file


Writing ugrid file ....
Finished writing ugrid file

Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 2
	Name = Farfield, index = 1
	Name = Wing1, index = 2
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 4
	Name = Farfield, index = 1
	Name = riteWing, index = 2
	Name = leftWing, index = 3
	Name = trailingEdge, index = 4

Getting mesh sizing parameters
	Mesh sizing name - Farfield
	Done getting mesh sizing parameters

Writing Binary VTK file ....
Finished writing Binary VTK file


Writing vtk file ....

Writing vtk surface file ....

capsGroups found:
  1: Farfield
  2: Wing1
Finished writing vtk file


Writing FAST file ....
Finished writing FAST file


Writing SU2 file ....
Finished writing SU2 file


Writing Binary STL file ....
Finished writing Binary STL file


Writing ASCII STL file ....
Finished writing ASCII STL file


Writing Tecplot file ....
Finished writing Tecplot file


Writing ugrid file ....
Finished writing ugrid file

ok
test_setInput (test_egadsTess.TestEGADS.test_setInput) ...  EGADS Info: 0 Objects, 0 Reference in Use (of 0) at Close!
ok
test_sphere (test_egadsTess.TestEGADS.test_sphere) ... Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 2
	Name = sphere, index = 1
	Name = farfield, index = 2
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 0
ok
test_torus (test_egadsTess.TestEGADS.test_torus) ... Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 2
	Name = torus, index = 1
	Name = farfield, index = 2
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 0
ok
test_Design_SensFile (test_fun3d.TestFUN3D.test_Design_SensFile) ... Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 3
	Name = Wing1, index = 1
	Name = Wing2, index = 2
	Name = Farfield, index = 3
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 3
	Name = Wing1, index = 1
	Name = Wing2, index = 2
	Name = Farfield, index = 3

Getting mesh sizing parameters
	Mesh sizing name - Farfield
	Done getting mesh sizing parameters
Getting surface mesh for body 1 (of 3)
Getting surface mesh for body 2 (of 3)
Getting surface mesh for body 3 (of 3)
Body 1 (of 3)
Number of nodes    = 6744
Number of elements = 13484
Number of triangle elements      = 13484
Number of quadrilateral elements = 0
Body 2 (of 3)
Number of nodes    = 4919
Number of elements = 9834
Number of triangle elements      = 9834
Number of quadrilateral elements = 0
Body 3 (of 3)
Number of nodes    = 193
Number of elements = 382
Number of triangle elements      = 382
Number of quadrilateral elements = 0
----------------------------
Total number of nodes    = 11856
Total number of elements = 23700
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 3
	Name = Wing1, index = 1
	Name = Wing2, index = 2
	Name = Farfield, index = 3
Number of surface: nodes - 11856, elements - 23700
Getting volume mesh

Generating volume mesh using TetGen.....

Tetgen input string = pYq1.500/0.000T1.00e-16A
Delaunizing vertices...
Delaunay seconds:  0.072303
Creating surface mesh ...
Surface mesh seconds:  0.009666
Recovering boundaries...
Boundary recovery seconds:  0.042994
Removing exterior tetrahedra ...
Spreading region attributes.
Exterior tets removal seconds:  0.014208
Recovering Delaunayness...
Delaunay recovery seconds:  0.025382
Refining mesh...
  15804 insertions, added 8282 points, 509703 tetrahedra in queue.
  5262 insertions, added 1835 points, 519709 tetrahedra in queue.
  7014 insertions, added 1702 points, 478782 tetrahedra in queue.
  9350 insertions, added 1438 points, 305677 tetrahedra in queue.
  12464 insertions, added 1266 points, 7034 tetrahedra in queue.
  16614 insertions, added 1316 points, 8631 tetrahedra in queue.
Refinement seconds:  3.37383
Smoothing vertices...
Mesh smoothing seconds:  0.753833
Improving mesh...
Mesh improvement seconds:  0.020291

Writing nodes.
Writing elements.
Writing faces.
Writing edges.

Output seconds:  0.00331
Total running seconds:  4.31597

Statistics:

  Input points: 11856
  Input facets: 23700
  Input segments: 35550
  Input holes: 2
  Input regions: 0

  Mesh points: 28176
  Mesh tetrahedra: 136458
  Mesh faces: 284766
  Mesh faces on exterior boundary: 23700
  Mesh faces on input facets: 23700
  Mesh edges on input segments: 35550
  Steiner points inside domain: 16320

Done meshing using TetGen!
Getting CFD boundary conditions
	Boundary condition name - Farfield
	Boundary condition name - Wing1
	Boundary condition name - Wing2
	Done getting CFD boundary conditions

Getting CFD design variables.......
	Number of design variables - 5
	Design Variable name - Mach
Warning: No initial value set for Mach
	Design Variable name - area
	Design Variable name - aspect
	Design Variable name - taper
	Design Variable name - twist
	Done getting CFD design variables
Python library was linked, but will not be used!
Creating FUN3D directory tree

Writing MAPBC file ....
Finished writing MAPBC file

Warning: The fun3d.nml file will be overwritten!
Writing fun3d.nml
Info: No recognized data transfer names found.
ok
test_Design_Sensitivity (test_fun3d.TestFUN3D.test_Design_Sensitivity) ... Getting CFD boundary conditions
	Boundary condition name - Farfield
	Boundary condition name - Wing1
	Boundary condition name - Wing2
	Done getting CFD boundary conditions

Getting CFD design variables.......
	Number of design variables - 6
	Design Variable name - Alpha
	Design Variable name - Beta
Warning: No initial value set for Beta
	Design Variable name - area
	Design Variable name - aspect
	Design Variable name - taper
	Design Variable name - twist
	Done getting CFD design variables
Getting CFD functional.......
	Number of design variables - 2
	Objective name - Composite
	Objective name - Lift^2
	Done getting CFD functional
Python library was linked, but will not be used!
Creating FUN3D directory tree
Writing rubber.data 

Writing MAPBC file ....
Finished writing MAPBC file

Warning: The fun3d.nml file will be overwritten!
Writing fun3d.nml
Info: No recognized data transfer names found.
Reading rubber.data 
Creating FUN3D directory tree
DesignVariable = Alpha
DesignVariable = Beta
DesignVariable = area
DesignVariable = aspect
DesignVariable = taper
DesignVariable = twist
Writing sensitivity file for body 1, File - Rubberize/model.tec.1.sd1
Writing sensitivity file for body 2, File - Rubberize/model.tec.2.sd1
Writing sensitivity file for body 3, File - Rubberize/model.tec.3.sd1
Writing rubber.data 

Writing MAPBC file ....
Finished writing MAPBC file


Using Python to write FUN3D namelist (fun3d.nml)
	Overwrite_NML is set to 'True' - a new namelist will be created
	Creating namelist
	Done writing nml file with Python
Info: No recognized data transfer names found.
Reading rubber.data 

Getting CFD design variables.......
	Number of design variables - 1
	Design Variable name - Alpha
	Done getting CFD design variables
Getting CFD functional.......
	Number of design variables - 2
	Objective name - Composite
	Objective name - Lift^2
	Done getting CFD functional
Creating FUN3D directory tree
DesignVariable = Alpha
Writing rubber.data 

Writing MAPBC file ....
Finished writing MAPBC file


Using Python to write FUN3D namelist (fun3d.nml)
	Overwrite_NML is set to 'True' - a new namelist will be created
	Creating namelist
	Done writing nml file with Python
Info: No recognized data transfer names found.
Reading rubber.data 
ok
test_Mesh_Morph_Sensitivity (test_fun3d.TestFUN3D.test_Mesh_Morph_Sensitivity) ... Getting CFD boundary conditions
	Boundary condition name - Farfield
	Boundary condition name - Wing1
	Boundary condition name - Wing2
	Done getting CFD boundary conditions

Getting CFD design variables.......
	Number of design variables - 6
	Design Variable name - Alpha
	Design Variable name - Beta
Warning: No initial value set for Beta
	Design Variable name - area
	Design Variable name - aspect
	Design Variable name - taper
	Design Variable name - twist
	Done getting CFD design variables
Getting CFD functional.......
	Number of design variables - 2
	Objective name - Composite
	Objective name - Lift^2
	Done getting CFD functional
Python library was linked, but will not be used!
Creating FUN3D directory tree
DesignVariable = Alpha
DesignVariable = Beta
DesignVariable = area
DesignVariable = aspect
DesignVariable = taper
DesignVariable = twist
Writing sensitivity file for body 1, File - Rubberize/model.tec.1.sd1
Writing sensitivity file for body 2, File - Rubberize/model.tec.2.sd1
Writing sensitivity file for body 3, File - Rubberize/model.tec.3.sd1
Writing rubber.data 
Writing surface file for 1 (of 3) in body 1 File - Flow/fun3d_CAPS_body1.dat
Writing surface file for 1 (of 3) in body 1 File - Flow/fun3d_CAPS_body1.dat
Writing surface file for 1 (of 3) in body 1 File - Flow/fun3d_CAPS_body1.dat

Writing MAPBC file ....
Finished writing MAPBC file

Warning: The fun3d.nml file will be overwritten!
Writing fun3d.nml
Info: No recognized data transfer names found.
Reading rubber.data 
Projecting tessellation 1 (of 3) on to new body
Projecting tessellation 2 (of 3) on to new body
Projecting tessellation 3 (of 3) on to new body
Python library was linked, but will not be used!
Creating FUN3D directory tree
DesignVariable = Alpha
DesignVariable = Beta
DesignVariable = area
DesignVariable = aspect
DesignVariable = taper
DesignVariable = twist
Writing sensitivity file for body 1, File - Rubberize/model.tec.1.sd1
Writing sensitivity file for body 2, File - Rubberize/model.tec.2.sd1
Writing sensitivity file for body 3, File - Rubberize/model.tec.3.sd1
Writing surface file for 1 (of 3) in body 1 File - Flow/fun3d_CAPS_body1.dat
Writing surface file for 1 (of 3) in body 1 File - Flow/fun3d_CAPS_body1.dat
Writing surface file for 1 (of 3) in body 1 File - Flow/fun3d_CAPS_body1.dat

Writing MAPBC file ....
Finished writing MAPBC file

Warning: The fun3d.nml file will be overwritten!
Writing fun3d.nml
Info: No recognized data transfer names found.
Reading rubber.data 
Projecting tessellation 1 (of 3) on to new body
Projecting tessellation 2 (of 3) on to new body
Projecting tessellation 3 (of 3) on to new body
Python library was linked, but will not be used!
Creating FUN3D directory tree
DesignVariable = Alpha
DesignVariable = Beta
DesignVariable = area
DesignVariable = aspect
DesignVariable = taper
DesignVariable = twist
Writing sensitivity file for body 1, File - Rubberize/model.tec.1.sd1
Writing sensitivity file for body 2, File - Rubberize/model.tec.2.sd1
Writing sensitivity file for body 3, File - Rubberize/model.tec.3.sd1
Writing surface file for 1 (of 3) in body 1 File - Flow/fun3d_CAPS_body1.dat
Writing surface file for 1 (of 3) in body 1 File - Flow/fun3d_CAPS_body1.dat
Writing surface file for 1 (of 3) in body 1 File - Flow/fun3d_CAPS_body1.dat

Writing MAPBC file ....
Finished writing MAPBC file

Warning: The fun3d.nml file will be overwritten!
Writing fun3d.nml
Info: No recognized data transfer names found.
Reading rubber.data 
ok
test_cythonNML (test_fun3d.TestFUN3D.test_cythonNML) ... Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 3
	Name = Wing1, index = 1
	Name = Wing2, index = 2
	Name = Farfield, index = 3
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 3
	Name = Wing1, index = 1
	Name = Wing2, index = 2
	Name = Farfield, index = 3

Getting mesh sizing parameters
	Mesh sizing name - Farfield
	Done getting mesh sizing parameters
Getting surface mesh for body 1 (of 3)
Getting surface mesh for body 2 (of 3)
Getting surface mesh for body 3 (of 3)
Body 1 (of 3)
Number of nodes    = 6744
Number of elements = 13484
Number of triangle elements      = 13484
Number of quadrilateral elements = 0
Body 2 (of 3)
Number of nodes    = 4919
Number of elements = 9834
Number of triangle elements      = 9834
Number of quadrilateral elements = 0
Body 3 (of 3)
Number of nodes    = 193
Number of elements = 382
Number of triangle elements      = 382
Number of quadrilateral elements = 0
----------------------------
Total number of nodes    = 11856
Total number of elements = 23700
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 3
	Name = Wing1, index = 1
	Name = Wing2, index = 2
	Name = Farfield, index = 3
Number of surface: nodes - 11856, elements - 23700
Getting volume mesh

Generating volume mesh using TetGen.....

Tetgen input string = pYq1.500/0.000T1.00e-16A
Delaunizing vertices...
Delaunay seconds:  0.071563
Creating surface mesh ...
Surface mesh seconds:  0.009872
Recovering boundaries...
Boundary recovery seconds:  0.042403
Removing exterior tetrahedra ...
Spreading region attributes.
Exterior tets removal seconds:  0.014223
Recovering Delaunayness...
Delaunay recovery seconds:  0.025348
Refining mesh...
  15804 insertions, added 8282 points, 509703 tetrahedra in queue.
  5262 insertions, added 1835 points, 519709 tetrahedra in queue.
  7014 insertions, added 1702 points, 478782 tetrahedra in queue.
  9350 insertions, added 1438 points, 305677 tetrahedra in queue.
  12464 insertions, added 1266 points, 7034 tetrahedra in queue.
  16614 insertions, added 1316 points, 8631 tetrahedra in queue.
Refinement seconds:  3.36283
Smoothing vertices...
Mesh smoothing seconds:  0.75268
Improving mesh...
Mesh improvement seconds:  0.020372

Writing nodes.
Writing elements.
Writing faces.
Writing edges.

Output seconds:  0.003453
Total running seconds:  4.30302

Statistics:

  Input points: 11856
  Input facets: 23700
  Input segments: 35550
  Input holes: 2
  Input regions: 0

  Mesh points: 28176
  Mesh tetrahedra: 136458
  Mesh faces: 284766
  Mesh faces on exterior boundary: 23700
  Mesh faces on input facets: 23700
  Mesh edges on input segments: 35550
  Steiner points inside domain: 16320

Done meshing using TetGen!
Getting CFD boundary conditions
	Boundary condition name - Farfield
	Boundary condition name - Wing1
	Boundary condition name - Wing2
	Done getting CFD boundary conditions

Writing MAPBC file ....
Finished writing MAPBC file


Using Python to write FUN3D namelist (fun3d.nml)

	Reading /Users/jenkins/workspace/ESP_bPreBuilt/ESP126/EngSketchPad/src/CAPS/aim/unitTest/pyCAPS/workDir_fun3dTest/Scratch/fun3dAIM4/fun3d.nml .....
	Appending namelist
	Done writing nml file with Python
Info: No recognized data transfer names found.
ok
test_cythonNMLError (test_fun3d.TestFUN3D.test_cythonNMLError) ... ok
test_cythonNMLReentrance (test_fun3d.TestFUN3D.test_cythonNMLReentrance) ... Getting CFD boundary conditions
	Boundary condition name - Farfield
	Boundary condition name - Wing1
	Boundary condition name - Wing2
	Done getting CFD boundary conditions

Writing MAPBC file ....
Finished writing MAPBC file


Using Python to write FUN3D namelist (fun3d.nml)
	/Users/jenkins/workspace/ESP_bPreBuilt/ESP126/EngSketchPad/src/CAPS/aim/unitTest/pyCAPS/workDir_fun3dTest/Scratch/fun3dAIM6/fun3d.nml not found!
	Creating namelist
	Done writing nml file with Python
Info: No recognized data transfer names found.

Writing MAPBC file ....
Finished writing MAPBC file


Using Python to write FUN3D namelist (fun3d.nml)

	Reading /Users/jenkins/workspace/ESP_bPreBuilt/ESP126/EngSketchPad/src/CAPS/aim/unitTest/pyCAPS/workDir_fun3dTest/Scratch/fun3dAIM6/fun3d.nml .....
	Appending namelist
	Done writing nml file with Python
Info: No recognized data transfer names found.
ok
test_invalidBoundary (test_fun3d.TestFUN3D.test_invalidBoundary) ... Getting CFD boundary conditions
	Boundary condition name - Wing1
ok
test_invalidBoundaryName (test_fun3d.TestFUN3D.test_invalidBoundaryName) ... Getting CFD boundary conditions
	Boundary condition name - Farfield
	Boundary condition name - Wing1
	Boundary condition name - X
ok
test_journal (test_fun3d.TestFUN3D.test_journal) ... Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 3
	Name = Wing1, index = 1
	Name = Wing2, index = 2
	Name = Farfield, index = 3
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 3
	Name = Wing1, index = 1
	Name = Wing2, index = 2
	Name = Farfield, index = 3

Getting mesh sizing parameters
	Mesh sizing name - Farfield
	Done getting mesh sizing parameters
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 3
	Name = Wing1, index = 1
	Name = Wing2, index = 2
	Name = Farfield, index = 3
Number of surface: nodes - 1205, elements - 2398
Getting volume mesh

Generating volume mesh using TetGen.....

Tetgen input string = pYq1.500/0.000QT1.00e-16A
Done meshing using TetGen!
Getting CFD boundary conditions
	Boundary condition name - Farfield
	Boundary condition name - Wing1
	Boundary condition name - Wing2
	Done getting CFD boundary conditions

Getting CFD design variables.......
	Number of design variables - 4
	Design Variable name - area
	Design Variable name - aspect
	Design Variable name - taper
	Design Variable name - twist
	Done getting CFD design variables
Python library was linked, but will not be used!
Creating FUN3D directory tree

Writing MAPBC file ....
Finished writing MAPBC file

Warning: The fun3d.nml file will be overwritten!
Writing fun3d.nml
Info: No recognized data transfer names found.
 EGADS Info: 0 Objects, 0 Reference in Use (of 0) at Close!
 CAPS Info: Hit last success -- going live!
 CAPS Info: Hit last success -- going live!
 CAPS Info: Hit last success -- going live!
 CAPS Info: Hit last success -- going live!
 CAPS Info: Hit last success -- going live!
 CAPS Info: Hit last success -- going live!
 CAPS Info: Hit last success -- going live!
 CAPS Info: Hit last success -- going live!
 CAPS Info: Hit last success -- going live!
 CAPS Info: Hit last success -- going live!
 CAPS Info: Hit last success -- going live!
 CAPS Info: Hit last success -- going live!
 CAPS Info: Hit last success -- going live!
 CAPS Info: Hit last success -- going live!
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 3
	Name = Wing1, index = 1
	Name = Wing2, index = 2
	Name = Farfield, index = 3
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 3
	Name = Wing1, index = 1
	Name = Wing2, index = 2
	Name = Farfield, index = 3

Getting mesh sizing parameters
	Mesh sizing name - Farfield
	Done getting mesh sizing parameters
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 3
	Name = Wing1, index = 1
	Name = Wing2, index = 2
	Name = Farfield, index = 3
Number of surface: nodes - 1205, elements - 2398
Getting volume mesh

Generating volume mesh using TetGen.....

Tetgen input string = pYq1.500/0.000QT1.00e-16A
Done meshing using TetGen!
Getting CFD boundary conditions
	Boundary condition name - Farfield
	Boundary condition name - Wing1
	Boundary condition name - Wing2
	Done getting CFD boundary conditions

Getting CFD design variables.......
	Number of design variables - 4
	Design Variable name - area
	Design Variable name - aspect
	Design Variable name - taper
	Design Variable name - twist
	Done getting CFD design variables
Python library was linked, but will not be used!
Creating FUN3D directory tree

Writing MAPBC file ....
Finished writing MAPBC file

Warning: The fun3d.nml file will be overwritten!
Writing fun3d.nml
Info: No recognized data transfer names found.
 CAPS Info: Hit last success -- going live!
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 3
	Name = Wing1, index = 1
	Name = Wing2, index = 2
	Name = Farfield, index = 3
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 3
	Name = Wing1, index = 1
	Name = Wing2, index = 2
	Name = Farfield, index = 3

Getting mesh sizing parameters
	Mesh sizing name - Farfield
	Done getting mesh sizing parameters
 CAPS Info: Hit last success -- going live!
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 3
	Name = Wing1, index = 1
	Name = Wing2, index = 2
	Name = Farfield, index = 3
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 3
	Name = Wing1, index = 1
	Name = Wing2, index = 2
	Name = Farfield, index = 3

Getting mesh sizing parameters
	Mesh sizing name - Farfield
	Done getting mesh sizing parameters
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 3
	Name = Wing1, index = 1
	Name = Wing2, index = 2
	Name = Farfield, index = 3
Getting CFD boundary conditions
	Boundary condition name - Farfield
	Boundary condition name - Wing1
	Boundary condition name - Wing2
	Done getting CFD boundary conditions

Getting CFD design variables.......
	Number of design variables - 4
	Design Variable name - area
	Design Variable name - aspect
	Design Variable name - taper
	Design Variable name - twist
	Done getting CFD design variables
 CAPS Info: Hit last success -- going live!
 CAPS Info: Hit last success -- going live!
 CAPS Info: Hit last success -- going live!
 CAPS Info: Hit last success -- going live!
 CAPS Info: Hit last success -- going live!
 CAPS Info: Hit last success -- going live!
ok
test_moving_body (test_fun3d.TestFUN3D.test_moving_body) ... Getting CFD boundary conditions
	Boundary condition name - Farfield
	Boundary condition name - Wing1
	Boundary condition name - Wing2
	Done getting CFD boundary conditions
Python library was linked, but will not be used!

Writing MAPBC file ....
Finished writing MAPBC file

Warning: The fun3d.nml file will be overwritten!
Writing fun3d.nml
Info: No recognized data transfer names found.
Writing moving_body.input
ok
test_overwriteNML (test_fun3d.TestFUN3D.test_overwriteNML) ... Getting CFD boundary conditions
	Boundary condition name - Farfield
	Boundary condition name - Wing1
	Boundary condition name - Wing2
	Done getting CFD boundary conditions
Python library was linked, but will not be used!

Writing MAPBC file ....
Finished writing MAPBC file

Since Python was not linked and/or being used, the "Overwrite_NML" input needs to be set to "True" to give permission to create a new fun3d.nml. fun3d.nml will NOT be updated!!
Info: No recognized data transfer names found.
ok
test_phase (test_fun3d.TestFUN3D.test_phase) ... Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 3
	Name = Wing1, index = 1
	Name = Wing2, index = 2
	Name = Farfield, index = 3
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 3
	Name = Wing1, index = 1
	Name = Wing2, index = 2
	Name = Farfield, index = 3

Getting mesh sizing parameters
	Mesh sizing name - Farfield
	Done getting mesh sizing parameters
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 3
	Name = Wing1, index = 1
	Name = Wing2, index = 2
	Name = Farfield, index = 3
Number of surface: nodes - 11856, elements - 23700
Getting volume mesh

Generating volume mesh using TetGen.....

Tetgen input string = pYq1.500/0.000QT1.00e-16A
Done meshing using TetGen!
Getting CFD boundary conditions
	Boundary condition name - Farfield
	Boundary condition name - Wing1
	Boundary condition name - Wing2
	Done getting CFD boundary conditions
Python library was linked, but will not be used!

Writing MAPBC file ....
Finished writing MAPBC file

Since Python was not linked and/or being used, the "Overwrite_NML" input needs to be set to "True" to give permission to create a new fun3d.nml. fun3d.nml will NOT be updated!!
Info: No recognized data transfer names found.
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 3
	Name = Wing1, index = 1
	Name = Wing2, index = 2
	Name = Farfield, index = 3
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 3
	Name = Wing1, index = 1
	Name = Wing2, index = 2
	Name = Farfield, index = 3

Getting mesh sizing parameters
	Mesh sizing name - Farfield
	Done getting mesh sizing parameters
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 3
	Name = Wing1, index = 1
	Name = Wing2, index = 2
	Name = Farfield, index = 3
Getting CFD boundary conditions
	Boundary condition name - Farfield
	Boundary condition name - Wing1
	Boundary condition name - Wing2
	Done getting CFD boundary conditions
Python library was linked, but will not be used!

Writing MAPBC file ....
Finished writing MAPBC file

Since Python was not linked and/or being used, the "Overwrite_NML" input needs to be set to "True" to give permission to create a new fun3d.nml. fun3d.nml will NOT be updated!!
Info: No recognized data transfer names found.
ok
test_reenter (test_fun3d.TestFUN3D.test_reenter) ... Getting CFD boundary conditions
	Boundary condition name - Farfield
	Boundary condition name - Wing1
	Boundary condition name - Wing2
	Done getting CFD boundary conditions
Python library was linked, but will not be used!

Writing MAPBC file ....
Finished writing MAPBC file

Warning: The fun3d.nml file will be overwritten!
Writing fun3d.nml
Info: No recognized data transfer names found.
Getting CFD boundary conditions
	Boundary condition name - Farfield
	Boundary condition name - Wing1
	Boundary condition name - Wing2
	Done getting CFD boundary conditions
Python library was linked, but will not be used!

Writing MAPBC file ....
Finished writing MAPBC file

Warning: The fun3d.nml file will be overwritten!
Writing fun3d.nml
Info: No recognized data transfer names found.
ok
test_symmetry (test_fun3d.TestFUN3D.test_symmetry) ... Getting CFD boundary conditions
	Boundary condition name - Farfield
	Boundary condition name - Wing1
	Boundary condition name - Wing2
	Done getting CFD boundary conditions
Python library was linked, but will not be used!

Writing MAPBC file ....
Finished writing MAPBC file

Since Python was not linked and/or being used, the "Overwrite_NML" input needs to be set to "True" to give permission to create a new fun3d.nml. fun3d.nml will NOT be updated!!
Info: No recognized data transfer names found.
ok
test_box1 (test_masstran.TestMasstran.test_box1) ... Mapping Csys attributes ................
	Number of unique Csys attributes = 0

Getting FEA coordinate systems.......
	Number of coordinate systems - 0
	No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
	Number of unique capsConstraint attributes = 0
Mapping capsLoad attributes ................
	Number of unique capsLoad attributes = 0
Mapping capsBound attributes ................
	Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
	Number of unique capsConnect attributes = 0
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = box1, index = 1
Setting FEA Data
	Mesh for body = 0
	Number of nodal coordinates = 2402
	Number of elements = 2400
	Elemental Nodes = 0
	Elemental Rods  = 0
	Elemental Tria3 = 0
	Elemental Quad4 = 2400

Getting FEA materials.......
	Number of materials - 2
	Material name - madeupium
	Material name - unobtainium
	Done getting FEA materials

Getting FEA properties.......
	Number of properties - 1
	Property name - box1
	Done getting FEA properties
Updating mesh element types based on properties input
Updating mesh element types based on properties input

Getting FEA design variables.......
	Number of design variables          - 7
	Design_Variable name - H
	Design_Variable name - L
	Design_Variable name - W
	Design_Variable name - m0
	Design_Variable name - m1
	Design_Variable name - x0
	Design_Variable name - x1
	Design_Variable_Relation name - rho_madeupium
	Name madeupium not found in attribute map!!!!
	Design_Variable_Relation name - rho_unobtainium
	Name unobtainium not found in attribute map!!!!
	Design_Variable_Relation name - thick_box1
	Number of design variable relations - 3
	Done getting FEA design variables
===&gt; L
Mapping Csys attributes ................
	Number of unique Csys attributes = 0

Getting FEA coordinate systems.......
	Number of coordinate systems - 0
	No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
	Number of unique capsConstraint attributes = 0
Mapping capsLoad attributes ................
	Number of unique capsLoad attributes = 0
Mapping capsBound attributes ................
	Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
	Number of unique capsConnect attributes = 0
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = box1, index = 1
Setting FEA Data
	Mesh for body = 0
	Number of nodal coordinates = 2402
	Number of elements = 2400
	Elemental Nodes = 0
	Elemental Rods  = 0
	Elemental Tria3 = 0
	Elemental Quad4 = 2400
Updating mesh element types based on properties input
Mapping Csys attributes ................
	Number of unique Csys attributes = 0

Getting FEA coordinate systems.......
	Number of coordinate systems - 0
	No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
	Number of unique capsConstraint attributes = 0
Mapping capsLoad attributes ................
	Number of unique capsLoad attributes = 0
Mapping capsBound attributes ................
	Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
	Number of unique capsConnect attributes = 0
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = box1, index = 1
Setting FEA Data
	Mesh for body = 0
	Number of nodal coordinates = 2402
	Number of elements = 2400
	Elemental Nodes = 0
	Elemental Rods  = 0
	Elemental Tria3 = 0
	Elemental Quad4 = 2400
Updating mesh element types based on properties input
===&gt; W
Mapping Csys attributes ................
	Number of unique Csys attributes = 0

Getting FEA coordinate systems.......
	Number of coordinate systems - 0
	No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
	Number of unique capsConstraint attributes = 0
Mapping capsLoad attributes ................
	Number of unique capsLoad attributes = 0
Mapping capsBound attributes ................
	Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
	Number of unique capsConnect attributes = 0
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = box1, index = 1
Setting FEA Data
	Mesh for body = 0
	Number of nodal coordinates = 2402
	Number of elements = 2400
	Elemental Nodes = 0
	Elemental Rods  = 0
	Elemental Tria3 = 0
	Elemental Quad4 = 2400
Updating mesh element types based on properties input
Mapping Csys attributes ................
	Number of unique Csys attributes = 0

Getting FEA coordinate systems.......
	Number of coordinate systems - 0
	No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
	Number of unique capsConstraint attributes = 0
Mapping capsLoad attributes ................
	Number of unique capsLoad attributes = 0
Mapping capsBound attributes ................
	Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
	Number of unique capsConnect attributes = 0
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = box1, index = 1
Setting FEA Data
	Mesh for body = 0
	Number of nodal coordinates = 2402
	Number of elements = 2400
	Elemental Nodes = 0
	Elemental Rods  = 0
	Elemental Tria3 = 0
	Elemental Quad4 = 2400
Updating mesh element types based on properties input
===&gt; H
Mapping Csys attributes ................
	Number of unique Csys attributes = 0

Getting FEA coordinate systems.......
	Number of coordinate systems - 0
	No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
	Number of unique capsConstraint attributes = 0
Mapping capsLoad attributes ................
	Number of unique capsLoad attributes = 0
Mapping capsBound attributes ................
	Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
	Number of unique capsConnect attributes = 0
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = box1, index = 1
Setting FEA Data
	Mesh for body = 0
	Number of nodal coordinates = 2402
	Number of elements = 2400
	Elemental Nodes = 0
	Elemental Rods  = 0
	Elemental Tria3 = 0
	Elemental Quad4 = 2400
Updating mesh element types based on properties input
Mapping Csys attributes ................
	Number of unique Csys attributes = 0

Getting FEA coordinate systems.......
	Number of coordinate systems - 0
	No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
	Number of unique capsConstraint attributes = 0
Mapping capsLoad attributes ................
	Number of unique capsLoad attributes = 0
Mapping capsBound attributes ................
	Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
	Number of unique capsConnect attributes = 0
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = box1, index = 1
Setting FEA Data
	Mesh for body = 0
	Number of nodal coordinates = 2402
	Number of elements = 2400
	Elemental Nodes = 0
	Elemental Rods  = 0
	Elemental Tria3 = 0
	Elemental Quad4 = 2400
Updating mesh element types based on properties input
===&gt; x0
Mapping Csys attributes ................
	Number of unique Csys attributes = 0

Getting FEA coordinate systems.......
	Number of coordinate systems - 0
	No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
	Number of unique capsConstraint attributes = 0
Mapping capsLoad attributes ................
	Number of unique capsLoad attributes = 0
Mapping capsBound attributes ................
	Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
	Number of unique capsConnect attributes = 0
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = box1, index = 1
Setting FEA Data
	Mesh for body = 0
	Number of nodal coordinates = 2402
	Number of elements = 2400
	Elemental Nodes = 0
	Elemental Rods  = 0
	Elemental Tria3 = 0
	Elemental Quad4 = 2400
Updating mesh element types based on properties input

Getting FEA design variables.......
	Number of design variables          - 4
	Design_Variable name - m0
	Design_Variable name - m1
	Design_Variable name - x0
	Design_Variable name - x1
	Design_Variable_Relation name - rho_madeupium
	Name madeupium not found in attribute map!!!!
	Design_Variable_Relation name - rho_unobtainium
	Name unobtainium not found in attribute map!!!!
	Design_Variable_Relation name - thick_box1
	Number of design variable relations - 3
	Done getting FEA design variables
Updating mesh element types based on properties input

Getting FEA design variables.......
	Number of design variables          - 4
	Design_Variable name - m0
	Design_Variable name - m1
	Design_Variable name - x0
	Design_Variable name - x1
	Design_Variable_Relation name - rho_madeupium
	Name madeupium not found in attribute map!!!!
	Design_Variable_Relation name - rho_unobtainium
	Name unobtainium not found in attribute map!!!!
	Design_Variable_Relation name - thick_box1
	Number of design variable relations - 3
	Done getting FEA design variables
===&gt; x1
Updating mesh element types based on properties input

Getting FEA design variables.......
	Number of design variables          - 4
	Design_Variable name - m0
	Design_Variable name - m1
	Design_Variable name - x0
	Design_Variable name - x1
	Design_Variable_Relation name - rho_madeupium
	Name madeupium not found in attribute map!!!!
	Design_Variable_Relation name - rho_unobtainium
	Name unobtainium not found in attribute map!!!!
	Design_Variable_Relation name - thick_box1
	Number of design variable relations - 3
	Done getting FEA design variables
Updating mesh element types based on properties input

Getting FEA design variables.......
	Number of design variables          - 4
	Design_Variable name - m0
	Design_Variable name - m1
	Design_Variable name - x0
	Design_Variable name - x1
	Design_Variable_Relation name - rho_madeupium
	Name madeupium not found in attribute map!!!!
	Design_Variable_Relation name - rho_unobtainium
	Name unobtainium not found in attribute map!!!!
	Design_Variable_Relation name - thick_box1
	Number of design variable relations - 3
	Done getting FEA design variables
===&gt; m0
Updating mesh element types based on properties input

Getting FEA design variables.......
	Number of design variables          - 4
	Design_Variable name - m0
	Design_Variable name - m1
	Design_Variable name - x0
	Design_Variable name - x1
	Design_Variable_Relation name - rho_madeupium
	Name madeupium not found in attribute map!!!!
	Design_Variable_Relation name - rho_unobtainium
	Name unobtainium not found in attribute map!!!!
	Design_Variable_Relation name - thick_box1
	Number of design variable relations - 3
	Done getting FEA design variables
Updating mesh element types based on properties input

Getting FEA design variables.......
	Number of design variables          - 4
	Design_Variable name - m0
	Design_Variable name - m1
	Design_Variable name - x0
	Design_Variable name - x1
	Design_Variable_Relation name - rho_madeupium
	Name madeupium not found in attribute map!!!!
	Design_Variable_Relation name - rho_unobtainium
	Name unobtainium not found in attribute map!!!!
	Design_Variable_Relation name - thick_box1
	Number of design variable relations - 3
	Done getting FEA design variables
===&gt; m1
Updating mesh element types based on properties input

Getting FEA design variables.......
	Number of design variables          - 4
	Design_Variable name - m0
	Design_Variable name - m1
	Design_Variable name - x0
	Design_Variable name - x1
	Design_Variable_Relation name - rho_madeupium
	Name madeupium not found in attribute map!!!!
	Design_Variable_Relation name - rho_unobtainium
	Name unobtainium not found in attribute map!!!!
	Design_Variable_Relation name - thick_box1
	Number of design variable relations - 3
	Done getting FEA design variables
Updating mesh element types based on properties input

Getting FEA design variables.......
	Number of design variables          - 4
	Design_Variable name - m0
	Design_Variable name - m1
	Design_Variable name - x0
	Design_Variable name - x1
	Design_Variable_Relation name - rho_madeupium
	Name madeupium not found in attribute map!!!!
	Design_Variable_Relation name - rho_unobtainium
	Name unobtainium not found in attribute map!!!!
	Design_Variable_Relation name - thick_box1
	Number of design variable relations - 3
	Done getting FEA design variables
ok
test_box2 (test_masstran.TestMasstran.test_box2) ... Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = box1, index = 1
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 0
Mapping Csys attributes ................
	Number of unique Csys attributes = 0

Getting FEA coordinate systems.......
	Number of coordinate systems - 0
	No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
	Number of unique capsConstraint attributes = 0
Mapping capsLoad attributes ................
	Number of unique capsLoad attributes = 0
Mapping capsBound attributes ................
	Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
	Number of unique capsConnect attributes = 0
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = box1, index = 1
Setting FEA Data
	Mesh for body = 0
	Number of nodal coordinates = 1692
	Number of elements = 3380
	Elemental Nodes = 0
	Elemental Rods  = 0
	Elemental Tria3 = 3380
	Elemental Quad4 = 0

Getting FEA properties.......
	Number of properties - 1
	Property name - box1
	Done getting FEA properties
Updating mesh element types based on properties input
Updating mesh element types based on properties input

Getting FEA design variables.......
	Number of design variables          - 7
	Design_Variable name - H
	Design_Variable name - L
	Design_Variable name - W
	Design_Variable name - m0
	Design_Variable name - m1
	Design_Variable name - x0
	Design_Variable name - x1
	Design_Variable_Relation name - rho_madeupium
	Name madeupium not found in attribute map!!!!
	Design_Variable_Relation name - rho_unobtainium
	Name unobtainium not found in attribute map!!!!
	Design_Variable_Relation name - thick_box1
	Number of design variable relations - 3
	Done getting FEA design variables
===&gt; L
Mapping Csys attributes ................
	Number of unique Csys attributes = 0

Getting FEA coordinate systems.......
	Number of coordinate systems - 0
	No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
	Number of unique capsConstraint attributes = 0
Mapping capsLoad attributes ................
	Number of unique capsLoad attributes = 0
Mapping capsBound attributes ................
	Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
	Number of unique capsConnect attributes = 0
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = box1, index = 1
Projecting tessellation 1 (of 1) on to new body
Setting FEA Data
	Mesh for body = 0
	Number of nodal coordinates = 1692
	Number of elements = 3380
	Elemental Nodes = 0
	Elemental Rods  = 0
	Elemental Tria3 = 3380
	Elemental Quad4 = 0
Updating mesh element types based on properties input
Mapping Csys attributes ................
	Number of unique Csys attributes = 0

Getting FEA coordinate systems.......
	Number of coordinate systems - 0
	No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
	Number of unique capsConstraint attributes = 0
Mapping capsLoad attributes ................
	Number of unique capsLoad attributes = 0
Mapping capsBound attributes ................
	Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
	Number of unique capsConnect attributes = 0
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = box1, index = 1
Projecting tessellation 1 (of 1) on to new body
Setting FEA Data
	Mesh for body = 0
	Number of nodal coordinates = 1692
	Number of elements = 3380
	Elemental Nodes = 0
	Elemental Rods  = 0
	Elemental Tria3 = 3380
	Elemental Quad4 = 0
Updating mesh element types based on properties input
===&gt; W
Mapping Csys attributes ................
	Number of unique Csys attributes = 0

Getting FEA coordinate systems.......
	Number of coordinate systems - 0
	No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
	Number of unique capsConstraint attributes = 0
Mapping capsLoad attributes ................
	Number of unique capsLoad attributes = 0
Mapping capsBound attributes ................
	Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
	Number of unique capsConnect attributes = 0
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = box1, index = 1
Projecting tessellation 1 (of 1) on to new body
Setting FEA Data
	Mesh for body = 0
	Number of nodal coordinates = 1692
	Number of elements = 3380
	Elemental Nodes = 0
	Elemental Rods  = 0
	Elemental Tria3 = 3380
	Elemental Quad4 = 0
Updating mesh element types based on properties input
Mapping Csys attributes ................
	Number of unique Csys attributes = 0

Getting FEA coordinate systems.......
	Number of coordinate systems - 0
	No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
	Number of unique capsConstraint attributes = 0
Mapping capsLoad attributes ................
	Number of unique capsLoad attributes = 0
Mapping capsBound attributes ................
	Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
	Number of unique capsConnect attributes = 0
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = box1, index = 1
Projecting tessellation 1 (of 1) on to new body
Setting FEA Data
	Mesh for body = 0
	Number of nodal coordinates = 1692
	Number of elements = 3380
	Elemental Nodes = 0
	Elemental Rods  = 0
	Elemental Tria3 = 3380
	Elemental Quad4 = 0
Updating mesh element types based on properties input
===&gt; H
Mapping Csys attributes ................
	Number of unique Csys attributes = 0

Getting FEA coordinate systems.......
	Number of coordinate systems - 0
	No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
	Number of unique capsConstraint attributes = 0
Mapping capsLoad attributes ................
	Number of unique capsLoad attributes = 0
Mapping capsBound attributes ................
	Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
	Number of unique capsConnect attributes = 0
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = box1, index = 1
Projecting tessellation 1 (of 1) on to new body
Setting FEA Data
	Mesh for body = 0
	Number of nodal coordinates = 1692
	Number of elements = 3380
	Elemental Nodes = 0
	Elemental Rods  = 0
	Elemental Tria3 = 3380
	Elemental Quad4 = 0
Updating mesh element types based on properties input
Mapping Csys attributes ................
	Number of unique Csys attributes = 0

Getting FEA coordinate systems.......
	Number of coordinate systems - 0
	No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
	Number of unique capsConstraint attributes = 0
Mapping capsLoad attributes ................
	Number of unique capsLoad attributes = 0
Mapping capsBound attributes ................
	Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
	Number of unique capsConnect attributes = 0
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = box1, index = 1
Projecting tessellation 1 (of 1) on to new body
Setting FEA Data
	Mesh for body = 0
	Number of nodal coordinates = 1692
	Number of elements = 3380
	Elemental Nodes = 0
	Elemental Rods  = 0
	Elemental Tria3 = 3380
	Elemental Quad4 = 0
Updating mesh element types based on properties input
===&gt; x0
Mapping Csys attributes ................
	Number of unique Csys attributes = 0

Getting FEA coordinate systems.......
	Number of coordinate systems - 0
	No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
	Number of unique capsConstraint attributes = 0
Mapping capsLoad attributes ................
	Number of unique capsLoad attributes = 0
Mapping capsBound attributes ................
	Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
	Number of unique capsConnect attributes = 0
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = box1, index = 1
Projecting tessellation 1 (of 1) on to new body
Setting FEA Data
	Mesh for body = 0
	Number of nodal coordinates = 1692
	Number of elements = 3380
	Elemental Nodes = 0
	Elemental Rods  = 0
	Elemental Tria3 = 3380
	Elemental Quad4 = 0
Updating mesh element types based on properties input

Getting FEA design variables.......
	Number of design variables          - 4
	Design_Variable name - m0
	Design_Variable name - m1
	Design_Variable name - x0
	Design_Variable name - x1
	Design_Variable_Relation name - rho_madeupium
	Name madeupium not found in attribute map!!!!
	Design_Variable_Relation name - rho_unobtainium
	Name unobtainium not found in attribute map!!!!
	Design_Variable_Relation name - thick_box1
	Number of design variable relations - 3
	Done getting FEA design variables
Updating mesh element types based on properties input

Getting FEA design variables.......
	Number of design variables          - 4
	Design_Variable name - m0
	Design_Variable name - m1
	Design_Variable name - x0
	Design_Variable name - x1
	Design_Variable_Relation name - rho_madeupium
	Name madeupium not found in attribute map!!!!
	Design_Variable_Relation name - rho_unobtainium
	Name unobtainium not found in attribute map!!!!
	Design_Variable_Relation name - thick_box1
	Number of design variable relations - 3
	Done getting FEA design variables
===&gt; x1
Updating mesh element types based on properties input

Getting FEA design variables.......
	Number of design variables          - 4
	Design_Variable name - m0
	Design_Variable name - m1
	Design_Variable name - x0
	Design_Variable name - x1
	Design_Variable_Relation name - rho_madeupium
	Name madeupium not found in attribute map!!!!
	Design_Variable_Relation name - rho_unobtainium
	Name unobtainium not found in attribute map!!!!
	Design_Variable_Relation name - thick_box1
	Number of design variable relations - 3
	Done getting FEA design variables
Updating mesh element types based on properties input

Getting FEA design variables.......
	Number of design variables          - 4
	Design_Variable name - m0
	Design_Variable name - m1
	Design_Variable name - x0
	Design_Variable name - x1
	Design_Variable_Relation name - rho_madeupium
	Name madeupium not found in attribute map!!!!
	Design_Variable_Relation name - rho_unobtainium
	Name unobtainium not found in attribute map!!!!
	Design_Variable_Relation name - thick_box1
	Number of design variable relations - 3
	Done getting FEA design variables
===&gt; m0
Updating mesh element types based on properties input

Getting FEA design variables.......
	Number of design variables          - 4
	Design_Variable name - m0
	Design_Variable name - m1
	Design_Variable name - x0
	Design_Variable name - x1
	Design_Variable_Relation name - rho_madeupium
	Name madeupium not found in attribute map!!!!
	Design_Variable_Relation name - rho_unobtainium
	Name unobtainium not found in attribute map!!!!
	Design_Variable_Relation name - thick_box1
	Number of design variable relations - 3
	Done getting FEA design variables
Updating mesh element types based on properties input

Getting FEA design variables.......
	Number of design variables          - 4
	Design_Variable name - m0
	Design_Variable name - m1
	Design_Variable name - x0
	Design_Variable name - x1
	Design_Variable_Relation name - rho_madeupium
	Name madeupium not found in attribute map!!!!
	Design_Variable_Relation name - rho_unobtainium
	Name unobtainium not found in attribute map!!!!
	Design_Variable_Relation name - thick_box1
	Number of design variable relations - 3
	Done getting FEA design variables
===&gt; m1
Updating mesh element types based on properties input

Getting FEA design variables.......
	Number of design variables          - 4
	Design_Variable name - m0
	Design_Variable name - m1
	Design_Variable name - x0
	Design_Variable name - x1
	Design_Variable_Relation name - rho_madeupium
	Name madeupium not found in attribute map!!!!
	Design_Variable_Relation name - rho_unobtainium
	Name unobtainium not found in attribute map!!!!
	Design_Variable_Relation name - thick_box1
	Number of design variable relations - 3
	Done getting FEA design variables
Updating mesh element types based on properties input

Getting FEA design variables.......
	Number of design variables          - 4
	Design_Variable name - m0
	Design_Variable name - m1
	Design_Variable name - x0
	Design_Variable name - x1
	Design_Variable_Relation name - rho_madeupium
	Name madeupium not found in attribute map!!!!
	Design_Variable_Relation name - rho_unobtainium
	Name unobtainium not found in attribute map!!!!
	Design_Variable_Relation name - thick_box1
	Number of design variable relations - 3
	Done getting FEA design variables
ok
test_box3 (test_masstran.TestMasstran.test_box3) ... Mapping Csys attributes ................
	Number of unique Csys attributes = 0

Getting FEA coordinate systems.......
	Number of coordinate systems - 0
	No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
	Number of unique capsConstraint attributes = 0
Mapping capsLoad attributes ................
	Number of unique capsLoad attributes = 0
Mapping capsBound attributes ................
	Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
	Number of unique capsConnect attributes = 0
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 2
	Name = box1, index = 1
	Name = box2, index = 2
Setting FEA Data
	Mesh for body = 0
	Number of nodal coordinates = 2402
	Number of elements = 2400
	Elemental Nodes = 0
	Elemental Rods  = 0
	Elemental Tria3 = 0
	Elemental Quad4 = 2400

Getting FEA properties.......
	Number of properties - 2
	Property name - box1
	Property name - box2
	Done getting FEA properties
Updating mesh element types based on properties input
Updating mesh element types based on properties input

Getting FEA design variables.......
	Number of design variables          - 7
	Design_Variable name - H
	Design_Variable name - L
	Design_Variable name - W
	Design_Variable name - m0
	Design_Variable name - m1
	Design_Variable name - x0
	Design_Variable name - x1
	Design_Variable_Relation name - rho_madeupium
	Name madeupium not found in attribute map!!!!
	Design_Variable_Relation name - rho_unobtainium
	Name unobtainium not found in attribute map!!!!
	Design_Variable_Relation name - thick_box1
	Design_Variable_Relation name - thick_box2
	Number of design variable relations - 4
	Done getting FEA design variables
===&gt; L
Mapping Csys attributes ................
	Number of unique Csys attributes = 0

Getting FEA coordinate systems.......
	Number of coordinate systems - 0
	No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
	Number of unique capsConstraint attributes = 0
Mapping capsLoad attributes ................
	Number of unique capsLoad attributes = 0
Mapping capsBound attributes ................
	Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
	Number of unique capsConnect attributes = 0
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 2
	Name = box1, index = 1
	Name = box2, index = 2
Setting FEA Data
	Mesh for body = 0
	Number of nodal coordinates = 2402
	Number of elements = 2400
	Elemental Nodes = 0
	Elemental Rods  = 0
	Elemental Tria3 = 0
	Elemental Quad4 = 2400
Updating mesh element types based on properties input
Mapping Csys attributes ................
	Number of unique Csys attributes = 0

Getting FEA coordinate systems.......
	Number of coordinate systems - 0
	No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
	Number of unique capsConstraint attributes = 0
Mapping capsLoad attributes ................
	Number of unique capsLoad attributes = 0
Mapping capsBound attributes ................
	Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
	Number of unique capsConnect attributes = 0
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 2
	Name = box1, index = 1
	Name = box2, index = 2
Setting FEA Data
	Mesh for body = 0
	Number of nodal coordinates = 2402
	Number of elements = 2400
	Elemental Nodes = 0
	Elemental Rods  = 0
	Elemental Tria3 = 0
	Elemental Quad4 = 2400
Updating mesh element types based on properties input
===&gt; W
Mapping Csys attributes ................
	Number of unique Csys attributes = 0

Getting FEA coordinate systems.......
	Number of coordinate systems - 0
	No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
	Number of unique capsConstraint attributes = 0
Mapping capsLoad attributes ................
	Number of unique capsLoad attributes = 0
Mapping capsBound attributes ................
	Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
	Number of unique capsConnect attributes = 0
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 2
	Name = box1, index = 1
	Name = box2, index = 2
Setting FEA Data
	Mesh for body = 0
	Number of nodal coordinates = 2402
	Number of elements = 2400
	Elemental Nodes = 0
	Elemental Rods  = 0
	Elemental Tria3 = 0
	Elemental Quad4 = 2400
Updating mesh element types based on properties input
Mapping Csys attributes ................
	Number of unique Csys attributes = 0

Getting FEA coordinate systems.......
	Number of coordinate systems - 0
	No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
	Number of unique capsConstraint attributes = 0
Mapping capsLoad attributes ................
	Number of unique capsLoad attributes = 0
Mapping capsBound attributes ................
	Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
	Number of unique capsConnect attributes = 0
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 2
	Name = box1, index = 1
	Name = box2, index = 2
Setting FEA Data
	Mesh for body = 0
	Number of nodal coordinates = 2402
	Number of elements = 2400
	Elemental Nodes = 0
	Elemental Rods  = 0
	Elemental Tria3 = 0
	Elemental Quad4 = 2400
Updating mesh element types based on properties input
===&gt; H
Mapping Csys attributes ................
	Number of unique Csys attributes = 0

Getting FEA coordinate systems.......
	Number of coordinate systems - 0
	No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
	Number of unique capsConstraint attributes = 0
Mapping capsLoad attributes ................
	Number of unique capsLoad attributes = 0
Mapping capsBound attributes ................
	Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
	Number of unique capsConnect attributes = 0
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 2
	Name = box1, index = 1
	Name = box2, index = 2
Setting FEA Data
	Mesh for body = 0
	Number of nodal coordinates = 2402
	Number of elements = 2400
	Elemental Nodes = 0
	Elemental Rods  = 0
	Elemental Tria3 = 0
	Elemental Quad4 = 2400
Updating mesh element types based on properties input
Mapping Csys attributes ................
	Number of unique Csys attributes = 0

Getting FEA coordinate systems.......
	Number of coordinate systems - 0
	No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
	Number of unique capsConstraint attributes = 0
Mapping capsLoad attributes ................
	Number of unique capsLoad attributes = 0
Mapping capsBound attributes ................
	Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
	Number of unique capsConnect attributes = 0
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 2
	Name = box1, index = 1
	Name = box2, index = 2
Setting FEA Data
	Mesh for body = 0
	Number of nodal coordinates = 2402
	Number of elements = 2400
	Elemental Nodes = 0
	Elemental Rods  = 0
	Elemental Tria3 = 0
	Elemental Quad4 = 2400
Updating mesh element types based on properties input
===&gt; x0
Mapping Csys attributes ................
	Number of unique Csys attributes = 0

Getting FEA coordinate systems.......
	Number of coordinate systems - 0
	No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
	Number of unique capsConstraint attributes = 0
Mapping capsLoad attributes ................
	Number of unique capsLoad attributes = 0
Mapping capsBound attributes ................
	Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
	Number of unique capsConnect attributes = 0
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 2
	Name = box1, index = 1
	Name = box2, index = 2
Setting FEA Data
	Mesh for body = 0
	Number of nodal coordinates = 2402
	Number of elements = 2400
	Elemental Nodes = 0
	Elemental Rods  = 0
	Elemental Tria3 = 0
	Elemental Quad4 = 2400
Updating mesh element types based on properties input

Getting FEA design variables.......
	Number of design variables          - 4
	Design_Variable name - m0
	Design_Variable name - m1
	Design_Variable name - x0
	Design_Variable name - x1
	Design_Variable_Relation name - rho_madeupium
	Name madeupium not found in attribute map!!!!
	Design_Variable_Relation name - rho_unobtainium
	Name unobtainium not found in attribute map!!!!
	Design_Variable_Relation name - thick_box1
	Design_Variable_Relation name - thick_box2
	Number of design variable relations - 4
	Done getting FEA design variables
Updating mesh element types based on properties input

Getting FEA design variables.......
	Number of design variables          - 4
	Design_Variable name - m0
	Design_Variable name - m1
	Design_Variable name - x0
	Design_Variable name - x1
	Design_Variable_Relation name - rho_madeupium
	Name madeupium not found in attribute map!!!!
	Design_Variable_Relation name - rho_unobtainium
	Name unobtainium not found in attribute map!!!!
	Design_Variable_Relation name - thick_box1
	Design_Variable_Relation name - thick_box2
	Number of design variable relations - 4
	Done getting FEA design variables
===&gt; x1
Updating mesh element types based on properties input

Getting FEA design variables.......
	Number of design variables          - 4
	Design_Variable name - m0
	Design_Variable name - m1
	Design_Variable name - x0
	Design_Variable name - x1
	Design_Variable_Relation name - rho_madeupium
	Name madeupium not found in attribute map!!!!
	Design_Variable_Relation name - rho_unobtainium
	Name unobtainium not found in attribute map!!!!
	Design_Variable_Relation name - thick_box1
	Design_Variable_Relation name - thick_box2
	Number of design variable relations - 4
	Done getting FEA design variables
Updating mesh element types based on properties input

Getting FEA design variables.......
	Number of design variables          - 4
	Design_Variable name - m0
	Design_Variable name - m1
	Design_Variable name - x0
	Design_Variable name - x1
	Design_Variable_Relation name - rho_madeupium
	Name madeupium not found in attribute map!!!!
	Design_Variable_Relation name - rho_unobtainium
	Name unobtainium not found in attribute map!!!!
	Design_Variable_Relation name - thick_box1
	Design_Variable_Relation name - thick_box2
	Number of design variable relations - 4
	Done getting FEA design variables
===&gt; m0
Updating mesh element types based on properties input

Getting FEA design variables.......
	Number of design variables          - 4
	Design_Variable name - m0
	Design_Variable name - m1
	Design_Variable name - x0
	Design_Variable name - x1
	Design_Variable_Relation name - rho_madeupium
	Name madeupium not found in attribute map!!!!
	Design_Variable_Relation name - rho_unobtainium
	Name unobtainium not found in attribute map!!!!
	Design_Variable_Relation name - thick_box1
	Design_Variable_Relation name - thick_box2
	Number of design variable relations - 4
	Done getting FEA design variables
Updating mesh element types based on properties input

Getting FEA design variables.......
	Number of design variables          - 4
	Design_Variable name - m0
	Design_Variable name - m1
	Design_Variable name - x0
	Design_Variable name - x1
	Design_Variable_Relation name - rho_madeupium
	Name madeupium not found in attribute map!!!!
	Design_Variable_Relation name - rho_unobtainium
	Name unobtainium not found in attribute map!!!!
	Design_Variable_Relation name - thick_box1
	Design_Variable_Relation name - thick_box2
	Number of design variable relations - 4
	Done getting FEA design variables
===&gt; m1
Updating mesh element types based on properties input

Getting FEA design variables.......
	Number of design variables          - 4
	Design_Variable name - m0
	Design_Variable name - m1
	Design_Variable name - x0
	Design_Variable name - x1
	Design_Variable_Relation name - rho_madeupium
	Name madeupium not found in attribute map!!!!
	Design_Variable_Relation name - rho_unobtainium
	Name unobtainium not found in attribute map!!!!
	Design_Variable_Relation name - thick_box1
	Design_Variable_Relation name - thick_box2
	Number of design variable relations - 4
	Done getting FEA design variables
Updating mesh element types based on properties input

Getting FEA design variables.......
	Number of design variables          - 4
	Design_Variable name - m0
	Design_Variable name - m1
	Design_Variable name - x0
	Design_Variable name - x1
	Design_Variable_Relation name - rho_madeupium
	Name madeupium not found in attribute map!!!!
	Design_Variable_Relation name - rho_unobtainium
	Name unobtainium not found in attribute map!!!!
	Design_Variable_Relation name - thick_box1
	Design_Variable_Relation name - thick_box2
	Number of design variable relations - 4
	Done getting FEA design variables
ok
test_journal (test_masstran.TestMasstran.test_journal) ... Mapping Csys attributes ................
	Number of unique Csys attributes = 0

Getting FEA coordinate systems.......
	Number of coordinate systems - 0
	No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
	Number of unique capsConstraint attributes = 0
Mapping capsLoad attributes ................
	Number of unique capsLoad attributes = 0
Mapping capsBound attributes ................
	Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
	Number of unique capsConnect attributes = 0
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 2
	Name = box1, index = 1
	Name = point, index = 2
Setting FEA Data
	Mesh for body = 0
	Number of nodal coordinates = 2168
	Number of elements = 4332
	Elemental Nodes = 0
	Elemental Rods  = 0
	Elemental Tria3 = 4332
	Elemental Quad4 = 0
Setting FEA Data
	Mesh for body = 1
	Number of nodal coordinates = 4048
	Number of elements = 8092
	Elemental Nodes = 0
	Elemental Rods  = 0
	Elemental Tria3 = 8092
	Elemental Quad4 = 0
Setting FEA Data
	Mesh for body = 2
	Number of nodal coordinates = 1
	Number of elements = 1
	Elemental Nodes = 1
	Elemental Rods  = 0
	Elemental Tria3 = 0
	Elemental Quad4 = 0
Combining multiple FEA meshes!
	Combined Number of nodal coordinates = 6217
	Combined Number of elements = 12425
	Combined Elemental Nodes = 1
	Combined Elemental Rods  = 0
	Combined Elemental Tria3 = 12424
	Combined Elemental Quad4 = 0

Getting FEA materials.......
	Number of materials - 2
	Material name - madeupium
	Material name - unobtainium
	Done getting FEA materials

Getting FEA properties.......
	Number of properties - 2
	Property name - box1
	Property name - point
	Done getting FEA properties
Updating mesh element types based on properties input
Mapping Csys attributes ................
	Number of unique Csys attributes = 0

Getting FEA coordinate systems.......
	Number of coordinate systems - 0
	No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
	Number of unique capsConstraint attributes = 0
Mapping capsLoad attributes ................
	Number of unique capsLoad attributes = 0
Mapping capsBound attributes ................
	Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
	Number of unique capsConnect attributes = 0
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 2
	Name = box1, index = 1
	Name = point, index = 2
Setting FEA Data
	Mesh for body = 0
	Number of nodal coordinates = 2168
	Number of elements = 4332
	Elemental Nodes = 0
	Elemental Rods  = 0
	Elemental Tria3 = 4332
	Elemental Quad4 = 0
Setting FEA Data
	Mesh for body = 1
	Number of nodal coordinates = 3908
	Number of elements = 7812
	Elemental Nodes = 0
	Elemental Rods  = 0
	Elemental Tria3 = 7812
	Elemental Quad4 = 0
Setting FEA Data
	Mesh for body = 2
	Number of nodal coordinates = 1
	Number of elements = 1
	Elemental Nodes = 1
	Elemental Rods  = 0
	Elemental Tria3 = 0
	Elemental Quad4 = 0
Combining multiple FEA meshes!
	Combined Number of nodal coordinates = 6077
	Combined Number of elements = 12145
	Combined Elemental Nodes = 1
	Combined Elemental Rods  = 0
	Combined Elemental Tria3 = 12144
	Combined Elemental Quad4 = 0
Updating mesh element types based on properties input
 EGADS Info: 0 Objects, 0 Reference in Use (of 0) at Close!
 CAPS Info: Hit last success -- going live!
 CAPS Info: Hit last success -- going live!
 CAPS Info: Hit last success -- going live!
 CAPS Info: Hit last success -- going live!
 CAPS Info: Hit last success -- going live!
 CAPS Info: Hit last success -- going live!
 CAPS Info: Hit last success -- going live!
 CAPS Info: Hit last success -- going live!
 CAPS Info: Hit last success -- going live!
Mapping Csys attributes ................
	Number of unique Csys attributes = 0

Getting FEA coordinate systems.......
	Number of coordinate systems - 0
	No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
	Number of unique capsConstraint attributes = 0
Mapping capsLoad attributes ................
	Number of unique capsLoad attributes = 0
Mapping capsBound attributes ................
	Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
	Number of unique capsConnect attributes = 0
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 2
	Name = box1, index = 1
	Name = point, index = 2
Setting FEA Data
	Mesh for body = 0
	Number of nodal coordinates = 2168
	Number of elements = 4332
	Elemental Nodes = 0
	Elemental Rods  = 0
	Elemental Tria3 = 4332
	Elemental Quad4 = 0
Setting FEA Data
	Mesh for body = 1
	Number of nodal coordinates = 4048
	Number of elements = 8092
	Elemental Nodes = 0
	Elemental Rods  = 0
	Elemental Tria3 = 8092
	Elemental Quad4 = 0
Setting FEA Data
	Mesh for body = 2
	Number of nodal coordinates = 1
	Number of elements = 1
	Elemental Nodes = 1
	Elemental Rods  = 0
	Elemental Tria3 = 0
	Elemental Quad4 = 0
Combining multiple FEA meshes!
	Combined Number of nodal coordinates = 6217
	Combined Number of elements = 12425
	Combined Elemental Nodes = 1
	Combined Elemental Rods  = 0
	Combined Elemental Tria3 = 12424
	Combined Elemental Quad4 = 0

Getting FEA materials.......
	Number of materials - 2
	Material name - madeupium
	Material name - unobtainium
	Done getting FEA materials

Getting FEA properties.......
	Number of properties - 2
	Property name - box1
	Property name - point
	Done getting FEA properties
Updating mesh element types based on properties input
 CAPS Info: Hit last success -- going live!
Mapping Csys attributes ................
	Number of unique Csys attributes = 0

Getting FEA coordinate systems.......
	Number of coordinate systems - 0
	No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
	Number of unique capsConstraint attributes = 0
Mapping capsLoad attributes ................
	Number of unique capsLoad attributes = 0
Mapping capsBound attributes ................
	Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
	Number of unique capsConnect attributes = 0
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 2
	Name = box1, index = 1
	Name = point, index = 2
Setting FEA Data
	Mesh for body = 0
	Number of nodal coordinates = 2168
	Number of elements = 4332
	Elemental Nodes = 0
	Elemental Rods  = 0
	Elemental Tria3 = 4332
	Elemental Quad4 = 0
Setting FEA Data
	Mesh for body = 1
	Number of nodal coordinates = 4048
	Number of elements = 8092
	Elemental Nodes = 0
	Elemental Rods  = 0
	Elemental Tria3 = 8092
	Elemental Quad4 = 0
Setting FEA Data
	Mesh for body = 2
	Number of nodal coordinates = 1
	Number of elements = 1
	Elemental Nodes = 1
	Elemental Rods  = 0
	Elemental Tria3 = 0
	Elemental Quad4 = 0
Combining multiple FEA meshes!
	Combined Number of nodal coordinates = 6217
	Combined Number of elements = 12425
	Combined Elemental Nodes = 1
	Combined Elemental Rods  = 0
	Combined Elemental Tria3 = 12424
	Combined Elemental Quad4 = 0

Getting FEA materials.......
	Number of materials - 2
	Material name - madeupium
	Material name - unobtainium
	Done getting FEA materials

Getting FEA properties.......
	Number of properties - 2
	Property name - box1
	Property name - point
	Done getting FEA properties
Updating mesh element types based on properties input
 CAPS Info: Hit last success -- going live!
 CAPS Info: Hit last success -- going live!
Mapping Csys attributes ................
	Number of unique Csys attributes = 0

Getting FEA coordinate systems.......
	Number of coordinate systems - 0
	No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
	Number of unique capsConstraint attributes = 0
Mapping capsLoad attributes ................
	Number of unique capsLoad attributes = 0
Mapping capsBound attributes ................
	Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
	Number of unique capsConnect attributes = 0
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 2
	Name = box1, index = 1
	Name = point, index = 2
Setting FEA Data
	Mesh for body = 0
	Number of nodal coordinates = 2168
	Number of elements = 4332
	Elemental Nodes = 0
	Elemental Rods  = 0
	Elemental Tria3 = 4332
	Elemental Quad4 = 0
Setting FEA Data
	Mesh for body = 1
	Number of nodal coordinates = 3908
	Number of elements = 7812
	Elemental Nodes = 0
	Elemental Rods  = 0
	Elemental Tria3 = 7812
	Elemental Quad4 = 0
Setting FEA Data
	Mesh for body = 2
	Number of nodal coordinates = 1
	Number of elements = 1
	Elemental Nodes = 1
	Elemental Rods  = 0
	Elemental Tria3 = 0
	Elemental Quad4 = 0
Combining multiple FEA meshes!
	Combined Number of nodal coordinates = 6077
	Combined Number of elements = 12145
	Combined Elemental Nodes = 1
	Combined Elemental Rods  = 0
	Combined Elemental Tria3 = 12144
	Combined Elemental Quad4 = 0

Getting FEA materials.......
	Number of materials - 2
	Material name - madeupium
	Material name - unobtainium
	Done getting FEA materials

Getting FEA properties.......
	Number of properties - 2
	Property name - box1
	Property name - point
	Done getting FEA properties
Updating mesh element types based on properties input
 CAPS Info: Hit last success -- going live!
Mapping Csys attributes ................
	Number of unique Csys attributes = 0

Getting FEA coordinate systems.......
	Number of coordinate systems - 0
	No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
	Number of unique capsConstraint attributes = 0
Mapping capsLoad attributes ................
	Number of unique capsLoad attributes = 0
Mapping capsBound attributes ................
	Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
	Number of unique capsConnect attributes = 0
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 2
	Name = box1, index = 1
	Name = point, index = 2
Setting FEA Data
	Mesh for body = 0
	Number of nodal coordinates = 2168
	Number of elements = 4332
	Elemental Nodes = 0
	Elemental Rods  = 0
	Elemental Tria3 = 4332
	Elemental Quad4 = 0
Setting FEA Data
	Mesh for body = 1
	Number of nodal coordinates = 3908
	Number of elements = 7812
	Elemental Nodes = 0
	Elemental Rods  = 0
	Elemental Tria3 = 7812
	Elemental Quad4 = 0
Setting FEA Data
	Mesh for body = 2
	Number of nodal coordinates = 1
	Number of elements = 1
	Elemental Nodes = 1
	Elemental Rods  = 0
	Elemental Tria3 = 0
	Elemental Quad4 = 0
Combining multiple FEA meshes!
	Combined Number of nodal coordinates = 6077
	Combined Number of elements = 12145
	Combined Elemental Nodes = 1
	Combined Elemental Rods  = 0
	Combined Elemental Tria3 = 12144
	Combined Elemental Quad4 = 0

Getting FEA materials.......
	Number of materials - 2
	Material name - madeupium
	Material name - unobtainium
	Done getting FEA materials

Getting FEA properties.......
	Number of properties - 2
	Property name - box1
	Property name - point
	Done getting FEA properties
Updating mesh element types based on properties input
ok
test_plate (test_masstran.TestMasstran.test_plate) ... Mapping Csys attributes ................
	Number of unique Csys attributes = 0

Getting FEA coordinate systems.......
	Number of coordinate systems - 0
	No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
	Number of unique capsConstraint attributes = 0
Mapping capsLoad attributes ................
	Number of unique capsLoad attributes = 0
Mapping capsBound attributes ................
	Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
	Number of unique capsConnect attributes = 0
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = box1, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
	Mesh for body = 0
	Number of nodal coordinates = 441
	Number of elements = 400
	Elemental Nodes = 0
	Elemental Rods  = 0
	Elemental Tria3 = 0
	Elemental Quad4 = 400

Getting FEA properties.......
	Number of properties - 1
	Property name - box1
	Done getting FEA properties
Updating mesh element types based on properties input
Updating mesh element types based on properties input

Getting FEA design variables.......
	Number of design variables          - 7
	Design_Variable name - H
	Design_Variable name - L
	Design_Variable name - W
	Design_Variable name - m0
	Design_Variable name - m1
	Design_Variable name - x0
	Design_Variable name - x1
	Design_Variable_Relation name - rho_madeupium
	Name madeupium not found in attribute map!!!!
	Design_Variable_Relation name - rho_unobtainium
	Name unobtainium not found in attribute map!!!!
	Design_Variable_Relation name - thick_box1
	Number of design variable relations - 3
	Done getting FEA design variables
===&gt; L
Mapping Csys attributes ................
	Number of unique Csys attributes = 0

Getting FEA coordinate systems.......
	Number of coordinate systems - 0
	No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
	Number of unique capsConstraint attributes = 0
Mapping capsLoad attributes ................
	Number of unique capsLoad attributes = 0
Mapping capsBound attributes ................
	Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
	Number of unique capsConnect attributes = 0
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = box1, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
	Mesh for body = 0
	Number of nodal coordinates = 441
	Number of elements = 400
	Elemental Nodes = 0
	Elemental Rods  = 0
	Elemental Tria3 = 0
	Elemental Quad4 = 400
Updating mesh element types based on properties input
Mapping Csys attributes ................
	Number of unique Csys attributes = 0

Getting FEA coordinate systems.......
	Number of coordinate systems - 0
	No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
	Number of unique capsConstraint attributes = 0
Mapping capsLoad attributes ................
	Number of unique capsLoad attributes = 0
Mapping capsBound attributes ................
	Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
	Number of unique capsConnect attributes = 0
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = box1, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
	Mesh for body = 0
	Number of nodal coordinates = 441
	Number of elements = 400
	Elemental Nodes = 0
	Elemental Rods  = 0
	Elemental Tria3 = 0
	Elemental Quad4 = 400
Updating mesh element types based on properties input
===&gt; W
Mapping Csys attributes ................
	Number of unique Csys attributes = 0

Getting FEA coordinate systems.......
	Number of coordinate systems - 0
	No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
	Number of unique capsConstraint attributes = 0
Mapping capsLoad attributes ................
	Number of unique capsLoad attributes = 0
Mapping capsBound attributes ................
	Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
	Number of unique capsConnect attributes = 0
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = box1, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
	Mesh for body = 0
	Number of nodal coordinates = 441
	Number of elements = 400
	Elemental Nodes = 0
	Elemental Rods  = 0
	Elemental Tria3 = 0
	Elemental Quad4 = 400
Updating mesh element types based on properties input
Mapping Csys attributes ................
	Number of unique Csys attributes = 0

Getting FEA coordinate systems.......
	Number of coordinate systems - 0
	No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
	Number of unique capsConstraint attributes = 0
Mapping capsLoad attributes ................
	Number of unique capsLoad attributes = 0
Mapping capsBound attributes ................
	Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
	Number of unique capsConnect attributes = 0
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = box1, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
	Mesh for body = 0
	Number of nodal coordinates = 441
	Number of elements = 400
	Elemental Nodes = 0
	Elemental Rods  = 0
	Elemental Tria3 = 0
	Elemental Quad4 = 400
Updating mesh element types based on properties input
===&gt; H
Mapping Csys attributes ................
	Number of unique Csys attributes = 0

Getting FEA coordinate systems.......
	Number of coordinate systems - 0
	No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
	Number of unique capsConstraint attributes = 0
Mapping capsLoad attributes ................
	Number of unique capsLoad attributes = 0
Mapping capsBound attributes ................
	Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
	Number of unique capsConnect attributes = 0
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = box1, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
	Mesh for body = 0
	Number of nodal coordinates = 441
	Number of elements = 400
	Elemental Nodes = 0
	Elemental Rods  = 0
	Elemental Tria3 = 0
	Elemental Quad4 = 400
Updating mesh element types based on properties input
Mapping Csys attributes ................
	Number of unique Csys attributes = 0

Getting FEA coordinate systems.......
	Number of coordinate systems - 0
	No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
	Number of unique capsConstraint attributes = 0
Mapping capsLoad attributes ................
	Number of unique capsLoad attributes = 0
Mapping capsBound attributes ................
	Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
	Number of unique capsConnect attributes = 0
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = box1, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
	Mesh for body = 0
	Number of nodal coordinates = 441
	Number of elements = 400
	Elemental Nodes = 0
	Elemental Rods  = 0
	Elemental Tria3 = 0
	Elemental Quad4 = 400
Updating mesh element types based on properties input
===&gt; x0
Mapping Csys attributes ................
	Number of unique Csys attributes = 0

Getting FEA coordinate systems.......
	Number of coordinate systems - 0
	No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
	Number of unique capsConstraint attributes = 0
Mapping capsLoad attributes ................
	Number of unique capsLoad attributes = 0
Mapping capsBound attributes ................
	Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
	Number of unique capsConnect attributes = 0
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = box1, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
	Mesh for body = 0
	Number of nodal coordinates = 441
	Number of elements = 400
	Elemental Nodes = 0
	Elemental Rods  = 0
	Elemental Tria3 = 0
	Elemental Quad4 = 400
Updating mesh element types based on properties input

Getting FEA design variables.......
	Number of design variables          - 4
	Design_Variable name - m0
	Design_Variable name - m1
	Design_Variable name - x0
	Design_Variable name - x1
	Design_Variable_Relation name - rho_madeupium
	Name madeupium not found in attribute map!!!!
	Design_Variable_Relation name - rho_unobtainium
	Name unobtainium not found in attribute map!!!!
	Design_Variable_Relation name - thick_box1
	Number of design variable relations - 3
	Done getting FEA design variables
Updating mesh element types based on properties input

Getting FEA design variables.......
	Number of design variables          - 4
	Design_Variable name - m0
	Design_Variable name - m1
	Design_Variable name - x0
	Design_Variable name - x1
	Design_Variable_Relation name - rho_madeupium
	Name madeupium not found in attribute map!!!!
	Design_Variable_Relation name - rho_unobtainium
	Name unobtainium not found in attribute map!!!!
	Design_Variable_Relation name - thick_box1
	Number of design variable relations - 3
	Done getting FEA design variables
===&gt; x1
Updating mesh element types based on properties input

Getting FEA design variables.......
	Number of design variables          - 4
	Design_Variable name - m0
	Design_Variable name - m1
	Design_Variable name - x0
	Design_Variable name - x1
	Design_Variable_Relation name - rho_madeupium
	Name madeupium not found in attribute map!!!!
	Design_Variable_Relation name - rho_unobtainium
	Name unobtainium not found in attribute map!!!!
	Design_Variable_Relation name - thick_box1
	Number of design variable relations - 3
	Done getting FEA design variables
Updating mesh element types based on properties input

Getting FEA design variables.......
	Number of design variables          - 4
	Design_Variable name - m0
	Design_Variable name - m1
	Design_Variable name - x0
	Design_Variable name - x1
	Design_Variable_Relation name - rho_madeupium
	Name madeupium not found in attribute map!!!!
	Design_Variable_Relation name - rho_unobtainium
	Name unobtainium not found in attribute map!!!!
	Design_Variable_Relation name - thick_box1
	Number of design variable relations - 3
	Done getting FEA design variables
===&gt; m0
Updating mesh element types based on properties input

Getting FEA design variables.......
	Number of design variables          - 4
	Design_Variable name - m0
	Design_Variable name - m1
	Design_Variable name - x0
	Design_Variable name - x1
	Design_Variable_Relation name - rho_madeupium
	Name madeupium not found in attribute map!!!!
	Design_Variable_Relation name - rho_unobtainium
	Name unobtainium not found in attribute map!!!!
	Design_Variable_Relation name - thick_box1
	Number of design variable relations - 3
	Done getting FEA design variables
Updating mesh element types based on properties input

Getting FEA design variables.......
	Number of design variables          - 4
	Design_Variable name - m0
	Design_Variable name - m1
	Design_Variable name - x0
	Design_Variable name - x1
	Design_Variable_Relation name - rho_madeupium
	Name madeupium not found in attribute map!!!!
	Design_Variable_Relation name - rho_unobtainium
	Name unobtainium not found in attribute map!!!!
	Design_Variable_Relation name - thick_box1
	Number of design variable relations - 3
	Done getting FEA design variables
===&gt; m1
Updating mesh element types based on properties input

Getting FEA design variables.......
	Number of design variables          - 4
	Design_Variable name - m0
	Design_Variable name - m1
	Design_Variable name - x0
	Design_Variable name - x1
	Design_Variable_Relation name - rho_madeupium
	Name madeupium not found in attribute map!!!!
	Design_Variable_Relation name - rho_unobtainium
	Name unobtainium not found in attribute map!!!!
	Design_Variable_Relation name - thick_box1
	Number of design variable relations - 3
	Done getting FEA design variables
Updating mesh element types based on properties input

Getting FEA design variables.......
	Number of design variables          - 4
	Design_Variable name - m0
	Design_Variable name - m1
	Design_Variable name - x0
	Design_Variable name - x1
	Design_Variable_Relation name - rho_madeupium
	Name madeupium not found in attribute map!!!!
	Design_Variable_Relation name - rho_unobtainium
	Name unobtainium not found in attribute map!!!!
	Design_Variable_Relation name - thick_box1
	Number of design variable relations - 3
	Done getting FEA design variables
ok
test_plate_point (test_masstran.TestMasstran.test_plate_point) ... Mapping Csys attributes ................
	Number of unique Csys attributes = 0

Getting FEA coordinate systems.......
	Number of coordinate systems - 0
	No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
	Number of unique capsConstraint attributes = 0
Mapping capsLoad attributes ................
	Number of unique capsLoad attributes = 0
Mapping capsBound attributes ................
	Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
	Number of unique capsConnect attributes = 0
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 2
	Name = box1, index = 1
	Name = point, index = 2
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
	Mesh for body = 0
	Number of nodal coordinates = 441
	Number of elements = 400
	Elemental Nodes = 0
	Elemental Rods  = 0
	Elemental Tria3 = 0
	Elemental Quad4 = 400
Setting FEA Data
	Mesh for body = 1
	Number of nodal coordinates = 1
	Number of elements = 1
	Elemental Nodes = 1
	Elemental Rods  = 0
	Elemental Tria3 = 0
	Elemental Quad4 = 0
Combining multiple FEA meshes!
	Combined Number of nodal coordinates = 442
	Combined Number of elements = 401
	Combined Elemental Nodes = 1
	Combined Elemental Rods  = 0
	Combined Elemental Tria3 = 0
	Combined Elemental Quad4 = 400

Getting FEA properties.......
	Number of properties - 2
	Property name - box1
	Property name - point
	Done getting FEA properties
Updating mesh element types based on properties input
Updating mesh element types based on properties input

Getting FEA design variables.......
	Number of design variables          - 7
	Design_Variable name - H
	Design_Variable name - L
	Design_Variable name - W
	Design_Variable name - m0
	Design_Variable name - m1
	Design_Variable name - x0
	Design_Variable name - x1
	Design_Variable_Relation name - mass_point
	Design_Variable_Relation name - rho_madeupium
	Name madeupium not found in attribute map!!!!
	Design_Variable_Relation name - rho_unobtainium
	Name unobtainium not found in attribute map!!!!
	Design_Variable_Relation name - thick_box1
	Number of design variable relations - 4
	Done getting FEA design variables
===&gt; L
Mapping Csys attributes ................
	Number of unique Csys attributes = 0

Getting FEA coordinate systems.......
	Number of coordinate systems - 0
	No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
	Number of unique capsConstraint attributes = 0
Mapping capsLoad attributes ................
	Number of unique capsLoad attributes = 0
Mapping capsBound attributes ................
	Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
	Number of unique capsConnect attributes = 0
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 2
	Name = box1, index = 1
	Name = point, index = 2
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
	Mesh for body = 0
	Number of nodal coordinates = 441
	Number of elements = 400
	Elemental Nodes = 0
	Elemental Rods  = 0
	Elemental Tria3 = 0
	Elemental Quad4 = 400
Setting FEA Data
	Mesh for body = 1
	Number of nodal coordinates = 1
	Number of elements = 1
	Elemental Nodes = 1
	Elemental Rods  = 0
	Elemental Tria3 = 0
	Elemental Quad4 = 0
Combining multiple FEA meshes!
	Combined Number of nodal coordinates = 442
	Combined Number of elements = 401
	Combined Elemental Nodes = 1
	Combined Elemental Rods  = 0
	Combined Elemental Tria3 = 0
	Combined Elemental Quad4 = 400
Updating mesh element types based on properties input
Mapping Csys attributes ................
	Number of unique Csys attributes = 0

Getting FEA coordinate systems.......
	Number of coordinate systems - 0
	No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
	Number of unique capsConstraint attributes = 0
Mapping capsLoad attributes ................
	Number of unique capsLoad attributes = 0
Mapping capsBound attributes ................
	Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
	Number of unique capsConnect attributes = 0
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 2
	Name = box1, index = 1
	Name = point, index = 2
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
	Mesh for body = 0
	Number of nodal coordinates = 441
	Number of elements = 400
	Elemental Nodes = 0
	Elemental Rods  = 0
	Elemental Tria3 = 0
	Elemental Quad4 = 400
Setting FEA Data
	Mesh for body = 1
	Number of nodal coordinates = 1
	Number of elements = 1
	Elemental Nodes = 1
	Elemental Rods  = 0
	Elemental Tria3 = 0
	Elemental Quad4 = 0
Combining multiple FEA meshes!
	Combined Number of nodal coordinates = 442
	Combined Number of elements = 401
	Combined Elemental Nodes = 1
	Combined Elemental Rods  = 0
	Combined Elemental Tria3 = 0
	Combined Elemental Quad4 = 400
Updating mesh element types based on properties input
===&gt; W
Mapping Csys attributes ................
	Number of unique Csys attributes = 0

Getting FEA coordinate systems.......
	Number of coordinate systems - 0
	No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
	Number of unique capsConstraint attributes = 0
Mapping capsLoad attributes ................
	Number of unique capsLoad attributes = 0
Mapping capsBound attributes ................
	Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
	Number of unique capsConnect attributes = 0
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 2
	Name = box1, index = 1
	Name = point, index = 2
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
	Mesh for body = 0
	Number of nodal coordinates = 441
	Number of elements = 400
	Elemental Nodes = 0
	Elemental Rods  = 0
	Elemental Tria3 = 0
	Elemental Quad4 = 400
Setting FEA Data
	Mesh for body = 1
	Number of nodal coordinates = 1
	Number of elements = 1
	Elemental Nodes = 1
	Elemental Rods  = 0
	Elemental Tria3 = 0
	Elemental Quad4 = 0
Combining multiple FEA meshes!
	Combined Number of nodal coordinates = 442
	Combined Number of elements = 401
	Combined Elemental Nodes = 1
	Combined Elemental Rods  = 0
	Combined Elemental Tria3 = 0
	Combined Elemental Quad4 = 400
Updating mesh element types based on properties input
Mapping Csys attributes ................
	Number of unique Csys attributes = 0

Getting FEA coordinate systems.......
	Number of coordinate systems - 0
	No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
	Number of unique capsConstraint attributes = 0
Mapping capsLoad attributes ................
	Number of unique capsLoad attributes = 0
Mapping capsBound attributes ................
	Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
	Number of unique capsConnect attributes = 0
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 2
	Name = box1, index = 1
	Name = point, index = 2
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
	Mesh for body = 0
	Number of nodal coordinates = 441
	Number of elements = 400
	Elemental Nodes = 0
	Elemental Rods  = 0
	Elemental Tria3 = 0
	Elemental Quad4 = 400
Setting FEA Data
	Mesh for body = 1
	Number of nodal coordinates = 1
	Number of elements = 1
	Elemental Nodes = 1
	Elemental Rods  = 0
	Elemental Tria3 = 0
	Elemental Quad4 = 0
Combining multiple FEA meshes!
	Combined Number of nodal coordinates = 442
	Combined Number of elements = 401
	Combined Elemental Nodes = 1
	Combined Elemental Rods  = 0
	Combined Elemental Tria3 = 0
	Combined Elemental Quad4 = 400
Updating mesh element types based on properties input
===&gt; H
Mapping Csys attributes ................
	Number of unique Csys attributes = 0

Getting FEA coordinate systems.......
	Number of coordinate systems - 0
	No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
	Number of unique capsConstraint attributes = 0
Mapping capsLoad attributes ................
	Number of unique capsLoad attributes = 0
Mapping capsBound attributes ................
	Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
	Number of unique capsConnect attributes = 0
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 2
	Name = box1, index = 1
	Name = point, index = 2
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
	Mesh for body = 0
	Number of nodal coordinates = 441
	Number of elements = 400
	Elemental Nodes = 0
	Elemental Rods  = 0
	Elemental Tria3 = 0
	Elemental Quad4 = 400
Setting FEA Data
	Mesh for body = 1
	Number of nodal coordinates = 1
	Number of elements = 1
	Elemental Nodes = 1
	Elemental Rods  = 0
	Elemental Tria3 = 0
	Elemental Quad4 = 0
Combining multiple FEA meshes!
	Combined Number of nodal coordinates = 442
	Combined Number of elements = 401
	Combined Elemental Nodes = 1
	Combined Elemental Rods  = 0
	Combined Elemental Tria3 = 0
	Combined Elemental Quad4 = 400
Updating mesh element types based on properties input
Mapping Csys attributes ................
	Number of unique Csys attributes = 0

Getting FEA coordinate systems.......
	Number of coordinate systems - 0
	No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
	Number of unique capsConstraint attributes = 0
Mapping capsLoad attributes ................
	Number of unique capsLoad attributes = 0
Mapping capsBound attributes ................
	Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
	Number of unique capsConnect attributes = 0
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 2
	Name = box1, index = 1
	Name = point, index = 2
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
	Mesh for body = 0
	Number of nodal coordinates = 441
	Number of elements = 400
	Elemental Nodes = 0
	Elemental Rods  = 0
	Elemental Tria3 = 0
	Elemental Quad4 = 400
Setting FEA Data
	Mesh for body = 1
	Number of nodal coordinates = 1
	Number of elements = 1
	Elemental Nodes = 1
	Elemental Rods  = 0
	Elemental Tria3 = 0
	Elemental Quad4 = 0
Combining multiple FEA meshes!
	Combined Number of nodal coordinates = 442
	Combined Number of elements = 401
	Combined Elemental Nodes = 1
	Combined Elemental Rods  = 0
	Combined Elemental Tria3 = 0
	Combined Elemental Quad4 = 400
Updating mesh element types based on properties input
===&gt; x0
Mapping Csys attributes ................
	Number of unique Csys attributes = 0

Getting FEA coordinate systems.......
	Number of coordinate systems - 0
	No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
	Number of unique capsConstraint attributes = 0
Mapping capsLoad attributes ................
	Number of unique capsLoad attributes = 0
Mapping capsBound attributes ................
	Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
	Number of unique capsConnect attributes = 0
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 2
	Name = box1, index = 1
	Name = point, index = 2
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
	Mesh for body = 0
	Number of nodal coordinates = 441
	Number of elements = 400
	Elemental Nodes = 0
	Elemental Rods  = 0
	Elemental Tria3 = 0
	Elemental Quad4 = 400
Setting FEA Data
	Mesh for body = 1
	Number of nodal coordinates = 1
	Number of elements = 1
	Elemental Nodes = 1
	Elemental Rods  = 0
	Elemental Tria3 = 0
	Elemental Quad4 = 0
Combining multiple FEA meshes!
	Combined Number of nodal coordinates = 442
	Combined Number of elements = 401
	Combined Elemental Nodes = 1
	Combined Elemental Rods  = 0
	Combined Elemental Tria3 = 0
	Combined Elemental Quad4 = 400
Updating mesh element types based on properties input

Getting FEA design variables.......
	Number of design variables          - 4
	Design_Variable name - m0
	Design_Variable name - m1
	Design_Variable name - x0
	Design_Variable name - x1
	Design_Variable_Relation name - mass_point
	Design_Variable_Relation name - rho_madeupium
	Name madeupium not found in attribute map!!!!
	Design_Variable_Relation name - rho_unobtainium
	Name unobtainium not found in attribute map!!!!
	Design_Variable_Relation name - thick_box1
	Number of design variable relations - 4
	Done getting FEA design variables
Updating mesh element types based on properties input

Getting FEA design variables.......
	Number of design variables          - 4
	Design_Variable name - m0
	Design_Variable name - m1
	Design_Variable name - x0
	Design_Variable name - x1
	Design_Variable_Relation name - mass_point
	Design_Variable_Relation name - rho_madeupium
	Name madeupium not found in attribute map!!!!
	Design_Variable_Relation name - rho_unobtainium
	Name unobtainium not found in attribute map!!!!
	Design_Variable_Relation name - thick_box1
	Number of design variable relations - 4
	Done getting FEA design variables
===&gt; x1
Updating mesh element types based on properties input

Getting FEA design variables.......
	Number of design variables          - 4
	Design_Variable name - m0
	Design_Variable name - m1
	Design_Variable name - x0
	Design_Variable name - x1
	Design_Variable_Relation name - mass_point
	Design_Variable_Relation name - rho_madeupium
	Name madeupium not found in attribute map!!!!
	Design_Variable_Relation name - rho_unobtainium
	Name unobtainium not found in attribute map!!!!
	Design_Variable_Relation name - thick_box1
	Number of design variable relations - 4
	Done getting FEA design variables
Updating mesh element types based on properties input

Getting FEA design variables.......
	Number of design variables          - 4
	Design_Variable name - m0
	Design_Variable name - m1
	Design_Variable name - x0
	Design_Variable name - x1
	Design_Variable_Relation name - mass_point
	Design_Variable_Relation name - rho_madeupium
	Name madeupium not found in attribute map!!!!
	Design_Variable_Relation name - rho_unobtainium
	Name unobtainium not found in attribute map!!!!
	Design_Variable_Relation name - thick_box1
	Number of design variable relations - 4
	Done getting FEA design variables
===&gt; m0
Updating mesh element types based on properties input

Getting FEA design variables.......
	Number of design variables          - 4
	Design_Variable name - m0
	Design_Variable name - m1
	Design_Variable name - x0
	Design_Variable name - x1
	Design_Variable_Relation name - mass_point
	Design_Variable_Relation name - rho_madeupium
	Name madeupium not found in attribute map!!!!
	Design_Variable_Relation name - rho_unobtainium
	Name unobtainium not found in attribute map!!!!
	Design_Variable_Relation name - thick_box1
	Number of design variable relations - 4
	Done getting FEA design variables
Updating mesh element types based on properties input

Getting FEA design variables.......
	Number of design variables          - 4
	Design_Variable name - m0
	Design_Variable name - m1
	Design_Variable name - x0
	Design_Variable name - x1
	Design_Variable_Relation name - mass_point
	Design_Variable_Relation name - rho_madeupium
	Name madeupium not found in attribute map!!!!
	Design_Variable_Relation name - rho_unobtainium
	Name unobtainium not found in attribute map!!!!
	Design_Variable_Relation name - thick_box1
	Number of design variable relations - 4
	Done getting FEA design variables
===&gt; m1
Updating mesh element types based on properties input

Getting FEA design variables.......
	Number of design variables          - 4
	Design_Variable name - m0
	Design_Variable name - m1
	Design_Variable name - x0
	Design_Variable name - x1
	Design_Variable_Relation name - mass_point
	Design_Variable_Relation name - rho_madeupium
	Name madeupium not found in attribute map!!!!
	Design_Variable_Relation name - rho_unobtainium
	Name unobtainium not found in attribute map!!!!
	Design_Variable_Relation name - thick_box1
	Number of design variable relations - 4
	Done getting FEA design variables
Updating mesh element types based on properties input

Getting FEA design variables.......
	Number of design variables          - 4
	Design_Variable name - m0
	Design_Variable name - m1
	Design_Variable name - x0
	Design_Variable name - x1
	Design_Variable_Relation name - mass_point
	Design_Variable_Relation name - rho_madeupium
	Name madeupium not found in attribute map!!!!
	Design_Variable_Relation name - rho_unobtainium
	Name unobtainium not found in attribute map!!!!
	Design_Variable_Relation name - thick_box1
	Number of design variable relations - 4
	Done getting FEA design variables
ok
test_Cheby_Modes (test_mses.TestMSES_Kulfan.test_Cheby_Modes) ... 
Getting CFD design variables.......
	Number of design variables - 4
	Design Variable name - alowervar
	Design Variable name - auppervar
	Design Variable name - classvar
	Design Variable name - ztailvar
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
ok
test_Cheby_Modes_Symmetric (test_mses.TestMSES_Kulfan.test_Cheby_Modes_Symmetric) ... 
Getting CFD design variables.......
	Number of design variables - 1
	Design Variable name - avar
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
ok
test_allInputs (test_mses.TestMSES_Kulfan.test_allInputs) ... ok
test_execute (test_mses.TestMSES_Kulfan.test_execute) ... ok
test_sensitivity_AnalysisIn (test_mses.TestMSES_Kulfan.test_sensitivity_AnalysisIn) ... ok
test_Cheby_Modes_Symmetric (test_mses.TestMSES_NACA.test_Cheby_Modes_Symmetric) ... 
Getting CFD design variables.......
	Number of design variables - 1
	Design Variable name - thick
	Done getting CFD design variables
ok
test_geom_sensitivity_CL (test_mses.TestMSES_NACA.test_geom_sensitivity_CL) ... 
Getting CFD design variables.......
	Number of design variables - 2
	Design Variable name - camber
	Design Variable name - thick
	Done getting CFD design variables
ok
test_journal (test_mses.TestMSES_NACA.test_journal) ... 
Getting CFD design variables.......
	Number of design variables - 1
	Design Variable name - thick
	Done getting CFD design variables
 EGADS Info: 0 Objects, 0 Reference in Use (of 0) at Close!
 CAPS Info: Hit last success -- going live!
 CAPS Info: Hit last success -- going live!
 CAPS Info: Hit last success -- going live!
 CAPS Info: Hit last success -- going live!
 CAPS Info: Hit last success -- going live!
 CAPS Info: Hit last success -- going live!

Getting CFD design variables.......
	Number of design variables - 1
	Design Variable name - thick
	Done getting CFD design variables
 CAPS Info: Hit last success -- going live!

Getting CFD design variables.......
	Number of design variables - 1
	Design Variable name - thick
	Done getting CFD design variables
 CAPS Info: Hit last success -- going live!
 CAPS Info: Hit last success -- going live!

Getting CFD design variables.......
	Number of design variables - 1
	Design Variable name - thick
	Done getting CFD design variables
 CAPS Info: Hit last success -- going live!

Getting CFD design variables.......
	Number of design variables - 1
	Design Variable name - thick
	Done getting CFD design variables
ok
test_MultiBody (test_pointwise.TestPointwise.test_MultiBody) ... skipped 'No pointwise executable'
test_SingleBody (test_pointwise.TestPointwise.test_SingleBody) ... skipped 'No pointwise executable'
test_all (test_pointwise.TestPointwise.test_all) ... skipped 'No pointwise executable'
test_box (test_pointwise.TestPointwise.test_box) ... skipped 'No pointwise executable'
test_bullet (test_pointwise.TestPointwise.test_bullet) ... skipped 'No pointwise executable'
test_cone (test_pointwise.TestPointwise.test_cone) ... skipped 'No pointwise executable'
test_cylinder (test_pointwise.TestPointwise.test_cylinder) ... skipped 'No pointwise executable'
test_executeError (test_pointwise.TestPointwise.test_executeError) ... skipped 'No pointwise executable'
test_reenter (test_pointwise.TestPointwise.test_reenter) ... skipped 'No pointwise executable'
test_sphere (test_pointwise.TestPointwise.test_sphere) ... skipped 'No pointwise executable'
 EGADS Info: 0 Objects, 0 Reference in Use (of 0) at Close!
test_Area_Mesh (test_refine.TestREFINE.test_Area_Mesh) ... Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 5
	Name = 2DSlice, index = 1
	Name = TunnelWall, index = 2
	Name = OutFlow, index = 3
	Name = InFlow, index = 4
	Name = Airfoil, index = 5
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 4
	Name = TunnelWall, index = 1
	Name = OutFlow, index = 2
	Name = InFlow, index = 3
	Name = Airfoil, index = 4
Getting 2D mesh for body 1 (of 1)
 
AFLR2    : ---------------------------------------
AFLR2    : AFLR2 LIBRARY
AFLR2    : ADVANCING-FRONT/LOCAL-RECONNECTION
AFLR2    : TRIA/QUAD GRID GENERATOR
AFLR2    : Version Number 9.18.1
AFLR2    : Version Date   06/11/24 @ 05:52PM
AFLR2    : Compile OS     Darwin 23.5.0 arm64
AFLR2    : Compile Date   06/11/24 @ 05:52PM
AFLR2    : Copyright 1994-2021, D.L. Marcum
AFLR2    : ---------------------------------------
 
AFLR2 IC : INPUT DATA CHECK
 
AFLR2 IC : Nodes, Faces      =        54         0
 
AFLR2    : CPU Time          =     0.000   seconds
 
AFLR2 EG : EDGE GRID RE-GENERATION
 
AFLR2 EG : Nodes, Edges      =        54        54
 
AFLR2    : CPU Time          =     0.000   seconds
 
AFLR2 IG : INITIAL GRID GENERATION
 
AFLR2 IG : Nodes, Faces      =         0         2
AFLR2 IG : Nodes, Faces      =        12        26
AFLR2 IG : Nodes, Faces      =        24        50
AFLR2 IG : Nodes, Faces      =        36        74
AFLR2 IG : Nodes, Faces      =        48        98
AFLR2 IG : Nodes, Faces      =        52       106
AFLR2 IG : Nodes, Faces      =        53       108
AFLR2 IG : Nodes, Faces      =        54       110
AFLR2 IG : Nodes, Faces      =        58       110
AFLR2 IG : Nodes, Faces      =        54        54
 
AFLR2    : CPU Time          =     0.000   seconds
 
AFLR2 GG : FIELD GRID GENERATION
 
AFLR2 GG : Nodes, Faces      =        54        54
AFLR2 GG : Nodes, Faces      =       100       146
AFLR2 GG : Nodes, Faces      =       122       190
AFLR2 GG : Nodes, Faces      =       138       222
AFLR2 GG : Nodes, Faces      =       153       252
AFLR2 GG : Nodes, Faces      =       168       282
AFLR2 GG : Nodes, Faces      =       180       306
AFLR2 GG : Nodes, Faces      =       192       330
AFLR2 GG : Nodes, Faces      =       201       348
AFLR2 GG : Nodes, Faces      =       210       366
AFLR2 GG : Nodes, Faces      =       216       378
AFLR2 GG : Nodes, Faces      =       221       388
AFLR2 GG : Nodes, Faces      =       224       394
AFLR2 GG : Nodes, Faces      =       225       396
 
AFLR2    : CPU Time          =     0.000   seconds
 
AFLR2 QI : QUALITY IMPROVEMENT
 
AFLR2 QI : Nodes, Faces      =       225       396
 
AFLR2    : CPU Time          =     0.000   seconds
 
AFLR2    : DONE

Writing AFLR3 file ....
Finished writing AFLR3 file

Number of nodes = 225
Number of elements = 450
Number of tris = 396
Number of quad = 0

Writing Binary VTK file ....
Finished writing Binary VTK file


Writing vtk file ....

Writing vtk general file ....
Finished writing vtk file


Writing FAST file ....
Finished writing FAST file


Writing SU2 file ....
Finished writing SU2 file


Writing Tecplot file ....
Finished writing Tecplot file


Writing ugrid file ....
Finished writing ugrid file


Writing Binary VTK file ....
Finished writing Binary VTK file


Writing vtk file ....

Writing vtk general file ....
Finished writing vtk file


Writing FAST file ....
Finished writing FAST file


Writing SU2 file ....
Finished writing SU2 file


Writing Tecplot file ....
Finished writing Tecplot file


Writing ugrid file ....
Finished writing ugrid file


Writing Binary VTK file ....
Finished writing Binary VTK file


Writing vtk file ....

Writing vtk general file ....
Finished writing vtk file


Writing FAST file ....
Finished writing FAST file


Writing SU2 file ....
Finished writing SU2 file


Writing Tecplot file ....
Finished writing Tecplot file


Writing ugrid file ....
Finished writing ugrid file

ok
test_all (test_refine.TestREFINE.test_all) ... Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 4
	Name = farfield, index = 1
	Name = box, index = 2
	Name = sphere, index = 3
	Name = boxhole, index = 4
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 1
	Name = box, index = 1
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 1
	Name = box, index = 1
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 4
	Name = farfield, index = 1
	Name = box, index = 2
	Name = sphere, index = 3
	Name = boxhole, index = 4
Getting volume mesh
 
AFLR2    : ---------------------------------------
AFLR2    : AFLR2 LIBRARY
AFLR2    : ADVANCING-FRONT/LOCAL-RECONNECTION
AFLR2    : TRIA/QUAD GRID GENERATOR
AFLR2    : Version Number 9.18.1
AFLR2    : Version Date   06/11/24 @ 05:52PM
AFLR2    : Compile OS     Darwin 23.5.0 arm64
AFLR2    : Compile Date   06/11/24 @ 05:52PM
AFLR2    : Copyright 1994-2021, D.L. Marcum
AFLR2    : ---------------------------------------
 
AFLR4    : ---------------------------------------
AFLR4    : AFLR4 LIBRARY
AFLR4    : ADVANCING-FRONT/LOCAL-RECONNECTION
AFLR4    : TRIA/QUAD SURFACE GRID GENERATOR
AFLR4    : Version Number 11.5.15
AFLR4    : Version Date   07/19/24 @ 07:04PM
AFLR4    : Compile OS     Darwin 23.5.0 arm64
AFLR4    : Compile Date   07/19/24 @ 07:06PM
AFLR4    : Copyright 1994-2021, D.L. Marcum
AFLR4    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.8.1
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.8.1
EGADS    : ---------------------------------------
Volume mesh:
	Number of nodes          = 1612
	Number of elements       = 8825
	Number of triangles      = 1216
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 7609
	Number of pyramids       = 0
	Number of prisms         = 0
	Number of hexahedrals    = 0
ok
test_box_volume (test_refine.TestREFINE.test_box_volume) ... Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 2
	Name = farfield, index = 1
	Name = box, index = 2
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 1
	Name = box, index = 1
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 1
	Name = box, index = 1
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 2
	Name = farfield, index = 1
	Name = box, index = 2
Getting volume mesh

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.8.1
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.8.1
EGADS    : ---------------------------------------
Volume mesh:
	Number of nodes          = 2600
	Number of elements       = 13872
	Number of triangles      = 2758
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 11114
	Number of pyramids       = 0
	Number of prisms         = 0
	Number of hexahedrals    = 0
ok
test_boxhole (test_refine.TestREFINE.test_boxhole) ... Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 2
	Name = farfield, index = 1
	Name = boxhole, index = 2
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 0
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 0
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 2
	Name = farfield, index = 1
	Name = boxhole, index = 2
Getting volume mesh

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.8.1
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.8.1
EGADS    : ---------------------------------------
Volume mesh:
	Number of nodes          = 1039
	Number of elements       = 5509
	Number of triangles      = 998
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 4511
	Number of pyramids       = 0
	Number of prisms         = 0
	Number of hexahedrals    = 0
ok
test_cfdSingleBody (test_refine.TestREFINE.test_cfdSingleBody) ... Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 2
	Name = Farfield, index = 1
	Name = Wing1, index = 2
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 4
	Name = Farfield, index = 1
	Name = riteWing, index = 2
	Name = leftWing, index = 3
	Name = trailingEdge, index = 4
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 4
	Name = Farfield, index = 1
	Name = riteWing, index = 2
	Name = leftWing, index = 3
	Name = trailingEdge, index = 4
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 2
	Name = Farfield, index = 1
	Name = Wing1, index = 2
Getting volume mesh

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.8.1
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.8.1
EGADS    : ---------------------------------------
Volume mesh:
	Number of nodes          = 17015
	Number of elements       = 97698
	Number of triangles      = 5384
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 92314
	Number of pyramids       = 0
	Number of prisms         = 0
	Number of hexahedrals    = 0

Writing Binary VTK file ....
Finished writing Binary VTK file


Writing vtk file ....

Writing vtk general file ....
Finished writing vtk file


Writing FAST file ....
Finished writing FAST file


Writing SU2 file ....
Finished writing SU2 file


Writing Tecplot file ....
Finished writing Tecplot file


Writing ugrid file ....
Finished writing ugrid file

Getting CFD boundary conditions
	Boundary condition name - Farfield
	Boundary condition name - Wing1
	Done getting CFD boundary conditions
Writing boundary flags
 - bcProps.surfaceProp[0].surfaceType = 3
 - bcProps.surfaceProp[1].surfaceType = 1
Done boundary flags
Warning: The su2 cfg file will be overwritten!
Write SU2 configuration file for version "Harrier (8.0.1)"

Writing Binary VTK file ....
Finished writing Binary VTK file


Writing vtk file ....

Writing vtk general file ....
Finished writing vtk file


Writing FAST file ....
Finished writing FAST file


Writing SU2 file ....
Finished writing SU2 file


Writing Tecplot file ....
Finished writing Tecplot file


Writing ugrid file ....
Finished writing ugrid file

Getting CFD boundary conditions
	Boundary condition name - Farfield
	Boundary condition name - Wing1
	Done getting CFD boundary conditions
Writing boundary flags
 - bcProps.surfaceProp[0].surfaceType = 3
 - bcProps.surfaceProp[1].surfaceType = 1
Done boundary flags
Warning: The su2 cfg file will be overwritten!
Write SU2 configuration file for version "Harrier (8.0.1)"

Writing Binary VTK file ....
Finished writing Binary VTK file


Writing vtk file ....

Writing vtk general file ....
Finished writing vtk file


Writing FAST file ....
Finished writing FAST file


Writing SU2 file ....
Finished writing SU2 file


Writing Tecplot file ....
Finished writing Tecplot file


Writing ugrid file ....
Finished writing ugrid file

Getting CFD boundary conditions
	Boundary condition name - Farfield
	Boundary condition name - Wing1
	Done getting CFD boundary conditions
Writing boundary flags
 - bcProps.surfaceProp[0].surfaceType = 3
 - bcProps.surfaceProp[1].surfaceType = 1
Done boundary flags
Warning: The su2 cfg file will be overwritten!
Write SU2 configuration file for version "Harrier (8.0.1)"
ok
test_fun3d (test_refine.TestREFINE.test_fun3d) ... Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 4
	Name = farfield, index = 1
	Name = box, index = 2
	Name = sphere, index = 3
	Name = boxhole, index = 4
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 1
	Name = box, index = 1
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 1
	Name = box, index = 1
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 4
	Name = farfield, index = 1
	Name = box, index = 2
	Name = sphere, index = 3
	Name = boxhole, index = 4
Getting volume mesh

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.8.1
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.8.1
EGADS    : ---------------------------------------
Volume mesh:
	Number of nodes          = 1612
	Number of elements       = 8825
	Number of triangles      = 1216
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 7609
	Number of pyramids       = 0
	Number of prisms         = 0
	Number of hexahedrals    = 0
ok
test_inputs (test_refine.TestREFINE.test_inputs) ... ok
test_phase (test_refine.TestREFINE.test_phase) ... Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 2
	Name = farfield, index = 1
	Name = box, index = 2
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 1
	Name = box, index = 1
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 1
	Name = box, index = 1
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 2
	Name = farfield, index = 1
	Name = box, index = 2
Getting volume mesh

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.8.1
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.8.1
EGADS    : ---------------------------------------
Volume mesh:
	Number of nodes          = 432
	Number of elements       = 2132
	Number of triangles      = 644
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 1488
	Number of pyramids       = 0
	Number of prisms         = 0
	Number of hexahedrals    = 0
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 2
	Name = farfield, index = 1
	Name = box, index = 2
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 1
	Name = box, index = 1
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 1
	Name = box, index = 1
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 2
	Name = farfield, index = 1
	Name = box, index = 2
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 2
	Name = farfield, index = 1
	Name = box, index = 2
ok
test_sphere (test_refine.TestREFINE.test_sphere) ... Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 2
	Name = farfield, index = 1
	Name = sphere, index = 2
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 0
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 0
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 2
	Name = farfield, index = 1
	Name = sphere, index = 2
Getting volume mesh

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.8.1
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.8.1
EGADS    : ---------------------------------------
Volume mesh:
	Number of nodes          = 935
	Number of elements       = 5010
	Number of triangles      = 758
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 4252
	Number of pyramids       = 0
	Number of prisms         = 0
	Number of hexahedrals    = 0
ok
test_inputs (test_su2.TestSU2.test_inputs) ... Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 3
	Name = Wing1, index = 1
	Name = Wing2, index = 2
	Name = Farfield, index = 3
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 3
	Name = Wing1, index = 1
	Name = Wing2, index = 2
	Name = Farfield, index = 3
AFLR4    : Proximity BG Surface Grid Generation Skipped
AFLR4    : No Modifications Required
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 3
	Name = Wing1, index = 1
	Name = Wing2, index = 2
	Name = Farfield, index = 3
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 3
	Name = Wing1, index = 1
	Name = Wing2, index = 2
	Name = Farfield, index = 3
Getting volume mesh
 
UG PARAM : SETTING INPUT PARAMETERS FROM ARGUMENT VECTOR
 
UG PARAM : mrecm                       = 3         
UG PARAM : mrecqm                      = 3         
UG PARAM : mpfrmt                      = 0         
 
AFLR2    : ---------------------------------------
AFLR2    : AFLR2 LIBRARY
AFLR2    : ADVANCING-FRONT/LOCAL-RECONNECTION
AFLR2    : TRIA/QUAD GRID GENERATOR
AFLR2    : Version Number 9.18.1
AFLR2    : Version Date   06/11/24 @ 05:52PM
AFLR2    : Compile OS     Darwin 23.5.0 arm64
AFLR2    : Compile Date   06/11/24 @ 05:52PM
AFLR2    : Copyright 1994-2021, D.L. Marcum
AFLR2    : ---------------------------------------
 
AFLR4    : ---------------------------------------
AFLR4    : AFLR4 LIBRARY
AFLR4    : ADVANCING-FRONT/LOCAL-RECONNECTION
AFLR4    : TRIA/QUAD SURFACE GRID GENERATOR
AFLR4    : Version Number 11.5.15
AFLR4    : Version Date   07/19/24 @ 07:04PM
AFLR4    : Compile OS     Darwin 23.5.0 arm64
AFLR4    : Compile Date   07/19/24 @ 07:06PM
AFLR4    : Copyright 1994-2021, D.L. Marcum
AFLR4    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.8.1
EGADS    : ---------------------------------------

EGADS    : EGADS CAD Geometry Setup

EGADS    : Model has 3 Active Bodies

EGADS    : Body 0 is a SolidBody
EGADS    : Body 0 has 1 Shells
EGADS    : Body 0 has 8 Faces
EGADS    : Body 0 has 15 Edges
EGADS    : Body 0 has 8 Loops
EGADS    : Body 0 has 9 Nodes
EGADS    : Body 1 is a SolidBody
EGADS    : Body 1 has 1 Shells
EGADS    : Body 1 has 8 Faces
EGADS    : Body 1 has 15 Edges
EGADS    : Body 1 has 8 Loops
EGADS    : Body 1 has 9 Nodes
EGADS    : Body 2 is a SolidBody
EGADS    : Body 2 has 1 Shells
EGADS    : Body 2 has 2 Faces
EGADS    : Body 2 has 6 Edges
EGADS    : Body 2 has 2 Loops
EGADS    : Body 2 has 2 Nodes

EGADS    : Check Grid BCs

EGADS    : Grid BCs are OK

EGADS    : Face Neighbor-Faces Information

EGADS    : QC  = Face Quad Combination Flag
EGADS    : IER = Face Isolated Edge Refinement Flag
EGADS    : ER  = Face Edge Refinement Factor
EGADS    :       Not applicable for Faces with a FarField Grid BC.
EGADS    : SF  = Face Scale Factor
EGADS    :       Not applicable for Faces with a FarField Grid BC.

EGADS    :   Face          Body    QC   IER       ER    Scale   Neighbor
EGADS    :     ID  Active    ID  Flag  Flag   Weight   Factor   Faces
EGADS    :      1     Yes     0     0     1        1        1   2 3 4 5
EGADS    :      2     Yes     0     0     1        1        1   1 3 4 6
EGADS    :      3     Yes     0     0     1        1        1   1 2 4 7
EGADS    :      4     Yes     0     0     1        1        1   1 2 3
EGADS    :      5     Yes     0     0     1        1        1   1 6 7 8
EGADS    :      6     Yes     0     0     1        1        1   2 5 7 8
EGADS    :      7     Yes     0     0     1        1        1   3 5 6 8
EGADS    :      8     Yes     0     0     1        1        1   5 6 7
EGADS    :      9     Yes     1     0     1        0       10   10 11 12 13
EGADS    :     10     Yes     1     0     1        0       10   9 11 12 14
EGADS    :     11     Yes     1     0     1        0       10   9 10 12 15
EGADS    :     12     Yes     1     0     1        0       10   9 10 11
EGADS    :     13     Yes     1     0     1        0       10   9 14 15 16
EGADS    :     14     Yes     1     0     1        0       10   10 13 15 16
EGADS    :     15     Yes     1     0     1        0       10   11 13 14 16
EGADS    :     16     Yes     1     0     1        0       10   13 14 15
EGADS    :     17     Yes     2     0     1       NA       NA   18
EGADS    :     18     Yes     2     0     1       NA       NA   17

EGADS    : Face Edges Information

EGADS    :   Face   Edges
EGADS    :      1   1 4 -3 -2
EGADS    :      2   3 7 -6 -5
EGADS    :      3   6 9 -1 -8
EGADS    :      4   -4 -9 -7
EGADS    :      5   -10 2 11 -12
EGADS    :      6   -11 5 13 -14
EGADS    :      7   -13 8 10 -15
EGADS    :      8   12 14 15
EGADS    :      9   16 19 -18 -17
EGADS    :     10   18 22 -21 -20
EGADS    :     11   21 24 -16 -23
EGADS    :     12   -19 -24 -22
EGADS    :     13   -25 17 26 -27
EGADS    :     14   -26 20 28 -29
EGADS    :     15   -28 23 25 -30
EGADS    :     16   27 29 30
EGADS    :     17   -31 -32 33 34
EGADS    :     18   -35 -34 36 32

EGADS    : Face Loops Information

EGADS    :   Face   Loops
EGADS    :      1   1
EGADS    :      2   2
EGADS    :      3   3
EGADS    :      4   4
EGADS    :      5   5
EGADS    :      6   6
EGADS    :      7   7
EGADS    :      8   8
EGADS    :      9   9
EGADS    :     10   10
EGADS    :     11   11
EGADS    :     12   12
EGADS    :     13   13
EGADS    :     14   14
EGADS    :     15   15
EGADS    :     16   16
EGADS    :     17   17
EGADS    :     18   18

EGADS    : Loop Edges Information

EGADS    :   Loop  Active   Edges
EGADS    :      1     Yes   1 4 -3 -2
EGADS    :      2     Yes   3 7 -6 -5
EGADS    :      3     Yes   6 9 -1 -8
EGADS    :      4     Yes   -4 -9 -7
EGADS    :      5     Yes   -10 2 11 -12
EGADS    :      6     Yes   -11 5 13 -14
EGADS    :      7     Yes   -13 8 10 -15
EGADS    :      8     Yes   12 14 15
EGADS    :      9     Yes   16 19 -18 -17
EGADS    :     10     Yes   18 22 -21 -20
EGADS    :     11     Yes   21 24 -16 -23
EGADS    :     12     Yes   -19 -24 -22
EGADS    :     13     Yes   -25 17 26 -27
EGADS    :     14     Yes   -26 20 28 -29
EGADS    :     15     Yes   -28 23 25 -30
EGADS    :     16     Yes   27 29 30
EGADS    :     17     Yes   -31 -32 33 34
EGADS    :     18     Yes   -35 -34 36 32

EGADS    : Edge Node, Scale Factor, and Neighbor-Faces Information

EGADS    : ESF = Edge Scale Factor
EGADS    :       Not applicable for DEGENERATE Edges or Edges with a FarField
EGADS    :       Grid BC Neighbor Face.

EGADS    :                                             Neighbor
EGADS    :   Edge  Body  Active Node1 Node2      ESF   Faces
EGADS    :      1     0     Yes     1     2        1   1 3
EGADS    :      2     0     Yes     1     3        1   1 5
EGADS    :      3     0     Yes     3     4        1   1 2
EGADS    :      4     0     Yes     2     4        1   1 4
EGADS    :      5     0     Yes     3     5        1   2 6
EGADS    :      6     0     Yes     5     6        1   2 3
EGADS    :      7     0     Yes     4     6        1   2 4
EGADS    :      8     0     Yes     5     1        1   3 7
EGADS    :      9     0     Yes     6     2        1   3 4
EGADS    :     10     0     Yes     1     7        1   5 7
EGADS    :     11     0     Yes     3     8        1   5 6
EGADS    :     12     0     Yes     7     8        1   5 8
EGADS    :     13     0     Yes     5     9        1   6 7
EGADS    :     14     0     Yes     8     9        1   6 8
EGADS    :     15     0     Yes     9     7        1   7 8
EGADS    :     16     1     Yes    10    11        1   9 11
EGADS    :     17     1     Yes    10    12        1   9 13
EGADS    :     18     1     Yes    12    13        1   9 10
EGADS    :     19     1     Yes    11    13        1   9 12
EGADS    :     20     1     Yes    12    14        1   10 14
EGADS    :     21     1     Yes    14    15        1   10 11
EGADS    :     22     1     Yes    13    15        1   10 12
EGADS    :     23     1     Yes    14    10        1   11 15
EGADS    :     24     1     Yes    15    11        1   11 12
EGADS    :     25     1     Yes    10    16        1   13 15
EGADS    :     26     1     Yes    12    17        1   13 14
EGADS    :     27     1     Yes    16    17        1   13 16
EGADS    :     28     1     Yes    14    18        1   14 15
EGADS    :     29     1     Yes    17    18        1   14 16
EGADS    :     30     1     Yes    18    16        1   15 16
EGADS    :     31     2   DEGEN    19    19        -   17
EGADS    :     32     2     Yes    20    19       NA   17 18
EGADS    :     33     2   DEGEN    20    20        -   17
EGADS    :     34     2     Yes    20    19       NA   17 18
EGADS    :     35     2   DEGEN    19    19        -   18
EGADS    :     36     2   DEGEN    20    20        -   18

EGADS    : Node Information

EGADS    :   Node  Active      Coordinates
EGADS    :      1     Yes       3.77246052                0    0.00459131419
EGADS    :      2     Yes       5.90487498       7.07106781                0
EGADS    :      3     Yes                0                0                0
EGADS    :      4     Yes        4.0824829       7.07106781      0.123425948
EGADS    :      5     Yes       3.77001182                0                0
EGADS    :      6     Yes       5.90282524       7.07106781                0
EGADS    :      7     Yes       5.90487498                0                0
EGADS    :      8     Yes        4.0824829                0      0.123425948
EGADS    :      9     Yes       5.90282524                0                0
EGADS    :     10     Yes       15.2802204                0    0.00183652568
EGADS    :     11     Yes       16.1331862       2.82842712                0
EGADS    :     12     Yes       13.7712362                0                0
EGADS    :     13     Yes       15.4042293       2.82842712     0.0493703791
EGADS    :     14     Yes       15.2792409                0                0
EGADS    :     15     Yes       16.1323663       2.82842712                0
EGADS    :     16     Yes       16.1331862                0                0
EGADS    :     17     Yes       15.4042293                0     0.0493703791
EGADS    :     18     Yes       16.1323663                0                0
EGADS    :     19     Yes                0                0               80
EGADS    :     20     Yes                0                0                0

EGADS    : Face and Edge Match Information

EGADS    : No Face Matches Found

AFLR4    : Surface Mesh Spacing Setup

AFLR4    : Max Bounding Box Length     = 160
AFLR4    : Min Bounding Box Length     = 160
AFLR4    : Max Ref Bounding Box Length = 16.1372
AFLR4    : Min Ref Bounding Box Length = 0.890888
AFLR4    : Reference Length            = 0.890888
AFLR4    : BL Thickness                = 0
AFLR4    : FarField Spacing            = 14.7419
AFLR4    : Abs Min Surf Spacing        = 0.00222722
AFLR4    : Min Surf Spacing            = 0.00445444
AFLR4    : Max Surf Spacing            = 0.0890888
AFLR4    : Global Scale Factor         = 1

AFLR4    : Geometry Definition Information

AFLR4    : Definition              Definition   Composite             Grid BC
AFLR4    :         ID                    Type          ID                Type
AFLR4    :          0     glue-only composite           -                   -
AFLR4    :          1            CAD geometry           0                 STD
AFLR4    :          2            CAD geometry           0                 STD
AFLR4    :          3            CAD geometry           0                 STD
AFLR4    :          4            CAD geometry           0                 STD
AFLR4    :          5            CAD geometry           0                 STD
AFLR4    :          6            CAD geometry           0                 STD
AFLR4    :          7            CAD geometry           0                 STD
AFLR4    :          8            CAD geometry           0                 STD
AFLR4    :          9            CAD geometry           0                 STD
AFLR4    :         10            CAD geometry           0                 STD
AFLR4    :         11            CAD geometry           0                 STD
AFLR4    :         12            CAD geometry           0                 STD
AFLR4    :         13            CAD geometry           0                 STD
AFLR4    :         14            CAD geometry           0                 STD
AFLR4    :         15            CAD geometry           0                 STD
AFLR4    :         16            CAD geometry           0                 STD
AFLR4    :         17            CAD geometry           0            FARFIELD
AFLR4    :         18            CAD geometry           0            FARFIELD

AFLR4    : Case has 2 Proximity Checking Components

AFLR4    : Component 1 includes Definitions 1 2 3 4 5 6 7 8
AFLR4    : Component 2 includes Definitions 9 10 11 12 13 14 15 16

AFLR4    : Define CAD surface definition 1
AFLR4    : Define CAD surface definition 2
AFLR4    : Define CAD surface definition 3
AFLR4    : Define CAD surface definition 4
AFLR4    : Define CAD surface definition 5
AFLR4    : Define CAD surface definition 6
AFLR4    : Define CAD surface definition 7
AFLR4    : Define CAD surface definition 8
AFLR4    : Define CAD surface definition 9
AFLR4    : Define CAD surface definition 10
AFLR4    : Define CAD surface definition 11
AFLR4    : Define CAD surface definition 12
AFLR4    : Define CAD surface definition 13
AFLR4    : Define CAD surface definition 14
AFLR4    : Define CAD surface definition 15
AFLR4    : Define CAD surface definition 16
AFLR4    : Define CAD surface definition 17
AFLR4    : Define CAD surface definition 18
 
AFLR43   : INPUT SURFACE MESH FROM TESS
 
AFLR43   : Quad Surface Faces=         0
AFLR43   : Tria Surface Faces=     11696
AFLR43   : Nodes             =      5854
 
 
UG PARAM : SETTING INPUT PARAMETERS FROM ARGUMENT VECTOR
 
UG PARAM : mrecm                       = 3         
UG PARAM : mrecqm                      = 3         
UG PARAM : mpfrmt                      = 0         
 
AFLR3    : ---------------------------------------
AFLR3    : AFLR3 LIBRARY
AFLR3    : ADVANCING-FRONT/LOCAL-RECONNECTION
AFLR3    : TETRAHEDRAL GRID GENERATOR
AFLR3    : Version Number 16.32.50
AFLR3    : Version Date   10/31/23 @ 06:31PM
AFLR3    : Compile OS     Darwin 23.3.0 arm64
AFLR3    : Compile Date   02/08/24 @ 04:22PM
AFLR3    : Copyright 1994-2021, D.L. Marcum
AFLR3    : ---------------------------------------
 
AFLR3 IC : INPUT SURFACE GRID CHECK
 
AFLR3 IC : Nodes, Elements   =      5854         0

UG3      : Boundary Conditions

UG3      :  B-Face ID            Boundary Condition
UG3      :          1                         Solid
UG3      :          2                         Solid
UG3      :          3                         Solid
UG3      :          4                         Solid
UG3      :          5                         Solid
UG3      :          6                         Solid
UG3      :          7                         Solid
UG3      :          8                         Solid
UG3      :          9                         Solid
UG3      :         10                         Solid
UG3      :         11                         Solid
UG3      :         12                         Solid
UG3      :         13                         Solid
UG3      :         14                         Solid
UG3      :         15                         Solid
UG3      :         16                         Solid
UG3      :         17                      FarField
UG3      :         18                      FarField
 
AFLR3    : CPU Time          =     0.007   seconds
 
AFLR3 IG : INITIAL VOLUME GRID GENERATION
 
AFLR3 IG : Nodes, Elements   =      5854         0
AFLR3 IG : Nodes, Elements   =         8        10
AFLR3 IG : Nodes, Elements   =      1172      6979
AFLR3 IG : Nodes, Elements   =      2344     15131
AFLR3 IG : Nodes, Elements   =      3516     23433
AFLR3 IG : Nodes, Elements   =      4688     31720
AFLR3 IG : Nodes, Elements   =      5860     39973
AFLR3 IG : Nodes, Elements   =      5861     39980
AFLR3 IG : Nodes, Elements   =      5861     39927
AFLR3 IG : Nodes, Elements   =      5861     39954
AFLR3 IG : Nodes, Elements   =      5861     39923
AFLR3 IG : Nodes, Elements   =      5854     23727
AFLR3 IG : Nodes, Elements   =      5854     23747
AFLR3 IG : Nodes, Elements   =      5854     19625
AFLR3 IG : Nodes, Elements   =      5854     17542
 
AFLR3    : CPU Time          =     0.071   seconds
 
AFLR3 GG : ISOTROPIC VOLUME GRID GENERATION
 
AFLR3 GG : Nodes, Elements   =      5854     17542
AFLR3 GG : Nodes, Elements   =      8536     25786
AFLR3 GG : Nodes, Elements   =      8536     37041
AFLR3 GG : Nodes, Elements   =      8536     34267
AFLR3 GG : Nodes, Elements   =      8536     32820
AFLR3 GG : Nodes, Elements   =     10830     40032
AFLR3 GG : Nodes, Elements   =     10830     50075
AFLR3 GG : Nodes, Elements   =     10830     47051
AFLR3 GG : Nodes, Elements   =     10830     46109
AFLR3 GG : Nodes, Elements   =     13376     54035
AFLR3 GG : Nodes, Elements   =     13376     65160
AFLR3 GG : Nodes, Elements   =     13376     61916
AFLR3 GG : Nodes, Elements   =     13376     61125
AFLR3 GG : Nodes, Elements   =     16078     69394
AFLR3 GG : Nodes, Elements   =     16078     81231
AFLR3 GG : Nodes, Elements   =     16078     77895
AFLR3 GG : Nodes, Elements   =     16078     77138
AFLR3 GG : Nodes, Elements   =     18865     85650
AFLR3 GG : Nodes, Elements   =     18865     97785
AFLR3 GG : Nodes, Elements   =     18865     94474
AFLR3 GG : Nodes, Elements   =     18865     93705
AFLR3 GG : Nodes, Elements   =     21890    102926
AFLR3 GG : Nodes, Elements   =     21890    115968
AFLR3 GG : Nodes, Elements   =     21890    112400
AFLR3 GG : Nodes, Elements   =     21890    111643
AFLR3 GG : Nodes, Elements   =     24980    121053
AFLR3 GG : Nodes, Elements   =     24980    134344
AFLR3 GG : Nodes, Elements   =     24980    130769
AFLR3 GG : Nodes, Elements   =     24980    129945
AFLR3 GG : Nodes, Elements   =     28259    139914
AFLR3 GG : Nodes, Elements   =     28259    153879
AFLR3 GG : Nodes, Elements   =     28259    150133
AFLR3 GG : Nodes, Elements   =     28259    149371
AFLR3 GG : Nodes, Elements   =     31552    159346
AFLR3 GG : Nodes, Elements   =     31552    173336
AFLR3 GG : Nodes, Elements   =     31552    169592
AFLR3 GG : Nodes, Elements   =     31552    168861
AFLR3 GG : Nodes, Elements   =     34922    179042
AFLR3 GG : Nodes, Elements   =     34922    193256
AFLR3 GG : Nodes, Elements   =     34922    189489
AFLR3 GG : Nodes, Elements   =     34922    188777
AFLR3 GG : Nodes, Elements   =     38260    198839
AFLR3 GG : Nodes, Elements   =     38260    213010
AFLR3 GG : Nodes, Elements   =     38260    209379
AFLR3 GG : Nodes, Elements   =     38260    208666
AFLR3 GG : Nodes, Elements   =     41613    218777
AFLR3 GG : Nodes, Elements   =     41613    232830
AFLR3 GG : Nodes, Elements   =     41613    229203
AFLR3 GG : Nodes, Elements   =     41613    228546
AFLR3 GG : Nodes, Elements   =     44853    238311
AFLR3 GG : Nodes, Elements   =     44853    251961
AFLR3 GG : Nodes, Elements   =     44853    248462
AFLR3 GG : Nodes, Elements   =     44853    247841
AFLR3 GG : Nodes, Elements   =     47944    257141
AFLR3 GG : Nodes, Elements   =     47944    270223
AFLR3 GG : Nodes, Elements   =     47944    266837
AFLR3 GG : Nodes, Elements   =     47944    266221
AFLR3 GG : Nodes, Elements   =     50866    275001
AFLR3 GG : Nodes, Elements   =     50866    287403
AFLR3 GG : Nodes, Elements   =     50866    284205
AFLR3 GG : Nodes, Elements   =     50866    283637
AFLR3 GG : Nodes, Elements   =     53688    292120
AFLR3 GG : Nodes, Elements   =     53688    303954
AFLR3 GG : Nodes, Elements   =     53688    300960
AFLR3 GG : Nodes, Elements   =     53688    300453
AFLR3 GG : Nodes, Elements   =     56252    308151
AFLR3 GG : Nodes, Elements   =     56252    318979
AFLR3 GG : Nodes, Elements   =     56252    316224
AFLR3 GG : Nodes, Elements   =     56252    315822
AFLR3 GG : Nodes, Elements   =     58659    323046
AFLR3 GG : Nodes, Elements   =     58659    333156
AFLR3 GG : Nodes, Elements   =     58659    330531
AFLR3 GG : Nodes, Elements   =     58659    330168
AFLR3 GG : Nodes, Elements   =     60799    336591
AFLR3 GG : Nodes, Elements   =     60799    345691
AFLR3 GG : Nodes, Elements   =     60799    343322
AFLR3 GG : Nodes, Elements   =     60799    343001
AFLR3 GG : Nodes, Elements   =     62679    348642
AFLR3 GG : Nodes, Elements   =     62679    356496
AFLR3 GG : Nodes, Elements   =     62679    354509
AFLR3 GG : Nodes, Elements   =     62679    354263
AFLR3 GG : Nodes, Elements   =     64243    358957
AFLR3 GG : Nodes, Elements   =     64243    365517
AFLR3 GG : Nodes, Elements   =     64243    363806
AFLR3 GG : Nodes, Elements   =     64243    363612
AFLR3 GG : Nodes, Elements   =     65573    367606
AFLR3 GG : Nodes, Elements   =     65573    373144
AFLR3 GG : Nodes, Elements   =     65573    371736
AFLR3 GG : Nodes, Elements   =     65573    371580
AFLR3 GG : Nodes, Elements   =     66592    374638
AFLR3 GG : Nodes, Elements   =     66592    378925
AFLR3 GG : Nodes, Elements   =     66592    377763
AFLR3 GG : Nodes, Elements   =     66592    377669
AFLR3 GG : Nodes, Elements   =     67321    379857
AFLR3 GG : Nodes, Elements   =     67321    382993
AFLR3 GG : Nodes, Elements   =     67321    382093
AFLR3 GG : Nodes, Elements   =     67321    382021
AFLR3 GG : Nodes, Elements   =     67827    383540
AFLR3 GG : Nodes, Elements   =     67827    385769
AFLR3 GG : Nodes, Elements   =     67827    385075
AFLR3 GG : Nodes, Elements   =     67827    385031
AFLR3 GG : Nodes, Elements   =     68120    385911
AFLR3 GG : Nodes, Elements   =     68120    387126
AFLR3 GG : Nodes, Elements   =     68120    386804
AFLR3 GG : Nodes, Elements   =     68120    386779
AFLR3 GG : Nodes, Elements   =     68302    387326
AFLR3 GG : Nodes, Elements   =     68302    388056
AFLR3 GG : Nodes, Elements   =     68302    387856
AFLR3 GG : Nodes, Elements   =     68302    387848
AFLR3 GG : Nodes, Elements   =     68376    388070
AFLR3 GG : Nodes, Elements   =     68376    388381
AFLR3 GG : Nodes, Elements   =     68376    388292
AFLR3 GG : Nodes, Elements   =     68376    388290
AFLR3 GG : Nodes, Elements   =     68408    388386
AFLR3 GG : Nodes, Elements   =     68408    388517
AFLR3 GG : Nodes, Elements   =     68408    388474
AFLR3 GG : Nodes, Elements   =     68417    388501
AFLR3 GG : Nodes, Elements   =     68417    388543
AFLR3 GG : Nodes, Elements   =     68417    388528
AFLR3 GG : Nodes, Elements   =     68417    388527
AFLR3 GG : Nodes, Elements   =     68422    388542
AFLR3 GG : Nodes, Elements   =     68422    388567
AFLR3 GG : Nodes, Elements   =     68422    388557
AFLR3 GG : Nodes, Elements   =     68422    388558
AFLR3 GG : Nodes, Elements   =     68424    388564
AFLR3 GG : Nodes, Elements   =     68424    388573
AFLR3 GG : Nodes, Elements   =     68424    388569
AFLR3 GG : Nodes, Elements   =     68441    388620
AFLR3 GG : Nodes, Elements   =     68441    388680
AFLR3 GG : Nodes, Elements   =     68441    388660
AFLR3 GG : Nodes, Elements   =     68441    388661
AFLR3 GG : Nodes, Elements   =     68444    388670
AFLR3 GG : Nodes, Elements   =     68444    388682
AFLR3 GG : Nodes, Elements   =     68444    388678
AFLR3 GG : Nodes, Elements   =     68445    388681
AFLR3 GG : Nodes, Elements   =     68445    388683
AFLR3 GG : Nodes, Elements   =     68445    388682
AFLR3 GG : Nodes, Elements   =     68445    388681
 
AFLR3    : CPU Time          =     1.902   seconds
 
AFLR3 QI : QUALITY IMPROVEMENT
 
AFLR3 QI : Nodes, Elements   =     68445    388681
AFLR3 QI : Nodes, Elements   =     67054    380776
AFLR3 QI : Nodes, Elements   =     66819    379453
AFLR3 QI : Nodes, Elements   =     66795    379315
AFLR3 QI : Nodes, Elements   =     66793    379303
AFLR3 QI : Nodes, Elements   =     66793    382971
AFLR3 QI : Nodes, Elements   =     66793    379109
AFLR3 QI : Nodes, Elements   =     66793    378682
AFLR3 QI : Nodes, Elements   =     66793    379082
AFLR3 QI : Nodes, Elements   =     66793    378439
AFLR3 QI : Nodes, Elements   =     66793    378244
AFLR3 QI : Nodes, Elements   =     66793    378540
AFLR3 QI : Nodes, Elements   =     66793    378214
AFLR3 QI : Nodes, Elements   =     66793    378129
AFLR3 QI : Nodes, Elements   =     66793    378403
AFLR3 QI : Nodes, Elements   =     66793    378131
AFLR3 QI : Nodes, Elements   =     66793    378081
AFLR3 QI : Nodes, Elements   =     66793    378344
AFLR3 QI : Nodes, Elements   =     66793    378087
AFLR3 QI : Nodes, Elements   =     66793    378043
AFLR3 QI : Nodes, Elements   =     66796    378056
AFLR3 QI : Nodes, Elements   =     66796    378318
AFLR3 QI : Nodes, Elements   =     66796    378073
AFLR3 QI : Nodes, Elements   =     66796    378055
AFLR3 QI : Nodes, Elements   =     66796    378331
AFLR3 QI : Nodes, Elements   =     66796    378067
AFLR3 QI : Nodes, Elements   =     66796    378027
AFLR3 QI : Nodes, Elements   =     66796    378055
 
AFLR3    : CPU Time          =     0.637   seconds
 
AFLR3 QRG: QUALITY GRID RE-GENERATION
 
AFLR3 QRG: Nodes, Elements   =     66796    378055
AFLR3 QRG: Nodes, Elements   =     66802    378089
AFLR3 QRG: Nodes, Elements   =     66806    378118
AFLR3 QRG: Nodes, Elements   =     66810    378136
AFLR3 QRG: Nodes, Elements   =     66813    378151
AFLR3 QRG: Nodes, Elements   =     66814    378157
 
AFLR3    : CPU Time          =     0.024   seconds
 
AFLR3    : DONE

UG3      : DIHEDRAL ANGLE CHECK

UG3      : No. Tet Elems     =    378157
UG3      : Min, Max Ang      =    0.9306     176.4
UG3      : Average Angle     =      70.2
UG3      : No. Angle&gt;160.0   =       150
UG3      : No. Angle&gt;179.9   =         0

UG3      : VOL CHECK

UG3      : Total-Volume      =  2.12e+06

UG3      : No. Tet Elems     =    378157
UG3      : Min Vol           =  6.65e-10
UG3      : Average Vol       =      5.61
UG3      : Total-Tet-Vol     =  2.12e+06
UG3      : No. Vol&lt;TOL       =         0

UG3      : Q VOL-LENGTH-RATIO CHECK
                      2/3        2
UG3      : Q = c * Vol   / sum( L  )
UG3      : 0 &lt;= Q &lt;= 1

UG3      : No. Tet Elems     =    378157
UG3      : Min, Max Q        =    0.0769         1
UG3      : Average Q         =     0.893
UG3      : No. Q&lt;       0.1  =        29
UG3      : No. Q&lt;      0.01  =         0

OVERALL  : CPU Time          =     2.910   seconds

UG3      : DIHEDRAL ANGLE CHECK

UG3      : No. Tet Elems     =    378157
UG3      : Min, Max Ang      =    0.9306     176.4
UG3      : Average Angle     =      70.2
UG3      : No. Angle&gt;160.0   =       150
UG3      : No. Angle&gt;179.9   =         0

UG3      : VOL CHECK

UG3      : Total-Volume      =  2.12e+06

UG3      : No. Tet Elems     =    378157
UG3      : Min Vol           =  6.65e-10
UG3      : Average Vol       =      5.61
UG3      : Total-Tet-Vol     =  2.12e+06
UG3      : No. Vol&lt;TOL       =         0

UG3      : Q VOL-LENGTH-RATIO CHECK
                      2/3        2
UG3      : Q = c * Vol   / sum( L  )
UG3      : 0 &lt;= Q &lt;= 1
UG3      : Note that L includes scaling for BL-aspect=ratio

UG3      : No. Tet Elems     =    378157
UG3      : Min, Max Q        =     0.107         1
UG3      : Average Q         =     0.874
UG3      : No. Q&lt;       0.1  =         0
UG3      : No. Q&lt;      0.01  =         0

UG3      : CPU Time          =     0.000   seconds

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.8.1
EGADS    : ---------------------------------------

EGADS    : CREATE EGADS TESS FROM AFLR3 DATA

EGADS    : CREATING TESSELLATION FOR BODY 0 EDGE 1
EGADS    : CREATING TESSELLATION FOR BODY 0 EDGE 2
EGADS    : CREATING TESSELLATION FOR BODY 0 EDGE 3
EGADS    : CREATING TESSELLATION FOR BODY 0 EDGE 4
EGADS    : CREATING TESSELLATION FOR BODY 0 EDGE 5
EGADS    : CREATING TESSELLATION FOR BODY 0 EDGE 6
EGADS    : CREATING TESSELLATION FOR BODY 0 EDGE 7
EGADS    : CREATING TESSELLATION FOR BODY 0 EDGE 8
EGADS    : CREATING TESSELLATION FOR BODY 0 EDGE 9
EGADS    : CREATING TESSELLATION FOR BODY 0 EDGE 10
EGADS    : CREATING TESSELLATION FOR BODY 0 EDGE 11
EGADS    : CREATING TESSELLATION FOR BODY 0 EDGE 12
EGADS    : CREATING TESSELLATION FOR BODY 0 EDGE 13
EGADS    : CREATING TESSELLATION FOR BODY 0 EDGE 14
EGADS    : CREATING TESSELLATION FOR BODY 0 EDGE 15

EGADS    : CREATING TESSELLATION FOR BODY 0 FACE 1
EGADS    : CREATING TESSELLATION FOR BODY 0 FACE 2
EGADS    : CREATING TESSELLATION FOR BODY 0 FACE 3
EGADS    : CREATING TESSELLATION FOR BODY 0 FACE 4
EGADS    : CREATING TESSELLATION FOR BODY 0 FACE 5
EGADS    : CREATING TESSELLATION FOR BODY 0 FACE 6
EGADS    : CREATING TESSELLATION FOR BODY 0 FACE 7
EGADS    : CREATING TESSELLATION FOR BODY 0 FACE 8

EGADS    : CREATING TESSELLATION FOR BODY 1 EDGE 16
EGADS    : CREATING TESSELLATION FOR BODY 1 EDGE 17
EGADS    : CREATING TESSELLATION FOR BODY 1 EDGE 18
EGADS    : CREATING TESSELLATION FOR BODY 1 EDGE 19
EGADS    : CREATING TESSELLATION FOR BODY 1 EDGE 20
EGADS    : CREATING TESSELLATION FOR BODY 1 EDGE 21
EGADS    : CREATING TESSELLATION FOR BODY 1 EDGE 22
EGADS    : CREATING TESSELLATION FOR BODY 1 EDGE 23
EGADS    : CREATING TESSELLATION FOR BODY 1 EDGE 24
EGADS    : CREATING TESSELLATION FOR BODY 1 EDGE 25
EGADS    : CREATING TESSELLATION FOR BODY 1 EDGE 26
EGADS    : CREATING TESSELLATION FOR BODY 1 EDGE 27
EGADS    : CREATING TESSELLATION FOR BODY 1 EDGE 28
EGADS    : CREATING TESSELLATION FOR BODY 1 EDGE 29
EGADS    : CREATING TESSELLATION FOR BODY 1 EDGE 30

EGADS    : CREATING TESSELLATION FOR BODY 1 FACE 9
EGADS    : CREATING TESSELLATION FOR BODY 1 FACE 10
EGADS    : CREATING TESSELLATION FOR BODY 1 FACE 11
EGADS    : CREATING TESSELLATION FOR BODY 1 FACE 12
EGADS    : CREATING TESSELLATION FOR BODY 1 FACE 13
EGADS    : CREATING TESSELLATION FOR BODY 1 FACE 14
EGADS    : CREATING TESSELLATION FOR BODY 1 FACE 15
EGADS    : CREATING TESSELLATION FOR BODY 1 FACE 16

EGADS    : CREATING TESSELLATION FOR BODY 2 EDGE 32
EGADS    : CREATING TESSELLATION FOR BODY 2 EDGE 34

EGADS    : CREATING TESSELLATION FOR BODY 2 FACE 17
EGADS    : CREATING TESSELLATION FOR BODY 2 FACE 18

EGADS    : EGADS TESS CREATED

EGADS    : CHECK TESS FACE NODE MAP

EGADS    : CHECKING NODE MAP FOR BODY 0 FACE 1
EGADS    : CHECKING NODE MAP FOR BODY 0 FACE 2
EGADS    : CHECKING NODE MAP FOR BODY 0 FACE 3
EGADS    : CHECKING NODE MAP FOR BODY 0 FACE 4
EGADS    : CHECKING NODE MAP FOR BODY 0 FACE 5
EGADS    : CHECKING NODE MAP FOR BODY 0 FACE 6
EGADS    : CHECKING NODE MAP FOR BODY 0 FACE 7
EGADS    : CHECKING NODE MAP FOR BODY 0 FACE 8
EGADS    : CHECKING NODE MAP FOR BODY 1 FACE 9
EGADS    : CHECKING NODE MAP FOR BODY 1 FACE 10
EGADS    : CHECKING NODE MAP FOR BODY 1 FACE 11
EGADS    : CHECKING NODE MAP FOR BODY 1 FACE 12
EGADS    : CHECKING NODE MAP FOR BODY 1 FACE 13
EGADS    : CHECKING NODE MAP FOR BODY 1 FACE 14
EGADS    : CHECKING NODE MAP FOR BODY 1 FACE 15
EGADS    : CHECKING NODE MAP FOR BODY 1 FACE 16
EGADS    : CHECKING NODE MAP FOR BODY 2 FACE 17
EGADS    : CHECKING NODE MAP FOR BODY 2 FACE 18
Volume mesh:
	Number of nodes          = 66814
	Number of elements       = 389853
	Number of triangles      = 11696
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 378157
	Number of pyramids       = 0
	Number of prisms         = 0
	Number of hexahedrals    = 0

Writing SU2 file ....
Finished writing SU2 file

Getting CFD boundary conditions
	Boundary condition name - Farfield
	Boundary condition name - Wing1
	Boundary condition name - Wing2
	Done getting CFD boundary conditions
Writing boundary flags
 - bcProps.surfaceProp[0].surfaceType = 3
 - bcProps.surfaceProp[1].surfaceType = 1
 - bcProps.surfaceProp[2].surfaceType = 1
Done boundary flags
Warning: The su2 cfg file will be overwritten!
Write SU2 configuration file for version "Cardinal"
Getting CFD boundary conditions
	Boundary condition name - Farfield
	Boundary condition name - Wing1
	Boundary condition name - Wing2
	Done getting CFD boundary conditions
Writing boundary flags
 - bcProps.surfaceProp[0].surfaceType = 3
 - bcProps.surfaceProp[1].surfaceType = 1
 - bcProps.surfaceProp[2].surfaceType = 1
Done boundary flags
Warning: The su2 cfg file will be overwritten!
Write SU2 configuration file for version "Raven"
Getting CFD boundary conditions
	Boundary condition name - Farfield
	Boundary condition name - Wing1
	Boundary condition name - Wing2
	Done getting CFD boundary conditions
Writing boundary flags
 - bcProps.surfaceProp[0].surfaceType = 3
 - bcProps.surfaceProp[1].surfaceType = 1
 - bcProps.surfaceProp[2].surfaceType = 1
Done boundary flags
Warning: The su2 cfg file will be overwritten!
Write SU2 configuration file for version "Falcon"
Getting CFD boundary conditions
	Boundary condition name - Farfield
	Boundary condition name - Wing1
	Boundary condition name - Wing2
	Done getting CFD boundary conditions
Writing boundary flags
 - bcProps.surfaceProp[0].surfaceType = 3
 - bcProps.surfaceProp[1].surfaceType = 1
 - bcProps.surfaceProp[2].surfaceType = 1
Done boundary flags
Warning: The su2 cfg file will be overwritten!
Write SU2 configuration file for version "BlackBird (7.5.1) "
ok
test_invalidBoundary (test_su2.TestSU2.test_invalidBoundary) ... Getting CFD boundary conditions
	Boundary condition name - Wing1
ok
test_invalidBoundaryName (test_su2.TestSU2.test_invalidBoundaryName) ... Getting CFD boundary conditions
	Boundary condition name - Farfield
	Boundary condition name - Wing1
	Boundary condition name - X
ok
test_journal (test_su2.TestSU2.test_journal) ... Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 3
	Name = Wing1, index = 1
	Name = Wing2, index = 2
	Name = Farfield, index = 3
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 3
	Name = Wing1, index = 1
	Name = Wing2, index = 2
	Name = Farfield, index = 3
AFLR4    : Proximity BG Surface Grid Generation Skipped
AFLR4    : No Modifications Required
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 3
	Name = Wing1, index = 1
	Name = Wing2, index = 2
	Name = Farfield, index = 3
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 3
	Name = Wing1, index = 1
	Name = Wing2, index = 2
	Name = Farfield, index = 3
Getting volume mesh

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.8.1
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.8.1
EGADS    : ---------------------------------------
Volume mesh:
	Number of nodes          = 66814
	Number of elements       = 389853
	Number of triangles      = 11696
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 378157
	Number of pyramids       = 0
	Number of prisms         = 0
	Number of hexahedrals    = 0

Writing SU2 file ....
Finished writing SU2 file

Getting CFD boundary conditions
	Boundary condition name - Farfield
	Boundary condition name - Wing1
	Boundary condition name - Wing2
	Done getting CFD boundary conditions
Warning: The su2 cfg file will be overwritten!
Write SU2 configuration file for version "Harrier (8.0.1)"
Running SU2 1
Getting CFD boundary conditions
	Boundary condition name - Farfield
	Boundary condition name - Wing1
	Boundary condition name - Wing2
	Done getting CFD boundary conditions
Writing boundary flags
 - bcProps.surfaceProp[0].surfaceType = 3
 - bcProps.surfaceProp[1].surfaceType = 2
 - bcProps.surfaceProp[2].surfaceType = 1
Done boundary flags
Warning: The su2 cfg file will be overwritten!
Write SU2 configuration file for version "Harrier (8.0.1)"
Running SU2 2
 EGADS Info: 0 Objects, 0 Reference in Use (of 0) at Close!
 CAPS Info: Hit last success -- going live!
 CAPS Info: Hit last success -- going live!
 CAPS Info: Hit last success -- going live!
 CAPS Info: Hit last success -- going live!
 CAPS Info: Hit last success -- going live!
 CAPS Info: Hit last success -- going live!
 CAPS Info: Hit last success -- going live!
 CAPS Info: Hit last success -- going live!
 CAPS Info: Hit last success -- going live!
 CAPS Info: Hit last success -- going live!
 CAPS Info: Hit last success -- going live!
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 3
	Name = Wing1, index = 1
	Name = Wing2, index = 2
	Name = Farfield, index = 3
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 3
	Name = Wing1, index = 1
	Name = Wing2, index = 2
	Name = Farfield, index = 3
AFLR4    : Proximity BG Surface Grid Generation Skipped
AFLR4    : No Modifications Required
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 3
	Name = Wing1, index = 1
	Name = Wing2, index = 2
	Name = Farfield, index = 3
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 3
	Name = Wing1, index = 1
	Name = Wing2, index = 2
	Name = Farfield, index = 3
Getting volume mesh

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.8.1
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.8.1
EGADS    : ---------------------------------------
Volume mesh:
	Number of nodes          = 66814
	Number of elements       = 389853
	Number of triangles      = 11696
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 378157
	Number of pyramids       = 0
	Number of prisms         = 0
	Number of hexahedrals    = 0

Writing SU2 file ....
Finished writing SU2 file

Getting CFD boundary conditions
	Boundary condition name - Farfield
	Boundary condition name - Wing1
	Boundary condition name - Wing2
	Done getting CFD boundary conditions
Warning: The su2 cfg file will be overwritten!
Write SU2 configuration file for version "Harrier (8.0.1)"
 CAPS Info: Hit last success -- going live!
Running SU2 1
 CAPS Info: Hit last success -- going live!
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 3
	Name = Wing1, index = 1
	Name = Wing2, index = 2
	Name = Farfield, index = 3
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 3
	Name = Wing1, index = 1
	Name = Wing2, index = 2
	Name = Farfield, index = 3
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 3
	Name = Wing1, index = 1
	Name = Wing2, index = 2
	Name = Farfield, index = 3
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 3
	Name = Wing1, index = 1
	Name = Wing2, index = 2
	Name = Farfield, index = 3
Getting CFD boundary conditions
	Boundary condition name - Farfield
	Boundary condition name - Wing1
	Boundary condition name - Wing2
	Done getting CFD boundary conditions
 CAPS Info: Hit last success -- going live!
 CAPS Info: Hit last success -- going live!
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 3
	Name = Wing1, index = 1
	Name = Wing2, index = 2
	Name = Farfield, index = 3
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 3
	Name = Wing1, index = 1
	Name = Wing2, index = 2
	Name = Farfield, index = 3
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 3
	Name = Wing1, index = 1
	Name = Wing2, index = 2
	Name = Farfield, index = 3
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 3
	Name = Wing1, index = 1
	Name = Wing2, index = 2
	Name = Farfield, index = 3
Getting CFD boundary conditions
	Boundary condition name - Farfield
	Boundary condition name - Wing1
	Boundary condition name - Wing2
	Done getting CFD boundary conditions
Writing boundary flags
 - bcProps.surfaceProp[0].surfaceType = 3
 - bcProps.surfaceProp[1].surfaceType = 2
 - bcProps.surfaceProp[2].surfaceType = 1
Done boundary flags
Warning: The su2 cfg file will be overwritten!
Write SU2 configuration file for version "Harrier (8.0.1)"
 CAPS Info: Hit last success -- going live!
Running SU2 2
 CAPS Info: Hit last success -- going live!
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 3
	Name = Wing1, index = 1
	Name = Wing2, index = 2
	Name = Farfield, index = 3
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 3
	Name = Wing1, index = 1
	Name = Wing2, index = 2
	Name = Farfield, index = 3
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 3
	Name = Wing1, index = 1
	Name = Wing2, index = 2
	Name = Farfield, index = 3
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 3
	Name = Wing1, index = 1
	Name = Wing2, index = 2
	Name = Farfield, index = 3
Getting CFD boundary conditions
	Boundary condition name - Farfield
	Boundary condition name - Wing1
	Boundary condition name - Wing2
	Done getting CFD boundary conditions
ok
test_phase (test_su2.TestSU2.test_phase) ... Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 3
	Name = Wing1, index = 1
	Name = Wing2, index = 2
	Name = Farfield, index = 3
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 3
	Name = Wing1, index = 1
	Name = Wing2, index = 2
	Name = Farfield, index = 3
AFLR4    : Proximity BG Surface Grid Generation Skipped
AFLR4    : No Modifications Required
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 3
	Name = Wing1, index = 1
	Name = Wing2, index = 2
	Name = Farfield, index = 3
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 3
	Name = Wing1, index = 1
	Name = Wing2, index = 2
	Name = Farfield, index = 3
Getting volume mesh

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.8.1
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.8.1
EGADS    : ---------------------------------------
Volume mesh:
	Number of nodes          = 66814
	Number of elements       = 389853
	Number of triangles      = 11696
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 378157
	Number of pyramids       = 0
	Number of prisms         = 0
	Number of hexahedrals    = 0

Writing SU2 file ....
Finished writing SU2 file

Getting CFD boundary conditions
	Boundary condition name - Farfield
	Boundary condition name - Wing1
	Boundary condition name - Wing2
	Done getting CFD boundary conditions
Warning: The su2 cfg file will be overwritten!
Write SU2 configuration file for version "Harrier (8.0.1)"
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 3
	Name = Wing1, index = 1
	Name = Wing2, index = 2
	Name = Farfield, index = 3
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 3
	Name = Wing1, index = 1
	Name = Wing2, index = 2
	Name = Farfield, index = 3
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 3
	Name = Wing1, index = 1
	Name = Wing2, index = 2
	Name = Farfield, index = 3
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 3
	Name = Wing1, index = 1
	Name = Wing2, index = 2
	Name = Farfield, index = 3
Getting CFD boundary conditions
	Boundary condition name - Farfield
	Boundary condition name - Wing1
	Boundary condition name - Wing2
	Done getting CFD boundary conditions
Writing boundary flags
 - bcProps.surfaceProp[0].surfaceType = 3
 - bcProps.surfaceProp[1].surfaceType = 1
 - bcProps.surfaceProp[2].surfaceType = 1
Done boundary flags
Warning: The su2 cfg file will be overwritten!
Write SU2 configuration file for version "Harrier (8.0.1)"
ok
test_reenter (test_su2.TestSU2.test_reenter) ... Getting CFD boundary conditions
	Boundary condition name - Farfield
	Boundary condition name - Wing1
	Boundary condition name - Wing2
	Done getting CFD boundary conditions
Writing boundary flags
 - bcProps.surfaceProp[0].surfaceType = 3
 - bcProps.surfaceProp[1].surfaceType = 1
 - bcProps.surfaceProp[2].surfaceType = 1
Done boundary flags
Warning: The su2 cfg file will be overwritten!
Write SU2 configuration file for version "BlackBird (7.5.1) "
Getting CFD boundary conditions
	Boundary condition name - Farfield
	Boundary condition name - Wing1
	Boundary condition name - Wing2
	Done getting CFD boundary conditions
Writing boundary flags
 - bcProps.surfaceProp[0].surfaceType = 3
 - bcProps.surfaceProp[1].surfaceType = 2
 - bcProps.surfaceProp[2].surfaceType = 1
Done boundary flags
Warning: The su2 cfg file will be overwritten!
Write SU2 configuration file for version "BlackBird (7.5.1) "
ok
test_units (test_su2.TestSU2.test_units) ... Getting CFD boundary conditions
	Boundary condition name - Farfield
	Boundary condition name - Wing1
	Boundary condition name - Wing2
	Done getting CFD boundary conditions
Warning: The su2 cfg file will be overwritten!
Write SU2 configuration file for version "Harrier (8.0.1)"
ok
test_PlateSensFile (test_tacs.TestTACS.test_PlateSensFile) ... Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = plate, index = 1
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 0
	Face 1 TFI quading disabled with attribute .qParams
Getting surface mesh for body 1 (of 1)
Body 1 (of 1)
Number of nodes    = 25
Number of elements = 16
Number of triangle elements      = 0
Number of quadrilateral elements = 16
----------------------------
Total number of nodes    = 25
Total number of elements = 16
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = plate, index = 1
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 0
	Face 1 TFI quading disabled with attribute .qParams
Getting surface mesh for body 1 (of 1)
Body 1 (of 1)
Number of nodes    = 25
Number of elements = 16
Number of triangle elements      = 0
Number of quadrilateral elements = 16
----------------------------
Total number of nodes    = 25
Total number of elements = 16
Mapping Csys attributes ................
	Number of unique Csys attributes = 0

Getting FEA coordinate systems.......
	Number of coordinate systems - 0
	No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
	Number of unique capsConstraint attributes = 1
	Name = plateEdge, index = 1
Mapping capsLoad attributes ................
	Number of unique capsLoad attributes = 1
	Name = plate, index = 1
Mapping capsBound attributes ................
	Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
	Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
	Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
	Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
	Mesh for body = 0
	Number of nodal coordinates = 25
	Number of elements = 16
	Elemental Nodes = 0
	Elemental Rods  = 0
	Elemental Tria3 = 0
	Elemental Quad4 = 16

Getting FEA materials.......
	Number of materials - 1
	Material name - Madeupium
	Done getting FEA materials

Getting FEA properties.......
	Number of properties - 1
	Property name - plate
	Done getting FEA properties
Updating mesh element types based on properties input

Getting FEA constraints.......
	Number of constraints - 1
	Constraint name - edgeConstraint
	No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement"
	Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults

Getting FEA loads.......
	Number of loads - 1
	Load name - appliedPressure
	Done getting FEA loads

Getting FEA design variables.......
	Number of design variables          - 2
	Design_Variable name - plateLength
	Design_Variable name - thick1
	Design_Variable_Relation name - thick1
	Number of design variable relations - 1
	Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL

Getting FEA analyses.......
	Number of analyses - 1
	Analysis name - Default
	Done getting FEA analyses

Writing Nastran grid and connectivity file (in small field format) ....
Finished writing Nastran grid file

Writing subElement types (if any) - appending mesh file

Writing TACS instruction file....
	Writing analysis cards
	Writing load ADD cards
	Writing constraint ADD cards
	Writing load cards
	Writing constraint cards
	Writing material cards
	Writing property cards
	Writing design variable cards
	Writing design variable relation cards
Mapping Csys attributes ................
	Number of unique Csys attributes = 0

Getting FEA coordinate systems.......
	Number of coordinate systems - 0
	No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
	Number of unique capsConstraint attributes = 1
	Name = plateEdge, index = 1
Mapping capsLoad attributes ................
	Number of unique capsLoad attributes = 1
	Name = plate, index = 1
Mapping capsBound attributes ................
	Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
	Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
	Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
	Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
	Mesh for body = 0
	Number of nodal coordinates = 25
	Number of elements = 16
	Elemental Nodes = 0
	Elemental Rods  = 0
	Elemental Tria3 = 0
	Elemental Quad4 = 16

Getting FEA materials.......
	Number of materials - 1
	Material name - Madeupium
	Done getting FEA materials

Getting FEA properties.......
	Number of properties - 1
	Property name - plate
	Done getting FEA properties
Updating mesh element types based on properties input

Getting FEA constraints.......
	Number of constraints - 1
	Constraint name - edgeConstraint
	No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement"
	Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults

Getting FEA loads.......
	Number of loads - 1
	Load name - appliedPressure
	Done getting FEA loads

Getting FEA design variables.......
	Number of design variables          - 2
	Design_Variable name - plateLength
	Design_Variable name - thick1
	Design_Variable_Relation name - thick1
	Number of design variable relations - 1
	Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL

Getting FEA analyses.......
	Number of analyses - 1
	Analysis name - Default
	Done getting FEA analyses

Writing Nastran grid and connectivity file (in small field format) ....
Finished writing Nastran grid file

Writing subElement types (if any) - appending mesh file

Writing TACS instruction file....
	Writing analysis cards
	Writing load ADD cards
	Writing constraint ADD cards
	Writing load cards
	Writing constraint cards
	Writing material cards
	Writing property cards
	Writing design variable cards
	Writing design variable relation cards
Mapping Csys attributes ................
	Number of unique Csys attributes = 0

Getting FEA coordinate systems.......
	Number of coordinate systems - 0
	No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
	Number of unique capsConstraint attributes = 1
	Name = plateEdge, index = 1
Mapping capsLoad attributes ................
	Number of unique capsLoad attributes = 1
	Name = plate, index = 1
Mapping capsBound attributes ................
	Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
	Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
	Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
	Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
	Mesh for body = 0
	Number of nodal coordinates = 25
	Number of elements = 16
	Elemental Nodes = 0
	Elemental Rods  = 0
	Elemental Tria3 = 0
	Elemental Quad4 = 16

Getting FEA materials.......
	Number of materials - 1
	Material name - Madeupium
	Done getting FEA materials

Getting FEA properties.......
	Number of properties - 1
	Property name - plate
	Done getting FEA properties
Updating mesh element types based on properties input

Getting FEA constraints.......
	Number of constraints - 1
	Constraint name - edgeConstraint
	No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement"
	Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults

Getting FEA loads.......
	Number of loads - 1
	Load name - appliedPressure
	Done getting FEA loads

Getting FEA design variables.......
	Number of design variables          - 2
	Design_Variable name - plateLength
	Design_Variable name - thick1
	Design_Variable_Relation name - thick1
	Number of design variable relations - 1
	Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL

Getting FEA analyses.......
	Number of analyses - 1
	Analysis name - Default
	Done getting FEA analyses

Writing Nastran grid and connectivity file (in small field format) ....
Finished writing Nastran grid file

Writing subElement types (if any) - appending mesh file

Writing TACS instruction file....
	Writing analysis cards
	Writing load ADD cards
	Writing constraint ADD cards
	Writing load cards
	Writing constraint cards
	Writing material cards
	Writing property cards
	Writing design variable cards
	Writing design variable relation cards
Mapping Csys attributes ................
	Number of unique Csys attributes = 0

Getting FEA coordinate systems.......
	Number of coordinate systems - 0
	No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
	Number of unique capsConstraint attributes = 1
	Name = plateEdge, index = 1
Mapping capsLoad attributes ................
	Number of unique capsLoad attributes = 1
	Name = plate, index = 1
Mapping capsBound attributes ................
	Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
	Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
	Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
	Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
	Mesh for body = 0
	Number of nodal coordinates = 25
	Number of elements = 16
	Elemental Nodes = 0
	Elemental Rods  = 0
	Elemental Tria3 = 0
	Elemental Quad4 = 16

Getting FEA materials.......
	Number of materials - 1
	Material name - Madeupium
	Done getting FEA materials

Getting FEA properties.......
	Number of properties - 1
	Property name - plate
	Done getting FEA properties
Updating mesh element types based on properties input

Getting FEA constraints.......
	Number of constraints - 1
	Constraint name - edgeConstraint
	No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement"
	Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults

Getting FEA loads.......
	Number of loads - 1
	Load name - appliedPressure
	Done getting FEA loads

Getting FEA design variables.......
	Number of design variables          - 2
	Design_Variable name - plateLength
	Design_Variable name - thick1
	Design_Variable_Relation name - thick1
	Number of design variable relations - 1
	Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL

Getting FEA analyses.......
	Number of analyses - 1
	Analysis name - Default
	Done getting FEA analyses

Writing Nastran grid and connectivity file (in small field format) ....
Finished writing Nastran grid file

Writing subElement types (if any) - appending mesh file

Writing TACS instruction file....
	Writing analysis cards
	Writing load ADD cards
	Writing constraint ADD cards
	Writing load cards
	Writing constraint cards
	Writing material cards
	Writing property cards
	Writing design variable cards
	Writing design variable relation cards
Mapping Csys attributes ................
	Number of unique Csys attributes = 0

Getting FEA coordinate systems.......
	Number of coordinate systems - 0
	No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
	Number of unique capsConstraint attributes = 1
	Name = plateEdge, index = 1
Mapping capsLoad attributes ................
	Number of unique capsLoad attributes = 1
	Name = plate, index = 1
Mapping capsBound attributes ................
	Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
	Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
	Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
	Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
	Mesh for body = 0
	Number of nodal coordinates = 25
	Number of elements = 16
	Elemental Nodes = 0
	Elemental Rods  = 0
	Elemental Tria3 = 0
	Elemental Quad4 = 16

Getting FEA materials.......
	Number of materials - 1
	Material name - Madeupium
	Done getting FEA materials

Getting FEA properties.......
	Number of properties - 1
	Property name - plate
	Done getting FEA properties
Updating mesh element types based on properties input

Getting FEA constraints.......
	Number of constraints - 1
	Constraint name - edgeConstraint
	No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement"
	Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults

Getting FEA loads.......
	Number of loads - 1
	Load name - appliedPressure
	Done getting FEA loads

Getting FEA design variables.......
	Number of design variables          - 2
	Design_Variable name - plateLength
	Design_Variable name - thick1
	Design_Variable_Relation name - thick1
	Number of design variable relations - 1
	Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL

Getting FEA analyses.......
	Number of analyses - 1
	Analysis name - Default
	Done getting FEA analyses

Writing Nastran grid and connectivity file (in small field format) ....
Finished writing Nastran grid file

Writing subElement types (if any) - appending mesh file

Writing TACS instruction file....
	Writing analysis cards
	Writing load ADD cards
	Writing constraint ADD cards
	Writing load cards
	Writing constraint cards
	Writing material cards
	Writing property cards
	Writing design variable cards
	Writing design variable relation cards
Mapping Csys attributes ................
	Number of unique Csys attributes = 0

Getting FEA coordinate systems.......
	Number of coordinate systems - 0
	No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
	Number of unique capsConstraint attributes = 1
	Name = plateEdge, index = 1
Mapping capsLoad attributes ................
	Number of unique capsLoad attributes = 1
	Name = plate, index = 1
Mapping capsBound attributes ................
	Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
	Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
	Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
	Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
	Mesh for body = 0
	Number of nodal coordinates = 25
	Number of elements = 16
	Elemental Nodes = 0
	Elemental Rods  = 0
	Elemental Tria3 = 0
	Elemental Quad4 = 16

Getting FEA materials.......
	Number of materials - 1
	Material name - Madeupium
	Done getting FEA materials

Getting FEA properties.......
	Number of properties - 1
	Property name - plate
	Done getting FEA properties
Updating mesh element types based on properties input

Getting FEA constraints.......
	Number of constraints - 1
	Constraint name - edgeConstraint
	No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement"
	Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults

Getting FEA loads.......
	Number of loads - 1
	Load name - appliedPressure
	Done getting FEA loads

Getting FEA design variables.......
	Number of design variables          - 2
	Design_Variable name - plateLength
	Design_Variable name - thick1
	Design_Variable_Relation name - thick1
	Number of design variable relations - 1
	Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL

Getting FEA analyses.......
	Number of analyses - 1
	Analysis name - Default
	Done getting FEA analyses

Writing Nastran grid and connectivity file (in small field format) ....
Finished writing Nastran grid file

Writing subElement types (if any) - appending mesh file

Writing TACS instruction file....
	Writing analysis cards
	Writing load ADD cards
	Writing constraint ADD cards
	Writing load cards
	Writing constraint cards
	Writing material cards
	Writing property cards
	Writing design variable cards
	Writing design variable relation cards
Mapping Csys attributes ................
	Number of unique Csys attributes = 0

Getting FEA coordinate systems.......
	Number of coordinate systems - 0
	No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
	Number of unique capsConstraint attributes = 1
	Name = plateEdge, index = 1
Mapping capsLoad attributes ................
	Number of unique capsLoad attributes = 1
	Name = plate, index = 1
Mapping capsBound attributes ................
	Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
	Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
	Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
	Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
	Mesh for body = 0
	Number of nodal coordinates = 25
	Number of elements = 16
	Elemental Nodes = 0
	Elemental Rods  = 0
	Elemental Tria3 = 0
	Elemental Quad4 = 16

Getting FEA materials.......
	Number of materials - 1
	Material name - Madeupium
	Done getting FEA materials

Getting FEA properties.......
	Number of properties - 1
	Property name - plate
	Done getting FEA properties
Updating mesh element types based on properties input

Getting FEA constraints.......
	Number of constraints - 1
	Constraint name - edgeConstraint
	No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement"
	Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults

Getting FEA loads.......
	Number of loads - 1
	Load name - appliedPressure
	Done getting FEA loads

Getting FEA design variables.......
	Number of design variables          - 2
	Design_Variable name - plateLength
	Design_Variable name - thick1
	Design_Variable_Relation name - thick1
	Number of design variable relations - 1
	Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL

Getting FEA analyses.......
	Number of analyses - 1
	Analysis name - Default
	Done getting FEA analyses

Writing Nastran grid and connectivity file (in small field format) ....
Finished writing Nastran grid file

Writing subElement types (if any) - appending mesh file

Writing TACS instruction file....
	Writing analysis cards
	Writing load ADD cards
	Writing constraint ADD cards
	Writing load cards
	Writing constraint cards
	Writing material cards
	Writing property cards
	Writing design variable cards
	Writing design variable relation cards
Mapping Csys attributes ................
	Number of unique Csys attributes = 0

Getting FEA coordinate systems.......
	Number of coordinate systems - 0
	No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
	Number of unique capsConstraint attributes = 1
	Name = plateEdge, index = 1
Mapping capsLoad attributes ................
	Number of unique capsLoad attributes = 1
	Name = plate, index = 1
Mapping capsBound attributes ................
	Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
	Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
	Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
	Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
	Mesh for body = 0
	Number of nodal coordinates = 25
	Number of elements = 16
	Elemental Nodes = 0
	Elemental Rods  = 0
	Elemental Tria3 = 0
	Elemental Quad4 = 16

Getting FEA materials.......
	Number of materials - 1
	Material name - Madeupium
	Done getting FEA materials

Getting FEA properties.......
	Number of properties - 1
	Property name - plate
	Done getting FEA properties
Updating mesh element types based on properties input

Getting FEA constraints.......
	Number of constraints - 1
	Constraint name - edgeConstraint
	No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement"
	Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults

Getting FEA loads.......
	Number of loads - 1
	Load name - appliedPressure
	Done getting FEA loads

Getting FEA design variables.......
	Number of design variables          - 2
	Design_Variable name - plateLength
	Design_Variable name - thick1
	Design_Variable_Relation name - thick1
	Number of design variable relations - 1
	Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL

Getting FEA analyses.......
	Number of analyses - 1
	Analysis name - Default
	Done getting FEA analyses

Writing Nastran grid and connectivity file (in small field format) ....
Finished writing Nastran grid file

Writing subElement types (if any) - appending mesh file

Writing TACS instruction file....
	Writing analysis cards
	Writing load ADD cards
	Writing constraint ADD cards
	Writing load cards
	Writing constraint cards
	Writing material cards
	Writing property cards
	Writing design variable cards
	Writing design variable relation cards
Mapping Csys attributes ................
	Number of unique Csys attributes = 0

Getting FEA coordinate systems.......
	Number of coordinate systems - 0
	No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
	Number of unique capsConstraint attributes = 1
	Name = plateEdge, index = 1
Mapping capsLoad attributes ................
	Number of unique capsLoad attributes = 1
	Name = plate, index = 1
Mapping capsBound attributes ................
	Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
	Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
	Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
	Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
	Mesh for body = 0
	Number of nodal coordinates = 25
	Number of elements = 16
	Elemental Nodes = 0
	Elemental Rods  = 0
	Elemental Tria3 = 0
	Elemental Quad4 = 16

Getting FEA materials.......
	Number of materials - 1
	Material name - Madeupium
	Done getting FEA materials

Getting FEA properties.......
	Number of properties - 1
	Property name - plate
	Done getting FEA properties
Updating mesh element types based on properties input

Getting FEA constraints.......
	Number of constraints - 1
	Constraint name - edgeConstraint
	No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement"
	Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults

Getting FEA loads.......
	Number of loads - 1
	Load name - appliedPressure
	Done getting FEA loads

Getting FEA design variables.......
	Number of design variables          - 2
	Design_Variable name - plateLength
	Design_Variable name - thick1
	Design_Variable_Relation name - thick1
	Number of design variable relations - 1
	Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL

Getting FEA analyses.......
	Number of analyses - 1
	Analysis name - Default
	Done getting FEA analyses

Writing Nastran grid and connectivity file (in small field format) ....
Finished writing Nastran grid file

Writing subElement types (if any) - appending mesh file

Writing TACS instruction file....
	Writing analysis cards
	Writing load ADD cards
	Writing constraint ADD cards
	Writing load cards
	Writing constraint cards
	Writing material cards
	Writing property cards
	Writing design variable cards
	Writing design variable relation cards
Mapping Csys attributes ................
	Number of unique Csys attributes = 0

Getting FEA coordinate systems.......
	Number of coordinate systems - 0
	No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
	Number of unique capsConstraint attributes = 1
	Name = plateEdge, index = 1
Mapping capsLoad attributes ................
	Number of unique capsLoad attributes = 1
	Name = plate, index = 1
Mapping capsBound attributes ................
	Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
	Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
	Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
	Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
	Mesh for body = 0
	Number of nodal coordinates = 25
	Number of elements = 16
	Elemental Nodes = 0
	Elemental Rods  = 0
	Elemental Tria3 = 0
	Elemental Quad4 = 16

Getting FEA materials.......
	Number of materials - 1
	Material name - Madeupium
	Done getting FEA materials

Getting FEA properties.......
	Number of properties - 1
	Property name - plate
	Done getting FEA properties
Updating mesh element types based on properties input

Getting FEA constraints.......
	Number of constraints - 1
	Constraint name - edgeConstraint
	No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement"
	Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults

Getting FEA loads.......
	Number of loads - 1
	Load name - appliedPressure
	Done getting FEA loads

Getting FEA design variables.......
	Number of design variables          - 2
	Design_Variable name - plateLength
	Design_Variable name - thick1
	Design_Variable_Relation name - thick1
	Number of design variable relations - 1
	Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL

Getting FEA analyses.......
	Number of analyses - 1
	Analysis name - Default
	Done getting FEA analyses

Writing Nastran grid and connectivity file (in small field format) ....
Finished writing Nastran grid file

Writing subElement types (if any) - appending mesh file

Writing TACS instruction file....
	Writing analysis cards
	Writing load ADD cards
	Writing constraint ADD cards
	Writing load cards
	Writing constraint cards
	Writing material cards
	Writing property cards
	Writing design variable cards
	Writing design variable relation cards
Mapping Csys attributes ................
	Number of unique Csys attributes = 0

Getting FEA coordinate systems.......
	Number of coordinate systems - 0
	No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
	Number of unique capsConstraint attributes = 1
	Name = plateEdge, index = 1
Mapping capsLoad attributes ................
	Number of unique capsLoad attributes = 1
	Name = plate, index = 1
Mapping capsBound attributes ................
	Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
	Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
	Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
	Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
	Mesh for body = 0
	Number of nodal coordinates = 25
	Number of elements = 16
	Elemental Nodes = 0
	Elemental Rods  = 0
	Elemental Tria3 = 0
	Elemental Quad4 = 16

Getting FEA materials.......
	Number of materials - 1
	Material name - Madeupium
	Done getting FEA materials

Getting FEA properties.......
	Number of properties - 1
	Property name - plate
	Done getting FEA properties
Updating mesh element types based on properties input

Getting FEA constraints.......
	Number of constraints - 1
	Constraint name - edgeConstraint
	No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement"
	Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults

Getting FEA loads.......
	Number of loads - 1
	Load name - appliedPressure
	Done getting FEA loads

Getting FEA design variables.......
	Number of design variables          - 2
	Design_Variable name - plateLength
	Design_Variable name - thick1
	Design_Variable_Relation name - thick1
	Number of design variable relations - 1
	Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL

Getting FEA analyses.......
	Number of analyses - 1
	Analysis name - Default
	Done getting FEA analyses

Writing Nastran grid and connectivity file (in small field format) ....
Finished writing Nastran grid file

Writing subElement types (if any) - appending mesh file

Writing TACS instruction file....
	Writing analysis cards
	Writing load ADD cards
	Writing constraint ADD cards
	Writing load cards
	Writing constraint cards
	Writing material cards
	Writing property cards
	Writing design variable cards
	Writing design variable relation cards
Mapping Csys attributes ................
	Number of unique Csys attributes = 0

Getting FEA coordinate systems.......
	Number of coordinate systems - 0
	No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
	Number of unique capsConstraint attributes = 1
	Name = plateEdge, index = 1
Mapping capsLoad attributes ................
	Number of unique capsLoad attributes = 1
	Name = plate, index = 1
Mapping capsBound attributes ................
	Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
	Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
	Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
	Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
	Mesh for body = 0
	Number of nodal coordinates = 25
	Number of elements = 16
	Elemental Nodes = 0
	Elemental Rods  = 0
	Elemental Tria3 = 0
	Elemental Quad4 = 16

Getting FEA materials.......
	Number of materials - 1
	Material name - Madeupium
	Done getting FEA materials

Getting FEA properties.......
	Number of properties - 1
	Property name - plate
	Done getting FEA properties
Updating mesh element types based on properties input

Getting FEA constraints.......
	Number of constraints - 1
	Constraint name - edgeConstraint
	No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement"
	Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults

Getting FEA loads.......
	Number of loads - 1
	Load name - appliedPressure
	Done getting FEA loads

Getting FEA design variables.......
	Number of design variables          - 2
	Design_Variable name - plateLength
	Design_Variable name - thick1
	Design_Variable_Relation name - thick1
	Number of design variable relations - 1
	Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL

Getting FEA analyses.......
	Number of analyses - 1
	Analysis name - Default
	Done getting FEA analyses

Writing Nastran grid and connectivity file (in small field format) ....
Finished writing Nastran grid file

Writing subElement types (if any) - appending mesh file

Writing TACS instruction file....
	Writing analysis cards
	Writing load ADD cards
	Writing constraint ADD cards
	Writing load cards
	Writing constraint cards
	Writing material cards
	Writing property cards
	Writing design variable cards
	Writing design variable relation cards
Mapping Csys attributes ................
	Number of unique Csys attributes = 0

Getting FEA coordinate systems.......
	Number of coordinate systems - 0
	No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
	Number of unique capsConstraint attributes = 1
	Name = plateEdge, index = 1
Mapping capsLoad attributes ................
	Number of unique capsLoad attributes = 1
	Name = plate, index = 1
Mapping capsBound attributes ................
	Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
	Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
	Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
	Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
	Mesh for body = 0
	Number of nodal coordinates = 25
	Number of elements = 16
	Elemental Nodes = 0
	Elemental Rods  = 0
	Elemental Tria3 = 0
	Elemental Quad4 = 16

Getting FEA materials.......
	Number of materials - 1
	Material name - Madeupium
	Done getting FEA materials

Getting FEA properties.......
	Number of properties - 1
	Property name - plate
	Done getting FEA properties
Updating mesh element types based on properties input

Getting FEA constraints.......
	Number of constraints - 1
	Constraint name - edgeConstraint
	No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement"
	Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults

Getting FEA loads.......
	Number of loads - 1
	Load name - appliedPressure
	Done getting FEA loads

Getting FEA design variables.......
	Number of design variables          - 2
	Design_Variable name - plateLength
	Design_Variable name - thick1
	Design_Variable_Relation name - thick1
	Number of design variable relations - 1
	Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL

Getting FEA analyses.......
	Number of analyses - 1
	Analysis name - Default
	Done getting FEA analyses

Writing Nastran grid and connectivity file (in small field format) ....
Finished writing Nastran grid file

Writing subElement types (if any) - appending mesh file

Writing TACS instruction file....
	Writing analysis cards
	Writing load ADD cards
	Writing constraint ADD cards
	Writing load cards
	Writing constraint cards
	Writing material cards
	Writing property cards
	Writing design variable cards
	Writing design variable relation cards
Mapping Csys attributes ................
	Number of unique Csys attributes = 0

Getting FEA coordinate systems.......
	Number of coordinate systems - 0
	No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
	Number of unique capsConstraint attributes = 1
	Name = plateEdge, index = 1
Mapping capsLoad attributes ................
	Number of unique capsLoad attributes = 1
	Name = plate, index = 1
Mapping capsBound attributes ................
	Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
	Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
	Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
	Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
	Mesh for body = 0
	Number of nodal coordinates = 25
	Number of elements = 16
	Elemental Nodes = 0
	Elemental Rods  = 0
	Elemental Tria3 = 0
	Elemental Quad4 = 16

Getting FEA materials.......
	Number of materials - 1
	Material name - Madeupium
	Done getting FEA materials

Getting FEA properties.......
	Number of properties - 1
	Property name - plate
	Done getting FEA properties
Updating mesh element types based on properties input

Getting FEA constraints.......
	Number of constraints - 1
	Constraint name - edgeConstraint
	No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement"
	Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults

Getting FEA loads.......
	Number of loads - 1
	Load name - appliedPressure
	Done getting FEA loads

Getting FEA design variables.......
	Number of design variables          - 2
	Design_Variable name - plateLength
	Design_Variable name - thick1
	Design_Variable_Relation name - thick1
	Number of design variable relations - 1
	Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL

Getting FEA analyses.......
	Number of analyses - 1
	Analysis name - Default
	Done getting FEA analyses

Writing Nastran grid and connectivity file (in small field format) ....
Finished writing Nastran grid file

Writing subElement types (if any) - appending mesh file

Writing TACS instruction file....
	Writing analysis cards
	Writing load ADD cards
	Writing constraint ADD cards
	Writing load cards
	Writing constraint cards
	Writing material cards
	Writing property cards
	Writing design variable cards
	Writing design variable relation cards
Mapping Csys attributes ................
	Number of unique Csys attributes = 0

Getting FEA coordinate systems.......
	Number of coordinate systems - 0
	No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
	Number of unique capsConstraint attributes = 1
	Name = plateEdge, index = 1
Mapping capsLoad attributes ................
	Number of unique capsLoad attributes = 1
	Name = plate, index = 1
Mapping capsBound attributes ................
	Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
	Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
	Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
	Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
	Mesh for body = 0
	Number of nodal coordinates = 25
	Number of elements = 16
	Elemental Nodes = 0
	Elemental Rods  = 0
	Elemental Tria3 = 0
	Elemental Quad4 = 16

Getting FEA materials.......
	Number of materials - 1
	Material name - Madeupium
	Done getting FEA materials

Getting FEA properties.......
	Number of properties - 1
	Property name - plate
	Done getting FEA properties
Updating mesh element types based on properties input

Getting FEA constraints.......
	Number of constraints - 1
	Constraint name - edgeConstraint
	No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement"
	Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults

Getting FEA loads.......
	Number of loads - 1
	Load name - appliedPressure
	Done getting FEA loads

Getting FEA design variables.......
	Number of design variables          - 2
	Design_Variable name - plateLength
	Design_Variable name - thick1
	Design_Variable_Relation name - thick1
	Number of design variable relations - 1
	Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL

Getting FEA analyses.......
	Number of analyses - 1
	Analysis name - Default
	Done getting FEA analyses

Writing Nastran grid and connectivity file (in small field format) ....
Finished writing Nastran grid file

Writing subElement types (if any) - appending mesh file

Writing TACS instruction file....
	Writing analysis cards
	Writing load ADD cards
	Writing constraint ADD cards
	Writing load cards
	Writing constraint cards
	Writing material cards
	Writing property cards
	Writing design variable cards
	Writing design variable relation cards
Mapping Csys attributes ................
	Number of unique Csys attributes = 0

Getting FEA coordinate systems.......
	Number of coordinate systems - 0
	No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
	Number of unique capsConstraint attributes = 1
	Name = plateEdge, index = 1
Mapping capsLoad attributes ................
	Number of unique capsLoad attributes = 1
	Name = plate, index = 1
Mapping capsBound attributes ................
	Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
	Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
	Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
	Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
	Mesh for body = 0
	Number of nodal coordinates = 25
	Number of elements = 16
	Elemental Nodes = 0
	Elemental Rods  = 0
	Elemental Tria3 = 0
	Elemental Quad4 = 16

Getting FEA materials.......
	Number of materials - 1
	Material name - Madeupium
	Done getting FEA materials

Getting FEA properties.......
	Number of properties - 1
	Property name - plate
	Done getting FEA properties
Updating mesh element types based on properties input

Getting FEA constraints.......
	Number of constraints - 1
	Constraint name - edgeConstraint
	No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement"
	Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults

Getting FEA loads.......
	Number of loads - 1
	Load name - appliedPressure
	Done getting FEA loads

Getting FEA design variables.......
	Number of design variables          - 2
	Design_Variable name - plateLength
	Design_Variable name - thick1
	Design_Variable_Relation name - thick1
	Number of design variable relations - 1
	Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL

Getting FEA analyses.......
	Number of analyses - 1
	Analysis name - Default
	Done getting FEA analyses

Writing Nastran grid and connectivity file (in small field format) ....
Finished writing Nastran grid file

Writing subElement types (if any) - appending mesh file

Writing TACS instruction file....
	Writing analysis cards
	Writing load ADD cards
	Writing constraint ADD cards
	Writing load cards
	Writing constraint cards
	Writing material cards
	Writing property cards
	Writing design variable cards
	Writing design variable relation cards
Mapping Csys attributes ................
	Number of unique Csys attributes = 0

Getting FEA coordinate systems.......
	Number of coordinate systems - 0
	No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
	Number of unique capsConstraint attributes = 1
	Name = plateEdge, index = 1
Mapping capsLoad attributes ................
	Number of unique capsLoad attributes = 1
	Name = plate, index = 1
Mapping capsBound attributes ................
	Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
	Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
	Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
	Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
	Mesh for body = 0
	Number of nodal coordinates = 25
	Number of elements = 16
	Elemental Nodes = 0
	Elemental Rods  = 0
	Elemental Tria3 = 0
	Elemental Quad4 = 16

Getting FEA materials.......
	Number of materials - 1
	Material name - Madeupium
	Done getting FEA materials

Getting FEA properties.......
	Number of properties - 1
	Property name - plate
	Done getting FEA properties
Updating mesh element types based on properties input

Getting FEA constraints.......
	Number of constraints - 1
	Constraint name - edgeConstraint
	No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement"
	Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults

Getting FEA loads.......
	Number of loads - 1
	Load name - appliedPressure
	Done getting FEA loads

Getting FEA design variables.......
	Number of design variables          - 2
	Design_Variable name - plateLength
	Design_Variable name - thick1
	Design_Variable_Relation name - thick1
	Number of design variable relations - 1
	Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL

Getting FEA analyses.......
	Number of analyses - 1
	Analysis name - Default
	Done getting FEA analyses

Writing Nastran grid and connectivity file (in small field format) ....
Finished writing Nastran grid file

Writing subElement types (if any) - appending mesh file

Writing TACS instruction file....
	Writing analysis cards
	Writing load ADD cards
	Writing constraint ADD cards
	Writing load cards
	Writing constraint cards
	Writing material cards
	Writing property cards
	Writing design variable cards
	Writing design variable relation cards
Mapping Csys attributes ................
	Number of unique Csys attributes = 0

Getting FEA coordinate systems.......
	Number of coordinate systems - 0
	No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
	Number of unique capsConstraint attributes = 1
	Name = plateEdge, index = 1
Mapping capsLoad attributes ................
	Number of unique capsLoad attributes = 1
	Name = plate, index = 1
Mapping capsBound attributes ................
	Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
	Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
	Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
	Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
	Mesh for body = 0
	Number of nodal coordinates = 25
	Number of elements = 16
	Elemental Nodes = 0
	Elemental Rods  = 0
	Elemental Tria3 = 0
	Elemental Quad4 = 16

Getting FEA materials.......
	Number of materials - 1
	Material name - Madeupium
	Done getting FEA materials

Getting FEA properties.......
	Number of properties - 1
	Property name - plate
	Done getting FEA properties
Updating mesh element types based on properties input

Getting FEA constraints.......
	Number of constraints - 1
	Constraint name - edgeConstraint
	No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement"
	Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults

Getting FEA loads.......
	Number of loads - 1
	Load name - appliedPressure
	Done getting FEA loads

Getting FEA design variables.......
	Number of design variables          - 2
	Design_Variable name - plateLength
	Design_Variable name - thick1
	Design_Variable_Relation name - thick1
	Number of design variable relations - 1
	Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL

Getting FEA analyses.......
	Number of analyses - 1
	Analysis name - Default
	Done getting FEA analyses

Writing Nastran grid and connectivity file (in small field format) ....
Finished writing Nastran grid file

Writing subElement types (if any) - appending mesh file

Writing TACS instruction file....
	Writing analysis cards
	Writing load ADD cards
	Writing constraint ADD cards
	Writing load cards
	Writing constraint cards
	Writing material cards
	Writing property cards
	Writing design variable cards
	Writing design variable relation cards
Mapping Csys attributes ................
	Number of unique Csys attributes = 0

Getting FEA coordinate systems.......
	Number of coordinate systems - 0
	No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
	Number of unique capsConstraint attributes = 1
	Name = plateEdge, index = 1
Mapping capsLoad attributes ................
	Number of unique capsLoad attributes = 1
	Name = plate, index = 1
Mapping capsBound attributes ................
	Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
	Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
	Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
	Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
	Mesh for body = 0
	Number of nodal coordinates = 25
	Number of elements = 16
	Elemental Nodes = 0
	Elemental Rods  = 0
	Elemental Tria3 = 0
	Elemental Quad4 = 16

Getting FEA materials.......
	Number of materials - 1
	Material name - Madeupium
	Done getting FEA materials

Getting FEA properties.......
	Number of properties - 1
	Property name - plate
	Done getting FEA properties
Updating mesh element types based on properties input

Getting FEA constraints.......
	Number of constraints - 1
	Constraint name - edgeConstraint
	No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement"
	Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults

Getting FEA loads.......
	Number of loads - 1
	Load name - appliedPressure
	Done getting FEA loads

Getting FEA design variables.......
	Number of design variables          - 2
	Design_Variable name - plateLength
	Design_Variable name - thick1
	Design_Variable_Relation name - thick1
	Number of design variable relations - 1
	Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL

Getting FEA analyses.......
	Number of analyses - 1
	Analysis name - Default
	Done getting FEA analyses

Writing Nastran grid and connectivity file (in small field format) ....
Finished writing Nastran grid file

Writing subElement types (if any) - appending mesh file

Writing TACS instruction file....
	Writing analysis cards
	Writing load ADD cards
	Writing constraint ADD cards
	Writing load cards
	Writing constraint cards
	Writing material cards
	Writing property cards
	Writing design variable cards
	Writing design variable relation cards
Mapping Csys attributes ................
	Number of unique Csys attributes = 0

Getting FEA coordinate systems.......
	Number of coordinate systems - 0
	No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
	Number of unique capsConstraint attributes = 1
	Name = plateEdge, index = 1
Mapping capsLoad attributes ................
	Number of unique capsLoad attributes = 1
	Name = plate, index = 1
Mapping capsBound attributes ................
	Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
	Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
	Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
	Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
	Mesh for body = 0
	Number of nodal coordinates = 25
	Number of elements = 16
	Elemental Nodes = 0
	Elemental Rods  = 0
	Elemental Tria3 = 0
	Elemental Quad4 = 16

Getting FEA materials.......
	Number of materials - 1
	Material name - Madeupium
	Done getting FEA materials

Getting FEA properties.......
	Number of properties - 1
	Property name - plate
	Done getting FEA properties
Updating mesh element types based on properties input

Getting FEA constraints.......
	Number of constraints - 1
	Constraint name - edgeConstraint
	No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement"
	Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults

Getting FEA loads.......
	Number of loads - 1
	Load name - appliedPressure
	Done getting FEA loads

Getting FEA design variables.......
	Number of design variables          - 2
	Design_Variable name - plateLength
	Design_Variable name - thick1
	Design_Variable_Relation name - thick1
	Number of design variable relations - 1
	Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL

Getting FEA analyses.......
	Number of analyses - 1
	Analysis name - Default
	Done getting FEA analyses

Writing Nastran grid and connectivity file (in small field format) ....
Finished writing Nastran grid file

Writing subElement types (if any) - appending mesh file

Writing TACS instruction file....
	Writing analysis cards
	Writing load ADD cards
	Writing constraint ADD cards
	Writing load cards
	Writing constraint cards
	Writing material cards
	Writing property cards
	Writing design variable cards
	Writing design variable relation cards
Mapping Csys attributes ................
	Number of unique Csys attributes = 0

Getting FEA coordinate systems.......
	Number of coordinate systems - 0
	No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
	Number of unique capsConstraint attributes = 1
	Name = plateEdge, index = 1
Mapping capsLoad attributes ................
	Number of unique capsLoad attributes = 1
	Name = plate, index = 1
Mapping capsBound attributes ................
	Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
	Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
	Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
	Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
	Mesh for body = 0
	Number of nodal coordinates = 25
	Number of elements = 16
	Elemental Nodes = 0
	Elemental Rods  = 0
	Elemental Tria3 = 0
	Elemental Quad4 = 16

Getting FEA materials.......
	Number of materials - 1
	Material name - Madeupium
	Done getting FEA materials

Getting FEA properties.......
	Number of properties - 1
	Property name - plate
	Done getting FEA properties
Updating mesh element types based on properties input

Getting FEA constraints.......
	Number of constraints - 1
	Constraint name - edgeConstraint
	No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement"
	Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults

Getting FEA loads.......
	Number of loads - 1
	Load name - appliedPressure
	Done getting FEA loads

Getting FEA design variables.......
	Number of design variables          - 2
	Design_Variable name - plateLength
	Design_Variable name - thick1
	Design_Variable_Relation name - thick1
	Number of design variable relations - 1
	Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL

Getting FEA analyses.......
	Number of analyses - 1
	Analysis name - Default
	Done getting FEA analyses

Writing Nastran grid and connectivity file (in small field format) ....
Finished writing Nastran grid file

Writing subElement types (if any) - appending mesh file

Writing TACS instruction file....
	Writing analysis cards
	Writing load ADD cards
	Writing constraint ADD cards
	Writing load cards
	Writing constraint cards
	Writing material cards
	Writing property cards
	Writing design variable cards
	Writing design variable relation cards
Mapping Csys attributes ................
	Number of unique Csys attributes = 0

Getting FEA coordinate systems.......
	Number of coordinate systems - 0
	No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
	Number of unique capsConstraint attributes = 1
	Name = plateEdge, index = 1
Mapping capsLoad attributes ................
	Number of unique capsLoad attributes = 1
	Name = plate, index = 1
Mapping capsBound attributes ................
	Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
	Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
	Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
	Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
	Mesh for body = 0
	Number of nodal coordinates = 25
	Number of elements = 16
	Elemental Nodes = 0
	Elemental Rods  = 0
	Elemental Tria3 = 0
	Elemental Quad4 = 16

Getting FEA materials.......
	Number of materials - 1
	Material name - Madeupium
	Done getting FEA materials

Getting FEA properties.......
	Number of properties - 1
	Property name - plate
	Done getting FEA properties
Updating mesh element types based on properties input

Getting FEA constraints.......
	Number of constraints - 1
	Constraint name - edgeConstraint
	No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement"
	Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults

Getting FEA loads.......
	Number of loads - 1
	Load name - appliedPressure
	Done getting FEA loads

Getting FEA design variables.......
	Number of design variables          - 2
	Design_Variable name - plateLength
	Design_Variable name - thick1
	Design_Variable_Relation name - thick1
	Number of design variable relations - 1
	Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL

Getting FEA analyses.......
	Number of analyses - 1
	Analysis name - Default
	Done getting FEA analyses

Writing Nastran grid and connectivity file (in small field format) ....
Finished writing Nastran grid file

Writing subElement types (if any) - appending mesh file

Writing TACS instruction file....
	Writing analysis cards
	Writing load ADD cards
	Writing constraint ADD cards
	Writing load cards
	Writing constraint cards
	Writing material cards
	Writing property cards
	Writing design variable cards
	Writing design variable relation cards
Mapping Csys attributes ................
	Number of unique Csys attributes = 0

Getting FEA coordinate systems.......
	Number of coordinate systems - 0
	No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
	Number of unique capsConstraint attributes = 1
	Name = plateEdge, index = 1
Mapping capsLoad attributes ................
	Number of unique capsLoad attributes = 1
	Name = plate, index = 1
Mapping capsBound attributes ................
	Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
	Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
	Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
	Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
	Mesh for body = 0
	Number of nodal coordinates = 25
	Number of elements = 16
	Elemental Nodes = 0
	Elemental Rods  = 0
	Elemental Tria3 = 0
	Elemental Quad4 = 16

Getting FEA materials.......
	Number of materials - 1
	Material name - Madeupium
	Done getting FEA materials

Getting FEA properties.......
	Number of properties - 1
	Property name - plate
	Done getting FEA properties
Updating mesh element types based on properties input

Getting FEA constraints.......
	Number of constraints - 1
	Constraint name - edgeConstraint
	No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement"
	Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults

Getting FEA loads.......
	Number of loads - 1
	Load name - appliedPressure
	Done getting FEA loads

Getting FEA design variables.......
	Number of design variables          - 2
	Design_Variable name - plateLength
	Design_Variable name - thick1
	Design_Variable_Relation name - thick1
	Number of design variable relations - 1
	Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL

Getting FEA analyses.......
	Number of analyses - 1
	Analysis name - Default
	Done getting FEA analyses

Writing Nastran grid and connectivity file (in small field format) ....
Finished writing Nastran grid file

Writing subElement types (if any) - appending mesh file

Writing TACS instruction file....
	Writing analysis cards
	Writing load ADD cards
	Writing constraint ADD cards
	Writing load cards
	Writing constraint cards
	Writing material cards
	Writing property cards
	Writing design variable cards
	Writing design variable relation cards
Mapping Csys attributes ................
	Number of unique Csys attributes = 0

Getting FEA coordinate systems.......
	Number of coordinate systems - 0
	No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
	Number of unique capsConstraint attributes = 1
	Name = plateEdge, index = 1
Mapping capsLoad attributes ................
	Number of unique capsLoad attributes = 1
	Name = plate, index = 1
Mapping capsBound attributes ................
	Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
	Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
	Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
	Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
	Mesh for body = 0
	Number of nodal coordinates = 25
	Number of elements = 16
	Elemental Nodes = 0
	Elemental Rods  = 0
	Elemental Tria3 = 0
	Elemental Quad4 = 16

Getting FEA materials.......
	Number of materials - 1
	Material name - Madeupium
	Done getting FEA materials

Getting FEA properties.......
	Number of properties - 1
	Property name - plate
	Done getting FEA properties
Updating mesh element types based on properties input

Getting FEA constraints.......
	Number of constraints - 1
	Constraint name - edgeConstraint
	No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement"
	Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults

Getting FEA loads.......
	Number of loads - 1
	Load name - appliedPressure
	Done getting FEA loads

Getting FEA design variables.......
	Number of design variables          - 2
	Design_Variable name - plateLength
	Design_Variable name - thick1
	Design_Variable_Relation name - thick1
	Number of design variable relations - 1
	Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL

Getting FEA analyses.......
	Number of analyses - 1
	Analysis name - Default
	Done getting FEA analyses

Writing Nastran grid and connectivity file (in small field format) ....
Finished writing Nastran grid file

Writing subElement types (if any) - appending mesh file

Writing TACS instruction file....
	Writing analysis cards
	Writing load ADD cards
	Writing constraint ADD cards
	Writing load cards
	Writing constraint cards
	Writing material cards
	Writing property cards
	Writing design variable cards
	Writing design variable relation cards
Mapping Csys attributes ................
	Number of unique Csys attributes = 0

Getting FEA coordinate systems.......
	Number of coordinate systems - 0
	No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
	Number of unique capsConstraint attributes = 1
	Name = plateEdge, index = 1
Mapping capsLoad attributes ................
	Number of unique capsLoad attributes = 1
	Name = plate, index = 1
Mapping capsBound attributes ................
	Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
	Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
	Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
	Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
	Mesh for body = 0
	Number of nodal coordinates = 25
	Number of elements = 16
	Elemental Nodes = 0
	Elemental Rods  = 0
	Elemental Tria3 = 0
	Elemental Quad4 = 16

Getting FEA materials.......
	Number of materials - 1
	Material name - Madeupium
	Done getting FEA materials

Getting FEA properties.......
	Number of properties - 1
	Property name - plate
	Done getting FEA properties
Updating mesh element types based on properties input

Getting FEA constraints.......
	Number of constraints - 1
	Constraint name - edgeConstraint
	No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement"
	Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults

Getting FEA loads.......
	Number of loads - 1
	Load name - appliedPressure
	Done getting FEA loads

Getting FEA design variables.......
	Number of design variables          - 2
	Design_Variable name - plateLength
	Design_Variable name - thick1
	Design_Variable_Relation name - thick1
	Number of design variable relations - 1
	Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL

Getting FEA analyses.......
	Number of analyses - 1
	Analysis name - Default
	Done getting FEA analyses

Writing Nastran grid and connectivity file (in small field format) ....
Finished writing Nastran grid file

Writing subElement types (if any) - appending mesh file

Writing TACS instruction file....
	Writing analysis cards
	Writing load ADD cards
	Writing constraint ADD cards
	Writing load cards
	Writing constraint cards
	Writing material cards
	Writing property cards
	Writing design variable cards
	Writing design variable relation cards
Mapping Csys attributes ................
	Number of unique Csys attributes = 0

Getting FEA coordinate systems.......
	Number of coordinate systems - 0
	No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
	Number of unique capsConstraint attributes = 1
	Name = plateEdge, index = 1
Mapping capsLoad attributes ................
	Number of unique capsLoad attributes = 1
	Name = plate, index = 1
Mapping capsBound attributes ................
	Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
	Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
	Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
	Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = plate, index = 1
Projecting tessellation 1 (of 1) on to new body
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
	Mesh for body = 0
	Number of nodal coordinates = 25
	Number of elements = 16
	Elemental Nodes = 0
	Elemental Rods  = 0
	Elemental Tria3 = 0
	Elemental Quad4 = 16

Getting FEA materials.......
	Number of materials - 1
	Material name - Madeupium
	Done getting FEA materials

Getting FEA properties.......
	Number of properties - 1
	Property name - plate
	Done getting FEA properties
Updating mesh element types based on properties input

Getting FEA constraints.......
	Number of constraints - 1
	Constraint name - edgeConstraint
	No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement"
	Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults

Getting FEA loads.......
	Number of loads - 1
	Load name - appliedPressure
	Done getting FEA loads

Getting FEA design variables.......
	Number of design variables          - 1
	Design_Variable name - plateWidth
	Number of design variable relations - 0
	Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL

Getting FEA analyses.......
	Number of analyses - 1
	Analysis name - Default
	Done getting FEA analyses

Writing Nastran grid and connectivity file (in small field format) ....
Finished writing Nastran grid file

Writing subElement types (if any) - appending mesh file

Writing TACS instruction file....
	Writing analysis cards
	Writing load ADD cards
	Writing constraint ADD cards
	Writing load cards
	Writing constraint cards
	Writing material cards
	Writing property cards
	Writing design variable cards
Mapping Csys attributes ................
	Number of unique Csys attributes = 0

Getting FEA coordinate systems.......
	Number of coordinate systems - 0
	No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
	Number of unique capsConstraint attributes = 1
	Name = plateEdge, index = 1
Mapping capsLoad attributes ................
	Number of unique capsLoad attributes = 1
	Name = plate, index = 1
Mapping capsBound attributes ................
	Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
	Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
	Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
	Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
	Mesh for body = 0
	Number of nodal coordinates = 25
	Number of elements = 16
	Elemental Nodes = 0
	Elemental Rods  = 0
	Elemental Tria3 = 0
	Elemental Quad4 = 16

Getting FEA materials.......
	Number of materials - 1
	Material name - Madeupium
	Done getting FEA materials

Getting FEA properties.......
	Number of properties - 1
	Property name - plate
	Done getting FEA properties
Updating mesh element types based on properties input

Getting FEA constraints.......
	Number of constraints - 1
	Constraint name - edgeConstraint
	No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement"
	Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults

Getting FEA loads.......
	Number of loads - 1
	Load name - appliedPressure
	Done getting FEA loads

Getting FEA design variables.......
	Number of design variables          - 1
	Design_Variable name - plateWidth
	Number of design variable relations - 0
	Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL

Getting FEA analyses.......
	Number of analyses - 1
	Analysis name - Default
	Done getting FEA analyses

Writing Nastran grid and connectivity file (in small field format) ....
Finished writing Nastran grid file

Writing subElement types (if any) - appending mesh file

Writing TACS instruction file....
	Writing analysis cards
	Writing load ADD cards
	Writing constraint ADD cards
	Writing load cards
	Writing constraint cards
	Writing material cards
	Writing property cards
	Writing design variable cards
Mapping Csys attributes ................
	Number of unique Csys attributes = 0

Getting FEA coordinate systems.......
	Number of coordinate systems - 0
	No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
	Number of unique capsConstraint attributes = 1
	Name = plateEdge, index = 1
Mapping capsLoad attributes ................
	Number of unique capsLoad attributes = 1
	Name = plate, index = 1
Mapping capsBound attributes ................
	Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
	Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
	Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
	Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
	Mesh for body = 0
	Number of nodal coordinates = 25
	Number of elements = 16
	Elemental Nodes = 0
	Elemental Rods  = 0
	Elemental Tria3 = 0
	Elemental Quad4 = 16

Getting FEA materials.......
	Number of materials - 1
	Material name - Madeupium
	Done getting FEA materials

Getting FEA properties.......
	Number of properties - 1
	Property name - plate
	Done getting FEA properties
Updating mesh element types based on properties input

Getting FEA constraints.......
	Number of constraints - 1
	Constraint name - edgeConstraint
	No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement"
	Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults

Getting FEA loads.......
	Number of loads - 1
	Load name - appliedPressure
	Done getting FEA loads

Getting FEA design variables.......
	Number of design variables          - 1
	Design_Variable name - plateWidth
	Number of design variable relations - 0
	Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL

Getting FEA analyses.......
	Number of analyses - 1
	Analysis name - Default
	Done getting FEA analyses

Writing Nastran grid and connectivity file (in small field format) ....
Finished writing Nastran grid file

Writing subElement types (if any) - appending mesh file

Writing TACS instruction file....
	Writing analysis cards
	Writing load ADD cards
	Writing constraint ADD cards
	Writing load cards
	Writing constraint cards
	Writing material cards
	Writing property cards
	Writing design variable cards
Mapping Csys attributes ................
	Number of unique Csys attributes = 0

Getting FEA coordinate systems.......
	Number of coordinate systems - 0
	No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
	Number of unique capsConstraint attributes = 1
	Name = plateEdge, index = 1
Mapping capsLoad attributes ................
	Number of unique capsLoad attributes = 1
	Name = plate, index = 1
Mapping capsBound attributes ................
	Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
	Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
	Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
	Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
	Mesh for body = 0
	Number of nodal coordinates = 25
	Number of elements = 16
	Elemental Nodes = 0
	Elemental Rods  = 0
	Elemental Tria3 = 0
	Elemental Quad4 = 16

Getting FEA materials.......
	Number of materials - 1
	Material name - Madeupium
	Done getting FEA materials

Getting FEA properties.......
	Number of properties - 1
	Property name - plate
	Done getting FEA properties
Updating mesh element types based on properties input

Getting FEA constraints.......
	Number of constraints - 1
	Constraint name - edgeConstraint
	No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement"
	Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults

Getting FEA loads.......
	Number of loads - 1
	Load name - appliedPressure
	Done getting FEA loads

Getting FEA design variables.......
	Number of design variables          - 1
	Design_Variable name - plateWidth
	Number of design variable relations - 0
	Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL

Getting FEA analyses.......
	Number of analyses - 1
	Analysis name - Default
	Done getting FEA analyses

Writing Nastran grid and connectivity file (in small field format) ....
Finished writing Nastran grid file

Writing subElement types (if any) - appending mesh file

Writing TACS instruction file....
	Writing analysis cards
	Writing load ADD cards
	Writing constraint ADD cards
	Writing load cards
	Writing constraint cards
	Writing material cards
	Writing property cards
	Writing design variable cards
Mapping Csys attributes ................
	Number of unique Csys attributes = 0

Getting FEA coordinate systems.......
	Number of coordinate systems - 0
	No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
	Number of unique capsConstraint attributes = 1
	Name = plateEdge, index = 1
Mapping capsLoad attributes ................
	Number of unique capsLoad attributes = 1
	Name = plate, index = 1
Mapping capsBound attributes ................
	Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
	Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
	Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
	Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
	Mesh for body = 0
	Number of nodal coordinates = 25
	Number of elements = 16
	Elemental Nodes = 0
	Elemental Rods  = 0
	Elemental Tria3 = 0
	Elemental Quad4 = 16

Getting FEA materials.......
	Number of materials - 1
	Material name - Madeupium
	Done getting FEA materials

Getting FEA properties.......
	Number of properties - 1
	Property name - plate
	Done getting FEA properties
Updating mesh element types based on properties input

Getting FEA constraints.......
	Number of constraints - 1
	Constraint name - edgeConstraint
	No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement"
	Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults

Getting FEA loads.......
	Number of loads - 1
	Load name - appliedPressure
	Done getting FEA loads

Getting FEA design variables.......
	Number of design variables          - 1
	Design_Variable name - plateWidth
	Number of design variable relations - 0
	Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL

Getting FEA analyses.......
	Number of analyses - 1
	Analysis name - Default
	Done getting FEA analyses

Writing Nastran grid and connectivity file (in small field format) ....
Finished writing Nastran grid file

Writing subElement types (if any) - appending mesh file

Writing TACS instruction file....
	Writing analysis cards
	Writing load ADD cards
	Writing constraint ADD cards
	Writing load cards
	Writing constraint cards
	Writing material cards
	Writing property cards
	Writing design variable cards
Mapping Csys attributes ................
	Number of unique Csys attributes = 0

Getting FEA coordinate systems.......
	Number of coordinate systems - 0
	No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
	Number of unique capsConstraint attributes = 1
	Name = plateEdge, index = 1
Mapping capsLoad attributes ................
	Number of unique capsLoad attributes = 1
	Name = plate, index = 1
Mapping capsBound attributes ................
	Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
	Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
	Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
	Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
	Mesh for body = 0
	Number of nodal coordinates = 25
	Number of elements = 16
	Elemental Nodes = 0
	Elemental Rods  = 0
	Elemental Tria3 = 0
	Elemental Quad4 = 16

Getting FEA materials.......
	Number of materials - 1
	Material name - Madeupium
	Done getting FEA materials

Getting FEA properties.......
	Number of properties - 1
	Property name - plate
	Done getting FEA properties
Updating mesh element types based on properties input

Getting FEA constraints.......
	Number of constraints - 1
	Constraint name - edgeConstraint
	No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement"
	Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults

Getting FEA loads.......
	Number of loads - 1
	Load name - appliedPressure
	Done getting FEA loads

Getting FEA design variables.......
	Number of design variables          - 1
	Design_Variable name - plateWidth
	Number of design variable relations - 0
	Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL

Getting FEA analyses.......
	Number of analyses - 1
	Analysis name - Default
	Done getting FEA analyses

Writing Nastran grid and connectivity file (in small field format) ....
Finished writing Nastran grid file

Writing subElement types (if any) - appending mesh file

Writing TACS instruction file....
	Writing analysis cards
	Writing load ADD cards
	Writing constraint ADD cards
	Writing load cards
	Writing constraint cards
	Writing material cards
	Writing property cards
	Writing design variable cards
Mapping Csys attributes ................
	Number of unique Csys attributes = 0

Getting FEA coordinate systems.......
	Number of coordinate systems - 0
	No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
	Number of unique capsConstraint attributes = 1
	Name = plateEdge, index = 1
Mapping capsLoad attributes ................
	Number of unique capsLoad attributes = 1
	Name = plate, index = 1
Mapping capsBound attributes ................
	Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
	Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
	Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
	Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
	Mesh for body = 0
	Number of nodal coordinates = 25
	Number of elements = 16
	Elemental Nodes = 0
	Elemental Rods  = 0
	Elemental Tria3 = 0
	Elemental Quad4 = 16

Getting FEA materials.......
	Number of materials - 1
	Material name - Madeupium
	Done getting FEA materials

Getting FEA properties.......
	Number of properties - 1
	Property name - plate
	Done getting FEA properties
Updating mesh element types based on properties input

Getting FEA constraints.......
	Number of constraints - 1
	Constraint name - edgeConstraint
	No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement"
	Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults

Getting FEA loads.......
	Number of loads - 1
	Load name - appliedPressure
	Done getting FEA loads

Getting FEA design variables.......
	Number of design variables          - 1
	Design_Variable name - plateWidth
	Number of design variable relations - 0
	Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL

Getting FEA analyses.......
	Number of analyses - 1
	Analysis name - Default
	Done getting FEA analyses

Writing Nastran grid and connectivity file (in small field format) ....
Finished writing Nastran grid file

Writing subElement types (if any) - appending mesh file

Writing TACS instruction file....
	Writing analysis cards
	Writing load ADD cards
	Writing constraint ADD cards
	Writing load cards
	Writing constraint cards
	Writing material cards
	Writing property cards
	Writing design variable cards
Mapping Csys attributes ................
	Number of unique Csys attributes = 0

Getting FEA coordinate systems.......
	Number of coordinate systems - 0
	No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
	Number of unique capsConstraint attributes = 1
	Name = plateEdge, index = 1
Mapping capsLoad attributes ................
	Number of unique capsLoad attributes = 1
	Name = plate, index = 1
Mapping capsBound attributes ................
	Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
	Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
	Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
	Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
	Mesh for body = 0
	Number of nodal coordinates = 25
	Number of elements = 16
	Elemental Nodes = 0
	Elemental Rods  = 0
	Elemental Tria3 = 0
	Elemental Quad4 = 16

Getting FEA materials.......
	Number of materials - 1
	Material name - Madeupium
	Done getting FEA materials

Getting FEA properties.......
	Number of properties - 1
	Property name - plate
	Done getting FEA properties
Updating mesh element types based on properties input

Getting FEA constraints.......
	Number of constraints - 1
	Constraint name - edgeConstraint
	No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement"
	Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults

Getting FEA loads.......
	Number of loads - 1
	Load name - appliedPressure
	Done getting FEA loads

Getting FEA design variables.......
	Number of design variables          - 1
	Design_Variable name - plateWidth
	Number of design variable relations - 0
	Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL

Getting FEA analyses.......
	Number of analyses - 1
	Analysis name - Default
	Done getting FEA analyses

Writing Nastran grid and connectivity file (in small field format) ....
Finished writing Nastran grid file

Writing subElement types (if any) - appending mesh file

Writing TACS instruction file....
	Writing analysis cards
	Writing load ADD cards
	Writing constraint ADD cards
	Writing load cards
	Writing constraint cards
	Writing material cards
	Writing property cards
	Writing design variable cards
Mapping Csys attributes ................
	Number of unique Csys attributes = 0

Getting FEA coordinate systems.......
	Number of coordinate systems - 0
	No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
	Number of unique capsConstraint attributes = 1
	Name = plateEdge, index = 1
Mapping capsLoad attributes ................
	Number of unique capsLoad attributes = 1
	Name = plate, index = 1
Mapping capsBound attributes ................
	Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
	Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
	Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
	Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
	Mesh for body = 0
	Number of nodal coordinates = 25
	Number of elements = 16
	Elemental Nodes = 0
	Elemental Rods  = 0
	Elemental Tria3 = 0
	Elemental Quad4 = 16

Getting FEA materials.......
	Number of materials - 1
	Material name - Madeupium
	Done getting FEA materials

Getting FEA properties.......
	Number of properties - 1
	Property name - plate
	Done getting FEA properties
Updating mesh element types based on properties input

Getting FEA constraints.......
	Number of constraints - 1
	Constraint name - edgeConstraint
	No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement"
	Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults

Getting FEA loads.......
	Number of loads - 1
	Load name - appliedPressure
	Done getting FEA loads

Getting FEA design variables.......
	Number of design variables          - 1
	Design_Variable name - plateWidth
	Number of design variable relations - 0
	Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL

Getting FEA analyses.......
	Number of analyses - 1
	Analysis name - Default
	Done getting FEA analyses

Writing Nastran grid and connectivity file (in small field format) ....
Finished writing Nastran grid file

Writing subElement types (if any) - appending mesh file

Writing TACS instruction file....
	Writing analysis cards
	Writing load ADD cards
	Writing constraint ADD cards
	Writing load cards
	Writing constraint cards
	Writing material cards
	Writing property cards
	Writing design variable cards
Mapping Csys attributes ................
	Number of unique Csys attributes = 0

Getting FEA coordinate systems.......
	Number of coordinate systems - 0
	No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
	Number of unique capsConstraint attributes = 1
	Name = plateEdge, index = 1
Mapping capsLoad attributes ................
	Number of unique capsLoad attributes = 1
	Name = plate, index = 1
Mapping capsBound attributes ................
	Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
	Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
	Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
	Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
	Mesh for body = 0
	Number of nodal coordinates = 25
	Number of elements = 16
	Elemental Nodes = 0
	Elemental Rods  = 0
	Elemental Tria3 = 0
	Elemental Quad4 = 16

Getting FEA materials.......
	Number of materials - 1
	Material name - Madeupium
	Done getting FEA materials

Getting FEA properties.......
	Number of properties - 1
	Property name - plate
	Done getting FEA properties
Updating mesh element types based on properties input

Getting FEA constraints.......
	Number of constraints - 1
	Constraint name - edgeConstraint
	No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement"
	Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults

Getting FEA loads.......
	Number of loads - 1
	Load name - appliedPressure
	Done getting FEA loads

Getting FEA design variables.......
	Number of design variables          - 1
	Design_Variable name - plateWidth
	Number of design variable relations - 0
	Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL

Getting FEA analyses.......
	Number of analyses - 1
	Analysis name - Default
	Done getting FEA analyses

Writing Nastran grid and connectivity file (in small field format) ....
Finished writing Nastran grid file

Writing subElement types (if any) - appending mesh file

Writing TACS instruction file....
	Writing analysis cards
	Writing load ADD cards
	Writing constraint ADD cards
	Writing load cards
	Writing constraint cards
	Writing material cards
	Writing property cards
	Writing design variable cards
Mapping Csys attributes ................
	Number of unique Csys attributes = 0

Getting FEA coordinate systems.......
	Number of coordinate systems - 0
	No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
	Number of unique capsConstraint attributes = 1
	Name = plateEdge, index = 1
Mapping capsLoad attributes ................
	Number of unique capsLoad attributes = 1
	Name = plate, index = 1
Mapping capsBound attributes ................
	Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
	Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
	Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
	Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
	Mesh for body = 0
	Number of nodal coordinates = 25
	Number of elements = 16
	Elemental Nodes = 0
	Elemental Rods  = 0
	Elemental Tria3 = 0
	Elemental Quad4 = 16

Getting FEA materials.......
	Number of materials - 1
	Material name - Madeupium
	Done getting FEA materials

Getting FEA properties.......
	Number of properties - 1
	Property name - plate
	Done getting FEA properties
Updating mesh element types based on properties input

Getting FEA constraints.......
	Number of constraints - 1
	Constraint name - edgeConstraint
	No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement"
	Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults

Getting FEA loads.......
	Number of loads - 1
	Load name - appliedPressure
	Done getting FEA loads

Getting FEA design variables.......
	Number of design variables          - 1
	Design_Variable name - plateWidth
	Number of design variable relations - 0
	Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL

Getting FEA analyses.......
	Number of analyses - 1
	Analysis name - Default
	Done getting FEA analyses

Writing Nastran grid and connectivity file (in small field format) ....
Finished writing Nastran grid file

Writing subElement types (if any) - appending mesh file

Writing TACS instruction file....
	Writing analysis cards
	Writing load ADD cards
	Writing constraint ADD cards
	Writing load cards
	Writing constraint cards
	Writing material cards
	Writing property cards
	Writing design variable cards
Mapping Csys attributes ................
	Number of unique Csys attributes = 0

Getting FEA coordinate systems.......
	Number of coordinate systems - 0
	No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
	Number of unique capsConstraint attributes = 1
	Name = plateEdge, index = 1
Mapping capsLoad attributes ................
	Number of unique capsLoad attributes = 1
	Name = plate, index = 1
Mapping capsBound attributes ................
	Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
	Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
	Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
	Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
	Mesh for body = 0
	Number of nodal coordinates = 25
	Number of elements = 16
	Elemental Nodes = 0
	Elemental Rods  = 0
	Elemental Tria3 = 0
	Elemental Quad4 = 16

Getting FEA materials.......
	Number of materials - 1
	Material name - Madeupium
	Done getting FEA materials

Getting FEA properties.......
	Number of properties - 1
	Property name - plate
	Done getting FEA properties
Updating mesh element types based on properties input

Getting FEA constraints.......
	Number of constraints - 1
	Constraint name - edgeConstraint
	No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement"
	Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults

Getting FEA loads.......
	Number of loads - 1
	Load name - appliedPressure
	Done getting FEA loads

Getting FEA design variables.......
	Number of design variables          - 1
	Design_Variable name - plateWidth
	Number of design variable relations - 0
	Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL

Getting FEA analyses.......
	Number of analyses - 1
	Analysis name - Default
	Done getting FEA analyses

Writing Nastran grid and connectivity file (in small field format) ....
Finished writing Nastran grid file

Writing subElement types (if any) - appending mesh file

Writing TACS instruction file....
	Writing analysis cards
	Writing load ADD cards
	Writing constraint ADD cards
	Writing load cards
	Writing constraint cards
	Writing material cards
	Writing property cards
	Writing design variable cards
Mapping Csys attributes ................
	Number of unique Csys attributes = 0

Getting FEA coordinate systems.......
	Number of coordinate systems - 0
	No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
	Number of unique capsConstraint attributes = 1
	Name = plateEdge, index = 1
Mapping capsLoad attributes ................
	Number of unique capsLoad attributes = 1
	Name = plate, index = 1
Mapping capsBound attributes ................
	Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
	Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
	Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
	Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
	Mesh for body = 0
	Number of nodal coordinates = 25
	Number of elements = 16
	Elemental Nodes = 0
	Elemental Rods  = 0
	Elemental Tria3 = 0
	Elemental Quad4 = 16

Getting FEA materials.......
	Number of materials - 1
	Material name - Madeupium
	Done getting FEA materials

Getting FEA properties.......
	Number of properties - 1
	Property name - plate
	Done getting FEA properties
Updating mesh element types based on properties input

Getting FEA constraints.......
	Number of constraints - 1
	Constraint name - edgeConstraint
	No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement"
	Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults

Getting FEA loads.......
	Number of loads - 1
	Load name - appliedPressure
	Done getting FEA loads

Getting FEA design variables.......
	Number of design variables          - 1
	Design_Variable name - plateWidth
	Number of design variable relations - 0
	Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL

Getting FEA analyses.......
	Number of analyses - 1
	Analysis name - Default
	Done getting FEA analyses

Writing Nastran grid and connectivity file (in small field format) ....
Finished writing Nastran grid file

Writing subElement types (if any) - appending mesh file

Writing TACS instruction file....
	Writing analysis cards
	Writing load ADD cards
	Writing constraint ADD cards
	Writing load cards
	Writing constraint cards
	Writing material cards
	Writing property cards
	Writing design variable cards
Mapping Csys attributes ................
	Number of unique Csys attributes = 0

Getting FEA coordinate systems.......
	Number of coordinate systems - 0
	No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
	Number of unique capsConstraint attributes = 1
	Name = plateEdge, index = 1
Mapping capsLoad attributes ................
	Number of unique capsLoad attributes = 1
	Name = plate, index = 1
Mapping capsBound attributes ................
	Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
	Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
	Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
	Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
	Mesh for body = 0
	Number of nodal coordinates = 25
	Number of elements = 16
	Elemental Nodes = 0
	Elemental Rods  = 0
	Elemental Tria3 = 0
	Elemental Quad4 = 16

Getting FEA materials.......
	Number of materials - 1
	Material name - Madeupium
	Done getting FEA materials

Getting FEA properties.......
	Number of properties - 1
	Property name - plate
	Done getting FEA properties
Updating mesh element types based on properties input

Getting FEA constraints.......
	Number of constraints - 1
	Constraint name - edgeConstraint
	No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement"
	Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults

Getting FEA loads.......
	Number of loads - 1
	Load name - appliedPressure
	Done getting FEA loads

Getting FEA design variables.......
	Number of design variables          - 1
	Design_Variable name - plateWidth
	Number of design variable relations - 0
	Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL

Getting FEA analyses.......
	Number of analyses - 1
	Analysis name - Default
	Done getting FEA analyses

Writing Nastran grid and connectivity file (in small field format) ....
Finished writing Nastran grid file

Writing subElement types (if any) - appending mesh file

Writing TACS instruction file....
	Writing analysis cards
	Writing load ADD cards
	Writing constraint ADD cards
	Writing load cards
	Writing constraint cards
	Writing material cards
	Writing property cards
	Writing design variable cards
Mapping Csys attributes ................
	Number of unique Csys attributes = 0

Getting FEA coordinate systems.......
	Number of coordinate systems - 0
	No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
	Number of unique capsConstraint attributes = 1
	Name = plateEdge, index = 1
Mapping capsLoad attributes ................
	Number of unique capsLoad attributes = 1
	Name = plate, index = 1
Mapping capsBound attributes ................
	Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
	Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
	Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
	Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
	Mesh for body = 0
	Number of nodal coordinates = 25
	Number of elements = 16
	Elemental Nodes = 0
	Elemental Rods  = 0
	Elemental Tria3 = 0
	Elemental Quad4 = 16

Getting FEA materials.......
	Number of materials - 1
	Material name - Madeupium
	Done getting FEA materials

Getting FEA properties.......
	Number of properties - 1
	Property name - plate
	Done getting FEA properties
Updating mesh element types based on properties input

Getting FEA constraints.......
	Number of constraints - 1
	Constraint name - edgeConstraint
	No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement"
	Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults

Getting FEA loads.......
	Number of loads - 1
	Load name - appliedPressure
	Done getting FEA loads

Getting FEA design variables.......
	Number of design variables          - 1
	Design_Variable name - plateWidth
	Number of design variable relations - 0
	Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL

Getting FEA analyses.......
	Number of analyses - 1
	Analysis name - Default
	Done getting FEA analyses

Writing Nastran grid and connectivity file (in small field format) ....
Finished writing Nastran grid file

Writing subElement types (if any) - appending mesh file

Writing TACS instruction file....
	Writing analysis cards
	Writing load ADD cards
	Writing constraint ADD cards
	Writing load cards
	Writing constraint cards
	Writing material cards
	Writing property cards
	Writing design variable cards
Mapping Csys attributes ................
	Number of unique Csys attributes = 0

Getting FEA coordinate systems.......
	Number of coordinate systems - 0
	No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
	Number of unique capsConstraint attributes = 1
	Name = plateEdge, index = 1
Mapping capsLoad attributes ................
	Number of unique capsLoad attributes = 1
	Name = plate, index = 1
Mapping capsBound attributes ................
	Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
	Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
	Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
	Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
	Mesh for body = 0
	Number of nodal coordinates = 25
	Number of elements = 16
	Elemental Nodes = 0
	Elemental Rods  = 0
	Elemental Tria3 = 0
	Elemental Quad4 = 16

Getting FEA materials.......
	Number of materials - 1
	Material name - Madeupium
	Done getting FEA materials

Getting FEA properties.......
	Number of properties - 1
	Property name - plate
	Done getting FEA properties
Updating mesh element types based on properties input

Getting FEA constraints.......
	Number of constraints - 1
	Constraint name - edgeConstraint
	No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement"
	Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults

Getting FEA loads.......
	Number of loads - 1
	Load name - appliedPressure
	Done getting FEA loads

Getting FEA design variables.......
	Number of design variables          - 1
	Design_Variable name - plateWidth
	Number of design variable relations - 0
	Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL

Getting FEA analyses.......
	Number of analyses - 1
	Analysis name - Default
	Done getting FEA analyses

Writing Nastran grid and connectivity file (in small field format) ....
Finished writing Nastran grid file

Writing subElement types (if any) - appending mesh file

Writing TACS instruction file....
	Writing analysis cards
	Writing load ADD cards
	Writing constraint ADD cards
	Writing load cards
	Writing constraint cards
	Writing material cards
	Writing property cards
	Writing design variable cards
Mapping Csys attributes ................
	Number of unique Csys attributes = 0

Getting FEA coordinate systems.......
	Number of coordinate systems - 0
	No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
	Number of unique capsConstraint attributes = 1
	Name = plateEdge, index = 1
Mapping capsLoad attributes ................
	Number of unique capsLoad attributes = 1
	Name = plate, index = 1
Mapping capsBound attributes ................
	Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
	Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
	Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
	Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
	Mesh for body = 0
	Number of nodal coordinates = 25
	Number of elements = 16
	Elemental Nodes = 0
	Elemental Rods  = 0
	Elemental Tria3 = 0
	Elemental Quad4 = 16

Getting FEA materials.......
	Number of materials - 1
	Material name - Madeupium
	Done getting FEA materials

Getting FEA properties.......
	Number of properties - 1
	Property name - plate
	Done getting FEA properties
Updating mesh element types based on properties input

Getting FEA constraints.......
	Number of constraints - 1
	Constraint name - edgeConstraint
	No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement"
	Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults

Getting FEA loads.......
	Number of loads - 1
	Load name - appliedPressure
	Done getting FEA loads

Getting FEA design variables.......
	Number of design variables          - 1
	Design_Variable name - plateWidth
	Number of design variable relations - 0
	Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL

Getting FEA analyses.......
	Number of analyses - 1
	Analysis name - Default
	Done getting FEA analyses

Writing Nastran grid and connectivity file (in small field format) ....
Finished writing Nastran grid file

Writing subElement types (if any) - appending mesh file

Writing TACS instruction file....
	Writing analysis cards
	Writing load ADD cards
	Writing constraint ADD cards
	Writing load cards
	Writing constraint cards
	Writing material cards
	Writing property cards
	Writing design variable cards
Mapping Csys attributes ................
	Number of unique Csys attributes = 0

Getting FEA coordinate systems.......
	Number of coordinate systems - 0
	No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
	Number of unique capsConstraint attributes = 1
	Name = plateEdge, index = 1
Mapping capsLoad attributes ................
	Number of unique capsLoad attributes = 1
	Name = plate, index = 1
Mapping capsBound attributes ................
	Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
	Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
	Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
	Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
	Mesh for body = 0
	Number of nodal coordinates = 25
	Number of elements = 16
	Elemental Nodes = 0
	Elemental Rods  = 0
	Elemental Tria3 = 0
	Elemental Quad4 = 16

Getting FEA materials.......
	Number of materials - 1
	Material name - Madeupium
	Done getting FEA materials

Getting FEA properties.......
	Number of properties - 1
	Property name - plate
	Done getting FEA properties
Updating mesh element types based on properties input

Getting FEA constraints.......
	Number of constraints - 1
	Constraint name - edgeConstraint
	No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement"
	Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults

Getting FEA loads.......
	Number of loads - 1
	Load name - appliedPressure
	Done getting FEA loads

Getting FEA design variables.......
	Number of design variables          - 1
	Design_Variable name - plateWidth
	Number of design variable relations - 0
	Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL

Getting FEA analyses.......
	Number of analyses - 1
	Analysis name - Default
	Done getting FEA analyses

Writing Nastran grid and connectivity file (in small field format) ....
Finished writing Nastran grid file

Writing subElement types (if any) - appending mesh file

Writing TACS instruction file....
	Writing analysis cards
	Writing load ADD cards
	Writing constraint ADD cards
	Writing load cards
	Writing constraint cards
	Writing material cards
	Writing property cards
	Writing design variable cards
Mapping Csys attributes ................
	Number of unique Csys attributes = 0

Getting FEA coordinate systems.......
	Number of coordinate systems - 0
	No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
	Number of unique capsConstraint attributes = 1
	Name = plateEdge, index = 1
Mapping capsLoad attributes ................
	Number of unique capsLoad attributes = 1
	Name = plate, index = 1
Mapping capsBound attributes ................
	Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
	Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
	Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
	Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
	Mesh for body = 0
	Number of nodal coordinates = 25
	Number of elements = 16
	Elemental Nodes = 0
	Elemental Rods  = 0
	Elemental Tria3 = 0
	Elemental Quad4 = 16

Getting FEA materials.......
	Number of materials - 1
	Material name - Madeupium
	Done getting FEA materials

Getting FEA properties.......
	Number of properties - 1
	Property name - plate
	Done getting FEA properties
Updating mesh element types based on properties input

Getting FEA constraints.......
	Number of constraints - 1
	Constraint name - edgeConstraint
	No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement"
	Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults

Getting FEA loads.......
	Number of loads - 1
	Load name - appliedPressure
	Done getting FEA loads

Getting FEA design variables.......
	Number of design variables          - 1
	Design_Variable name - plateWidth
	Number of design variable relations - 0
	Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL

Getting FEA analyses.......
	Number of analyses - 1
	Analysis name - Default
	Done getting FEA analyses

Writing Nastran grid and connectivity file (in small field format) ....
Finished writing Nastran grid file

Writing subElement types (if any) - appending mesh file

Writing TACS instruction file....
	Writing analysis cards
	Writing load ADD cards
	Writing constraint ADD cards
	Writing load cards
	Writing constraint cards
	Writing material cards
	Writing property cards
	Writing design variable cards
Mapping Csys attributes ................
	Number of unique Csys attributes = 0

Getting FEA coordinate systems.......
	Number of coordinate systems - 0
	No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
	Number of unique capsConstraint attributes = 1
	Name = plateEdge, index = 1
Mapping capsLoad attributes ................
	Number of unique capsLoad attributes = 1
	Name = plate, index = 1
Mapping capsBound attributes ................
	Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
	Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
	Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
	Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
	Mesh for body = 0
	Number of nodal coordinates = 25
	Number of elements = 16
	Elemental Nodes = 0
	Elemental Rods  = 0
	Elemental Tria3 = 0
	Elemental Quad4 = 16

Getting FEA materials.......
	Number of materials - 1
	Material name - Madeupium
	Done getting FEA materials

Getting FEA properties.......
	Number of properties - 1
	Property name - plate
	Done getting FEA properties
Updating mesh element types based on properties input

Getting FEA constraints.......
	Number of constraints - 1
	Constraint name - edgeConstraint
	No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement"
	Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults

Getting FEA loads.......
	Number of loads - 1
	Load name - appliedPressure
	Done getting FEA loads

Getting FEA design variables.......
	Number of design variables          - 1
	Design_Variable name - plateWidth
	Number of design variable relations - 0
	Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL

Getting FEA analyses.......
	Number of analyses - 1
	Analysis name - Default
	Done getting FEA analyses

Writing Nastran grid and connectivity file (in small field format) ....
Finished writing Nastran grid file

Writing subElement types (if any) - appending mesh file

Writing TACS instruction file....
	Writing analysis cards
	Writing load ADD cards
	Writing constraint ADD cards
	Writing load cards
	Writing constraint cards
	Writing material cards
	Writing property cards
	Writing design variable cards
Mapping Csys attributes ................
	Number of unique Csys attributes = 0

Getting FEA coordinate systems.......
	Number of coordinate systems - 0
	No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
	Number of unique capsConstraint attributes = 1
	Name = plateEdge, index = 1
Mapping capsLoad attributes ................
	Number of unique capsLoad attributes = 1
	Name = plate, index = 1
Mapping capsBound attributes ................
	Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
	Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
	Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
	Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
	Mesh for body = 0
	Number of nodal coordinates = 25
	Number of elements = 16
	Elemental Nodes = 0
	Elemental Rods  = 0
	Elemental Tria3 = 0
	Elemental Quad4 = 16

Getting FEA materials.......
	Number of materials - 1
	Material name - Madeupium
	Done getting FEA materials

Getting FEA properties.......
	Number of properties - 1
	Property name - plate
	Done getting FEA properties
Updating mesh element types based on properties input

Getting FEA constraints.......
	Number of constraints - 1
	Constraint name - edgeConstraint
	No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement"
	Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults

Getting FEA loads.......
	Number of loads - 1
	Load name - appliedPressure
	Done getting FEA loads

Getting FEA design variables.......
	Number of design variables          - 1
	Design_Variable name - plateWidth
	Number of design variable relations - 0
	Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL

Getting FEA analyses.......
	Number of analyses - 1
	Analysis name - Default
	Done getting FEA analyses

Writing Nastran grid and connectivity file (in small field format) ....
Finished writing Nastran grid file

Writing subElement types (if any) - appending mesh file

Writing TACS instruction file....
	Writing analysis cards
	Writing load ADD cards
	Writing constraint ADD cards
	Writing load cards
	Writing constraint cards
	Writing material cards
	Writing property cards
	Writing design variable cards
Mapping Csys attributes ................
	Number of unique Csys attributes = 0

Getting FEA coordinate systems.......
	Number of coordinate systems - 0
	No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
	Number of unique capsConstraint attributes = 1
	Name = plateEdge, index = 1
Mapping capsLoad attributes ................
	Number of unique capsLoad attributes = 1
	Name = plate, index = 1
Mapping capsBound attributes ................
	Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
	Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
	Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
	Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
	Mesh for body = 0
	Number of nodal coordinates = 25
	Number of elements = 16
	Elemental Nodes = 0
	Elemental Rods  = 0
	Elemental Tria3 = 0
	Elemental Quad4 = 16

Getting FEA materials.......
	Number of materials - 1
	Material name - Madeupium
	Done getting FEA materials

Getting FEA properties.......
	Number of properties - 1
	Property name - plate
	Done getting FEA properties
Updating mesh element types based on properties input

Getting FEA constraints.......
	Number of constraints - 1
	Constraint name - edgeConstraint
	No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement"
	Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults

Getting FEA loads.......
	Number of loads - 1
	Load name - appliedPressure
	Done getting FEA loads

Getting FEA design variables.......
	Number of design variables          - 1
	Design_Variable name - plateWidth
	Number of design variable relations - 0
	Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL

Getting FEA analyses.......
	Number of analyses - 1
	Analysis name - Default
	Done getting FEA analyses

Writing Nastran grid and connectivity file (in small field format) ....
Finished writing Nastran grid file

Writing subElement types (if any) - appending mesh file

Writing TACS instruction file....
	Writing analysis cards
	Writing load ADD cards
	Writing constraint ADD cards
	Writing load cards
	Writing constraint cards
	Writing material cards
	Writing property cards
	Writing design variable cards
Mapping Csys attributes ................
	Number of unique Csys attributes = 0

Getting FEA coordinate systems.......
	Number of coordinate systems - 0
	No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
	Number of unique capsConstraint attributes = 1
	Name = plateEdge, index = 1
Mapping capsLoad attributes ................
	Number of unique capsLoad attributes = 1
	Name = plate, index = 1
Mapping capsBound attributes ................
	Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
	Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
	Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
	Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
	Mesh for body = 0
	Number of nodal coordinates = 25
	Number of elements = 16
	Elemental Nodes = 0
	Elemental Rods  = 0
	Elemental Tria3 = 0
	Elemental Quad4 = 16

Getting FEA materials.......
	Number of materials - 1
	Material name - Madeupium
	Done getting FEA materials

Getting FEA properties.......
	Number of properties - 1
	Property name - plate
	Done getting FEA properties
Updating mesh element types based on properties input

Getting FEA constraints.......
	Number of constraints - 1
	Constraint name - edgeConstraint
	No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement"
	Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults

Getting FEA loads.......
	Number of loads - 1
	Load name - appliedPressure
	Done getting FEA loads

Getting FEA design variables.......
	Number of design variables          - 1
	Design_Variable name - plateWidth
	Number of design variable relations - 0
	Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL

Getting FEA analyses.......
	Number of analyses - 1
	Analysis name - Default
	Done getting FEA analyses

Writing Nastran grid and connectivity file (in small field format) ....
Finished writing Nastran grid file

Writing subElement types (if any) - appending mesh file

Writing TACS instruction file....
	Writing analysis cards
	Writing load ADD cards
	Writing constraint ADD cards
	Writing load cards
	Writing constraint cards
	Writing material cards
	Writing property cards
	Writing design variable cards
Mapping Csys attributes ................
	Number of unique Csys attributes = 0

Getting FEA coordinate systems.......
	Number of coordinate systems - 0
	No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
	Number of unique capsConstraint attributes = 1
	Name = plateEdge, index = 1
Mapping capsLoad attributes ................
	Number of unique capsLoad attributes = 1
	Name = plate, index = 1
Mapping capsBound attributes ................
	Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
	Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
	Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
	Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
	Mesh for body = 0
	Number of nodal coordinates = 25
	Number of elements = 16
	Elemental Nodes = 0
	Elemental Rods  = 0
	Elemental Tria3 = 0
	Elemental Quad4 = 16

Getting FEA materials.......
	Number of materials - 1
	Material name - Madeupium
	Done getting FEA materials

Getting FEA properties.......
	Number of properties - 1
	Property name - plate
	Done getting FEA properties
Updating mesh element types based on properties input

Getting FEA constraints.......
	Number of constraints - 1
	Constraint name - edgeConstraint
	No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement"
	Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults

Getting FEA loads.......
	Number of loads - 1
	Load name - appliedPressure
	Done getting FEA loads

Getting FEA design variables.......
	Number of design variables          - 1
	Design_Variable name - plateWidth
	Number of design variable relations - 0
	Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL

Getting FEA analyses.......
	Number of analyses - 1
	Analysis name - Default
	Done getting FEA analyses

Writing Nastran grid and connectivity file (in small field format) ....
Finished writing Nastran grid file

Writing subElement types (if any) - appending mesh file

Writing TACS instruction file....
	Writing analysis cards
	Writing load ADD cards
	Writing constraint ADD cards
	Writing load cards
	Writing constraint cards
	Writing material cards
	Writing property cards
	Writing design variable cards
Mapping Csys attributes ................
	Number of unique Csys attributes = 0

Getting FEA coordinate systems.......
	Number of coordinate systems - 0
	No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
	Number of unique capsConstraint attributes = 1
	Name = plateEdge, index = 1
Mapping capsLoad attributes ................
	Number of unique capsLoad attributes = 1
	Name = plate, index = 1
Mapping capsBound attributes ................
	Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
	Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
	Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
	Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
	Mesh for body = 0
	Number of nodal coordinates = 25
	Number of elements = 16
	Elemental Nodes = 0
	Elemental Rods  = 0
	Elemental Tria3 = 0
	Elemental Quad4 = 16

Getting FEA materials.......
	Number of materials - 1
	Material name - Madeupium
	Done getting FEA materials

Getting FEA properties.......
	Number of properties - 1
	Property name - plate
	Done getting FEA properties
Updating mesh element types based on properties input

Getting FEA constraints.......
	Number of constraints - 1
	Constraint name - edgeConstraint
	No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement"
	Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults

Getting FEA loads.......
	Number of loads - 1
	Load name - appliedPressure
	Done getting FEA loads

Getting FEA design variables.......
	Number of design variables          - 1
	Design_Variable name - plateWidth
	Number of design variable relations - 0
	Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL

Getting FEA analyses.......
	Number of analyses - 1
	Analysis name - Default
	Done getting FEA analyses

Writing Nastran grid and connectivity file (in small field format) ....
Finished writing Nastran grid file

Writing subElement types (if any) - appending mesh file

Writing TACS instruction file....
	Writing analysis cards
	Writing load ADD cards
	Writing constraint ADD cards
	Writing load cards
	Writing constraint cards
	Writing material cards
	Writing property cards
	Writing design variable cards
Mapping Csys attributes ................
	Number of unique Csys attributes = 0

Getting FEA coordinate systems.......
	Number of coordinate systems - 0
	No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
	Number of unique capsConstraint attributes = 1
	Name = plateEdge, index = 1
Mapping capsLoad attributes ................
	Number of unique capsLoad attributes = 1
	Name = plate, index = 1
Mapping capsBound attributes ................
	Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
	Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
	Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
	Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = plate, index = 1
Projecting tessellation 1 (of 1) on to new body
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
	Mesh for body = 0
	Number of nodal coordinates = 25
	Number of elements = 16
	Elemental Nodes = 0
	Elemental Rods  = 0
	Elemental Tria3 = 0
	Elemental Quad4 = 16

Getting FEA materials.......
	Number of materials - 1
	Material name - Madeupium
	Done getting FEA materials

Getting FEA properties.......
	Number of properties - 1
	Property name - plate
	Done getting FEA properties
Updating mesh element types based on properties input

Getting FEA constraints.......
	Number of constraints - 1
	Constraint name - edgeConstraint
	No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement"
	Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults

Getting FEA loads.......
	Number of loads - 1
	Load name - appliedPressure
	Done getting FEA loads

Getting FEA design variables.......
	Number of design variables          - 1
	Design_Variable name - plateWidth
	Number of design variable relations - 0
	Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL

Getting FEA analyses.......
	Number of analyses - 1
	Analysis name - Default
	Done getting FEA analyses

Writing Nastran grid and connectivity file (in small field format) ....
Finished writing Nastran grid file

Writing subElement types (if any) - appending mesh file

Writing TACS instruction file....
	Writing analysis cards
	Writing load ADD cards
	Writing constraint ADD cards
	Writing load cards
	Writing constraint cards
	Writing material cards
	Writing property cards
	Writing design variable cards
Mapping Csys attributes ................
	Number of unique Csys attributes = 0

Getting FEA coordinate systems.......
	Number of coordinate systems - 0
	No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
	Number of unique capsConstraint attributes = 1
	Name = plateEdge, index = 1
Mapping capsLoad attributes ................
	Number of unique capsLoad attributes = 1
	Name = plate, index = 1
Mapping capsBound attributes ................
	Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
	Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
	Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
	Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
	Mesh for body = 0
	Number of nodal coordinates = 25
	Number of elements = 16
	Elemental Nodes = 0
	Elemental Rods  = 0
	Elemental Tria3 = 0
	Elemental Quad4 = 16

Getting FEA materials.......
	Number of materials - 1
	Material name - Madeupium
	Done getting FEA materials

Getting FEA properties.......
	Number of properties - 1
	Property name - plate
	Done getting FEA properties
Updating mesh element types based on properties input

Getting FEA constraints.......
	Number of constraints - 1
	Constraint name - edgeConstraint
	No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement"
	Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults

Getting FEA loads.......
	Number of loads - 1
	Load name - appliedPressure
	Done getting FEA loads

Getting FEA design variables.......
	Number of design variables          - 1
	Design_Variable name - plateWidth
	Number of design variable relations - 0
	Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL

Getting FEA analyses.......
	Number of analyses - 1
	Analysis name - Default
	Done getting FEA analyses

Writing Nastran grid and connectivity file (in small field format) ....
Finished writing Nastran grid file

Writing subElement types (if any) - appending mesh file

Writing TACS instruction file....
	Writing analysis cards
	Writing load ADD cards
	Writing constraint ADD cards
	Writing load cards
	Writing constraint cards
	Writing material cards
	Writing property cards
	Writing design variable cards
Mapping Csys attributes ................
	Number of unique Csys attributes = 0

Getting FEA coordinate systems.......
	Number of coordinate systems - 0
	No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
	Number of unique capsConstraint attributes = 1
	Name = plateEdge, index = 1
Mapping capsLoad attributes ................
	Number of unique capsLoad attributes = 1
	Name = plate, index = 1
Mapping capsBound attributes ................
	Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
	Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
	Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
	Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
	Mesh for body = 0
	Number of nodal coordinates = 25
	Number of elements = 16
	Elemental Nodes = 0
	Elemental Rods  = 0
	Elemental Tria3 = 0
	Elemental Quad4 = 16

Getting FEA materials.......
	Number of materials - 1
	Material name - Madeupium
	Done getting FEA materials

Getting FEA properties.......
	Number of properties - 1
	Property name - plate
	Done getting FEA properties
Updating mesh element types based on properties input

Getting FEA constraints.......
	Number of constraints - 1
	Constraint name - edgeConstraint
	No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement"
	Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults

Getting FEA loads.......
	Number of loads - 1
	Load name - appliedPressure
	Done getting FEA loads

Getting FEA design variables.......
	Number of design variables          - 1
	Design_Variable name - plateWidth
	Number of design variable relations - 0
	Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL

Getting FEA analyses.......
	Number of analyses - 1
	Analysis name - Default
	Done getting FEA analyses

Writing Nastran grid and connectivity file (in small field format) ....
Finished writing Nastran grid file

Writing subElement types (if any) - appending mesh file

Writing TACS instruction file....
	Writing analysis cards
	Writing load ADD cards
	Writing constraint ADD cards
	Writing load cards
	Writing constraint cards
	Writing material cards
	Writing property cards
	Writing design variable cards
Mapping Csys attributes ................
	Number of unique Csys attributes = 0

Getting FEA coordinate systems.......
	Number of coordinate systems - 0
	No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
	Number of unique capsConstraint attributes = 1
	Name = plateEdge, index = 1
Mapping capsLoad attributes ................
	Number of unique capsLoad attributes = 1
	Name = plate, index = 1
Mapping capsBound attributes ................
	Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
	Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
	Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
	Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
	Mesh for body = 0
	Number of nodal coordinates = 25
	Number of elements = 16
	Elemental Nodes = 0
	Elemental Rods  = 0
	Elemental Tria3 = 0
	Elemental Quad4 = 16

Getting FEA materials.......
	Number of materials - 1
	Material name - Madeupium
	Done getting FEA materials

Getting FEA properties.......
	Number of properties - 1
	Property name - plate
	Done getting FEA properties
Updating mesh element types based on properties input

Getting FEA constraints.......
	Number of constraints - 1
	Constraint name - edgeConstraint
	No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement"
	Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults

Getting FEA loads.......
	Number of loads - 1
	Load name - appliedPressure
	Done getting FEA loads

Getting FEA design variables.......
	Number of design variables          - 1
	Design_Variable name - plateWidth
	Number of design variable relations - 0
	Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL

Getting FEA analyses.......
	Number of analyses - 1
	Analysis name - Default
	Done getting FEA analyses

Writing Nastran grid and connectivity file (in small field format) ....
Finished writing Nastran grid file

Writing subElement types (if any) - appending mesh file

Writing TACS instruction file....
	Writing analysis cards
	Writing load ADD cards
	Writing constraint ADD cards
	Writing load cards
	Writing constraint cards
	Writing material cards
	Writing property cards
	Writing design variable cards
Mapping Csys attributes ................
	Number of unique Csys attributes = 0

Getting FEA coordinate systems.......
	Number of coordinate systems - 0
	No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
	Number of unique capsConstraint attributes = 1
	Name = plateEdge, index = 1
Mapping capsLoad attributes ................
	Number of unique capsLoad attributes = 1
	Name = plate, index = 1
Mapping capsBound attributes ................
	Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
	Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
	Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
	Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
	Mesh for body = 0
	Number of nodal coordinates = 25
	Number of elements = 16
	Elemental Nodes = 0
	Elemental Rods  = 0
	Elemental Tria3 = 0
	Elemental Quad4 = 16

Getting FEA materials.......
	Number of materials - 1
	Material name - Madeupium
	Done getting FEA materials

Getting FEA properties.......
	Number of properties - 1
	Property name - plate
	Done getting FEA properties
Updating mesh element types based on properties input

Getting FEA constraints.......
	Number of constraints - 1
	Constraint name - edgeConstraint
	No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement"
	Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults

Getting FEA loads.......
	Number of loads - 1
	Load name - appliedPressure
	Done getting FEA loads

Getting FEA design variables.......
	Number of design variables          - 1
	Design_Variable name - plateWidth
	Number of design variable relations - 0
	Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL

Getting FEA analyses.......
	Number of analyses - 1
	Analysis name - Default
	Done getting FEA analyses

Writing Nastran grid and connectivity file (in small field format) ....
Finished writing Nastran grid file

Writing subElement types (if any) - appending mesh file

Writing TACS instruction file....
	Writing analysis cards
	Writing load ADD cards
	Writing constraint ADD cards
	Writing load cards
	Writing constraint cards
	Writing material cards
	Writing property cards
	Writing design variable cards
Mapping Csys attributes ................
	Number of unique Csys attributes = 0

Getting FEA coordinate systems.......
	Number of coordinate systems - 0
	No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
	Number of unique capsConstraint attributes = 1
	Name = plateEdge, index = 1
Mapping capsLoad attributes ................
	Number of unique capsLoad attributes = 1
	Name = plate, index = 1
Mapping capsBound attributes ................
	Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
	Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
	Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
	Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
	Mesh for body = 0
	Number of nodal coordinates = 25
	Number of elements = 16
	Elemental Nodes = 0
	Elemental Rods  = 0
	Elemental Tria3 = 0
	Elemental Quad4 = 16

Getting FEA materials.......
	Number of materials - 1
	Material name - Madeupium
	Done getting FEA materials

Getting FEA properties.......
	Number of properties - 1
	Property name - plate
	Done getting FEA properties
Updating mesh element types based on properties input

Getting FEA constraints.......
	Number of constraints - 1
	Constraint name - edgeConstraint
	No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement"
	Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults

Getting FEA loads.......
	Number of loads - 1
	Load name - appliedPressure
	Done getting FEA loads

Getting FEA design variables.......
	Number of design variables          - 1
	Design_Variable name - plateWidth
	Number of design variable relations - 0
	Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL

Getting FEA analyses.......
	Number of analyses - 1
	Analysis name - Default
	Done getting FEA analyses

Writing Nastran grid and connectivity file (in small field format) ....
Finished writing Nastran grid file

Writing subElement types (if any) - appending mesh file

Writing TACS instruction file....
	Writing analysis cards
	Writing load ADD cards
	Writing constraint ADD cards
	Writing load cards
	Writing constraint cards
	Writing material cards
	Writing property cards
	Writing design variable cards
Mapping Csys attributes ................
	Number of unique Csys attributes = 0

Getting FEA coordinate systems.......
	Number of coordinate systems - 0
	No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
	Number of unique capsConstraint attributes = 1
	Name = plateEdge, index = 1
Mapping capsLoad attributes ................
	Number of unique capsLoad attributes = 1
	Name = plate, index = 1
Mapping capsBound attributes ................
	Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
	Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
	Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
	Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
	Mesh for body = 0
	Number of nodal coordinates = 25
	Number of elements = 16
	Elemental Nodes = 0
	Elemental Rods  = 0
	Elemental Tria3 = 0
	Elemental Quad4 = 16

Getting FEA materials.......
	Number of materials - 1
	Material name - Madeupium
	Done getting FEA materials

Getting FEA properties.......
	Number of properties - 1
	Property name - plate
	Done getting FEA properties
Updating mesh element types based on properties input

Getting FEA constraints.......
	Number of constraints - 1
	Constraint name - edgeConstraint
	No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement"
	Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults

Getting FEA loads.......
	Number of loads - 1
	Load name - appliedPressure
	Done getting FEA loads

Getting FEA design variables.......
	Number of design variables          - 1
	Design_Variable name - plateWidth
	Number of design variable relations - 0
	Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL

Getting FEA analyses.......
	Number of analyses - 1
	Analysis name - Default
	Done getting FEA analyses

Writing Nastran grid and connectivity file (in small field format) ....
Finished writing Nastran grid file

Writing subElement types (if any) - appending mesh file

Writing TACS instruction file....
	Writing analysis cards
	Writing load ADD cards
	Writing constraint ADD cards
	Writing load cards
	Writing constraint cards
	Writing material cards
	Writing property cards
	Writing design variable cards
Mapping Csys attributes ................
	Number of unique Csys attributes = 0

Getting FEA coordinate systems.......
	Number of coordinate systems - 0
	No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
	Number of unique capsConstraint attributes = 1
	Name = plateEdge, index = 1
Mapping capsLoad attributes ................
	Number of unique capsLoad attributes = 1
	Name = plate, index = 1
Mapping capsBound attributes ................
	Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
	Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
	Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
	Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
	Mesh for body = 0
	Number of nodal coordinates = 25
	Number of elements = 16
	Elemental Nodes = 0
	Elemental Rods  = 0
	Elemental Tria3 = 0
	Elemental Quad4 = 16

Getting FEA materials.......
	Number of materials - 1
	Material name - Madeupium
	Done getting FEA materials

Getting FEA properties.......
	Number of properties - 1
	Property name - plate
	Done getting FEA properties
Updating mesh element types based on properties input

Getting FEA constraints.......
	Number of constraints - 1
	Constraint name - edgeConstraint
	No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement"
	Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults

Getting FEA loads.......
	Number of loads - 1
	Load name - appliedPressure
	Done getting FEA loads

Getting FEA design variables.......
	Number of design variables          - 1
	Design_Variable name - plateWidth
	Number of design variable relations - 0
	Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL

Getting FEA analyses.......
	Number of analyses - 1
	Analysis name - Default
	Done getting FEA analyses

Writing Nastran grid and connectivity file (in small field format) ....
Finished writing Nastran grid file

Writing subElement types (if any) - appending mesh file

Writing TACS instruction file....
	Writing analysis cards
	Writing load ADD cards
	Writing constraint ADD cards
	Writing load cards
	Writing constraint cards
	Writing material cards
	Writing property cards
	Writing design variable cards
Mapping Csys attributes ................
	Number of unique Csys attributes = 0

Getting FEA coordinate systems.......
	Number of coordinate systems - 0
	No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
	Number of unique capsConstraint attributes = 1
	Name = plateEdge, index = 1
Mapping capsLoad attributes ................
	Number of unique capsLoad attributes = 1
	Name = plate, index = 1
Mapping capsBound attributes ................
	Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
	Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
	Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
	Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
	Mesh for body = 0
	Number of nodal coordinates = 25
	Number of elements = 16
	Elemental Nodes = 0
	Elemental Rods  = 0
	Elemental Tria3 = 0
	Elemental Quad4 = 16

Getting FEA materials.......
	Number of materials - 1
	Material name - Madeupium
	Done getting FEA materials

Getting FEA properties.......
	Number of properties - 1
	Property name - plate
	Done getting FEA properties
Updating mesh element types based on properties input

Getting FEA constraints.......
	Number of constraints - 1
	Constraint name - edgeConstraint
	No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement"
	Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults

Getting FEA loads.......
	Number of loads - 1
	Load name - appliedPressure
	Done getting FEA loads

Getting FEA design variables.......
	Number of design variables          - 1
	Design_Variable name - plateWidth
	Number of design variable relations - 0
	Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL

Getting FEA analyses.......
	Number of analyses - 1
	Analysis name - Default
	Done getting FEA analyses

Writing Nastran grid and connectivity file (in small field format) ....
Finished writing Nastran grid file

Writing subElement types (if any) - appending mesh file

Writing TACS instruction file....
	Writing analysis cards
	Writing load ADD cards
	Writing constraint ADD cards
	Writing load cards
	Writing constraint cards
	Writing material cards
	Writing property cards
	Writing design variable cards
Mapping Csys attributes ................
	Number of unique Csys attributes = 0

Getting FEA coordinate systems.......
	Number of coordinate systems - 0
	No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
	Number of unique capsConstraint attributes = 1
	Name = plateEdge, index = 1
Mapping capsLoad attributes ................
	Number of unique capsLoad attributes = 1
	Name = plate, index = 1
Mapping capsBound attributes ................
	Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
	Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
	Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
	Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
	Mesh for body = 0
	Number of nodal coordinates = 25
	Number of elements = 16
	Elemental Nodes = 0
	Elemental Rods  = 0
	Elemental Tria3 = 0
	Elemental Quad4 = 16

Getting FEA materials.......
	Number of materials - 1
	Material name - Madeupium
	Done getting FEA materials

Getting FEA properties.......
	Number of properties - 1
	Property name - plate
	Done getting FEA properties
Updating mesh element types based on properties input

Getting FEA constraints.......
	Number of constraints - 1
	Constraint name - edgeConstraint
	No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement"
	Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults

Getting FEA loads.......
	Number of loads - 1
	Load name - appliedPressure
	Done getting FEA loads

Getting FEA design variables.......
	Number of design variables          - 1
	Design_Variable name - plateWidth
	Number of design variable relations - 0
	Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL

Getting FEA analyses.......
	Number of analyses - 1
	Analysis name - Default
	Done getting FEA analyses

Writing Nastran grid and connectivity file (in small field format) ....
Finished writing Nastran grid file

Writing subElement types (if any) - appending mesh file

Writing TACS instruction file....
	Writing analysis cards
	Writing load ADD cards
	Writing constraint ADD cards
	Writing load cards
	Writing constraint cards
	Writing material cards
	Writing property cards
	Writing design variable cards
Mapping Csys attributes ................
	Number of unique Csys attributes = 0

Getting FEA coordinate systems.......
	Number of coordinate systems - 0
	No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
	Number of unique capsConstraint attributes = 1
	Name = plateEdge, index = 1
Mapping capsLoad attributes ................
	Number of unique capsLoad attributes = 1
	Name = plate, index = 1
Mapping capsBound attributes ................
	Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
	Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
	Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
	Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
	Mesh for body = 0
	Number of nodal coordinates = 25
	Number of elements = 16
	Elemental Nodes = 0
	Elemental Rods  = 0
	Elemental Tria3 = 0
	Elemental Quad4 = 16

Getting FEA materials.......
	Number of materials - 1
	Material name - Madeupium
	Done getting FEA materials

Getting FEA properties.......
	Number of properties - 1
	Property name - plate
	Done getting FEA properties
Updating mesh element types based on properties input

Getting FEA constraints.......
	Number of constraints - 1
	Constraint name - edgeConstraint
	No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement"
	Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults

Getting FEA loads.......
	Number of loads - 1
	Load name - appliedPressure
	Done getting FEA loads

Getting FEA design variables.......
	Number of design variables          - 1
	Design_Variable name - plateWidth
	Number of design variable relations - 0
	Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL

Getting FEA analyses.......
	Number of analyses - 1
	Analysis name - Default
	Done getting FEA analyses

Writing Nastran grid and connectivity file (in small field format) ....
Finished writing Nastran grid file

Writing subElement types (if any) - appending mesh file

Writing TACS instruction file....
	Writing analysis cards
	Writing load ADD cards
	Writing constraint ADD cards
	Writing load cards
	Writing constraint cards
	Writing material cards
	Writing property cards
	Writing design variable cards
Mapping Csys attributes ................
	Number of unique Csys attributes = 0

Getting FEA coordinate systems.......
	Number of coordinate systems - 0
	No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
	Number of unique capsConstraint attributes = 1
	Name = plateEdge, index = 1
Mapping capsLoad attributes ................
	Number of unique capsLoad attributes = 1
	Name = plate, index = 1
Mapping capsBound attributes ................
	Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
	Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
	Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
	Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
	Mesh for body = 0
	Number of nodal coordinates = 25
	Number of elements = 16
	Elemental Nodes = 0
	Elemental Rods  = 0
	Elemental Tria3 = 0
	Elemental Quad4 = 16

Getting FEA materials.......
	Number of materials - 1
	Material name - Madeupium
	Done getting FEA materials

Getting FEA properties.......
	Number of properties - 1
	Property name - plate
	Done getting FEA properties
Updating mesh element types based on properties input

Getting FEA constraints.......
	Number of constraints - 1
	Constraint name - edgeConstraint
	No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement"
	Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults

Getting FEA loads.......
	Number of loads - 1
	Load name - appliedPressure
	Done getting FEA loads

Getting FEA design variables.......
	Number of design variables          - 1
	Design_Variable name - plateWidth
	Number of design variable relations - 0
	Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL

Getting FEA analyses.......
	Number of analyses - 1
	Analysis name - Default
	Done getting FEA analyses

Writing Nastran grid and connectivity file (in small field format) ....
Finished writing Nastran grid file

Writing subElement types (if any) - appending mesh file

Writing TACS instruction file....
	Writing analysis cards
	Writing load ADD cards
	Writing constraint ADD cards
	Writing load cards
	Writing constraint cards
	Writing material cards
	Writing property cards
	Writing design variable cards
Mapping Csys attributes ................
	Number of unique Csys attributes = 0

Getting FEA coordinate systems.......
	Number of coordinate systems - 0
	No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
	Number of unique capsConstraint attributes = 1
	Name = plateEdge, index = 1
Mapping capsLoad attributes ................
	Number of unique capsLoad attributes = 1
	Name = plate, index = 1
Mapping capsBound attributes ................
	Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
	Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
	Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
	Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
	Mesh for body = 0
	Number of nodal coordinates = 25
	Number of elements = 16
	Elemental Nodes = 0
	Elemental Rods  = 0
	Elemental Tria3 = 0
	Elemental Quad4 = 16

Getting FEA materials.......
	Number of materials - 1
	Material name - Madeupium
	Done getting FEA materials

Getting FEA properties.......
	Number of properties - 1
	Property name - plate
	Done getting FEA properties
Updating mesh element types based on properties input

Getting FEA constraints.......
	Number of constraints - 1
	Constraint name - edgeConstraint
	No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement"
	Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults

Getting FEA loads.......
	Number of loads - 1
	Load name - appliedPressure
	Done getting FEA loads

Getting FEA design variables.......
	Number of design variables          - 1
	Design_Variable name - plateWidth
	Number of design variable relations - 0
	Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL

Getting FEA analyses.......
	Number of analyses - 1
	Analysis name - Default
	Done getting FEA analyses

Writing Nastran grid and connectivity file (in small field format) ....
Finished writing Nastran grid file

Writing subElement types (if any) - appending mesh file

Writing TACS instruction file....
	Writing analysis cards
	Writing load ADD cards
	Writing constraint ADD cards
	Writing load cards
	Writing constraint cards
	Writing material cards
	Writing property cards
	Writing design variable cards
Mapping Csys attributes ................
	Number of unique Csys attributes = 0

Getting FEA coordinate systems.......
	Number of coordinate systems - 0
	No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
	Number of unique capsConstraint attributes = 1
	Name = plateEdge, index = 1
Mapping capsLoad attributes ................
	Number of unique capsLoad attributes = 1
	Name = plate, index = 1
Mapping capsBound attributes ................
	Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
	Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
	Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
	Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
	Mesh for body = 0
	Number of nodal coordinates = 25
	Number of elements = 16
	Elemental Nodes = 0
	Elemental Rods  = 0
	Elemental Tria3 = 0
	Elemental Quad4 = 16

Getting FEA materials.......
	Number of materials - 1
	Material name - Madeupium
	Done getting FEA materials

Getting FEA properties.......
	Number of properties - 1
	Property name - plate
	Done getting FEA properties
Updating mesh element types based on properties input

Getting FEA constraints.......
	Number of constraints - 1
	Constraint name - edgeConstraint
	No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement"
	Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults

Getting FEA loads.......
	Number of loads - 1
	Load name - appliedPressure
	Done getting FEA loads

Getting FEA design variables.......
	Number of design variables          - 1
	Design_Variable name - plateWidth
	Number of design variable relations - 0
	Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL

Getting FEA analyses.......
	Number of analyses - 1
	Analysis name - Default
	Done getting FEA analyses

Writing Nastran grid and connectivity file (in small field format) ....
Finished writing Nastran grid file

Writing subElement types (if any) - appending mesh file

Writing TACS instruction file....
	Writing analysis cards
	Writing load ADD cards
	Writing constraint ADD cards
	Writing load cards
	Writing constraint cards
	Writing material cards
	Writing property cards
	Writing design variable cards
Mapping Csys attributes ................
	Number of unique Csys attributes = 0

Getting FEA coordinate systems.......
	Number of coordinate systems - 0
	No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
	Number of unique capsConstraint attributes = 1
	Name = plateEdge, index = 1
Mapping capsLoad attributes ................
	Number of unique capsLoad attributes = 1
	Name = plate, index = 1
Mapping capsBound attributes ................
	Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
	Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
	Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
	Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
	Mesh for body = 0
	Number of nodal coordinates = 25
	Number of elements = 16
	Elemental Nodes = 0
	Elemental Rods  = 0
	Elemental Tria3 = 0
	Elemental Quad4 = 16

Getting FEA materials.......
	Number of materials - 1
	Material name - Madeupium
	Done getting FEA materials

Getting FEA properties.......
	Number of properties - 1
	Property name - plate
	Done getting FEA properties
Updating mesh element types based on properties input

Getting FEA constraints.......
	Number of constraints - 1
	Constraint name - edgeConstraint
	No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement"
	Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults

Getting FEA loads.......
	Number of loads - 1
	Load name - appliedPressure
	Done getting FEA loads

Getting FEA design variables.......
	Number of design variables          - 1
	Design_Variable name - plateWidth
	Number of design variable relations - 0
	Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL

Getting FEA analyses.......
	Number of analyses - 1
	Analysis name - Default
	Done getting FEA analyses

Writing Nastran grid and connectivity file (in small field format) ....
Finished writing Nastran grid file

Writing subElement types (if any) - appending mesh file

Writing TACS instruction file....
	Writing analysis cards
	Writing load ADD cards
	Writing constraint ADD cards
	Writing load cards
	Writing constraint cards
	Writing material cards
	Writing property cards
	Writing design variable cards
Mapping Csys attributes ................
	Number of unique Csys attributes = 0

Getting FEA coordinate systems.......
	Number of coordinate systems - 0
	No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
	Number of unique capsConstraint attributes = 1
	Name = plateEdge, index = 1
Mapping capsLoad attributes ................
	Number of unique capsLoad attributes = 1
	Name = plate, index = 1
Mapping capsBound attributes ................
	Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
	Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
	Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
	Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
	Mesh for body = 0
	Number of nodal coordinates = 25
	Number of elements = 16
	Elemental Nodes = 0
	Elemental Rods  = 0
	Elemental Tria3 = 0
	Elemental Quad4 = 16

Getting FEA materials.......
	Number of materials - 1
	Material name - Madeupium
	Done getting FEA materials

Getting FEA properties.......
	Number of properties - 1
	Property name - plate
	Done getting FEA properties
Updating mesh element types based on properties input

Getting FEA constraints.......
	Number of constraints - 1
	Constraint name - edgeConstraint
	No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement"
	Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults

Getting FEA loads.......
	Number of loads - 1
	Load name - appliedPressure
	Done getting FEA loads

Getting FEA design variables.......
	Number of design variables          - 1
	Design_Variable name - plateWidth
	Number of design variable relations - 0
	Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL

Getting FEA analyses.......
	Number of analyses - 1
	Analysis name - Default
	Done getting FEA analyses

Writing Nastran grid and connectivity file (in small field format) ....
Finished writing Nastran grid file

Writing subElement types (if any) - appending mesh file

Writing TACS instruction file....
	Writing analysis cards
	Writing load ADD cards
	Writing constraint ADD cards
	Writing load cards
	Writing constraint cards
	Writing material cards
	Writing property cards
	Writing design variable cards
Mapping Csys attributes ................
	Number of unique Csys attributes = 0

Getting FEA coordinate systems.......
	Number of coordinate systems - 0
	No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
	Number of unique capsConstraint attributes = 1
	Name = plateEdge, index = 1
Mapping capsLoad attributes ................
	Number of unique capsLoad attributes = 1
	Name = plate, index = 1
Mapping capsBound attributes ................
	Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
	Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
	Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
	Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
	Mesh for body = 0
	Number of nodal coordinates = 25
	Number of elements = 16
	Elemental Nodes = 0
	Elemental Rods  = 0
	Elemental Tria3 = 0
	Elemental Quad4 = 16

Getting FEA materials.......
	Number of materials - 1
	Material name - Madeupium
	Done getting FEA materials

Getting FEA properties.......
	Number of properties - 1
	Property name - plate
	Done getting FEA properties
Updating mesh element types based on properties input

Getting FEA constraints.......
	Number of constraints - 1
	Constraint name - edgeConstraint
	No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement"
	Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults

Getting FEA loads.......
	Number of loads - 1
	Load name - appliedPressure
	Done getting FEA loads

Getting FEA design variables.......
	Number of design variables          - 1
	Design_Variable name - plateWidth
	Number of design variable relations - 0
	Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL

Getting FEA analyses.......
	Number of analyses - 1
	Analysis name - Default
	Done getting FEA analyses

Writing Nastran grid and connectivity file (in small field format) ....
Finished writing Nastran grid file

Writing subElement types (if any) - appending mesh file

Writing TACS instruction file....
	Writing analysis cards
	Writing load ADD cards
	Writing constraint ADD cards
	Writing load cards
	Writing constraint cards
	Writing material cards
	Writing property cards
	Writing design variable cards
Mapping Csys attributes ................
	Number of unique Csys attributes = 0

Getting FEA coordinate systems.......
	Number of coordinate systems - 0
	No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
	Number of unique capsConstraint attributes = 1
	Name = plateEdge, index = 1
Mapping capsLoad attributes ................
	Number of unique capsLoad attributes = 1
	Name = plate, index = 1
Mapping capsBound attributes ................
	Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
	Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
	Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
	Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
	Mesh for body = 0
	Number of nodal coordinates = 25
	Number of elements = 16
	Elemental Nodes = 0
	Elemental Rods  = 0
	Elemental Tria3 = 0
	Elemental Quad4 = 16

Getting FEA materials.......
	Number of materials - 1
	Material name - Madeupium
	Done getting FEA materials

Getting FEA properties.......
	Number of properties - 1
	Property name - plate
	Done getting FEA properties
Updating mesh element types based on properties input

Getting FEA constraints.......
	Number of constraints - 1
	Constraint name - edgeConstraint
	No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement"
	Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults

Getting FEA loads.......
	Number of loads - 1
	Load name - appliedPressure
	Done getting FEA loads

Getting FEA design variables.......
	Number of design variables          - 1
	Design_Variable name - plateWidth
	Number of design variable relations - 0
	Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL

Getting FEA analyses.......
	Number of analyses - 1
	Analysis name - Default
	Done getting FEA analyses

Writing Nastran grid and connectivity file (in small field format) ....
Finished writing Nastran grid file

Writing subElement types (if any) - appending mesh file

Writing TACS instruction file....
	Writing analysis cards
	Writing load ADD cards
	Writing constraint ADD cards
	Writing load cards
	Writing constraint cards
	Writing material cards
	Writing property cards
	Writing design variable cards
Mapping Csys attributes ................
	Number of unique Csys attributes = 0

Getting FEA coordinate systems.......
	Number of coordinate systems - 0
	No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
	Number of unique capsConstraint attributes = 1
	Name = plateEdge, index = 1
Mapping capsLoad attributes ................
	Number of unique capsLoad attributes = 1
	Name = plate, index = 1
Mapping capsBound attributes ................
	Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
	Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
	Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
	Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
	Mesh for body = 0
	Number of nodal coordinates = 25
	Number of elements = 16
	Elemental Nodes = 0
	Elemental Rods  = 0
	Elemental Tria3 = 0
	Elemental Quad4 = 16

Getting FEA materials.......
	Number of materials - 1
	Material name - Madeupium
	Done getting FEA materials

Getting FEA properties.......
	Number of properties - 1
	Property name - plate
	Done getting FEA properties
Updating mesh element types based on properties input

Getting FEA constraints.......
	Number of constraints - 1
	Constraint name - edgeConstraint
	No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement"
	Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults

Getting FEA loads.......
	Number of loads - 1
	Load name - appliedPressure
	Done getting FEA loads

Getting FEA design variables.......
	Number of design variables          - 1
	Design_Variable name - plateWidth
	Number of design variable relations - 0
	Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL

Getting FEA analyses.......
	Number of analyses - 1
	Analysis name - Default
	Done getting FEA analyses

Writing Nastran grid and connectivity file (in small field format) ....
Finished writing Nastran grid file

Writing subElement types (if any) - appending mesh file

Writing TACS instruction file....
	Writing analysis cards
	Writing load ADD cards
	Writing constraint ADD cards
	Writing load cards
	Writing constraint cards
	Writing material cards
	Writing property cards
	Writing design variable cards
Mapping Csys attributes ................
	Number of unique Csys attributes = 0

Getting FEA coordinate systems.......
	Number of coordinate systems - 0
	No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
	Number of unique capsConstraint attributes = 1
	Name = plateEdge, index = 1
Mapping capsLoad attributes ................
	Number of unique capsLoad attributes = 1
	Name = plate, index = 1
Mapping capsBound attributes ................
	Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
	Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
	Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
	Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
	Mesh for body = 0
	Number of nodal coordinates = 25
	Number of elements = 16
	Elemental Nodes = 0
	Elemental Rods  = 0
	Elemental Tria3 = 0
	Elemental Quad4 = 16

Getting FEA materials.......
	Number of materials - 1
	Material name - Madeupium
	Done getting FEA materials

Getting FEA properties.......
	Number of properties - 1
	Property name - plate
	Done getting FEA properties
Updating mesh element types based on properties input

Getting FEA constraints.......
	Number of constraints - 1
	Constraint name - edgeConstraint
	No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement"
	Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults

Getting FEA loads.......
	Number of loads - 1
	Load name - appliedPressure
	Done getting FEA loads

Getting FEA design variables.......
	Number of design variables          - 1
	Design_Variable name - plateWidth
	Number of design variable relations - 0
	Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL

Getting FEA analyses.......
	Number of analyses - 1
	Analysis name - Default
	Done getting FEA analyses

Writing Nastran grid and connectivity file (in small field format) ....
Finished writing Nastran grid file

Writing subElement types (if any) - appending mesh file

Writing TACS instruction file....
	Writing analysis cards
	Writing load ADD cards
	Writing constraint ADD cards
	Writing load cards
	Writing constraint cards
	Writing material cards
	Writing property cards
	Writing design variable cards
Mapping Csys attributes ................
	Number of unique Csys attributes = 0

Getting FEA coordinate systems.......
	Number of coordinate systems - 0
	No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
	Number of unique capsConstraint attributes = 1
	Name = plateEdge, index = 1
Mapping capsLoad attributes ................
	Number of unique capsLoad attributes = 1
	Name = plate, index = 1
Mapping capsBound attributes ................
	Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
	Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
	Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
	Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
	Mesh for body = 0
	Number of nodal coordinates = 25
	Number of elements = 16
	Elemental Nodes = 0
	Elemental Rods  = 0
	Elemental Tria3 = 0
	Elemental Quad4 = 16

Getting FEA materials.......
	Number of materials - 1
	Material name - Madeupium
	Done getting FEA materials

Getting FEA properties.......
	Number of properties - 1
	Property name - plate
	Done getting FEA properties
Updating mesh element types based on properties input

Getting FEA constraints.......
	Number of constraints - 1
	Constraint name - edgeConstraint
	No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement"
	Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults

Getting FEA loads.......
	Number of loads - 1
	Load name - appliedPressure
	Done getting FEA loads

Getting FEA design variables.......
	Number of design variables          - 1
	Design_Variable name - plateWidth
	Number of design variable relations - 0
	Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL

Getting FEA analyses.......
	Number of analyses - 1
	Analysis name - Default
	Done getting FEA analyses

Writing Nastran grid and connectivity file (in small field format) ....
Finished writing Nastran grid file

Writing subElement types (if any) - appending mesh file

Writing TACS instruction file....
	Writing analysis cards
	Writing load ADD cards
	Writing constraint ADD cards
	Writing load cards
	Writing constraint cards
	Writing material cards
	Writing property cards
	Writing design variable cards
Mapping Csys attributes ................
	Number of unique Csys attributes = 0

Getting FEA coordinate systems.......
	Number of coordinate systems - 0
	No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
	Number of unique capsConstraint attributes = 1
	Name = plateEdge, index = 1
Mapping capsLoad attributes ................
	Number of unique capsLoad attributes = 1
	Name = plate, index = 1
Mapping capsBound attributes ................
	Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
	Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
	Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
	Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
	Mesh for body = 0
	Number of nodal coordinates = 25
	Number of elements = 16
	Elemental Nodes = 0
	Elemental Rods  = 0
	Elemental Tria3 = 0
	Elemental Quad4 = 16

Getting FEA materials.......
	Number of materials - 1
	Material name - Madeupium
	Done getting FEA materials

Getting FEA properties.......
	Number of properties - 1
	Property name - plate
	Done getting FEA properties
Updating mesh element types based on properties input

Getting FEA constraints.......
	Number of constraints - 1
	Constraint name - edgeConstraint
	No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement"
	Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults

Getting FEA loads.......
	Number of loads - 1
	Load name - appliedPressure
	Done getting FEA loads

Getting FEA design variables.......
	Number of design variables          - 1
	Design_Variable name - plateWidth
	Number of design variable relations - 0
	Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL

Getting FEA analyses.......
	Number of analyses - 1
	Analysis name - Default
	Done getting FEA analyses

Writing Nastran grid and connectivity file (in small field format) ....
Finished writing Nastran grid file

Writing subElement types (if any) - appending mesh file

Writing TACS instruction file....
	Writing analysis cards
	Writing load ADD cards
	Writing constraint ADD cards
	Writing load cards
	Writing constraint cards
	Writing material cards
	Writing property cards
	Writing design variable cards
Mapping Csys attributes ................
	Number of unique Csys attributes = 0

Getting FEA coordinate systems.......
	Number of coordinate systems - 0
	No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
	Number of unique capsConstraint attributes = 1
	Name = plateEdge, index = 1
Mapping capsLoad attributes ................
	Number of unique capsLoad attributes = 1
	Name = plate, index = 1
Mapping capsBound attributes ................
	Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
	Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
	Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
	Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
	Mesh for body = 0
	Number of nodal coordinates = 25
	Number of elements = 16
	Elemental Nodes = 0
	Elemental Rods  = 0
	Elemental Tria3 = 0
	Elemental Quad4 = 16

Getting FEA materials.......
	Number of materials - 1
	Material name - Madeupium
	Done getting FEA materials

Getting FEA properties.......
	Number of properties - 1
	Property name - plate
	Done getting FEA properties
Updating mesh element types based on properties input

Getting FEA constraints.......
	Number of constraints - 1
	Constraint name - edgeConstraint
	No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement"
	Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults

Getting FEA loads.......
	Number of loads - 1
	Load name - appliedPressure
	Done getting FEA loads

Getting FEA design variables.......
	Number of design variables          - 1
	Design_Variable name - plateWidth
	Number of design variable relations - 0
	Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL

Getting FEA analyses.......
	Number of analyses - 1
	Analysis name - Default
	Done getting FEA analyses

Writing Nastran grid and connectivity file (in small field format) ....
Finished writing Nastran grid file

Writing subElement types (if any) - appending mesh file

Writing TACS instruction file....
	Writing analysis cards
	Writing load ADD cards
	Writing constraint ADD cards
	Writing load cards
	Writing constraint cards
	Writing material cards
	Writing property cards
	Writing design variable cards
Mapping Csys attributes ................
	Number of unique Csys attributes = 0

Getting FEA coordinate systems.......
	Number of coordinate systems - 0
	No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
	Number of unique capsConstraint attributes = 1
	Name = plateEdge, index = 1
Mapping capsLoad attributes ................
	Number of unique capsLoad attributes = 1
	Name = plate, index = 1
Mapping capsBound attributes ................
	Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
	Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
	Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
	Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
	Mesh for body = 0
	Number of nodal coordinates = 25
	Number of elements = 16
	Elemental Nodes = 0
	Elemental Rods  = 0
	Elemental Tria3 = 0
	Elemental Quad4 = 16

Getting FEA materials.......
	Number of materials - 1
	Material name - Madeupium
	Done getting FEA materials

Getting FEA properties.......
	Number of properties - 1
	Property name - plate
	Done getting FEA properties
Updating mesh element types based on properties input

Getting FEA constraints.......
	Number of constraints - 1
	Constraint name - edgeConstraint
	No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement"
	Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults

Getting FEA loads.......
	Number of loads - 1
	Load name - appliedPressure
	Done getting FEA loads

Getting FEA design variables.......
	Number of design variables          - 1
	Design_Variable name - plateWidth
	Number of design variable relations - 0
	Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL

Getting FEA analyses.......
	Number of analyses - 1
	Analysis name - Default
	Done getting FEA analyses

Writing Nastran grid and connectivity file (in small field format) ....
Finished writing Nastran grid file

Writing subElement types (if any) - appending mesh file

Writing TACS instruction file....
	Writing analysis cards
	Writing load ADD cards
	Writing constraint ADD cards
	Writing load cards
	Writing constraint cards
	Writing material cards
	Writing property cards
	Writing design variable cards
Mapping Csys attributes ................
	Number of unique Csys attributes = 0

Getting FEA coordinate systems.......
	Number of coordinate systems - 0
	No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
	Number of unique capsConstraint attributes = 1
	Name = plateEdge, index = 1
Mapping capsLoad attributes ................
	Number of unique capsLoad attributes = 1
	Name = plate, index = 1
Mapping capsBound attributes ................
	Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
	Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
	Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
	Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
	Mesh for body = 0
	Number of nodal coordinates = 25
	Number of elements = 16
	Elemental Nodes = 0
	Elemental Rods  = 0
	Elemental Tria3 = 0
	Elemental Quad4 = 16

Getting FEA materials.......
	Number of materials - 1
	Material name - Madeupium
	Done getting FEA materials

Getting FEA properties.......
	Number of properties - 1
	Property name - plate
	Done getting FEA properties
Updating mesh element types based on properties input

Getting FEA constraints.......
	Number of constraints - 1
	Constraint name - edgeConstraint
	No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement"
	Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults

Getting FEA loads.......
	Number of loads - 1
	Load name - appliedPressure
	Done getting FEA loads

Getting FEA design variables.......
	Number of design variables          - 1
	Design_Variable name - plateWidth
	Number of design variable relations - 0
	Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL

Getting FEA analyses.......
	Number of analyses - 1
	Analysis name - Default
	Done getting FEA analyses

Writing Nastran grid and connectivity file (in small field format) ....
Finished writing Nastran grid file

Writing subElement types (if any) - appending mesh file

Writing TACS instruction file....
	Writing analysis cards
	Writing load ADD cards
	Writing constraint ADD cards
	Writing load cards
	Writing constraint cards
	Writing material cards
	Writing property cards
	Writing design variable cards
Mapping Csys attributes ................
	Number of unique Csys attributes = 0

Getting FEA coordinate systems.......
	Number of coordinate systems - 0
	No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
	Number of unique capsConstraint attributes = 1
	Name = plateEdge, index = 1
Mapping capsLoad attributes ................
	Number of unique capsLoad attributes = 1
	Name = plate, index = 1
Mapping capsBound attributes ................
	Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
	Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
	Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
	Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
	Mesh for body = 0
	Number of nodal coordinates = 25
	Number of elements = 16
	Elemental Nodes = 0
	Elemental Rods  = 0
	Elemental Tria3 = 0
	Elemental Quad4 = 16

Getting FEA materials.......
	Number of materials - 1
	Material name - Madeupium
	Done getting FEA materials

Getting FEA properties.......
	Number of properties - 1
	Property name - plate
	Done getting FEA properties
Updating mesh element types based on properties input

Getting FEA constraints.......
	Number of constraints - 1
	Constraint name - edgeConstraint
	No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement"
	Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults

Getting FEA loads.......
	Number of loads - 1
	Load name - appliedPressure
	Done getting FEA loads

Getting FEA design variables.......
	Number of design variables          - 1
	Design_Variable name - thick1
	Design_Variable_Relation name - thick1
	Number of design variable relations - 1
	Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL

Getting FEA analyses.......
	Number of analyses - 1
	Analysis name - Default
	Done getting FEA analyses

Writing Nastran grid and connectivity file (in small field format) ....
Finished writing Nastran grid file

Writing subElement types (if any) - appending mesh file

Writing TACS instruction file....
	Writing analysis cards
	Writing load ADD cards
	Writing constraint ADD cards
	Writing load cards
	Writing constraint cards
	Writing material cards
	Writing property cards
	Writing design variable cards
	Writing design variable relation cards
Mapping Csys attributes ................
	Number of unique Csys attributes = 0

Getting FEA coordinate systems.......
	Number of coordinate systems - 0
	No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
	Number of unique capsConstraint attributes = 1
	Name = plateEdge, index = 1
Mapping capsLoad attributes ................
	Number of unique capsLoad attributes = 1
	Name = plate, index = 1
Mapping capsBound attributes ................
	Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
	Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
	Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
	Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
	Mesh for body = 0
	Number of nodal coordinates = 25
	Number of elements = 16
	Elemental Nodes = 0
	Elemental Rods  = 0
	Elemental Tria3 = 0
	Elemental Quad4 = 16

Getting FEA materials.......
	Number of materials - 1
	Material name - Madeupium
	Done getting FEA materials

Getting FEA properties.......
	Number of properties - 1
	Property name - plate
	Done getting FEA properties
Updating mesh element types based on properties input

Getting FEA constraints.......
	Number of constraints - 1
	Constraint name - edgeConstraint
	No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement"
	Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults

Getting FEA loads.......
	Number of loads - 1
	Load name - appliedPressure
	Done getting FEA loads

Getting FEA design variables.......
	Number of design variables          - 1
	Design_Variable name - thick1
	Design_Variable_Relation name - thick1
	Number of design variable relations - 1
	Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL

Getting FEA analyses.......
	Number of analyses - 1
	Analysis name - Default
	Done getting FEA analyses

Writing Nastran grid and connectivity file (in small field format) ....
Finished writing Nastran grid file

Writing subElement types (if any) - appending mesh file

Writing TACS instruction file....
	Writing analysis cards
	Writing load ADD cards
	Writing constraint ADD cards
	Writing load cards
	Writing constraint cards
	Writing material cards
	Writing property cards
	Writing design variable cards
	Writing design variable relation cards
Mapping Csys attributes ................
	Number of unique Csys attributes = 0

Getting FEA coordinate systems.......
	Number of coordinate systems - 0
	No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
	Number of unique capsConstraint attributes = 1
	Name = plateEdge, index = 1
Mapping capsLoad attributes ................
	Number of unique capsLoad attributes = 1
	Name = plate, index = 1
Mapping capsBound attributes ................
	Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
	Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
	Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
	Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
	Mesh for body = 0
	Number of nodal coordinates = 25
	Number of elements = 16
	Elemental Nodes = 0
	Elemental Rods  = 0
	Elemental Tria3 = 0
	Elemental Quad4 = 16

Getting FEA materials.......
	Number of materials - 1
	Material name - Madeupium
	Done getting FEA materials

Getting FEA properties.......
	Number of properties - 1
	Property name - plate
	Done getting FEA properties
Updating mesh element types based on properties input

Getting FEA constraints.......
	Number of constraints - 1
	Constraint name - edgeConstraint
	No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement"
	Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults

Getting FEA loads.......
	Number of loads - 1
	Load name - appliedPressure
	Done getting FEA loads

Getting FEA design variables.......
	Number of design variables          - 1
	Design_Variable name - thick1
	Design_Variable_Relation name - thick1
	Number of design variable relations - 1
	Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL

Getting FEA analyses.......
	Number of analyses - 1
	Analysis name - Default
	Done getting FEA analyses

Writing Nastran grid and connectivity file (in small field format) ....
Finished writing Nastran grid file

Writing subElement types (if any) - appending mesh file

Writing TACS instruction file....
	Writing analysis cards
	Writing load ADD cards
	Writing constraint ADD cards
	Writing load cards
	Writing constraint cards
	Writing material cards
	Writing property cards
	Writing design variable cards
	Writing design variable relation cards
Mapping Csys attributes ................
	Number of unique Csys attributes = 0

Getting FEA coordinate systems.......
	Number of coordinate systems - 0
	No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
	Number of unique capsConstraint attributes = 1
	Name = plateEdge, index = 1
Mapping capsLoad attributes ................
	Number of unique capsLoad attributes = 1
	Name = plate, index = 1
Mapping capsBound attributes ................
	Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
	Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
	Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
	Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
	Mesh for body = 0
	Number of nodal coordinates = 25
	Number of elements = 16
	Elemental Nodes = 0
	Elemental Rods  = 0
	Elemental Tria3 = 0
	Elemental Quad4 = 16

Getting FEA materials.......
	Number of materials - 1
	Material name - Madeupium
	Done getting FEA materials

Getting FEA properties.......
	Number of properties - 1
	Property name - plate
	Done getting FEA properties
Updating mesh element types based on properties input

Getting FEA constraints.......
	Number of constraints - 1
	Constraint name - edgeConstraint
	No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement"
	Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults

Getting FEA loads.......
	Number of loads - 1
	Load name - appliedPressure
	Done getting FEA loads

Getting FEA design variables.......
	Number of design variables          - 1
	Design_Variable name - thick1
	Design_Variable_Relation name - thick1
	Number of design variable relations - 1
	Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL

Getting FEA analyses.......
	Number of analyses - 1
	Analysis name - Default
	Done getting FEA analyses

Writing Nastran grid and connectivity file (in small field format) ....
Finished writing Nastran grid file

Writing subElement types (if any) - appending mesh file

Writing TACS instruction file....
	Writing analysis cards
	Writing load ADD cards
	Writing constraint ADD cards
	Writing load cards
	Writing constraint cards
	Writing material cards
	Writing property cards
	Writing design variable cards
	Writing design variable relation cards
Mapping Csys attributes ................
	Number of unique Csys attributes = 0

Getting FEA coordinate systems.......
	Number of coordinate systems - 0
	No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
	Number of unique capsConstraint attributes = 1
	Name = plateEdge, index = 1
Mapping capsLoad attributes ................
	Number of unique capsLoad attributes = 1
	Name = plate, index = 1
Mapping capsBound attributes ................
	Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
	Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
	Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
	Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
	Mesh for body = 0
	Number of nodal coordinates = 25
	Number of elements = 16
	Elemental Nodes = 0
	Elemental Rods  = 0
	Elemental Tria3 = 0
	Elemental Quad4 = 16

Getting FEA materials.......
	Number of materials - 1
	Material name - Madeupium
	Done getting FEA materials

Getting FEA properties.......
	Number of properties - 1
	Property name - plate
	Done getting FEA properties
Updating mesh element types based on properties input

Getting FEA constraints.......
	Number of constraints - 1
	Constraint name - edgeConstraint
	No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement"
	Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults

Getting FEA loads.......
	Number of loads - 1
	Load name - appliedPressure
	Done getting FEA loads

Getting FEA design variables.......
	Number of design variables          - 1
	Design_Variable name - thick1
	Design_Variable_Relation name - thick1
	Number of design variable relations - 1
	Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL

Getting FEA analyses.......
	Number of analyses - 1
	Analysis name - Default
	Done getting FEA analyses

Writing Nastran grid and connectivity file (in small field format) ....
Finished writing Nastran grid file

Writing subElement types (if any) - appending mesh file

Writing TACS instruction file....
	Writing analysis cards
	Writing load ADD cards
	Writing constraint ADD cards
	Writing load cards
	Writing constraint cards
	Writing material cards
	Writing property cards
	Writing design variable cards
	Writing design variable relation cards
Mapping Csys attributes ................
	Number of unique Csys attributes = 0

Getting FEA coordinate systems.......
	Number of coordinate systems - 0
	No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
	Number of unique capsConstraint attributes = 1
	Name = plateEdge, index = 1
Mapping capsLoad attributes ................
	Number of unique capsLoad attributes = 1
	Name = plate, index = 1
Mapping capsBound attributes ................
	Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
	Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
	Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
	Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
	Mesh for body = 0
	Number of nodal coordinates = 25
	Number of elements = 16
	Elemental Nodes = 0
	Elemental Rods  = 0
	Elemental Tria3 = 0
	Elemental Quad4 = 16

Getting FEA materials.......
	Number of materials - 1
	Material name - Madeupium
	Done getting FEA materials

Getting FEA properties.......
	Number of properties - 1
	Property name - plate
	Done getting FEA properties
Updating mesh element types based on properties input

Getting FEA constraints.......
	Number of constraints - 1
	Constraint name - edgeConstraint
	No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement"
	Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults

Getting FEA loads.......
	Number of loads - 1
	Load name - appliedPressure
	Done getting FEA loads

Getting FEA design variables.......
	Number of design variables          - 1
	Design_Variable name - thick1
	Design_Variable_Relation name - thick1
	Number of design variable relations - 1
	Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL

Getting FEA analyses.......
	Number of analyses - 1
	Analysis name - Default
	Done getting FEA analyses

Writing Nastran grid and connectivity file (in small field format) ....
Finished writing Nastran grid file

Writing subElement types (if any) - appending mesh file

Writing TACS instruction file....
	Writing analysis cards
	Writing load ADD cards
	Writing constraint ADD cards
	Writing load cards
	Writing constraint cards
	Writing material cards
	Writing property cards
	Writing design variable cards
	Writing design variable relation cards
Mapping Csys attributes ................
	Number of unique Csys attributes = 0

Getting FEA coordinate systems.......
	Number of coordinate systems - 0
	No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
	Number of unique capsConstraint attributes = 1
	Name = plateEdge, index = 1
Mapping capsLoad attributes ................
	Number of unique capsLoad attributes = 1
	Name = plate, index = 1
Mapping capsBound attributes ................
	Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
	Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
	Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
	Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
	Mesh for body = 0
	Number of nodal coordinates = 25
	Number of elements = 16
	Elemental Nodes = 0
	Elemental Rods  = 0
	Elemental Tria3 = 0
	Elemental Quad4 = 16

Getting FEA materials.......
	Number of materials - 1
	Material name - Madeupium
	Done getting FEA materials

Getting FEA properties.......
	Number of properties - 1
	Property name - plate
	Done getting FEA properties
Updating mesh element types based on properties input

Getting FEA constraints.......
	Number of constraints - 1
	Constraint name - edgeConstraint
	No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement"
	Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults

Getting FEA loads.......
	Number of loads - 1
	Load name - appliedPressure
	Done getting FEA loads

Getting FEA design variables.......
	Number of design variables          - 1
	Design_Variable name - thick1
	Design_Variable_Relation name - thick1
	Number of design variable relations - 1
	Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL

Getting FEA analyses.......
	Number of analyses - 1
	Analysis name - Default
	Done getting FEA analyses

Writing Nastran grid and connectivity file (in small field format) ....
Finished writing Nastran grid file

Writing subElement types (if any) - appending mesh file

Writing TACS instruction file....
	Writing analysis cards
	Writing load ADD cards
	Writing constraint ADD cards
	Writing load cards
	Writing constraint cards
	Writing material cards
	Writing property cards
	Writing design variable cards
	Writing design variable relation cards
Mapping Csys attributes ................
	Number of unique Csys attributes = 0

Getting FEA coordinate systems.......
	Number of coordinate systems - 0
	No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
	Number of unique capsConstraint attributes = 1
	Name = plateEdge, index = 1
Mapping capsLoad attributes ................
	Number of unique capsLoad attributes = 1
	Name = plate, index = 1
Mapping capsBound attributes ................
	Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
	Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
	Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
	Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
	Mesh for body = 0
	Number of nodal coordinates = 25
	Number of elements = 16
	Elemental Nodes = 0
	Elemental Rods  = 0
	Elemental Tria3 = 0
	Elemental Quad4 = 16

Getting FEA materials.......
	Number of materials - 1
	Material name - Madeupium
	Done getting FEA materials

Getting FEA properties.......
	Number of properties - 1
	Property name - plate
	Done getting FEA properties
Updating mesh element types based on properties input

Getting FEA constraints.......
	Number of constraints - 1
	Constraint name - edgeConstraint
	No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement"
	Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults

Getting FEA loads.......
	Number of loads - 1
	Load name - appliedPressure
	Done getting FEA loads

Getting FEA design variables.......
	Number of design variables          - 1
	Design_Variable name - thick1
	Design_Variable_Relation name - thick1
	Number of design variable relations - 1
	Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL

Getting FEA analyses.......
	Number of analyses - 1
	Analysis name - Default
	Done getting FEA analyses

Writing Nastran grid and connectivity file (in small field format) ....
Finished writing Nastran grid file

Writing subElement types (if any) - appending mesh file

Writing TACS instruction file....
	Writing analysis cards
	Writing load ADD cards
	Writing constraint ADD cards
	Writing load cards
	Writing constraint cards
	Writing material cards
	Writing property cards
	Writing design variable cards
	Writing design variable relation cards
Mapping Csys attributes ................
	Number of unique Csys attributes = 0

Getting FEA coordinate systems.......
	Number of coordinate systems - 0
	No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
	Number of unique capsConstraint attributes = 1
	Name = plateEdge, index = 1
Mapping capsLoad attributes ................
	Number of unique capsLoad attributes = 1
	Name = plate, index = 1
Mapping capsBound attributes ................
	Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
	Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
	Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
	Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
	Mesh for body = 0
	Number of nodal coordinates = 25
	Number of elements = 16
	Elemental Nodes = 0
	Elemental Rods  = 0
	Elemental Tria3 = 0
	Elemental Quad4 = 16

Getting FEA materials.......
	Number of materials - 1
	Material name - Madeupium
	Done getting FEA materials

Getting FEA properties.......
	Number of properties - 1
	Property name - plate
	Done getting FEA properties
Updating mesh element types based on properties input

Getting FEA constraints.......
	Number of constraints - 1
	Constraint name - edgeConstraint
	No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement"
	Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults

Getting FEA loads.......
	Number of loads - 1
	Load name - appliedPressure
	Done getting FEA loads

Getting FEA design variables.......
	Number of design variables          - 1
	Design_Variable name - thick1
	Design_Variable_Relation name - thick1
	Number of design variable relations - 1
	Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL

Getting FEA analyses.......
	Number of analyses - 1
	Analysis name - Default
	Done getting FEA analyses

Writing Nastran grid and connectivity file (in small field format) ....
Finished writing Nastran grid file

Writing subElement types (if any) - appending mesh file

Writing TACS instruction file....
	Writing analysis cards
	Writing load ADD cards
	Writing constraint ADD cards
	Writing load cards
	Writing constraint cards
	Writing material cards
	Writing property cards
	Writing design variable cards
	Writing design variable relation cards
Mapping Csys attributes ................
	Number of unique Csys attributes = 0

Getting FEA coordinate systems.......
	Number of coordinate systems - 0
	No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
	Number of unique capsConstraint attributes = 1
	Name = plateEdge, index = 1
Mapping capsLoad attributes ................
	Number of unique capsLoad attributes = 1
	Name = plate, index = 1
Mapping capsBound attributes ................
	Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
	Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
	Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
	Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
	Mesh for body = 0
	Number of nodal coordinates = 25
	Number of elements = 16
	Elemental Nodes = 0
	Elemental Rods  = 0
	Elemental Tria3 = 0
	Elemental Quad4 = 16

Getting FEA materials.......
	Number of materials - 1
	Material name - Madeupium
	Done getting FEA materials

Getting FEA properties.......
	Number of properties - 1
	Property name - plate
	Done getting FEA properties
Updating mesh element types based on properties input

Getting FEA constraints.......
	Number of constraints - 1
	Constraint name - edgeConstraint
	No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement"
	Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults

Getting FEA loads.......
	Number of loads - 1
	Load name - appliedPressure
	Done getting FEA loads

Getting FEA design variables.......
	Number of design variables          - 1
	Design_Variable name - thick1
	Design_Variable_Relation name - thick1
	Number of design variable relations - 1
	Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL

Getting FEA analyses.......
	Number of analyses - 1
	Analysis name - Default
	Done getting FEA analyses

Writing Nastran grid and connectivity file (in small field format) ....
Finished writing Nastran grid file

Writing subElement types (if any) - appending mesh file

Writing TACS instruction file....
	Writing analysis cards
	Writing load ADD cards
	Writing constraint ADD cards
	Writing load cards
	Writing constraint cards
	Writing material cards
	Writing property cards
	Writing design variable cards
	Writing design variable relation cards
Mapping Csys attributes ................
	Number of unique Csys attributes = 0

Getting FEA coordinate systems.......
	Number of coordinate systems - 0
	No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
	Number of unique capsConstraint attributes = 1
	Name = plateEdge, index = 1
Mapping capsLoad attributes ................
	Number of unique capsLoad attributes = 1
	Name = plate, index = 1
Mapping capsBound attributes ................
	Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
	Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
	Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
	Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
	Mesh for body = 0
	Number of nodal coordinates = 25
	Number of elements = 16
	Elemental Nodes = 0
	Elemental Rods  = 0
	Elemental Tria3 = 0
	Elemental Quad4 = 16

Getting FEA materials.......
	Number of materials - 1
	Material name - Madeupium
	Done getting FEA materials

Getting FEA properties.......
	Number of properties - 1
	Property name - plate
	Done getting FEA properties
Updating mesh element types based on properties input

Getting FEA constraints.......
	Number of constraints - 1
	Constraint name - edgeConstraint
	No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement"
	Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults

Getting FEA loads.......
	Number of loads - 1
	Load name - appliedPressure
	Done getting FEA loads

Getting FEA design variables.......
	Number of design variables          - 1
	Design_Variable name - thick1
	Design_Variable_Relation name - thick1
	Number of design variable relations - 1
	Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL

Getting FEA analyses.......
	Number of analyses - 1
	Analysis name - Default
	Done getting FEA analyses

Writing Nastran grid and connectivity file (in small field format) ....
Finished writing Nastran grid file

Writing subElement types (if any) - appending mesh file

Writing TACS instruction file....
	Writing analysis cards
	Writing load ADD cards
	Writing constraint ADD cards
	Writing load cards
	Writing constraint cards
	Writing material cards
	Writing property cards
	Writing design variable cards
	Writing design variable relation cards
Mapping Csys attributes ................
	Number of unique Csys attributes = 0

Getting FEA coordinate systems.......
	Number of coordinate systems - 0
	No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
	Number of unique capsConstraint attributes = 1
	Name = plateEdge, index = 1
Mapping capsLoad attributes ................
	Number of unique capsLoad attributes = 1
	Name = plate, index = 1
Mapping capsBound attributes ................
	Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
	Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
	Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
	Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
	Mesh for body = 0
	Number of nodal coordinates = 25
	Number of elements = 16
	Elemental Nodes = 0
	Elemental Rods  = 0
	Elemental Tria3 = 0
	Elemental Quad4 = 16

Getting FEA materials.......
	Number of materials - 1
	Material name - Madeupium
	Done getting FEA materials

Getting FEA properties.......
	Number of properties - 1
	Property name - plate
	Done getting FEA properties
Updating mesh element types based on properties input

Getting FEA constraints.......
	Number of constraints - 1
	Constraint name - edgeConstraint
	No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement"
	Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults

Getting FEA loads.......
	Number of loads - 1
	Load name - appliedPressure
	Done getting FEA loads

Getting FEA design variables.......
	Number of design variables          - 1
	Design_Variable name - thick1
	Design_Variable_Relation name - thick1
	Number of design variable relations - 1
	Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL

Getting FEA analyses.......
	Number of analyses - 1
	Analysis name - Default
	Done getting FEA analyses

Writing Nastran grid and connectivity file (in small field format) ....
Finished writing Nastran grid file

Writing subElement types (if any) - appending mesh file

Writing TACS instruction file....
	Writing analysis cards
	Writing load ADD cards
	Writing constraint ADD cards
	Writing load cards
	Writing constraint cards
	Writing material cards
	Writing property cards
	Writing design variable cards
	Writing design variable relation cards
Mapping Csys attributes ................
	Number of unique Csys attributes = 0

Getting FEA coordinate systems.......
	Number of coordinate systems - 0
	No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
	Number of unique capsConstraint attributes = 1
	Name = plateEdge, index = 1
Mapping capsLoad attributes ................
	Number of unique capsLoad attributes = 1
	Name = plate, index = 1
Mapping capsBound attributes ................
	Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
	Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
	Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
	Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
	Mesh for body = 0
	Number of nodal coordinates = 25
	Number of elements = 16
	Elemental Nodes = 0
	Elemental Rods  = 0
	Elemental Tria3 = 0
	Elemental Quad4 = 16

Getting FEA materials.......
	Number of materials - 1
	Material name - Madeupium
	Done getting FEA materials

Getting FEA properties.......
	Number of properties - 1
	Property name - plate
	Done getting FEA properties
Updating mesh element types based on properties input

Getting FEA constraints.......
	Number of constraints - 1
	Constraint name - edgeConstraint
	No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement"
	Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults

Getting FEA loads.......
	Number of loads - 1
	Load name - appliedPressure
	Done getting FEA loads

Getting FEA design variables.......
	Number of design variables          - 1
	Design_Variable name - thick1
	Design_Variable_Relation name - thick1
	Number of design variable relations - 1
	Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL

Getting FEA analyses.......
	Number of analyses - 1
	Analysis name - Default
	Done getting FEA analyses

Writing Nastran grid and connectivity file (in small field format) ....
Finished writing Nastran grid file

Writing subElement types (if any) - appending mesh file

Writing TACS instruction file....
	Writing analysis cards
	Writing load ADD cards
	Writing constraint ADD cards
	Writing load cards
	Writing constraint cards
	Writing material cards
	Writing property cards
	Writing design variable cards
	Writing design variable relation cards
Mapping Csys attributes ................
	Number of unique Csys attributes = 0

Getting FEA coordinate systems.......
	Number of coordinate systems - 0
	No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
	Number of unique capsConstraint attributes = 1
	Name = plateEdge, index = 1
Mapping capsLoad attributes ................
	Number of unique capsLoad attributes = 1
	Name = plate, index = 1
Mapping capsBound attributes ................
	Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
	Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
	Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
	Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
	Mesh for body = 0
	Number of nodal coordinates = 25
	Number of elements = 16
	Elemental Nodes = 0
	Elemental Rods  = 0
	Elemental Tria3 = 0
	Elemental Quad4 = 16

Getting FEA materials.......
	Number of materials - 1
	Material name - Madeupium
	Done getting FEA materials

Getting FEA properties.......
	Number of properties - 1
	Property name - plate
	Done getting FEA properties
Updating mesh element types based on properties input

Getting FEA constraints.......
	Number of constraints - 1
	Constraint name - edgeConstraint
	No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement"
	Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults

Getting FEA loads.......
	Number of loads - 1
	Load name - appliedPressure
	Done getting FEA loads

Getting FEA design variables.......
	Number of design variables          - 1
	Design_Variable name - thick1
	Design_Variable_Relation name - thick1
	Number of design variable relations - 1
	Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL

Getting FEA analyses.......
	Number of analyses - 1
	Analysis name - Default
	Done getting FEA analyses

Writing Nastran grid and connectivity file (in small field format) ....
Finished writing Nastran grid file

Writing subElement types (if any) - appending mesh file

Writing TACS instruction file....
	Writing analysis cards
	Writing load ADD cards
	Writing constraint ADD cards
	Writing load cards
	Writing constraint cards
	Writing material cards
	Writing property cards
	Writing design variable cards
	Writing design variable relation cards
Mapping Csys attributes ................
	Number of unique Csys attributes = 0

Getting FEA coordinate systems.......
	Number of coordinate systems - 0
	No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
	Number of unique capsConstraint attributes = 1
	Name = plateEdge, index = 1
Mapping capsLoad attributes ................
	Number of unique capsLoad attributes = 1
	Name = plate, index = 1
Mapping capsBound attributes ................
	Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
	Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
	Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
	Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
	Mesh for body = 0
	Number of nodal coordinates = 25
	Number of elements = 16
	Elemental Nodes = 0
	Elemental Rods  = 0
	Elemental Tria3 = 0
	Elemental Quad4 = 16

Getting FEA materials.......
	Number of materials - 1
	Material name - Madeupium
	Done getting FEA materials

Getting FEA properties.......
	Number of properties - 1
	Property name - plate
	Done getting FEA properties
Updating mesh element types based on properties input

Getting FEA constraints.......
	Number of constraints - 1
	Constraint name - edgeConstraint
	No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement"
	Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults

Getting FEA loads.......
	Number of loads - 1
	Load name - appliedPressure
	Done getting FEA loads

Getting FEA design variables.......
	Number of design variables          - 1
	Design_Variable name - thick1
	Design_Variable_Relation name - thick1
	Number of design variable relations - 1
	Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL

Getting FEA analyses.......
	Number of analyses - 1
	Analysis name - Default
	Done getting FEA analyses

Writing Nastran grid and connectivity file (in small field format) ....
Finished writing Nastran grid file

Writing subElement types (if any) - appending mesh file

Writing TACS instruction file....
	Writing analysis cards
	Writing load ADD cards
	Writing constraint ADD cards
	Writing load cards
	Writing constraint cards
	Writing material cards
	Writing property cards
	Writing design variable cards
	Writing design variable relation cards
Mapping Csys attributes ................
	Number of unique Csys attributes = 0

Getting FEA coordinate systems.......
	Number of coordinate systems - 0
	No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
	Number of unique capsConstraint attributes = 1
	Name = plateEdge, index = 1
Mapping capsLoad attributes ................
	Number of unique capsLoad attributes = 1
	Name = plate, index = 1
Mapping capsBound attributes ................
	Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
	Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
	Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
	Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
	Mesh for body = 0
	Number of nodal coordinates = 25
	Number of elements = 16
	Elemental Nodes = 0
	Elemental Rods  = 0
	Elemental Tria3 = 0
	Elemental Quad4 = 16

Getting FEA materials.......
	Number of materials - 1
	Material name - Madeupium
	Done getting FEA materials

Getting FEA properties.......
	Number of properties - 1
	Property name - plate
	Done getting FEA properties
Updating mesh element types based on properties input

Getting FEA constraints.......
	Number of constraints - 1
	Constraint name - edgeConstraint
	No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement"
	Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults

Getting FEA loads.......
	Number of loads - 1
	Load name - appliedPressure
	Done getting FEA loads

Getting FEA design variables.......
	Number of design variables          - 1
	Design_Variable name - thick1
	Design_Variable_Relation name - thick1
	Number of design variable relations - 1
	Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL

Getting FEA analyses.......
	Number of analyses - 1
	Analysis name - Default
	Done getting FEA analyses

Writing Nastran grid and connectivity file (in small field format) ....
Finished writing Nastran grid file

Writing subElement types (if any) - appending mesh file

Writing TACS instruction file....
	Writing analysis cards
	Writing load ADD cards
	Writing constraint ADD cards
	Writing load cards
	Writing constraint cards
	Writing material cards
	Writing property cards
	Writing design variable cards
	Writing design variable relation cards
Mapping Csys attributes ................
	Number of unique Csys attributes = 0

Getting FEA coordinate systems.......
	Number of coordinate systems - 0
	No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
	Number of unique capsConstraint attributes = 1
	Name = plateEdge, index = 1
Mapping capsLoad attributes ................
	Number of unique capsLoad attributes = 1
	Name = plate, index = 1
Mapping capsBound attributes ................
	Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
	Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
	Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
	Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
	Mesh for body = 0
	Number of nodal coordinates = 25
	Number of elements = 16
	Elemental Nodes = 0
	Elemental Rods  = 0
	Elemental Tria3 = 0
	Elemental Quad4 = 16

Getting FEA materials.......
	Number of materials - 1
	Material name - Madeupium
	Done getting FEA materials

Getting FEA properties.......
	Number of properties - 1
	Property name - plate
	Done getting FEA properties
Updating mesh element types based on properties input

Getting FEA constraints.......
	Number of constraints - 1
	Constraint name - edgeConstraint
	No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement"
	Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults

Getting FEA loads.......
	Number of loads - 1
	Load name - appliedPressure
	Done getting FEA loads

Getting FEA design variables.......
	Number of design variables          - 1
	Design_Variable name - thick1
	Design_Variable_Relation name - thick1
	Number of design variable relations - 1
	Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL

Getting FEA analyses.......
	Number of analyses - 1
	Analysis name - Default
	Done getting FEA analyses

Writing Nastran grid and connectivity file (in small field format) ....
Finished writing Nastran grid file

Writing subElement types (if any) - appending mesh file

Writing TACS instruction file....
	Writing analysis cards
	Writing load ADD cards
	Writing constraint ADD cards
	Writing load cards
	Writing constraint cards
	Writing material cards
	Writing property cards
	Writing design variable cards
	Writing design variable relation cards
Mapping Csys attributes ................
	Number of unique Csys attributes = 0

Getting FEA coordinate systems.......
	Number of coordinate systems - 0
	No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
	Number of unique capsConstraint attributes = 1
	Name = plateEdge, index = 1
Mapping capsLoad attributes ................
	Number of unique capsLoad attributes = 1
	Name = plate, index = 1
Mapping capsBound attributes ................
	Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
	Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
	Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
	Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
	Mesh for body = 0
	Number of nodal coordinates = 25
	Number of elements = 16
	Elemental Nodes = 0
	Elemental Rods  = 0
	Elemental Tria3 = 0
	Elemental Quad4 = 16

Getting FEA materials.......
	Number of materials - 1
	Material name - Madeupium
	Done getting FEA materials

Getting FEA properties.......
	Number of properties - 1
	Property name - plate
	Done getting FEA properties
Updating mesh element types based on properties input

Getting FEA constraints.......
	Number of constraints - 1
	Constraint name - edgeConstraint
	No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement"
	Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults

Getting FEA loads.......
	Number of loads - 1
	Load name - appliedPressure
	Done getting FEA loads

Getting FEA design variables.......
	Number of design variables          - 1
	Design_Variable name - thick1
	Design_Variable_Relation name - thick1
	Number of design variable relations - 1
	Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL

Getting FEA analyses.......
	Number of analyses - 1
	Analysis name - Default
	Done getting FEA analyses

Writing Nastran grid and connectivity file (in small field format) ....
Finished writing Nastran grid file

Writing subElement types (if any) - appending mesh file

Writing TACS instruction file....
	Writing analysis cards
	Writing load ADD cards
	Writing constraint ADD cards
	Writing load cards
	Writing constraint cards
	Writing material cards
	Writing property cards
	Writing design variable cards
	Writing design variable relation cards
Mapping Csys attributes ................
	Number of unique Csys attributes = 0

Getting FEA coordinate systems.......
	Number of coordinate systems - 0
	No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
	Number of unique capsConstraint attributes = 1
	Name = plateEdge, index = 1
Mapping capsLoad attributes ................
	Number of unique capsLoad attributes = 1
	Name = plate, index = 1
Mapping capsBound attributes ................
	Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
	Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
	Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
	Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
	Mesh for body = 0
	Number of nodal coordinates = 25
	Number of elements = 16
	Elemental Nodes = 0
	Elemental Rods  = 0
	Elemental Tria3 = 0
	Elemental Quad4 = 16

Getting FEA materials.......
	Number of materials - 1
	Material name - Madeupium
	Done getting FEA materials

Getting FEA properties.......
	Number of properties - 1
	Property name - plate
	Done getting FEA properties
Updating mesh element types based on properties input

Getting FEA constraints.......
	Number of constraints - 1
	Constraint name - edgeConstraint
	No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement"
	Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults

Getting FEA loads.......
	Number of loads - 1
	Load name - appliedPressure
	Done getting FEA loads

Getting FEA design variables.......
	Number of design variables          - 1
	Design_Variable name - thick1
	Design_Variable_Relation name - thick1
	Number of design variable relations - 1
	Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL

Getting FEA analyses.......
	Number of analyses - 1
	Analysis name - Default
	Done getting FEA analyses

Writing Nastran grid and connectivity file (in small field format) ....
Finished writing Nastran grid file

Writing subElement types (if any) - appending mesh file

Writing TACS instruction file....
	Writing analysis cards
	Writing load ADD cards
	Writing constraint ADD cards
	Writing load cards
	Writing constraint cards
	Writing material cards
	Writing property cards
	Writing design variable cards
	Writing design variable relation cards
Mapping Csys attributes ................
	Number of unique Csys attributes = 0

Getting FEA coordinate systems.......
	Number of coordinate systems - 0
	No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
	Number of unique capsConstraint attributes = 1
	Name = plateEdge, index = 1
Mapping capsLoad attributes ................
	Number of unique capsLoad attributes = 1
	Name = plate, index = 1
Mapping capsBound attributes ................
	Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
	Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
	Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
	Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
	Mesh for body = 0
	Number of nodal coordinates = 25
	Number of elements = 16
	Elemental Nodes = 0
	Elemental Rods  = 0
	Elemental Tria3 = 0
	Elemental Quad4 = 16

Getting FEA materials.......
	Number of materials - 1
	Material name - Madeupium
	Done getting FEA materials

Getting FEA properties.......
	Number of properties - 1
	Property name - plate
	Done getting FEA properties
Updating mesh element types based on properties input

Getting FEA constraints.......
	Number of constraints - 1
	Constraint name - edgeConstraint
	No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement"
	Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults

Getting FEA loads.......
	Number of loads - 1
	Load name - appliedPressure
	Done getting FEA loads

Getting FEA design variables.......
	Number of design variables          - 1
	Design_Variable name - thick1
	Design_Variable_Relation name - thick1
	Number of design variable relations - 1
	Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL

Getting FEA analyses.......
	Number of analyses - 1
	Analysis name - Default
	Done getting FEA analyses

Writing Nastran grid and connectivity file (in small field format) ....
Finished writing Nastran grid file

Writing subElement types (if any) - appending mesh file

Writing TACS instruction file....
	Writing analysis cards
	Writing load ADD cards
	Writing constraint ADD cards
	Writing load cards
	Writing constraint cards
	Writing material cards
	Writing property cards
	Writing design variable cards
	Writing design variable relation cards
Mapping Csys attributes ................
	Number of unique Csys attributes = 0

Getting FEA coordinate systems.......
	Number of coordinate systems - 0
	No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
	Number of unique capsConstraint attributes = 1
	Name = plateEdge, index = 1
Mapping capsLoad attributes ................
	Number of unique capsLoad attributes = 1
	Name = plate, index = 1
Mapping capsBound attributes ................
	Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
	Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
	Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
	Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
	Mesh for body = 0
	Number of nodal coordinates = 25
	Number of elements = 16
	Elemental Nodes = 0
	Elemental Rods  = 0
	Elemental Tria3 = 0
	Elemental Quad4 = 16

Getting FEA materials.......
	Number of materials - 1
	Material name - Madeupium
	Done getting FEA materials

Getting FEA properties.......
	Number of properties - 1
	Property name - plate
	Done getting FEA properties
Updating mesh element types based on properties input

Getting FEA constraints.......
	Number of constraints - 1
	Constraint name - edgeConstraint
	No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement"
	Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults

Getting FEA loads.......
	Number of loads - 1
	Load name - appliedPressure
	Done getting FEA loads

Getting FEA design variables.......
	Number of design variables          - 1
	Design_Variable name - thick1
	Design_Variable_Relation name - thick1
	Number of design variable relations - 1
	Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL

Getting FEA analyses.......
	Number of analyses - 1
	Analysis name - Default
	Done getting FEA analyses

Writing Nastran grid and connectivity file (in small field format) ....
Finished writing Nastran grid file

Writing subElement types (if any) - appending mesh file

Writing TACS instruction file....
	Writing analysis cards
	Writing load ADD cards
	Writing constraint ADD cards
	Writing load cards
	Writing constraint cards
	Writing material cards
	Writing property cards
	Writing design variable cards
	Writing design variable relation cards
Mapping Csys attributes ................
	Number of unique Csys attributes = 0

Getting FEA coordinate systems.......
	Number of coordinate systems - 0
	No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
	Number of unique capsConstraint attributes = 1
	Name = plateEdge, index = 1
Mapping capsLoad attributes ................
	Number of unique capsLoad attributes = 1
	Name = plate, index = 1
Mapping capsBound attributes ................
	Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
	Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
	Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
	Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
	Mesh for body = 0
	Number of nodal coordinates = 25
	Number of elements = 16
	Elemental Nodes = 0
	Elemental Rods  = 0
	Elemental Tria3 = 0
	Elemental Quad4 = 16

Getting FEA materials.......
	Number of materials - 1
	Material name - Madeupium
	Done getting FEA materials

Getting FEA properties.......
	Number of properties - 1
	Property name - plate
	Done getting FEA properties
Updating mesh element types based on properties input

Getting FEA constraints.......
	Number of constraints - 1
	Constraint name - edgeConstraint
	No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement"
	Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults

Getting FEA loads.......
	Number of loads - 1
	Load name - appliedPressure
	Done getting FEA loads

Getting FEA design variables.......
	Number of design variables          - 1
	Design_Variable name - thick1
	Design_Variable_Relation name - thick1
	Number of design variable relations - 1
	Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL

Getting FEA analyses.......
	Number of analyses - 1
	Analysis name - Default
	Done getting FEA analyses

Writing Nastran grid and connectivity file (in small field format) ....
Finished writing Nastran grid file

Writing subElement types (if any) - appending mesh file

Writing TACS instruction file....
	Writing analysis cards
	Writing load ADD cards
	Writing constraint ADD cards
	Writing load cards
	Writing constraint cards
	Writing material cards
	Writing property cards
	Writing design variable cards
	Writing design variable relation cards
Mapping Csys attributes ................
	Number of unique Csys attributes = 0

Getting FEA coordinate systems.......
	Number of coordinate systems - 0
	No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
	Number of unique capsConstraint attributes = 1
	Name = plateEdge, index = 1
Mapping capsLoad attributes ................
	Number of unique capsLoad attributes = 1
	Name = plate, index = 1
Mapping capsBound attributes ................
	Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
	Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
	Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
	Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
	Mesh for body = 0
	Number of nodal coordinates = 25
	Number of elements = 16
	Elemental Nodes = 0
	Elemental Rods  = 0
	Elemental Tria3 = 0
	Elemental Quad4 = 16

Getting FEA materials.......
	Number of materials - 1
	Material name - Madeupium
	Done getting FEA materials

Getting FEA properties.......
	Number of properties - 1
	Property name - plate
	Done getting FEA properties
Updating mesh element types based on properties input

Getting FEA constraints.......
	Number of constraints - 1
	Constraint name - edgeConstraint
	No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement"
	Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults

Getting FEA loads.......
	Number of loads - 1
	Load name - appliedPressure
	Done getting FEA loads

Getting FEA design variables.......
	Number of design variables          - 1
	Design_Variable name - thick1
	Design_Variable_Relation name - thick1
	Number of design variable relations - 1
	Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL

Getting FEA analyses.......
	Number of analyses - 1
	Analysis name - Default
	Done getting FEA analyses

Writing Nastran grid and connectivity file (in small field format) ....
Finished writing Nastran grid file

Writing subElement types (if any) - appending mesh file

Writing TACS instruction file....
	Writing analysis cards
	Writing load ADD cards
	Writing constraint ADD cards
	Writing load cards
	Writing constraint cards
	Writing material cards
	Writing property cards
	Writing design variable cards
	Writing design variable relation cards
Mapping Csys attributes ................
	Number of unique Csys attributes = 0

Getting FEA coordinate systems.......
	Number of coordinate systems - 0
	No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
	Number of unique capsConstraint attributes = 1
	Name = plateEdge, index = 1
Mapping capsLoad attributes ................
	Number of unique capsLoad attributes = 1
	Name = plate, index = 1
Mapping capsBound attributes ................
	Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
	Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
	Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
	Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
	Mesh for body = 0
	Number of nodal coordinates = 25
	Number of elements = 16
	Elemental Nodes = 0
	Elemental Rods  = 0
	Elemental Tria3 = 0
	Elemental Quad4 = 16

Getting FEA materials.......
	Number of materials - 1
	Material name - Madeupium
	Done getting FEA materials

Getting FEA properties.......
	Number of properties - 1
	Property name - plate
	Done getting FEA properties
Updating mesh element types based on properties input

Getting FEA constraints.......
	Number of constraints - 1
	Constraint name - edgeConstraint
	No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement"
	Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults

Getting FEA loads.......
	Number of loads - 1
	Load name - appliedPressure
	Done getting FEA loads

Getting FEA design variables.......
	Number of design variables          - 1
	Design_Variable name - thick1
	Design_Variable_Relation name - thick1
	Number of design variable relations - 1
	Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL

Getting FEA analyses.......
	Number of analyses - 1
	Analysis name - Default
	Done getting FEA analyses

Writing Nastran grid and connectivity file (in small field format) ....
Finished writing Nastran grid file

Writing subElement types (if any) - appending mesh file

Writing TACS instruction file....
	Writing analysis cards
	Writing load ADD cards
	Writing constraint ADD cards
	Writing load cards
	Writing constraint cards
	Writing material cards
	Writing property cards
	Writing design variable cards
	Writing design variable relation cards
Mapping Csys attributes ................
	Number of unique Csys attributes = 0

Getting FEA coordinate systems.......
	Number of coordinate systems - 0
	No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
	Number of unique capsConstraint attributes = 1
	Name = plateEdge, index = 1
Mapping capsLoad attributes ................
	Number of unique capsLoad attributes = 1
	Name = plate, index = 1
Mapping capsBound attributes ................
	Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
	Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
	Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
	Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
	Mesh for body = 0
	Number of nodal coordinates = 25
	Number of elements = 16
	Elemental Nodes = 0
	Elemental Rods  = 0
	Elemental Tria3 = 0
	Elemental Quad4 = 16

Getting FEA materials.......
	Number of materials - 1
	Material name - Madeupium
	Done getting FEA materials

Getting FEA properties.......
	Number of properties - 1
	Property name - plate
	Done getting FEA properties
Updating mesh element types based on properties input

Getting FEA constraints.......
	Number of constraints - 1
	Constraint name - edgeConstraint
	No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement"
	Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults

Getting FEA loads.......
	Number of loads - 1
	Load name - appliedPressure
	Done getting FEA loads

Getting FEA design variables.......
	Number of design variables          - 1
	Design_Variable name - thick1
	Design_Variable_Relation name - thick1
	Number of design variable relations - 1
	Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL

Getting FEA analyses.......
	Number of analyses - 1
	Analysis name - Default
	Done getting FEA analyses

Writing Nastran grid and connectivity file (in small field format) ....
Finished writing Nastran grid file

Writing subElement types (if any) - appending mesh file

Writing TACS instruction file....
	Writing analysis cards
	Writing load ADD cards
	Writing constraint ADD cards
	Writing load cards
	Writing constraint cards
	Writing material cards
	Writing property cards
	Writing design variable cards
	Writing design variable relation cards
ok
test_Multiple_Mesh (test_tetgen.TestTETGEN.test_Multiple_Mesh) ... ERROR:: BAD STATUS = -276 from matsol (called from solveSketchOrig:63376)
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 7
	Name = box, index = 1
	Name = cylinder, index = 2
	Name = cone, index = 3
	Name = torus, index = 4
	Name = sphere, index = 5
	Name = boxhole, index = 6
	Name = bullet, index = 7
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 1
	Name = box, index = 1
Getting surface mesh for body 1 (of 7)
Getting surface mesh for body 2 (of 7)
Getting surface mesh for body 3 (of 7)
Getting surface mesh for body 4 (of 7)
Getting surface mesh for body 5 (of 7)
Getting surface mesh for body 6 (of 7)
 1F924CC00 EGADS Info: Face #3 -&gt; Edge #9 (9) Internally in Loop 4 7, sen = -1!
 174073000 EGADS Info: Face #5 -&gt; Edge #17 (9) Internally in Loop 7 4, sen = -1!
 1F924CC00 EGADS Info: Face #3 -&gt; Edge #9 (9) Internally in Loop 7 4, sen = 1!
 174073000 EGADS Info: Face #5 -&gt; Edge #17 (9) Internally in Loop 4 7, sen = 1!
Getting surface mesh for body 7 (of 7)
Body 1 (of 7)
Number of nodes    = 98
Number of elements = 192
Number of triangle elements      = 192
Number of quadrilateral elements = 0
Body 2 (of 7)
Number of nodes    = 298
Number of elements = 592
Number of triangle elements      = 592
Number of quadrilateral elements = 0
Body 3 (of 7)
Number of nodes    = 488
Number of elements = 972
Number of triangle elements      = 972
Number of quadrilateral elements = 0
Body 4 (of 7)
Number of nodes    = 2048
Number of elements = 4096
Number of triangle elements      = 4096
Number of quadrilateral elements = 0
Body 5 (of 7)
Number of nodes    = 152
Number of elements = 300
Number of triangle elements      = 300
Number of quadrilateral elements = 0
Body 6 (of 7)
Number of nodes    = 624
Number of elements = 1248
Number of triangle elements      = 1248
Number of quadrilateral elements = 0
Body 7 (of 7)
Number of nodes    = 489
Number of elements = 974
Number of triangle elements      = 974
Number of quadrilateral elements = 0
----------------------------
Total number of nodes    = 4197
Total number of elements = 8374
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 7
	Name = box, index = 1
	Name = cylinder, index = 2
	Name = cone, index = 3
	Name = torus, index = 4
	Name = sphere, index = 5
	Name = boxhole, index = 6
	Name = bullet, index = 7
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Body 1 number of surface: nodes - 98, elements - 192
Body 2 number of surface: nodes - 298, elements - 592
Body 3 number of surface: nodes - 488, elements - 972
Body 4 number of surface: nodes - 2048, elements - 4096
Body 5 number of surface: nodes - 152, elements - 300
Body 6 number of surface: nodes - 624, elements - 1248
Body 7 number of surface: nodes - 489, elements - 974
Getting volume mesh for body 1 (of 7)
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = box, index = 1

Generating volume mesh using TetGen.....

Tetgen input string = pYq1.500/0.000QT1.00e-16A
Done meshing using TetGen!
Getting volume mesh for body 2 (of 7)
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = cylinder, index = 1

Generating volume mesh using TetGen.....

Tetgen input string = pYq1.500/0.000QT1.00e-16A
Done meshing using TetGen!
Getting volume mesh for body 3 (of 7)
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = cone, index = 1

Generating volume mesh using TetGen.....

Tetgen input string = pYq1.500/0.000QT1.00e-16A
Done meshing using TetGen!
Getting volume mesh for body 4 (of 7)
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = torus, index = 1

Generating volume mesh using TetGen.....

Tetgen input string = pYq1.500/0.000QT1.00e-16A
Done meshing using TetGen!
Getting volume mesh for body 5 (of 7)
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = sphere, index = 1

Generating volume mesh using TetGen.....

Tetgen input string = pYq1.500/0.000QT1.00e-16A
Done meshing using TetGen!
Getting volume mesh for body 6 (of 7)
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = boxhole, index = 1

Generating volume mesh using TetGen.....

Tetgen input string = pYq1.500/0.000QT1.00e-16A
Done meshing using TetGen!
Getting volume mesh for body 7 (of 7)
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = bullet, index = 1

Generating volume mesh using TetGen.....

Tetgen input string = pYq1.500/0.000QT1.00e-16A
Done meshing using TetGen!
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 7
	Name = box, index = 1
	Name = cylinder, index = 2
	Name = cone, index = 3
	Name = torus, index = 4
	Name = sphere, index = 5
	Name = boxhole, index = 6
	Name = bullet, index = 7
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Body 1 number of surface: nodes - 98, elements - 192
Body 2 number of surface: nodes - 298, elements - 592
Body 3 number of surface: nodes - 488, elements - 972
Body 4 number of surface: nodes - 2048, elements - 4096
Body 5 number of surface: nodes - 152, elements - 300
Body 6 number of surface: nodes - 624, elements - 1248
Body 7 number of surface: nodes - 489, elements - 974
Getting volume mesh

Generating volume mesh using TetGen.....

Tetgen input string = pYq1.500/0.000QT1.00e-16A

Generating volume mesh using TetGen.....

Tetgen input string = pYq1.500/0.000QT1.00e-16A

Generating volume mesh using TetGen.....

Tetgen input string = pYq1.500/0.000QT1.00e-16A

Generating volume mesh using TetGen.....

Tetgen input string = pYq1.500/0.000QT1.00e-16A

Generating volume mesh using TetGen.....

Tetgen input string = pYq1.500/0.000QT1.00e-16A

Generating volume mesh using TetGen.....

Tetgen input string = pYq1.500/0.000QT1.00e-16A

Generating volume mesh using TetGen.....

Tetgen input string = pYq1.500/0.000QT1.00e-16A
Done meshing using TetGen!
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 7
	Name = box, index = 1
	Name = cylinder, index = 2
	Name = cone, index = 3
	Name = torus, index = 4
	Name = sphere, index = 5
	Name = boxhole, index = 6
	Name = bullet, index = 7
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Number of surface: nodes - 4197, elements - 8374
Getting volume mesh

Generating volume mesh using TetGen.....

Tetgen input string = pYq1.500/0.000QT1.00e-16A
Done meshing using TetGen!
ok
test_faceMatch_MultiDomain (test_tetgen.TestTETGEN.test_faceMatch_MultiDomain) ... ../csmData/MultiDomain/example1.csm
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = dummy_att, index = 1
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 0
Getting surface mesh for body 1 (of 2)
Getting surface mesh for body 2 (of 2)
Body 1 (of 2)
Number of nodes    = 374
Number of elements = 744
Number of triangle elements      = 744
Number of quadrilateral elements = 0
Body 2 (of 2)
Number of nodes    = 98
Number of elements = 192
Number of triangle elements      = 192
Number of quadrilateral elements = 0
----------------------------
Total number of nodes    = 472
Total number of elements = 936
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = dummy_att, index = 1
Body 1 number of surface: nodes - 374, elements - 744
Body 2 number of surface: nodes - 98, elements - 192
Getting volume mesh

Generating volume mesh using TetGen.....

Tetgen input string = pYq1.500/0.000QT1.00e-16A

Generating volume mesh using TetGen.....

Tetgen input string = pYq1.500/0.000QT1.00e-16A
Done meshing using TetGen!
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = dummy_att, index = 1
Body 1 number of surface: nodes - 374, elements - 744
Body 2 number of surface: nodes - 98, elements - 192
Getting volume mesh for body 1 (of 2)
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = dummy_att, index = 1

Generating volume mesh using TetGen.....

Tetgen input string = pYq1.500/0.000QT1.00e-16A
Done meshing using TetGen!
Getting volume mesh for body 2 (of 2)
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = dummy_att, index = 1

Generating volume mesh using TetGen.....

Tetgen input string = pYq1.500/0.000QT1.00e-16A
Done meshing using TetGen!
../csmData/MultiDomain/example2.csm
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = dummy_att, index = 1
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 0
Getting surface mesh for body 1 (of 3)
Getting surface mesh for body 2 (of 3)
Getting surface mesh for body 3 (of 3)
Body 1 (of 3)
Number of nodes    = 386
Number of elements = 768
Number of triangle elements      = 768
Number of quadrilateral elements = 0
Body 2 (of 3)
Number of nodes    = 98
Number of elements = 192
Number of triangle elements      = 192
Number of quadrilateral elements = 0
Body 3 (of 3)
Number of nodes    = 98
Number of elements = 192
Number of triangle elements      = 192
Number of quadrilateral elements = 0
----------------------------
Total number of nodes    = 582
Total number of elements = 1152
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = dummy_att, index = 1
Body 1 number of surface: nodes - 386, elements - 768
Body 2 number of surface: nodes - 98, elements - 192
Body 3 number of surface: nodes - 98, elements - 192
Getting volume mesh

Generating volume mesh using TetGen.....

Tetgen input string = pYq1.500/0.000QT1.00e-16A

Generating volume mesh using TetGen.....

Tetgen input string = pYq1.500/0.000QT1.00e-16A

Generating volume mesh using TetGen.....

Tetgen input string = pYq1.500/0.000QT1.00e-16A
Done meshing using TetGen!
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = dummy_att, index = 1
Body 1 number of surface: nodes - 386, elements - 768
Body 2 number of surface: nodes - 98, elements - 192
Body 3 number of surface: nodes - 98, elements - 192
Getting volume mesh for body 1 (of 3)
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = dummy_att, index = 1

Generating volume mesh using TetGen.....

Tetgen input string = pYq1.500/0.000QT1.00e-16A
Done meshing using TetGen!
Getting volume mesh for body 2 (of 3)
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = dummy_att, index = 1

Generating volume mesh using TetGen.....

Tetgen input string = pYq1.500/0.000QT1.00e-16A
Done meshing using TetGen!
Getting volume mesh for body 3 (of 3)
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = dummy_att, index = 1

Generating volume mesh using TetGen.....

Tetgen input string = pYq1.500/0.000QT1.00e-16A
Done meshing using TetGen!
../csmData/MultiDomain/example3.csm
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = dummy_att, index = 1
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 0
Getting surface mesh for body 1 (of 3)
Getting surface mesh for body 2 (of 3)
Getting surface mesh for body 3 (of 3)
Body 1 (of 3)
Number of nodes    = 351
Number of elements = 698
Number of triangle elements      = 698
Number of quadrilateral elements = 0
Body 2 (of 3)
Number of nodes    = 98
Number of elements = 192
Number of triangle elements      = 192
Number of quadrilateral elements = 0
Body 3 (of 3)
Number of nodes    = 42
Number of elements = 80
Number of triangle elements      = 80
Number of quadrilateral elements = 0
----------------------------
Total number of nodes    = 491
Total number of elements = 970
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = dummy_att, index = 1
Body 1 number of surface: nodes - 351, elements - 698
Body 2 number of surface: nodes - 98, elements - 192
Body 3 number of surface: nodes - 42, elements - 80
Getting volume mesh

Generating volume mesh using TetGen.....

Tetgen input string = pYq1.500/0.000QT1.00e-16A

Generating volume mesh using TetGen.....

Tetgen input string = pYq1.500/0.000QT1.00e-16A

Generating volume mesh using TetGen.....

Tetgen input string = pYq1.500/0.000QT1.00e-16A
Done meshing using TetGen!
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = dummy_att, index = 1
Body 1 number of surface: nodes - 351, elements - 698
Body 2 number of surface: nodes - 98, elements - 192
Body 3 number of surface: nodes - 42, elements - 80
Getting volume mesh for body 1 (of 3)
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = dummy_att, index = 1

Generating volume mesh using TetGen.....

Tetgen input string = pYq1.500/0.000QT1.00e-16A
Done meshing using TetGen!
Getting volume mesh for body 2 (of 3)
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = dummy_att, index = 1

Generating volume mesh using TetGen.....

Tetgen input string = pYq1.500/0.000QT1.00e-16A
Done meshing using TetGen!
Getting volume mesh for body 3 (of 3)
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = dummy_att, index = 1

Generating volume mesh using TetGen.....

Tetgen input string = pYq1.500/0.000QT1.00e-16A
Done meshing using TetGen!
../csmData/MultiDomain/example4.csm
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = dummy_att, index = 1
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 0
Getting surface mesh for body 1 (of 3)
Getting surface mesh for body 2 (of 3)
Getting surface mesh for body 3 (of 3)
Body 1 (of 3)
Number of nodes    = 376
Number of elements = 748
Number of triangle elements      = 748
Number of quadrilateral elements = 0
Body 2 (of 3)
Number of nodes    = 98
Number of elements = 192
Number of triangle elements      = 192
Number of quadrilateral elements = 0
Body 3 (of 3)
Number of nodes    = 42
Number of elements = 80
Number of triangle elements      = 80
Number of quadrilateral elements = 0
----------------------------
Total number of nodes    = 516
Total number of elements = 1020
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = dummy_att, index = 1
Body 1 number of surface: nodes - 376, elements - 748
Body 2 number of surface: nodes - 98, elements - 192
Body 3 number of surface: nodes - 42, elements - 80
Getting volume mesh

Generating volume mesh using TetGen.....

Tetgen input string = pYq1.500/0.000QT1.00e-16A

Generating volume mesh using TetGen.....

Tetgen input string = pYq1.500/0.000QT1.00e-16A

Generating volume mesh using TetGen.....

Tetgen input string = pYq1.500/0.000QT1.00e-16A
Done meshing using TetGen!
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = dummy_att, index = 1
Body 1 number of surface: nodes - 376, elements - 748
Body 2 number of surface: nodes - 98, elements - 192
Body 3 number of surface: nodes - 42, elements - 80
Getting volume mesh for body 1 (of 3)
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = dummy_att, index = 1

Generating volume mesh using TetGen.....

Tetgen input string = pYq1.500/0.000QT1.00e-16A
Done meshing using TetGen!
Getting volume mesh for body 2 (of 3)
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = dummy_att, index = 1

Generating volume mesh using TetGen.....

Tetgen input string = pYq1.500/0.000QT1.00e-16A
Done meshing using TetGen!
Getting volume mesh for body 3 (of 3)
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = dummy_att, index = 1

Generating volume mesh using TetGen.....

Tetgen input string = pYq1.500/0.000QT1.00e-16A
Done meshing using TetGen!
../csmData/MultiDomain/example6.csm
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = dummy_att, index = 1
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 0
Getting surface mesh for body 1 (of 3)
Getting surface mesh for body 2 (of 3)
Getting surface mesh for body 3 (of 3)
Body 1 (of 3)
Number of nodes    = 370
Number of elements = 736
Number of triangle elements      = 736
Number of quadrilateral elements = 0
Body 2 (of 3)
Number of nodes    = 42
Number of elements = 80
Number of triangle elements      = 80
Number of quadrilateral elements = 0
Body 3 (of 3)
Number of nodes    = 42
Number of elements = 80
Number of triangle elements      = 80
Number of quadrilateral elements = 0
----------------------------
Total number of nodes    = 454
Total number of elements = 896
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = dummy_att, index = 1
Body 1 number of surface: nodes - 370, elements - 736
Body 2 number of surface: nodes - 42, elements - 80
Body 3 number of surface: nodes - 42, elements - 80
Getting volume mesh

Generating volume mesh using TetGen.....

Tetgen input string = pYq1.500/0.000QT1.00e-16A

Generating volume mesh using TetGen.....

Tetgen input string = pYq1.500/0.000QT1.00e-16A

Generating volume mesh using TetGen.....

Tetgen input string = pYq1.500/0.000QT1.00e-16A
Done meshing using TetGen!
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = dummy_att, index = 1
Body 1 number of surface: nodes - 370, elements - 736
Body 2 number of surface: nodes - 42, elements - 80
Body 3 number of surface: nodes - 42, elements - 80
Getting volume mesh for body 1 (of 3)
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = dummy_att, index = 1

Generating volume mesh using TetGen.....

Tetgen input string = pYq1.500/0.000QT1.00e-16A
Done meshing using TetGen!
Getting volume mesh for body 2 (of 3)
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = dummy_att, index = 1

Generating volume mesh using TetGen.....

Tetgen input string = pYq1.500/0.000QT1.00e-16A
Done meshing using TetGen!
Getting volume mesh for body 3 (of 3)
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = dummy_att, index = 1

Generating volume mesh using TetGen.....

Tetgen input string = pYq1.500/0.000QT1.00e-16A
Done meshing using TetGen!
../csmData/MultiDomain/example7.csm
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = dummy_att, index = 1
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 0
Getting surface mesh for body 1 (of 3)
Getting surface mesh for body 2 (of 3)
Getting surface mesh for body 3 (of 3)
Body 1 (of 3)
Number of nodes    = 370
Number of elements = 736
Number of triangle elements      = 736
Number of quadrilateral elements = 0
Body 2 (of 3)
Number of nodes    = 126
Number of elements = 252
Number of triangle elements      = 252
Number of quadrilateral elements = 0
Body 3 (of 3)
Number of nodes    = 20
Number of elements = 36
Number of triangle elements      = 36
Number of quadrilateral elements = 0
----------------------------
Total number of nodes    = 516
Total number of elements = 1024
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = dummy_att, index = 1
Body 1 number of surface: nodes - 370, elements - 736
Body 2 number of surface: nodes - 126, elements - 252
Body 3 number of surface: nodes - 20, elements - 36
Getting volume mesh

Generating volume mesh using TetGen.....

Tetgen input string = pYq1.500/0.000QT1.00e-16A

Generating volume mesh using TetGen.....

Tetgen input string = pYq1.500/0.000QT1.00e-16A

Generating volume mesh using TetGen.....

Tetgen input string = pYq1.500/0.000QT1.00e-16A
Done meshing using TetGen!
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = dummy_att, index = 1
Body 1 number of surface: nodes - 370, elements - 736
Body 2 number of surface: nodes - 126, elements - 252
Body 3 number of surface: nodes - 20, elements - 36
Getting volume mesh for body 1 (of 3)
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = dummy_att, index = 1

Generating volume mesh using TetGen.....

Tetgen input string = pYq1.500/0.000QT1.00e-16A
Done meshing using TetGen!
Getting volume mesh for body 2 (of 3)
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = dummy_att, index = 1

Generating volume mesh using TetGen.....

Tetgen input string = pYq1.500/0.000QT1.00e-16A
Done meshing using TetGen!
Getting volume mesh for body 3 (of 3)
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = dummy_att, index = 1

Generating volume mesh using TetGen.....

Tetgen input string = pYq1.500/0.000QT1.00e-16A
Done meshing using TetGen!
../csmData/MultiDomain/example8.csm
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = dummy_att, index = 1
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 0
Getting surface mesh for body 1 (of 3)
Getting surface mesh for body 2 (of 3)
Getting surface mesh for body 3 (of 3)
Body 1 (of 3)
Number of nodes    = 109
Number of elements = 214
Number of triangle elements      = 214
Number of quadrilateral elements = 0
Body 2 (of 3)
Number of nodes    = 48
Number of elements = 96
Number of triangle elements      = 96
Number of quadrilateral elements = 0
Body 3 (of 3)
Number of nodes    = 12
Number of elements = 20
Number of triangle elements      = 20
Number of quadrilateral elements = 0
----------------------------
Total number of nodes    = 169
Total number of elements = 330
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = dummy_att, index = 1
Body 1 number of surface: nodes - 109, elements - 214
Body 2 number of surface: nodes - 48, elements - 96
Body 3 number of surface: nodes - 12, elements - 20
Getting volume mesh

Generating volume mesh using TetGen.....

Tetgen input string = pYq1.500/0.000QT1.00e-16A

Generating volume mesh using TetGen.....

Tetgen input string = pYq1.500/0.000QT1.00e-16A

Generating volume mesh using TetGen.....

Tetgen input string = pYq1.500/0.000QT1.00e-16A
Done meshing using TetGen!
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = dummy_att, index = 1
Body 1 number of surface: nodes - 109, elements - 214
Body 2 number of surface: nodes - 48, elements - 96
Body 3 number of surface: nodes - 12, elements - 20
Getting volume mesh for body 1 (of 3)
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = dummy_att, index = 1

Generating volume mesh using TetGen.....

Tetgen input string = pYq1.500/0.000QT1.00e-16A
Done meshing using TetGen!
Getting volume mesh for body 2 (of 3)
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = dummy_att, index = 1

Generating volume mesh using TetGen.....

Tetgen input string = pYq1.500/0.000QT1.00e-16A
Done meshing using TetGen!
Getting volume mesh for body 3 (of 3)
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = dummy_att, index = 1

Generating volume mesh using TetGen.....

Tetgen input string = pYq1.500/0.000QT1.00e-16A
Done meshing using TetGen!
../csmData/MultiDomain/example9.csm
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = dummy_att, index = 1
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 0
Getting surface mesh for body 1 (of 2)
Getting surface mesh for body 2 (of 2)
Body 1 (of 2)
Number of nodes    = 536
Number of elements = 1072
Number of triangle elements      = 1072
Number of quadrilateral elements = 0
Body 2 (of 2)
Number of nodes    = 544
Number of elements = 1084
Number of triangle elements      = 1084
Number of quadrilateral elements = 0
----------------------------
Total number of nodes    = 1080
Total number of elements = 2156
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = dummy_att, index = 1
Body 1 number of surface: nodes - 536, elements - 1072
Body 2 number of surface: nodes - 544, elements - 1084
Getting volume mesh

Generating volume mesh using TetGen.....

Tetgen input string = pYq1.500/0.000QT1.00e-16A

Generating volume mesh using TetGen.....

Tetgen input string = pYq1.500/0.000QT1.00e-16A
Done meshing using TetGen!
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = dummy_att, index = 1
Body 1 number of surface: nodes - 536, elements - 1072
Body 2 number of surface: nodes - 544, elements - 1084
Getting volume mesh for body 1 (of 2)
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = dummy_att, index = 1

Generating volume mesh using TetGen.....

Tetgen input string = pYq1.500/0.000QT1.00e-16A
Done meshing using TetGen!
Getting volume mesh for body 2 (of 2)
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = dummy_att, index = 1

Generating volume mesh using TetGen.....

Tetgen input string = pYq1.500/0.000QT1.00e-16A
Done meshing using TetGen!
../csmData/MultiDomain/multi_prim.csm
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = dummy_att, index = 1
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 0
Getting surface mesh for body 1 (of 5)
Getting surface mesh for body 2 (of 5)
Getting surface mesh for body 3 (of 5)
Getting surface mesh for body 4 (of 5)
Getting surface mesh for body 5 (of 5)
Body 1 (of 5)
Number of nodes    = 1351
Number of elements = 2682
Number of triangle elements      = 2682
Number of quadrilateral elements = 0
Body 2 (of 5)
Number of nodes    = 288
Number of elements = 572
Number of triangle elements      = 572
Number of quadrilateral elements = 0
Body 3 (of 5)
Number of nodes    = 173
Number of elements = 342
Number of triangle elements      = 342
Number of quadrilateral elements = 0
Body 4 (of 5)
Number of nodes    = 26
Number of elements = 48
Number of triangle elements      = 48
Number of quadrilateral elements = 0
Body 5 (of 5)
Number of nodes    = 482
Number of elements = 960
Number of triangle elements      = 960
Number of quadrilateral elements = 0
----------------------------
Total number of nodes    = 2320
Total number of elements = 4604
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = dummy_att, index = 1
Body 1 number of surface: nodes - 1351, elements - 2682
Body 2 number of surface: nodes - 288, elements - 572
Body 3 number of surface: nodes - 173, elements - 342
Body 4 number of surface: nodes - 26, elements - 48
Body 5 number of surface: nodes - 482, elements - 960
Getting volume mesh

Generating volume mesh using TetGen.....

Tetgen input string = pYq1.500/0.000QT1.00e-16A

Generating volume mesh using TetGen.....

Tetgen input string = pYq1.500/0.000QT1.00e-16A

Generating volume mesh using TetGen.....

Tetgen input string = pYq1.500/0.000QT1.00e-16A

Generating volume mesh using TetGen.....

Tetgen input string = pYq1.500/0.000QT1.00e-16A

Generating volume mesh using TetGen.....

Tetgen input string = pYq1.500/0.000QT1.00e-16A
Done meshing using TetGen!
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = dummy_att, index = 1
Body 1 number of surface: nodes - 1351, elements - 2682
Body 2 number of surface: nodes - 288, elements - 572
Body 3 number of surface: nodes - 173, elements - 342
Body 4 number of surface: nodes - 26, elements - 48
Body 5 number of surface: nodes - 482, elements - 960
Getting volume mesh for body 1 (of 5)
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = dummy_att, index = 1

Generating volume mesh using TetGen.....

Tetgen input string = pYq1.500/0.000QT1.00e-16A
Done meshing using TetGen!
Getting volume mesh for body 2 (of 5)
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = dummy_att, index = 1

Generating volume mesh using TetGen.....

Tetgen input string = pYq1.500/0.000QT1.00e-16A
Done meshing using TetGen!
Getting volume mesh for body 3 (of 5)
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = dummy_att, index = 1

Generating volume mesh using TetGen.....

Tetgen input string = pYq1.500/0.000QT1.00e-16A
Done meshing using TetGen!
Getting volume mesh for body 4 (of 5)
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = dummy_att, index = 1

Generating volume mesh using TetGen.....

Tetgen input string = pYq1.500/0.000QT1.00e-16A
Done meshing using TetGen!
Getting volume mesh for body 5 (of 5)
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = dummy_att, index = 1

Generating volume mesh using TetGen.....

Tetgen input string = pYq1.500/0.000QT1.00e-16A
Done meshing using TetGen!
../csmData/MultiDomain/cyl_seam.csm
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = dummy_att, index = 1
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 0
Getting surface mesh for body 1 (of 2)
Getting surface mesh for body 2 (of 2)
Body 1 (of 2)
Number of nodes    = 443
Number of elements = 882
Number of triangle elements      = 882
Number of quadrilateral elements = 0
Body 2 (of 2)
Number of nodes    = 522
Number of elements = 1044
Number of triangle elements      = 1044
Number of quadrilateral elements = 0
----------------------------
Total number of nodes    = 965
Total number of elements = 1926
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = dummy_att, index = 1
Body 1 number of surface: nodes - 443, elements - 882
Body 2 number of surface: nodes - 522, elements - 1044
Getting volume mesh

Generating volume mesh using TetGen.....

Tetgen input string = pYq1.500/0.000QT1.00e-16A

Generating volume mesh using TetGen.....

Tetgen input string = pYq1.500/0.000QT1.00e-16A
Done meshing using TetGen!
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = dummy_att, index = 1
Body 1 number of surface: nodes - 443, elements - 882
Body 2 number of surface: nodes - 522, elements - 1044
Getting volume mesh for body 1 (of 2)
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = dummy_att, index = 1

Generating volume mesh using TetGen.....

Tetgen input string = pYq1.500/0.000QT1.00e-16A
Done meshing using TetGen!
Getting volume mesh for body 2 (of 2)
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = dummy_att, index = 1

Generating volume mesh using TetGen.....

Tetgen input string = pYq1.500/0.000QT1.00e-16A
Done meshing using TetGen!
ok
test_journal (test_tetgen.TestTETGEN.test_journal) ... Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 2
	Name = Farfield, index = 1
	Name = Wing1, index = 2
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 4
	Name = Farfield, index = 1
	Name = riteWing, index = 2
	Name = leftWing, index = 3
	Name = trailingEdge, index = 4

Getting mesh sizing parameters
	Mesh sizing name - Farfield
	Done getting mesh sizing parameters
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 2
	Name = Farfield, index = 1
	Name = Wing1, index = 2
Number of surface: nodes - 7151, elements - 14294
Getting volume mesh

Generating volume mesh using TetGen.....

Tetgen input string = pYq1.500/0.000QT1.00e-16A
Done meshing using TetGen!
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 2
	Name = Farfield, index = 1
	Name = Wing1, index = 2
Number of surface: nodes - 7151, elements - 14294
Getting volume mesh

Generating volume mesh using TetGen.....

Tetgen input string = pYq2.000/0.000QT1.00e-16A
Done meshing using TetGen!
 EGADS Info: 0 Objects, 0 Reference in Use (of 0) at Close!
 CAPS Info: Hit last success -- going live!
 CAPS Info: Hit last success -- going live!
 CAPS Info: Hit last success -- going live!
 CAPS Info: Hit last success -- going live!
 CAPS Info: Hit last success -- going live!
 CAPS Info: Hit last success -- going live!
 CAPS Info: Hit last success -- going live!
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 2
	Name = Farfield, index = 1
	Name = Wing1, index = 2
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 4
	Name = Farfield, index = 1
	Name = riteWing, index = 2
	Name = leftWing, index = 3
	Name = trailingEdge, index = 4

Getting mesh sizing parameters
	Mesh sizing name - Farfield
	Done getting mesh sizing parameters
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 2
	Name = Farfield, index = 1
	Name = Wing1, index = 2
Number of surface: nodes - 7151, elements - 14294
Getting volume mesh

Generating volume mesh using TetGen.....

Tetgen input string = pYq1.500/0.000QT1.00e-16A
Done meshing using TetGen!
 CAPS Info: Hit last success -- going live!
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 2
	Name = Farfield, index = 1
	Name = Wing1, index = 2
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 4
	Name = Farfield, index = 1
	Name = riteWing, index = 2
	Name = leftWing, index = 3
	Name = trailingEdge, index = 4

Getting mesh sizing parameters
	Mesh sizing name - Farfield
	Done getting mesh sizing parameters
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 2
	Name = Farfield, index = 1
	Name = Wing1, index = 2
 CAPS Info: Hit last success -- going live!
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 2
	Name = Farfield, index = 1
	Name = Wing1, index = 2
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 4
	Name = Farfield, index = 1
	Name = riteWing, index = 2
	Name = leftWing, index = 3
	Name = trailingEdge, index = 4

Getting mesh sizing parameters
	Mesh sizing name - Farfield
	Done getting mesh sizing parameters
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 2
	Name = Farfield, index = 1
	Name = Wing1, index = 2
 CAPS Info: Hit last success -- going live!
 CAPS Info: Hit last success -- going live!
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 2
	Name = Farfield, index = 1
	Name = Wing1, index = 2
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 4
	Name = Farfield, index = 1
	Name = riteWing, index = 2
	Name = leftWing, index = 3
	Name = trailingEdge, index = 4

Getting mesh sizing parameters
	Mesh sizing name - Farfield
	Done getting mesh sizing parameters
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 2
	Name = Farfield, index = 1
	Name = Wing1, index = 2
Number of surface: nodes - 7151, elements - 14294
Getting volume mesh

Generating volume mesh using TetGen.....

Tetgen input string = pYq2.000/0.000QT1.00e-16A
Done meshing using TetGen!
 CAPS Info: Hit last success -- going live!
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 2
	Name = Farfield, index = 1
	Name = Wing1, index = 2
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 4
	Name = Farfield, index = 1
	Name = riteWing, index = 2
	Name = leftWing, index = 3
	Name = trailingEdge, index = 4

Getting mesh sizing parameters
	Mesh sizing name - Farfield
	Done getting mesh sizing parameters
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 2
	Name = Farfield, index = 1
	Name = Wing1, index = 2
ok
test_phase (test_tetgen.TestTETGEN.test_phase) ... Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 2
	Name = Farfield, index = 1
	Name = Wing1, index = 2
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 4
	Name = Farfield, index = 1
	Name = riteWing, index = 2
	Name = leftWing, index = 3
	Name = trailingEdge, index = 4

Getting mesh sizing parameters
	Mesh sizing name - Farfield
	Done getting mesh sizing parameters
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 2
	Name = Farfield, index = 1
	Name = Wing1, index = 2
Number of surface: nodes - 7151, elements - 14294
Getting volume mesh

Generating volume mesh using TetGen.....

Tetgen input string = pYq1.500/0.000QT1.00e-16A
Done meshing using TetGen!
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 2
	Name = Farfield, index = 1
	Name = Wing1, index = 2
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 4
	Name = Farfield, index = 1
	Name = riteWing, index = 2
	Name = leftWing, index = 3
	Name = trailingEdge, index = 4

Getting mesh sizing parameters
	Mesh sizing name - Farfield
	Done getting mesh sizing parameters
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 2
	Name = Farfield, index = 1
	Name = Wing1, index = 2
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 2
	Name = Farfield, index = 1
	Name = Wing1, index = 2
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 4
	Name = Farfield, index = 1
	Name = riteWing, index = 2
	Name = leftWing, index = 3
	Name = trailingEdge, index = 4

Getting mesh sizing parameters
	Mesh sizing name - Farfield
	Done getting mesh sizing parameters
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 2
	Name = Farfield, index = 1
	Name = Wing1, index = 2
Number of surface: nodes - 5882, elements - 11756
Getting volume mesh

Generating volume mesh using TetGen.....

Tetgen input string = pYq1.500/0.000QT1.00e-16A
Done meshing using TetGen!
ok
test_reenter (test_tetgen.TestTETGEN.test_reenter) ... Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 2
	Name = Farfield, index = 1
	Name = Wing1, index = 2
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 4
	Name = Farfield, index = 1
	Name = riteWing, index = 2
	Name = leftWing, index = 3
	Name = trailingEdge, index = 4

Getting mesh sizing parameters
	Mesh sizing name - Farfield
	Done getting mesh sizing parameters
Getting surface mesh for body 1 (of 1)
Body 1 (of 1)
Number of nodes    = 7151
Number of elements = 14294
Number of triangle elements      = 14294
Number of quadrilateral elements = 0
----------------------------
Total number of nodes    = 7151
Total number of elements = 14294
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 2
	Name = Farfield, index = 1
	Name = Wing1, index = 2
Number of surface: nodes - 7151, elements - 14294
Getting volume mesh

Generating volume mesh using TetGen.....

Tetgen input string = pYq1.500/0.000QT1.00e-16A
Done meshing using TetGen!

Writing Binary VTK file ....
Finished writing Binary VTK file


Writing vtk file ....

Writing vtk general file ....
Finished writing vtk file


Writing FAST file ....
Finished writing FAST file


Writing SU2 file ....
Finished writing SU2 file


Writing Binary STL file ....
Finished writing Binary STL file


Writing ASCII STL file ....
Finished writing ASCII STL file


Writing Tecplot file ....
Finished writing Tecplot file

Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 2
	Name = Farfield, index = 1
	Name = Wing1, index = 2
Number of surface: nodes - 7151, elements - 14294
Getting volume mesh

Generating volume mesh using TetGen.....

Tetgen input string = pYq2.000/0.000QT1.00e-16A
Done meshing using TetGen!

Writing Binary VTK file ....
Finished writing Binary VTK file


Writing vtk file ....

Writing vtk general file ....
Finished writing vtk file


Writing FAST file ....
Finished writing FAST file


Writing SU2 file ....
Finished writing SU2 file


Writing Binary STL file ....
Finished writing Binary STL file


Writing ASCII STL file ....
Finished writing ASCII STL file


Writing Tecplot file ....
Finished writing Tecplot file

ok
test_setInput (test_tetgen.TestTETGEN.test_setInput) ...  EGADS Info: 0 Objects, 0 Reference in Use (of 0) at Close!
ok
test_Cl (test_xfoil.Testxfoil_Kulfan.test_Cl) ... ok
test_alpha_custom_increment (test_xfoil.Testxfoil_Kulfan.test_alpha_custom_increment) ... ok
test_CL_uniform_increment (test_xfoil.Testxfoil_NACA.test_CL_uniform_increment) ... ok
test_Cl (test_xfoil.Testxfoil_NACA.test_Cl) ... ok
test_alpha_custom_increment (test_xfoil.Testxfoil_NACA.test_alpha_custom_increment) ... ok
test_alpha_uniform_inrement (test_xfoil.Testxfoil_NACA.test_alpha_uniform_inrement) ... ok
test_append (test_xfoil.Testxfoil_NACA.test_append) ... ok
test_normalize (test_xfoil.Testxfoil_NACA.test_normalize) ... ok
test_phase (test_xfoil.Testxfoil_NACA.test_phase) ... ok
test_Cl (test_xfoil.Testxfoil_Parsec.test_Cl) ... ok
test_alpha_custom_increment (test_xfoil.Testxfoil_Parsec.test_alpha_custom_increment) ... ok
test_Output (test_zaero.TestZAERO.test_Output) ... ok
test_inputs (test_zaero.TestZAERO.test_inputs) ... Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 6
	Name = Ribs, index = 1
	Name = Skin, index = 2
	Name = Spar1, index = 3
	Name = Rib_Root, index = 4
	Name = Spar2, index = 5
	Name = Rib_Root_Point, index = 6
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 2
	Name = LeadingEdge, index = 1
	Name = TrailingEdge, index = 2
Getting surface mesh for body 1 (of 2)
Getting surface mesh for body 2 (of 2)
Body 1 (of 2)
Number of nodes    = 1220
Number of elements = 2680
Number of triangle elements      = 2680
Number of quadrilateral elements = 0
Body 2 (of 2)
Number of nodes    = 1
Number of elements = 0
Number of triangle elements      = 0
Number of quadrilateral elements = 0
----------------------------
Total number of nodes    = 1221
Total number of elements = 2680
Mapping Csys attributes ................
	Number of unique Csys attributes = 0

Getting FEA coordinate systems.......
	Number of coordinate systems - 0
	No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
	Number of unique capsConstraint attributes = 1
	Name = Rib_Root_Point, index = 1
Mapping capsLoad attributes ................
	Number of unique capsLoad attributes = 0
Mapping capsBound attributes ................
	Number of unique capsBound attributes = 1
	Name = Skin_Top, index = 1
Mapping capsConnect attributes ................
	Number of unique capsConnect attributes = 1
	Name = Rib_Root, index = 1
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 6
	Name = Ribs, index = 1
	Name = Skin, index = 2
	Name = Spar1, index = 3
	Name = Rib_Root, index = 4
	Name = Spar2, index = 5
	Name = Rib_Root_Point, index = 6
Setting FEA Data
	Mesh for body = 0
	Number of nodal coordinates = 1220
	Number of elements = 2680
	Elemental Nodes = 0
	Elemental Rods  = 0
	Elemental Tria3 = 2680
	Elemental Quad4 = 0
Setting FEA Data
	Mesh for body = 1
	Number of nodal coordinates = 1
	Number of elements = 1
	Elemental Nodes = 1
	Elemental Rods  = 0
	Elemental Tria3 = 0
	Elemental Quad4 = 0
Combining multiple FEA meshes!
	Combined Number of nodal coordinates = 1221
	Combined Number of elements = 2681
	Combined Elemental Nodes = 1
	Combined Elemental Rods  = 0
	Combined Elemental Tria3 = 2680
	Combined Elemental Quad4 = 0

Getting FEA materials.......
	Number of materials - 1
	Material name - madeupium
	Done getting FEA materials

Getting FEA properties.......
	Number of properties - 6
	Property name - Rib_Root
	Property name - Rib_Root_Point
	Property name - Ribs
	Property name - Skin
	Property name - Spar1
	Property name - Spar2
	Done getting FEA properties
Updating mesh element types based on properties input

'Smart_Restart' is ON
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = Wing, index = 1
Getting vortex lattice surface data
	VLM surface name - WingSurface
	Done getting vortex lattice surface data
Getting vortex lattice control surface data
	VLM control surface name - CntrlLE
	VLM control surface name - CntrlTE
	Done getting vortex lattice control surface data

Getting FEA vortex lattice mesh

Getting ZAERO UAIC Configurations.......
	Number of UAIC Configurations - 2

	UAIC Configuration: climb, id = 1
	- Mach Number : 0.200000
	- Reduced Freq: [0.020000, ... , 0.250000]

	UAIC Configuration: cruise, id = 2
	- Mach Number : 0.700000
	- Reduced Freq: [0.040000, ... , 0.350000]

Getting ZAERO Analysis Subcases.......
	Number of Analysis Subcases - 2

	Analysis Subcase: FlutterCruise, id = 1
	- Discipline : flutter
	- UAIC       : cruise

	Analysis Subcase: Trim, id = 2
	- Discipline : Trim
	- UAIC       : climb

Getting ZAERO Trim Variables.......
	Number of Trim Variables - 2

	Trim Variable: ANGLEA
	- Label : ALPHA
	- Value : free

	Trim Variable: URDD3
	- Label : NZ
	- Value : 1.0

	Updating StaticAeroelastic subcase: Trim
	- vectorToCG -&gt; [0.345898, 1.652951, -0.041403]
	- weight -&gt; 476456.149985
	- weightMomentOfInertia -&gt; [304902.643270, 98963.803823, 69822.813293, 6179.981375, 19723.152208, 370546.335525]
ok

----------------------------------------------------------------------
Ran 154 tests in 466.696s

OK (skipped=10)
+ cd /Users/jenkins/workspace/ESP_bPreBuilt/ESP126/EngSketchPad/CAPSexamples/regressionTest
+ ./execute_CTestRegression.sh
No options provided...defaulting to ALL
Running.... MINIMAL c-Tests
Running.... LINEARAERO c-Tests

=================================================
+ echo './avlTest test;'
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESP126/EngSketchPad/CAPSexamples/regressionTest/cCAPSlog.txt
./avlTest test;
+ ./avlTest 0
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESP126/EngSketchPad/CAPSexamples/regressionTest/cCAPSlog.txt


Attention: avlTest is hard coded to look for ../csmData/avlWingTail.csm
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 2
	Name = Wing, index = 1
	Name = Vertical_Tail, index = 2
Getting vortex lattice control surface data
	VLM control surface name - WingRightLE
	VLM control surface name - WingRightTE
	VLM control surface name - Tail
	Done getting vortex lattice control surface data
Getting vortex lattice surface data
	VLM surface name - Wing
	No "groupName" variable provided or no matches found, going to use tuple name
	VLM surface name - Vertical_Tail
	No "groupName" variable provided or no matches found, going to use tuple name
	Done getting vortex lattice surface data
Warning: Control WingLeftLE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftTE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftLE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftTE not found in controls tuple! Only defaults will be used.
Writing surface - Wing (ID = 0)
	Section 1 of 3 (ID = 1)
	  Control surface 1 of 2 
	  Control surface 2 of 2 
	Section 2 of 3 (ID = 0)
	  Control surface 1 of 4 
	  Control surface 2 of 4 
	  Control surface 3 of 4 
	  Control surface 4 of 4 
	Section 3 of 3 (ID = 2)
	  Control surface 1 of 2 
	  Control surface 2 of 2 
Writing surface - Vertical_Tail (ID = 1)
	Section 1 of 2 (ID = 0)
	  Control surface 1 of 1 
	Section 2 of 2 (ID = 1)
	  Control surface 1 of 1 


Running AVL!


Value of Cltot = 0.619913

StripForces

Wing = {"Xle":[1.565221892029e+00,1.512117367810e+00,1.409527304938e+00,1.264443046659e+00,1.086751845411e+00,8.885630629098e-01,6.833829371601e-01,4.851941546545e-01,3.075029533974e-01,1.624186951053e-01,5.982863221714e-02,6.724107980270e-03,6.724107971058e-03,5.982863219013e-02,1.624186950623e-01,3.075029533414e-01,4.851941545893e-01,6.833829370902e-01,8.885630628399e-01,1.086751845346e+00,1.264443046603e+00,1.409527304895e+00,1.512117367783e+00,1.565221892020e+00],"Yle":[-3.856416046770e+00,-3.725576361740e+00,-3.472813499993e+00,-3.115352832843e+00,-2.677554714026e+00,-2.189254361841e+00,-1.683728638332e+00,-1.195428286135e+00,-7.576301672945e-01,-4.001695001132e-01,-1.474066383261e-01,-1.656695325269e-02,1.656695322999e-02,1.474066382596e-01,4.001695000074e-01,7.576301671565e-01,1.195428285974e+00,1.683728638159e+00,2.189254361668e+00,2.677554713865e+00,3.115352832706e+00,3.472813499887e+00,3.725576361674e+00,3.856416046747e+00],"Zle":[2.486597711706e-01,2.402232939480e-01,2.239252714835e-01,2.008763870743e-01,1.726473841027e-01,1.411620224705e-01,1.085659775407e-01,7.708061590764e-02,4.885161293456e-02,2.580272852328e-02,9.504706056265e-03,1.068228830823e-03,1.068228829360e-03,9.504706051974e-03,2.580272851645e-02,4.885161292566e-02,7.708061589728e-02,1.085659775295e-01,1.411620224593e-01,1.726473840924e-01,2.008763870654e-01,2.239252714767e-01,2.402232939437e-01,2.486597711692e-01],"Chord":[9.710071581587e-01,9.928137666999e-01,1.034940899447e+00,1.094517661923e+00,1.167483996219e+00,1.248867367237e+00,1.333121632734e+00,1.414505003754e+00,1.487471338054e+00,1.547048100535e+00,1.589175233289e+00,1.610981841837e+00,1.610981841841e+00,1.589175233300e+00,1.547048100553e+00,1.487471338077e+00,1.414505003781e+00,1.333121632763e+00,1.248867367266e+00,1.167483996246e+00,1.094517661946e+00,1.034940899465e+00,9.928137667110e-01,9.710071581625e-01],"Area":[6.420432739224e-02,1.924649501823e-01,3.191588402418e-01,4.398794051499e-01,5.463997379092e-01,6.272332670617e-01,6.695492724342e-01,6.620092145623e-01,5.978048871833e-01,4.770843222898e-01,3.080744268775e-01,1.065203328294e-01,1.065203327570e-01,3.080744268129e-01,4.770843222394e-01,5.978048871514e-01,6.620092145502e-01,6.695492724407e-01,6.272332670835e-01,5.463997379421e-01,4.398794051895e-01,3.191588402846e-01,1.924649502262e-01,6.420432743628e-02],"c_cl":[1.751976980130e-01,4.816388142977e-01,7.134545983421e-01,8.955798774849e-01,1.045275116632e+00,1.165642609065e+00,1.251488483105e+00,1.294909342036e+00,1.290147495293e+00,1.237589733954e+00,1.147354354589e+00,1.069716379937e+00,1.027204841579e+00,9.123069911134e-01,8.271224835183e-01,7.465072383823e-01,6.622506856520e-01,5.718077594714e-01,4.773770050899e-01,3.839108464450e-01,2.965810831876e-01,2.166269422077e-01,1.372747954615e-01,4.847522879848e-02],"ai":[2.423376448059e-01,1.891573605669e-01,1.387726073609e-01,1.136377561110e-01,1.056109957987e-01,1.077519869781e-01,1.163918473303e-01,1.297918603655e-01,1.465983278745e-01,1.624995174599e-01,1.707158095744e-01,1.656351191924e-01,-7.833998870070e-02,-4.190817556553e-02,-1.699095118257e-02,-7.589503463777e-04,7.958849673277e-03,1.019416065188e-02,8.688915578617e-03,6.053380335312e-03,5.120395026966e-03,9.296755297777e-03,2.004804046056e-02,3.330492577563e-02],"cl_norm":[2.044051829731e-01,5.494672225940e-01,7.808579037666e-01,9.268407130704e-01,1.014078158135e+00,1.057019341175e+00,1.062951411331e+00,1.036333388587e+00,9.816462634652e-01,9.051794884118e-01,8.167547094730e-01,7.499676468296e-01,7.211772113978e-01,6.503467495436e-01,6.057660560785e-01,5.686988847404e-01,5.305932247981e-01,4.861412346267e-01,4.332732553833e-01,3.727603475166e-01,3.071901673655e-01,2.373206031154e-01,1.568074209165e-01,5.666485024183e-02],"cl":[1.803741931755e-01,4.848688546456e-01,6.890559834541e-01,8.178762563193e-01,8.948575908400e-01,9.327503738518e-01,9.379850374383e-01,9.144963748396e-01,8.662385668547e-01,7.987616435479e-01,7.207325646086e-01,6.617973538491e-01,6.363916792637e-01,5.738884333901e-01,5.345488897542e-01,5.018395375442e-01,4.682137871228e-01,4.289878157184e-01,3.823352848865e-01,3.289366049978e-01,2.710752133780e-01,2.094198967377e-01,1.383722840114e-01,5.000302093674e-02],"cd":[4.708816796009e-03,1.893013552459e-02,2.388458719214e-02,2.809788812558e-02,3.450496926229e-02,4.310977683932e-02,5.296690620746e-02,6.273588035903e-02,7.092746653689e-02,7.623132904844e-02,7.793919402367e-02,1.330641046360e-01,7.642533954135e-02,1.575280561792e-02,1.020926164298e-02,5.734996040024e-03,2.453990236867e-03,7.034156943368e-05,-1.681061755703e-03,-2.904871637690e-03,-3.696799546923e-03,-4.291551637880e-03,-4.755989795801e-03,-4.178738547363e-03],"cdv":[0.000000000000e+00,0.000000000000e+00,0.000000000000e+00,0.000000000000e+00,0.000000000000e+00,0.000000000000e+00,0.000000000000e+00,0.000000000000e+00,0.000000000000e+00,0.000000000000e+00,0.000000000000e+00,0.000000000000e+00,0.000000000000e+00,0.000000000000e+00,0.000000000000e+00,0.000000000000e+00,0.000000000000e+00,0.000000000000e+00,0.000000000000e+00,0.000000000000e+00,0.000000000000e+00,0.000000000000e+00,0.000000000000e+00,0.000000000000e+00],"cm_c/4":[-6.175122770628e-02,-1.541367450247e-01,-1.990020049076e-01,-2.179523703797e-01,-2.259241555999e-01,-2.291785023831e-01,-2.301045091167e-01,-2.293937884748e-01,-2.266765134793e-01,-2.205756980543e-01,-2.089282623641e-01,-1.947906406100e-01,-1.847119741766e-01,-1.559354818193e-01,-1.355315131375e-01,-1.232795365876e-01,-1.170486694970e-01,-1.141869860843e-01,-1.128288355903e-01,-1.117855412668e-01,-1.094863434131e-01,-1.016126232938e-01,-7.889656776595e-02,-3.215621313953e-02],"cm_LE":[-9.907391078322e-02,-2.553625521059e-01,-3.443180862959e-01,-3.917771248733e-01,-4.170475207534e-01,-4.288879437377e-01,-4.309998082913e-01,-4.249313258857e-01,-4.112512348867e-01,-3.899661415021e-01,-3.610798550198e-01,-3.345295675167e-01,-3.190696575593e-01,-2.776668920569e-01,-2.496150543392e-01,-2.306580335185e-01,-2.170714278266e-01,-2.053105443163e-01,-1.932221818516e-01,-1.798625218872e-01,-1.643057066256e-01,-1.427050164897e-01,-1.051753523062e-01,-4.137433282272e-02],"C.P.x/c":[5.923506801009e-01,5.678936810396e-01,5.388038268096e-01,5.164857534324e-01,5.024693961503e-01,4.957018606561e-01,4.953178888068e-01,5.008416597224e-01,5.116790825908e-01,5.261470832206e-01,5.398832002652e-01,5.443357803973e-01,5.402488831883e-01,5.217174153488e-01,5.035437183301e-01,4.956552889214e-01,4.999897967898e-01,5.161776906019e-01,5.451044281037e-01,5.898391652627e-01,6.538965497759e-01,7.352099770688e-01,8.201760893059e-01,8.930854083839e-01]}

Vertical_Tail = {"Xle":[5.481142821257e+00,5.457739875756e+00,5.413224828118e+00,5.351955121359e+00,5.279928261269e+00,5.204194738752e+00,5.132167878660e+00,5.070898171897e+00,5.026383124254e+00,5.002980178746e+00],"Yle":[0.000000000000e+00,0.000000000000e+00,0.000000000000e+00,0.000000000000e+00,0.000000000000e+00,0.000000000000e+00,0.000000000000e+00,0.000000000000e+00,0.000000000000e+00,0.000000000000e+00],"Zle":[1.462285642514e+00,1.415479751513e+00,1.326449656236e+00,1.203910242719e+00,1.059856522538e+00,9.083894775049e-01,7.643357573198e-01,6.417963437947e-01,5.527662485071e-01,5.059603574925e-01],"Chord":[7.291641787429e-01,7.525671242437e-01,7.970821718820e-01,8.583518786405e-01,9.303787387310e-01,1.006112261248e+00,1.078139121340e+00,1.139408828103e+00,1.183923875746e+00,1.207326821254e+00],"Area":[1.727730179136e-02,5.174997687051e-02,8.537019049526e-02,1.158415604078e-01,1.391867381176e-01,1.505166423044e-01,1.455036346588e-01,1.220345306258e-01,8.141205112924e-02,2.860720599220e-02],"c_cl":[4.143502484419e-02,1.146121890397e-01,1.669674480705e-01,2.000258625576e-01,2.165069436650e-01,2.173612378317e-01,2.020982864242e-01,1.687203348327e-01,1.143884794131e-01,4.073751989365e-02],"ai":[2.065296924523e-01,1.849180223915e-01,1.591285664757e-01,1.456224964408e-01,1.435231644007e-01,1.506386553621e-01,1.666466052407e-01,1.914179167695e-01,2.193221173430e-01,2.365321328633e-01],"cl_norm":[6.579957348177e-02,1.763463053601e-01,2.425545992662e-01,2.698370559986e-01,2.694590983040e-01,2.501591871290e-01,2.170544160382e-01,1.714623014106e-01,1.118766125250e-01,3.907064104111e-02],"cl":[5.682537081790e-02,1.522949719002e-01,2.094733190134e-01,2.330348048803e-01,2.327083956801e-01,2.160407403863e-01,1.874510278163e-01,1.480770823179e-01,9.661810337338e-02,3.374191575678e-02],"cd":[4.670566079260e-03,1.374698956983e-02,1.845844898552e-02,2.032218684725e-02,2.072187092673e-02,2.023884851599e-02,1.896705322934e-02,1.657142171121e-02,1.222733795468e-02,5.106244760924e-03],"cdv":[0.000000000000e+00,0.000000000000e+00,0.000000000000e+00,0.000000000000e+00,0.000000000000e+00,0.000000000000e+00,0.000000000000e+00,0.000000000000e+00,0.000000000000e+00,0.000000000000e+00],"cm_c/4":[-3.303465544544e-02,-8.761746958838e-02,-1.194746602282e-01,-1.341488123563e-01,-1.380350789963e-01,-1.339349413680e-01,-1.218867053325e-01,-1.002593790936e-01,-6.716156843032e-02,-2.373448304337e-02],"cm_LE":[-4.232877133357e-02,-1.126299441676e-01,-1.539951982649e-01,-1.724118490116e-01,-1.757829360724e-01,-1.683239687784e-01,-1.510824211718e-01,-1.228726806389e-01,-8.171902803731e-02,-2.878672165377e-02],"C.P.x/c":[8.313363814431e-01,8.253142634661e-01,8.203574125378e-01,8.256599853193e-01,8.431675932569e-01,8.699522420101e-01,9.002322593392e-01,9.270755982234e-01,9.451240614895e-01,9.534124326091e-01]}


real	0m0.474s
user	0m0.259s
sys	0m0.083s
+ status=0
+ set +x

=============================================
CAPS verification (using c-executables) case ./avlTest passed (as expected)
=============================================


=================================================
+ echo './msesTest test;'
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESP126/EngSketchPad/CAPSexamples/regressionTest/cCAPSlog.txt
./msesTest test;
+ ./msesTest 0
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESP126/EngSketchPad/CAPSexamples/regressionTest/cCAPSlog.txt


Attention: msesTest is hard coded to look for ../csmData/airfoilSection.csm

Value of CL = 0.276892 

real	0m1.312s
user	0m1.089s
sys	0m0.042s
+ status=0
+ set +x

=============================================
CAPS verification (using c-executables) case ./msesTest passed (as expected)
=============================================


=================================================
+ echo './frictionTest test;'
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESP126/EngSketchPad/CAPSexamples/regressionTest/cCAPSlog.txt
./frictionTest test;
+ ./frictionTest 0
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESP126/EngSketchPad/CAPSexamples/regressionTest/cCAPSlog.txt


Attention: frictionTest is hard coded to look for ../csmData/frictionWingTailFuselage.csm
To not make system calls to the friction executable the second command line option may be supplied - 0 = no analysis , &gt;0 run analysis (default).

Lifting Surface: Body = 1, units m
	XLE:   1.571946 -3.872983 0.249728
	XTE:   2.536563 -3.872983 0.335335
	Chord: 0.968408
	Arc:   1.985181
	T/C:   0.155975
	Type: Wing
Lifting Surface: Body = 2, units m
	XLE:   0.000000 0.000000 0.000000
	XTE:   1.614012 0.000000 0.002015
	Chord: 1.614013
	Arc:   3.308635
	T/C:   0.127839
	Type: Wing
Lifting Surface: Body = 3, units m
	XLE:   1.571946 3.872983 0.249728
	XTE:   2.536563 3.872983 0.335335
	Chord: 0.968408
	Arc:   1.985181
	T/C:   0.155975
	Type: Wing
Lifting Surface: Body = 4, units m
	XLE:   5.484123 0.000000 1.468246
	XTE:   6.210307 0.000915 1.468246
	Chord: 0.726185
	Arc:   1.482717
	T/C:   0.120035
	Type: VTail
Lifting Surface: Body = 5, units m
	XLE:   5.000000 0.000000 0.500000
	XTE:   6.210307 0.001525 0.500000
	Chord: 1.210308
	Arc:   2.471195
	T/C:   0.120035
	Type: VTail
Lifting Surface: Body = 6, units m
	XLE:   5.484123 -0.968246 0.500000
	XTE:   6.210307 -0.968246 0.500915
	Chord: 0.726185
	Arc:   1.482717
	T/C:   0.120035
	Type: HTail
Lifting Surface: Body = 7, units m
	XLE:   5.484123 0.968246 0.500000
	XTE:   6.210307 0.968246 0.500915
	Chord: 0.726185
	Arc:   1.482717
	T/C:   0.120035
	Type: HTail
Body of Revolution: Body = 8, units m
	Arc: 0.000000
	Diameter: 0.000000
	Type: Fuse
Body of Revolution: Body = 9, units m
	Arc: 3.714180
	Diameter: 1.020621
	Type: Fuse
Body of Revolution: Body = 10, units m
	Arc: 2.771209
	Diameter: 0.645497
	Type: Fuse
Body of Revolution: Body = 11, units m
	Arc: 1.013945
	Diameter: 0.322749
	Type: Fuse
Body of Revolution: Body = 12, units m
	Arc: 0.101394
	Diameter: 0.032275
	Type: Fuse
Number of sections 4, number of revolution sections 1
Number of Mach-Altitude cases = 2


Running FRICTION!


Value of CDfric = 0.009900

Value of CDfric = 0.009190

real	0m0.694s
user	0m0.186s
sys	0m0.038s
+ status=0
+ set +x

=============================================
CAPS verification (using c-executables) case ./frictionTest passed (as expected)
=============================================

Running.... MESH c-Tests
Running.... CFD c-Tests

=================================================
+ echo './fun3dAFLR2Test test;'
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESP126/EngSketchPad/CAPSexamples/regressionTest/cCAPSlog.txt
./fun3dAFLR2Test test;
+ ./fun3dAFLR2Test 0
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESP126/EngSketchPad/CAPSexamples/regressionTest/cCAPSlog.txt


Attention: fun3dAFLR2Test is hard coded to look for ../csmData/cfd2D.csm
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 5
	Name = 2DSlice, index = 1
	Name = TunnelWall, index = 2
	Name = OutFlow, index = 3
	Name = InFlow, index = 4
	Name = Airfoil, index = 5
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 4
	Name = TunnelWall, index = 1
	Name = OutFlow, index = 2
	Name = InFlow, index = 3
	Name = Airfoil, index = 4
Getting 2D mesh for body 1 (of 1)
 
UG PARAM : SETTING INPUT PARAMETERS FROM ARGUMENT VECTOR
 
UG PARAM : mquad                       = 1         
UG PARAM : mpp                         = 3         
 
AFLR2    : ---------------------------------------
AFLR2    : AFLR2 LIBRARY
AFLR2    : ADVANCING-FRONT/LOCAL-RECONNECTION
AFLR2    : TRIA/QUAD GRID GENERATOR
AFLR2    : Version Number 9.18.1
AFLR2    : Version Date   06/11/24 @ 05:52PM
AFLR2    : Compile OS     Darwin 23.5.0 arm64
AFLR2    : Compile Date   06/11/24 @ 05:52PM
AFLR2    : Copyright 1994-2021, D.L. Marcum
AFLR2    : ---------------------------------------
 
AFLR2 IC : INPUT DATA CHECK
 
AFLR2 IC : Nodes, Faces      =       841         0
 
AFLR2    : CPU Time          =     0.000   seconds
 
AFLR2 EG : EDGE GRID RE-GENERATION
 
AFLR2 EG : Nodes, Edges      =       841       841
 
AFLR2    : CPU Time          =     0.000   seconds
 
AFLR2 IG : INITIAL GRID GENERATION
 
AFLR2 IG : Nodes, Faces      =         0         2
AFLR2 IG : Nodes, Faces      =       168       338
AFLR2 IG : Nodes, Faces      =       336       674
AFLR2 IG : Nodes, Faces      =       504      1010
AFLR2 IG : Nodes, Faces      =       617      1236
AFLR2 IG : Nodes, Faces      =       672      1346
AFLR2 IG : Nodes, Faces      =       741      1484
AFLR2 IG : Nodes, Faces      =       803      1608
AFLR2 IG : Nodes, Faces      =       840      1682
AFLR2 IG : Nodes, Faces      =       841      1684
AFLR2 IG : Nodes, Faces      =       845      1684
AFLR2 IG : Nodes, Faces      =       841       841
 
AFLR2    : CPU Time          =     0.002   seconds
 
AFLR2 GG : FIELD GRID GENERATION
 
AFLR2 GGp: Nodes, Faces      =       841       841
AFLR2 GGp: Nodes, Faces      =      1648      2455
AFLR2 GGp: Nodes, Faces      =      2446      4051
AFLR2 GGp: Nodes, Faces      =      3257      5673
AFLR2 GGp: Nodes, Faces      =      4054      7267
AFLR2 GGp: Nodes, Faces      =      4821      8801
AFLR2 GGp: Nodes, Faces      =      5577     10313
AFLR2 GGp: Nodes, Faces      =      6325     11809
AFLR2 GGp: Nodes, Faces      =      7053     13265
AFLR2 GGp: Nodes, Faces      =      7732     14623
AFLR2 GGp: Nodes, Faces      =      8394     15947
AFLR2 GGp: Nodes, Faces      =      9022     17203
AFLR2 GGp: Nodes, Faces      =      9620     18399
AFLR2 GGp: Nodes, Faces      =     10176     19511
AFLR2 GGp: Nodes, Faces      =     10689     20537
AFLR2 GGp: Nodes, Faces      =     11181     21521
AFLR2 GGp: Nodes, Faces      =     11646     22451
AFLR2 GGp: Nodes, Faces      =     12098     23355
AFLR2 GGp: Nodes, Faces      =     12529     24217
AFLR2 GGp: Nodes, Faces      =     12943     25045
AFLR2 GGp: Nodes, Faces      =     13331     25821
AFLR2 GGp: Nodes, Faces      =     13710     26579
AFLR2 GGp: Nodes, Faces      =     14061     27281
AFLR2 GGp: Nodes, Faces      =     14424     28007
AFLR2 GGp: Nodes, Faces      =     14774     28707
AFLR2 GGp: Nodes, Faces      =     15107     29373
AFLR2 GGp: Nodes, Faces      =     15422     30003
AFLR2 GGp: Nodes, Faces      =     15707     30573
AFLR2 GGp: Nodes, Faces      =     15982     31123
AFLR2 GGp: Nodes, Faces      =     16233     31625
AFLR2 GGp: Nodes, Faces      =     16473     32105
AFLR2 GGp: Nodes, Faces      =     16685     32529
AFLR2 GGp: Nodes, Faces      =     16898     32955
AFLR2 GGp: Nodes, Faces      =     17104     33367
AFLR2 GGp: Nodes, Faces      =     17291     33741
AFLR2 GGp: Nodes, Faces      =     17468     34095
AFLR2 GGp: Nodes, Faces      =     17627     34413
AFLR2 GGp: Nodes, Faces      =     17781     34721
AFLR2 GGp: Nodes, Faces      =     17929     35017
AFLR2 GGp: Nodes, Faces      =     18060     35279
AFLR2 GGp: Nodes, Faces      =     18186     35531
AFLR2 GGp: Nodes, Faces      =     18292     35743
AFLR2 GGp: Nodes, Faces      =     18403     35965
AFLR2 GGp: Nodes, Faces      =     18499     36157
AFLR2 GGp: Nodes, Faces      =     18568     36295
AFLR2 GGp: Nodes, Faces      =     18603     36365
AFLR2 GGp: Nodes, Faces      =     18615     36389
 
AFLR2    : CPU Time          =     0.036   seconds
 
AFLR2 QI : QUALITY IMPROVEMENT
 
AFLR2 QI : Nodes, Faces      =     18615     36389
AFLR2 QI : Nodes, Faces      =     18608      1893
AFLR2 QI : Nodes, Faces      =     18608     17241
AFLR2 QI : Nodes, Faces      =     18608     36375
AFLR2 QI : Nodes, Faces      =     18606      1789
AFLR2 QI : Nodes, Faces      =     18606     17291
AFLR2 QI : Nodes, Faces      =     18606     36371
AFLR2 QI : Nodes, Faces      =     18604      1971
AFLR2 QI : Nodes, Faces      =     18604     17198
AFLR2 QI : Nodes, Faces      =     18604     36367
AFLR2 QI : Nodes, Faces      =     18604      2161
AFLR2 QI : Nodes, Faces      =     18604     17103
AFLR2 QI : Nodes, Faces      =     18604     36367
AFLR2 QI : Nodes, Faces      =     18604      2149
AFLR2 QI : Nodes, Faces      =     18604     17109
AFLR2 QI : Nodes, Faces      =     18604      2149
AFLR2 QI : Nodes, Faces      =     18604     17109
 
AFLR2    : CPU Time          =     0.014   seconds
 
AFLR2    : DONE

Writing AFLR3 file ....
Finished writing AFLR3 file

Number of nodes = 18604
Number of elements = 20099
Number of tris = 2149
Number of quad = 17109

Writing Tecplot file ....
Tecplot expects 2D meshes in the x-y plane... attempting to rotate mesh!
Swapping z and y coordinates!
Finished writing Tecplot file

Getting CFD boundary conditions
	Boundary condition name - Airfoil
	Boundary condition name - TunnelWall
	Boundary condition name - InFlow
	Boundary condition name - OutFlow
	Done getting CFD boundary conditions
Python library was linked, but will not be used!

Creating a 3D volume mesh from a 2D surface
	Number of Nodes =  37208
	Number of Prisms =  2149
	Number of Hexahedral =  17109

Writing AFLR3 file ....
Finished writing AFLR3 file


Writing MAPBC file ....
Finished writing MAPBC file

Warning: The fun3d.nml file will be overwritten!
Writing fun3d.nml
Info: No recognized data transfer names found.
 NOT Running fun3d!

real	0m0.765s
user	0m0.601s
sys	0m0.298s
+ status=0
+ set +x

=============================================
CAPS verification (using c-executables) case ./fun3dAFLR2Test passed (as expected)
=============================================


=================================================
+ echo './fun3dTetgenTest test;'
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESP126/EngSketchPad/CAPSexamples/regressionTest/cCAPSlog.txt
./fun3dTetgenTest test;
+ ./fun3dTetgenTest 0
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESP126/EngSketchPad/CAPSexamples/regressionTest/cCAPSlog.txt


Attention: fun3dTetgenTest is hard coded to look for ../csmData/cfdMultiBody.csm
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 3
	Name = Wing1, index = 1
	Name = Wing2, index = 2
	Name = Farfield, index = 3
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 3
	Name = Wing1, index = 1
	Name = Wing2, index = 2
	Name = Farfield, index = 3
Getting surface mesh for body 1 (of 3)
Getting surface mesh for body 2 (of 3)
Getting surface mesh for body 3 (of 3)
Body 1 (of 3)
Number of nodes    = 9573
Number of elements = 19142
Number of triangle elements      = 19142
Number of quadrilateral elements = 0
Body 2 (of 3)
Number of nodes    = 6160
Number of elements = 12316
Number of triangle elements      = 12316
Number of quadrilateral elements = 0
Body 3 (of 3)
Number of nodes    = 258
Number of elements = 512
Number of triangle elements      = 512
Number of quadrilateral elements = 0
----------------------------
Total number of nodes    = 15991
Total number of elements = 31970
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 3
	Name = Wing1, index = 1
	Name = Wing2, index = 2
	Name = Farfield, index = 3
Number of surface: nodes - 15991, elements - 31970
Getting volume mesh

Generating volume mesh using TetGen.....

Tetgen input string = pYq1.500/0.000T1.00e-16A
Delaunizing vertices...
Delaunay seconds:  0.097915
Creating surface mesh ...
Surface mesh seconds:  0.013378
Recovering boundaries...
Boundary recovery seconds:  0.064629
Removing exterior tetrahedra ...
Spreading region attributes.
Exterior tets removal seconds:  0.020058
Recovering Delaunayness...
Delaunay recovery seconds:  0.037709
Refining mesh...
  21316 insertions, added 16799 points, 789925 tetrahedra in queue.
  7098 insertions, added 2909 points, 350791 tetrahedra in queue.
Refinement seconds:  0.751594
Smoothing vertices...
Mesh smoothing seconds:  0.999561
Improving mesh...
Mesh improvement seconds:  0.026511

Writing nodes.
Writing elements.
Writing faces.
Writing edges.

Output seconds:  0.00464
Total running seconds:  2.01617

Statistics:

  Input points: 15991
  Input facets: 31970
  Input segments: 47955
  Input holes: 2
  Input regions: 0

  Mesh points: 37026
  Mesh tetrahedra: 178572
  Mesh faces: 373129
  Mesh faces on exterior boundary: 31970
  Mesh faces on input facets: 31970
  Mesh edges on input segments: 47955
  Steiner points inside domain: 21035

Done meshing using TetGen!
Getting CFD boundary conditions
	Boundary condition name - Wing1
	Boundary condition name - Wing2
	Boundary condition name - Farfield
	Done getting CFD boundary conditions
Python library was linked, but will not be used!

Writing MAPBC file ....
Finished writing MAPBC file

Warning: The fun3d.nml file will be overwritten!
Writing fun3d.nml
Info: No recognized data transfer names found.
 NOT Running fun3d!

real	0m3.828s
user	0m4.143s
sys	0m0.110s
+ status=0
+ set +x

=============================================
CAPS verification (using c-executables) case ./fun3dTetgenTest passed (as expected)
=============================================

Running.... STRUCTURE c-Tests

=================================================
+ echo './interferenceTest test;'
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESP126/EngSketchPad/CAPSexamples/regressionTest/cCAPSlog.txt
./interferenceTest test;
+ ./interferenceTest
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESP126/EngSketchPad/CAPSexamples/regressionTest/cCAPSlog.txt


Note: interferenceTest uses ../csmData/interference.csm
 classifyClouds: EG_generalBoolean = -7!
 classifyClouds: EG_generalBoolean = -7!
 classifyClouds: EG_generalBoolean = -7!
 classifyClouds: EG_generalBoolean = -7!
  1:  1.000000e+00  Box
  2:  5.850521e-01  Sphere
  3:  7.191810e-01  Cylinder
  4:  4.000000e+01  OuterBox

  0.000000e+00  -2.586798e-02   0.000000e+00   0.000000e+00 
 -2.586798e-02   0.000000e+00   0.000000e+00  -2.804399e-02 
  0.000000e+00   0.000000e+00   0.000000e+00   0.000000e+00 
  0.000000e+00  -2.804399e-02   0.000000e+00   1.000000e+00 

 classifyClouds: EG_generalBoolean = -7!
 classifyClouds: EG_generalBoolean = -7!
  1:  1.000000e+00  Box
  2:  5.886885e-01  Sphere
  3:  7.235323e-01  Cylinder

  0.000000e+00  -2.066118e-02   0.000000e+00 
 -2.066118e-02   0.000000e+00   0.000000e+00 
  0.000000e+00   0.000000e+00   0.000000e+00 


real	0m2.421s
user	0m3.859s
sys	0m0.046s
+ status=0
+ set +x

=============================================
CAPS verification (using c-executables) case ./interferenceTest passed (as expected)
=============================================


=================================================
+ echo './hsmCantileverPlateTest test;'
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESP126/EngSketchPad/CAPSexamples/regressionTest/cCAPSlog.txt
./hsmCantileverPlateTest test;
+ ./hsmCantileverPlateTest 0
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESP126/EngSketchPad/CAPSexamples/regressionTest/cCAPSlog.txt


Attention: hsmCantileverPlate is hard coded to look for ../csmData/feaJoinedPlate.csm
Mapping Csys attributes ................
	Number of unique Csys attributes = 1
	Name = plate, index = 1

Getting FEA coordinate systems.......
	Number of coordinate systems - 1
	Coordinate system name - plate
Mapping capsConstraint attributes ................
	Number of unique capsConstraint attributes = 1
	Name = plateEdge, index = 1
Mapping capsLoad attributes ................
	Number of unique capsLoad attributes = 1
	Name = plateTip, index = 1
Mapping capsBound attributes ................
	Number of unique capsBound attributes = 0
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = plate, index = 1
Creating HSM BEM
	Getting quads for BEM!
	Number of nodal coordinates = 40
	Number of elements = 51
	Elemental Tria3 = 0
	Elemental Quad4 = 27

Getting FEA materials.......
	Number of materials - 1
	Material name - Madeupium
	No "materialType" specified for Material tuple Madeupium, defaulting to "Isotropic"
	Done getting FEA materials

Getting FEA properties.......
	Number of properties - 1
	Property name - plate
	No "material" specified for Property tuple plate, defaulting to an index of 1
	Done getting FEA properties

Getting FEA constraints.......
	Number of constraints - 1
	Constraint name - edgeConstraint
	No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement"
	Done getting FEA constraints

Getting FEA loads.......
	Number of loads - 1
	Load name - appliedLoad
	Done getting FEA loads

Writing Nastran grid and connectivity file (in small field format) ....
Finished writing Nastran grid file

Max Adjacency set to = 9
MaxDim = 4, numBCEdge = 3, numBCNode = 4, numJoint = 0
NEED TO ADD MORE CODE TO hsm_setGlobalParameter
NEED TO ADD MORE CODE TO hsm_setNodeBCParameter
NumBCNode = 4
-&gt;HSMSOL
 Matrix Non-zero Entries = 1313

 Converging HSM equation system ...
  iter     dr         dd         dp         rlx   max
   1    0.314E+01  0.628E+01  0.000E+00    0.080  ddx @ (   1.00   0.00   0.00)
   1*   0.341E-01  0.000E+00  0.000E+00    1.000  drx @ (   1.00   0.10   0.00)
   1*   0.326E-02  0.000E+00  0.000E+00    1.000  drx @ (   1.00   0.07   0.00)
   1*   0.438E-04  0.000E+00  0.000E+00    1.000  drx @ (   1.00   0.00   0.00)
   2    0.274E+01  0.521E+01  0.106E-07    0.096  ddx @ (   1.00   0.07   0.00)
   2*   0.321E-01  0.000E+00  0.000E+00    1.000  drx @ (   1.00   0.10   0.00)
   2*   0.373E-02  0.000E+00  0.000E+00    1.000  drz @ (   1.00   0.03   0.00)
   2*   0.777E-04  0.000E+00  0.000E+00    1.000  drz @ (   1.00   0.03   0.00)
   3    0.202E+01  0.439E+01  0.928E-07    0.114  ddz @ (   1.00   0.07   0.00)
   3*   0.442E-01  0.000E+00  0.000E+00    1.000  drz @ (   1.00   0.07   0.00)
   3*   0.623E-02  0.000E+00  0.000E+00    1.000  drz @ (   1.00   0.03   0.00)
   3*   0.163E-03  0.000E+00  0.000E+00    1.000  drz @ (   1.00   0.03   0.00)
   3*   0.167E-06  0.000E+00  0.000E+00    1.000  drz @ (   1.00   0.00   0.00)
   4    0.192E+01  0.476E+01  0.126E-07    0.105  ddz @ (   1.00   0.03   0.00)
   4*   0.335E-01  0.000E+00  0.000E+00    1.000  drz @ (   1.00   0.10   0.00)
   4*   0.332E-02  0.000E+00  0.000E+00    1.000  drz @ (   1.00   0.10   0.00)
   4*   0.451E-04  0.000E+00  0.000E+00    1.000  drz @ (   1.00   0.10   0.00)
   5    0.187E+01  0.394E+01  0.254E-07    0.127  ddz @ (   1.00   0.07   0.00)
   5*   0.353E-01  0.000E+00  0.000E+00    1.000  drz @ (   1.00   0.00   0.00)
   5*   0.379E-02  0.000E+00  0.000E+00    1.000  drz @ (   1.00   0.00   0.00)
   5*   0.638E-04  0.000E+00  0.000E+00    1.000  drz @ (   1.00   0.00   0.00)
   6    0.156E+01  0.300E+01  0.112E-06    0.166  ddx @ (   1.00   0.07   0.00)
   6*   0.326E-01  0.000E+00  0.000E+00    1.000  drz @ (   1.00   0.10   0.00)
   6*   0.575E-02  0.000E+00  0.000E+00    1.000  drx @ (   1.00   0.00   0.00)
   6*   0.193E-03  0.000E+00  0.000E+00    1.000  drx @ (   1.00   0.00   0.00)
   6*   0.272E-06  0.000E+00  0.000E+00    1.000  drx @ (   1.00   0.00   0.00)
   7    0.103E+01  0.323E+01  0.345E-07    0.155  ddx @ (   1.00   0.03   0.00)
   7*   0.259E-01  0.000E+00  0.000E+00    1.000  drx @ (   1.00   0.00   0.00)
   7*   0.297E-02  0.000E+00  0.000E+00    1.000  drx @ (   1.00   0.00   0.00)
   7*   0.435E-04  0.000E+00  0.000E+00    1.000  drx @ (   1.00   0.00   0.00)
   8    0.756E+00  0.259E+01  0.139E-07    0.193  ddx @ (   1.00   0.03   0.00)
   8*   0.295E-01  0.000E+00  0.000E+00    1.000  drx @ (   1.00   0.10   0.00)
   8*   0.350E-02  0.000E+00  0.000E+00    1.000  drx @ (   1.00   0.10   0.00)
   8*   0.587E-04  0.000E+00  0.000E+00    1.000  drx @ (   1.00   0.10   0.00)
   9    0.678E+00  0.179E+01  0.639E-07    0.279  ddx @ (   0.89   0.00   0.00)
   9*   0.330E-01  0.000E+00  0.000E+00    1.000  drx @ (   1.00   0.00   0.00)
   9*   0.457E-02  0.000E+00  0.000E+00    1.000  drx @ (   1.00   0.10   0.00)
   9*   0.167E-03  0.000E+00  0.000E+00    1.000  drz @ (   1.00   0.10   0.00)
   9*   0.264E-06  0.000E+00  0.000E+00    1.000  drz @ (   1.00   0.10   0.00)
  10    0.452E+00  0.171E+01  0.499E-07    0.292  ddz @ (   1.00   0.10   0.00)
  10*   0.166E-01  0.000E+00  0.000E+00    1.000  drz @ (   1.00   0.00   0.00)
  10*   0.239E-02  0.000E+00  0.000E+00    1.000  drz @ (   1.00   0.00   0.00)
  10*   0.393E-04  0.000E+00  0.000E+00    1.000  drz @ (   1.00   0.00   0.00)
  iter     dr         dd         dp         rlx   max
  11    0.257E+00  0.120E+01  0.614E-08    0.417  ddz @ (   1.00   0.00   0.00)
  11*   0.206E-01  0.000E+00  0.000E+00    1.000  drz @ (   1.00   0.10   0.00)
  11*   0.283E-02  0.000E+00  0.000E+00    1.000  drz @ (   1.00   0.10   0.00)
  11*   0.488E-04  0.000E+00  0.000E+00    1.000  drz @ (   1.00   0.10   0.00)
  12    0.131E+00  0.647E+00  0.288E-08    0.772  ddz @ (   0.89   0.10   0.00)
  12*   0.238E-01  0.000E+00  0.000E+00    1.000  drz @ (   1.00   0.00   0.00)
  12*   0.357E-02  0.000E+00  0.000E+00    1.000  drz @ (   1.00   0.00   0.00)
  12*   0.849E-04  0.000E+00  0.000E+00    1.000  drx @ (   1.00   0.00   0.00)
  13    0.393E-01  0.238E+00  0.325E-07    1.000  ddx @ (   1.00   0.03   0.00)
  13*   0.335E-02  0.000E+00  0.000E+00    1.000  drz @ (   1.00   0.10   0.00)
  13*   0.936E-04  0.000E+00  0.000E+00    1.000  drx @ (   1.00   0.10   0.00)
  14    0.475E-03  0.514E-02  0.635E-07    1.000  ddx @ (   1.00   0.00   0.00)
  15    0.893E-06  0.651E-06  0.135E-08    1.000  drx @ (   1.00   0.00   0.00)
  16    0.573E-10  0.216E-09  0.140E-11    1.000  ddx @ (   0.44   0.10   0.00)
  17    0.253E-15  0.930E-15  0.713E-15    1.000  ddx @ (   0.56   0.10   0.00)

 Converging n vectors ...
 it =  1    dn =  0.193E+01   rlx = 1.000  (   9 )
 it =  2    dn =  0.583E-15   rlx = 1.000  (  31 )

 Converging e1,e2 vectors ...
 it =  1    de =  0.285E+01   rlx = 0.351  (  24 )
 it =  2    de =  0.269E+01   rlx = 0.372  (  14 )
 it =  3    de =  0.202E+01   rlx = 0.494  (  14 )
 it =  4    de =  0.122E+01   rlx = 0.820  (  14 )
 it =  5    de =  0.378E+00   rlx = 1.000  (  14 )
 it =  6    de =  0.127E-01   rlx = 1.000  (  40 )
 it =  7    de =  0.524E-06   rlx = 1.000  (  40 )
 it =  8    de =  0.128E-15   rlx = 1.000  (  22 )

 Calculating  strains, stress resultants ...
Writing HSM solution to Tecplot File - hsm_CAPS.dat

real	0m0.628s
user	0m0.251s
sys	0m0.037s
+ status=0
+ set +x

=============================================
CAPS verification (using c-executables) case ./hsmCantileverPlateTest passed (as expected)
=============================================


=================================================
+ echo './hsmSimplePlateTest test;'
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESP126/EngSketchPad/CAPSexamples/regressionTest/cCAPSlog.txt
./hsmSimplePlateTest test;
+ ./hsmSimplePlateTest 0
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESP126/EngSketchPad/CAPSexamples/regressionTest/cCAPSlog.txt


Attention: hsmTest2 is hard coded to look for ../csmData/feaSimplePlate.csm
Mapping Csys attributes ................
	Number of unique Csys attributes = 0

Getting FEA coordinate systems.......
	Number of coordinate systems - 0
	No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
	Number of unique capsConstraint attributes = 1
	Name = plateEdge, index = 1
Mapping capsLoad attributes ................
	Number of unique capsLoad attributes = 1
	Name = plate, index = 1
Mapping capsBound attributes ................
	Number of unique capsBound attributes = 0
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = plate, index = 1
Creating HSM BEM
	Number of nodal coordinates = 100
	Number of elements = 198
	Elemental Tria3 = 162
	Elemental Quad4 = 0

Getting FEA materials.......
	Number of materials - 1
	Material name - Madeupium
	No "materialType" specified for Material tuple Madeupium, defaulting to "Isotropic"
	Done getting FEA materials

Getting FEA properties.......
	Number of properties - 1
	Property name - plate
	No "material" specified for Property tuple plate, defaulting to an index of 1
	Done getting FEA properties

Getting FEA constraints.......
	Number of constraints - 1
	Constraint name - edgeConstraint
	No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement"
	Done getting FEA constraints

Getting FEA loads.......
	Number of loads - 1
	Load name - appliedLoad
	Done getting FEA loads

Writing Nastran grid and connectivity file (in small field format) ....
Finished writing Nastran grid file

Max Adjacency set to = 7
MaxDim = 36, numBCEdge = 0, numBCNode = 36, numJoint = 0
NEED TO ADD MORE CODE TO hsm_setGlobalParameter
NEED TO ADD MORE CODE TO hsm_setNodeBCParameter
NumBCNode = 36
-&gt;HSMSOL
 Matrix Non-zero Entries = 8026

 Converging HSM equation system ...
  iter     dr         dd         dp         rlx   max
   1    0.609E+00  0.519E+01  0.240E+01    0.096  ddy @ (   0.28   0.25   0.00)
   1*   0.571E-01  0.000E+00  0.000E+00    1.000  drz @ (   0.17   0.11   0.00)
   1*   0.159E-01  0.000E+00  0.000E+00    1.000  drz @ (   0.17   0.11   0.00)
   1*   0.254E-02  0.000E+00  0.000E+00    1.000  drz @ (   0.11   0.14   0.00)
   1*   0.837E-04  0.000E+00  0.000E+00    1.000  drz @ (   0.06   0.14   0.00)
   2    0.769E-02  0.753E+00  0.105E+01    0.478  dps @ (   0.00   0.00   0.00)
   2*   0.329E-03  0.000E+00  0.000E+00    1.000  drx @ (   0.06   0.06   0.00)
   2*   0.641E-06  0.000E+00  0.000E+00    1.000  drz @ (   0.06   0.08   0.00)
   3    0.264E-02  0.213E+00  0.280E+00    1.000  dps @ (   0.50   0.00   0.00)
   3*   0.194E-03  0.000E+00  0.000E+00    1.000  drz @ (   0.39   0.11   0.00)
   3*   0.741E-06  0.000E+00  0.000E+00    1.000  drx @ (   0.44   0.03   0.00)
   4    0.119E-03  0.159E-01  0.631E-01    1.000  dps @ (   0.39   0.14   0.00)
   4*   0.306E-05  0.000E+00  0.000E+00    1.000  drx @ (   0.44   0.22   0.00)
   5    0.133E-05  0.441E-03  0.208E-02    1.000  dps @ (   0.06   0.06   0.00)
   6    0.233E-08  0.153E-06  0.694E-06    1.000  dps @ (   0.50   0.00   0.00)
   7    0.378E-15  0.119E-12  0.317E-12    1.000  dps @ (   0.50   0.00   0.00)

 Converging n vectors ...
 it =  1    dn =  0.117E+01   rlx = 1.000  (  66 )
 it =  2    dn =  0.236E-15   rlx = 1.000  (  81 )

 Converging e1,e2 vectors ...
 it =  1    de =  0.357E+00   rlx = 1.000  (  94 )
 it =  2    de =  0.167E+00   rlx = 1.000  (  67 )
 it =  3    de =  0.245E-01   rlx = 1.000  (  76 )
 it =  4    de =  0.567E-02   rlx = 1.000  (  59 )
 it =  5    de =  0.192E-02   rlx = 1.000  (  59 )
 it =  6    de =  0.648E-03   rlx = 1.000  (  59 )
 it =  7    de =  0.219E-03   rlx = 1.000  (  59 )
 it =  8    de =  0.740E-04   rlx = 1.000  (  59 )
 it =  9    de =  0.250E-04   rlx = 1.000  (  59 )
 it = 10    de =  0.845E-05   rlx = 1.000  (  59 )
 it = 11    de =  0.286E-05   rlx = 1.000  (  59 )
 it = 12    de =  0.965E-06   rlx = 1.000  (  59 )
 it = 13    de =  0.326E-06   rlx = 1.000  (  59 )
 it = 14    de =  0.110E-06   rlx = 1.000  (  59 )
 it = 15    de =  0.372E-07   rlx = 1.000  (  59 )
 it = 16    de =  0.126E-07   rlx = 1.000  (  59 )
 it = 17    de =  0.425E-08   rlx = 1.000  (  59 )
 it = 18    de =  0.144E-08   rlx = 1.000  (  59 )
 it = 19    de =  0.485E-09   rlx = 1.000  (  59 )
 it = 20    de =  0.164E-09   rlx = 1.000  (  59 )

 Calculating  strains, stress resultants ...
Writing HSM solution to Tecplot File - hsm_CAPS.dat

real	0m0.587s
user	0m0.404s
sys	0m0.021s
+ status=0
+ set +x

=============================================
CAPS verification (using c-executables) case ./hsmSimplePlateTest passed (as expected)
=============================================


=================================================
+ echo './hsmJoinedPlateTest test;'
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESP126/EngSketchPad/CAPSexamples/regressionTest/cCAPSlog.txt
./hsmJoinedPlateTest test;
+ ./hsmJoinedPlateTest 0
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESP126/EngSketchPad/CAPSexamples/regressionTest/cCAPSlog.txt


Attention: hsmJoinedPlate is hard coded to look for ../csmData/feaJoinedPlate.csm
Mapping Csys attributes ................
	Number of unique Csys attributes = 0

Getting FEA coordinate systems.......
	Number of coordinate systems - 0
	No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
	Number of unique capsConstraint attributes = 1
	Name = plateEdge, index = 1
Mapping capsLoad attributes ................
	Number of unique capsLoad attributes = 1
	Name = plateTip, index = 1
Mapping capsBound attributes ................
	Number of unique capsBound attributes = 0
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = plate, index = 1
Creating HSM BEM
	Getting quads for BEM!
	Number of nodal coordinates = 40
	Number of elements = 56
	Elemental Tria3 = 0
	Elemental Quad4 = 16

Getting FEA materials.......
	Number of materials - 1
	Material name - Madeupium
	No "materialType" specified for Material tuple Madeupium, defaulting to "Isotropic"
	Done getting FEA materials

Getting FEA properties.......
	Number of properties - 1
	Property name - plate
	No "material" specified for Property tuple plate, defaulting to an index of 1
	Done getting FEA properties

Getting FEA constraints.......
	Number of constraints - 1
	Constraint name - edgeConstraint
	No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement"
	Done getting FEA constraints

Getting FEA loads.......
	Number of loads - 1
	Load name - appliedLoad
	Done getting FEA loads

Writing Nastran grid and connectivity file (in small field format) ....
Finished writing Nastran grid file

Max Adjacency set to = 16
MaxDim = 13, numBCEdge = 2, numBCNode = 4, numJoint = 13
NEED TO ADD MORE CODE TO hsm_setGlobalParameter
NEED TO ADD MORE CODE TO hsm_setNodeBCParameter
NumBCNode = 4
-&gt;HSMSOL
 Matrix Non-zero Entries = 1242

 Converging HSM equation system ...
  iter     dr         dd         dp         rlx   max
   1    0.314E+01  0.628E+01  0.000E+00    0.080  ddx @ (   1.00   0.00   0.00)
   1*   0.341E-01  0.000E+00  0.000E+00    1.000  drx @ (   1.00   0.10   0.00)
   1*   0.325E-02  0.000E+00  0.000E+00    1.000  drx @ (   1.00   0.05   0.00)
   1*   0.434E-04  0.000E+00  0.000E+00    1.000  drx @ (   1.00   0.00   0.00)
   2    0.274E+01  0.521E+01  0.118E-07    0.096  ddx @ (   1.00   0.05   0.00)
   2*   0.321E-01  0.000E+00  0.000E+00    1.000  drx @ (   1.00   0.10   0.00)
   2*   0.373E-02  0.000E+00  0.000E+00    1.000  drz @ (   1.00   0.05   0.00)
   2*   0.772E-04  0.000E+00  0.000E+00    1.000  drz @ (   1.00   0.05   0.00)
   3    0.202E+01  0.439E+01  0.107E-06    0.114  ddz @ (   1.00   0.05   0.00)
   3*   0.442E-01  0.000E+00  0.000E+00    1.000  drz @ (   1.00   0.05   0.00)
   3*   0.622E-02  0.000E+00  0.000E+00    1.000  drz @ (   1.00   0.05   0.00)
   3*   0.162E-03  0.000E+00  0.000E+00    1.000  drz @ (   1.00   0.05   0.00)
   3*   0.163E-06  0.000E+00  0.000E+00    1.000  drz @ (   1.00   0.10   0.00)
   4    0.192E+01  0.476E+01  0.147E-07    0.105  ddz @ (   1.00   0.05   0.00)
   4*   0.335E-01  0.000E+00  0.000E+00    1.000  drz @ (   1.00   0.10   0.00)
   4*   0.332E-02  0.000E+00  0.000E+00    1.000  drz @ (   1.00   0.10   0.00)
   4*   0.448E-04  0.000E+00  0.000E+00    1.000  drz @ (   1.00   0.10   0.00)
   5    0.187E+01  0.395E+01  0.296E-07    0.127  ddz @ (   1.00   0.05   0.00)
   5*   0.353E-01  0.000E+00  0.000E+00    1.000  drz @ (   1.00   0.10   0.00)
   5*   0.379E-02  0.000E+00  0.000E+00    1.000  drz @ (   1.00   0.10   0.00)
   5*   0.636E-04  0.000E+00  0.000E+00    1.000  drz @ (   1.00   0.10   0.00)
   6    0.156E+01  0.301E+01  0.131E-06    0.166  ddx @ (   1.00   0.05   0.00)
   6*   0.326E-01  0.000E+00  0.000E+00    1.000  drz @ (   1.00   0.00   0.00)
   6*   0.575E-02  0.000E+00  0.000E+00    1.000  drx @ (   1.00   0.00   0.00)
   6*   0.191E-03  0.000E+00  0.000E+00    1.000  drx @ (   1.00   0.00   0.00)
   6*   0.265E-06  0.000E+00  0.000E+00    1.000  drx @ (   1.00   0.00   0.00)
   7    0.103E+01  0.323E+01  0.408E-07    0.155  ddx @ (   1.00   0.05   0.00)
   7*   0.259E-01  0.000E+00  0.000E+00    1.000  drx @ (   1.00   0.10   0.00)
   7*   0.297E-02  0.000E+00  0.000E+00    1.000  drx @ (   1.00   0.10   0.00)
   7*   0.432E-04  0.000E+00  0.000E+00    1.000  drx @ (   1.00   0.10   0.00)
   8    0.757E+00  0.260E+01  0.162E-07    0.192  ddx @ (   1.00   0.05   0.00)
   8*   0.296E-01  0.000E+00  0.000E+00    1.000  drx @ (   1.00   0.10   0.00)
   8*   0.351E-02  0.000E+00  0.000E+00    1.000  drx @ (   1.00   0.10   0.00)
   8*   0.586E-04  0.000E+00  0.000E+00    1.000  drx @ (   1.00   0.10   0.00)
   9    0.680E+00  0.181E+01  0.753E-07    0.276  ddx @ (   0.88   0.00   0.00)
   9*   0.329E-01  0.000E+00  0.000E+00    1.000  drx @ (   1.00   0.00   0.00)
   9*   0.452E-02  0.000E+00  0.000E+00    1.000  drx @ (   1.00   0.10   0.00)
   9*   0.159E-03  0.000E+00  0.000E+00    1.000  drz @ (   1.00   0.10   0.00)
   9*   0.238E-06  0.000E+00  0.000E+00    1.000  drz @ (   1.00   0.10   0.00)
  10    0.457E+00  0.172E+01  0.586E-07    0.290  ddz @ (   1.00   0.10   0.00)
  10*   0.166E-01  0.000E+00  0.000E+00    1.000  drz @ (   1.00   0.10   0.00)
  10*   0.239E-02  0.000E+00  0.000E+00    1.000  drz @ (   1.00   0.10   0.00)
  10*   0.392E-04  0.000E+00  0.000E+00    1.000  drz @ (   1.00   0.10   0.00)
  iter     dr         dd         dp         rlx   max
  11    0.258E+00  0.122E+01  0.666E-08    0.411  ddz @ (   1.00   0.10   0.00)
  11*   0.207E-01  0.000E+00  0.000E+00    1.000  drz @ (   1.00   0.00   0.00)
  11*   0.284E-02  0.000E+00  0.000E+00    1.000  drz @ (   1.00   0.00   0.00)
  11*   0.486E-04  0.000E+00  0.000E+00    1.000  drz @ (   1.00   0.00   0.00)
  12    0.135E+00  0.660E+00  0.377E-08    0.758  ddz @ (   0.88   0.00   0.00)
  12*   0.242E-01  0.000E+00  0.000E+00    1.000  drz @ (   1.00   0.00   0.00)
  12*   0.368E-02  0.000E+00  0.000E+00    1.000  drz @ (   1.00   0.00   0.00)
  12*   0.869E-04  0.000E+00  0.000E+00    1.000  drx @ (   1.00   0.00   0.00)
  13    0.430E-01  0.257E+00  0.505E-07    1.000  ddx @ (   1.00   0.05   0.00)
  13*   0.395E-02  0.000E+00  0.000E+00    1.000  drz @ (   1.00   0.00   0.00)
  13*   0.128E-03  0.000E+00  0.000E+00    1.000  drx @ (   1.00   0.00   0.00)
  13*   0.196E-06  0.000E+00  0.000E+00    1.000  drx @ (   1.00   0.10   0.00)
  14    0.656E-03  0.680E-02  0.885E-07    1.000  ddx @ (   1.00   0.00   0.00)
  15    0.156E-05  0.177E-05  0.268E-10    1.000  ddx @ (   1.00   0.10   0.00)
  16    0.273E-09  0.106E-08  0.893E-11    1.000  ddx @ (   0.50   0.05   0.00)
  17    0.138E-15  0.353E-15  0.907E-15    1.000  dps @ (   0.38   0.10   0.00)

 Converging n vectors ...
 it =  1    dn =  0.197E+01   rlx = 1.000  (  17 )
 it =  2    dn =  0.866E-15   rlx = 1.000  (  18 )

 Converging e1,e2 vectors ...
 it =  1    de =  0.753E+01   rlx = 0.133  (   1 )
 it =  2    de =  0.309E+01   rlx = 0.324  (  20 )
 it =  3    de =  0.324E+01   rlx = 0.309  (   2 )
 it =  4    de =  0.226E+01   rlx = 0.443  (   2 )
 it =  5    de =  0.140E+01   rlx = 0.716  (   2 )
 it =  6    de =  0.660E+00   rlx = 1.000  (   2 )
 it =  7    de =  0.860E-01   rlx = 1.000  (   2 )
 it =  8    de =  0.228E-03   rlx = 1.000  (   2 )
 it =  9    de =  0.428E-11   rlx = 1.000  (   2 )

 Calculating  strains, stress resultants ...
Writing HSM solution to Tecplot File - hsm_CAPS.dat

real	0m0.406s
user	0m0.208s
sys	0m0.028s
+ status=0
+ set +x

=============================================
CAPS verification (using c-executables) case ./hsmJoinedPlateTest passed (as expected)
=============================================

Running.... AEROELASTIC c-Tests
=================================================
Did not run examples for:

awave
pointwise
Mystran
=================================================

All tests pass!


=================================================
=================================================
+ ./execute_PyTestRegression.sh

=================================================
Using python : /Users/jenkins/workspace/ESP_bPreBuilt/ESP126/Python-3.11.9/bin/python
=================================================

No options provided...defaulting to ALL
Running.... LINEARAERO PyTests

avl: /Users/jenkins/workspace/ESP_bPreBuilt/ESP126/EngSketchPad/bin/avl

=================================================
+ echo 'avl_PyTest.py test;'
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESP126/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
avl_PyTest.py test;
+ python -u avl_PyTest.py -outLevel=0
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESP126/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
Loading AIM
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = Wing, index = 1
Getting vortex lattice surface data
	VLM surface name - Wing
	Done getting vortex lattice surface data
Writing surface - Wing (ID = 0)
	Section 1 of 3 (ID = 0)
	Section 2 of 3 (ID = 1)
	Section 3 of 3 (ID = 2)
CXtot   0.0006119078685800925
CYtot   -6.292592518559147e-15
CZtot   -0.3012861394881712
Cltot   -4.783069014642483e-14
Cmtot   -0.1945055953448147
Cntot   -2.338890054396671e-15
Cl'tot  -4.786422456048383e-14
Cn'tot  -1.50377318550154e-15
CLtot   0.3012509314146395
CDtot   0.00464635348821979
CDvis   0.0
CLff    0.3009503023516151
CYff    -7.7198870803959e-15
CDind   0.00464635348821979
CDff    0.004968969500894849
e       0.9669902146155998
StripForces 
Wing  cl =  [0.02994790451338, 0.08555545178909, 0.1329003532584, 0.1733025192691, 0.2100182422829, 0.2453427152542, 0.279274699636, 0.3101221284185, 0.3355632628219, 0.3531618776071, 0.3603457261529, 0.3542128805661, 0.3542128805657, 0.3603457261529, 0.3531618776083, 0.3355632628247, 0.3101221284231, 0.2792746996423, 0.2453427152618, 0.2100182422917, 0.1733025192796, 0.132900353272, 0.08555545180763, 0.0299479045407]
Wing  cd =  [-0.004234137763148, -0.004494543653181, -0.003752887372721, -0.002739626801633, -0.001762021024329, -0.0007386538946456, 0.0005114598078319, 0.00211914728609, 0.00414518990896, 0.006609094404164, 0.009540018987574, 0.01315518814705, 0.01315518814715, 0.00954001898777, 0.006609094404422, 0.004145189909247, 0.002119147286374, 0.0005114598080921, -0.0007386538944123, -0.001762021024098, -0.002739626801367, -0.003752887372442, -0.004494543653152, -0.00423413776453]

real	0m0.451s
user	0m0.574s
sys	0m0.184s
+ status=0
+ set +x

=================================================
CAPS verification (using pyCAPS) case avl_PyTest.py passed (as expected)
=================================================


=================================================
+ echo 'avl_AutoSpan_PyTest.py test;'
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESP126/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
avl_AutoSpan_PyTest.py test;
+ python -u avl_AutoSpan_PyTest.py -outLevel=0
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESP126/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
Loading AIM
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 3
	Name = Wing1, index = 1
	Name = Wing2, index = 2
	Name = Wing3, index = 3
Getting vortex lattice surface data
	VLM surface name - Wing1
	VLM surface name - Wing2
	VLM surface name - Wing3
	Done getting vortex lattice surface data
Warning: Control WingHinge1 not found in controls tuple! Only defaults will be used.
Warning: Control WingHinge1 not found in controls tuple! Only defaults will be used.
Warning: Control WingHinge1 not found in controls tuple! Only defaults will be used.
Warning: Control WingHinge1 not found in controls tuple! Only defaults will be used.
Writing surface - Wing1 (ID = 0)
	Section 1 of 3 (ID = 0)
	Section 2 of 3 (ID = 1)
	Section 3 of 3 (ID = 2)
Writing surface - Wing2 (ID = 1)
	Section 1 of 7 (ID = 0)
	Section 2 of 7 (ID = 1)
	Section 3 of 7 (ID = 2)
	Section 4 of 7 (ID = 3)
	Section 5 of 7 (ID = 4)
	Section 6 of 7 (ID = 5)
	Section 7 of 7 (ID = 6)
Writing surface - Wing3 (ID = 2)
	Section 1 of 7 (ID = 0)
	Section 2 of 7 (ID = 3)
	  Control surface 1 of 1 
	Section 3 of 7 (ID = 4)
	  Control surface 1 of 1 
	Section 4 of 7 (ID = 1)
	Section 5 of 7 (ID = 5)
	  Control surface 1 of 1 
	Section 6 of 7 (ID = 6)
	  Control surface 1 of 1 
	Section 7 of 7 (ID = 2)
CXtot   -0.04120015660053111
CYtot   2.462543613195682e-10
CZtot   -1.125018850856348
Cltot   1.184580814522611e-09
Cmtot   -1.954741252395341
Cntot   -1.790133030044494e-10
Cl'tot  1.181276184205198e-09
Cn'tot  -1.996598242441884e-10
CLtot   1.124128463157939
CDtot   0.06082816785187402
CDvis   0.0
CLff    1.123105484603622
CYff    2.611430934031642e-10
CDind   0.06082816785187402
CDff    -0.2032104788139517
e       -0.3293015989519321

real	0m5.447s
user	0m5.802s
sys	0m4.400s
+ status=0
+ set +x

=================================================
CAPS verification (using pyCAPS) case avl_AutoSpan_PyTest.py passed (as expected)
=================================================


=================================================
+ echo 'avl_DesignSweep_PyTest.py test;'
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESP126/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
avl_DesignSweep_PyTest.py test;
+ python -u avl_DesignSweep_PyTest.py -outLevel=0 -noPlotData
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESP126/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 2
	Name = Wing, index = 1
	Name = Vertical_Tail, index = 2
Getting vortex lattice surface data
	VLM surface name - Vertical_Tail
	No "groupName" variable provided or no matches found, going to use tuple name
	VLM surface name - Wing
	Done getting vortex lattice surface data
Warning: Control Tail not found in controls tuple! Only defaults will be used.
Warning: Control Tail not found in controls tuple! Only defaults will be used.
Warning: Control WingRightLE not found in controls tuple! Only defaults will be used.
Warning: Control WingRightTE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftLE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftTE not found in controls tuple! Only defaults will be used.
Warning: Control WingRightLE not found in controls tuple! Only defaults will be used.
Warning: Control WingRightTE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftLE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftTE not found in controls tuple! Only defaults will be used.
Writing surface - Vertical_Tail (ID = 0)
	Section 1 of 2 (ID = 0)
	  Control surface 1 of 1 
	Section 2 of 2 (ID = 1)
	  Control surface 1 of 1 
Writing surface - Wing (ID = 1)
	Section 1 of 3 (ID = 1)
	  Control surface 1 of 2 
	  Control surface 2 of 2 
	Section 2 of 3 (ID = 0)
	  Control surface 1 of 4 
	  Control surface 2 of 4 
	  Control surface 3 of 4 
	  Control surface 4 of 4 
	Section 3 of 3 (ID = 2)
	  Control surface 1 of 2 
	  Control surface 2 of 2 
Cd = 0.002572533601550775
Cl = 0.2009337808873524
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 2
	Name = Wing, index = 1
	Name = Vertical_Tail, index = 2
Getting vortex lattice surface data
	VLM surface name - Vertical_Tail
	No "groupName" variable provided or no matches found, going to use tuple name
	VLM surface name - Wing
	Done getting vortex lattice surface data
Warning: Control Tail not found in controls tuple! Only defaults will be used.
Warning: Control Tail not found in controls tuple! Only defaults will be used.
Warning: Control WingRightLE not found in controls tuple! Only defaults will be used.
Warning: Control WingRightTE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftLE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftTE not found in controls tuple! Only defaults will be used.
Warning: Control WingRightLE not found in controls tuple! Only defaults will be used.
Warning: Control WingRightTE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftLE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftTE not found in controls tuple! Only defaults will be used.
Writing surface - Vertical_Tail (ID = 0)
	Section 1 of 2 (ID = 0)
	  Control surface 1 of 1 
	Section 2 of 2 (ID = 1)
	  Control surface 1 of 1 
Writing surface - Wing (ID = 1)
	Section 1 of 3 (ID = 1)
	  Control surface 1 of 2 
	  Control surface 2 of 2 
	Section 2 of 3 (ID = 0)
	  Control surface 1 of 4 
	  Control surface 2 of 4 
	  Control surface 3 of 4 
	  Control surface 4 of 4 
	Section 3 of 3 (ID = 2)
	  Control surface 1 of 2 
	  Control surface 2 of 2 
Cd = 0.002586364230241802
Cl = 0.2015191856814851
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 2
	Name = Wing, index = 1
	Name = Vertical_Tail, index = 2
Getting vortex lattice surface data
	VLM surface name - Vertical_Tail
	No "groupName" variable provided or no matches found, going to use tuple name
	VLM surface name - Wing
	Done getting vortex lattice surface data
Warning: Control Tail not found in controls tuple! Only defaults will be used.
Warning: Control Tail not found in controls tuple! Only defaults will be used.
Warning: Control WingRightLE not found in controls tuple! Only defaults will be used.
Warning: Control WingRightTE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftLE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftTE not found in controls tuple! Only defaults will be used.
Warning: Control WingRightLE not found in controls tuple! Only defaults will be used.
Warning: Control WingRightTE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftLE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftTE not found in controls tuple! Only defaults will be used.
Writing surface - Vertical_Tail (ID = 0)
	Section 1 of 2 (ID = 0)
	  Control surface 1 of 1 
	Section 2 of 2 (ID = 1)
	  Control surface 1 of 1 
Writing surface - Wing (ID = 1)
	Section 1 of 3 (ID = 1)
	  Control surface 1 of 2 
	  Control surface 2 of 2 
	Section 2 of 3 (ID = 0)
	  Control surface 1 of 4 
	  Control surface 2 of 4 
	  Control surface 3 of 4 
	  Control surface 4 of 4 
	Section 3 of 3 (ID = 2)
	  Control surface 1 of 2 
	  Control surface 2 of 2 
Cd = 0.002609799718816161
Cl = 0.202507529643332
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 2
	Name = Wing, index = 1
	Name = Vertical_Tail, index = 2
Getting vortex lattice surface data
	VLM surface name - Vertical_Tail
	No "groupName" variable provided or no matches found, going to use tuple name
	VLM surface name - Wing
	Done getting vortex lattice surface data
Warning: Control Tail not found in controls tuple! Only defaults will be used.
Warning: Control Tail not found in controls tuple! Only defaults will be used.
Warning: Control WingRightLE not found in controls tuple! Only defaults will be used.
Warning: Control WingRightTE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftLE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftTE not found in controls tuple! Only defaults will be used.
Warning: Control WingRightLE not found in controls tuple! Only defaults will be used.
Warning: Control WingRightTE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftLE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftTE not found in controls tuple! Only defaults will be used.
Writing surface - Vertical_Tail (ID = 0)
	Section 1 of 2 (ID = 0)
	  Control surface 1 of 1 
	Section 2 of 2 (ID = 1)
	  Control surface 1 of 1 
Writing surface - Wing (ID = 1)
	Section 1 of 3 (ID = 1)
	  Control surface 1 of 2 
	  Control surface 2 of 2 
	Section 2 of 3 (ID = 0)
	  Control surface 1 of 4 
	  Control surface 2 of 4 
	  Control surface 3 of 4 
	  Control surface 4 of 4 
	Section 3 of 3 (ID = 2)
	  Control surface 1 of 2 
	  Control surface 2 of 2 
Cd = 0.002643444008424624
Cl = 0.2039185811658769
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 2
	Name = Wing, index = 1
	Name = Vertical_Tail, index = 2
Getting vortex lattice surface data
	VLM surface name - Vertical_Tail
	No "groupName" variable provided or no matches found, going to use tuple name
	VLM surface name - Wing
	Done getting vortex lattice surface data
Warning: Control Tail not found in controls tuple! Only defaults will be used.
Warning: Control Tail not found in controls tuple! Only defaults will be used.
Warning: Control WingRightLE not found in controls tuple! Only defaults will be used.
Warning: Control WingRightTE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftLE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftTE not found in controls tuple! Only defaults will be used.
Warning: Control WingRightLE not found in controls tuple! Only defaults will be used.
Warning: Control WingRightTE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftLE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftTE not found in controls tuple! Only defaults will be used.
Writing surface - Vertical_Tail (ID = 0)
	Section 1 of 2 (ID = 0)
	  Control surface 1 of 1 
	Section 2 of 2 (ID = 1)
	  Control surface 1 of 1 
Writing surface - Wing (ID = 1)
	Section 1 of 3 (ID = 1)
	  Control surface 1 of 2 
	  Control surface 2 of 2 
	Section 2 of 3 (ID = 0)
	  Control surface 1 of 4 
	  Control surface 2 of 4 
	  Control surface 3 of 4 
	  Control surface 4 of 4 
	Section 3 of 3 (ID = 2)
	  Control surface 1 of 2 
	  Control surface 2 of 2 
Cd = 0.002688200920998204
Cl = 0.2057816377790584
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 2
	Name = Wing, index = 1
	Name = Vertical_Tail, index = 2
Getting vortex lattice surface data
	VLM surface name - Vertical_Tail
	No "groupName" variable provided or no matches found, going to use tuple name
	VLM surface name - Wing
	Done getting vortex lattice surface data
Warning: Control Tail not found in controls tuple! Only defaults will be used.
Warning: Control Tail not found in controls tuple! Only defaults will be used.
Warning: Control WingRightLE not found in controls tuple! Only defaults will be used.
Warning: Control WingRightTE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftLE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftTE not found in controls tuple! Only defaults will be used.
Warning: Control WingRightLE not found in controls tuple! Only defaults will be used.
Warning: Control WingRightTE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftLE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftTE not found in controls tuple! Only defaults will be used.
Writing surface - Vertical_Tail (ID = 0)
	Section 1 of 2 (ID = 0)
	  Control surface 1 of 1 
	Section 2 of 2 (ID = 1)
	  Control surface 1 of 1 
Writing surface - Wing (ID = 1)
	Section 1 of 3 (ID = 1)
	  Control surface 1 of 2 
	  Control surface 2 of 2 
	Section 2 of 3 (ID = 0)
	  Control surface 1 of 4 
	  Control surface 2 of 4 
	  Control surface 3 of 4 
	  Control surface 4 of 4 
	Section 3 of 3 (ID = 2)
	  Control surface 1 of 2 
	  Control surface 2 of 2 
Cd = 0.002745342060015943
Cl = 0.2081373840559949
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 2
	Name = Wing, index = 1
	Name = Vertical_Tail, index = 2
Getting vortex lattice surface data
	VLM surface name - Vertical_Tail
	No "groupName" variable provided or no matches found, going to use tuple name
	VLM surface name - Wing
	Done getting vortex lattice surface data
Warning: Control Tail not found in controls tuple! Only defaults will be used.
Warning: Control Tail not found in controls tuple! Only defaults will be used.
Warning: Control WingRightLE not found in controls tuple! Only defaults will be used.
Warning: Control WingRightTE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftLE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftTE not found in controls tuple! Only defaults will be used.
Warning: Control WingRightLE not found in controls tuple! Only defaults will be used.
Warning: Control WingRightTE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftLE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftTE not found in controls tuple! Only defaults will be used.
Writing surface - Vertical_Tail (ID = 0)
	Section 1 of 2 (ID = 0)
	  Control surface 1 of 1 
	Section 2 of 2 (ID = 1)
	  Control surface 1 of 1 
Writing surface - Wing (ID = 1)
	Section 1 of 3 (ID = 1)
	  Control surface 1 of 2 
	  Control surface 2 of 2 
	Section 2 of 3 (ID = 0)
	  Control surface 1 of 4 
	  Control surface 2 of 4 
	  Control surface 3 of 4 
	  Control surface 4 of 4 
	Section 3 of 3 (ID = 2)
	  Control surface 1 of 2 
	  Control surface 2 of 2 
Cd = 0.002816610334298771
Cl = 0.2110406736705562
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 2
	Name = Wing, index = 1
	Name = Vertical_Tail, index = 2
Getting vortex lattice surface data
	VLM surface name - Vertical_Tail
	No "groupName" variable provided or no matches found, going to use tuple name
	VLM surface name - Wing
	Done getting vortex lattice surface data
Warning: Control Tail not found in controls tuple! Only defaults will be used.
Warning: Control Tail not found in controls tuple! Only defaults will be used.
Warning: Control WingRightLE not found in controls tuple! Only defaults will be used.
Warning: Control WingRightTE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftLE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftTE not found in controls tuple! Only defaults will be used.
Warning: Control WingRightLE not found in controls tuple! Only defaults will be used.
Warning: Control WingRightTE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftLE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftTE not found in controls tuple! Only defaults will be used.
Writing surface - Vertical_Tail (ID = 0)
	Section 1 of 2 (ID = 0)
	  Control surface 1 of 1 
	Section 2 of 2 (ID = 1)
	  Control surface 1 of 1 
Writing surface - Wing (ID = 1)
	Section 1 of 3 (ID = 1)
	  Control surface 1 of 2 
	  Control surface 2 of 2 
	Section 2 of 3 (ID = 0)
	  Control surface 1 of 4 
	  Control surface 2 of 4 
	  Control surface 3 of 4 
	  Control surface 4 of 4 
	Section 3 of 3 (ID = 2)
	  Control surface 1 of 2 
	  Control surface 2 of 2 
Cd = 0.002904376657734716
Cl = 0.2145646488015997
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 2
	Name = Wing, index = 1
	Name = Vertical_Tail, index = 2
Getting vortex lattice surface data
	VLM surface name - Vertical_Tail
	No "groupName" variable provided or no matches found, going to use tuple name
	VLM surface name - Wing
	Done getting vortex lattice surface data
Warning: Control Tail not found in controls tuple! Only defaults will be used.
Warning: Control Tail not found in controls tuple! Only defaults will be used.
Warning: Control WingRightLE not found in controls tuple! Only defaults will be used.
Warning: Control WingRightTE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftLE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftTE not found in controls tuple! Only defaults will be used.
Warning: Control WingRightLE not found in controls tuple! Only defaults will be used.
Warning: Control WingRightTE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftLE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftTE not found in controls tuple! Only defaults will be used.
Writing surface - Vertical_Tail (ID = 0)
	Section 1 of 2 (ID = 0)
	  Control surface 1 of 1 
	Section 2 of 2 (ID = 1)
	  Control surface 1 of 1 
Writing surface - Wing (ID = 1)
	Section 1 of 3 (ID = 1)
	  Control surface 1 of 2 
	  Control surface 2 of 2 
	Section 2 of 3 (ID = 0)
	  Control surface 1 of 4 
	  Control surface 2 of 4 
	  Control surface 3 of 4 
	  Control surface 4 of 4 
	Section 3 of 3 (ID = 2)
	  Control surface 1 of 2 
	  Control surface 2 of 2 
Cd = 0.003011879793042747
Cl = 0.2188068842334945
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 2
	Name = Wing, index = 1
	Name = Vertical_Tail, index = 2
Getting vortex lattice surface data
	VLM surface name - Vertical_Tail
	No "groupName" variable provided or no matches found, going to use tuple name
	VLM surface name - Wing
	Done getting vortex lattice surface data
Warning: Control Tail not found in controls tuple! Only defaults will be used.
Warning: Control Tail not found in controls tuple! Only defaults will be used.
Warning: Control WingRightLE not found in controls tuple! Only defaults will be used.
Warning: Control WingRightTE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftLE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftTE not found in controls tuple! Only defaults will be used.
Warning: Control WingRightLE not found in controls tuple! Only defaults will be used.
Warning: Control WingRightTE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftLE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftTE not found in controls tuple! Only defaults will be used.
Writing surface - Vertical_Tail (ID = 0)
	Section 1 of 2 (ID = 0)
	  Control surface 1 of 1 
	Section 2 of 2 (ID = 1)
	  Control surface 1 of 1 
Writing surface - Wing (ID = 1)
	Section 1 of 3 (ID = 1)
	  Control surface 1 of 2 
	  Control surface 2 of 2 
	Section 2 of 3 (ID = 0)
	  Control surface 1 of 4 
	  Control surface 2 of 4 
	  Control surface 3 of 4 
	  Control surface 4 of 4 
	Section 3 of 3 (ID = 2)
	  Control surface 1 of 2 
	  Control surface 2 of 2 
Cd = 0.003143602034586226
Cl = 0.2238987294815726
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 2
	Name = Wing, index = 1
	Name = Vertical_Tail, index = 2
Getting vortex lattice surface data
	VLM surface name - Vertical_Tail
	No "groupName" variable provided or no matches found, going to use tuple name
	VLM surface name - Wing
	Done getting vortex lattice surface data
Warning: Control Tail not found in controls tuple! Only defaults will be used.
Warning: Control Tail not found in controls tuple! Only defaults will be used.
Warning: Control WingRightLE not found in controls tuple! Only defaults will be used.
Warning: Control WingRightTE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftLE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftTE not found in controls tuple! Only defaults will be used.
Warning: Control WingRightLE not found in controls tuple! Only defaults will be used.
Warning: Control WingRightTE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftLE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftTE not found in controls tuple! Only defaults will be used.
Writing surface - Vertical_Tail (ID = 0)
	Section 1 of 2 (ID = 0)
	  Control surface 1 of 1 
	Section 2 of 2 (ID = 1)
	  Control surface 1 of 1 
Writing surface - Wing (ID = 1)
	Section 1 of 3 (ID = 1)
	  Control surface 1 of 2 
	  Control surface 2 of 2 
	Section 2 of 3 (ID = 0)
	  Control surface 1 of 4 
	  Control surface 2 of 4 
	  Control surface 3 of 4 
	  Control surface 4 of 4 
	Section 3 of 3 (ID = 2)
	  Control surface 1 of 2 
	  Control surface 2 of 2 
Cd = 0.003305877285452361
Cl = 0.2300199286487156
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 2
	Name = Wing, index = 1
	Name = Vertical_Tail, index = 2
Getting vortex lattice surface data
	VLM surface name - Vertical_Tail
	No "groupName" variable provided or no matches found, going to use tuple name
	VLM surface name - Wing
	Done getting vortex lattice surface data
Warning: Control Tail not found in controls tuple! Only defaults will be used.
Warning: Control Tail not found in controls tuple! Only defaults will be used.
Warning: Control WingRightLE not found in controls tuple! Only defaults will be used.
Warning: Control WingRightTE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftLE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftTE not found in controls tuple! Only defaults will be used.
Warning: Control WingRightLE not found in controls tuple! Only defaults will be used.
Warning: Control WingRightTE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftLE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftTE not found in controls tuple! Only defaults will be used.
Writing surface - Vertical_Tail (ID = 0)
	Section 1 of 2 (ID = 0)
	  Control surface 1 of 1 
	Section 2 of 2 (ID = 1)
	  Control surface 1 of 1 
Writing surface - Wing (ID = 1)
	Section 1 of 3 (ID = 1)
	  Control surface 1 of 2 
	  Control surface 2 of 2 
	Section 2 of 3 (ID = 0)
	  Control surface 1 of 4 
	  Control surface 2 of 4 
	  Control surface 3 of 4 
	  Control surface 4 of 4 
	Section 3 of 3 (ID = 2)
	  Control surface 1 of 2 
	  Control surface 2 of 2 
Cd = 0.003507917885472537
Cl = 0.2374223860296633
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 2
	Name = Wing, index = 1
	Name = Vertical_Tail, index = 2
Getting vortex lattice surface data
	VLM surface name - Vertical_Tail
	No "groupName" variable provided or no matches found, going to use tuple name
	VLM surface name - Wing
	Done getting vortex lattice surface data
Warning: Control Tail not found in controls tuple! Only defaults will be used.
Warning: Control Tail not found in controls tuple! Only defaults will be used.
Warning: Control WingRightLE not found in controls tuple! Only defaults will be used.
Warning: Control WingRightTE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftLE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftTE not found in controls tuple! Only defaults will be used.
Warning: Control WingRightLE not found in controls tuple! Only defaults will be used.
Warning: Control WingRightTE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftLE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftTE not found in controls tuple! Only defaults will be used.
Writing surface - Vertical_Tail (ID = 0)
	Section 1 of 2 (ID = 0)
	  Control surface 1 of 1 
	Section 2 of 2 (ID = 1)
	  Control surface 1 of 1 
Writing surface - Wing (ID = 1)
	Section 1 of 3 (ID = 1)
	  Control surface 1 of 2 
	  Control surface 2 of 2 
	Section 2 of 3 (ID = 0)
	  Control surface 1 of 4 
	  Control surface 2 of 4 
	  Control surface 3 of 4 
	  Control surface 4 of 4 
	Section 3 of 3 (ID = 2)
	  Control surface 1 of 2 
	  Control surface 2 of 2 
Cd = 0.003763643677259966
Cl = 0.2464707142744908
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 2
	Name = Wing, index = 1
	Name = Vertical_Tail, index = 2
Getting vortex lattice surface data
	VLM surface name - Vertical_Tail
	No "groupName" variable provided or no matches found, going to use tuple name
	VLM surface name - Wing
	Done getting vortex lattice surface data
Warning: Control Tail not found in controls tuple! Only defaults will be used.
Warning: Control Tail not found in controls tuple! Only defaults will be used.
Warning: Control WingRightLE not found in controls tuple! Only defaults will be used.
Warning: Control WingRightTE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftLE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftTE not found in controls tuple! Only defaults will be used.
Warning: Control WingRightLE not found in controls tuple! Only defaults will be used.
Warning: Control WingRightTE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftLE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftTE not found in controls tuple! Only defaults will be used.
Writing surface - Vertical_Tail (ID = 0)
	Section 1 of 2 (ID = 0)
	  Control surface 1 of 1 
	Section 2 of 2 (ID = 1)
	  Control surface 1 of 1 
Writing surface - Wing (ID = 1)
	Section 1 of 3 (ID = 1)
	  Control surface 1 of 2 
	  Control surface 2 of 2 
	Section 2 of 3 (ID = 0)
	  Control surface 1 of 4 
	  Control surface 2 of 4 
	  Control surface 3 of 4 
	  Control surface 4 of 4 
	Section 3 of 3 (ID = 2)
	  Control surface 1 of 2 
	  Control surface 2 of 2 
Cd = 0.004095167898227208
Cl = 0.25771580677477
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 2
	Name = Wing, index = 1
	Name = Vertical_Tail, index = 2
Getting vortex lattice surface data
	VLM surface name - Vertical_Tail
	No "groupName" variable provided or no matches found, going to use tuple name
	VLM surface name - Wing
	Done getting vortex lattice surface data
Warning: Control Tail not found in controls tuple! Only defaults will be used.
Warning: Control Tail not found in controls tuple! Only defaults will be used.
Warning: Control WingRightLE not found in controls tuple! Only defaults will be used.
Warning: Control WingRightTE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftLE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftTE not found in controls tuple! Only defaults will be used.
Warning: Control WingRightLE not found in controls tuple! Only defaults will be used.
Warning: Control WingRightTE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftLE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftTE not found in controls tuple! Only defaults will be used.
Writing surface - Vertical_Tail (ID = 0)
	Section 1 of 2 (ID = 0)
	  Control surface 1 of 1 
	Section 2 of 2 (ID = 1)
	  Control surface 1 of 1 
Writing surface - Wing (ID = 1)
	Section 1 of 3 (ID = 1)
	  Control surface 1 of 2 
	  Control surface 2 of 2 
	Section 2 of 3 (ID = 0)
	  Control surface 1 of 4 
	  Control surface 2 of 4 
	  Control surface 3 of 4 
	  Control surface 4 of 4 
	Section 3 of 3 (ID = 2)
	  Control surface 1 of 2 
	  Control surface 2 of 2 
Cd = 0.004540047408135333
Cl = 0.2720394012163583
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 2
	Name = Wing, index = 1
	Name = Vertical_Tail, index = 2
Getting vortex lattice surface data
	VLM surface name - Vertical_Tail
	No "groupName" variable provided or no matches found, going to use tuple name
	VLM surface name - Wing
	Done getting vortex lattice surface data
Warning: Control Tail not found in controls tuple! Only defaults will be used.
Warning: Control Tail not found in controls tuple! Only defaults will be used.
Warning: Control WingRightLE not found in controls tuple! Only defaults will be used.
Warning: Control WingRightTE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftLE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftTE not found in controls tuple! Only defaults will be used.
Warning: Control WingRightLE not found in controls tuple! Only defaults will be used.
Warning: Control WingRightTE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftLE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftTE not found in controls tuple! Only defaults will be used.
Writing surface - Vertical_Tail (ID = 0)
	Section 1 of 2 (ID = 0)
	  Control surface 1 of 1 
	Section 2 of 2 (ID = 1)
	  Control surface 1 of 1 
Writing surface - Wing (ID = 1)
	Section 1 of 3 (ID = 1)
	  Control surface 1 of 2 
	  Control surface 2 of 2 
	Section 2 of 3 (ID = 0)
	  Control surface 1 of 4 
	  Control surface 2 of 4 
	  Control surface 3 of 4 
	  Control surface 4 of 4 
	Section 3 of 3 (ID = 2)
	  Control surface 1 of 2 
	  Control surface 2 of 2 
Cd = 0.005168237926851883
Cl = 0.2909701507463254
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 2
	Name = Wing, index = 1
	Name = Vertical_Tail, index = 2
Getting vortex lattice surface data
	VLM surface name - Vertical_Tail
	No "groupName" variable provided or no matches found, going to use tuple name
	VLM surface name - Wing
	Done getting vortex lattice surface data
Warning: Control Tail not found in controls tuple! Only defaults will be used.
Warning: Control Tail not found in controls tuple! Only defaults will be used.
Warning: Control WingRightLE not found in controls tuple! Only defaults will be used.
Warning: Control WingRightTE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftLE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftTE not found in controls tuple! Only defaults will be used.
Warning: Control WingRightLE not found in controls tuple! Only defaults will be used.
Warning: Control WingRightTE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftLE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftTE not found in controls tuple! Only defaults will be used.
Writing surface - Vertical_Tail (ID = 0)
	Section 1 of 2 (ID = 0)
	  Control surface 1 of 1 
	Section 2 of 2 (ID = 1)
	  Control surface 1 of 1 
Writing surface - Wing (ID = 1)
	Section 1 of 3 (ID = 1)
	  Control surface 1 of 2 
	  Control surface 2 of 2 
	Section 2 of 3 (ID = 0)
	  Control surface 1 of 4 
	  Control surface 2 of 4 
	  Control surface 3 of 4 
	  Control surface 4 of 4 
	Section 3 of 3 (ID = 2)
	  Control surface 1 of 2 
	  Control surface 2 of 2 
Cd = 0.006128930715329168
Cl = 0.317487548593558
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 2
	Name = Wing, index = 1
	Name = Vertical_Tail, index = 2
Getting vortex lattice surface data
	VLM surface name - Vertical_Tail
	No "groupName" variable provided or no matches found, going to use tuple name
	VLM surface name - Wing
	Done getting vortex lattice surface data
Warning: Control Tail not found in controls tuple! Only defaults will be used.
Warning: Control Tail not found in controls tuple! Only defaults will be used.
Warning: Control WingRightLE not found in controls tuple! Only defaults will be used.
Warning: Control WingRightTE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftLE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftTE not found in controls tuple! Only defaults will be used.
Warning: Control WingRightLE not found in controls tuple! Only defaults will be used.
Warning: Control WingRightTE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftLE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftTE not found in controls tuple! Only defaults will be used.
Writing surface - Vertical_Tail (ID = 0)
	Section 1 of 2 (ID = 0)
	  Control surface 1 of 1 
	Section 2 of 2 (ID = 1)
	  Control surface 1 of 1 
Writing surface - Wing (ID = 1)
	Section 1 of 3 (ID = 1)
	  Control surface 1 of 2 
	  Control surface 2 of 2 
	Section 2 of 3 (ID = 0)
	  Control surface 1 of 4 
	  Control surface 2 of 4 
	  Control surface 3 of 4 
	  Control surface 4 of 4 
	Section 3 of 3 (ID = 2)
	  Control surface 1 of 2 
	  Control surface 2 of 2 
Cd = 0.007818359051271666
Cl = 0.3586078919918751
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 2
	Name = Wing, index = 1
	Name = Vertical_Tail, index = 2
Getting vortex lattice surface data
	VLM surface name - Vertical_Tail
	No "groupName" variable provided or no matches found, going to use tuple name
	VLM surface name - Wing
	Done getting vortex lattice surface data
Warning: Control Tail not found in controls tuple! Only defaults will be used.
Warning: Control Tail not found in controls tuple! Only defaults will be used.
Warning: Control WingRightLE not found in controls tuple! Only defaults will be used.
Warning: Control WingRightTE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftLE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftTE not found in controls tuple! Only defaults will be used.
Warning: Control WingRightLE not found in controls tuple! Only defaults will be used.
Warning: Control WingRightTE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftLE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftTE not found in controls tuple! Only defaults will be used.
Writing surface - Vertical_Tail (ID = 0)
	Section 1 of 2 (ID = 0)
	  Control surface 1 of 1 
	Section 2 of 2 (ID = 1)
	  Control surface 1 of 1 
Writing surface - Wing (ID = 1)
	Section 1 of 3 (ID = 1)
	  Control surface 1 of 2 
	  Control surface 2 of 2 
	Section 2 of 3 (ID = 0)
	  Control surface 1 of 4 
	  Control surface 2 of 4 
	  Control surface 3 of 4 
	  Control surface 4 of 4 
	Section 3 of 3 (ID = 2)
	  Control surface 1 of 2 
	  Control surface 2 of 2 
Cd = 0.01186220444373961
Cl = 0.4382638635243895
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 2
	Name = Wing, index = 1
	Name = Vertical_Tail, index = 2
Getting vortex lattice surface data
	VLM surface name - Vertical_Tail
	No "groupName" variable provided or no matches found, going to use tuple name
	VLM surface name - Wing
	Done getting vortex lattice surface data
Warning: Control Tail not found in controls tuple! Only defaults will be used.
Warning: Control Tail not found in controls tuple! Only defaults will be used.
Warning: Control WingRightLE not found in controls tuple! Only defaults will be used.
Warning: Control WingRightTE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftLE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftTE not found in controls tuple! Only defaults will be used.
Warning: Control WingRightLE not found in controls tuple! Only defaults will be used.
Warning: Control WingRightTE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftLE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftTE not found in controls tuple! Only defaults will be used.
Writing surface - Vertical_Tail (ID = 0)
	Section 1 of 2 (ID = 0)
	  Control surface 1 of 1 
	Section 2 of 2 (ID = 1)
	  Control surface 1 of 1 
Writing surface - Wing (ID = 1)
	Section 1 of 3 (ID = 1)
	  Control surface 1 of 2 
	  Control surface 2 of 2 
	Section 2 of 3 (ID = 0)
	  Control surface 1 of 4 
	  Control surface 2 of 4 
	  Control surface 3 of 4 
	  Control surface 4 of 4 
	Section 3 of 3 (ID = 2)
	  Control surface 1 of 2 
	  Control surface 2 of 2 
Cd = 0.002572533601550775
Cl = 0.2009337808873524
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 2
	Name = Wing, index = 1
	Name = Vertical_Tail, index = 2
Getting vortex lattice surface data
	VLM surface name - Vertical_Tail
	No "groupName" variable provided or no matches found, going to use tuple name
	VLM surface name - Wing
	Done getting vortex lattice surface data
Warning: Control Tail not found in controls tuple! Only defaults will be used.
Warning: Control Tail not found in controls tuple! Only defaults will be used.
Warning: Control WingRightLE not found in controls tuple! Only defaults will be used.
Warning: Control WingRightTE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftLE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftTE not found in controls tuple! Only defaults will be used.
Warning: Control WingRightLE not found in controls tuple! Only defaults will be used.
Warning: Control WingRightTE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftLE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftTE not found in controls tuple! Only defaults will be used.
Writing surface - Vertical_Tail (ID = 0)
	Section 1 of 2 (ID = 0)
	  Control surface 1 of 1 
	Section 2 of 2 (ID = 1)
	  Control surface 1 of 1 
Writing surface - Wing (ID = 1)
	Section 1 of 3 (ID = 1)
	  Control surface 1 of 2 
	  Control surface 2 of 2 
	Section 2 of 3 (ID = 0)
	  Control surface 1 of 4 
	  Control surface 2 of 4 
	  Control surface 3 of 4 
	  Control surface 4 of 4 
	Section 3 of 3 (ID = 2)
	  Control surface 1 of 2 
	  Control surface 2 of 2 
Cd = 0.002586364230241802
Cl = 0.2015191856814851
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 2
	Name = Wing, index = 1
	Name = Vertical_Tail, index = 2
Getting vortex lattice surface data
	VLM surface name - Vertical_Tail
	No "groupName" variable provided or no matches found, going to use tuple name
	VLM surface name - Wing
	Done getting vortex lattice surface data
Warning: Control Tail not found in controls tuple! Only defaults will be used.
Warning: Control Tail not found in controls tuple! Only defaults will be used.
Warning: Control WingRightLE not found in controls tuple! Only defaults will be used.
Warning: Control WingRightTE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftLE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftTE not found in controls tuple! Only defaults will be used.
Warning: Control WingRightLE not found in controls tuple! Only defaults will be used.
Warning: Control WingRightTE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftLE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftTE not found in controls tuple! Only defaults will be used.
Writing surface - Vertical_Tail (ID = 0)
	Section 1 of 2 (ID = 0)
	  Control surface 1 of 1 
	Section 2 of 2 (ID = 1)
	  Control surface 1 of 1 
Writing surface - Wing (ID = 1)
	Section 1 of 3 (ID = 1)
	  Control surface 1 of 2 
	  Control surface 2 of 2 
	Section 2 of 3 (ID = 0)
	  Control surface 1 of 4 
	  Control surface 2 of 4 
	  Control surface 3 of 4 
	  Control surface 4 of 4 
	Section 3 of 3 (ID = 2)
	  Control surface 1 of 2 
	  Control surface 2 of 2 
Cd = 0.002609799718816161
Cl = 0.202507529643332
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 2
	Name = Wing, index = 1
	Name = Vertical_Tail, index = 2
Getting vortex lattice surface data
	VLM surface name - Vertical_Tail
	No "groupName" variable provided or no matches found, going to use tuple name
	VLM surface name - Wing
	Done getting vortex lattice surface data
Warning: Control Tail not found in controls tuple! Only defaults will be used.
Warning: Control Tail not found in controls tuple! Only defaults will be used.
Warning: Control WingRightLE not found in controls tuple! Only defaults will be used.
Warning: Control WingRightTE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftLE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftTE not found in controls tuple! Only defaults will be used.
Warning: Control WingRightLE not found in controls tuple! Only defaults will be used.
Warning: Control WingRightTE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftLE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftTE not found in controls tuple! Only defaults will be used.
Writing surface - Vertical_Tail (ID = 0)
	Section 1 of 2 (ID = 0)
	  Control surface 1 of 1 
	Section 2 of 2 (ID = 1)
	  Control surface 1 of 1 
Writing surface - Wing (ID = 1)
	Section 1 of 3 (ID = 1)
	  Control surface 1 of 2 
	  Control surface 2 of 2 
	Section 2 of 3 (ID = 0)
	  Control surface 1 of 4 
	  Control surface 2 of 4 
	  Control surface 3 of 4 
	  Control surface 4 of 4 
	Section 3 of 3 (ID = 2)
	  Control surface 1 of 2 
	  Control surface 2 of 2 
Cd = 0.002643444008424624
Cl = 0.2039185811658769
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 2
	Name = Wing, index = 1
	Name = Vertical_Tail, index = 2
Getting vortex lattice surface data
	VLM surface name - Vertical_Tail
	No "groupName" variable provided or no matches found, going to use tuple name
	VLM surface name - Wing
	Done getting vortex lattice surface data
Warning: Control Tail not found in controls tuple! Only defaults will be used.
Warning: Control Tail not found in controls tuple! Only defaults will be used.
Warning: Control WingRightLE not found in controls tuple! Only defaults will be used.
Warning: Control WingRightTE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftLE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftTE not found in controls tuple! Only defaults will be used.
Warning: Control WingRightLE not found in controls tuple! Only defaults will be used.
Warning: Control WingRightTE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftLE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftTE not found in controls tuple! Only defaults will be used.
Writing surface - Vertical_Tail (ID = 0)
	Section 1 of 2 (ID = 0)
	  Control surface 1 of 1 
	Section 2 of 2 (ID = 1)
	  Control surface 1 of 1 
Writing surface - Wing (ID = 1)
	Section 1 of 3 (ID = 1)
	  Control surface 1 of 2 
	  Control surface 2 of 2 
	Section 2 of 3 (ID = 0)
	  Control surface 1 of 4 
	  Control surface 2 of 4 
	  Control surface 3 of 4 
	  Control surface 4 of 4 
	Section 3 of 3 (ID = 2)
	  Control surface 1 of 2 
	  Control surface 2 of 2 
Cd = 0.002688200920998204
Cl = 0.2057816377790584
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 2
	Name = Wing, index = 1
	Name = Vertical_Tail, index = 2
Getting vortex lattice surface data
	VLM surface name - Vertical_Tail
	No "groupName" variable provided or no matches found, going to use tuple name
	VLM surface name - Wing
	Done getting vortex lattice surface data
Warning: Control Tail not found in controls tuple! Only defaults will be used.
Warning: Control Tail not found in controls tuple! Only defaults will be used.
Warning: Control WingRightLE not found in controls tuple! Only defaults will be used.
Warning: Control WingRightTE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftLE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftTE not found in controls tuple! Only defaults will be used.
Warning: Control WingRightLE not found in controls tuple! Only defaults will be used.
Warning: Control WingRightTE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftLE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftTE not found in controls tuple! Only defaults will be used.
Writing surface - Vertical_Tail (ID = 0)
	Section 1 of 2 (ID = 0)
	  Control surface 1 of 1 
	Section 2 of 2 (ID = 1)
	  Control surface 1 of 1 
Writing surface - Wing (ID = 1)
	Section 1 of 3 (ID = 1)
	  Control surface 1 of 2 
	  Control surface 2 of 2 
	Section 2 of 3 (ID = 0)
	  Control surface 1 of 4 
	  Control surface 2 of 4 
	  Control surface 3 of 4 
	  Control surface 4 of 4 
	Section 3 of 3 (ID = 2)
	  Control surface 1 of 2 
	  Control surface 2 of 2 
Cd = 0.002745342060015943
Cl = 0.2081373840559949
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 2
	Name = Wing, index = 1
	Name = Vertical_Tail, index = 2
Getting vortex lattice surface data
	VLM surface name - Vertical_Tail
	No "groupName" variable provided or no matches found, going to use tuple name
	VLM surface name - Wing
	Done getting vortex lattice surface data
Warning: Control Tail not found in controls tuple! Only defaults will be used.
Warning: Control Tail not found in controls tuple! Only defaults will be used.
Warning: Control WingRightLE not found in controls tuple! Only defaults will be used.
Warning: Control WingRightTE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftLE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftTE not found in controls tuple! Only defaults will be used.
Warning: Control WingRightLE not found in controls tuple! Only defaults will be used.
Warning: Control WingRightTE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftLE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftTE not found in controls tuple! Only defaults will be used.
Writing surface - Vertical_Tail (ID = 0)
	Section 1 of 2 (ID = 0)
	  Control surface 1 of 1 
	Section 2 of 2 (ID = 1)
	  Control surface 1 of 1 
Writing surface - Wing (ID = 1)
	Section 1 of 3 (ID = 1)
	  Control surface 1 of 2 
	  Control surface 2 of 2 
	Section 2 of 3 (ID = 0)
	  Control surface 1 of 4 
	  Control surface 2 of 4 
	  Control surface 3 of 4 
	  Control surface 4 of 4 
	Section 3 of 3 (ID = 2)
	  Control surface 1 of 2 
	  Control surface 2 of 2 
Cd = 0.002816610334298771
Cl = 0.2110406736705562
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 2
	Name = Wing, index = 1
	Name = Vertical_Tail, index = 2
Getting vortex lattice surface data
	VLM surface name - Vertical_Tail
	No "groupName" variable provided or no matches found, going to use tuple name
	VLM surface name - Wing
	Done getting vortex lattice surface data
Warning: Control Tail not found in controls tuple! Only defaults will be used.
Warning: Control Tail not found in controls tuple! Only defaults will be used.
Warning: Control WingRightLE not found in controls tuple! Only defaults will be used.
Warning: Control WingRightTE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftLE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftTE not found in controls tuple! Only defaults will be used.
Warning: Control WingRightLE not found in controls tuple! Only defaults will be used.
Warning: Control WingRightTE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftLE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftTE not found in controls tuple! Only defaults will be used.
Writing surface - Vertical_Tail (ID = 0)
	Section 1 of 2 (ID = 0)
	  Control surface 1 of 1 
	Section 2 of 2 (ID = 1)
	  Control surface 1 of 1 
Writing surface - Wing (ID = 1)
	Section 1 of 3 (ID = 1)
	  Control surface 1 of 2 
	  Control surface 2 of 2 
	Section 2 of 3 (ID = 0)
	  Control surface 1 of 4 
	  Control surface 2 of 4 
	  Control surface 3 of 4 
	  Control surface 4 of 4 
	Section 3 of 3 (ID = 2)
	  Control surface 1 of 2 
	  Control surface 2 of 2 
Cd = 0.002904376657734716
Cl = 0.2145646488015997
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 2
	Name = Wing, index = 1
	Name = Vertical_Tail, index = 2
Getting vortex lattice surface data
	VLM surface name - Vertical_Tail
	No "groupName" variable provided or no matches found, going to use tuple name
	VLM surface name - Wing
	Done getting vortex lattice surface data
Warning: Control Tail not found in controls tuple! Only defaults will be used.
Warning: Control Tail not found in controls tuple! Only defaults will be used.
Warning: Control WingRightLE not found in controls tuple! Only defaults will be used.
Warning: Control WingRightTE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftLE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftTE not found in controls tuple! Only defaults will be used.
Warning: Control WingRightLE not found in controls tuple! Only defaults will be used.
Warning: Control WingRightTE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftLE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftTE not found in controls tuple! Only defaults will be used.
Writing surface - Vertical_Tail (ID = 0)
	Section 1 of 2 (ID = 0)
	  Control surface 1 of 1 
	Section 2 of 2 (ID = 1)
	  Control surface 1 of 1 
Writing surface - Wing (ID = 1)
	Section 1 of 3 (ID = 1)
	  Control surface 1 of 2 
	  Control surface 2 of 2 
	Section 2 of 3 (ID = 0)
	  Control surface 1 of 4 
	  Control surface 2 of 4 
	  Control surface 3 of 4 
	  Control surface 4 of 4 
	Section 3 of 3 (ID = 2)
	  Control surface 1 of 2 
	  Control surface 2 of 2 
Cd = 0.003011879793042747
Cl = 0.2188068842334945
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 2
	Name = Wing, index = 1
	Name = Vertical_Tail, index = 2
Getting vortex lattice surface data
	VLM surface name - Vertical_Tail
	No "groupName" variable provided or no matches found, going to use tuple name
	VLM surface name - Wing
	Done getting vortex lattice surface data
Warning: Control Tail not found in controls tuple! Only defaults will be used.
Warning: Control Tail not found in controls tuple! Only defaults will be used.
Warning: Control WingRightLE not found in controls tuple! Only defaults will be used.
Warning: Control WingRightTE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftLE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftTE not found in controls tuple! Only defaults will be used.
Warning: Control WingRightLE not found in controls tuple! Only defaults will be used.
Warning: Control WingRightTE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftLE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftTE not found in controls tuple! Only defaults will be used.
Writing surface - Vertical_Tail (ID = 0)
	Section 1 of 2 (ID = 0)
	  Control surface 1 of 1 
	Section 2 of 2 (ID = 1)
	  Control surface 1 of 1 
Writing surface - Wing (ID = 1)
	Section 1 of 3 (ID = 1)
	  Control surface 1 of 2 
	  Control surface 2 of 2 
	Section 2 of 3 (ID = 0)
	  Control surface 1 of 4 
	  Control surface 2 of 4 
	  Control surface 3 of 4 
	  Control surface 4 of 4 
	Section 3 of 3 (ID = 2)
	  Control surface 1 of 2 
	  Control surface 2 of 2 
Cd = 0.003143602034586226
Cl = 0.2238987294815726
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 2
	Name = Wing, index = 1
	Name = Vertical_Tail, index = 2
Getting vortex lattice surface data
	VLM surface name - Vertical_Tail
	No "groupName" variable provided or no matches found, going to use tuple name
	VLM surface name - Wing
	Done getting vortex lattice surface data
Warning: Control Tail not found in controls tuple! Only defaults will be used.
Warning: Control Tail not found in controls tuple! Only defaults will be used.
Warning: Control WingRightLE not found in controls tuple! Only defaults will be used.
Warning: Control WingRightTE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftLE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftTE not found in controls tuple! Only defaults will be used.
Warning: Control WingRightLE not found in controls tuple! Only defaults will be used.
Warning: Control WingRightTE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftLE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftTE not found in controls tuple! Only defaults will be used.
Writing surface - Vertical_Tail (ID = 0)
	Section 1 of 2 (ID = 0)
	  Control surface 1 of 1 
	Section 2 of 2 (ID = 1)
	  Control surface 1 of 1 
Writing surface - Wing (ID = 1)
	Section 1 of 3 (ID = 1)
	  Control surface 1 of 2 
	  Control surface 2 of 2 
	Section 2 of 3 (ID = 0)
	  Control surface 1 of 4 
	  Control surface 2 of 4 
	  Control surface 3 of 4 
	  Control surface 4 of 4 
	Section 3 of 3 (ID = 2)
	  Control surface 1 of 2 
	  Control surface 2 of 2 
Cd = 0.003305877285452361
Cl = 0.2300199286487156
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 2
	Name = Wing, index = 1
	Name = Vertical_Tail, index = 2
Getting vortex lattice surface data
	VLM surface name - Vertical_Tail
	No "groupName" variable provided or no matches found, going to use tuple name
	VLM surface name - Wing
	Done getting vortex lattice surface data
Warning: Control Tail not found in controls tuple! Only defaults will be used.
Warning: Control Tail not found in controls tuple! Only defaults will be used.
Warning: Control WingRightLE not found in controls tuple! Only defaults will be used.
Warning: Control WingRightTE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftLE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftTE not found in controls tuple! Only defaults will be used.
Warning: Control WingRightLE not found in controls tuple! Only defaults will be used.
Warning: Control WingRightTE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftLE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftTE not found in controls tuple! Only defaults will be used.
Writing surface - Vertical_Tail (ID = 0)
	Section 1 of 2 (ID = 0)
	  Control surface 1 of 1 
	Section 2 of 2 (ID = 1)
	  Control surface 1 of 1 
Writing surface - Wing (ID = 1)
	Section 1 of 3 (ID = 1)
	  Control surface 1 of 2 
	  Control surface 2 of 2 
	Section 2 of 3 (ID = 0)
	  Control surface 1 of 4 
	  Control surface 2 of 4 
	  Control surface 3 of 4 
	  Control surface 4 of 4 
	Section 3 of 3 (ID = 2)
	  Control surface 1 of 2 
	  Control surface 2 of 2 
Cd = 0.003507917885472537
Cl = 0.2374223860296633
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 2
	Name = Wing, index = 1
	Name = Vertical_Tail, index = 2
Getting vortex lattice surface data
	VLM surface name - Vertical_Tail
	No "groupName" variable provided or no matches found, going to use tuple name
	VLM surface name - Wing
	Done getting vortex lattice surface data
Warning: Control Tail not found in controls tuple! Only defaults will be used.
Warning: Control Tail not found in controls tuple! Only defaults will be used.
Warning: Control WingRightLE not found in controls tuple! Only defaults will be used.
Warning: Control WingRightTE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftLE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftTE not found in controls tuple! Only defaults will be used.
Warning: Control WingRightLE not found in controls tuple! Only defaults will be used.
Warning: Control WingRightTE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftLE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftTE not found in controls tuple! Only defaults will be used.
Writing surface - Vertical_Tail (ID = 0)
	Section 1 of 2 (ID = 0)
	  Control surface 1 of 1 
	Section 2 of 2 (ID = 1)
	  Control surface 1 of 1 
Writing surface - Wing (ID = 1)
	Section 1 of 3 (ID = 1)
	  Control surface 1 of 2 
	  Control surface 2 of 2 
	Section 2 of 3 (ID = 0)
	  Control surface 1 of 4 
	  Control surface 2 of 4 
	  Control surface 3 of 4 
	  Control surface 4 of 4 
	Section 3 of 3 (ID = 2)
	  Control surface 1 of 2 
	  Control surface 2 of 2 
Cd = 0.003763643677259966
Cl = 0.2464707142744908
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 2
	Name = Wing, index = 1
	Name = Vertical_Tail, index = 2
Getting vortex lattice surface data
	VLM surface name - Vertical_Tail
	No "groupName" variable provided or no matches found, going to use tuple name
	VLM surface name - Wing
	Done getting vortex lattice surface data
Warning: Control Tail not found in controls tuple! Only defaults will be used.
Warning: Control Tail not found in controls tuple! Only defaults will be used.
Warning: Control WingRightLE not found in controls tuple! Only defaults will be used.
Warning: Control WingRightTE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftLE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftTE not found in controls tuple! Only defaults will be used.
Warning: Control WingRightLE not found in controls tuple! Only defaults will be used.
Warning: Control WingRightTE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftLE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftTE not found in controls tuple! Only defaults will be used.
Writing surface - Vertical_Tail (ID = 0)
	Section 1 of 2 (ID = 0)
	  Control surface 1 of 1 
	Section 2 of 2 (ID = 1)
	  Control surface 1 of 1 
Writing surface - Wing (ID = 1)
	Section 1 of 3 (ID = 1)
	  Control surface 1 of 2 
	  Control surface 2 of 2 
	Section 2 of 3 (ID = 0)
	  Control surface 1 of 4 
	  Control surface 2 of 4 
	  Control surface 3 of 4 
	  Control surface 4 of 4 
	Section 3 of 3 (ID = 2)
	  Control surface 1 of 2 
	  Control surface 2 of 2 
Cd = 0.004095167898227208
Cl = 0.25771580677477
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 2
	Name = Wing, index = 1
	Name = Vertical_Tail, index = 2
Getting vortex lattice surface data
	VLM surface name - Vertical_Tail
	No "groupName" variable provided or no matches found, going to use tuple name
	VLM surface name - Wing
	Done getting vortex lattice surface data
Warning: Control Tail not found in controls tuple! Only defaults will be used.
Warning: Control Tail not found in controls tuple! Only defaults will be used.
Warning: Control WingRightLE not found in controls tuple! Only defaults will be used.
Warning: Control WingRightTE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftLE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftTE not found in controls tuple! Only defaults will be used.
Warning: Control WingRightLE not found in controls tuple! Only defaults will be used.
Warning: Control WingRightTE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftLE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftTE not found in controls tuple! Only defaults will be used.
Writing surface - Vertical_Tail (ID = 0)
	Section 1 of 2 (ID = 0)
	  Control surface 1 of 1 
	Section 2 of 2 (ID = 1)
	  Control surface 1 of 1 
Writing surface - Wing (ID = 1)
	Section 1 of 3 (ID = 1)
	  Control surface 1 of 2 
	  Control surface 2 of 2 
	Section 2 of 3 (ID = 0)
	  Control surface 1 of 4 
	  Control surface 2 of 4 
	  Control surface 3 of 4 
	  Control surface 4 of 4 
	Section 3 of 3 (ID = 2)
	  Control surface 1 of 2 
	  Control surface 2 of 2 
Cd = 0.004540047408135333
Cl = 0.2720394012163583
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 2
	Name = Wing, index = 1
	Name = Vertical_Tail, index = 2
Getting vortex lattice surface data
	VLM surface name - Vertical_Tail
	No "groupName" variable provided or no matches found, going to use tuple name
	VLM surface name - Wing
	Done getting vortex lattice surface data
Warning: Control Tail not found in controls tuple! Only defaults will be used.
Warning: Control Tail not found in controls tuple! Only defaults will be used.
Warning: Control WingRightLE not found in controls tuple! Only defaults will be used.
Warning: Control WingRightTE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftLE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftTE not found in controls tuple! Only defaults will be used.
Warning: Control WingRightLE not found in controls tuple! Only defaults will be used.
Warning: Control WingRightTE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftLE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftTE not found in controls tuple! Only defaults will be used.
Writing surface - Vertical_Tail (ID = 0)
	Section 1 of 2 (ID = 0)
	  Control surface 1 of 1 
	Section 2 of 2 (ID = 1)
	  Control surface 1 of 1 
Writing surface - Wing (ID = 1)
	Section 1 of 3 (ID = 1)
	  Control surface 1 of 2 
	  Control surface 2 of 2 
	Section 2 of 3 (ID = 0)
	  Control surface 1 of 4 
	  Control surface 2 of 4 
	  Control surface 3 of 4 
	  Control surface 4 of 4 
	Section 3 of 3 (ID = 2)
	  Control surface 1 of 2 
	  Control surface 2 of 2 
Cd = 0.005168237926851883
Cl = 0.2909701507463254
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 2
	Name = Wing, index = 1
	Name = Vertical_Tail, index = 2
Getting vortex lattice surface data
	VLM surface name - Vertical_Tail
	No "groupName" variable provided or no matches found, going to use tuple name
	VLM surface name - Wing
	Done getting vortex lattice surface data
Warning: Control Tail not found in controls tuple! Only defaults will be used.
Warning: Control Tail not found in controls tuple! Only defaults will be used.
Warning: Control WingRightLE not found in controls tuple! Only defaults will be used.
Warning: Control WingRightTE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftLE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftTE not found in controls tuple! Only defaults will be used.
Warning: Control WingRightLE not found in controls tuple! Only defaults will be used.
Warning: Control WingRightTE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftLE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftTE not found in controls tuple! Only defaults will be used.
Writing surface - Vertical_Tail (ID = 0)
	Section 1 of 2 (ID = 0)
	  Control surface 1 of 1 
	Section 2 of 2 (ID = 1)
	  Control surface 1 of 1 
Writing surface - Wing (ID = 1)
	Section 1 of 3 (ID = 1)
	  Control surface 1 of 2 
	  Control surface 2 of 2 
	Section 2 of 3 (ID = 0)
	  Control surface 1 of 4 
	  Control surface 2 of 4 
	  Control surface 3 of 4 
	  Control surface 4 of 4 
	Section 3 of 3 (ID = 2)
	  Control surface 1 of 2 
	  Control surface 2 of 2 
Cd = 0.006128930715329168
Cl = 0.317487548593558
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 2
	Name = Wing, index = 1
	Name = Vertical_Tail, index = 2
Getting vortex lattice surface data
	VLM surface name - Vertical_Tail
	No "groupName" variable provided or no matches found, going to use tuple name
	VLM surface name - Wing
	Done getting vortex lattice surface data
Warning: Control Tail not found in controls tuple! Only defaults will be used.
Warning: Control Tail not found in controls tuple! Only defaults will be used.
Warning: Control WingRightLE not found in controls tuple! Only defaults will be used.
Warning: Control WingRightTE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftLE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftTE not found in controls tuple! Only defaults will be used.
Warning: Control WingRightLE not found in controls tuple! Only defaults will be used.
Warning: Control WingRightTE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftLE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftTE not found in controls tuple! Only defaults will be used.
Writing surface - Vertical_Tail (ID = 0)
	Section 1 of 2 (ID = 0)
	  Control surface 1 of 1 
	Section 2 of 2 (ID = 1)
	  Control surface 1 of 1 
Writing surface - Wing (ID = 1)
	Section 1 of 3 (ID = 1)
	  Control surface 1 of 2 
	  Control surface 2 of 2 
	Section 2 of 3 (ID = 0)
	  Control surface 1 of 4 
	  Control surface 2 of 4 
	  Control surface 3 of 4 
	  Control surface 4 of 4 
	Section 3 of 3 (ID = 2)
	  Control surface 1 of 2 
	  Control surface 2 of 2 
Cd = 0.007818359051271666
Cl = 0.3586078919918751
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 2
	Name = Wing, index = 1
	Name = Vertical_Tail, index = 2
Getting vortex lattice surface data
	VLM surface name - Vertical_Tail
	No "groupName" variable provided or no matches found, going to use tuple name
	VLM surface name - Wing
	Done getting vortex lattice surface data
Warning: Control Tail not found in controls tuple! Only defaults will be used.
Warning: Control Tail not found in controls tuple! Only defaults will be used.
Warning: Control WingRightLE not found in controls tuple! Only defaults will be used.
Warning: Control WingRightTE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftLE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftTE not found in controls tuple! Only defaults will be used.
Warning: Control WingRightLE not found in controls tuple! Only defaults will be used.
Warning: Control WingRightTE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftLE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftTE not found in controls tuple! Only defaults will be used.
Writing surface - Vertical_Tail (ID = 0)
	Section 1 of 2 (ID = 0)
	  Control surface 1 of 1 
	Section 2 of 2 (ID = 1)
	  Control surface 1 of 1 
Writing surface - Wing (ID = 1)
	Section 1 of 3 (ID = 1)
	  Control surface 1 of 2 
	  Control surface 2 of 2 
	Section 2 of 3 (ID = 0)
	  Control surface 1 of 4 
	  Control surface 2 of 4 
	  Control surface 3 of 4 
	  Control surface 4 of 4 
	Section 3 of 3 (ID = 2)
	  Control surface 1 of 2 
	  Control surface 2 of 2 
Cd = 0.01186220444373961
Cl = 0.4382638635243895
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 2
	Name = Wing, index = 1
	Name = Vertical_Tail, index = 2
Getting vortex lattice surface data
	VLM surface name - Vertical_Tail
	No "groupName" variable provided or no matches found, going to use tuple name
	VLM surface name - Wing
	Done getting vortex lattice surface data
Warning: Control Tail not found in controls tuple! Only defaults will be used.
Warning: Control Tail not found in controls tuple! Only defaults will be used.
Warning: Control WingRightLE not found in controls tuple! Only defaults will be used.
Warning: Control WingRightTE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftLE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftTE not found in controls tuple! Only defaults will be used.
Warning: Control WingRightLE not found in controls tuple! Only defaults will be used.
Warning: Control WingRightTE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftLE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftTE not found in controls tuple! Only defaults will be used.
Writing surface - Vertical_Tail (ID = 0)
	Section 1 of 2 (ID = 0)
	  Control surface 1 of 1 
	Section 2 of 2 (ID = 1)
	  Control surface 1 of 1 
Writing surface - Wing (ID = 1)
	Section 1 of 3 (ID = 1)
	  Control surface 1 of 2 
	  Control surface 2 of 2 
	Section 2 of 3 (ID = 0)
	  Control surface 1 of 4 
	  Control surface 2 of 4 
	  Control surface 3 of 4 
	  Control surface 4 of 4 
	Section 3 of 3 (ID = 2)
	  Control surface 1 of 2 
	  Control surface 2 of 2 
Cd = 0.002572533601550775
Cl = 0.2009337808873524
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 2
	Name = Wing, index = 1
	Name = Vertical_Tail, index = 2
Getting vortex lattice surface data
	VLM surface name - Vertical_Tail
	No "groupName" variable provided or no matches found, going to use tuple name
	VLM surface name - Wing
	Done getting vortex lattice surface data
Warning: Control Tail not found in controls tuple! Only defaults will be used.
Warning: Control Tail not found in controls tuple! Only defaults will be used.
Warning: Control WingRightLE not found in controls tuple! Only defaults will be used.
Warning: Control WingRightTE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftLE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftTE not found in controls tuple! Only defaults will be used.
Warning: Control WingRightLE not found in controls tuple! Only defaults will be used.
Warning: Control WingRightTE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftLE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftTE not found in controls tuple! Only defaults will be used.
Writing surface - Vertical_Tail (ID = 0)
	Section 1 of 2 (ID = 0)
	  Control surface 1 of 1 
	Section 2 of 2 (ID = 1)
	  Control surface 1 of 1 
Writing surface - Wing (ID = 1)
	Section 1 of 3 (ID = 1)
	  Control surface 1 of 2 
	  Control surface 2 of 2 
	Section 2 of 3 (ID = 0)
	  Control surface 1 of 4 
	  Control surface 2 of 4 
	  Control surface 3 of 4 
	  Control surface 4 of 4 
	Section 3 of 3 (ID = 2)
	  Control surface 1 of 2 
	  Control surface 2 of 2 
Cd = 0.002586364230241802
Cl = 0.2015191856814851
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 2
	Name = Wing, index = 1
	Name = Vertical_Tail, index = 2
Getting vortex lattice surface data
	VLM surface name - Vertical_Tail
	No "groupName" variable provided or no matches found, going to use tuple name
	VLM surface name - Wing
	Done getting vortex lattice surface data
Warning: Control Tail not found in controls tuple! Only defaults will be used.
Warning: Control Tail not found in controls tuple! Only defaults will be used.
Warning: Control WingRightLE not found in controls tuple! Only defaults will be used.
Warning: Control WingRightTE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftLE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftTE not found in controls tuple! Only defaults will be used.
Warning: Control WingRightLE not found in controls tuple! Only defaults will be used.
Warning: Control WingRightTE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftLE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftTE not found in controls tuple! Only defaults will be used.
Writing surface - Vertical_Tail (ID = 0)
	Section 1 of 2 (ID = 0)
	  Control surface 1 of 1 
	Section 2 of 2 (ID = 1)
	  Control surface 1 of 1 
Writing surface - Wing (ID = 1)
	Section 1 of 3 (ID = 1)
	  Control surface 1 of 2 
	  Control surface 2 of 2 
	Section 2 of 3 (ID = 0)
	  Control surface 1 of 4 
	  Control surface 2 of 4 
	  Control surface 3 of 4 
	  Control surface 4 of 4 
	Section 3 of 3 (ID = 2)
	  Control surface 1 of 2 
	  Control surface 2 of 2 
Cd = 0.002609799718816161
Cl = 0.202507529643332
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 2
	Name = Wing, index = 1
	Name = Vertical_Tail, index = 2
Getting vortex lattice surface data
	VLM surface name - Vertical_Tail
	No "groupName" variable provided or no matches found, going to use tuple name
	VLM surface name - Wing
	Done getting vortex lattice surface data
Warning: Control Tail not found in controls tuple! Only defaults will be used.
Warning: Control Tail not found in controls tuple! Only defaults will be used.
Warning: Control WingRightLE not found in controls tuple! Only defaults will be used.
Warning: Control WingRightTE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftLE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftTE not found in controls tuple! Only defaults will be used.
Warning: Control WingRightLE not found in controls tuple! Only defaults will be used.
Warning: Control WingRightTE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftLE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftTE not found in controls tuple! Only defaults will be used.
Writing surface - Vertical_Tail (ID = 0)
	Section 1 of 2 (ID = 0)
	  Control surface 1 of 1 
	Section 2 of 2 (ID = 1)
	  Control surface 1 of 1 
Writing surface - Wing (ID = 1)
	Section 1 of 3 (ID = 1)
	  Control surface 1 of 2 
	  Control surface 2 of 2 
	Section 2 of 3 (ID = 0)
	  Control surface 1 of 4 
	  Control surface 2 of 4 
	  Control surface 3 of 4 
	  Control surface 4 of 4 
	Section 3 of 3 (ID = 2)
	  Control surface 1 of 2 
	  Control surface 2 of 2 
Cd = 0.002643444008424624
Cl = 0.2039185811658769
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 2
	Name = Wing, index = 1
	Name = Vertical_Tail, index = 2
Getting vortex lattice surface data
	VLM surface name - Vertical_Tail
	No "groupName" variable provided or no matches found, going to use tuple name
	VLM surface name - Wing
	Done getting vortex lattice surface data
Warning: Control Tail not found in controls tuple! Only defaults will be used.
Warning: Control Tail not found in controls tuple! Only defaults will be used.
Warning: Control WingRightLE not found in controls tuple! Only defaults will be used.
Warning: Control WingRightTE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftLE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftTE not found in controls tuple! Only defaults will be used.
Warning: Control WingRightLE not found in controls tuple! Only defaults will be used.
Warning: Control WingRightTE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftLE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftTE not found in controls tuple! Only defaults will be used.
Writing surface - Vertical_Tail (ID = 0)
	Section 1 of 2 (ID = 0)
	  Control surface 1 of 1 
	Section 2 of 2 (ID = 1)
	  Control surface 1 of 1 
Writing surface - Wing (ID = 1)
	Section 1 of 3 (ID = 1)
	  Control surface 1 of 2 
	  Control surface 2 of 2 
	Section 2 of 3 (ID = 0)
	  Control surface 1 of 4 
	  Control surface 2 of 4 
	  Control surface 3 of 4 
	  Control surface 4 of 4 
	Section 3 of 3 (ID = 2)
	  Control surface 1 of 2 
	  Control surface 2 of 2 
Cd = 0.002688200920998204
Cl = 0.2057816377790584
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 2
	Name = Wing, index = 1
	Name = Vertical_Tail, index = 2
Getting vortex lattice surface data
	VLM surface name - Vertical_Tail
	No "groupName" variable provided or no matches found, going to use tuple name
	VLM surface name - Wing
	Done getting vortex lattice surface data
Warning: Control Tail not found in controls tuple! Only defaults will be used.
Warning: Control Tail not found in controls tuple! Only defaults will be used.
Warning: Control WingRightLE not found in controls tuple! Only defaults will be used.
Warning: Control WingRightTE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftLE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftTE not found in controls tuple! Only defaults will be used.
Warning: Control WingRightLE not found in controls tuple! Only defaults will be used.
Warning: Control WingRightTE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftLE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftTE not found in controls tuple! Only defaults will be used.
Writing surface - Vertical_Tail (ID = 0)
	Section 1 of 2 (ID = 0)
	  Control surface 1 of 1 
	Section 2 of 2 (ID = 1)
	  Control surface 1 of 1 
Writing surface - Wing (ID = 1)
	Section 1 of 3 (ID = 1)
	  Control surface 1 of 2 
	  Control surface 2 of 2 
	Section 2 of 3 (ID = 0)
	  Control surface 1 of 4 
	  Control surface 2 of 4 
	  Control surface 3 of 4 
	  Control surface 4 of 4 
	Section 3 of 3 (ID = 2)
	  Control surface 1 of 2 
	  Control surface 2 of 2 
Cd = 0.002745342060015943
Cl = 0.2081373840559949
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 2
	Name = Wing, index = 1
	Name = Vertical_Tail, index = 2
Getting vortex lattice surface data
	VLM surface name - Vertical_Tail
	No "groupName" variable provided or no matches found, going to use tuple name
	VLM surface name - Wing
	Done getting vortex lattice surface data
Warning: Control Tail not found in controls tuple! Only defaults will be used.
Warning: Control Tail not found in controls tuple! Only defaults will be used.
Warning: Control WingRightLE not found in controls tuple! Only defaults will be used.
Warning: Control WingRightTE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftLE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftTE not found in controls tuple! Only defaults will be used.
Warning: Control WingRightLE not found in controls tuple! Only defaults will be used.
Warning: Control WingRightTE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftLE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftTE not found in controls tuple! Only defaults will be used.
Writing surface - Vertical_Tail (ID = 0)
	Section 1 of 2 (ID = 0)
	  Control surface 1 of 1 
	Section 2 of 2 (ID = 1)
	  Control surface 1 of 1 
Writing surface - Wing (ID = 1)
	Section 1 of 3 (ID = 1)
	  Control surface 1 of 2 
	  Control surface 2 of 2 
	Section 2 of 3 (ID = 0)
	  Control surface 1 of 4 
	  Control surface 2 of 4 
	  Control surface 3 of 4 
	  Control surface 4 of 4 
	Section 3 of 3 (ID = 2)
	  Control surface 1 of 2 
	  Control surface 2 of 2 
Cd = 0.002816610334298771
Cl = 0.2110406736705562
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 2
	Name = Wing, index = 1
	Name = Vertical_Tail, index = 2
Getting vortex lattice surface data
	VLM surface name - Vertical_Tail
	No "groupName" variable provided or no matches found, going to use tuple name
	VLM surface name - Wing
	Done getting vortex lattice surface data
Warning: Control Tail not found in controls tuple! Only defaults will be used.
Warning: Control Tail not found in controls tuple! Only defaults will be used.
Warning: Control WingRightLE not found in controls tuple! Only defaults will be used.
Warning: Control WingRightTE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftLE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftTE not found in controls tuple! Only defaults will be used.
Warning: Control WingRightLE not found in controls tuple! Only defaults will be used.
Warning: Control WingRightTE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftLE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftTE not found in controls tuple! Only defaults will be used.
Writing surface - Vertical_Tail (ID = 0)
	Section 1 of 2 (ID = 0)
	  Control surface 1 of 1 
	Section 2 of 2 (ID = 1)
	  Control surface 1 of 1 
Writing surface - Wing (ID = 1)
	Section 1 of 3 (ID = 1)
	  Control surface 1 of 2 
	  Control surface 2 of 2 
	Section 2 of 3 (ID = 0)
	  Control surface 1 of 4 
	  Control surface 2 of 4 
	  Control surface 3 of 4 
	  Control surface 4 of 4 
	Section 3 of 3 (ID = 2)
	  Control surface 1 of 2 
	  Control surface 2 of 2 
Cd = 0.002904376657734716
Cl = 0.2145646488015997
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 2
	Name = Wing, index = 1
	Name = Vertical_Tail, index = 2
Getting vortex lattice surface data
	VLM surface name - Vertical_Tail
	No "groupName" variable provided or no matches found, going to use tuple name
	VLM surface name - Wing
	Done getting vortex lattice surface data
Warning: Control Tail not found in controls tuple! Only defaults will be used.
Warning: Control Tail not found in controls tuple! Only defaults will be used.
Warning: Control WingRightLE not found in controls tuple! Only defaults will be used.
Warning: Control WingRightTE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftLE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftTE not found in controls tuple! Only defaults will be used.
Warning: Control WingRightLE not found in controls tuple! Only defaults will be used.
Warning: Control WingRightTE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftLE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftTE not found in controls tuple! Only defaults will be used.
Writing surface - Vertical_Tail (ID = 0)
	Section 1 of 2 (ID = 0)
	  Control surface 1 of 1 
	Section 2 of 2 (ID = 1)
	  Control surface 1 of 1 
Writing surface - Wing (ID = 1)
	Section 1 of 3 (ID = 1)
	  Control surface 1 of 2 
	  Control surface 2 of 2 
	Section 2 of 3 (ID = 0)
	  Control surface 1 of 4 
	  Control surface 2 of 4 
	  Control surface 3 of 4 
	  Control surface 4 of 4 
	Section 3 of 3 (ID = 2)
	  Control surface 1 of 2 
	  Control surface 2 of 2 
Cd = 0.003011879793042747
Cl = 0.2188068842334945
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 2
	Name = Wing, index = 1
	Name = Vertical_Tail, index = 2
Getting vortex lattice surface data
	VLM surface name - Vertical_Tail
	No "groupName" variable provided or no matches found, going to use tuple name
	VLM surface name - Wing
	Done getting vortex lattice surface data
Warning: Control Tail not found in controls tuple! Only defaults will be used.
Warning: Control Tail not found in controls tuple! Only defaults will be used.
Warning: Control WingRightLE not found in controls tuple! Only defaults will be used.
Warning: Control WingRightTE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftLE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftTE not found in controls tuple! Only defaults will be used.
Warning: Control WingRightLE not found in controls tuple! Only defaults will be used.
Warning: Control WingRightTE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftLE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftTE not found in controls tuple! Only defaults will be used.
Writing surface - Vertical_Tail (ID = 0)
	Section 1 of 2 (ID = 0)
	  Control surface 1 of 1 
	Section 2 of 2 (ID = 1)
	  Control surface 1 of 1 
Writing surface - Wing (ID = 1)
	Section 1 of 3 (ID = 1)
	  Control surface 1 of 2 
	  Control surface 2 of 2 
	Section 2 of 3 (ID = 0)
	  Control surface 1 of 4 
	  Control surface 2 of 4 
	  Control surface 3 of 4 
	  Control surface 4 of 4 
	Section 3 of 3 (ID = 2)
	  Control surface 1 of 2 
	  Control surface 2 of 2 
Cd = 0.003143602034586226
Cl = 0.2238987294815726
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 2
	Name = Wing, index = 1
	Name = Vertical_Tail, index = 2
Getting vortex lattice surface data
	VLM surface name - Vertical_Tail
	No "groupName" variable provided or no matches found, going to use tuple name
	VLM surface name - Wing
	Done getting vortex lattice surface data
Warning: Control Tail not found in controls tuple! Only defaults will be used.
Warning: Control Tail not found in controls tuple! Only defaults will be used.
Warning: Control WingRightLE not found in controls tuple! Only defaults will be used.
Warning: Control WingRightTE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftLE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftTE not found in controls tuple! Only defaults will be used.
Warning: Control WingRightLE not found in controls tuple! Only defaults will be used.
Warning: Control WingRightTE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftLE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftTE not found in controls tuple! Only defaults will be used.
Writing surface - Vertical_Tail (ID = 0)
	Section 1 of 2 (ID = 0)
	  Control surface 1 of 1 
	Section 2 of 2 (ID = 1)
	  Control surface 1 of 1 
Writing surface - Wing (ID = 1)
	Section 1 of 3 (ID = 1)
	  Control surface 1 of 2 
	  Control surface 2 of 2 
	Section 2 of 3 (ID = 0)
	  Control surface 1 of 4 
	  Control surface 2 of 4 
	  Control surface 3 of 4 
	  Control surface 4 of 4 
	Section 3 of 3 (ID = 2)
	  Control surface 1 of 2 
	  Control surface 2 of 2 
Cd = 0.003305877285452361
Cl = 0.2300199286487156
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 2
	Name = Wing, index = 1
	Name = Vertical_Tail, index = 2
Getting vortex lattice surface data
	VLM surface name - Vertical_Tail
	No "groupName" variable provided or no matches found, going to use tuple name
	VLM surface name - Wing
	Done getting vortex lattice surface data
Warning: Control Tail not found in controls tuple! Only defaults will be used.
Warning: Control Tail not found in controls tuple! Only defaults will be used.
Warning: Control WingRightLE not found in controls tuple! Only defaults will be used.
Warning: Control WingRightTE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftLE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftTE not found in controls tuple! Only defaults will be used.
Warning: Control WingRightLE not found in controls tuple! Only defaults will be used.
Warning: Control WingRightTE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftLE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftTE not found in controls tuple! Only defaults will be used.
Writing surface - Vertical_Tail (ID = 0)
	Section 1 of 2 (ID = 0)
	  Control surface 1 of 1 
	Section 2 of 2 (ID = 1)
	  Control surface 1 of 1 
Writing surface - Wing (ID = 1)
	Section 1 of 3 (ID = 1)
	  Control surface 1 of 2 
	  Control surface 2 of 2 
	Section 2 of 3 (ID = 0)
	  Control surface 1 of 4 
	  Control surface 2 of 4 
	  Control surface 3 of 4 
	  Control surface 4 of 4 
	Section 3 of 3 (ID = 2)
	  Control surface 1 of 2 
	  Control surface 2 of 2 
Cd = 0.003507917885472537
Cl = 0.2374223860296633
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 2
	Name = Wing, index = 1
	Name = Vertical_Tail, index = 2
Getting vortex lattice surface data
	VLM surface name - Vertical_Tail
	No "groupName" variable provided or no matches found, going to use tuple name
	VLM surface name - Wing
	Done getting vortex lattice surface data
Warning: Control Tail not found in controls tuple! Only defaults will be used.
Warning: Control Tail not found in controls tuple! Only defaults will be used.
Warning: Control WingRightLE not found in controls tuple! Only defaults will be used.
Warning: Control WingRightTE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftLE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftTE not found in controls tuple! Only defaults will be used.
Warning: Control WingRightLE not found in controls tuple! Only defaults will be used.
Warning: Control WingRightTE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftLE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftTE not found in controls tuple! Only defaults will be used.
Writing surface - Vertical_Tail (ID = 0)
	Section 1 of 2 (ID = 0)
	  Control surface 1 of 1 
	Section 2 of 2 (ID = 1)
	  Control surface 1 of 1 
Writing surface - Wing (ID = 1)
	Section 1 of 3 (ID = 1)
	  Control surface 1 of 2 
	  Control surface 2 of 2 
	Section 2 of 3 (ID = 0)
	  Control surface 1 of 4 
	  Control surface 2 of 4 
	  Control surface 3 of 4 
	  Control surface 4 of 4 
	Section 3 of 3 (ID = 2)
	  Control surface 1 of 2 
	  Control surface 2 of 2 
Cd = 0.003763643677259966
Cl = 0.2464707142744908
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 2
	Name = Wing, index = 1
	Name = Vertical_Tail, index = 2
Getting vortex lattice surface data
	VLM surface name - Vertical_Tail
	No "groupName" variable provided or no matches found, going to use tuple name
	VLM surface name - Wing
	Done getting vortex lattice surface data
Warning: Control Tail not found in controls tuple! Only defaults will be used.
Warning: Control Tail not found in controls tuple! Only defaults will be used.
Warning: Control WingRightLE not found in controls tuple! Only defaults will be used.
Warning: Control WingRightTE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftLE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftTE not found in controls tuple! Only defaults will be used.
Warning: Control WingRightLE not found in controls tuple! Only defaults will be used.
Warning: Control WingRightTE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftLE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftTE not found in controls tuple! Only defaults will be used.
Writing surface - Vertical_Tail (ID = 0)
	Section 1 of 2 (ID = 0)
	  Control surface 1 of 1 
	Section 2 of 2 (ID = 1)
	  Control surface 1 of 1 
Writing surface - Wing (ID = 1)
	Section 1 of 3 (ID = 1)
	  Control surface 1 of 2 
	  Control surface 2 of 2 
	Section 2 of 3 (ID = 0)
	  Control surface 1 of 4 
	  Control surface 2 of 4 
	  Control surface 3 of 4 
	  Control surface 4 of 4 
	Section 3 of 3 (ID = 2)
	  Control surface 1 of 2 
	  Control surface 2 of 2 
Cd = 0.004095167898227208
Cl = 0.25771580677477
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 2
	Name = Wing, index = 1
	Name = Vertical_Tail, index = 2
Getting vortex lattice surface data
	VLM surface name - Vertical_Tail
	No "groupName" variable provided or no matches found, going to use tuple name
	VLM surface name - Wing
	Done getting vortex lattice surface data
Warning: Control Tail not found in controls tuple! Only defaults will be used.
Warning: Control Tail not found in controls tuple! Only defaults will be used.
Warning: Control WingRightLE not found in controls tuple! Only defaults will be used.
Warning: Control WingRightTE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftLE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftTE not found in controls tuple! Only defaults will be used.
Warning: Control WingRightLE not found in controls tuple! Only defaults will be used.
Warning: Control WingRightTE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftLE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftTE not found in controls tuple! Only defaults will be used.
Writing surface - Vertical_Tail (ID = 0)
	Section 1 of 2 (ID = 0)
	  Control surface 1 of 1 
	Section 2 of 2 (ID = 1)
	  Control surface 1 of 1 
Writing surface - Wing (ID = 1)
	Section 1 of 3 (ID = 1)
	  Control surface 1 of 2 
	  Control surface 2 of 2 
	Section 2 of 3 (ID = 0)
	  Control surface 1 of 4 
	  Control surface 2 of 4 
	  Control surface 3 of 4 
	  Control surface 4 of 4 
	Section 3 of 3 (ID = 2)
	  Control surface 1 of 2 
	  Control surface 2 of 2 
Cd = 0.004540047408135333
Cl = 0.2720394012163583
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 2
	Name = Wing, index = 1
	Name = Vertical_Tail, index = 2
Getting vortex lattice surface data
	VLM surface name - Vertical_Tail
	No "groupName" variable provided or no matches found, going to use tuple name
	VLM surface name - Wing
	Done getting vortex lattice surface data
Warning: Control Tail not found in controls tuple! Only defaults will be used.
Warning: Control Tail not found in controls tuple! Only defaults will be used.
Warning: Control WingRightLE not found in controls tuple! Only defaults will be used.
Warning: Control WingRightTE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftLE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftTE not found in controls tuple! Only defaults will be used.
Warning: Control WingRightLE not found in controls tuple! Only defaults will be used.
Warning: Control WingRightTE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftLE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftTE not found in controls tuple! Only defaults will be used.
Writing surface - Vertical_Tail (ID = 0)
	Section 1 of 2 (ID = 0)
	  Control surface 1 of 1 
	Section 2 of 2 (ID = 1)
	  Control surface 1 of 1 
Writing surface - Wing (ID = 1)
	Section 1 of 3 (ID = 1)
	  Control surface 1 of 2 
	  Control surface 2 of 2 
	Section 2 of 3 (ID = 0)
	  Control surface 1 of 4 
	  Control surface 2 of 4 
	  Control surface 3 of 4 
	  Control surface 4 of 4 
	Section 3 of 3 (ID = 2)
	  Control surface 1 of 2 
	  Control surface 2 of 2 
Cd = 0.005168237926851883
Cl = 0.2909701507463254
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 2
	Name = Wing, index = 1
	Name = Vertical_Tail, index = 2
Getting vortex lattice surface data
	VLM surface name - Vertical_Tail
	No "groupName" variable provided or no matches found, going to use tuple name
	VLM surface name - Wing
	Done getting vortex lattice surface data
Warning: Control Tail not found in controls tuple! Only defaults will be used.
Warning: Control Tail not found in controls tuple! Only defaults will be used.
Warning: Control WingRightLE not found in controls tuple! Only defaults will be used.
Warning: Control WingRightTE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftLE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftTE not found in controls tuple! Only defaults will be used.
Warning: Control WingRightLE not found in controls tuple! Only defaults will be used.
Warning: Control WingRightTE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftLE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftTE not found in controls tuple! Only defaults will be used.
Writing surface - Vertical_Tail (ID = 0)
	Section 1 of 2 (ID = 0)
	  Control surface 1 of 1 
	Section 2 of 2 (ID = 1)
	  Control surface 1 of 1 
Writing surface - Wing (ID = 1)
	Section 1 of 3 (ID = 1)
	  Control surface 1 of 2 
	  Control surface 2 of 2 
	Section 2 of 3 (ID = 0)
	  Control surface 1 of 4 
	  Control surface 2 of 4 
	  Control surface 3 of 4 
	  Control surface 4 of 4 
	Section 3 of 3 (ID = 2)
	  Control surface 1 of 2 
	  Control surface 2 of 2 
Cd = 0.006128930715329168
Cl = 0.317487548593558
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 2
	Name = Wing, index = 1
	Name = Vertical_Tail, index = 2
Getting vortex lattice surface data
	VLM surface name - Vertical_Tail
	No "groupName" variable provided or no matches found, going to use tuple name
	VLM surface name - Wing
	Done getting vortex lattice surface data
Warning: Control Tail not found in controls tuple! Only defaults will be used.
Warning: Control Tail not found in controls tuple! Only defaults will be used.
Warning: Control WingRightLE not found in controls tuple! Only defaults will be used.
Warning: Control WingRightTE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftLE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftTE not found in controls tuple! Only defaults will be used.
Warning: Control WingRightLE not found in controls tuple! Only defaults will be used.
Warning: Control WingRightTE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftLE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftTE not found in controls tuple! Only defaults will be used.
Writing surface - Vertical_Tail (ID = 0)
	Section 1 of 2 (ID = 0)
	  Control surface 1 of 1 
	Section 2 of 2 (ID = 1)
	  Control surface 1 of 1 
Writing surface - Wing (ID = 1)
	Section 1 of 3 (ID = 1)
	  Control surface 1 of 2 
	  Control surface 2 of 2 
	Section 2 of 3 (ID = 0)
	  Control surface 1 of 4 
	  Control surface 2 of 4 
	  Control surface 3 of 4 
	  Control surface 4 of 4 
	Section 3 of 3 (ID = 2)
	  Control surface 1 of 2 
	  Control surface 2 of 2 
Cd = 0.007818359051271666
Cl = 0.3586078919918751
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 2
	Name = Wing, index = 1
	Name = Vertical_Tail, index = 2
Getting vortex lattice surface data
	VLM surface name - Vertical_Tail
	No "groupName" variable provided or no matches found, going to use tuple name
	VLM surface name - Wing
	Done getting vortex lattice surface data
Warning: Control Tail not found in controls tuple! Only defaults will be used.
Warning: Control Tail not found in controls tuple! Only defaults will be used.
Warning: Control WingRightLE not found in controls tuple! Only defaults will be used.
Warning: Control WingRightTE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftLE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftTE not found in controls tuple! Only defaults will be used.
Warning: Control WingRightLE not found in controls tuple! Only defaults will be used.
Warning: Control WingRightTE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftLE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftTE not found in controls tuple! Only defaults will be used.
Writing surface - Vertical_Tail (ID = 0)
	Section 1 of 2 (ID = 0)
	  Control surface 1 of 1 
	Section 2 of 2 (ID = 1)
	  Control surface 1 of 1 
Writing surface - Wing (ID = 1)
	Section 1 of 3 (ID = 1)
	  Control surface 1 of 2 
	  Control surface 2 of 2 
	Section 2 of 3 (ID = 0)
	  Control surface 1 of 4 
	  Control surface 2 of 4 
	  Control surface 3 of 4 
	  Control surface 4 of 4 
	Section 3 of 3 (ID = 2)
	  Control surface 1 of 2 
	  Control surface 2 of 2 
Cd = 0.01186220444373961
Cl = 0.4382638635243895
Cl[0] =  0.2009337808873524
Cd[0] =  0.002572533601550775

real	0m16.441s
user	0m8.254s
sys	0m8.193s
+ status=0
+ set +x

=================================================
CAPS verification (using pyCAPS) case avl_DesignSweep_PyTest.py passed (as expected)
=================================================


=================================================
+ echo 'avl_ControlSurf_PyTest.py test;'
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESP126/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
avl_ControlSurf_PyTest.py test;
+ python -u avl_ControlSurf_PyTest.py -outLevel=0
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESP126/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
Loading AIM
Setting design parameters
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 2
	Name = Wing, index = 1
	Name = Vertical_Tail, index = 2
Getting vortex lattice control surface data
	VLM control surface name - Tail
	VLM control surface name - WingRightLE
	VLM control surface name - WingRightTE
	Done getting vortex lattice control surface data
Getting vortex lattice surface data
	VLM surface name - Vertical_Tail
	No "groupName" variable provided or no matches found, going to use tuple name
	VLM surface name - Wing
	Done getting vortex lattice surface data
Warning: Control WingLeftLE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftTE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftLE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftTE not found in controls tuple! Only defaults will be used.
Writing surface - Vertical_Tail (ID = 0)
	Section 1 of 2 (ID = 0)
	  Control surface 1 of 1 
	Section 2 of 2 (ID = 1)
	  Control surface 1 of 1 
Writing surface - Wing (ID = 1)
	Section 1 of 3 (ID = 1)
	  Control surface 1 of 2 
	  Control surface 2 of 2 
	Section 2 of 3 (ID = 0)
	  Control surface 1 of 4 
	  Control surface 2 of 4 
	  Control surface 3 of 4 
	  Control surface 4 of 4 
	Section 3 of 3 (ID = 2)
	  Control surface 1 of 2 
	  Control surface 2 of 2 
Alpha  1.0
Beta   0.0
Mach   0.5
pb/2V  -0.0
qc/2V  0.0
rb/2V  -0.0
p'b/2V -0.0
r'b/2V -0.0
CXtot  -0.01911479917641001
CYtot  0.03828770401115553
CZtot  -0.6203123021537938
Cltot  0.05803020542928473
Cmtot  -0.3649415791575079
Cntot  -0.02051317548232544
Cl'tot 0.05766336287208538
Cn'tot -0.02152281795713262
CLtot  0.6198842263414319
CDtot  0.02993783031514586
CDvis  0.0
CLff   0.6192452092592853
CYff   0.03287079625844261
CDind  0.02993783031514586
CDff   0.0286101982265777
e      0.7130586920543264

real	0m0.521s
user	0m0.632s
sys	0m0.196s
+ status=0
+ set +x

=================================================
CAPS verification (using pyCAPS) case avl_ControlSurf_PyTest.py passed (as expected)
=================================================


=================================================
+ echo 'avl_EigenValue_PyTest.py test;'
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESP126/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
avl_EigenValue_PyTest.py test;
+ python -u avl_EigenValue_PyTest.py -outLevel=0
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESP126/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
Loading AIM
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = Wing, index = 1
Getting vortex lattice surface data
	VLM surface name - Wing
	Done getting vortex lattice surface data
Writing surface - Wing (ID = 0)
	Section 1 of 3 (ID = 0)
	Section 2 of 3 (ID = 1)
	Section 3 of 3 (ID = 2)
Writing mass properties file: caps.mass
Parsing MassProp
Note: The following floating-point exceptions are signalling: IEEE_DIVIDE_BY_ZERO
EigenValues  {'case 1': [[0.48252996, 1.0092579], [0.48252996, -1.0092579], [-6.42569, 0.0], [-1.2733929, 0.0], [-0.0011487329, 0.0], [-1.2380479, 0.49321593], [-1.2380479, -0.49321593], [0.77888703, 0.0]]}

real	0m0.467s
user	0m0.567s
sys	0m0.178s
+ status=0
+ set +x

=================================================
CAPS verification (using pyCAPS) case avl_EigenValue_PyTest.py passed (as expected)
=================================================


=================================================
+ echo 'avl_OpenMDAO_3_PyTest.py test;'
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESP126/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
avl_OpenMDAO_3_PyTest.py test;
+ python -u avl_OpenMDAO_3_PyTest.py -outLevel=0
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESP126/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
[VIGGEN.MIT.EDU:39227] shmem: mmap: an error occurred while determining whether or not /var/folders/l7/7s0m18td3fxg_w_dxpkj1d600000gp/T//ompi.VIGGEN.502/jf.0/691077120/sm_segment.VIGGEN.502.29310000.0 could be created.
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = Wing, index = 1
Getting vortex lattice surface data
	VLM surface name - Wing
	Done getting vortex lattice surface data
Writing surface - Wing (ID = 0)
	Section 1 of 3 (ID = 0)
	Section 2 of 3 (ID = 1)
	Section 3 of 3 (ID = 2)
Alpha [2.] Beta [3.] Cmtot2 [0.04166298]
Alpha [2.] Beta [3.] Cmtot2 [0.04166298]
Cmtot2_Alpha [[0.68007176]]
Cmtot2_Beta [[0.0008466]]
RUNNING THE L-BFGS-B CODE

           * * *

Machine precision = 2.220D-16
 N =            2     M =           10

At X0         0 variables are exactly at the bounds

At iterate    0    f=  4.16630D-02    |proj g|=  6.80072D-01
Alpha [1.31992824] Beta [2.9991534] Cmtot2 [0.03401795]
Cmtot2_Alpha [[0.60837327]]
Cmtot2_Beta [[0.0015253]]

At iterate    1    f=  3.40180D-02    |proj g|=  6.08373D-01
Alpha [-4.45133036] Beta [2.92288326] Cmtot2 [0.00071304]
Cmtot2_Alpha [[0.07860089]]
Cmtot2_Beta [[0.00107544]]

At iterate    2    f=  7.13044D-04    |proj g|=  7.86009D-02
Alpha [-5.30773219] Beta [2.90057802] Cmtot2 [2.43104345e-05]
Cmtot2_Alpha [[0.01420175]]
Cmtot2_Beta [[0.00021881]]

At iterate    3    f=  2.43104D-05    |proj g|=  1.42017D-02
Alpha [-5.49659696] Beta [2.89526135] Cmtot2 [3.72334444e-08]
Cmtot2_Alpha [[0.00055304]]
Cmtot2_Beta [[8.73257587e-06]]

At iterate    4    f=  3.72334D-08    |proj g|=  5.53036D-04
Alpha [-5.50424967] Beta [2.89504288] Cmtot2 [2.19764419e-12]
Cmtot2_Alpha [[4.24792989e-06]]
Cmtot2_Beta [[6.7141843e-08]]

At iterate    5    f=  2.19764D-12    |proj g|=  4.24793D-06

           * * *

Tit   = total number of iterations
Tnf   = total number of function evaluations
Tnint = total number of segments explored during Cauchy searches
Skip  = number of BFGS updates skipped
Nact  = number of active bounds at final generalized Cauchy point
Projg = norm of the final projected gradient
F     = final function value

           * * *

   N    Tit     Tnf  Tnint  Skip  Nact     Projg        F
    2      5      6      5     0     0   4.248D-06   2.198D-12
  F =   2.1976441939068914E-012

CONVERGENCE: REL_REDUCTION_OF_F_&lt;=_FACTR*EPSMCH             
Optimization Complete
-----------------------------------
Optimized values: [-5.50424967] [2.89504288]

real	0m30.400s
user	0m5.657s
sys	0m1.085s
+ status=0
+ set +x

=================================================
CAPS verification (using pyCAPS) case avl_OpenMDAO_3_PyTest.py passed (as expected)
=================================================

friction: /Users/jenkins/workspace/ESP_bPreBuilt/ESP126/EngSketchPad/bin/friction

=================================================
+ echo 'friction_PyTest.py test;'
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESP126/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
friction_PyTest.py test;
+ python -u friction_PyTest.py -outLevel=0
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESP126/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
Loading AIM
Setting Mach &amp; Altitude Values
Lifting Surface: Body = 1, units m
	XLE:   1.571946 -3.872983 0.249728
	XTE:   2.536563 -3.872983 0.335335
	Chord: 0.968408
	Arc:   1.985181
	T/C:   0.155975
	Type: Wing
Lifting Surface: Body = 2, units m
	XLE:   0.000000 0.000000 0.000000
	XTE:   1.614012 0.000000 0.002015
	Chord: 1.614013
	Arc:   3.308635
	T/C:   0.127839
	Type: Wing
Lifting Surface: Body = 3, units m
	XLE:   1.571946 3.872983 0.249728
	XTE:   2.536563 3.872983 0.335335
	Chord: 0.968408
	Arc:   1.985181
	T/C:   0.155975
	Type: Wing
Lifting Surface: Body = 4, units m
	XLE:   5.484123 0.000000 1.468246
	XTE:   6.210307 0.000915 1.468246
	Chord: 0.726185
	Arc:   1.482717
	T/C:   0.120035
	Type: VTail
Lifting Surface: Body = 5, units m
	XLE:   5.000000 0.000000 0.500000
	XTE:   6.210307 0.001525 0.500000
	Chord: 1.210308
	Arc:   2.471195
	T/C:   0.120035
	Type: VTail
Lifting Surface: Body = 6, units m
	XLE:   5.484123 -0.968246 0.500000
	XTE:   6.210307 -0.968246 0.500915
	Chord: 0.726185
	Arc:   1.482717
	T/C:   0.120035
	Type: HTail
Lifting Surface: Body = 7, units m
	XLE:   5.484123 0.968246 0.500000
	XTE:   6.210307 0.968246 0.500915
	Chord: 0.726185
	Arc:   1.482717
	T/C:   0.120035
	Type: HTail
Body of Revolution: Body = 8, units m
	Arc: 0.000000
	Diameter: 0.000000
	Type: Fuse
Body of Revolution: Body = 9, units m
	Arc: 3.714180
	Diameter: 1.020621
	Type: Fuse
Body of Revolution: Body = 10, units m
	Arc: 2.771209
	Diameter: 0.645497
	Type: Fuse
Body of Revolution: Body = 11, units m
	Arc: 1.013945
	Diameter: 0.322749
	Type: Fuse
Body of Revolution: Body = 12, units m
	Arc: 0.101394
	Diameter: 0.032275
	Type: Fuse
Number of sections 4, number of revolution sections 1
Number of Mach-Altitude cases = 2
Total drag = [0.0132, 0.01226]
Form drag = [0.0033, 0.00307]
Friction drag = [0.0099, 0.00919]

real	0m0.268s
user	0m0.353s
sys	0m0.067s
+ status=0
+ set +x

=================================================
CAPS verification (using pyCAPS) case friction_PyTest.py passed (as expected)
=================================================

tsfoil2: /Users/jenkins/util/tsfoil/tsfoil2

=================================================
+ echo 'tsfoil_PyTest.py test;'
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESP126/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
tsfoil_PyTest.py test;
+ python -u tsfoil_PyTest.py -outLevel=0
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESP126/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
Getting results
PAUSE Press the ENTER key to exit
To resume execution, type go.  Other input will terminate the job.
Note: The following floating-point exceptions are signalling: IEEE_OVERFLOW_FLAG IEEE_UNDERFLOW_FLAG
Cl =  0.933371
Cd =  0.000284
Cd Wave =  0.0
Cm =  -0.203435
Cp _Critcal =  -1.303869

real	0m0.424s
user	0m0.521s
sys	0m0.056s
+ status=0
+ set +x

=================================================
CAPS verification (using pyCAPS) case tsfoil_PyTest.py passed (as expected)
=================================================

mses: /Users/jenkins/workspace/ESP_bPreBuilt/ESP126/EngSketchPad/bin/mses

=================================================
+ echo 'mses_PyTest.py test;'
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESP126/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
mses_PyTest.py test;
+ python -u mses_PyTest.py -outLevel=0 -noPlotData
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESP126/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
Cl =  0.3783791085548177
Cd =  0.007775858417209677
Cm =  0.005262636995835036

real	0m1.836s
user	0m2.052s
sys	0m0.087s
+ status=0
+ set +x

=================================================
CAPS verification (using pyCAPS) case mses_PyTest.py passed (as expected)
=================================================


=================================================
+ echo 'mses_OpenMDAO_3_PyTest.py test;'
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESP126/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
mses_OpenMDAO_3_PyTest.py test;
+ python -u mses_OpenMDAO_3_PyTest.py -outLevel=0
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESP126/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
[VIGGEN.MIT.EDU:39362] shmem: mmap: an error occurred while determining whether or not /var/folders/l7/7s0m18td3fxg_w_dxpkj1d600000gp/T//ompi.VIGGEN.502/jf.0/4166778880/sm_segment.VIGGEN.502.f85c0000.0 could be created.

Getting CFD design variables.......
	Number of design variables - 1
	Design Variable name - camber
	Done getting CFD design variables
camber [0.1] CD [0.01326534]
camber [0.1] CD [0.01326534]
CD_camber [[0.1764758]]
RUNNING THE L-BFGS-B CODE

           * * *

Machine precision = 2.220D-16
 N =            1     M =           10

At X0         1 variables are exactly at the bounds

At iterate    0    f=  1.32653D-02    |proj g|=  1.76476D-01
camber [-0.0764758] CD [0.01022332]
CD_camber [[-0.08759853]]

At iterate    1    f=  1.02233D-02    |proj g|=  8.75985D-02
camber [-0.01793539] CD [0.00770373]
CD_camber [[-0.01328932]]

At iterate    2    f=  7.70373D-03    |proj g|=  1.32893D-02
camber [-0.00746613] CD [0.00760241]
CD_camber [[-0.00542337]]

At iterate    3    f=  7.60241D-03    |proj g|=  5.42337D-03
camber [-0.00024784] CD [0.00758207]
CD_camber [[-0.00011854]]

At iterate    4    f=  7.58207D-03    |proj g|=  1.18538D-04
camber [-8.65457493e-05] CD [0.00758207]
CD_camber [[-3.94469721e-06]]
camber [-0.00019629] CD [0.00758207]
CD_camber [[-8.4257979e-05]]

At iterate    5    f=  7.58207D-03    |proj g|=  8.42580D-05

           * * *

Tit   = total number of iterations
Tnf   = total number of function evaluations
Tnint = total number of segments explored during Cauchy searches
Skip  = number of BFGS updates skipped
Nact  = number of active bounds at final generalized Cauchy point
Projg = norm of the final projected gradient
F     = final function value

           * * *

   N    Tit     Tnf  Tnint  Skip  Nact     Projg        F
    1      5      7      5     0     0   8.426D-05   7.582D-03
  F =   7.5820667358142552E-003

CONVERGENCE: REL_REDUCTION_OF_F_&lt;=_FACTR*EPSMCH             
Optimization Complete
-----------------------------------
Optimized values: [-0.00019629]

real	0m13.740s
user	0m14.043s
sys	0m0.319s
+ status=0
+ set +x

=================================================
CAPS verification (using pyCAPS) case mses_OpenMDAO_3_PyTest.py passed (as expected)
=================================================

xfoil: /Users/jenkins/workspace/ESP_bPreBuilt/ESP126/EngSketchPad/bin/xfoil

=================================================
+ echo 'xfoil_PyTest.py test;'
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESP126/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
xfoil_PyTest.py test;
+ python -u xfoil_PyTest.py -outLevel=0 -noPlotData
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESP126/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
Cl =  [1.05475230551148, 1.36488869373725, 1.56607214272246, 2.03059709357768, 1.9727108312095, 1.87307153172323, 1.76050475760053]
Cd =  [0.0131991208831308, 0.0166540240605859, 0.0200551482562657, 0.0458671341873005, 0.0754256009397268, 0.0994469174479059, 0.127479430989221]
Alpha =  [0.0, 3.0, 5.0, 11.0, 13.0, 14.0, 15.0]
Transition location =  [0.49604411072842, 0.461377732041756, 0.442376568202227, 0.361251636144409, 0.276104140854608, 0.214381239321802, 0.132988264746433]

real	0m1.918s
user	0m2.153s
sys	0m0.071s
+ status=0
+ set +x

=================================================
CAPS verification (using pyCAPS) case xfoil_PyTest.py passed (as expected)
=================================================

Running.... MESH PyTests


=================================================
+ echo 'egadsTess_PyTest.py test;'
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESP126/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
egadsTess_PyTest.py test;
+ python -u egadsTess_PyTest.py -outLevel=0
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESP126/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 7
	Name = Ribs, index = 1
	Name = Skin, index = 2
	Name = Spar1, index = 3
	Name = Rib_Root, index = 4
	Name = Spar2, index = 5
	Name = Rib_Root_Point, index = 6
	Name = Wing, index = 7
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 2
	Name = LeadingEdge, index = 1
	Name = TrailingEdge, index = 2

Getting mesh sizing parameters
	Mesh sizing name - LeadingEdge
	Done getting mesh sizing parameters
Getting surface mesh for body 1 (of 4)
Getting surface mesh for body 2 (of 4)
Getting surface mesh for body 3 (of 4)
Getting surface mesh for body 4 (of 4)
Body 1 (of 4)
Number of nodes    = 3793
Number of elements = 4001
Number of triangle elements      = 0
Number of quadrilateral elements = 4001
Body 2 (of 4)
Number of nodes    = 1
Number of elements = 0
Number of triangle elements      = 0
Number of quadrilateral elements = 0
Body 3 (of 4)
Number of nodes    = 76
Number of elements = 55
Number of triangle elements      = 0
Number of quadrilateral elements = 55
Body 4 (of 4)
Number of nodes    = 100
Number of elements = 73
Number of triangle elements      = 0
Number of quadrilateral elements = 73
----------------------------
Total number of nodes    = 3970
Total number of elements = 4129

Writing Tecplot file ....
Finished writing Tecplot file


Writing ASCII STL file ....
Finished writing ASCII STL file


Writing ugrid file ....
Finished writing ugrid file


real	0m3.534s
user	0m9.999s
sys	0m5.103s
+ status=0
+ set +x

=================================================
CAPS verification (using pyCAPS) case egadsTess_PyTest.py passed (as expected)
=================================================


=================================================
+ echo 'egadsTess_Box_Quad_Pytest.py test;'
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESP126/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
egadsTess_Box_Quad_Pytest.py test;
+ python -u egadsTess_Box_Quad_Pytest.py -outLevel=0
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESP126/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 3
	Name = box1, index = 1
	Name = box2, index = 2
	Name = box3, index = 3
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 0
	Face 3 TFI quading disabled with attribute .qParams
	Face 4 TFI quading disabled with attribute .qParams
	TFI quading on all faces disabled with .qParams attribute on the body
Getting surface mesh for body 1 (of 3)
Getting surface mesh for body 2 (of 3)
Getting surface mesh for body 3 (of 3)
Body 1 (of 3)
Number of nodes    = 602
Number of elements = 600
Number of triangle elements      = 0
Number of quadrilateral elements = 600
Body 2 (of 3)
Number of nodes    = 537
Number of elements = 535
Number of triangle elements      = 0
Number of quadrilateral elements = 535
Body 3 (of 3)
Number of nodes    = 1356
Number of elements = 1354
Number of triangle elements      = 0
Number of quadrilateral elements = 1354
----------------------------
Total number of nodes    = 2495
Total number of elements = 2489

Writing Tecplot file ....
Finished writing Tecplot file


Writing ASCII STL file ....
Finished writing ASCII STL file


Writing ugrid file ....
Finished writing ugrid file


real	0m2.096s
user	0m2.624s
sys	0m0.049s
+ status=0
+ set +x

=================================================
CAPS verification (using pyCAPS) case egadsTess_Box_Quad_Pytest.py passed (as expected)
=================================================


=================================================
+ echo 'egadsTess_Spheres_Quad_PyTest.py test;'
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESP126/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
egadsTess_Spheres_Quad_PyTest.py test;
+ python -u egadsTess_Spheres_Quad_PyTest.py -outLevel=0
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESP126/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = Spheres, index = 1
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 0
	Face 4 has a degenerate edge - no TFI quading
	Face 5 has a degenerate edge - no TFI quading
Getting surface mesh for body 1 (of 1)
Body 1 (of 1)
Number of nodes    = 5907
Number of elements = 5905
Number of triangle elements      = 0
Number of quadrilateral elements = 5905
----------------------------
Total number of nodes    = 5907
Total number of elements = 5905

Writing Tecplot file ....
Finished writing Tecplot file


Writing ASCII STL file ....
Finished writing ASCII STL file


Writing ugrid file ....
Finished writing ugrid file


real	0m4.812s
user	0m7.643s
sys	0m0.118s
+ status=0
+ set +x

=================================================
CAPS verification (using pyCAPS) case egadsTess_Spheres_Quad_PyTest.py passed (as expected)
=================================================


=================================================
+ echo 'egadsTess_Nose_Quad_PyTest.py test;'
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESP126/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
egadsTess_Nose_Quad_PyTest.py test;
+ python -u egadsTess_Nose_Quad_PyTest.py -outLevel=0
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESP126/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = nose, index = 1
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 0
	Face 2 has a degenerate edge - no TFI quading
Getting surface mesh for body 1 (of 1)
 EG_getSidepoint: LineSearch Failed (0.000000 0.973785)!
 EG_getSidepoint: LineSearch Failed (2.750998 0.986828)!
 EG_getSidepoint: LineSearch Failed (2.750998 0.986828)!
 EG_getSidepoint: LineSearch Failed (2.750998 0.986828)!
 EG_getSidepoint: LineSearch Failed (1.013231 0.966690)!
 EG_getSidepoint: LineSearch Failed (2.750998 0.986828)!
 EG_getSidepoint: LineSearch Failed (1.004202 0.966536)!
 EG_getSidepoint: LineSearch Failed (2.750998 0.986828)!
 EG_getSidepoint: LineSearch Failed (1.004202 0.966536)!
 EG_getSidepoint: LineSearch Failed (2.750998 0.986828)!
 EG_getSidepoint: LineSearch Failed (1.004202 0.966536)!
 EG_getSidepoint: LineSearch Failed (2.750998 0.986828)!
 EG_getSidepoint: LineSearch Failed (1.004202 0.966536)!
 EG_getSidepoint: LineSearch Failed (2.750998 0.986828)!
 EG_getSidepoint: LineSearch Failed (1.046938 0.962477)!
 EG_getSidepoint: LineSearch Failed (2.750998 0.986828)!
 EG_getSidepoint: LineSearch Failed (1.035877 0.957484)!
 EG_getSidepoint: LineSearch Failed (2.750998 0.986828)!
 EG_getSidepoint: LineSearch Failed (1.015407 0.966058)!
 EG_getSidepoint: LineSearch Failed (2.750998 0.986828)!
 EG_getSidepoint: LineSearch Failed (0.856444 0.971910)!
 EG_getSidepoint: LineSearch Failed (2.750998 0.986828)!
 EG_getSidepoint: LineSearch Failed (0.813517 0.972994)!
 EG_getSidepoint: LineSearch Failed (0.719835 0.974156)!
 EG_getSidepoint: LineSearch Failed (0.719835 0.974156)!
 EG_getSidepoint: LineSearch Failed (0.719835 0.974156)!
 EG_getSidepoint: LineSearch Failed (0.719835 0.974156)!
 EG_getSidepoint: LineSearch Failed (0.719835 0.974156)!
 EG_getSidepoint: LineSearch Failed (0.719835 0.974156)!
 EG_getSidepoint: LineSearch Failed (0.719835 0.974156)!
 EG_getSidepoint: LineSearch Failed (0.719835 0.974156)!
 EG_getSidepoint: LineSearch Failed (0.719835 0.974156)!
 EG_getSidepoint: LineSearch Failed (0.719835 0.974156)!
Body 1 (of 1)
Number of nodes    = 1498
Number of elements = 1496
Number of triangle elements      = 0
Number of quadrilateral elements = 1496
----------------------------
Total number of nodes    = 1498
Total number of elements = 1496

Writing Tecplot file ....
Finished writing Tecplot file


Writing ASCII STL file ....
Finished writing ASCII STL file


Writing ugrid file ....
Finished writing ugrid file


real	0m1.798s
user	0m2.181s
sys	0m0.074s
+ status=0
+ set +x

=================================================
CAPS verification (using pyCAPS) case egadsTess_Nose_Quad_PyTest.py passed (as expected)
=================================================


=================================================
+ echo 'aflr2_PyTest.py test;'
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESP126/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
aflr2_PyTest.py test;
+ python -u aflr2_PyTest.py -outLevel=0
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESP126/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 5
	Name = 2DSlice, index = 1
	Name = TunnelWall, index = 2
	Name = OutFlow, index = 3
	Name = InFlow, index = 4
	Name = Airfoil, index = 5
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 4
	Name = TunnelWall, index = 1
	Name = OutFlow, index = 2
	Name = InFlow, index = 3
	Name = Airfoil, index = 4

Getting mesh sizing parameters
	Mesh sizing name - 2DSlice
	Mesh sizing name - Airfoil
	Mesh sizing name - InFlow
	Mesh sizing name - OutFlow
	Mesh sizing name - TunnelWall
	Done getting mesh sizing parameters
Getting 2D mesh for body 1 (of 1)
 
AFLR2    : ---------------------------------------
AFLR2    : AFLR2 LIBRARY
AFLR2    : ADVANCING-FRONT/LOCAL-RECONNECTION
AFLR2    : TRIA/QUAD GRID GENERATOR
AFLR2    : Version Number 9.18.1
AFLR2    : Version Date   06/11/24 @ 05:52PM
AFLR2    : Compile OS     Darwin 23.5.0 arm64
AFLR2    : Compile Date   06/11/24 @ 05:52PM
AFLR2    : Copyright 1994-2021, D.L. Marcum
AFLR2    : ---------------------------------------
 
AFLR2 IC : INPUT DATA CHECK
 
AFLR2 IC : Nodes, Faces      =       344         0
 
AFLR2    : CPU Time          =     0.000   seconds
 
AFLR2 EG : EDGE GRID RE-GENERATION
 
AFLR2 EG : Nodes, Edges      =       344       344
 
AFLR2    : CPU Time          =     0.000   seconds
 
AFLR2 IG : INITIAL GRID GENERATION
 
AFLR2 IG : Nodes, Faces      =         0         2
AFLR2 IG : Nodes, Faces      =        70       142
AFLR2 IG : Nodes, Faces      =       140       282
AFLR2 IG : Nodes, Faces      =       210       422
AFLR2 IG : Nodes, Faces      =       280       562
AFLR2 IG : Nodes, Faces      =       316       634
AFLR2 IG : Nodes, Faces      =       344       690
AFLR2 IG : Nodes, Faces      =       348       690
AFLR2 IG : Nodes, Faces      =       344       344
 
AFLR2    : CPU Time          =     0.000   seconds
 
AFLR2 GG : FIELD GRID GENERATION
 
AFLR2 GGp: Nodes, Faces      =       344       344
AFLR2 GGp: Nodes, Faces      =       681      1018
AFLR2 GGp: Nodes, Faces      =      1013      1682
AFLR2 GGp: Nodes, Faces      =      1339      2334
AFLR2 GGp: Nodes, Faces      =      1652      2960
AFLR2 GGp: Nodes, Faces      =      1957      3570
AFLR2 GGp: Nodes, Faces      =      2252      4160
AFLR2 GGp: Nodes, Faces      =      2526      4708
AFLR2 GGp: Nodes, Faces      =      2809      5274
AFLR2 GGp: Nodes, Faces      =      3083      5822
AFLR2 GGp: Nodes, Faces      =      3327      6310
AFLR2 GGp: Nodes, Faces      =      3564      6784
AFLR2 GGp: Nodes, Faces      =      3788      7232
AFLR2 GGp: Nodes, Faces      =      3995      7646
AFLR2 GGp: Nodes, Faces      =      4194      8044
AFLR2 GGp: Nodes, Faces      =      4394      8444
AFLR2 GGp: Nodes, Faces      =      4585      8826
AFLR2 GGp: Nodes, Faces      =      4772      9200
AFLR2 GGp: Nodes, Faces      =      4943      9542
AFLR2 GGp: Nodes, Faces      =      5129      9914
AFLR2 GGp: Nodes, Faces      =      5293     10242
AFLR2 GGp: Nodes, Faces      =      5447     10550
AFLR2 GGp: Nodes, Faces      =      5594     10844
AFLR2 GGp: Nodes, Faces      =      5716     11088
AFLR2 GGp: Nodes, Faces      =      5830     11316
AFLR2 GGp: Nodes, Faces      =      5909     11474
AFLR2 GGp: Nodes, Faces      =      5964     11584
AFLR2 GGp: Nodes, Faces      =      6006     11668
AFLR2 GGp: Nodes, Faces      =      6025     11706
AFLR2 GGp: Nodes, Faces      =      6034     11724
 
AFLR2    : CPU Time          =     0.009   seconds
 
AFLR2 QI : QUALITY IMPROVEMENT
 
AFLR2 QI : Nodes, Faces      =      6034     11724
AFLR2 QI : Nodes, Faces      =      6033       454
AFLR2 QI : Nodes, Faces      =      6033      5634
AFLR2 QI : Nodes, Faces      =      6033     11722
AFLR2 QI : Nodes, Faces      =      6032       462
AFLR2 QI : Nodes, Faces      =      6032      5629
AFLR2 QI : Nodes, Faces      =      6032     11720
AFLR2 QI : Nodes, Faces      =      6032       456
AFLR2 QI : Nodes, Faces      =      6032      5632
AFLR2 QI : Nodes, Faces      =      6032     11720
AFLR2 QI : Nodes, Faces      =      6032       474
AFLR2 QI : Nodes, Faces      =      6032      5623
AFLR2 QI : Nodes, Faces      =      6032     11720
AFLR2 QI : Nodes, Faces      =      6031       486
AFLR2 QI : Nodes, Faces      =      6031      5616
AFLR2 QI : Nodes, Faces      =      6031       488
AFLR2 QI : Nodes, Faces      =      6031      5616
 
AFLR2    : CPU Time          =     0.004   seconds
 
AFLR2    : DONE
EGADS Internal: Face 1, Side 4741 4722 complete [but 7915] (EG_makeConnect)!
EGADS Internal: Face 1, Side 4741 4912 complete [but 7916] (EG_makeConnect)!
EGADS Internal: Face 1, Side 5850 5858 complete [but 8742] (EG_makeConnect)!
EGADS Internal: Face 1, Side 5850 5851 complete [but 8742] (EG_makeConnect)!
EGADS Internal: Face 1, Side 5858 5851 complete [but 8791] (EG_makeConnect)!
EGADS Internal: Face 1, Side 4912 4722 complete [but 9417] (EG_makeConnect)!

Writing AFLR3 file ....
Finished writing AFLR3 file

Number of nodes = 6031
Number of elements = 6448
Number of tris = 488
Number of quad = 5616
EGADS Internal: Face 1, Side 4741 4722 complete [but 7915] (EG_makeConnect)!
EGADS Internal: Face 1, Side 4741 4912 complete [but 7916] (EG_makeConnect)!
EGADS Internal: Face 1, Side 5850 5858 complete [but 8742] (EG_makeConnect)!
EGADS Internal: Face 1, Side 5850 5851 complete [but 8742] (EG_makeConnect)!
EGADS Internal: Face 1, Side 5858 5851 complete [but 8791] (EG_makeConnect)!
EGADS Internal: Face 1, Side 4912 4722 complete [but 9417] (EG_makeConnect)!
EGADS Internal: Face 1, Side 4741 4722 complete [but 7915] (EG_makeConnect)!
EGADS Internal: Face 1, Side 4741 4912 complete [but 7916] (EG_makeConnect)!
EGADS Internal: Face 1, Side 5850 5858 complete [but 8742] (EG_makeConnect)!
EGADS Internal: Face 1, Side 5850 5851 complete [but 8742] (EG_makeConnect)!
EGADS Internal: Face 1, Side 5858 5851 complete [but 8791] (EG_makeConnect)!
EGADS Internal: Face 1, Side 4912 4722 complete [but 9417] (EG_makeConnect)!

Writing Tecplot file ....
Tecplot expects 2D meshes in the x-y plane... attempting to rotate mesh!
Swapping z and y coordinates!
Finished writing Tecplot file


real	0m0.420s
user	0m0.672s
sys	0m0.354s
+ status=0
+ set +x

=================================================
CAPS verification (using pyCAPS) case aflr2_PyTest.py passed (as expected)
=================================================


=================================================
+ echo 'aflr4_PyTest.py test;'
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESP126/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
aflr4_PyTest.py test;
+ python -u aflr4_PyTest.py -outLevel=0
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESP126/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 4
	Name = Wing1, index = 1
	Name = Wing2, index = 2
	Name = Wake, index = 3
	Name = Farfield, index = 4
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 4
	Name = Wing1, index = 1
	Name = Wing2, index = 2
	Name = Wake, index = 3
	Name = Farfield, index = 4
AFLR4    : Proximity BG Surface Grid Generation Skipped
AFLR4    : No Modifications Required

Writing Tecplot file ....
Finished writing Tecplot file


Writing ASCII STL file ....
Finished writing ASCII STL file


Writing ugrid file ....
Finished writing ugrid file


real	0m1.282s
user	0m1.468s
sys	0m0.116s
+ status=0
+ set +x

=================================================
CAPS verification (using pyCAPS) case aflr4_PyTest.py passed (as expected)
=================================================


=================================================
+ echo 'aflr4_Symmetry_PyTest.py test;'
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESP126/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
aflr4_Symmetry_PyTest.py test;
+ python -u aflr4_Symmetry_PyTest.py -outLevel=0
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESP126/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 4
	Name = Farfield, index = 1
	Name = Symmetry, index = 2
	Name = Wing1, index = 3
	Name = Wing2, index = 4
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 4
	Name = Farfield, index = 1
	Name = Symmetry, index = 2
	Name = Wing1, index = 3
	Name = Wing2, index = 4

Getting mesh sizing parameters
	Mesh sizing name - Farfield
	Mesh sizing name - Symmetry
	Done getting mesh sizing parameters
AFLR4    : Proximity BG Surface Grid Generation Skipped
AFLR4    : No Modifications Required

Writing Tecplot file ....
Finished writing Tecplot file


Writing ugrid file ....
Finished writing ugrid file


real	0m1.197s
user	0m1.397s
sys	0m0.230s
+ status=0
+ set +x

=================================================
CAPS verification (using pyCAPS) case aflr4_Symmetry_PyTest.py passed (as expected)
=================================================


=================================================
+ echo 'aflr4_Generic_Missile.py test;'
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESP126/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
aflr4_Generic_Missile.py test;
+ python -u aflr4_Generic_Missile.py -outLevel=0
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESP126/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 2
	Name = MissileOML, index = 1
	Name = Farfield, index = 2
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 0

Writing Tecplot file ....
Finished writing Tecplot file


Writing ugrid file ....
Finished writing ugrid file


real	0m3.653s
user	0m6.824s
sys	0m0.281s
+ status=0
+ set +x

=================================================
CAPS verification (using pyCAPS) case aflr4_Generic_Missile.py passed (as expected)
=================================================


=================================================
+ echo 'aflr4_TipTreat_PyTest.py test;'
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESP126/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
aflr4_TipTreat_PyTest.py test;
+ python -u aflr4_TipTreat_PyTest.py -outLevel=0 -noPlotData
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESP126/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 2
	Name = Wing, index = 1
	Name = Farfield, index = 2
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 0

Writing Tecplot file ....
Finished writing Tecplot file

Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 2
	Name = Wing, index = 1
	Name = Farfield, index = 2
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 0

Writing Tecplot file ....
Finished writing Tecplot file

Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 2
	Name = Wing, index = 1
	Name = Farfield, index = 2
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 0

Writing Tecplot file ....
Finished writing Tecplot file

Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 2
	Name = Wing, index = 1
	Name = Farfield, index = 2
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 0

Writing Tecplot file ....
Finished writing Tecplot file


real	0m4.714s
user	0m4.856s
sys	0m0.156s
+ status=0
+ set +x

=================================================
CAPS verification (using pyCAPS) case aflr4_TipTreat_PyTest.py passed (as expected)
=================================================


=================================================
+ echo 'aflr4_and_aflr3_PyTest.py test;'
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESP126/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
aflr4_and_aflr3_PyTest.py test;
+ python -u aflr4_and_aflr3_PyTest.py -outLevel=0
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESP126/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 4
	Name = Wing1, index = 1
	Name = Wing2, index = 2
	Name = Wake, index = 3
	Name = Farfield, index = 4
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 4
	Name = Wing1, index = 1
	Name = Wing2, index = 2
	Name = Wake, index = 3
	Name = Farfield, index = 4
AFLR4    : Proximity BG Surface Grid Generation Skipped
AFLR4    : No Modifications Required

Writing Tecplot file ....
Finished writing Tecplot file


Writing ASCII STL file ....
Finished writing ASCII STL file


Writing ugrid file ....
Finished writing ugrid file

Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 4
	Name = Wing1, index = 1
	Name = Wing2, index = 2
	Name = Wake, index = 3
	Name = Farfield, index = 4
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 4
	Name = Wing1, index = 1
	Name = Wing2, index = 2
	Name = Wake, index = 3
	Name = Farfield, index = 4

Getting mesh sizing parameters
	Mesh sizing name - Wing1
	Mesh sizing name - Wing2
	Done getting mesh sizing parameters
Getting volume mesh
 
AFLR2    : ---------------------------------------
AFLR2    : AFLR2 LIBRARY
AFLR2    : ADVANCING-FRONT/LOCAL-RECONNECTION
AFLR2    : TRIA/QUAD GRID GENERATOR
AFLR2    : Version Number 9.18.1
AFLR2    : Version Date   06/11/24 @ 05:52PM
AFLR2    : Compile OS     Darwin 23.5.0 arm64
AFLR2    : Compile Date   06/11/24 @ 05:52PM
AFLR2    : Copyright 1994-2021, D.L. Marcum
AFLR2    : ---------------------------------------
 
AFLR4    : ---------------------------------------
AFLR4    : AFLR4 LIBRARY
AFLR4    : ADVANCING-FRONT/LOCAL-RECONNECTION
AFLR4    : TRIA/QUAD SURFACE GRID GENERATOR
AFLR4    : Version Number 11.5.15
AFLR4    : Version Date   07/19/24 @ 07:04PM
AFLR4    : Compile OS     Darwin 23.5.0 arm64
AFLR4    : Compile Date   07/19/24 @ 07:06PM
AFLR4    : Copyright 1994-2021, D.L. Marcum
AFLR4    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.8.1
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.8.1
EGADS    : ---------------------------------------
Volume mesh:
	Number of nodes          = 150214
	Number of elements       = 450024
	Number of triangles      = 14380
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 214592
	Number of pyramids       = 425
	Number of prisms         = 220627
	Number of hexahedrals    = 0

Writing Tecplot file ....
Finished writing Tecplot file


real	0m6.580s
user	0m6.663s
sys	0m0.203s
+ status=0
+ set +x

=================================================
CAPS verification (using pyCAPS) case aflr4_and_aflr3_PyTest.py passed (as expected)
=================================================


=================================================
+ echo 'aflr4_and_aflr3_Symmetry_PyTest.py test;'
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESP126/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
aflr4_and_aflr3_Symmetry_PyTest.py test;
+ python -u aflr4_and_aflr3_Symmetry_PyTest.py -outLevel=0
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESP126/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 4
	Name = Farfield, index = 1
	Name = Symmetry, index = 2
	Name = Wing1, index = 3
	Name = Wing2, index = 4
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 4
	Name = Farfield, index = 1
	Name = Symmetry, index = 2
	Name = Wing1, index = 3
	Name = Wing2, index = 4

Getting mesh sizing parameters
	Mesh sizing name - Farfield
	Mesh sizing name - Symmetry
	Done getting mesh sizing parameters
AFLR4    : Proximity BG Surface Grid Generation Skipped
AFLR4    : No Modifications Required

Writing Tecplot file ....
Finished writing Tecplot file

Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 4
	Name = Farfield, index = 1
	Name = Symmetry, index = 2
	Name = Wing1, index = 3
	Name = Wing2, index = 4
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 4
	Name = Farfield, index = 1
	Name = Symmetry, index = 2
	Name = Wing1, index = 3
	Name = Wing2, index = 4

Getting mesh sizing parameters
	Mesh sizing name - Wing1
	Mesh sizing name - Wing2
	Done getting mesh sizing parameters
Getting volume mesh
 
AFLR2    : ---------------------------------------
AFLR2    : AFLR2 LIBRARY
AFLR2    : ADVANCING-FRONT/LOCAL-RECONNECTION
AFLR2    : TRIA/QUAD GRID GENERATOR
AFLR2    : Version Number 9.18.1
AFLR2    : Version Date   06/11/24 @ 05:52PM
AFLR2    : Compile OS     Darwin 23.5.0 arm64
AFLR2    : Compile Date   06/11/24 @ 05:52PM
AFLR2    : Copyright 1994-2021, D.L. Marcum
AFLR2    : ---------------------------------------
 
AFLR4    : ---------------------------------------
AFLR4    : AFLR4 LIBRARY
AFLR4    : ADVANCING-FRONT/LOCAL-RECONNECTION
AFLR4    : TRIA/QUAD SURFACE GRID GENERATOR
AFLR4    : Version Number 11.5.15
AFLR4    : Version Date   07/19/24 @ 07:04PM
AFLR4    : Compile OS     Darwin 23.5.0 arm64
AFLR4    : Compile Date   07/19/24 @ 07:06PM
AFLR4    : Copyright 1994-2021, D.L. Marcum
AFLR4    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.8.1
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.8.1
EGADS    : ---------------------------------------
Volume mesh:
	Number of nodes          = 333315
	Number of elements       = 1070337
	Number of triangles      = 44382
	Number of quadrilatarals = 1613
	Number of tetrahedrals   = 574947
	Number of pyramids       = 327
	Number of prisms         = 449068
	Number of hexahedrals    = 0

Writing Tecplot file ....
Finished writing Tecplot file


real	0m14.018s
user	0m14.003s
sys	0m0.423s
+ status=0
+ set +x

=================================================
CAPS verification (using pyCAPS) case aflr4_and_aflr3_Symmetry_PyTest.py passed (as expected)
=================================================


=================================================
+ echo 'aflr4_QuadMesh_PyTest.py test;'
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESP126/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
aflr4_QuadMesh_PyTest.py test;
+ python -u aflr4_QuadMesh_PyTest.py -outLevel=0
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESP126/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 5
	Name = Ribs, index = 1
	Name = Skin, index = 2
	Name = Spar1, index = 3
	Name = Rib_Root, index = 4
	Name = Spar2, index = 5
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 2
	Name = LeadingEdge, index = 1
	Name = TrailingEdge, index = 2

Writing Tecplot file ....
Finished writing Tecplot file


Writing ugrid file ....
Finished writing ugrid file


real	0m3.966s
user	0m10.458s
sys	0m4.729s
+ status=0
+ set +x

=================================================
CAPS verification (using pyCAPS) case aflr4_QuadMesh_PyTest.py passed (as expected)
=================================================


=================================================
+ echo 'aflr4_and_Tetgen_PyTest.py test;'
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESP126/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
aflr4_and_Tetgen_PyTest.py test;
+ python -u aflr4_and_Tetgen_PyTest.py -outLevel=0
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESP126/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 3
	Name = Wing1, index = 1
	Name = Wing2, index = 2
	Name = Farfield, index = 3
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 3
	Name = Wing1, index = 1
	Name = Wing2, index = 2
	Name = Farfield, index = 3
AFLR4    : Proximity BG Surface Grid Generation Skipped
AFLR4    : No Modifications Required

Writing Tecplot file ....
Finished writing Tecplot file

Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 3
	Name = Wing1, index = 1
	Name = Wing2, index = 2
	Name = Farfield, index = 3
Number of surface: nodes - 30048, elements - 60084
Getting volume mesh

Generating volume mesh using TetGen.....

Tetgen input string = pYq1.500/0.000QT1.00e-16A
Done meshing using TetGen!

Writing Tecplot file ....
Finished writing Tecplot file


real	0m5.800s
user	0m5.889s
sys	0m0.204s
+ status=0
+ set +x

=================================================
CAPS verification (using pyCAPS) case aflr4_and_Tetgen_PyTest.py passed (as expected)
=================================================


=================================================
+ echo 'aflr4_tetgen_Regions_PyTest.py test;'
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESP126/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
aflr4_tetgen_Regions_PyTest.py test;
+ python -u aflr4_tetgen_Regions_PyTest.py -outLevel=0
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESP126/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 2
	Name = box, index = 1
	Name = cut, index = 2
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 0
 
AFLR2    : ---------------------------------------
AFLR2    : AFLR2 LIBRARY
AFLR2    : ADVANCING-FRONT/LOCAL-RECONNECTION
AFLR2    : TRIA/QUAD GRID GENERATOR
AFLR2    : Version Number 9.18.1
AFLR2    : Version Date   06/11/24 @ 05:52PM
AFLR2    : Compile OS     Darwin 23.5.0 arm64
AFLR2    : Compile Date   06/11/24 @ 05:52PM
AFLR2    : Copyright 1994-2021, D.L. Marcum
AFLR2    : ---------------------------------------
 
AFLR4    : ---------------------------------------
AFLR4    : AFLR4 LIBRARY
AFLR4    : ADVANCING-FRONT/LOCAL-RECONNECTION
AFLR4    : TRIA/QUAD SURFACE GRID GENERATOR
AFLR4    : Version Number 11.5.15
AFLR4    : Version Date   07/19/24 @ 07:04PM
AFLR4    : Compile OS     Darwin 23.5.0 arm64
AFLR4    : Compile Date   07/19/24 @ 07:06PM
AFLR4    : Copyright 1994-2021, D.L. Marcum
AFLR4    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.8.1
EGADS    : ---------------------------------------

EGADS    : EGADS CAD Geometry Setup

EGADS    : Model has 1 Active Bodies

EGADS    : Body 0 is a SheetBody
EGADS    : Body 0 has 1 Shells
EGADS    : Body 0 has 11 Faces
EGADS    : Body 0 has 20 Edges
EGADS    : Body 0 has 11 Loops
EGADS    : Body 0 has 12 Nodes

EGADS    : Check Grid BCs

EGADS    : Grid BCs are OK

EGADS    : Face Neighbor-Faces Information

EGADS    : QC  = Face Quad Combination Flag
EGADS    : IER = Face Isolated Edge Refinement Flag
EGADS    : ER  = Face Edge Refinement Factor
EGADS    :       Not applicable for Faces with a FarField Grid BC.
EGADS    : SF  = Face Scale Factor
EGADS    :       Not applicable for Faces with a FarField Grid BC.

EGADS    :   Face          Body    QC   IER       ER    Scale   Neighbor
EGADS    :     ID  Active    ID  Flag  Flag   Weight   Factor   Faces
EGADS    :      1     Yes     0     0     1        0        1   2 6 8 10 11
EGADS    :      2     Yes     0     0     1        0        1   1 3 7 9 11
EGADS    :      3     Yes     0     0     1        0        1   2 4 6 9 11
EGADS    :      4     Yes     0     0     1        0        1   3 5 7 9 11
EGADS    :      5     Yes     0     0     1        0        1   4 6 8 10 11
EGADS    :      6     Yes     0     0     1        0        1   1 3 5 10 11
EGADS    :      7     Yes     0     0     1        0        1   2 4 8 9 11
EGADS    :      8     Yes     0     0     1        0        1   1 5 7 10 11
EGADS    :      9     Yes     0     0     1        0        1   2 3 4 7
EGADS    :     10     Yes     0     0     1        0        1   1 5 6 8
EGADS    :     11     Yes     0     0     1        0        1   1 2 3 4 5 6 7 8

EGADS    : Face Edges Information

EGADS    :   Face   Edges
EGADS    :      1   -1 2 3 -4
EGADS    :      2   -5 6 7 -2
EGADS    :      3   8 5 9 -10
EGADS    :      4   10 11 -12 -13
EGADS    :      5   14 15 -16 -11
EGADS    :      6   1 -17 -14 -9
EGADS    :      7   -18 12 -19 -7
EGADS    :      8   16 20 -3 19
EGADS    :      9   13 18 -6 -8
EGADS    :     10   -15 17 4 -20
EGADS    :     11   11 -19 -2 9

EGADS    : Face Loops Information

EGADS    :   Face   Loops
EGADS    :      1   1
EGADS    :      2   2
EGADS    :      3   3
EGADS    :      4   4
EGADS    :      5   5
EGADS    :      6   6
EGADS    :      7   7
EGADS    :      8   8
EGADS    :      9   9
EGADS    :     10   10
EGADS    :     11   11

EGADS    : Loop Edges Information

EGADS    :   Loop  Active   Edges
EGADS    :      1     Yes   -1 2 3 -4
EGADS    :      2     Yes   -5 6 7 -2
EGADS    :      3     Yes   8 5 9 -10
EGADS    :      4     Yes   10 11 -12 -13
EGADS    :      5     Yes   14 15 -16 -11
EGADS    :      6     Yes   1 -17 -14 -9
EGADS    :      7     Yes   -18 12 -19 -7
EGADS    :      8     Yes   16 20 -3 19
EGADS    :      9     Yes   13 18 -6 -8
EGADS    :     10     Yes   -15 17 4 -20
EGADS    :     11     Yes   11 -19 -2 9

EGADS    : Edge Node, Scale Factor, and Neighbor-Faces Information

EGADS    : ESF = Edge Scale Factor
EGADS    :       Not applicable for DEGENERATE Edges or Edges with a FarField
EGADS    :       Grid BC Neighbor Face.

EGADS    :                                             Neighbor
EGADS    :   Edge  Body  Active Node1 Node2      ESF   Faces
EGADS    :      1     0     Yes     1     2        1   1 6
EGADS    :      2     0     Yes     1     3        1   1 2 11
EGADS    :      3     0     Yes     3     4        1   1 8
EGADS    :      4     0     Yes     2     4        1   1 10
EGADS    :      5     0     Yes     5     1        1   2 3
EGADS    :      6     0     Yes     5     6        1   2 9
EGADS    :      7     0     Yes     6     3        1   2 7
EGADS    :      8     0     Yes     7     5        1   3 9
EGADS    :      9     0     Yes     1     8        1   3 6 11
EGADS    :     10     0     Yes     7     8        1   3 4
EGADS    :     11     0     Yes     8     9        1   4 5 11
EGADS    :     12     0     Yes    10     9        1   4 7
EGADS    :     13     0     Yes     7    10        1   4 9
EGADS    :     14     0     Yes     8    11        1   5 6
EGADS    :     15     0     Yes    11    12        1   5 10
EGADS    :     16     0     Yes     9    12        1   5 8
EGADS    :     17     0     Yes    11     2        1   6 10
EGADS    :     18     0     Yes    10     6        1   7 9
EGADS    :     19     0     Yes     3     9        1   7 8 11
EGADS    :     20     0     Yes    12     4        1   8 10

EGADS    : Node Information

EGADS    :   Node  Active      Coordinates
EGADS    :      1     Yes                1                0                0
EGADS    :      2     Yes                1                0                2
EGADS    :      3     Yes                1                1                1
EGADS    :      4     Yes                1                1                2
EGADS    :      5     Yes                1                0                0
EGADS    :      6     Yes                1                1                0
EGADS    :      7     Yes                0                0                0
EGADS    :      8     Yes                0                0                0
EGADS    :      9     Yes                0                1                1
EGADS    :     10     Yes                0                1                0
EGADS    :     11     Yes                0                0                2
EGADS    :     12     Yes                0                1                2

EGADS    : Face and Edge Match Information

EGADS    : No Face Matches Found

AFLR4    : Surface Mesh Spacing Setup

AFLR4    : Max Bounding Box Length     = 4
AFLR4    : Min Bounding Box Length     = 2
AFLR4    : Max Ref Bounding Box Length = 4
AFLR4    : Min Ref Bounding Box Length = 2
AFLR4    : Reference Length            = 1
AFLR4    : BL Thickness                = 0
AFLR4    : Abs Min Surf Spacing        = 0.0025
AFLR4    : Min Surf Spacing            = 0.01
AFLR4    : Max Surf Spacing            = 0.2
AFLR4    : Global Scale Factor         = 1

AFLR4    : Geometry Definition Information

AFLR4    : Definition              Definition   Composite             Grid BC
AFLR4    :         ID                    Type          ID                Type
AFLR4    :          0     glue-only composite           -                   -
AFLR4    :          1            CAD geometry           0            STD w/BL
AFLR4    :          2            CAD geometry           0            STD w/BL
AFLR4    :          3            CAD geometry           0            STD w/BL
AFLR4    :          4            CAD geometry           0            STD w/BL
AFLR4    :          5            CAD geometry           0            STD w/BL
AFLR4    :          6            CAD geometry           0            STD w/BL
AFLR4    :          7            CAD geometry           0            STD w/BL
AFLR4    :          8            CAD geometry           0            STD w/BL
AFLR4    :          9            CAD geometry           0            STD w/BL
AFLR4    :         10            CAD geometry           0            STD w/BL
AFLR4    :         11            CAD geometry           0              TRANSP

AFLR4    : Define CAD surface definition 1
AFLR4    : Define CAD surface definition 2
AFLR4    : Define CAD surface definition 3
AFLR4    : Define CAD surface definition 4
AFLR4    : Define CAD surface definition 5
AFLR4    : Define CAD surface definition 6
AFLR4    : Define CAD surface definition 7
AFLR4    : Define CAD surface definition 8
AFLR4    : Define CAD surface definition 9
AFLR4    : Define CAD surface definition 10
AFLR4    : Define CAD surface definition 11

AFLR4    : Surface Grid Generation

AFLR4    : Generate optimal mesh on surface definition 1
AFLR2    : Nodes, Trias,Quads=       137       228         0
AFLR4    : Nodes, Trias,Quads=       131       216         0

AFLR4    : Generate optimal mesh on surface definition 2
AFLR2    : Nodes, Trias,Quads=       137       228         0
AFLR4    : Nodes, Trias,Quads=       132       218         0

AFLR4    : Generate optimal mesh on surface definition 3
AFLR2    : Nodes, Trias,Quads=        76       120         0
AFLR4    : Nodes, Trias,Quads=        72       112         0

AFLR4    : Generate optimal mesh on surface definition 4
AFLR2    : Nodes, Trias,Quads=       137       228         0
AFLR4    : Nodes, Trias,Quads=       132       218         0

AFLR4    : Generate optimal mesh on surface definition 5
AFLR2    : Nodes, Trias,Quads=       137       228         0
AFLR4    : Nodes, Trias,Quads=       131       216         0

AFLR4    : Generate optimal mesh on surface definition 6
AFLR2    : Nodes, Trias,Quads=       196       340         0
AFLR4    : Nodes, Trias,Quads=       192       332         0

AFLR4    : Generate optimal mesh on surface definition 7
AFLR2    : Nodes, Trias,Quads=       196       340         0
AFLR4    : Nodes, Trias,Quads=       192       332         0

AFLR4    : Generate optimal mesh on surface definition 8
AFLR2    : Nodes, Trias,Quads=        76       120         0
AFLR4    : Nodes, Trias,Quads=        72       112         0

AFLR4    : Generate optimal mesh on surface definition 9
AFLR2    : Nodes, Trias,Quads=       136       230         0
AFLR4    : Nodes, Trias,Quads=       132       222         0

AFLR4    : Generate optimal mesh on surface definition 10
AFLR2    : Nodes, Trias,Quads=       136       230         0
AFLR4    : Nodes, Trias,Quads=       132       222         0

AFLR4    : Generate optimal mesh on surface definition 11
AFLR2    : Nodes, Trias,Quads=       184       318         0
AFLR4    : Nodes, Trias,Quads=       178       306         0

DGEOM    : Add surface definitions to composite definition 0
DGEOM    : Glue composite surface definition 0
DGEOM    : Nodes,Faces,BEdges=      1232      2506       464

AFLR4    : Curvature BG Surface Grid Generation

AFLR4    : Nodes, Faces      =      1232      2506

AFLR4    : Surface Grid Generation

AFLR4    : Generate optimal mesh on surface definition 1
AFLR2    : Nodes, Trias,Quads=       140       234         0
AFLR4    : Nodes, Trias,Quads=       134       222         0

AFLR4    : Generate optimal mesh on surface definition 2
AFLR2    : Nodes, Trias,Quads=       140       234         0
AFLR4    : Nodes, Trias,Quads=       133       220         0

AFLR4    : Generate optimal mesh on surface definition 3
AFLR2    : Nodes, Trias,Quads=        76       120         0
AFLR4    : Nodes, Trias,Quads=        72       112         0

AFLR4    : Generate optimal mesh on surface definition 4
AFLR2    : Nodes, Trias,Quads=       141       236         0
AFLR4    : Nodes, Trias,Quads=       133       220         0

AFLR4    : Generate optimal mesh on surface definition 5
AFLR2    : Nodes, Trias,Quads=       141       236         0
AFLR4    : Nodes, Trias,Quads=       133       220         0

AFLR4    : Generate optimal mesh on surface definition 6
AFLR2    : Nodes, Trias,Quads=       207       362         0
AFLR4    : Nodes, Trias,Quads=       192       332         0

AFLR4    : Generate optimal mesh on surface definition 7
AFLR2    : Nodes, Trias,Quads=       205       358         0
AFLR4    : Nodes, Trias,Quads=       192       332         0

AFLR4    : Generate optimal mesh on surface definition 8
AFLR2    : Nodes, Trias,Quads=        76       120         0
AFLR4    : Nodes, Trias,Quads=        72       112         0

AFLR4    : Generate optimal mesh on surface definition 9
AFLR2    : Nodes, Trias,Quads=       136       230         0
AFLR4    : Nodes, Trias,Quads=       132       222         0

AFLR4    : Generate optimal mesh on surface definition 10
AFLR2    : Nodes, Trias,Quads=       137       232         0
AFLR4    : Nodes, Trias,Quads=       132       222         0

AFLR4    : Generate optimal mesh on surface definition 11
AFLR2    : Nodes, Trias,Quads=       193       336         0
AFLR4    : Nodes, Trias,Quads=       183       316         0

DGEOM    : Add surface definitions to composite definition 0
DGEOM    : Glue composite surface definition 0
DGEOM    : Nodes,Faces,BEdges=      1244      2530       464

OVERALL  : CPU Time          =     0.048   seconds
Body 1 (of 1)
Number of nodes    = 1244
Number of elements = 2530
Number of triangle elements      = 2530
Number of quadrilateral elements = 0
----------------------------
Total number of nodes    = 1244
Total number of elements = 2530
Total number of triangle elements      = 2530
Total number of quadrilateral elements = 0
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 2
	Name = box, index = 1
	Name = cut, index = 2
Number of surface: nodes - 1244, elements - 2530
Getting volume mesh

Generating volume mesh using TetGen.....

Tetgen input string = pYq1.500/0.000T1.00e-16A
Delaunizing vertices...
Delaunay seconds:  0.019871
Creating surface mesh ...
Surface mesh seconds:  0.000688
Recovering boundaries...
Boundary recovery seconds:  0.008788
Removing exterior tetrahedra ...
Spreading region attributes.
Exterior tets removal seconds:  0.000389
Recovering Delaunayness...
Delaunay recovery seconds:  0.005326
Refining mesh...
Refinement seconds:  0.010017
Smoothing vertices...
Mesh smoothing seconds:  0.020961
Improving mesh...
Mesh improvement seconds:  0.000751

Writing nodes.
Writing elements.
Writing faces.
Writing edges.

Output seconds:  0.000142
Total running seconds:  0.066985

Statistics:

  Input points: 1244
  Input facets: 2530
  Input segments: 3771
  Input holes: 0
  Input regions: 2

  Mesh points: 1454
  Mesh tetrahedra: 5098
  Mesh faces: 11303
  Mesh faces on exterior boundary: 2214
  Mesh faces on input facets: 2530
  Mesh edges on input segments: 3771
  Steiner points inside domain: 210

Done meshing using TetGen!

Writing vtk file ....

Writing vtk general file ....
Finished writing vtk file


Writing Tecplot file ....
Finished writing Tecplot file


real	0m0.383s
user	0m0.565s
sys	0m0.087s
+ status=0
+ set +x

=================================================
CAPS verification (using pyCAPS) case aflr4_tetgen_Regions_PyTest.py passed (as expected)
=================================================


=================================================
+ echo 'tetgen_PyTest.py test;'
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESP126/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
tetgen_PyTest.py test;
+ python -u tetgen_PyTest.py -outLevel=0
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESP126/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 3
	Name = Wing1, index = 1
	Name = Wing2, index = 2
	Name = Farfield, index = 3
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 3
	Name = Wing1, index = 1
	Name = Wing2, index = 2
	Name = Farfield, index = 3
Getting surface mesh for body 1 (of 3)
Getting surface mesh for body 2 (of 3)
Getting surface mesh for body 3 (of 3)
Body 1 (of 3)
Number of nodes    = 2236
Number of elements = 4468
Number of triangle elements      = 4468
Number of quadrilateral elements = 0
Body 2 (of 3)
Number of nodes    = 636
Number of elements = 1268
Number of triangle elements      = 1268
Number of quadrilateral elements = 0
Body 3 (of 3)
Number of nodes    = 258
Number of elements = 512
Number of triangle elements      = 512
Number of quadrilateral elements = 0
----------------------------
Total number of nodes    = 3130
Total number of elements = 6248

Writing Tecplot file ....
Finished writing Tecplot file

Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 3
	Name = Wing1, index = 1
	Name = Wing2, index = 2
	Name = Farfield, index = 3
Number of surface: nodes - 3130, elements - 6248
Getting volume mesh

Generating volume mesh using TetGen.....

Tetgen input string = pYq1.500/0.000T1.00e-16A
Delaunizing vertices...
Delaunay seconds:  0.01326
Creating surface mesh ...
Surface mesh seconds:  0.001698
Recovering boundaries...
Boundary recovery seconds:  0.039672
Removing exterior tetrahedra ...
Spreading region attributes.
Exterior tets removal seconds:  0.002344
Suppressing Steiner points ...
Steiner suppression seconds:  5e-06
Recovering Delaunayness...
Delaunay recovery seconds:  0.00483
Refining mesh...
  4177 insertions, added 2159 points, 136953 tetrahedra in queue.
  1390 insertions, added 372 points, 139199 tetrahedra in queue.
  1853 insertions, added 454 points, 136118 tetrahedra in queue.
  2470 insertions, added 521 points, 118263 tetrahedra in queue.
  3293 insertions, added 464 points, 66933 tetrahedra in queue.
  4389 insertions, added 406 points, 1337 tetrahedra in queue.
  5851 insertions, added 599 points, 33 tetrahedra in queue.
Refinement seconds:  0.343795
Smoothing vertices...
Mesh smoothing seconds:  0.18073
Improving mesh...
Mesh improvement seconds:  0.00599
Jettisoning redundant points.

Writing nodes.
Writing elements.
Writing faces.
Writing edges.

Output seconds:  0.000564
Total running seconds:  0.593005

Statistics:

  Input points: 3130
  Input facets: 6248
  Input segments: 9372
  Input holes: 2
  Input regions: 0

  Mesh points: 8156
  Mesh tetrahedra: 40155
  Mesh faces: 83435
  Mesh faces on exterior boundary: 6250
  Mesh faces on input facets: 6250
  Mesh edges on input segments: 9373
  Steiner points on input segments:  1
  Steiner points inside domain: 5025

Done meshing using TetGen!
Volume mesher did not preserve surface elements - data transfer will NOT be possible.

Writing Tecplot file ....
Finished writing Tecplot file


real	0m1.339s
user	0m1.592s
sys	0m0.127s
+ status=0
+ set +x

=================================================
CAPS verification (using pyCAPS) case tetgen_PyTest.py passed (as expected)
=================================================


=================================================
+ echo 'tetgen_Holes_PyTest.py test;'
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESP126/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
tetgen_Holes_PyTest.py test;
+ python -u tetgen_Holes_PyTest.py -outLevel=0
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESP126/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 2
	Name = box, index = 1
	Name = cut, index = 2
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 0
Getting surface mesh for body 1 (of 1)
Body 1 (of 1)
Number of nodes    = 8995
Number of elements = 18112
Number of triangle elements      = 18112
Number of quadrilateral elements = 0
----------------------------
Total number of nodes    = 8995
Total number of elements = 18112

Writing Tecplot file ....
Finished writing Tecplot file


Writing vtk file ....

Writing vtk surface file ....

capsGroups found:
  1: box
  2: cut
Finished writing vtk file

Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 2
	Name = box, index = 1
	Name = cut, index = 2
Number of surface: nodes - 8995, elements - 18112
Getting volume mesh

Generating volume mesh using TetGen.....

Tetgen input string = pYq1.500/0.000T1.00e-16A
Delaunizing vertices...
Delaunay seconds:  0.154076
Creating surface mesh ...
Surface mesh seconds:  0.00472
Recovering boundaries...
Boundary recovery seconds:  0.054226
Removing exterior tetrahedra ...
Spreading region attributes.
Exterior tets removal seconds:  0.004389
Recovering Delaunayness...
Delaunay recovery seconds:  0.033488
Refining mesh...
Refinement seconds:  0.133818
Smoothing vertices...
Mesh smoothing seconds:  0.149059
Improving mesh...
Mesh improvement seconds:  0.005243
Jettisoning redundant points.

Writing nodes.
Writing elements.
Writing faces.
Writing edges.

Output seconds:  0.000984
Total running seconds:  0.540165

Statistics:

  Input points: 8995
  Input facets: 18112
  Input segments: 27104
  Input holes: 1
  Input regions: 0

  Mesh points: 7154
  Mesh tetrahedra: 27977
  Mesh faces: 60994
  Mesh faces on exterior boundary: 10080
  Mesh faces on input facets: 10080
  Mesh edges on input segments: 15120
  Steiner points inside domain: 2112

Done meshing using TetGen!
Volume mesher did not preserve surface elements - data transfer will NOT be possible.

Writing Tecplot file ....
Finished writing Tecplot file


Writing vtk file ....

Writing vtk general file ....
Finished writing vtk file


real	0m1.211s
user	0m1.439s
sys	0m0.088s
+ status=0
+ set +x

=================================================
CAPS verification (using pyCAPS) case tetgen_Holes_PyTest.py passed (as expected)
=================================================


=================================================
+ echo 'tetgen_Regions_PyTest.py test;'
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESP126/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
tetgen_Regions_PyTest.py test;
+ python -u tetgen_Regions_PyTest.py -outLevel=0
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESP126/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 2
	Name = box, index = 1
	Name = cut, index = 2
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 0
Getting surface mesh for body 1 (of 1)
Body 1 (of 1)
Number of nodes    = 8995
Number of elements = 18112
Number of triangle elements      = 18112
Number of quadrilateral elements = 0
----------------------------
Total number of nodes    = 8995
Total number of elements = 18112

Writing Tecplot file ....
Finished writing Tecplot file


Writing vtk file ....

Writing vtk surface file ....

capsGroups found:
  1: box
  2: cut
Finished writing vtk file

Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 2
	Name = box, index = 1
	Name = cut, index = 2
Number of surface: nodes - 8995, elements - 18112
Getting volume mesh

Generating volume mesh using TetGen.....

Tetgen input string = pYq1.500/0.000T1.00e-16A
Delaunizing vertices...
Delaunay seconds:  0.155512
Creating surface mesh ...
Surface mesh seconds:  0.005184
Recovering boundaries...
Boundary recovery seconds:  0.055244
Removing exterior tetrahedra ...
Spreading region attributes.
Exterior tets removal seconds:  0.003265
Recovering Delaunayness...
Delaunay recovery seconds:  0.064816
Refining mesh...
Refinement seconds:  0.273324
Smoothing vertices...
Mesh smoothing seconds:  0.315623
Improving mesh...
Mesh improvement seconds:  0.009422

Writing nodes.
Writing elements.
Writing faces.
Writing edges.

Output seconds:  0.001374
Total running seconds:  0.883939

Statistics:

  Input points: 8995
  Input facets: 18112
  Input segments: 27104
  Input holes: 0
  Input regions: 2

  Mesh points: 13174
  Mesh tetrahedra: 55665
  Mesh faces: 119362
  Mesh faces on exterior boundary: 16064
  Mesh faces on input facets: 18112
  Mesh edges on input segments: 27104
  Steiner points inside domain: 4179

Done meshing using TetGen!

Writing Tecplot file ....
Finished writing Tecplot file


Writing vtk file ....

Writing vtk general file ....
Finished writing vtk file


real	0m1.587s
user	0m1.810s
sys	0m0.091s
+ status=0
+ set +x

=================================================
CAPS verification (using pyCAPS) case tetgen_Regions_PyTest.py passed (as expected)
=================================================

delaundo: /Users/jenkins/util/delaundo/delaundo/src/delaundo

=================================================
+ echo 'delaundo_PyTest.py test;'
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESP126/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
delaundo_PyTest.py test;
+ python -u delaundo_PyTest.py -outLevel=0
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESP126/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 6
	Name = 2DSlice, index = 1
	Name = TunnelWall, index = 2
	Name = OutFlow, index = 3
	Name = InFlow, index = 4
	Name = Airfoil, index = 5
	Name = AirfoilTE, index = 6
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 6
	Name = 2DSlice, index = 1
	Name = TunnelWall, index = 2
	Name = OutFlow, index = 3
	Name = InFlow, index = 4
	Name = Airfoil, index = 5
	Name = AirfoilTE, index = 6

Getting mesh sizing parameters
	Mesh sizing name - Airfoil
	Mesh sizing name - AirfoilTE
	Mesh sizing name - InFlow
	Mesh sizing name - OutFlow
	Mesh sizing name - TunnelWall
	Done getting mesh sizing parameters
Getting edge discretization for body 1
	Delaundo expects 2D meshes in the x-y plane... attempting to rotate mesh through node swapping!
	Swapping z and y coordinates!
Writing delaundo control file - delaundo.ctr
	Writing out *.pts file
Reading delaundo mesh file - delaundo_CAPS.mesh
	Swapping y and z coordinates!

Writing Tecplot file ....
Tecplot expects 2D meshes in the x-y plane... attempting to rotate mesh!
Swapping z and y coordinates!
Finished writing Tecplot file


Writing ugrid file ....
Finished writing ugrid file


real	0m0.526s
user	0m0.614s
sys	0m0.248s
+ status=0
+ set +x

=================================================
CAPS verification (using pyCAPS) case delaundo_PyTest.py passed (as expected)
=================================================

Running.... CFD PyTests


=================================================
+ echo 'su2_and_AFLR2_NodeDist_PyTest.py test;'
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESP126/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
su2_and_AFLR2_NodeDist_PyTest.py test;
+ python -u su2_and_AFLR2_NodeDist_PyTest.py -outLevel=0
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESP126/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 5
	Name = 2DSlice, index = 1
	Name = TunnelWall, index = 2
	Name = OutFlow, index = 3
	Name = InFlow, index = 4
	Name = Airfoil, index = 5
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 4
	Name = TunnelWall, index = 1
	Name = OutFlow, index = 2
	Name = InFlow, index = 3
	Name = Airfoil, index = 4

Getting mesh sizing parameters
	Mesh sizing name - 2DSlice
	Mesh sizing name - Airfoil
	Mesh sizing name - InFlow
	Mesh sizing name - OutFlow
	Mesh sizing name - TunnelWall
	Done getting mesh sizing parameters
Getting 2D mesh for body 1 (of 1)
 
AFLR2    : ---------------------------------------
AFLR2    : AFLR2 LIBRARY
AFLR2    : ADVANCING-FRONT/LOCAL-RECONNECTION
AFLR2    : TRIA/QUAD GRID GENERATOR
AFLR2    : Version Number 9.18.1
AFLR2    : Version Date   06/11/24 @ 05:52PM
AFLR2    : Compile OS     Darwin 23.5.0 arm64
AFLR2    : Compile Date   06/11/24 @ 05:52PM
AFLR2    : Copyright 1994-2021, D.L. Marcum
AFLR2    : ---------------------------------------
 
AFLR2 IC : INPUT DATA CHECK
 
AFLR2 IC : Nodes, Faces      =       224         0
 
AFLR2    : CPU Time          =     0.000   seconds
 
AFLR2 EG : EDGE GRID RE-GENERATION
 
AFLR2 EG : Nodes, Edges      =       224       224
 
AFLR2    : CPU Time          =     0.000   seconds
 
AFLR2 IG : INITIAL GRID GENERATION
 
AFLR2 IG : Nodes, Faces      =         0         2
AFLR2 IG : Nodes, Faces      =        46        94
AFLR2 IG : Nodes, Faces      =        92       186
AFLR2 IG : Nodes, Faces      =       138       278
AFLR2 IG : Nodes, Faces      =       184       370
AFLR2 IG : Nodes, Faces      =       196       394
AFLR2 IG : Nodes, Faces      =       224       450
AFLR2 IG : Nodes, Faces      =       228       450
AFLR2 IG : Nodes, Faces      =       224       224
 
AFLR2    : CPU Time          =     0.000   seconds
 
AFLR2 GG : FIELD GRID GENERATION
 
AFLR2 GG : Nodes, Faces      =       224       224
AFLR2 GG : Nodes, Faces      =       440       656
AFLR2 GG : Nodes, Faces      =       649      1074
AFLR2 GG : Nodes, Faces      =       853      1482
AFLR2 GG : Nodes, Faces      =      1050      1876
AFLR2 GG : Nodes, Faces      =      1238      2252
AFLR2 GG : Nodes, Faces      =      1421      2618
AFLR2 GG : Nodes, Faces      =      1594      2964
AFLR2 GG : Nodes, Faces      =      1760      3296
AFLR2 GG : Nodes, Faces      =      1915      3606
AFLR2 GG : Nodes, Faces      =      2063      3902
AFLR2 GG : Nodes, Faces      =      2202      4180
AFLR2 GG : Nodes, Faces      =      2314      4404
AFLR2 GG : Nodes, Faces      =      2423      4622
AFLR2 GG : Nodes, Faces      =      2528      4832
AFLR2 GG : Nodes, Faces      =      2634      5044
AFLR2 GG : Nodes, Faces      =      2732      5240
AFLR2 GG : Nodes, Faces      =      2831      5438
AFLR2 GG : Nodes, Faces      =      2927      5630
AFLR2 GG : Nodes, Faces      =      3018      5812
AFLR2 GG : Nodes, Faces      =      3109      5994
AFLR2 GG : Nodes, Faces      =      3202      6180
AFLR2 GG : Nodes, Faces      =      3295      6366
AFLR2 GG : Nodes, Faces      =      3386      6548
AFLR2 GG : Nodes, Faces      =      3464      6704
AFLR2 GG : Nodes, Faces      =      3535      6846
AFLR2 GG : Nodes, Faces      =      3594      6964
AFLR2 GG : Nodes, Faces      =      3639      7054
AFLR2 GG : Nodes, Faces      =      3671      7118
AFLR2 GG : Nodes, Faces      =      3691      7158
AFLR2 GG : Nodes, Faces      =      3705      7186
AFLR2 GG : Nodes, Faces      =      3712      7200
AFLR2 GG : Nodes, Faces      =      3715      7206
 
AFLR2    : CPU Time          =     0.004   seconds
 
AFLR2 QI : QUALITY IMPROVEMENT
 
AFLR2 QI : Nodes, Faces      =      3715      7206
 
AFLR2    : CPU Time          =     0.000   seconds
 
AFLR2    : DONE

Writing AFLR3 file ....
Finished writing AFLR3 file

Number of nodes = 3715
Number of elements = 7430
Number of tris = 7206
Number of quad = 0

Writing SU2 file ....
SU2 expects 2D meshes in the x-y plane... attempting to rotate mesh!
Swapping z and y coordinates!
Finished writing SU2 file

Getting CFD boundary conditions
	Boundary condition name - Airfoil
	Boundary condition name - InFlow
	Boundary condition name - OutFlow
	Boundary condition name - TunnelWall
	Done getting CFD boundary conditions
Warning: The su2 cfg file will be overwritten!
Write SU2 configuration file for version "Harrier (8.0.1)"


Running SU2......

-------------------------------------------------------------------------
|    ___ _   _ ___                                                      |
|   / __| | | |_  )   Release 8.0.0 "Harrier"                           |
|   \__ \ |_| |/ /                                                      |
|   |___/\___//___|   Suite (Computational Fluid Dynamics Code)         |
|                                                                       |
-------------------------------------------------------------------------
| SU2 Project Website: <a href='https://su2code.github.io'>https://su2code.github.io</a>                        |
|                                                                       |
| The SU2 Project is maintained by the SU2 Foundation                   |
| (<a href='http://su2foundation.org'>http://su2foundation.org</a>)                                            |
-------------------------------------------------------------------------
| Copyright 2012-2023, SU2 Contributors                                 |
|                                                                       |
| SU2 is free software; you can redistribute it and/or                  |
| modify it under the terms of the GNU Lesser General Public            |
| License as published by the Free Software Foundation; either          |
| version 2.1 of the License, or (at your option) any later version.    |
|                                                                       |
| SU2 is distributed in the hope that it will be useful,                |
| but WITHOUT ANY WARRANTY; without even the implied warranty of        |
| MERCHANTABILITY or FITNESS FOR A PARTICULAR PURPOSE. See the GNU      |
| Lesser General Public License for more details.                       |
|                                                                       |
| You should have received a copy of the GNU Lesser General Public      |
| License along with SU2. If not, see &lt;<a href='http://www.gnu.org/licenses/'>http://www.gnu.org/licenses/</a>&gt;.   |
-------------------------------------------------------------------------

Parsing config file for zone 0

----------------- Physical Case Definition ( Zone 0 ) -------------------
Compressible Euler equations.
Mach number: 0.4.
Angle of attack (AoA): 0 deg, and angle of sideslip (AoS): 0 deg.
No restart solution, use the values at infinity (freestream).
Dimensional simulation.
The reference area is 1 m^2.
The semi-span will be computed using the max y(3D) value.
The reference length is 1 m.
Reference origin for moment evaluation is (0, 0, 0).
Surface(s) where the force coefficients are evaluated: BC_5.

Surface(s) plotted in the output file: BC_5, BC_2.
Input mesh file name: ../aflr2/aflr2_CAPS.su2

--------------- Space Numerical Integration ( Zone 0 ) ------------------
Roe (with entropy fix = 0.001) solver for the flow inviscid terms.
Standard Roe without low-dissipation function.
Second order integration in space, with slope limiter.
Venkatakrishnan slope-limiting method, with constant: 0.05.
The reference element size is: 1. 
Gradient for upwind reconstruction: inverse-distance weighted Least-Squares.
Gradient for viscous and source terms: inverse-distance weighted Least-Squares.

--------------- Time Numerical Integration  ( Zone 0 ) ------------------
Local time stepping (steady state simulation).
Euler implicit method for the flow equations.
FGMRES is used for solving the linear system.
Using a ILU(0) preconditioning.
Convergence criteria of the linear solver: 1e-06.
Max number of linear iterations: 10.
V Multigrid Cycle, with 2 multigrid levels.
Damping factor for the residual restriction: 0.75.
Damping factor for the correction prolongation: 0.75.
No CFL adaptation.
+-------------------------------------------+
|  MG Level| Presmooth|PostSmooth|CorrectSmo|
+-------------------------------------------+
|         0|         1|         0|         0|
|         1|         2|         0|         0|
|         2|         3|         0|         0|
+-------------------------------------------+
Courant-Friedrichs-Lewy number:       10

------------------ Convergence Criteria  ( Zone 0 ) ---------------------
Maximum number of solver subiterations: 10.
Begin convergence monitoring at iteration 5.
Residual minimum value: 1e-14.
Cauchy series min. value: 1e-10.
Number of Cauchy elements: 100.
Begin windowed time average at iteration 0.

-------------------- Output Information ( Zone 0 ) ----------------------
File writing frequency: 
+------------------------------------+
|                     File| Frequency|
+------------------------------------+
|                  RESTART|       250|
|              SURFACE_CSV|       250|
|                  TECPLOT|       250|
|          SURFACE_TECPLOT|       250|
+------------------------------------+
Writing the convergence history file every 1 inner iterations.
Writing the screen convergence history every 1 inner iterations.
The tabular file format is CSV (.csv).
Convergence history file name: history.
Forces breakdown file name: forces_breakdown_pyCAPS_SU2_aflr2.dat.
Surface file name: surface_flow_pyCAPS_SU2_aflr2.
Volume file name: flow_pyCAPS_SU2_aflr2.
Restart file name: restart_flow_pyCAPS_SU2_aflr2.dat.

------------- Config File Boundary Information ( Zone 0 ) ---------------
+-----------------------------------------------------------------------+
|                        Marker Type|                        Marker Name|
+-----------------------------------------------------------------------+
|                         Euler wall|                               BC_5|
|                                   |                               BC_2|
+-----------------------------------------------------------------------+
|                     Inlet boundary|                               BC_4|
+-----------------------------------------------------------------------+
|                    Outlet boundary|                               BC_3|
+-----------------------------------------------------------------------+

-------------------- Output Preprocessing ( Zone 0 ) --------------------

WARNING: SURFACE_PRESSURE_DROP can only be computed for at least 2 surfaces (outlet, inlet, ...)

Screen output fields: TIME_ITER, OUTER_ITER, INNER_ITER, CUR_TIME, TIME_STEP, WALL_TIME, RMS_DENSITY, RMS_MOMENTUM-X, RMS_MOMENTUM-Y, RMS_ENERGY, EFFICIENCY
History output group(s): ITER, TIME_DOMAIN, WALL_TIME, RMS_RES, AERO_COEFF
Convergence field(s): RMS_DENSITY
Warning: No (valid) fields chosen for time convergence monitoring. Time convergence monitoring inactive.
Volume output fields: COORDINATES, SOLUTION, PRIMITIVE

------------------- Geometry Preprocessing ( Zone 0 ) -------------------
Two dimensional problem.
3715 grid points.
7206 volume elements.
4 surface markers.
98 boundary elements in index 0 (Marker = BC_2).
24 boundary elements in index 1 (Marker = BC_3).
24 boundary elements in index 2 (Marker = BC_4).
78 boundary elements in index 3 (Marker = BC_5).
7206 triangles.
Setting point connectivity.
Renumbering points (Reverse Cuthill McKee Ordering).
Recomputing point connectivity.
Setting element connectivity.
Checking the numerical grid orientation.
There has been a re-orientation of 7206 TRIANGLE volume elements.
There has been a re-orientation of 73 LINE surface elements.
Identifying edges and vertices.
Setting the control volume structure.
Area of the computational grid: 999.917.
Searching for the closest normal neighbors to the surfaces.
Storing a mapping from global to local point index.
Compute the surface curvature.
Max K: 177.06. Mean K: 1.97231. Standard deviation K: 13.0434.
Checking for periodicity.
Computing mesh quality statistics for the dual control volumes.
+--------------------------------------------------------------+
|           Mesh Quality Metric|        Minimum|        Maximum|
+--------------------------------------------------------------+
|    Orthogonality Angle (deg.)|        63.4343|             90|
|     CV Face Area Aspect Ratio|              1|        5.23543|
|           CV Sub-Volume Ratio|              1|        3.11804|
+--------------------------------------------------------------+
Setting the multigrid structure.
+-------------------------------------------+
|  MG Level|       CVs|Aggl. Rate|       CFL|
+-------------------------------------------+
|         0|      3715|    1/1.00|        10|
|         1|      1048|    1/3.54|   7.96696|
|         2|       298|    1/3.52|   6.37252|
+-------------------------------------------+
Finding max control volume width.
Wetted area = 2.06136 m.
Area projection in the x-plane = 0.178383 m, y-plane = 0.994925 m.
Max. coordinate in the x-direction = 1 m, y-direction = 0.138389 m.
Min. coordinate in the x-direction = -0.000250564 m, y-direction = -0.0151999 m.
Checking if Euler &amp; Symmetry markers are straight/plane:
Boundary marker BC_5 is NOT a single straight.
Boundary marker BC_2 is NOT a single straight.
Computing wall distances.

-------------------- Solver Preprocessing ( Zone 0 ) --------------------
Inviscid flow: Computing density based on free-stream
temperature and pressure using the ideal gas law.
Force coefficients computed using free-stream values.

-- Models:
+------------------------------------------------------------------------------+
|          Viscosity Model|        Conductivity Model|              Fluid Model|
+------------------------------------------------------------------------------+
|                        -|                         -|             STANDARD_AIR|
+------------------------------------------------------------------------------+
-- Fluid properties:
+------------------------------------------------------------------------------+
|                  Name|    Dim. value|    Ref. value|      Unit|Non-dim. value|
+------------------------------------------------------------------------------+
|          Gas Constant|       287.058|             1|  N.m/kg.K|       287.058|
|      Spec. Heat Ratio|             -|             -|         -|           1.4|
+------------------------------------------------------------------------------+
-- Initial and free-stream conditions:
+------------------------------------------------------------------------------+
|                  Name|    Dim. value|    Ref. value|      Unit|Non-dim. value|
+------------------------------------------------------------------------------+
|       Static Pressure|        101325|             1|        Pa|        101325|
|               Density|       1.22498|             1|    kg/m^3|       1.22498|
|           Temperature|        288.15|             1|         K|        288.15|
|          Total Energy|        216054|             1|   m^2/s^2|        216054|
|            Velocity-X|       136.119|             1|       m/s|       136.119|
|            Velocity-Y|             0|             1|       m/s|             0|
|    Velocity Magnitude|       136.119|             1|       m/s|       136.119|
+------------------------------------------------------------------------------+
|           Mach Number|             -|             -|         -|           0.4|
+------------------------------------------------------------------------------+
Initialize Jacobian structure (Euler). MG level: 0.
Initialize Jacobian structure (Euler). MG level: 1.
Initialize Jacobian structure (Euler). MG level: 2.

------------------- Numerics Preprocessing ( Zone 0 ) -------------------

----------------- Integration Preprocessing ( Zone 0 ) ------------------

------------------- Iteration Preprocessing ( Zone 0 ) ------------------
Euler/Navier-Stokes/RANS fluid iteration.

------------------------------ Begin Solver -----------------------------

Simulation Run using the Single-zone Driver
WARNING: SU2 was not compiled for an AVX-capable architecture. Performance could be better,
         see <a href='https://su2code.github.io/docs_v7/Build-SU2-Linux-MacOS/#compiler-optimizations'>https://su2code.github.io/docs_v7/Build-SU2-Linux-MacOS/#compiler-optimizations</a>
WARNING: SU2 was not compiled for an AVX-capable architecture. Performance could be better,
         see <a href='https://su2code.github.io/docs_v7/Build-SU2-Linux-MacOS/#compiler-optimizations'>https://su2code.github.io/docs_v7/Build-SU2-Linux-MacOS/#compiler-optimizations</a>
WARNING: SU2 was not compiled for an AVX-capable architecture. Performance could be better,
         see <a href='https://su2code.github.io/docs_v7/Build-SU2-Linux-MacOS/#compiler-optimizations'>https://su2code.github.io/docs_v7/Build-SU2-Linux-MacOS/#compiler-optimizations</a>
+----------------------------------------------------------------------------------------------------------------------------------------------+
|   Time_Iter|  Outer_Iter|  Inner_Iter|    Cur_Time|   Time_Step|   Time(sec)|    rms[Rho]|   rms[RhoU]|   rms[RhoV]|   rms[RhoE]|        CEff|
+----------------------------------------------------------------------------------------------------------------------------------------------+
|           0|           0|           0|  0.0000e+00|  0.0000e+00|  1.9921e-02|   -0.385358|    2.453598|    1.625650|    5.369499|    0.360138|
|           0|           0|           1|  0.0000e+00|  0.0000e+00|  1.9595e-02|   -0.512634|    2.087781|    1.374671|    4.973554|    1.183036|
|           0|           0|           2|  0.0000e+00|  0.0000e+00|  1.9360e-02|   -0.792582|    1.733529|    1.142729|    4.657622|    3.896320|
|           0|           0|           3|  0.0000e+00|  0.0000e+00|  1.9236e-02|   -0.880738|    1.486539|    1.023158|    4.334759|   14.592265|
|           0|           0|           4|  0.0000e+00|  0.0000e+00|  1.9159e-02|   -0.987528|    1.351478|    0.932491|    4.191092|  111.166022|
|           0|           0|           5|  0.0000e+00|  0.0000e+00|  1.9109e-02|   -1.104038|    1.188715|    0.874764|    3.951825| -483.924340|
|           0|           0|           6|  0.0000e+00|  0.0000e+00|  1.9068e-02|   -1.178622|    1.124587|    0.844310|    3.820426|  127.331200|
|           0|           0|           7|  0.0000e+00|  0.0000e+00|  1.9035e-02|   -1.243517|    1.097463|    0.824869|    3.768858|   40.162273|
|           0|           0|           8|  0.0000e+00|  0.0000e+00|  1.9010e-02|   -1.287932|    1.075843|    0.810639|    3.733440|   25.154653|
|           0|           0|           9|  0.0000e+00|  0.0000e+00|  1.8993e-02|   -1.300689|    1.046363|    0.775886|    3.684245|   21.097801|

----------------------------- Solver Exit -------------------------------

Maximum number of iterations reached (ITER = 10) before convergence.
+-----------------------------------------------------------------------+
|      Convergence Field     |     Value    |   Criterion  |  Converged |
+-----------------------------------------------------------------------+
|                    rms[Rho]|      -1.30069|         &lt; -14|          No|
+-----------------------------------------------------------------------+
-------------------------------------------------------------------------
+-----------------------------------------------------------------------+
|        File Writing Summary       |              Filename             |
+-----------------------------------------------------------------------+
|SU2 binary restart                 |restart_flow_pyCAPS_SU2_aflr2.dat  |

Writing the forces breakdown file (forces_breakdown_pyCAPS_SU2_aflr2.dat).
|CSV file                           |surface_flow_pyCAPS_SU2_aflr2.csv  |

Writing the forces breakdown file (forces_breakdown_pyCAPS_SU2_aflr2.dat).
|Tecplot binary                     |flow_pyCAPS_SU2_aflr2.szplt        |

Writing the forces breakdown file (forces_breakdown_pyCAPS_SU2_aflr2.dat).
|Tecplot binary surface             |surface_flow_pyCAPS_SU2_aflr2.szplt|
Error in tecFileWriterClose: Not all node map values for zone 1 have been written.
Currently need 352 more values.0: Error finishing Tecplot file output.

Writing the forces breakdown file (forces_breakdown_pyCAPS_SU2_aflr2.dat).
+-----------------------------------------------------------------------+

--------------------------- Finalizing Solver ---------------------------
Deleted CNumerics container.
Deleted CIntegration container.
Deleted CSolver container.
Deleted CIteration container.
Deleted CInterface container.
Deleted CGeometry container.
Deleted CFreeFormDefBox class.
Deleted CSurfaceMovement class.
Deleted CVolumetricMovement class.
Deleted CConfig container.
Deleted nInst container.
Deleted COutput class.
-------------------------------------------------------------------------

------------------------- Exit Success (SU2_CFD) ------------------------

Total Force - Pressure + Viscous
Cl =  0.650457 Cd =  0.030831
Cmz =  0.373226
Cx =  0.030831 Cy =  0.650457
Pressure Contribution
Cl_p =  0.650457 Cd_p =  0.030831
Cmz_p =  0.373226
Cx_p =  0.030831 Cy_p =  0.650457
Viscous Contribution
Cl_v =  0.0 Cd_v =  0.0
Cmz_v =  0.0
Cx_v =  0.0 Cy_v =  0.0

real	0m0.970s
user	0m0.930s
sys	0m0.399s
+ status=0
+ set +x

=================================================
CAPS verification (using pyCAPS) case su2_and_AFLR2_NodeDist_PyTest.py passed (as expected)
=================================================


=================================================
+ echo 'su2_and_AFLR2_PyTest.py test;'
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESP126/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
su2_and_AFLR2_PyTest.py test;
+ python -u su2_and_AFLR2_PyTest.py -outLevel=0
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESP126/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
Saving geometry
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 5
	Name = 2DSlice, index = 1
	Name = TunnelWall, index = 2
	Name = OutFlow, index = 3
	Name = InFlow, index = 4
	Name = Airfoil, index = 5
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 4
	Name = TunnelWall, index = 1
	Name = OutFlow, index = 2
	Name = InFlow, index = 3
	Name = Airfoil, index = 4

Getting mesh sizing parameters
	Mesh sizing name - 2DSlice
	Mesh sizing name - Airfoil
	Mesh sizing name - InFlow
	Mesh sizing name - OutFlow
	Mesh sizing name - TunnelWall
	Done getting mesh sizing parameters
Getting 2D mesh for body 1 (of 1)
 
AFLR2    : ---------------------------------------
AFLR2    : AFLR2 LIBRARY
AFLR2    : ADVANCING-FRONT/LOCAL-RECONNECTION
AFLR2    : TRIA/QUAD GRID GENERATOR
AFLR2    : Version Number 9.18.1
AFLR2    : Version Date   06/11/24 @ 05:52PM
AFLR2    : Compile OS     Darwin 23.5.0 arm64
AFLR2    : Compile Date   06/11/24 @ 05:52PM
AFLR2    : Copyright 1994-2021, D.L. Marcum
AFLR2    : ---------------------------------------
 
AFLR2 IC : INPUT DATA CHECK
 
AFLR2 IC : Nodes, Faces      =       545         0
 
AFLR2    : CPU Time          =     0.000   seconds
 
AFLR2 EG : EDGE GRID RE-GENERATION
 
AFLR2 EG : Nodes, Edges      =       545       545
 
AFLR2    : CPU Time          =     0.000   seconds
 
AFLR2 IG : INITIAL GRID GENERATION
 
AFLR2 IG : Nodes, Faces      =         0         2
AFLR2 IG : Nodes, Faces      =       110       222
AFLR2 IG : Nodes, Faces      =       220       442
AFLR2 IG : Nodes, Faces      =       330       662
AFLR2 IG : Nodes, Faces      =       440       882
AFLR2 IG : Nodes, Faces      =       517      1036
AFLR2 IG : Nodes, Faces      =       545      1092
AFLR2 IG : Nodes, Faces      =       549      1092
AFLR2 IG : Nodes, Faces      =       545       545
 
AFLR2    : CPU Time          =     0.001   seconds
 
AFLR2 GG : FIELD GRID GENERATION
 
AFLR2 GGp: Nodes, Faces      =       545       545
AFLR2 GGp: Nodes, Faces      =      1083      1621
AFLR2 GGp: Nodes, Faces      =      1616      2687
AFLR2 GGp: Nodes, Faces      =      2144      3743
AFLR2 GGp: Nodes, Faces      =      2661      4777
AFLR2 GGp: Nodes, Faces      =      3171      5797
AFLR2 GGp: Nodes, Faces      =      3672      6799
AFLR2 GGp: Nodes, Faces      =      4158      7771
AFLR2 GGp: Nodes, Faces      =      4653      8761
AFLR2 GGp: Nodes, Faces      =      5142      9739
AFLR2 GGp: Nodes, Faces      =      5608     10671
AFLR2 GGp: Nodes, Faces      =      6055     11565
AFLR2 GGp: Nodes, Faces      =      6482     12419
AFLR2 GGp: Nodes, Faces      =      6880     13215
AFLR2 GGp: Nodes, Faces      =      7257     13969
AFLR2 GGp: Nodes, Faces      =      7614     14683
AFLR2 GGp: Nodes, Faces      =      7947     15349
AFLR2 GGp: Nodes, Faces      =      8276     16007
AFLR2 GGp: Nodes, Faces      =      8575     16605
AFLR2 GGp: Nodes, Faces      =      8869     17193
AFLR2 GGp: Nodes, Faces      =      9140     17735
AFLR2 GGp: Nodes, Faces      =      9401     18257
AFLR2 GGp: Nodes, Faces      =      9654     18763
AFLR2 GGp: Nodes, Faces      =      9887     19229
AFLR2 GGp: Nodes, Faces      =     10110     19675
AFLR2 GGp: Nodes, Faces      =     10315     20085
AFLR2 GGp: Nodes, Faces      =     10497     20449
AFLR2 GGp: Nodes, Faces      =     10656     20767
AFLR2 GGp: Nodes, Faces      =     10791     21037
AFLR2 GGp: Nodes, Faces      =     10919     21293
AFLR2 GGp: Nodes, Faces      =     11022     21499
AFLR2 GGp: Nodes, Faces      =     11092     21639
AFLR2 GGp: Nodes, Faces      =     11145     21745
AFLR2 GGp: Nodes, Faces      =     11156     21767
 
AFLR2    : CPU Time          =     0.021   seconds
 
AFLR2 QI : QUALITY IMPROVEMENT
 
AFLR2 QI : Nodes, Faces      =     11156     21767
AFLR2 QI : Nodes, Faces      =     11155       819
AFLR2 QI : Nodes, Faces      =     11155     10473
AFLR2 QI : Nodes, Faces      =     11155     21765
AFLR2 QI : Nodes, Faces      =     11154       811
AFLR2 QI : Nodes, Faces      =     11154     10476
AFLR2 QI : Nodes, Faces      =     11154     21763
AFLR2 QI : Nodes, Faces      =     11154       805
AFLR2 QI : Nodes, Faces      =     11154     10479
AFLR2 QI : Nodes, Faces      =     11154     21763
AFLR2 QI : Nodes, Faces      =     11154       911
AFLR2 QI : Nodes, Faces      =     11154     10426
AFLR2 QI : Nodes, Faces      =     11154     21763
AFLR2 QI : Nodes, Faces      =     11153       915
AFLR2 QI : Nodes, Faces      =     11153     10423
AFLR2 QI : Nodes, Faces      =     11153       917
AFLR2 QI : Nodes, Faces      =     11153     10423
 
AFLR2    : CPU Time          =     0.008   seconds
 
AFLR2    : DONE
EGADS Internal: Face 1, Side 11077 11153 complete [but 18248] (EG_makeConnect)!
EGADS Internal: Face 1, Side 10985 11077 complete [but 18248] (EG_makeConnect)!
EGADS Internal: Face 1, Side 10985 11152 complete [but 18249] (EG_makeConnect)!
EGADS Internal: Face 1, Side 11152 11153 complete [but 19022] (EG_makeConnect)!

Writing AFLR3 file ....
Finished writing AFLR3 file

Number of nodes = 11153
Number of elements = 11885
Number of tris = 917
Number of quad = 10423
EGADS Internal: Face 1, Side 11077 11153 complete [but 18248] (EG_makeConnect)!
EGADS Internal: Face 1, Side 10985 11077 complete [but 18248] (EG_makeConnect)!
EGADS Internal: Face 1, Side 10985 11152 complete [but 18249] (EG_makeConnect)!
EGADS Internal: Face 1, Side 11152 11153 complete [but 19022] (EG_makeConnect)!
EGADS Internal: Face 1, Side 11077 11153 complete [but 18248] (EG_makeConnect)!
EGADS Internal: Face 1, Side 10985 11077 complete [but 18248] (EG_makeConnect)!
EGADS Internal: Face 1, Side 10985 11152 complete [but 18249] (EG_makeConnect)!
EGADS Internal: Face 1, Side 11152 11153 complete [but 19022] (EG_makeConnect)!

Writing Tecplot file ....
Tecplot expects 2D meshes in the x-y plane... attempting to rotate mesh!
Swapping z and y coordinates!
Finished writing Tecplot file


Writing SU2 file ....
SU2 expects 2D meshes in the x-y plane... attempting to rotate mesh!
Swapping z and y coordinates!
Finished writing SU2 file

Getting CFD boundary conditions
	Boundary condition name - Airfoil
	Boundary condition name - InFlow
	Boundary condition name - OutFlow
	Boundary condition name - TunnelWall
	Done getting CFD boundary conditions
Warning: The su2 cfg file will be overwritten!
Write SU2 configuration file for version "Harrier (8.0.1)"


Running SU2......

-------------------------------------------------------------------------
|    ___ _   _ ___                                                      |
|   / __| | | |_  )   Release 8.0.0 "Harrier"                           |
|   \__ \ |_| |/ /                                                      |
|   |___/\___//___|   Suite (Computational Fluid Dynamics Code)         |
|                                                                       |
-------------------------------------------------------------------------
| SU2 Project Website: <a href='https://su2code.github.io'>https://su2code.github.io</a>                        |
|                                                                       |
| The SU2 Project is maintained by the SU2 Foundation                   |
| (<a href='http://su2foundation.org'>http://su2foundation.org</a>)                                            |
-------------------------------------------------------------------------
| Copyright 2012-2023, SU2 Contributors                                 |
|                                                                       |
| SU2 is free software; you can redistribute it and/or                  |
| modify it under the terms of the GNU Lesser General Public            |
| License as published by the Free Software Foundation; either          |
| version 2.1 of the License, or (at your option) any later version.    |
|                                                                       |
| SU2 is distributed in the hope that it will be useful,                |
| but WITHOUT ANY WARRANTY; without even the implied warranty of        |
| MERCHANTABILITY or FITNESS FOR A PARTICULAR PURPOSE. See the GNU      |
| Lesser General Public License for more details.                       |
|                                                                       |
| You should have received a copy of the GNU Lesser General Public      |
| License along with SU2. If not, see &lt;<a href='http://www.gnu.org/licenses/'>http://www.gnu.org/licenses/</a>&gt;.   |
-------------------------------------------------------------------------

Parsing config file for zone 0

----------------- Physical Case Definition ( Zone 0 ) -------------------
Compressible Euler equations.
Mach number: 0.4.
Angle of attack (AoA): 0 deg, and angle of sideslip (AoS): 0 deg.
No restart solution, use the values at infinity (freestream).
Dimensional simulation.
The reference area is 1 m^2.
The semi-span will be computed using the max y(3D) value.
The reference length is 1 m.
Reference origin for moment evaluation is (0, 0, 0).
Surface(s) where the force coefficients are evaluated: BC_5.

Surface(s) plotted in the output file: BC_5, BC_2.
Input mesh file name: ../aflr2/aflr2_CAPS.su2

--------------- Space Numerical Integration ( Zone 0 ) ------------------
Roe (with entropy fix = 0.001) solver for the flow inviscid terms.
Standard Roe without low-dissipation function.
Second order integration in space, with slope limiter.
Venkatakrishnan slope-limiting method, with constant: 0.05.
The reference element size is: 1. 
Gradient for upwind reconstruction: inverse-distance weighted Least-Squares.
Gradient for viscous and source terms: inverse-distance weighted Least-Squares.

--------------- Time Numerical Integration  ( Zone 0 ) ------------------
Local time stepping (steady state simulation).
Euler implicit method for the flow equations.
FGMRES is used for solving the linear system.
Using a ILU(0) preconditioning.
Convergence criteria of the linear solver: 1e-06.
Max number of linear iterations: 10.
V Multigrid Cycle, with 2 multigrid levels.
Damping factor for the residual restriction: 0.75.
Damping factor for the correction prolongation: 0.75.
No CFL adaptation.
+-------------------------------------------+
|  MG Level| Presmooth|PostSmooth|CorrectSmo|
+-------------------------------------------+
|         0|         1|         0|         0|
|         1|         2|         0|         0|
|         2|         3|         0|         0|
+-------------------------------------------+
Courant-Friedrichs-Lewy number:       10

------------------ Convergence Criteria  ( Zone 0 ) ---------------------
Maximum number of solver subiterations: 10.
Begin convergence monitoring at iteration 5.
Residual minimum value: 1e-14.
Cauchy series min. value: 1e-10.
Number of Cauchy elements: 100.
Begin windowed time average at iteration 0.

-------------------- Output Information ( Zone 0 ) ----------------------
File writing frequency: 
+------------------------------------+
|                     File| Frequency|
+------------------------------------+
|                  RESTART|       250|
|              SURFACE_CSV|       250|
|                  TECPLOT|       250|
|          SURFACE_TECPLOT|       250|
+------------------------------------+
Writing the convergence history file every 1 inner iterations.
Writing the screen convergence history every 1 inner iterations.
The tabular file format is CSV (.csv).
Convergence history file name: history.
Forces breakdown file name: forces_breakdown_pyCAPS_su2_aflr2.dat.
Surface file name: surface_flow_pyCAPS_su2_aflr2.
Volume file name: flow_pyCAPS_su2_aflr2.
Restart file name: restart_flow_pyCAPS_su2_aflr2.dat.

------------- Config File Boundary Information ( Zone 0 ) ---------------
+-----------------------------------------------------------------------+
|                        Marker Type|                        Marker Name|
+-----------------------------------------------------------------------+
|                         Euler wall|                               BC_5|
|                                   |                               BC_2|
+-----------------------------------------------------------------------+
|                     Inlet boundary|                               BC_4|
+-----------------------------------------------------------------------+
|                    Outlet boundary|                               BC_3|
+-----------------------------------------------------------------------+

-------------------- Output Preprocessing ( Zone 0 ) --------------------

WARNING: SURFACE_PRESSURE_DROP can only be computed for at least 2 surfaces (outlet, inlet, ...)

Screen output fields: TIME_ITER, OUTER_ITER, INNER_ITER, CUR_TIME, TIME_STEP, WALL_TIME, RMS_DENSITY, RMS_MOMENTUM-X, RMS_MOMENTUM-Y, RMS_ENERGY, EFFICIENCY
History output group(s): ITER, TIME_DOMAIN, WALL_TIME, RMS_RES, AERO_COEFF
Convergence field(s): RMS_DENSITY
Warning: No (valid) fields chosen for time convergence monitoring. Time convergence monitoring inactive.
Volume output fields: COORDINATES, SOLUTION, PRIMITIVE

------------------- Geometry Preprocessing ( Zone 0 ) -------------------
Two dimensional problem.
11153 grid points.
11340 volume elements.
4 surface markers.
98 boundary elements in index 0 (Marker = BC_2).
24 boundary elements in index 1 (Marker = BC_3).
24 boundary elements in index 2 (Marker = BC_4).
399 boundary elements in index 3 (Marker = BC_5).
917 triangles.
10423 quadrilaterals.
Setting point connectivity.
Renumbering points (Reverse Cuthill McKee Ordering).
Recomputing point connectivity.
Setting element connectivity.
Checking the numerical grid orientation.
There has been a re-orientation of 917 TRIANGLE volume elements.
There has been a re-orientation of 10423 QUADRILATERAL volume elements.
There has been a re-orientation of 73 LINE surface elements.
Identifying edges and vertices.
Setting the control volume structure.
Area of the computational grid: 999.878.
Searching for the closest normal neighbors to the surfaces.
Storing a mapping from global to local point index.
Compute the surface curvature.
Max K: 385.665. Mean K: 2.15881. Standard deviation K: 17.7215.
Checking for periodicity.
Computing mesh quality statistics for the dual control volumes.
+--------------------------------------------------------------+
|           Mesh Quality Metric|        Minimum|        Maximum|
+--------------------------------------------------------------+
|    Orthogonality Angle (deg.)|        49.3184|             90|
|     CV Face Area Aspect Ratio|        1.00035|        33.4982|
|           CV Sub-Volume Ratio|        1.00001|        7.89914|
+--------------------------------------------------------------+
Setting the multigrid structure.
+-------------------------------------------+
|  MG Level|       CVs|Aggl. Rate|       CFL|
+-------------------------------------------+
|         0|     11153|    1/1.00|        10|
|         1|      2702|    1/4.13|   7.38309|
|         2|       549|    1/4.92|   4.99198|
+-------------------------------------------+
Finding max control volume width.
Wetted area = 2.06265 m.
Area projection in the x-plane = 0.211192 m, y-plane = 0.997011 m.
Max. coordinate in the x-direction = 1 m, y-direction = 0.102037 m.
Min. coordinate in the x-direction = 0.000323229 m, y-direction = -0.108492 m.
Checking if Euler &amp; Symmetry markers are straight/plane:
Boundary marker BC_5 is NOT a single straight.
Boundary marker BC_2 is NOT a single straight.
Computing wall distances.

-------------------- Solver Preprocessing ( Zone 0 ) --------------------
Inviscid flow: Computing density based on free-stream
temperature and pressure using the ideal gas law.
Force coefficients computed using free-stream values.

-- Models:
+------------------------------------------------------------------------------+
|          Viscosity Model|        Conductivity Model|              Fluid Model|
+------------------------------------------------------------------------------+
|                        -|                         -|             STANDARD_AIR|
+------------------------------------------------------------------------------+
-- Fluid properties:
+------------------------------------------------------------------------------+
|                  Name|    Dim. value|    Ref. value|      Unit|Non-dim. value|
+------------------------------------------------------------------------------+
|          Gas Constant|       287.058|             1|  N.m/kg.K|       287.058|
|      Spec. Heat Ratio|             -|             -|         -|           1.4|
+------------------------------------------------------------------------------+
-- Initial and free-stream conditions:
+------------------------------------------------------------------------------+
|                  Name|    Dim. value|    Ref. value|      Unit|Non-dim. value|
+------------------------------------------------------------------------------+
|       Static Pressure|        101325|             1|        Pa|        101325|
|               Density|       1.22498|             1|    kg/m^3|       1.22498|
|           Temperature|        288.15|             1|         K|        288.15|
|          Total Energy|        216054|             1|   m^2/s^2|        216054|
|            Velocity-X|       136.119|             1|       m/s|       136.119|
|            Velocity-Y|             0|             1|       m/s|             0|
|    Velocity Magnitude|       136.119|             1|       m/s|       136.119|
+------------------------------------------------------------------------------+
|           Mach Number|             -|             -|         -|           0.4|
+------------------------------------------------------------------------------+
Initialize Jacobian structure (Euler). MG level: 0.
Initialize Jacobian structure (Euler). MG level: 1.
Initialize Jacobian structure (Euler). MG level: 2.

------------------- Numerics Preprocessing ( Zone 0 ) -------------------

----------------- Integration Preprocessing ( Zone 0 ) ------------------

------------------- Iteration Preprocessing ( Zone 0 ) ------------------
Euler/Navier-Stokes/RANS fluid iteration.

------------------------------ Begin Solver -----------------------------

Simulation Run using the Single-zone Driver
WARNING: SU2 was not compiled for an AVX-capable architecture. Performance could be better,
         see <a href='https://su2code.github.io/docs_v7/Build-SU2-Linux-MacOS/#compiler-optimizations'>https://su2code.github.io/docs_v7/Build-SU2-Linux-MacOS/#compiler-optimizations</a>
WARNING: SU2 was not compiled for an AVX-capable architecture. Performance could be better,
         see <a href='https://su2code.github.io/docs_v7/Build-SU2-Linux-MacOS/#compiler-optimizations'>https://su2code.github.io/docs_v7/Build-SU2-Linux-MacOS/#compiler-optimizations</a>
WARNING: SU2 was not compiled for an AVX-capable architecture. Performance could be better,
         see <a href='https://su2code.github.io/docs_v7/Build-SU2-Linux-MacOS/#compiler-optimizations'>https://su2code.github.io/docs_v7/Build-SU2-Linux-MacOS/#compiler-optimizations</a>
+----------------------------------------------------------------------------------------------------------------------------------------------+
|   Time_Iter|  Outer_Iter|  Inner_Iter|    Cur_Time|   Time_Step|   Time(sec)|    rms[Rho]|   rms[RhoU]|   rms[RhoV]|   rms[RhoE]|        CEff|
+----------------------------------------------------------------------------------------------------------------------------------------------+
|           0|           0|           0|  0.0000e+00|  0.0000e+00|  5.1371e-02|    0.071067|    2.739763|    1.616077|    5.599701|    0.055267|
|           0|           0|           1|  0.0000e+00|  0.0000e+00|  4.9765e-02|   -0.447576|    2.193837|    1.571349|    5.070382|    0.046028|
|           0|           0|           2|  0.0000e+00|  0.0000e+00|  4.9125e-02|   -0.561159|    2.074597|    1.490746|    4.953698|    0.033910|
|           0|           0|           3|  0.0000e+00|  0.0000e+00|  4.8755e-02|   -0.723326|    1.921155|    1.390756|    4.790278|    0.049695|
|           0|           0|           4|  0.0000e+00|  0.0000e+00|  4.8679e-02|   -0.876572|    1.825653|    1.275093|    4.637161|    0.133976|
|           0|           0|           5|  0.0000e+00|  0.0000e+00|  4.8564e-02|   -1.029177|    1.759196|    1.156078|    4.482282|    0.368542|
|           0|           0|           6|  0.0000e+00|  0.0000e+00|  4.8424e-02|   -1.215334|    1.704909|    1.114966|    4.286060|    0.974759|
|           0|           0|           7|  0.0000e+00|  0.0000e+00|  4.8364e-02|   -1.329970|    1.644937|    1.145030|    4.116982|    2.716332|
|           0|           0|           8|  0.0000e+00|  0.0000e+00|  4.8290e-02|   -1.270672|    1.570739|    1.155400|    4.139480|   16.569216|
|           0|           0|           9|  0.0000e+00|  0.0000e+00|  4.8223e-02|   -1.221243|    1.499646|    1.130319|    4.189559|   -6.277653|

----------------------------- Solver Exit -------------------------------

Maximum number of iterations reached (ITER = 10) before convergence.
+-----------------------------------------------------------------------+
|      Convergence Field     |     Value    |   Criterion  |  Converged |
+-----------------------------------------------------------------------+
|                    rms[Rho]|      -1.22124|         &lt; -14|          No|
+-----------------------------------------------------------------------+
-------------------------------------------------------------------------
+-----------------------------------------------------------------------+
|        File Writing Summary       |              Filename             |
+-----------------------------------------------------------------------+
|SU2 binary restart                 |restart_flow_pyCAPS_su2_aflr2.dat  |

Writing the forces breakdown file (forces_breakdown_pyCAPS_su2_aflr2.dat).
|CSV file                           |surface_flow_pyCAPS_su2_aflr2.csv  |

Writing the forces breakdown file (forces_breakdown_pyCAPS_su2_aflr2.dat).
|Tecplot binary                     |flow_pyCAPS_su2_aflr2.szplt        |

Writing the forces breakdown file (forces_breakdown_pyCAPS_su2_aflr2.dat).
|Tecplot binary surface             |surface_flow_pyCAPS_su2_aflr2.szplt|
Error in tecFileWriterClose: Not all node map values for zone 1 have been written.
Currently need 994 more values.0: Error finishing Tecplot file output.

Writing the forces breakdown file (forces_breakdown_pyCAPS_su2_aflr2.dat).
+-----------------------------------------------------------------------+

--------------------------- Finalizing Solver ---------------------------
Deleted CNumerics container.
Deleted CIntegration container.
Deleted CSolver container.
Deleted CIteration container.
Deleted CInterface container.
Deleted CGeometry container.
Deleted CFreeFormDefBox class.
Deleted CSurfaceMovement class.
Deleted CVolumetricMovement class.
Deleted CConfig container.
Deleted nInst container.
Deleted COutput class.
-------------------------------------------------------------------------

------------------------- Exit Success (SU2_CFD) ------------------------

Total Force - Pressure + Viscous
Cl =  0.072253 Cd =  -0.01151
Cmz =  0.070975
Cx =  -0.01151 Cy =  0.072253
Pressure Contribution
Cl_p =  0.072253 Cd_p =  -0.01151
Cmz_p =  0.070975
Cx_p =  -0.01151 Cy_p =  0.072253
Viscous Contribution
Cl_v =  0.0 Cd_v =  0.0
Cmz_v =  0.0
Cx_v =  0.0 Cy_v =  0.0

real	0m1.374s
user	0m1.472s
sys	0m0.638s
+ status=0
+ set +x

=================================================
CAPS verification (using pyCAPS) case su2_and_AFLR2_PyTest.py passed (as expected)
=================================================


=================================================
+ echo 'su2_and_AFLR4_AFLR3_PyTest.py test;'
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESP126/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
su2_and_AFLR4_AFLR3_PyTest.py test;
+ python -u su2_and_AFLR4_AFLR3_PyTest.py -outLevel=0
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESP126/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 4
	Name = Wing1, index = 1
	Name = Wing2, index = 2
	Name = Wake, index = 3
	Name = Farfield, index = 4
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 4
	Name = Wing1, index = 1
	Name = Wing2, index = 2
	Name = Wake, index = 3
	Name = Farfield, index = 4
AFLR4    : Proximity BG Surface Grid Generation Skipped
AFLR4    : No Modifications Required

Writing Tecplot file ....
Finished writing Tecplot file

Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 4
	Name = Wing1, index = 1
	Name = Wing2, index = 2
	Name = Wake, index = 3
	Name = Farfield, index = 4
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 4
	Name = Wing1, index = 1
	Name = Wing2, index = 2
	Name = Wake, index = 3
	Name = Farfield, index = 4
Getting volume mesh
 
AFLR2    : ---------------------------------------
AFLR2    : AFLR2 LIBRARY
AFLR2    : ADVANCING-FRONT/LOCAL-RECONNECTION
AFLR2    : TRIA/QUAD GRID GENERATOR
AFLR2    : Version Number 9.18.1
AFLR2    : Version Date   06/11/24 @ 05:52PM
AFLR2    : Compile OS     Darwin 23.5.0 arm64
AFLR2    : Compile Date   06/11/24 @ 05:52PM
AFLR2    : Copyright 1994-2021, D.L. Marcum
AFLR2    : ---------------------------------------
 
AFLR4    : ---------------------------------------
AFLR4    : AFLR4 LIBRARY
AFLR4    : ADVANCING-FRONT/LOCAL-RECONNECTION
AFLR4    : TRIA/QUAD SURFACE GRID GENERATOR
AFLR4    : Version Number 11.5.15
AFLR4    : Version Date   07/19/24 @ 07:04PM
AFLR4    : Compile OS     Darwin 23.5.0 arm64
AFLR4    : Compile Date   07/19/24 @ 07:06PM
AFLR4    : Copyright 1994-2021, D.L. Marcum
AFLR4    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.8.1
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.8.1
EGADS    : ---------------------------------------
Volume mesh:
	Number of nodes          = 38294
	Number of elements       = 220670
	Number of triangles      = 12448
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 208222
	Number of pyramids       = 0
	Number of prisms         = 0
	Number of hexahedrals    = 0

Writing Tecplot file ....
Finished writing Tecplot file


Writing SU2 file ....
Finished writing SU2 file

Getting CFD boundary conditions
	Boundary condition name - Farfield
	Boundary condition name - Wake
	Boundary condition name - Wing1
	Boundary condition name - Wing2
	Done getting CFD boundary conditions
Warning: The su2 cfg file will be overwritten!
Write SU2 configuration file for version "Harrier (8.0.1)"


Running SU2......

-------------------------------------------------------------------------
|    ___ _   _ ___                                                      |
|   / __| | | |_  )   Release 8.0.0 "Harrier"                           |
|   \__ \ |_| |/ /                                                      |
|   |___/\___//___|   Suite (Computational Fluid Dynamics Code)         |
|                                                                       |
-------------------------------------------------------------------------
| SU2 Project Website: <a href='https://su2code.github.io'>https://su2code.github.io</a>                        |
|                                                                       |
| The SU2 Project is maintained by the SU2 Foundation                   |
| (<a href='http://su2foundation.org'>http://su2foundation.org</a>)                                            |
-------------------------------------------------------------------------
| Copyright 2012-2023, SU2 Contributors                                 |
|                                                                       |
| SU2 is free software; you can redistribute it and/or                  |
| modify it under the terms of the GNU Lesser General Public            |
| License as published by the Free Software Foundation; either          |
| version 2.1 of the License, or (at your option) any later version.    |
|                                                                       |
| SU2 is distributed in the hope that it will be useful,                |
| but WITHOUT ANY WARRANTY; without even the implied warranty of        |
| MERCHANTABILITY or FITNESS FOR A PARTICULAR PURPOSE. See the GNU      |
| Lesser General Public License for more details.                       |
|                                                                       |
| You should have received a copy of the GNU Lesser General Public      |
| License along with SU2. If not, see &lt;<a href='http://www.gnu.org/licenses/'>http://www.gnu.org/licenses/</a>&gt;.   |
-------------------------------------------------------------------------

Parsing config file for zone 0

----------------- Physical Case Definition ( Zone 0 ) -------------------
Compressible Euler equations.
Mach number: 0.5901.
Angle of attack (AoA): 1 deg, and angle of sideslip (AoS): 0 deg.
No restart solution, use the values at infinity (freestream).
Dimensional simulation.
The reference area is 50 m^2.
The semi-span will be computed using the max y(3D) value.
The reference length is 15.8114 m.
Surface(s) where the force coefficients are evaluated and 
their reference origin for moment computation: 
   - BC_1 (0, 0, 0).
   - BC_2 (0, 0, 0) m.
Surface(s) plotted in the output file: BC_1, BC_2.
Input mesh file name: ../aflr3/aflr3_CAPS.su2

--------------- Space Numerical Integration ( Zone 0 ) ------------------
Roe (with entropy fix = 0.001) solver for the flow inviscid terms.
Standard Roe without low-dissipation function.
Second order integration in space, with slope limiter.
Venkatakrishnan slope-limiting method, with constant: 0.05.
The reference element size is: 1. 
Gradient for upwind reconstruction: inverse-distance weighted Least-Squares.
Gradient for viscous and source terms: inverse-distance weighted Least-Squares.

--------------- Time Numerical Integration  ( Zone 0 ) ------------------
Local time stepping (steady state simulation).
Euler implicit method for the flow equations.
FGMRES is used for solving the linear system.
Using a ILU(0) preconditioning.
Convergence criteria of the linear solver: 1e-06.
Max number of linear iterations: 10.
V Multigrid Cycle, with 2 multigrid levels.
Damping factor for the residual restriction: 0.75.
Damping factor for the correction prolongation: 0.75.
No CFL adaptation.
+-------------------------------------------+
|  MG Level| Presmooth|PostSmooth|CorrectSmo|
+-------------------------------------------+
|         0|         1|         0|         0|
|         1|         2|         0|         0|
|         2|         3|         0|         0|
+-------------------------------------------+
Courant-Friedrichs-Lewy number:       10

------------------ Convergence Criteria  ( Zone 0 ) ---------------------
Maximum number of solver subiterations: 10.
Begin convergence monitoring at iteration 5.
Residual minimum value: 1e-8.
Cauchy series min. value: 1e-10.
Number of Cauchy elements: 100.
Begin windowed time average at iteration 0.

-------------------- Output Information ( Zone 0 ) ----------------------
File writing frequency: 
+------------------------------------+
|                     File| Frequency|
+------------------------------------+
|                  RESTART|       250|
|              SURFACE_CSV|       250|
|                 PARAVIEW|       250|
|         SURFACE_PARAVIEW|       250|
+------------------------------------+
Writing the convergence history file every 1 inner iterations.
Writing the screen convergence history every 1 inner iterations.
The tabular file format is CSV (.csv).
Convergence history file name: history.
Forces breakdown file name: forces_breakdown_su2AFLRTest.dat.
Surface file name: surface_flow_su2AFLRTest.
Volume file name: flow_su2AFLRTest.
Restart file name: restart_flow_su2AFLRTest.dat.

------------- Config File Boundary Information ( Zone 0 ) ---------------
+-----------------------------------------------------------------------+
|                        Marker Type|                        Marker Name|
+-----------------------------------------------------------------------+
|                         Euler wall|                               BC_1|
|                                   |                               BC_2|
+-----------------------------------------------------------------------+
|                          Far-field|                               BC_4|
+-----------------------------------------------------------------------+
|                  Internal boundary|                               BC_3|
+-----------------------------------------------------------------------+

-------------------- Output Preprocessing ( Zone 0 ) --------------------

WARNING: SURFACE_PRESSURE_DROP can only be computed for at least 2 surfaces (outlet, inlet, ...)

Screen output fields: TIME_ITER, OUTER_ITER, INNER_ITER, CUR_TIME, TIME_STEP, WALL_TIME, RMS_DENSITY, RMS_MOMENTUM-X, RMS_MOMENTUM-Y, RMS_ENERGY, EFFICIENCY
History output group(s): ITER, TIME_DOMAIN, WALL_TIME, RMS_RES, AERO_COEFF
Convergence field(s): RMS_DENSITY
Warning: No (valid) fields chosen for time convergence monitoring. Time convergence monitoring inactive.
Volume output fields: COORDINATES, SOLUTION, PRIMITIVE

------------------- Geometry Preprocessing ( Zone 0 ) -------------------
Three dimensional problem.
38294 grid points.
208222 volume elements.
4 surface markers.
6596 boundary elements in index 0 (Marker = BC_1).
5358 boundary elements in index 1 (Marker = BC_2).
74 boundary elements in index 2 (Marker = BC_3).
420 boundary elements in index 3 (Marker = BC_4).
208222 tetrahedra.
Setting point connectivity.
Renumbering points (Reverse Cuthill McKee Ordering).
Recomputing point connectivity.
Setting element connectivity.
Checking the numerical grid orientation.
All volume elements are correctly orientend.
All surface elements are correctly orientend.
Identifying edges and vertices.
Setting the control volume structure.
Volume of the computational grid: 2.08667e+06.
Searching for the closest normal neighbors to the surfaces.
Storing a mapping from global to local point index.
Compute the surface curvature.
Max K: 4873.1. Mean K: 61.8586. Standard deviation K: 266.922.
Checking for periodicity.
Computing mesh quality statistics for the dual control volumes.
+--------------------------------------------------------------+
|           Mesh Quality Metric|        Minimum|        Maximum|
+--------------------------------------------------------------+
|    Orthogonality Angle (deg.)|        17.2334|        86.3276|
|     CV Face Area Aspect Ratio|        1.07899|          19318|
|           CV Sub-Volume Ratio|        1.06845|         686951|
+--------------------------------------------------------------+
Setting the multigrid structure.
+-------------------------------------------+
|  MG Level|       CVs|Aggl. Rate|       CFL|
+-------------------------------------------+
|         0|     38294|    1/1.00|        10|
|         1|      6362|    1/6.02|   8.24604|
|         2|      1011|    1/6.29|   6.69971|
+-------------------------------------------+
Finding max control volume width.
Semi-span length = 7.90569 m.
Wetted area = 118.038 m^2.
Area projection in the x-plane = 11.1427 m^2, y-plane = 4.96714 m^2, z-plane = 55.4173 m^2.
Max. coordinate in the x-direction = 12.6407 m, y-direction = 7.90569 m, z-direction = 0.582636 m.
Min. coordinate in the x-direction = 0 m, y-direction = -7.90569 m, z-direction = -0.41192 m.
Checking if Euler &amp; Symmetry markers are straight/plane:
Boundary marker BC_1 is NOT a single plane.
Boundary marker BC_2 is NOT a single plane.
Computing wall distances.

-------------------- Solver Preprocessing ( Zone 0 ) --------------------
Inviscid flow: Computing density based on free-stream
temperature and pressure using the ideal gas law.
Force coefficients computed using free-stream values.

-- Models:
+------------------------------------------------------------------------------+
|          Viscosity Model|        Conductivity Model|              Fluid Model|
+------------------------------------------------------------------------------+
|                        -|                         -|             STANDARD_AIR|
+------------------------------------------------------------------------------+
-- Fluid properties:
+------------------------------------------------------------------------------+
|                  Name|    Dim. value|    Ref. value|      Unit|Non-dim. value|
+------------------------------------------------------------------------------+
|          Gas Constant|       287.058|             1|  N.m/kg.K|       287.058|
|      Spec. Heat Ratio|             -|             -|         -|           1.4|
+------------------------------------------------------------------------------+
-- Initial and free-stream conditions:
+------------------------------------------------------------------------------+
|                  Name|    Dim. value|    Ref. value|      Unit|Non-dim. value|
+------------------------------------------------------------------------------+
|       Static Pressure|        101325|             1|        Pa|        101325|
|               Density|       1.22498|             1|    kg/m^3|       1.22498|
|           Temperature|        288.15|             1|         K|        288.15|
|          Total Energy|        226952|             1|   m^2/s^2|        226952|
|            Velocity-X|       200.779|             1|       m/s|       200.779|
|            Velocity-Y|             0|             1|       m/s|             0|
|            Velocity-Z|       3.50461|             1|       m/s|       3.50461|
|    Velocity Magnitude|       200.809|             1|       m/s|       200.809|
+------------------------------------------------------------------------------+
|           Mach Number|             -|             -|         -|        0.5901|
+------------------------------------------------------------------------------+
Initialize Jacobian structure (Euler). MG level: 0.
Initialize Jacobian structure (Euler). MG level: 1.
Initialize Jacobian structure (Euler). MG level: 2.

------------------- Numerics Preprocessing ( Zone 0 ) -------------------

----------------- Integration Preprocessing ( Zone 0 ) ------------------

------------------- Iteration Preprocessing ( Zone 0 ) ------------------
Euler/Navier-Stokes/RANS fluid iteration.

------------------------------ Begin Solver -----------------------------

Simulation Run using the Single-zone Driver
WARNING: SU2 was not compiled for an AVX-capable architecture. Performance could be better,
         see <a href='https://su2code.github.io/docs_v7/Build-SU2-Linux-MacOS/#compiler-optimizations'>https://su2code.github.io/docs_v7/Build-SU2-Linux-MacOS/#compiler-optimizations</a>
WARNING: SU2 was not compiled for an AVX-capable architecture. Performance could be better,
         see <a href='https://su2code.github.io/docs_v7/Build-SU2-Linux-MacOS/#compiler-optimizations'>https://su2code.github.io/docs_v7/Build-SU2-Linux-MacOS/#compiler-optimizations</a>
WARNING: SU2 was not compiled for an AVX-capable architecture. Performance could be better,
         see <a href='https://su2code.github.io/docs_v7/Build-SU2-Linux-MacOS/#compiler-optimizations'>https://su2code.github.io/docs_v7/Build-SU2-Linux-MacOS/#compiler-optimizations</a>
+----------------------------------------------------------------------------------------------------------------------------------------------+
|   Time_Iter|  Outer_Iter|  Inner_Iter|    Cur_Time|   Time_Step|   Time(sec)|    rms[Rho]|   rms[RhoU]|   rms[RhoV]|   rms[RhoE]|        CEff|
+----------------------------------------------------------------------------------------------------------------------------------------------+
|           0|           0|           0|  0.0000e+00|  0.0000e+00|  5.8704e-01|   -0.059021|    2.303387|    2.039067|    5.431874|    1.970398|
|           0|           0|           1|  0.0000e+00|  0.0000e+00|  5.8534e-01|    0.002899|    2.488448|    2.194491|    5.502382|    2.658900|
|           0|           0|           2|  0.0000e+00|  0.0000e+00|  5.8524e-01|    0.026727|    2.569164|    2.438598|    5.519932|    4.074903|
|           0|           0|           3|  0.0000e+00|  0.0000e+00|  5.8436e-01|   -0.027928|    2.600852|    2.572666|    5.452520|    6.012667|
|           0|           0|           4|  0.0000e+00|  0.0000e+00|  5.8546e-01|   -0.066798|    2.611567|    2.619922|    5.409363|    7.697173|
|           0|           0|           5|  0.0000e+00|  0.0000e+00|  5.8341e-01|   -0.081876|    2.604321|    2.627463|    5.405669|    8.898085|
|           0|           0|           6|  0.0000e+00|  0.0000e+00|  5.8288e-01|   -0.109417|    2.568028|    2.631615|    5.384249|    9.783851|
|           0|           0|           7|  0.0000e+00|  0.0000e+00|  5.7931e-01|   -0.154243|    2.498102|    2.636523|    5.332167|   10.298250|
|           0|           0|           8|  0.0000e+00|  0.0000e+00|  5.8156e-01|   -0.209194|    2.421734|    2.624341|    5.261991|   10.394140|
|           0|           0|           9|  0.0000e+00|  0.0000e+00|  5.8379e-01|   -0.261272|    2.383246|    2.583148|    5.205405|   10.176655|

----------------------------- Solver Exit -------------------------------

Maximum number of iterations reached (ITER = 10) before convergence.
+-----------------------------------------------------------------------+
|      Convergence Field     |     Value    |   Criterion  |  Converged |
+-----------------------------------------------------------------------+
|                    rms[Rho]|     -0.261272|          &lt; -8|          No|
+-----------------------------------------------------------------------+
-------------------------------------------------------------------------
+-----------------------------------------------------------------------+
|        File Writing Summary       |              Filename             |
+-----------------------------------------------------------------------+
|SU2 binary restart                 |restart_flow_su2AFLRTest.dat       |

Writing the forces breakdown file (forces_breakdown_su2AFLRTest.dat).
|CSV file                           |surface_flow_su2AFLRTest.csv       |

Writing the forces breakdown file (forces_breakdown_su2AFLRTest.dat).
|Paraview                           |flow_su2AFLRTest.vtu               |

Writing the forces breakdown file (forces_breakdown_su2AFLRTest.dat).
|Paraview surface                   |surface_flow_su2AFLRTest.vtu       |

Writing the forces breakdown file (forces_breakdown_su2AFLRTest.dat).
+-----------------------------------------------------------------------+

--------------------------- Finalizing Solver ---------------------------
Deleted CNumerics container.
Deleted CIntegration container.
Deleted CSolver container.
Deleted CIteration container.
Deleted CInterface container.
Deleted CGeometry container.
Deleted CFreeFormDefBox class.
Deleted CSurfaceMovement class.
Deleted CVolumetricMovement class.
Deleted CConfig container.
Deleted nInst container.
Deleted COutput class.
-------------------------------------------------------------------------

------------------------- Exit Success (SU2_CFD) ------------------------

Total Force - Pressure + Viscous
Cl =  0.795414 Cd =  0.078161
Cmx =  0.000364 Cmy =  -0.203015 Cmz =  0.000109
Cx =  0.064267 Cy =  0.000149 Cz =  0.796657
Pressure Contribution
Cl_p =  0.795414 Cd_p =  0.078161
Cmx_p =  0.000364 Cmy_p =  -0.203015 Cmz_p =  0.000109
Cx_p =  0.064267 Cy_p =  0.000149 Cz_p =  0.796657
Viscous Contribution
Cl_v =  0.0 Cd_v =  0.0
Cmx_v =  0.0 Cmy_v =  0.0 Cmz_v =  0.0
Cx_v =  0.0 Cy_v =  0.0 Cz_v =  0.0

real	0m16.562s
user	0m16.437s
sys	0m0.381s
+ status=0
+ set +x

=================================================
CAPS verification (using pyCAPS) case su2_and_AFLR4_AFLR3_PyTest.py passed (as expected)
=================================================


=================================================
+ echo 'su2_Morph_PyTest.py test;'
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESP126/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
su2_Morph_PyTest.py test;
+ python -u su2_Morph_PyTest.py -outLevel=0
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESP126/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 4
	Name = Wing1, index = 1
	Name = Wing2, index = 2
	Name = Wake, index = 3
	Name = Farfield, index = 4
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 4
	Name = Wing1, index = 1
	Name = Wing2, index = 2
	Name = Wake, index = 3
	Name = Farfield, index = 4
AFLR4    : Proximity BG Surface Grid Generation Skipped
AFLR4    : No Modifications Required

Writing Tecplot file ....
Finished writing Tecplot file

Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 4
	Name = Wing1, index = 1
	Name = Wing2, index = 2
	Name = Wake, index = 3
	Name = Farfield, index = 4
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 4
	Name = Wing1, index = 1
	Name = Wing2, index = 2
	Name = Wake, index = 3
	Name = Farfield, index = 4
Getting volume mesh
 
AFLR2    : ---------------------------------------
AFLR2    : AFLR2 LIBRARY
AFLR2    : ADVANCING-FRONT/LOCAL-RECONNECTION
AFLR2    : TRIA/QUAD GRID GENERATOR
AFLR2    : Version Number 9.18.1
AFLR2    : Version Date   06/11/24 @ 05:52PM
AFLR2    : Compile OS     Darwin 23.5.0 arm64
AFLR2    : Compile Date   06/11/24 @ 05:52PM
AFLR2    : Copyright 1994-2021, D.L. Marcum
AFLR2    : ---------------------------------------
 
AFLR4    : ---------------------------------------
AFLR4    : AFLR4 LIBRARY
AFLR4    : ADVANCING-FRONT/LOCAL-RECONNECTION
AFLR4    : TRIA/QUAD SURFACE GRID GENERATOR
AFLR4    : Version Number 11.5.15
AFLR4    : Version Date   07/19/24 @ 07:04PM
AFLR4    : Compile OS     Darwin 23.5.0 arm64
AFLR4    : Compile Date   07/19/24 @ 07:06PM
AFLR4    : Copyright 1994-2021, D.L. Marcum
AFLR4    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.8.1
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.8.1
EGADS    : ---------------------------------------
Volume mesh:
	Number of nodes          = 56425
	Number of elements       = 326721
	Number of triangles      = 15872
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 310849
	Number of pyramids       = 0
	Number of prisms         = 0
	Number of hexahedrals    = 0

Writing Tecplot file ....
Finished writing Tecplot file


Writing SU2 file ....
Finished writing SU2 file

Getting CFD boundary conditions
	Boundary condition name - Farfield
	Boundary condition name - Wake
	Boundary condition name - Wing1
	Boundary condition name - Wing2
	Done getting CFD boundary conditions
Writing SU2 surface file
Writing SU2 Motion File - su2AFLRTest_motion.dat
Writing boundary flags
 - bcProps.surfaceProp[0].surfaceType = 3
 - bcProps.surfaceProp[1].surfaceType = 15
 - bcProps.surfaceProp[2].surfaceType = 1
 - bcProps.surfaceProp[3].surfaceType = 1
Done boundary flags
Warning: The su2 cfg file will be overwritten!
Write SU2 configuration file for version "Harrier (8.0.1)"


Running SU2......

-------------------------------------------------------------------------
|    ___ _   _ ___                                                      |
|   / __| | | |_  )   Release 8.0.0 "Harrier"                           |
|   \__ \ |_| |/ /                                                      |
|   |___/\___//___|   Suite (Computational Fluid Dynamics Code)         |
|                                                                       |
-------------------------------------------------------------------------
| SU2 Project Website: <a href='https://su2code.github.io'>https://su2code.github.io</a>                        |
|                                                                       |
| The SU2 Project is maintained by the SU2 Foundation                   |
| (<a href='http://su2foundation.org'>http://su2foundation.org</a>)                                            |
-------------------------------------------------------------------------
| Copyright 2012-2023, SU2 Contributors                                 |
|                                                                       |
| SU2 is free software; you can redistribute it and/or                  |
| modify it under the terms of the GNU Lesser General Public            |
| License as published by the Free Software Foundation; either          |
| version 2.1 of the License, or (at your option) any later version.    |
|                                                                       |
| SU2 is distributed in the hope that it will be useful,                |
| but WITHOUT ANY WARRANTY; without even the implied warranty of        |
| MERCHANTABILITY or FITNESS FOR A PARTICULAR PURPOSE. See the GNU      |
| Lesser General Public License for more details.                       |
|                                                                       |
| You should have received a copy of the GNU Lesser General Public      |
| License along with SU2. If not, see &lt;<a href='http://www.gnu.org/licenses/'>http://www.gnu.org/licenses/</a>&gt;.   |
-------------------------------------------------------------------------

Parsing config file for zone 0

----------------- Physical Case Definition ( Zone 0 ) -------------------
Compressible Euler equations.
Mach number: 0.5901.
Angle of attack (AoA): 1 deg, and angle of sideslip (AoS): 0 deg.
No restart solution, use the values at infinity (freestream).
Dimensional simulation.
The reference area is 40 m^2.
The semi-span will be computed using the max y(3D) value.
The reference length is 14.1421 m.
Surface(s) where the force coefficients are evaluated and 
their reference origin for moment computation: 
   - BC_1 (0, 0, 0).
   - BC_2 (0, 0, 0) m.
Surface(s) plotted in the output file: BC_1, BC_2.
Surface(s) affected by the design variables: BC_1, BC_2.
Input mesh file name: ../volumeMesh/aflr3_CAPS.su2

--------------- Space Numerical Integration ( Zone 0 ) ------------------
Roe (with entropy fix = 0.001) solver for the flow inviscid terms.
Standard Roe without low-dissipation function.
Second order integration in space, with slope limiter.
Venkatakrishnan slope-limiting method, with constant: 0.05.
The reference element size is: 1. 
Gradient for upwind reconstruction: inverse-distance weighted Least-Squares.
Gradient for viscous and source terms: inverse-distance weighted Least-Squares.

--------------- Time Numerical Integration  ( Zone 0 ) ------------------
Local time stepping (steady state simulation).
Euler implicit method for the flow equations.
FGMRES is used for solving the linear system.
Using a ILU(0) preconditioning.
Convergence criteria of the linear solver: 1e-06.
Max number of linear iterations: 10.
V Multigrid Cycle, with 2 multigrid levels.
Damping factor for the residual restriction: 0.75.
Damping factor for the correction prolongation: 0.75.
No CFL adaptation.
+-------------------------------------------+
|  MG Level| Presmooth|PostSmooth|CorrectSmo|
+-------------------------------------------+
|         0|         1|         0|         0|
|         1|         2|         0|         0|
|         2|         3|         0|         0|
+-------------------------------------------+
Courant-Friedrichs-Lewy number:       10

------------------ Convergence Criteria  ( Zone 0 ) ---------------------
Maximum number of solver subiterations: 10.
Begin convergence monitoring at iteration 5.
Residual minimum value: 1e-8.
Cauchy series min. value: 1e-10.
Number of Cauchy elements: 100.
Begin windowed time average at iteration 0.

-------------------- Output Information ( Zone 0 ) ----------------------
File writing frequency: 
+------------------------------------+
|                     File| Frequency|
+------------------------------------+
|                  RESTART|       250|
|              SURFACE_CSV|       250|
|                 PARAVIEW|       250|
|         SURFACE_PARAVIEW|       250|
+------------------------------------+
Writing the convergence history file every 1 inner iterations.
Writing the screen convergence history every 1 inner iterations.
The tabular file format is CSV (.csv).
Convergence history file name: history.
Forces breakdown file name: forces_breakdown_su2AFLRTest.dat.
Surface file name: surface_flow_su2AFLRTest.
Volume file name: flow_su2AFLRTest.
Restart file name: restart_flow_su2AFLRTest.dat.

------------- Config File Boundary Information ( Zone 0 ) ---------------
+-----------------------------------------------------------------------+
|                        Marker Type|                        Marker Name|
+-----------------------------------------------------------------------+
|                         Euler wall|                               BC_1|
|                                   |                               BC_2|
+-----------------------------------------------------------------------+
|                          Far-field|                               BC_4|
+-----------------------------------------------------------------------+
|                  Internal boundary|                               BC_3|
+-----------------------------------------------------------------------+

-------------------- Output Preprocessing ( Zone 0 ) --------------------

WARNING: SURFACE_PRESSURE_DROP can only be computed for at least 2 surfaces (outlet, inlet, ...)

Screen output fields: TIME_ITER, OUTER_ITER, INNER_ITER, CUR_TIME, TIME_STEP, WALL_TIME, RMS_DENSITY, RMS_MOMENTUM-X, RMS_MOMENTUM-Y, RMS_ENERGY, EFFICIENCY
History output group(s): ITER, TIME_DOMAIN, WALL_TIME, RMS_RES, AERO_COEFF
Convergence field(s): RMS_DENSITY
Warning: No (valid) fields chosen for time convergence monitoring. Time convergence monitoring inactive.
Volume output fields: COORDINATES, SOLUTION, PRIMITIVE

------------------- Geometry Preprocessing ( Zone 0 ) -------------------
Three dimensional problem.
56425 grid points.
310849 volume elements.
4 surface markers.
9958 boundary elements in index 0 (Marker = BC_1).
5414 boundary elements in index 1 (Marker = BC_2).
80 boundary elements in index 2 (Marker = BC_3).
420 boundary elements in index 3 (Marker = BC_4).
310849 tetrahedra.
Setting point connectivity.
Renumbering points (Reverse Cuthill McKee Ordering).
Recomputing point connectivity.
Setting element connectivity.
Checking the numerical grid orientation.
All volume elements are correctly orientend.
All surface elements are correctly orientend.
Identifying edges and vertices.
Setting the control volume structure.
Volume of the computational grid: 2.08667e+06.
Searching for the closest normal neighbors to the surfaces.
Storing a mapping from global to local point index.
Compute the surface curvature.
Max K: 5523.74. Mean K: 58.8177. Standard deviation K: 282.533.
Checking for periodicity.
Computing mesh quality statistics for the dual control volumes.
+--------------------------------------------------------------+
|           Mesh Quality Metric|        Minimum|        Maximum|
+--------------------------------------------------------------+
|    Orthogonality Angle (deg.)|        29.2241|        86.0517|
|     CV Face Area Aspect Ratio|        1.12536|         4445.2|
|           CV Sub-Volume Ratio|        1.02845|        57909.8|
+--------------------------------------------------------------+
Setting the multigrid structure.
+-------------------------------------------+
|  MG Level|       CVs|Aggl. Rate|       CFL|
+-------------------------------------------+
|         0|     56425|    1/1.00|        10|
|         1|      9299|    1/6.07|   8.22393|
|         2|      1430|     1/6.5|   6.60902|
+-------------------------------------------+
Finding max control volume width.
Semi-span length = 7.07107 m.
Wetted area = 96.2324 m^2.
Area projection in the x-plane = 7.65774 m^2, y-plane = 4.21853 m^2, z-plane = 45.5887 m^2.
Max. coordinate in the x-direction = 12.3872 m, y-direction = 7.07107 m, z-direction = 0.521791 m.
Min. coordinate in the x-direction = 0 m, y-direction = -7.07107 m, z-direction = -0.0650201 m.
Checking if Euler &amp; Symmetry markers are straight/plane:
Boundary marker BC_1 is NOT a single plane.
Boundary marker BC_2 is NOT a single plane.
Computing wall distances.

-------------------- Solver Preprocessing ( Zone 0 ) --------------------
Inviscid flow: Computing density based on free-stream
temperature and pressure using the ideal gas law.
Force coefficients computed using free-stream values.

-- Models:
+------------------------------------------------------------------------------+
|          Viscosity Model|        Conductivity Model|              Fluid Model|
+------------------------------------------------------------------------------+
|                        -|                         -|             STANDARD_AIR|
+------------------------------------------------------------------------------+
-- Fluid properties:
+------------------------------------------------------------------------------+
|                  Name|    Dim. value|    Ref. value|      Unit|Non-dim. value|
+------------------------------------------------------------------------------+
|          Gas Constant|       287.058|             1|  N.m/kg.K|       287.058|
|      Spec. Heat Ratio|             -|             -|         -|           1.4|
+------------------------------------------------------------------------------+
-- Initial and free-stream conditions:
+------------------------------------------------------------------------------+
|                  Name|    Dim. value|    Ref. value|      Unit|Non-dim. value|
+------------------------------------------------------------------------------+
|       Static Pressure|        101325|             1|        Pa|        101325|
|               Density|       1.22498|             1|    kg/m^3|       1.22498|
|           Temperature|        288.15|             1|         K|        288.15|
|          Total Energy|        226952|             1|   m^2/s^2|        226952|
|            Velocity-X|       200.779|             1|       m/s|       200.779|
|            Velocity-Y|             0|             1|       m/s|             0|
|            Velocity-Z|       3.50461|             1|       m/s|       3.50461|
|    Velocity Magnitude|       200.809|             1|       m/s|       200.809|
+------------------------------------------------------------------------------+
|           Mach Number|             -|             -|         -|        0.5901|
+------------------------------------------------------------------------------+
Initialize Jacobian structure (Euler). MG level: 0.
Initialize Jacobian structure (Euler). MG level: 1.
Initialize Jacobian structure (Euler). MG level: 2.

------------------- Numerics Preprocessing ( Zone 0 ) -------------------

----------------- Integration Preprocessing ( Zone 0 ) ------------------

------------------- Iteration Preprocessing ( Zone 0 ) ------------------
Euler/Navier-Stokes/RANS fluid iteration.

------------------------------ Begin Solver -----------------------------

Simulation Run using the Single-zone Driver
WARNING: SU2 was not compiled for an AVX-capable architecture. Performance could be better,
         see <a href='https://su2code.github.io/docs_v7/Build-SU2-Linux-MacOS/#compiler-optimizations'>https://su2code.github.io/docs_v7/Build-SU2-Linux-MacOS/#compiler-optimizations</a>
WARNING: SU2 was not compiled for an AVX-capable architecture. Performance could be better,
         see <a href='https://su2code.github.io/docs_v7/Build-SU2-Linux-MacOS/#compiler-optimizations'>https://su2code.github.io/docs_v7/Build-SU2-Linux-MacOS/#compiler-optimizations</a>
WARNING: SU2 was not compiled for an AVX-capable architecture. Performance could be better,
         see <a href='https://su2code.github.io/docs_v7/Build-SU2-Linux-MacOS/#compiler-optimizations'>https://su2code.github.io/docs_v7/Build-SU2-Linux-MacOS/#compiler-optimizations</a>
+----------------------------------------------------------------------------------------------------------------------------------------------+
|   Time_Iter|  Outer_Iter|  Inner_Iter|    Cur_Time|   Time_Step|   Time(sec)|    rms[Rho]|   rms[RhoU]|   rms[RhoV]|   rms[RhoE]|        CEff|
+----------------------------------------------------------------------------------------------------------------------------------------------+
|           0|           0|           0|  0.0000e+00|  0.0000e+00|  8.8576e-01|   -0.459271|    1.871877|    1.655308|    5.031624|    0.762262|
|           0|           0|           1|  0.0000e+00|  0.0000e+00|  8.7906e-01|   -0.456941|    2.040681|    1.747831|    5.043074|    1.447848|
|           0|           0|           2|  0.0000e+00|  0.0000e+00|  8.7573e-01|   -0.398416|    2.120447|    1.970735|    5.091930|    3.304023|
|           0|           0|           3|  0.0000e+00|  0.0000e+00|  8.7394e-01|   -0.382713|    2.165329|    2.106879|    5.096084|    7.146675|
|           0|           0|           4|  0.0000e+00|  0.0000e+00|  8.7279e-01|   -0.387623|    2.192520|    2.179204|    5.084553|   12.977091|
|           0|           0|           5|  0.0000e+00|  0.0000e+00|  8.7198e-01|   -0.395260|    2.209372|    2.208904|    5.080255|   20.307648|
|           0|           0|           6|  0.0000e+00|  0.0000e+00|  8.7164e-01|   -0.386688|    2.193854|    2.231688|    5.091259|   28.440654|
|           0|           0|           7|  0.0000e+00|  0.0000e+00|  8.7202e-01|   -0.387582|    2.150321|    2.255497|    5.085909|   33.542538|
|           0|           0|           8|  0.0000e+00|  0.0000e+00|  8.7194e-01|   -0.424592|    2.094097|    2.270673|    5.038598|   31.887370|
|           0|           0|           9|  0.0000e+00|  0.0000e+00|  8.7250e-01|   -0.488373|    2.035089|    2.263820|    4.964251|   26.644721|

----------------------------- Solver Exit -------------------------------

Maximum number of iterations reached (ITER = 10) before convergence.
+-----------------------------------------------------------------------+
|      Convergence Field     |     Value    |   Criterion  |  Converged |
+-----------------------------------------------------------------------+
|                    rms[Rho]|     -0.488373|          &lt; -8|          No|
+-----------------------------------------------------------------------+
-------------------------------------------------------------------------
+-----------------------------------------------------------------------+
|        File Writing Summary       |              Filename             |
+-----------------------------------------------------------------------+
|SU2 binary restart                 |restart_flow_su2AFLRTest.dat       |

Writing the forces breakdown file (forces_breakdown_su2AFLRTest.dat).
|CSV file                           |surface_flow_su2AFLRTest.csv       |

Writing the forces breakdown file (forces_breakdown_su2AFLRTest.dat).
|Paraview                           |flow_su2AFLRTest.vtu               |

Writing the forces breakdown file (forces_breakdown_su2AFLRTest.dat).
|Paraview surface                   |surface_flow_su2AFLRTest.vtu       |

Writing the forces breakdown file (forces_breakdown_su2AFLRTest.dat).
+-----------------------------------------------------------------------+

--------------------------- Finalizing Solver ---------------------------
Deleted CNumerics container.
Deleted CIntegration container.
Deleted CSolver container.
Deleted CIteration container.
Deleted CInterface container.
Deleted CGeometry container.
Deleted CFreeFormDefBox class.
Deleted CSurfaceMovement class.
Deleted CVolumetricMovement class.
Deleted CConfig container.
Deleted nInst container.
Deleted COutput class.
-------------------------------------------------------------------------

------------------------- Exit Success (SU2_CFD) ------------------------

Total Force - Pressure + Viscous
Cl =  0.522817 Cd =  0.019622
Projecting tessellation 1 (of 4) on to new body
Projecting tessellation 2 (of 4) on to new body
Projecting tessellation 3 (of 4) on to new body
Projecting tessellation 4 (of 4) on to new body
Getting CFD boundary conditions
	Boundary condition name - Farfield
	Boundary condition name - Wake
	Boundary condition name - Wing1
	Boundary condition name - Wing2
	Done getting CFD boundary conditions
Writing SU2 surface file
Writing SU2 Motion File - su2AFLRTest_motion.dat
Writing boundary flags
 - bcProps.surfaceProp[0].surfaceType = 3
 - bcProps.surfaceProp[1].surfaceType = 15
 - bcProps.surfaceProp[2].surfaceType = 1
 - bcProps.surfaceProp[3].surfaceType = 1
Done boundary flags
Warning: The su2 cfg file will be overwritten!
Write SU2 configuration file for version "Harrier (8.0.1)"


Mesh Morphing......

-------------------------------------------------------------------------
|    ___ _   _ ___                                                      |
|   / __| | | |_  )   Release 8.0.0 "Harrier"                           |
|   \__ \ |_| |/ /                                                      |
|   |___/\___//___|   Suite (Mesh Deformation Code)                     |
|                                                                       |
-------------------------------------------------------------------------
| SU2 Project Website: <a href='https://su2code.github.io'>https://su2code.github.io</a>                        |
|                                                                       |
| The SU2 Project is maintained by the SU2 Foundation                   |
| (<a href='http://su2foundation.org'>http://su2foundation.org</a>)                                            |
-------------------------------------------------------------------------
| Copyright 2012-2023, SU2 Contributors                                 |
|                                                                       |
| SU2 is free software; you can redistribute it and/or                  |
| modify it under the terms of the GNU Lesser General Public            |
| License as published by the Free Software Foundation; either          |
| version 2.1 of the License, or (at your option) any later version.    |
|                                                                       |
| SU2 is distributed in the hope that it will be useful,                |
| but WITHOUT ANY WARRANTY; without even the implied warranty of        |
| MERCHANTABILITY or FITNESS FOR A PARTICULAR PURPOSE. See the GNU      |
| Lesser General Public License for more details.                       |
|                                                                       |
| You should have received a copy of the GNU Lesser General Public      |
| License along with SU2. If not, see &lt;<a href='http://www.gnu.org/licenses/'>http://www.gnu.org/licenses/</a>&gt;.   |
-------------------------------------------------------------------------

----------------- Physical Case Definition ( Zone 0 ) -------------------
Input mesh file name: aflr3_CAPS.su2

---------------- Grid deformation parameters ( Zone 0 )  ----------------
Grid deformation using a linear elasticity method.


-------------------- Output Information ( Zone 0 ) ----------------------
Output mesh file name: aflr3_CAPS.su2. 
Cell stiffness scaled by distance to nearest solid surface.

------------- Config File Boundary Information ( Zone 0 ) ---------------
+-----------------------------------------------------------------------+
|                        Marker Type|                        Marker Name|
+-----------------------------------------------------------------------+
|                         Euler wall|                               BC_1|
|                                   |                               BC_2|
+-----------------------------------------------------------------------+
|                          Far-field|                               BC_4|
+-----------------------------------------------------------------------+
|                  Internal boundary|                               BC_3|
+-----------------------------------------------------------------------+
Three dimensional problem.
56425 grid points.
310849 volume elements.
4 surface markers.
9958 boundary elements in index 0 (Marker = BC_1).
5414 boundary elements in index 1 (Marker = BC_2).
80 boundary elements in index 2 (Marker = BC_3).
420 boundary elements in index 3 (Marker = BC_4).
310849 tetrahedra.

----------------------- Preprocessing computations ----------------------
Setting local point connectivity.
Checking the numerical grid orientation of the interior elements.
All volume elements are correctly orientend.
All surface elements are correctly orientend.
Identify edges and vertices.
Setting the bound control volume structure.
Volume of the computational grid: 2.08667e+06.
  Info: Ignoring the following volume output fields/groups:
  SOLUTION
Volume output fields: COORDINATES
  Info: Ignoring the following screen output fields:
  RMS_DENSITY, RMS_MOMENTUM-X, RMS_MOMENTUM-Y, RMS_ENERGY, EFFICIENCY
Screen output fields: TIME_ITER, OUTER_ITER, INNER_ITER, CUR_TIME, TIME_STEP, WALL_TIME
  Info: Ignoring the following history output groups:
  RMS_RES, AERO_COEFF
History output group(s): ITER, TIME_DOMAIN, WALL_TIME
Ignoring Convergence Field(s): RMS_DENSITY 
Warning: No (valid) fields chosen for convergence monitoring. Convergence monitoring inactive.
Warning: No (valid) fields chosen for time convergence monitoring. Time convergence monitoring inactive.

--------------------- Surface grid deformation (ZONE 0) -----------------
Performing the deformation of the surface grid.
Updating the surface coordinates from the input file.

------------------- Volumetric grid deformation (ZONE 0) ----------------
Performing the deformation of the volumetric grid.

WARNING: Convexity is not checked for 3D elements (issue #1171).


Completed in 3.993225 seconds on 1 core.

----------------------- Write deformed grid files -----------------------
|SU2 mesh                           |aflr3_CAPS.su2                     |
|CSV file                           |surface_deformed.csv               |
|Paraview                           |volume_deformed.vtu                |
|Paraview surface                   |surface_deformed.vtu               |
Adding any FFD information to the SU2 file.

------------------------- Finalize Solver -------------------------
Deleted CNumerics container.
Deleted CSolver container.
Deleted CGeometry container.
Deleted CSurfaceMovement class.
Deleted CVolumetricMovement class.
Deleted CConfig container.
Deleted COutput class.

------------------------- Exit Success (SU2_DEF) ------------------------



Running SU2......

-------------------------------------------------------------------------
|    ___ _   _ ___                                                      |
|   / __| | | |_  )   Release 8.0.0 "Harrier"                           |
|   \__ \ |_| |/ /                                                      |
|   |___/\___//___|   Suite (Computational Fluid Dynamics Code)         |
|                                                                       |
-------------------------------------------------------------------------
| SU2 Project Website: <a href='https://su2code.github.io'>https://su2code.github.io</a>                        |
|                                                                       |
| The SU2 Project is maintained by the SU2 Foundation                   |
| (<a href='http://su2foundation.org'>http://su2foundation.org</a>)                                            |
-------------------------------------------------------------------------
| Copyright 2012-2023, SU2 Contributors                                 |
|                                                                       |
| SU2 is free software; you can redistribute it and/or                  |
| modify it under the terms of the GNU Lesser General Public            |
| License as published by the Free Software Foundation; either          |
| version 2.1 of the License, or (at your option) any later version.    |
|                                                                       |
| SU2 is distributed in the hope that it will be useful,                |
| but WITHOUT ANY WARRANTY; without even the implied warranty of        |
| MERCHANTABILITY or FITNESS FOR A PARTICULAR PURPOSE. See the GNU      |
| Lesser General Public License for more details.                       |
|                                                                       |
| You should have received a copy of the GNU Lesser General Public      |
| License along with SU2. If not, see &lt;<a href='http://www.gnu.org/licenses/'>http://www.gnu.org/licenses/</a>&gt;.   |
-------------------------------------------------------------------------

Parsing config file for zone 0

----------------- Physical Case Definition ( Zone 0 ) -------------------
Compressible Euler equations.
Mach number: 0.5901.
Angle of attack (AoA): 1 deg, and angle of sideslip (AoS): 0 deg.
No restart solution, use the values at infinity (freestream).
Dimensional simulation.
The reference area is 40 m^2.
The semi-span will be computed using the max y(3D) value.
The reference length is 14.1421 m.
Surface(s) where the force coefficients are evaluated and 
their reference origin for moment computation: 
   - BC_1 (0, 0, 0).
   - BC_2 (0, 0, 0) m.
Surface(s) plotted in the output file: BC_1, BC_2.
Surface(s) affected by the design variables: BC_1, BC_2.
Input mesh file name: aflr3_CAPS.su2

--------------- Space Numerical Integration ( Zone 0 ) ------------------
Roe (with entropy fix = 0.001) solver for the flow inviscid terms.
Standard Roe without low-dissipation function.
Second order integration in space, with slope limiter.
Venkatakrishnan slope-limiting method, with constant: 0.05.
The reference element size is: 1. 
Gradient for upwind reconstruction: inverse-distance weighted Least-Squares.
Gradient for viscous and source terms: inverse-distance weighted Least-Squares.

--------------- Time Numerical Integration  ( Zone 0 ) ------------------
Local time stepping (steady state simulation).
Euler implicit method for the flow equations.
FGMRES is used for solving the linear system.
Using a ILU(0) preconditioning.
Convergence criteria of the linear solver: 1e-06.
Max number of linear iterations: 10.
V Multigrid Cycle, with 2 multigrid levels.
Damping factor for the residual restriction: 0.75.
Damping factor for the correction prolongation: 0.75.
No CFL adaptation.
+-------------------------------------------+
|  MG Level| Presmooth|PostSmooth|CorrectSmo|
+-------------------------------------------+
|         0|         1|         0|         0|
|         1|         2|         0|         0|
|         2|         3|         0|         0|
+-------------------------------------------+
Courant-Friedrichs-Lewy number:       10

------------------ Convergence Criteria  ( Zone 0 ) ---------------------
Maximum number of solver subiterations: 10.
Begin convergence monitoring at iteration 5.
Residual minimum value: 1e-8.
Cauchy series min. value: 1e-10.
Number of Cauchy elements: 100.
Begin windowed time average at iteration 0.

-------------------- Output Information ( Zone 0 ) ----------------------
File writing frequency: 
+------------------------------------+
|                     File| Frequency|
+------------------------------------+
|                  RESTART|       250|
|              SURFACE_CSV|       250|
|                 PARAVIEW|       250|
|         SURFACE_PARAVIEW|       250|
+------------------------------------+
Writing the convergence history file every 1 inner iterations.
Writing the screen convergence history every 1 inner iterations.
The tabular file format is CSV (.csv).
Convergence history file name: history.
Forces breakdown file name: forces_breakdown_su2AFLRTest.dat.
Surface file name: surface_flow_su2AFLRTest.
Volume file name: flow_su2AFLRTest.
Restart file name: restart_flow_su2AFLRTest.dat.

------------- Config File Boundary Information ( Zone 0 ) ---------------
+-----------------------------------------------------------------------+
|                        Marker Type|                        Marker Name|
+-----------------------------------------------------------------------+
|                         Euler wall|                               BC_1|
|                                   |                               BC_2|
+-----------------------------------------------------------------------+
|                          Far-field|                               BC_4|
+-----------------------------------------------------------------------+
|                  Internal boundary|                               BC_3|
+-----------------------------------------------------------------------+

-------------------- Output Preprocessing ( Zone 0 ) --------------------

WARNING: SURFACE_PRESSURE_DROP can only be computed for at least 2 surfaces (outlet, inlet, ...)

Screen output fields: TIME_ITER, OUTER_ITER, INNER_ITER, CUR_TIME, TIME_STEP, WALL_TIME, RMS_DENSITY, RMS_MOMENTUM-X, RMS_MOMENTUM-Y, RMS_ENERGY, EFFICIENCY
History output group(s): ITER, TIME_DOMAIN, WALL_TIME, RMS_RES, AERO_COEFF
Convergence field(s): RMS_DENSITY
Warning: No (valid) fields chosen for time convergence monitoring. Time convergence monitoring inactive.
Volume output fields: COORDINATES, SOLUTION, PRIMITIVE

------------------- Geometry Preprocessing ( Zone 0 ) -------------------
Three dimensional problem.
56425 grid points.
310849 volume elements.
4 surface markers.
9958 boundary elements in index 0 (Marker = BC_1).
5414 boundary elements in index 1 (Marker = BC_2).
80 boundary elements in index 2 (Marker = BC_3).
420 boundary elements in index 3 (Marker = BC_4).
310849 tetrahedra.
Setting point connectivity.
Renumbering points (Reverse Cuthill McKee Ordering).
Recomputing point connectivity.
Setting element connectivity.
Checking the numerical grid orientation.
All volume elements are correctly orientend.
All surface elements are correctly orientend.
Identifying edges and vertices.
Setting the control volume structure.
Volume of the computational grid: 2.08667e+06.
Searching for the closest normal neighbors to the surfaces.
Storing a mapping from global to local point index.
Compute the surface curvature.
Max K: 5523.56. Mean K: 58.7619. Standard deviation K: 282.437.
Checking for periodicity.
Computing mesh quality statistics for the dual control volumes.
+--------------------------------------------------------------+
|           Mesh Quality Metric|        Minimum|        Maximum|
+--------------------------------------------------------------+
|    Orthogonality Angle (deg.)|        26.9796|        85.7696|
|     CV Face Area Aspect Ratio|        1.13453|        4556.55|
|           CV Sub-Volume Ratio|        1.03232|        75345.6|
+--------------------------------------------------------------+
Setting the multigrid structure.
+-------------------------------------------+
|  MG Level|       CVs|Aggl. Rate|       CFL|
+-------------------------------------------+
|         0|     56425|    1/1.00|        10|
|         1|      9299|    1/6.07|   8.22393|
|         2|      1430|     1/6.5|   6.60902|
+-------------------------------------------+
Finding max control volume width.
Semi-span length = 7.07107 m.
Wetted area = 95.6308 m^2.
Area projection in the x-plane = 9.17945 m^2, y-plane = 4.04295 m^2, z-plane = 44.962 m^2.
Max. coordinate in the x-direction = 12.3585 m, y-direction = 7.07107 m, z-direction = 0.521791 m.
Min. coordinate in the x-direction = 0 m, y-direction = -7.07107 m, z-direction = -0.400127 m.
Checking if Euler &amp; Symmetry markers are straight/plane:
Boundary marker BC_1 is NOT a single plane.
Boundary marker BC_2 is NOT a single plane.
Computing wall distances.

-------------------- Solver Preprocessing ( Zone 0 ) --------------------
Inviscid flow: Computing density based on free-stream
temperature and pressure using the ideal gas law.
Force coefficients computed using free-stream values.

-- Models:
+------------------------------------------------------------------------------+
|          Viscosity Model|        Conductivity Model|              Fluid Model|
+------------------------------------------------------------------------------+
|                        -|                         -|             STANDARD_AIR|
+------------------------------------------------------------------------------+
-- Fluid properties:
+------------------------------------------------------------------------------+
|                  Name|    Dim. value|    Ref. value|      Unit|Non-dim. value|
+------------------------------------------------------------------------------+
|          Gas Constant|       287.058|             1|  N.m/kg.K|       287.058|
|      Spec. Heat Ratio|             -|             -|         -|           1.4|
+------------------------------------------------------------------------------+
-- Initial and free-stream conditions:
+------------------------------------------------------------------------------+
|                  Name|    Dim. value|    Ref. value|      Unit|Non-dim. value|
+------------------------------------------------------------------------------+
|       Static Pressure|        101325|             1|        Pa|        101325|
|               Density|       1.22498|             1|    kg/m^3|       1.22498|
|           Temperature|        288.15|             1|         K|        288.15|
|          Total Energy|        226952|             1|   m^2/s^2|        226952|
|            Velocity-X|       200.779|             1|       m/s|       200.779|
|            Velocity-Y|             0|             1|       m/s|             0|
|            Velocity-Z|       3.50461|             1|       m/s|       3.50461|
|    Velocity Magnitude|       200.809|             1|       m/s|       200.809|
+------------------------------------------------------------------------------+
|           Mach Number|             -|             -|         -|        0.5901|
+------------------------------------------------------------------------------+
Initialize Jacobian structure (Euler). MG level: 0.
Initialize Jacobian structure (Euler). MG level: 1.
Initialize Jacobian structure (Euler). MG level: 2.

------------------- Numerics Preprocessing ( Zone 0 ) -------------------

----------------- Integration Preprocessing ( Zone 0 ) ------------------

------------------- Iteration Preprocessing ( Zone 0 ) ------------------
Euler/Navier-Stokes/RANS fluid iteration.

------------------------------ Begin Solver -----------------------------

Simulation Run using the Single-zone Driver
WARNING: SU2 was not compiled for an AVX-capable architecture. Performance could be better,
         see <a href='https://su2code.github.io/docs_v7/Build-SU2-Linux-MacOS/#compiler-optimizations'>https://su2code.github.io/docs_v7/Build-SU2-Linux-MacOS/#compiler-optimizations</a>
WARNING: SU2 was not compiled for an AVX-capable architecture. Performance could be better,
         see <a href='https://su2code.github.io/docs_v7/Build-SU2-Linux-MacOS/#compiler-optimizations'>https://su2code.github.io/docs_v7/Build-SU2-Linux-MacOS/#compiler-optimizations</a>
WARNING: SU2 was not compiled for an AVX-capable architecture. Performance could be better,
         see <a href='https://su2code.github.io/docs_v7/Build-SU2-Linux-MacOS/#compiler-optimizations'>https://su2code.github.io/docs_v7/Build-SU2-Linux-MacOS/#compiler-optimizations</a>
+----------------------------------------------------------------------------------------------------------------------------------------------+
|   Time_Iter|  Outer_Iter|  Inner_Iter|    Cur_Time|   Time_Step|   Time(sec)|    rms[Rho]|   rms[RhoU]|   rms[RhoV]|   rms[RhoE]|        CEff|
+----------------------------------------------------------------------------------------------------------------------------------------------+
|           0|           0|           0|  0.0000e+00|  0.0000e+00|  8.8331e-01|   -0.398750|    1.977474|    1.644084|    5.092145|    1.923782|
|           0|           0|           1|  0.0000e+00|  0.0000e+00|  8.7882e-01|   -0.248975|    2.258948|    1.976579|    5.257848|    2.578720|
|           0|           0|           2|  0.0000e+00|  0.0000e+00|  8.7633e-01|   -0.198142|    2.347683|    2.225644|    5.300689|    3.981171|
|           0|           0|           3|  0.0000e+00|  0.0000e+00|  8.7615e-01|   -0.214514|    2.375555|    2.358260|    5.270011|    5.965906|
|           0|           0|           4|  0.0000e+00|  0.0000e+00|  8.7501e-01|   -0.239435|    2.394864|    2.421022|    5.239901|    7.849147|
|           0|           0|           5|  0.0000e+00|  0.0000e+00|  8.7426e-01|   -0.262371|    2.404237|    2.445537|    5.228001|    9.366346|
|           0|           0|           6|  0.0000e+00|  0.0000e+00|  8.7433e-01|   -0.284513|    2.389017|    2.460376|    5.215548|   10.610658|
|           0|           0|           7|  0.0000e+00|  0.0000e+00|  8.7394e-01|   -0.311476|    2.344163|    2.476241|    5.184871|   11.527148|
|           0|           0|           8|  0.0000e+00|  0.0000e+00|  8.7459e-01|   -0.361259|    2.273271|    2.486137|    5.118277|   12.003369|
|           0|           0|           9|  0.0000e+00|  0.0000e+00|  8.7380e-01|   -0.414971|    2.206048|    2.472056|    5.049690|   12.052158|

----------------------------- Solver Exit -------------------------------

Maximum number of iterations reached (ITER = 10) before convergence.
+-----------------------------------------------------------------------+
|      Convergence Field     |     Value    |   Criterion  |  Converged |
+-----------------------------------------------------------------------+
|                    rms[Rho]|     -0.414971|          &lt; -8|          No|
+-----------------------------------------------------------------------+
-------------------------------------------------------------------------
+-----------------------------------------------------------------------+
|        File Writing Summary       |              Filename             |
+-----------------------------------------------------------------------+
|SU2 binary restart                 |restart_flow_su2AFLRTest.dat       |

Writing the forces breakdown file (forces_breakdown_su2AFLRTest.dat).
|CSV file                           |surface_flow_su2AFLRTest.csv       |

Writing the forces breakdown file (forces_breakdown_su2AFLRTest.dat).
|Paraview                           |flow_su2AFLRTest.vtu               |

Writing the forces breakdown file (forces_breakdown_su2AFLRTest.dat).
|Paraview surface                   |surface_flow_su2AFLRTest.vtu       |

Writing the forces breakdown file (forces_breakdown_su2AFLRTest.dat).
+-----------------------------------------------------------------------+

--------------------------- Finalizing Solver ---------------------------
Deleted CNumerics container.
Deleted CIntegration container.
Deleted CSolver container.
Deleted CIteration container.
Deleted CInterface container.
Deleted CGeometry container.
Deleted CFreeFormDefBox class.
Deleted CSurfaceMovement class.
Deleted CVolumetricMovement class.
Deleted CConfig container.
Deleted nInst container.
Deleted COutput class.
-------------------------------------------------------------------------

------------------------- Exit Success (SU2_CFD) ------------------------

Total Force - Pressure + Viscous
Cl =  0.884977 Cd =  0.073429

real	0m38.544s
user	0m37.525s
sys	0m1.197s
+ status=0
+ set +x

=================================================
CAPS verification (using pyCAPS) case su2_Morph_PyTest.py passed (as expected)
=================================================

delaundo: /Users/jenkins/util/delaundo/delaundo/src/delaundo

=================================================
+ echo 'su2_and_Delaundo_PyTest.py test;'
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESP126/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
su2_and_Delaundo_PyTest.py test;
+ python -u su2_and_Delaundo_PyTest.py -outLevel=0
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESP126/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 5
	Name = 2DSlice, index = 1
	Name = TunnelWall, index = 2
	Name = OutFlow, index = 3
	Name = InFlow, index = 4
	Name = Airfoil, index = 5
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 5
	Name = 2DSlice, index = 1
	Name = TunnelWall, index = 2
	Name = OutFlow, index = 3
	Name = InFlow, index = 4
	Name = Airfoil, index = 5

Getting mesh sizing parameters
	Mesh sizing name - 2DSlice
	Mesh sizing name - Airfoil
	Mesh sizing name - InFlow
	Mesh sizing name - OutFlow
	Mesh sizing name - TunnelWall
	Done getting mesh sizing parameters
Getting edge discretization for body 1
	Delaundo expects 2D meshes in the x-y plane... attempting to rotate mesh through node swapping!
	Swapping z and y coordinates!
Writing delaundo control file - delaundo.ctr
	Writing out *.pts file
Reading delaundo mesh file - delaundo_CAPS.mesh
	Swapping y and z coordinates!

Writing Tecplot file ....
Tecplot expects 2D meshes in the x-y plane... attempting to rotate mesh!
Swapping z and y coordinates!
Finished writing Tecplot file


Writing SU2 file ....
SU2 expects 2D meshes in the x-y plane... attempting to rotate mesh!
Swapping z and y coordinates!
Finished writing SU2 file

Getting CFD boundary conditions
	Boundary condition name - Airfoil
	Boundary condition name - InFlow
	Boundary condition name - OutFlow
	Boundary condition name - TunnelWall
	Warning: No boundary condition specified for capsGroup 2DSlice!
	Done getting CFD boundary conditions
Warning: The su2 cfg file will be overwritten!
Write SU2 configuration file for version "Harrier (8.0.1)"


Running SU2......

-------------------------------------------------------------------------
|    ___ _   _ ___                                                      |
|   / __| | | |_  )   Release 8.0.0 "Harrier"                           |
|   \__ \ |_| |/ /                                                      |
|   |___/\___//___|   Suite (Computational Fluid Dynamics Code)         |
|                                                                       |
-------------------------------------------------------------------------
| SU2 Project Website: <a href='https://su2code.github.io'>https://su2code.github.io</a>                        |
|                                                                       |
| The SU2 Project is maintained by the SU2 Foundation                   |
| (<a href='http://su2foundation.org'>http://su2foundation.org</a>)                                            |
-------------------------------------------------------------------------
| Copyright 2012-2023, SU2 Contributors                                 |
|                                                                       |
| SU2 is free software; you can redistribute it and/or                  |
| modify it under the terms of the GNU Lesser General Public            |
| License as published by the Free Software Foundation; either          |
| version 2.1 of the License, or (at your option) any later version.    |
|                                                                       |
| SU2 is distributed in the hope that it will be useful,                |
| but WITHOUT ANY WARRANTY; without even the implied warranty of        |
| MERCHANTABILITY or FITNESS FOR A PARTICULAR PURPOSE. See the GNU      |
| Lesser General Public License for more details.                       |
|                                                                       |
| You should have received a copy of the GNU Lesser General Public      |
| License along with SU2. If not, see &lt;<a href='http://www.gnu.org/licenses/'>http://www.gnu.org/licenses/</a>&gt;.   |
-------------------------------------------------------------------------

Parsing config file for zone 0

----------------- Physical Case Definition ( Zone 0 ) -------------------
Compressible Euler equations.
Mach number: 0.4.
Angle of attack (AoA): 0 deg, and angle of sideslip (AoS): 0 deg.
No restart solution, use the values at infinity (freestream).
Dimensional simulation.
The reference area is 1 m^2.
The semi-span will be computed using the max y(3D) value.
The reference length is 1 m.
Reference origin for moment evaluation is (0, 0, 0).
Surface(s) where the force coefficients are evaluated: BC_5.

Surface(s) plotted in the output file: BC_5, BC_2.
Input mesh file name: ../delaundo/delaundo_CAPS.su2

--------------- Space Numerical Integration ( Zone 0 ) ------------------
Roe (with entropy fix = 0.001) solver for the flow inviscid terms.
Standard Roe without low-dissipation function.
Second order integration in space, with slope limiter.
Venkatakrishnan slope-limiting method, with constant: 0.05.
The reference element size is: 1. 
Gradient for upwind reconstruction: inverse-distance weighted Least-Squares.
Gradient for viscous and source terms: inverse-distance weighted Least-Squares.

--------------- Time Numerical Integration  ( Zone 0 ) ------------------
Local time stepping (steady state simulation).
Euler implicit method for the flow equations.
FGMRES is used for solving the linear system.
Using a ILU(0) preconditioning.
Convergence criteria of the linear solver: 1e-06.
Max number of linear iterations: 10.
V Multigrid Cycle, with 2 multigrid levels.
Damping factor for the residual restriction: 0.75.
Damping factor for the correction prolongation: 0.75.
No CFL adaptation.
+-------------------------------------------+
|  MG Level| Presmooth|PostSmooth|CorrectSmo|
+-------------------------------------------+
|         0|         1|         0|         0|
|         1|         2|         0|         0|
|         2|         3|         0|         0|
+-------------------------------------------+
Courant-Friedrichs-Lewy number:       10

------------------ Convergence Criteria  ( Zone 0 ) ---------------------
Maximum number of solver subiterations: 10.
Begin convergence monitoring at iteration 5.
Residual minimum value: 1e-14.
Cauchy series min. value: 1e-10.
Number of Cauchy elements: 100.
Begin windowed time average at iteration 0.

-------------------- Output Information ( Zone 0 ) ----------------------
File writing frequency: 
+------------------------------------+
|                     File| Frequency|
+------------------------------------+
|                  RESTART|       250|
|              SURFACE_CSV|       250|
|                  TECPLOT|       250|
|          SURFACE_TECPLOT|       250|
+------------------------------------+
Writing the convergence history file every 1 inner iterations.
Writing the screen convergence history every 1 inner iterations.
The tabular file format is CSV (.csv).
Convergence history file name: history.
Forces breakdown file name: forces_breakdown_su2_CAPS.dat.
Surface file name: surface_flow_su2_CAPS.
Volume file name: flow_su2_CAPS.
Restart file name: restart_flow_su2_CAPS.dat.

------------- Config File Boundary Information ( Zone 0 ) ---------------
+-----------------------------------------------------------------------+
|                        Marker Type|                        Marker Name|
+-----------------------------------------------------------------------+
|                         Euler wall|                               BC_5|
|                                   |                               BC_2|
+-----------------------------------------------------------------------+
|                     Inlet boundary|                               BC_4|
+-----------------------------------------------------------------------+
|                    Outlet boundary|                               BC_3|
+-----------------------------------------------------------------------+

-------------------- Output Preprocessing ( Zone 0 ) --------------------

WARNING: SURFACE_PRESSURE_DROP can only be computed for at least 2 surfaces (outlet, inlet, ...)

Screen output fields: TIME_ITER, OUTER_ITER, INNER_ITER, CUR_TIME, TIME_STEP, WALL_TIME, RMS_DENSITY, RMS_MOMENTUM-X, RMS_MOMENTUM-Y, RMS_ENERGY, EFFICIENCY
History output group(s): ITER, TIME_DOMAIN, WALL_TIME, RMS_RES, AERO_COEFF
Convergence field(s): RMS_DENSITY
Warning: No (valid) fields chosen for time convergence monitoring. Time convergence monitoring inactive.
Volume output fields: COORDINATES, SOLUTION, PRIMITIVE

------------------- Geometry Preprocessing ( Zone 0 ) -------------------
Two dimensional problem.
6317 grid points.
12340 volume elements.
5 surface markers.
24 boundary elements in index 0 (Marker = BC_2).
24 boundary elements in index 1 (Marker = BC_3).
24 boundary elements in index 2 (Marker = BC_2).
24 boundary elements in index 3 (Marker = BC_4).
198 boundary elements in index 4 (Marker = BC_5).
12340 triangles.
Setting point connectivity.
Renumbering points (Reverse Cuthill McKee Ordering).
Recomputing point connectivity.
Setting element connectivity.
Checking the numerical grid orientation.
All volume elements are correctly orientend.
There has been a re-orientation of 294 LINE surface elements.
Identifying edges and vertices.
Setting the control volume structure.
Area of the computational grid: 999.917.
Searching for the closest normal neighbors to the surfaces.
Storing a mapping from global to local point index.
Compute the surface curvature.
Max K: 1792.95. Mean K: 10.8142. Standard deviation K: 104.33.
Checking for periodicity.
Computing mesh quality statistics for the dual control volumes.
+--------------------------------------------------------------+
|           Mesh Quality Metric|        Minimum|        Maximum|
+--------------------------------------------------------------+
|    Orthogonality Angle (deg.)|        45.3524|        89.2595|
|     CV Face Area Aspect Ratio|        1.03245|        15.7138|
|           CV Sub-Volume Ratio|              1|        7.93643|
+--------------------------------------------------------------+
Setting the multigrid structure.
+-------------------------------------------+
|  MG Level|       CVs|Aggl. Rate|       CFL|
+-------------------------------------------+
|         0|      6317|    1/1.00|        10|
|         1|      1792|    1/3.53|   7.98923|
|         2|       509|    1/3.52|   6.38684|
+-------------------------------------------+
Finding max control volume width.
Wetted area = 2.07206 m.
Area projection in the x-plane = 0.179342 m, y-plane = 1.00053 m.
Max. coordinate in the x-direction = 1 m, y-direction = 0.138492 m.
Min. coordinate in the x-direction = -0.00104578 m, y-direction = -0.0151891 m.
Checking if Euler &amp; Symmetry markers are straight/plane:
Boundary marker BC_5 is NOT a single straight.
Boundary marker BC_2 is a single straight.
Computing wall distances.

-------------------- Solver Preprocessing ( Zone 0 ) --------------------
Inviscid flow: Computing density based on free-stream
temperature and pressure using the ideal gas law.
Force coefficients computed using free-stream values.

-- Models:
+------------------------------------------------------------------------------+
|          Viscosity Model|        Conductivity Model|              Fluid Model|
+------------------------------------------------------------------------------+
|                        -|                         -|             STANDARD_AIR|
+------------------------------------------------------------------------------+
-- Fluid properties:
+------------------------------------------------------------------------------+
|                  Name|    Dim. value|    Ref. value|      Unit|Non-dim. value|
+------------------------------------------------------------------------------+
|          Gas Constant|       287.058|             1|  N.m/kg.K|       287.058|
|      Spec. Heat Ratio|             -|             -|         -|           1.4|
+------------------------------------------------------------------------------+
-- Initial and free-stream conditions:
+------------------------------------------------------------------------------+
|                  Name|    Dim. value|    Ref. value|      Unit|Non-dim. value|
+------------------------------------------------------------------------------+
|       Static Pressure|        101325|             1|        Pa|        101325|
|               Density|       1.22498|             1|    kg/m^3|       1.22498|
|           Temperature|        288.15|             1|         K|        288.15|
|          Total Energy|        216054|             1|   m^2/s^2|        216054|
|            Velocity-X|       136.119|             1|       m/s|       136.119|
|            Velocity-Y|             0|             1|       m/s|             0|
|    Velocity Magnitude|       136.119|             1|       m/s|       136.119|
+------------------------------------------------------------------------------+
|           Mach Number|             -|             -|         -|           0.4|
+------------------------------------------------------------------------------+
Initialize Jacobian structure (Euler). MG level: 0.
Initialize Jacobian structure (Euler). MG level: 1.
Initialize Jacobian structure (Euler). MG level: 2.

------------------- Numerics Preprocessing ( Zone 0 ) -------------------

----------------- Integration Preprocessing ( Zone 0 ) ------------------

------------------- Iteration Preprocessing ( Zone 0 ) ------------------
Euler/Navier-Stokes/RANS fluid iteration.

------------------------------ Begin Solver -----------------------------

Simulation Run using the Single-zone Driver
WARNING: SU2 was not compiled for an AVX-capable architecture. Performance could be better,
         see <a href='https://su2code.github.io/docs_v7/Build-SU2-Linux-MacOS/#compiler-optimizations'>https://su2code.github.io/docs_v7/Build-SU2-Linux-MacOS/#compiler-optimizations</a>
WARNING: SU2 was not compiled for an AVX-capable architecture. Performance could be better,
         see <a href='https://su2code.github.io/docs_v7/Build-SU2-Linux-MacOS/#compiler-optimizations'>https://su2code.github.io/docs_v7/Build-SU2-Linux-MacOS/#compiler-optimizations</a>
WARNING: SU2 was not compiled for an AVX-capable architecture. Performance could be better,
         see <a href='https://su2code.github.io/docs_v7/Build-SU2-Linux-MacOS/#compiler-optimizations'>https://su2code.github.io/docs_v7/Build-SU2-Linux-MacOS/#compiler-optimizations</a>
+----------------------------------------------------------------------------------------------------------------------------------------------+
|   Time_Iter|  Outer_Iter|  Inner_Iter|    Cur_Time|   Time_Step|   Time(sec)|    rms[Rho]|   rms[RhoU]|   rms[RhoV]|   rms[RhoE]|        CEff|
+----------------------------------------------------------------------------------------------------------------------------------------------+
|           0|           0|           0|  0.0000e+00|  0.0000e+00|  3.5159e-02|   -1.163068|    1.073873|    1.341547|    4.312268|    0.062082|
|           0|           0|           1|  0.0000e+00|  0.0000e+00|  3.4608e-02|   -1.558471|    0.813117|    0.969484|    3.926501|    0.143132|
|           0|           0|           2|  0.0000e+00|  0.0000e+00|  3.4381e-02|   -1.599269|    0.950037|    1.012154|    3.879885|    0.386300|
|           0|           0|           3|  0.0000e+00|  0.0000e+00|  3.4018e-02|   -1.661284|    1.005970|    1.023067|    3.797319|    0.981260|
|           0|           0|           4|  0.0000e+00|  0.0000e+00|  3.3884e-02|   -1.658421|    1.009907|    0.965279|    3.792658|    2.399755|
|           0|           0|           5|  0.0000e+00|  0.0000e+00|  3.3757e-02|   -1.630602|    0.996801|    0.859556|    3.833204|    6.390579|
|           0|           0|           6|  0.0000e+00|  0.0000e+00|  3.3659e-02|   -1.628009|    1.002770|    0.822847|    3.846297|   27.872536|
|           0|           0|           7|  0.0000e+00|  0.0000e+00|  3.3579e-02|   -1.646113|    1.024424|    0.882502|    3.830202|  -48.293527|
|           0|           0|           8|  0.0000e+00|  0.0000e+00|  3.3516e-02|   -1.672152|    1.033657|    0.939200|    3.797228|  -22.113788|
|           0|           0|           9|  0.0000e+00|  0.0000e+00|  3.3458e-02|   -1.695131|    1.018255|    0.944150|    3.765919|  -19.281368|

----------------------------- Solver Exit -------------------------------

Maximum number of iterations reached (ITER = 10) before convergence.
+-----------------------------------------------------------------------+
|      Convergence Field     |     Value    |   Criterion  |  Converged |
+-----------------------------------------------------------------------+
|                    rms[Rho]|      -1.69513|         &lt; -14|          No|
+-----------------------------------------------------------------------+
-------------------------------------------------------------------------
+-----------------------------------------------------------------------+
|        File Writing Summary       |              Filename             |
+-----------------------------------------------------------------------+
|SU2 binary restart                 |restart_flow_su2_CAPS.dat          |

Writing the forces breakdown file (forces_breakdown_su2_CAPS.dat).
|CSV file                           |surface_flow_su2_CAPS.csv          |

Writing the forces breakdown file (forces_breakdown_su2_CAPS.dat).
|Tecplot binary                     |flow_su2_CAPS.szplt                |

Writing the forces breakdown file (forces_breakdown_su2_CAPS.dat).
|Tecplot binary surface             |surface_flow_su2_CAPS.szplt        |
Error in tecFileWriterClose: Not all node map values for zone 1 have been written.
Currently need 492 more values.0: Error finishing Tecplot file output.

Writing the forces breakdown file (forces_breakdown_su2_CAPS.dat).
+-----------------------------------------------------------------------+

--------------------------- Finalizing Solver ---------------------------
Deleted CNumerics container.
Deleted CIntegration container.
Deleted CSolver container.
Deleted CIteration container.
Deleted CInterface container.
Deleted CGeometry container.
Deleted CFreeFormDefBox class.
Deleted CSurfaceMovement class.
Deleted CVolumetricMovement class.
Deleted CConfig container.
Deleted nInst container.
Deleted COutput class.
-------------------------------------------------------------------------

------------------------- Exit Success (SU2_CFD) ------------------------

Total Force - Pressure + Viscous
Cl =  0.805707 Cd =  -0.041787
Cmz =  0.408515
Cx =  -0.041787 Cy =  0.805707
Pressure Contribution
Cl_p =  0.805707 Cd_p =  -0.041787
Cmz_p =  0.408515
Cx_p =  -0.041787 Cy_p =  0.805707
Viscous Contribution
Cl_v =  0.0 Cd_v =  0.0
Cmz_v =  0.0
Cx_v =  0.0 Cy_v =  0.0

real	0m1.029s
user	0m1.143s
sys	0m0.452s
+ status=0
+ set +x

=================================================
CAPS verification (using pyCAPS) case su2_and_Delaundo_PyTest.py passed (as expected)
=================================================


=================================================
+ echo 'su2_and_Tetgen_PyTest.py test;'
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESP126/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
su2_and_Tetgen_PyTest.py test;
+ python -u su2_and_Tetgen_PyTest.py -outLevel=0
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESP126/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 3
	Name = Wing1, index = 1
	Name = Wing2, index = 2
	Name = Farfield, index = 3
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 3
	Name = Wing1, index = 1
	Name = Wing2, index = 2
	Name = Farfield, index = 3
Getting surface mesh for body 1 (of 3)
Getting surface mesh for body 2 (of 3)
Getting surface mesh for body 3 (of 3)
Body 1 (of 3)
Number of nodes    = 2236
Number of elements = 4468
Number of triangle elements      = 4468
Number of quadrilateral elements = 0
Body 2 (of 3)
Number of nodes    = 636
Number of elements = 1268
Number of triangle elements      = 1268
Number of quadrilateral elements = 0
Body 3 (of 3)
Number of nodes    = 258
Number of elements = 512
Number of triangle elements      = 512
Number of quadrilateral elements = 0
----------------------------
Total number of nodes    = 3130
Total number of elements = 6248

Writing Tecplot file ....
Finished writing Tecplot file

Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 3
	Name = Wing1, index = 1
	Name = Wing2, index = 2
	Name = Farfield, index = 3
Number of surface: nodes - 3130, elements - 6248
Getting volume mesh

Generating volume mesh using TetGen.....

Tetgen input string = pYq1.500/0.000T1.00e-16A
Delaunizing vertices...
Delaunay seconds:  0.012926
Creating surface mesh ...
Surface mesh seconds:  0.00172
Recovering boundaries...
Boundary recovery seconds:  0.03339
Removing exterior tetrahedra ...
Spreading region attributes.
Exterior tets removal seconds:  0.00234
Suppressing Steiner points ...
Steiner suppression seconds:  6e-06
Recovering Delaunayness...
Delaunay recovery seconds:  0.004903
Refining mesh...
  4180 insertions, added 2142 points, 134947 tetrahedra in queue.
  1391 insertions, added 431 points, 139550 tetrahedra in queue.
  1855 insertions, added 477 points, 138154 tetrahedra in queue.
  2472 insertions, added 613 points, 122807 tetrahedra in queue.
  3296 insertions, added 507 points, 67228 tetrahedra in queue.
  4393 insertions, added 431 points, 1310 tetrahedra in queue.
Refinement seconds:  0.285763
Smoothing vertices...
Mesh smoothing seconds:  0.182626
Improving mesh...
Mesh improvement seconds:  0.006148
Jettisoning redundant points.

Writing nodes.
Writing elements.
Writing faces.
Writing edges.

Output seconds:  0.00056
Total running seconds:  0.530502

Statistics:

  Input points: 3130
  Input facets: 6248
  Input segments: 9372
  Input holes: 2
  Input regions: 0

  Mesh points: 8227
  Mesh tetrahedra: 40661
  Mesh faces: 84447
  Mesh faces on exterior boundary: 6250
  Mesh faces on input facets: 6250
  Mesh edges on input segments: 9373
  Steiner points on input segments:  1
  Steiner points inside domain: 5096

Done meshing using TetGen!
Volume mesher did not preserve surface elements - data transfer will NOT be possible.

Writing SU2 file ....
Finished writing SU2 file

Getting CFD boundary conditions
	Boundary condition name - Farfield
	Boundary condition name - Wing1
	Boundary condition name - Wing2
	Done getting CFD boundary conditions
Warning: The su2 cfg file will be overwritten!
Write SU2 configuration file for version "Harrier (8.0.1)"


Running SU2......

-------------------------------------------------------------------------
|    ___ _   _ ___                                                      |
|   / __| | | |_  )   Release 8.0.0 "Harrier"                           |
|   \__ \ |_| |/ /                                                      |
|   |___/\___//___|   Suite (Computational Fluid Dynamics Code)         |
|                                                                       |
-------------------------------------------------------------------------
| SU2 Project Website: <a href='https://su2code.github.io'>https://su2code.github.io</a>                        |
|                                                                       |
| The SU2 Project is maintained by the SU2 Foundation                   |
| (<a href='http://su2foundation.org'>http://su2foundation.org</a>)                                            |
-------------------------------------------------------------------------
| Copyright 2012-2023, SU2 Contributors                                 |
|                                                                       |
| SU2 is free software; you can redistribute it and/or                  |
| modify it under the terms of the GNU Lesser General Public            |
| License as published by the Free Software Foundation; either          |
| version 2.1 of the License, or (at your option) any later version.    |
|                                                                       |
| SU2 is distributed in the hope that it will be useful,                |
| but WITHOUT ANY WARRANTY; without even the implied warranty of        |
| MERCHANTABILITY or FITNESS FOR A PARTICULAR PURPOSE. See the GNU      |
| Lesser General Public License for more details.                       |
|                                                                       |
| You should have received a copy of the GNU Lesser General Public      |
| License along with SU2. If not, see &lt;<a href='http://www.gnu.org/licenses/'>http://www.gnu.org/licenses/</a>&gt;.   |
-------------------------------------------------------------------------

Parsing config file for zone 0

----------------- Physical Case Definition ( Zone 0 ) -------------------
Compressible Euler equations.
Mach number: 0.5901.
Angle of attack (AoA): 1 deg, and angle of sideslip (AoS): 0 deg.
No restart solution, use the values at infinity (freestream).
Dimensional simulation.
The reference area is 50 m^2.
The semi-span will be computed using the max y(3D) value.
The reference length is 15.8114 m.
Surface(s) where the force coefficients are evaluated and 
their reference origin for moment computation: 
   - BC_1 (0, 0, 0).
   - BC_2 (0, 0, 0) m.
Surface(s) plotted in the output file: BC_1, BC_2.
Input mesh file name: ../myMesh/tetgen_CAPS.su2

--------------- Space Numerical Integration ( Zone 0 ) ------------------
Roe (with entropy fix = 0.001) solver for the flow inviscid terms.
Standard Roe without low-dissipation function.
Second order integration in space, with slope limiter.
Venkatakrishnan slope-limiting method, with constant: 0.05.
The reference element size is: 1. 
Gradient for upwind reconstruction: inverse-distance weighted Least-Squares.
Gradient for viscous and source terms: inverse-distance weighted Least-Squares.

--------------- Time Numerical Integration  ( Zone 0 ) ------------------
Local time stepping (steady state simulation).
Euler implicit method for the flow equations.
FGMRES is used for solving the linear system.
Using a ILU(0) preconditioning.
Convergence criteria of the linear solver: 1e-06.
Max number of linear iterations: 10.
V Multigrid Cycle, with 2 multigrid levels.
Damping factor for the residual restriction: 0.75.
Damping factor for the correction prolongation: 0.75.
No CFL adaptation.
+-------------------------------------------+
|  MG Level| Presmooth|PostSmooth|CorrectSmo|
+-------------------------------------------+
|         0|         1|         0|         0|
|         1|         2|         0|         0|
|         2|         3|         0|         0|
+-------------------------------------------+
Courant-Friedrichs-Lewy number:       10

------------------ Convergence Criteria  ( Zone 0 ) ---------------------
Maximum number of solver subiterations: 5.
Begin convergence monitoring at iteration 5.
Residual minimum value: 1e-14.
Cauchy series min. value: 1e-10.
Number of Cauchy elements: 100.
Begin windowed time average at iteration 0.

-------------------- Output Information ( Zone 0 ) ----------------------
File writing frequency: 
+------------------------------------+
|                     File| Frequency|
+------------------------------------+
|                  RESTART|       250|
|              SURFACE_CSV|       250|
|                 PARAVIEW|       250|
|         SURFACE_PARAVIEW|       250|
+------------------------------------+
Writing the convergence history file every 1 inner iterations.
Writing the screen convergence history every 1 inner iterations.
The tabular file format is CSV (.csv).
Convergence history file name: history.
Forces breakdown file name: forces_breakdown_pyCAPS_SU2_Tetgen.dat.
Surface file name: surface_flow_pyCAPS_SU2_Tetgen.
Volume file name: flow_pyCAPS_SU2_Tetgen.
Restart file name: restart_flow_pyCAPS_SU2_Tetgen.dat.

------------- Config File Boundary Information ( Zone 0 ) ---------------
+-----------------------------------------------------------------------+
|                        Marker Type|                        Marker Name|
+-----------------------------------------------------------------------+
|                         Euler wall|                               BC_1|
|                                   |                               BC_2|
+-----------------------------------------------------------------------+
|                          Far-field|                               BC_3|
+-----------------------------------------------------------------------+

-------------------- Output Preprocessing ( Zone 0 ) --------------------

WARNING: SURFACE_PRESSURE_DROP can only be computed for at least 2 surfaces (outlet, inlet, ...)

Screen output fields: TIME_ITER, OUTER_ITER, INNER_ITER, CUR_TIME, TIME_STEP, WALL_TIME, RMS_DENSITY, RMS_MOMENTUM-X, RMS_MOMENTUM-Y, RMS_ENERGY, EFFICIENCY
History output group(s): ITER, TIME_DOMAIN, WALL_TIME, RMS_RES, AERO_COEFF
Convergence field(s): RMS_DENSITY
Warning: No (valid) fields chosen for time convergence monitoring. Time convergence monitoring inactive.
Volume output fields: COORDINATES, SOLUTION, PRIMITIVE

------------------- Geometry Preprocessing ( Zone 0 ) -------------------
Three dimensional problem.
8227 grid points.
40661 volume elements.
3 surface markers.
4468 boundary elements in index 0 (Marker = BC_1).
1270 boundary elements in index 1 (Marker = BC_2).
512 boundary elements in index 2 (Marker = BC_3).
40661 tetrahedra.
Setting point connectivity.
Renumbering points (Reverse Cuthill McKee Ordering).
Recomputing point connectivity.
Setting element connectivity.
Checking the numerical grid orientation.
All volume elements are correctly orientend.
All surface elements are correctly orientend.
Identifying edges and vertices.
Setting the control volume structure.
Volume of the computational grid: 2.08741e+06.
Searching for the closest normal neighbors to the surfaces.
Storing a mapping from global to local point index.
Compute the surface curvature.
Max K: 414.134. Mean K: 30.6158. Standard deviation K: 37.5195.
Checking for periodicity.
Computing mesh quality statistics for the dual control volumes.
+--------------------------------------------------------------+
|           Mesh Quality Metric|        Minimum|        Maximum|
+--------------------------------------------------------------+
|    Orthogonality Angle (deg.)|        2.25569|         83.562|
|     CV Face Area Aspect Ratio|        1.40614|        7154.17|
|           CV Sub-Volume Ratio|        1.02596|         261709|
+--------------------------------------------------------------+
Setting the multigrid structure.
+-------------------------------------------+
|  MG Level|       CVs|Aggl. Rate|       CFL|
+-------------------------------------------+
|         0|      8227|    1/1.00|        10|
|         1|      1360|    1/6.05|   8.23235|
|         2|       235|    1/5.79|   6.87793|
+-------------------------------------------+
Finding max control volume width.
Semi-span length = 7.90569 m.
Wetted area = 120.046 m^2.
Area projection in the x-plane = 10.7914 m^2, y-plane = 4.5843 m^2, z-plane = 57.287 m^2.
Max. coordinate in the x-direction = 12.6407 m, y-direction = 7.90569 m, z-direction = 0.557773 m.
Min. coordinate in the x-direction = -0.00409054 m, y-direction = -7.90569 m, z-direction = -0.41192 m.
Checking if Euler &amp; Symmetry markers are straight/plane:
Boundary marker BC_1 is NOT a single plane.
Boundary marker BC_2 is NOT a single plane.
Computing wall distances.

-------------------- Solver Preprocessing ( Zone 0 ) --------------------
Inviscid flow: Computing density based on free-stream
temperature and pressure using the ideal gas law.
Force coefficients computed using free-stream values.

-- Models:
+------------------------------------------------------------------------------+
|          Viscosity Model|        Conductivity Model|              Fluid Model|
+------------------------------------------------------------------------------+
|                        -|                         -|             STANDARD_AIR|
+------------------------------------------------------------------------------+
-- Fluid properties:
+------------------------------------------------------------------------------+
|                  Name|    Dim. value|    Ref. value|      Unit|Non-dim. value|
+------------------------------------------------------------------------------+
|          Gas Constant|       287.058|             1|  N.m/kg.K|       287.058|
|      Spec. Heat Ratio|             -|             -|         -|           1.4|
+------------------------------------------------------------------------------+
-- Initial and free-stream conditions:
+------------------------------------------------------------------------------+
|                  Name|    Dim. value|    Ref. value|      Unit|Non-dim. value|
+------------------------------------------------------------------------------+
|       Static Pressure|        101325|             1|        Pa|        101325|
|               Density|       1.22498|             1|    kg/m^3|       1.22498|
|           Temperature|        288.15|             1|         K|        288.15|
|          Total Energy|        226952|             1|   m^2/s^2|        226952|
|            Velocity-X|       200.779|             1|       m/s|       200.779|
|            Velocity-Y|             0|             1|       m/s|             0|
|            Velocity-Z|       3.50461|             1|       m/s|       3.50461|
|    Velocity Magnitude|       200.809|             1|       m/s|       200.809|
+------------------------------------------------------------------------------+
|           Mach Number|             -|             -|         -|        0.5901|
+------------------------------------------------------------------------------+
Initialize Jacobian structure (Euler). MG level: 0.
Initialize Jacobian structure (Euler). MG level: 1.
Initialize Jacobian structure (Euler). MG level: 2.

------------------- Numerics Preprocessing ( Zone 0 ) -------------------

----------------- Integration Preprocessing ( Zone 0 ) ------------------

------------------- Iteration Preprocessing ( Zone 0 ) ------------------
Euler/Navier-Stokes/RANS fluid iteration.

------------------------------ Begin Solver -----------------------------

Simulation Run using the Single-zone Driver
WARNING: SU2 was not compiled for an AVX-capable architecture. Performance could be better,
         see <a href='https://su2code.github.io/docs_v7/Build-SU2-Linux-MacOS/#compiler-optimizations'>https://su2code.github.io/docs_v7/Build-SU2-Linux-MacOS/#compiler-optimizations</a>
WARNING: SU2 was not compiled for an AVX-capable architecture. Performance could be better,
         see <a href='https://su2code.github.io/docs_v7/Build-SU2-Linux-MacOS/#compiler-optimizations'>https://su2code.github.io/docs_v7/Build-SU2-Linux-MacOS/#compiler-optimizations</a>
WARNING: SU2 was not compiled for an AVX-capable architecture. Performance could be better,
         see <a href='https://su2code.github.io/docs_v7/Build-SU2-Linux-MacOS/#compiler-optimizations'>https://su2code.github.io/docs_v7/Build-SU2-Linux-MacOS/#compiler-optimizations</a>
+----------------------------------------------------------------------------------------------------------------------------------------------+
|   Time_Iter|  Outer_Iter|  Inner_Iter|    Cur_Time|   Time_Step|   Time(sec)|    rms[Rho]|   rms[RhoU]|   rms[RhoV]|   rms[RhoE]|        CEff|
+----------------------------------------------------------------------------------------------------------------------------------------------+
|           0|           0|           0|  0.0000e+00|  0.0000e+00|  1.0810e-01|    0.614349|    3.046325|    2.089422|    6.105244|    1.831854|
|           0|           0|           1|  0.0000e+00|  0.0000e+00|  1.0697e-01|    0.764583|    3.258604|    2.974732|    6.265552|    2.165840|
|           0|           0|           2|  0.0000e+00|  0.0000e+00|  1.0656e-01|    0.642409|    3.278261|    3.214494|    6.139447|    3.169947|
|           0|           0|           3|  0.0000e+00|  0.0000e+00|  1.0628e-01|    0.541917|    3.250446|    3.272037|    6.028748|    4.533401|
|           0|           0|           4|  0.0000e+00|  0.0000e+00|  1.0610e-01|    0.535101|    3.187480|    3.218588|    6.011712|    5.728616|

----------------------------- Solver Exit -------------------------------

Maximum number of iterations reached (ITER = 5) before convergence.
+-----------------------------------------------------------------------+
|      Convergence Field     |     Value    |   Criterion  |  Converged |
+-----------------------------------------------------------------------+
|                    rms[Rho]|      0.535101|         &lt; -14|          No|
+-----------------------------------------------------------------------+
-------------------------------------------------------------------------
+-----------------------------------------------------------------------+
|        File Writing Summary       |              Filename             |
+-----------------------------------------------------------------------+
|SU2 binary restart                 |restart_flow_pyCAPS_SU2_Tetgen.dat |

Writing the forces breakdown file (forces_breakdown_pyCAPS_SU2_Tetgen.dat).
|CSV file                           |surface_flow_pyCAPS_SU2_Tetgen.csv |

Writing the forces breakdown file (forces_breakdown_pyCAPS_SU2_Tetgen.dat).
|Paraview                           |flow_pyCAPS_SU2_Tetgen.vtu         |

Writing the forces breakdown file (forces_breakdown_pyCAPS_SU2_Tetgen.dat).
|Paraview surface                   |surface_flow_pyCAPS_SU2_Tetgen.vtu |

Writing the forces breakdown file (forces_breakdown_pyCAPS_SU2_Tetgen.dat).
+-----------------------------------------------------------------------+

--------------------------- Finalizing Solver ---------------------------
Deleted CNumerics container.
Deleted CIntegration container.
Deleted CSolver container.
Deleted CIteration container.
Deleted CInterface container.
Deleted CGeometry container.
Deleted CFreeFormDefBox class.
Deleted CSurfaceMovement class.
Deleted CVolumetricMovement class.
Deleted CConfig container.
Deleted nInst container.
Deleted COutput class.
-------------------------------------------------------------------------

------------------------- Exit Success (SU2_CFD) ------------------------

Total Force - Pressure + Viscous
Cl =  0.763097 Cd =  0.133208
Cmx =  -0.004493 Cmy =  -0.215511 Cmz =  0.000816
Cx =  0.11987 Cy =  0.0005 Cz =  0.765306

real	0m2.653s
user	0m2.796s
sys	0m0.255s
+ status=0
+ set +x

=================================================
CAPS verification (using pyCAPS) case su2_and_Tetgen_PyTest.py passed (as expected)
=================================================


=================================================
+ echo 'su2_X43a_PyTest.py test;'
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESP126/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
su2_X43a_PyTest.py test;
+ python -u su2_X43a_PyTest.py -outLevel=0
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESP126/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 7
	Name = fuselage, index = 1
	Name = verticalCS, index = 2
	Name = fuselage_base, index = 3
	Name = horizontalCS, index = 4
	Name = inlet, index = 5
	Name = hollowInlet, index = 6
	Name = Farfield, index = 7
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 0
Getting surface mesh for body 1 (of 2)
Getting surface mesh for body 2 (of 2)
Body 1 (of 2)
Number of nodes    = 3808
Number of elements = 7616
Number of triangle elements      = 7616
Number of quadrilateral elements = 0
Body 2 (of 2)
Number of nodes    = 5678
Number of elements = 11352
Number of triangle elements      = 11352
Number of quadrilateral elements = 0
----------------------------
Total number of nodes    = 9486
Total number of elements = 18968

Writing Tecplot file ....
Finished writing Tecplot file

Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 7
	Name = fuselage, index = 1
	Name = verticalCS, index = 2
	Name = fuselage_base, index = 3
	Name = horizontalCS, index = 4
	Name = inlet, index = 5
	Name = hollowInlet, index = 6
	Name = Farfield, index = 7
Number of surface: nodes - 9486, elements - 18968
Getting volume mesh

Generating volume mesh using TetGen.....

Tetgen input string = pYq1.500/0.000T1.00e-16A
Delaunizing vertices...
Delaunay seconds:  0.03305
Creating surface mesh ...
Surface mesh seconds:  0.006547
Recovering boundaries...
Warning:  2 segments are not recovered.
Boundary recovery seconds:  0.101178
Removing exterior tetrahedra ...
Spreading region attributes.
Exterior tets removal seconds:  0.005628
Suppressing Steiner points ...
Steiner suppression seconds:  8e-06
Recovering Delaunayness...
Delaunay recovery seconds:  0.014486
Refining mesh...
  12647 insertions, added 5230 points, 2965 tetrahedra in queue.
Refinement seconds:  0.302775
Smoothing vertices...
Mesh smoothing seconds:  0.241869
Improving mesh...
Mesh improvement seconds:  0.009977
Jettisoning redundant points.

Writing nodes.
Writing elements.
Writing faces.
Writing edges.

Output seconds:  0.001853
Total running seconds:  0.717613

Statistics:

  Input points: 9486
  Input facets: 18968
  Input segments: 28452
  Input holes: 6
  Input regions: 0

  Mesh points: 14837
  Mesh tetrahedra: 61060
  Mesh faces: 131604
  Mesh faces on exterior boundary: 18968
  Mesh faces on input facets: 18968
  Mesh edges on input segments: 28452
  Steiner points inside domain: 5351

Done meshing using TetGen!

Writing SU2 file ....
Finished writing SU2 file

Getting CFD boundary conditions
	Boundary condition name - Farfield
	Boundary condition name - fuselage
	Boundary condition name - fuselage_base
	Boundary condition name - hollowInlet
	Boundary condition name - horizontalCS
	Boundary condition name - inlet
	Boundary condition name - verticalCS
	Done getting CFD boundary conditions
Writing boundary flags
 - bcProps.surfaceProp[0].surfaceType = 3
 - bcProps.surfaceProp[1].surfaceType = 1
 - bcProps.surfaceProp[2].surfaceType = 1
 - bcProps.surfaceProp[3].surfaceType = 1
 - bcProps.surfaceProp[4].surfaceType = 1
 - bcProps.surfaceProp[5].surfaceType = 1
 - bcProps.surfaceProp[6].surfaceType = 1
Done boundary flags
Warning: The su2 cfg file will be overwritten!
Write SU2 configuration file for version "Harrier (8.0.1)"


Running SU2......

-------------------------------------------------------------------------
|    ___ _   _ ___                                                      |
|   / __| | | |_  )   Release 8.0.0 "Harrier"                           |
|   \__ \ |_| |/ /                                                      |
|   |___/\___//___|   Suite (Computational Fluid Dynamics Code)         |
|                                                                       |
-------------------------------------------------------------------------
| SU2 Project Website: <a href='https://su2code.github.io'>https://su2code.github.io</a>                        |
|                                                                       |
| The SU2 Project is maintained by the SU2 Foundation                   |
| (<a href='http://su2foundation.org'>http://su2foundation.org</a>)                                            |
-------------------------------------------------------------------------
| Copyright 2012-2023, SU2 Contributors                                 |
|                                                                       |
| SU2 is free software; you can redistribute it and/or                  |
| modify it under the terms of the GNU Lesser General Public            |
| License as published by the Free Software Foundation; either          |
| version 2.1 of the License, or (at your option) any later version.    |
|                                                                       |
| SU2 is distributed in the hope that it will be useful,                |
| but WITHOUT ANY WARRANTY; without even the implied warranty of        |
| MERCHANTABILITY or FITNESS FOR A PARTICULAR PURPOSE. See the GNU      |
| Lesser General Public License for more details.                       |
|                                                                       |
| You should have received a copy of the GNU Lesser General Public      |
| License along with SU2. If not, see &lt;<a href='http://www.gnu.org/licenses/'>http://www.gnu.org/licenses/</a>&gt;.   |
-------------------------------------------------------------------------

Parsing config file for zone 0

----------------- Physical Case Definition ( Zone 0 ) -------------------
Compressible Euler equations.
Mach number: 3.5.
Angle of attack (AoA): 3 deg, and angle of sideslip (AoS): 0 deg.
No restart solution, use the values at infinity (freestream).
Dimensional simulation.
The reference area is 1 m^2.
The semi-span will be computed using the max y(3D) value.
The reference length is 1 m.
Surface(s) where the force coefficients are evaluated and 
their reference origin for moment computation: 
   - BC_1 (0, 0, 0).
   - BC_3 (0, 0, 0).
   - BC_4 (0, 0, 0).
   - BC_2 (0, 0, 0).
   - BC_5 (0, 0, 0).
   - BC_6 (0, 0, 0) m.
Surface(s) plotted in the output file: BC_1, BC_3, BC_6, BC_4, BC_5, BC_2.
Input mesh file name: ../myMesh/tetgen_CAPS.su2

--------------- Space Numerical Integration ( Zone 0 ) ------------------
Roe (with entropy fix = 0.001) solver for the flow inviscid terms.
Standard Roe without low-dissipation function.
Second order integration in space, with slope limiter.
Venkatakrishnan slope-limiting method, with constant: 0.05.
The reference element size is: 1. 
Gradient for upwind reconstruction: inverse-distance weighted Least-Squares.
Gradient for viscous and source terms: inverse-distance weighted Least-Squares.

--------------- Time Numerical Integration  ( Zone 0 ) ------------------
Local time stepping (steady state simulation).
Euler implicit method for the flow equations.
FGMRES is used for solving the linear system.
Using a ILU(0) preconditioning.
Convergence criteria of the linear solver: 1e-06.
Max number of linear iterations: 10.
V Multigrid Cycle, with 2 multigrid levels.
Damping factor for the residual restriction: 0.75.
Damping factor for the correction prolongation: 0.75.
No CFL adaptation.
+-------------------------------------------+
|  MG Level| Presmooth|PostSmooth|CorrectSmo|
+-------------------------------------------+
|         0|         1|         0|         0|
|         1|         2|         0|         0|
|         2|         3|         0|         0|
+-------------------------------------------+
Courant-Friedrichs-Lewy number:       10

------------------ Convergence Criteria  ( Zone 0 ) ---------------------
Maximum number of solver subiterations: 5.
Begin convergence monitoring at iteration 5.
Residual minimum value: 1e-14.
Cauchy series min. value: 1e-10.
Number of Cauchy elements: 100.
Begin windowed time average at iteration 0.

-------------------- Output Information ( Zone 0 ) ----------------------
File writing frequency: 
+------------------------------------+
|                     File| Frequency|
+------------------------------------+
|                  RESTART|       250|
|              SURFACE_CSV|       250|
|                 PARAVIEW|       250|
|         SURFACE_PARAVIEW|       250|
+------------------------------------+
Writing the convergence history file every 1 inner iterations.
Writing the screen convergence history every 1 inner iterations.
The tabular file format is CSV (.csv).
Convergence history file name: history.
Forces breakdown file name: forces_breakdown_x43a_Test.dat.
Surface file name: surface_flow_x43a_Test.
Volume file name: flow_x43a_Test.
Restart file name: restart_flow_x43a_Test.dat.

------------- Config File Boundary Information ( Zone 0 ) ---------------
+-----------------------------------------------------------------------+
|                        Marker Type|                        Marker Name|
+-----------------------------------------------------------------------+
|                         Euler wall|                               BC_1|
|                                   |                               BC_3|
|                                   |                               BC_6|
|                                   |                               BC_4|
|                                   |                               BC_5|
|                                   |                               BC_2|
+-----------------------------------------------------------------------+
|                          Far-field|                               BC_7|
+-----------------------------------------------------------------------+

-------------------- Output Preprocessing ( Zone 0 ) --------------------

WARNING: SURFACE_PRESSURE_DROP can only be computed for at least 2 surfaces (outlet, inlet, ...)

Screen output fields: TIME_ITER, OUTER_ITER, INNER_ITER, CUR_TIME, TIME_STEP, WALL_TIME, RMS_DENSITY, RMS_MOMENTUM-X, RMS_MOMENTUM-Y, RMS_ENERGY, EFFICIENCY
History output group(s): ITER, TIME_DOMAIN, WALL_TIME, RMS_RES, AERO_COEFF
Convergence field(s): RMS_DENSITY
Warning: No (valid) fields chosen for time convergence monitoring. Time convergence monitoring inactive.
Volume output fields: COORDINATES, SOLUTION, PRIMITIVE

------------------- Geometry Preprocessing ( Zone 0 ) -------------------
Three dimensional problem.
14837 grid points.
61060 volume elements.
7 surface markers.
4460 boundary elements in index 0 (Marker = BC_1).
1682 boundary elements in index 1 (Marker = BC_2).
92 boundary elements in index 2 (Marker = BC_3).
696 boundary elements in index 3 (Marker = BC_4).
434 boundary elements in index 4 (Marker = BC_5).
252 boundary elements in index 5 (Marker = BC_6).
11352 boundary elements in index 6 (Marker = BC_7).
61060 tetrahedra.
Setting point connectivity.
Renumbering points (Reverse Cuthill McKee Ordering).
Recomputing point connectivity.
Setting element connectivity.
Checking the numerical grid orientation.
All volume elements are correctly orientend.
All surface elements are correctly orientend.
Identifying edges and vertices.
Setting the control volume structure.
Volume of the computational grid: 2.67745e+08.
Searching for the closest normal neighbors to the surfaces.
Storing a mapping from global to local point index.
Compute the surface curvature.
Max K: 95.6599. Mean K: 0.6569. Standard deviation K: 2.74489.
Checking for periodicity.
Computing mesh quality statistics for the dual control volumes.
+--------------------------------------------------------------+
|           Mesh Quality Metric|        Minimum|        Maximum|
+--------------------------------------------------------------+
|    Orthogonality Angle (deg.)|       0.041314|        84.1309|
|     CV Face Area Aspect Ratio|        1.66509|        8739.77|
|           CV Sub-Volume Ratio|              1|    1.06812e+07|
+--------------------------------------------------------------+
Setting the multigrid structure.
+-------------------------------------------+
|  MG Level|       CVs|Aggl. Rate|       CFL|
+-------------------------------------------+
|         0|     14837|    1/1.00|        10|
|         1|      2949|    1/5.03|   8.75388|
|         2|       771|    1/3.82|   8.39625|
+-------------------------------------------+
Finding max control volume width.
Semi-span length = 30 m.
Wetted area = 13761 m^2.
Area projection in the x-plane = 776.902 m^2, y-plane = 2106.32 m^2, z-plane = 5468.8 m^2.
Max. coordinate in the x-direction = 150 m, y-direction = 30 m, z-direction = 19 m.
Min. coordinate in the x-direction = 0 m, y-direction = -30 m, z-direction = -10.3 m.
Checking if Euler &amp; Symmetry markers are straight/plane:
Boundary marker BC_1 is NOT a single plane.
Boundary marker BC_3 is a single plane.
Boundary marker BC_6 is NOT a single plane.
Boundary marker BC_4 is NOT a single plane.
Boundary marker BC_5 is NOT a single plane.
Boundary marker BC_2 is NOT a single plane.
Computing wall distances.

-------------------- Solver Preprocessing ( Zone 0 ) --------------------
Inviscid flow: Computing density based on free-stream
temperature and pressure using the ideal gas law.
Force coefficients computed using free-stream values.

-- Models:
+------------------------------------------------------------------------------+
|          Viscosity Model|        Conductivity Model|              Fluid Model|
+------------------------------------------------------------------------------+
|                        -|                         -|             STANDARD_AIR|
+------------------------------------------------------------------------------+
-- Fluid properties:
+------------------------------------------------------------------------------+
|                  Name|    Dim. value|    Ref. value|      Unit|Non-dim. value|
+------------------------------------------------------------------------------+
|          Gas Constant|       287.058|             1|  N.m/kg.K|       287.058|
|      Spec. Heat Ratio|             -|             -|         -|           1.4|
+------------------------------------------------------------------------------+
-- Initial and free-stream conditions:
+------------------------------------------------------------------------------+
|                  Name|    Dim. value|    Ref. value|      Unit|Non-dim. value|
+------------------------------------------------------------------------------+
|       Static Pressure|        101325|             1|        Pa|        101325|
|               Density|       1.22498|             1|    kg/m^3|       1.22498|
|           Temperature|        288.15|             1|         K|        288.15|
|          Total Energy|        916077|             1|   m^2/s^2|        916077|
|            Velocity-X|       1189.41|             1|       m/s|       1189.41|
|            Velocity-Y|             0|             1|       m/s|             0|
|            Velocity-Z|       62.3342|             1|       m/s|       62.3342|
|    Velocity Magnitude|       1191.04|             1|       m/s|       1191.04|
+------------------------------------------------------------------------------+
|           Mach Number|             -|             -|         -|           3.5|
+------------------------------------------------------------------------------+
Initialize Jacobian structure (Euler). MG level: 0.
Initialize Jacobian structure (Euler). MG level: 1.
Initialize Jacobian structure (Euler). MG level: 2.

------------------- Numerics Preprocessing ( Zone 0 ) -------------------

----------------- Integration Preprocessing ( Zone 0 ) ------------------

------------------- Iteration Preprocessing ( Zone 0 ) ------------------
Euler/Navier-Stokes/RANS fluid iteration.

------------------------------ Begin Solver -----------------------------

Simulation Run using the Single-zone Driver
WARNING: SU2 was not compiled for an AVX-capable architecture. Performance could be better,
         see <a href='https://su2code.github.io/docs_v7/Build-SU2-Linux-MacOS/#compiler-optimizations'>https://su2code.github.io/docs_v7/Build-SU2-Linux-MacOS/#compiler-optimizations</a>
WARNING: SU2 was not compiled for an AVX-capable architecture. Performance could be better,
         see <a href='https://su2code.github.io/docs_v7/Build-SU2-Linux-MacOS/#compiler-optimizations'>https://su2code.github.io/docs_v7/Build-SU2-Linux-MacOS/#compiler-optimizations</a>
WARNING: SU2 was not compiled for an AVX-capable architecture. Performance could be better,
         see <a href='https://su2code.github.io/docs_v7/Build-SU2-Linux-MacOS/#compiler-optimizations'>https://su2code.github.io/docs_v7/Build-SU2-Linux-MacOS/#compiler-optimizations</a>
+----------------------------------------------------------------------------------------------------------------------------------------------+
|   Time_Iter|  Outer_Iter|  Inner_Iter|    Cur_Time|   Time_Step|   Time(sec)|    rms[Rho]|   rms[RhoU]|   rms[RhoV]|   rms[RhoE]|        CEff|
+----------------------------------------------------------------------------------------------------------------------------------------------+
|           0|           0|           0|  0.0000e+00|  0.0000e+00|  2.0792e-01|    2.731580|    5.652568|    4.717779|    8.731055|   -0.598944|
|           0|           0|           1|  0.0000e+00|  0.0000e+00|  2.0660e-01|    3.160279|    6.272701|    5.760915|    9.118543|   -0.210439|
|           0|           0|           2|  0.0000e+00|  0.0000e+00|  2.0308e-01|    3.354228|    6.489942|    5.827928|    9.330964|   -0.113496|
|           0|           0|           3|  0.0000e+00|  0.0000e+00|  2.0321e-01|    3.254338|    6.351828|    5.711746|    9.239524|   -0.118542|
|           0|           0|           4|  0.0000e+00|  0.0000e+00|  2.0334e-01|    3.176424|    6.240821|    5.574708|    9.151588|   -0.137089|

----------------------------- Solver Exit -------------------------------

Maximum number of iterations reached (ITER = 5) before convergence.
+-----------------------------------------------------------------------+
|      Convergence Field     |     Value    |   Criterion  |  Converged |
+-----------------------------------------------------------------------+
|                    rms[Rho]|       3.17642|         &lt; -14|          No|
+-----------------------------------------------------------------------+
-------------------------------------------------------------------------
+-----------------------------------------------------------------------+
|        File Writing Summary       |              Filename             |
+-----------------------------------------------------------------------+
|SU2 binary restart                 |restart_flow_x43a_Test.dat         |

Writing the forces breakdown file (forces_breakdown_x43a_Test.dat).
|CSV file                           |surface_flow_x43a_Test.csv         |

Writing the forces breakdown file (forces_breakdown_x43a_Test.dat).
|Paraview                           |flow_x43a_Test.vtu                 |

Writing the forces breakdown file (forces_breakdown_x43a_Test.dat).
|Paraview surface                   |surface_flow_x43a_Test.vtu         |

Writing the forces breakdown file (forces_breakdown_x43a_Test.dat).
+-----------------------------------------------------------------------+
Warning: there are 184 non-physical points in the solution.
Warning: 87 reconstructed states for upwinding are non-physical.

--------------------------- Finalizing Solver ---------------------------
Deleted CNumerics container.
Deleted CIntegration container.
Deleted CSolver container.
Deleted CIteration container.
Deleted CInterface container.
Deleted CGeometry container.
Deleted CFreeFormDefBox class.
Deleted CSurfaceMovement class.
Deleted CVolumetricMovement class.
Deleted CConfig container.
Deleted nInst container.
Deleted COutput class.
-------------------------------------------------------------------------

------------------------- Exit Success (SU2_CFD) ------------------------

Total Force - Pressure + Viscous
Cl =  -13.538631 Cd =  98.758301
Cmx =  8.179386 Cmy =  10547.449834 Cmz =  -80.129826
Cx =  99.331513 Cy =  -1.05082 Cz =  -8.351467

real	0m5.227s
user	0m6.941s
sys	0m0.820s
+ status=0
+ set +x

=================================================
CAPS verification (using pyCAPS) case su2_X43a_PyTest.py passed (as expected)
=================================================

./execute_PyTestRegression.sh: line 413: ulimit: stack size: cannot modify limit: Operation not permitted
flowCart: /Users/jenkins/util/cart3d/cart3d_v1.5.9_OSX64_ICC--22.11.16/bin/OSX64_ICC//flowCart

=================================================
+ echo 'cart3d_PyTest.py test;'
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESP126/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
cart3d_PyTest.py test;
+ python -u cart3d_PyTest.py -outLevel=0
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESP126/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
Loading AIM
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = Wing, index = 1
 Body size = 3.796888
 Tessellating body 1 with  MaxEdge = 0.094922  Sag = 0.003797  Angle = 15.000000
 Executing: autoInputs -r 30.000000 -nDiv 6 -maxR 9  &gt; autoInputs.out
 Executing: ./aero.csh &gt; aero.out
C_A  0.023693377
C_Y  -0.0012129282
C_N  0.065395002
C_D  0.025961197
C_S  -0.0012129282
C_L  0.064528278
C_l  0.0510971
C_m  0.000248187
C_n  -0.017525
C_M_x  0.0504544
C_M_y  0.000248187
C_M_z  -0.0192976

real	0m8.547s
user	0m14.988s
sys	0m0.330s
+ status=0
+ set +x

=================================================
CAPS verification (using pyCAPS) case cart3d_PyTest.py passed (as expected)
=================================================


=================================================
+ echo 'cart3d_OpenMDAO_3_alpha_PyTest.py test;'
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESP126/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
cart3d_OpenMDAO_3_alpha_PyTest.py test;
+ python -u cart3d_OpenMDAO_3_alpha_PyTest.py -outLevel=0
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESP126/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
----------------------------------------
&gt;&gt;&gt; alpha [2.]
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = Wing, index = 1

Getting CFD design variables.......
	Number of design variables - 1
	Design Variable name - alpha
	Done getting CFD design variables
Getting CFD functional.......
	Number of design variables - 1
	Objective name - CL2
	Done getting CFD functional
 Body size = 3.625615
 Tessellating body 1 with  MaxEdge = 0.090640  Sag = 0.003626  Angle = 15.000000
 Executing: autoInputs -r 30.000000 -nDiv 5 -maxR 7  -mesh2d &gt; autoInputs.out
 o Evaluating Cart3D functionals and/or gradients
   ATTENTION: using static geometry ../inputs/Components.i.tri
   (18:55:03) Running aero.csh on 2 core(s) in M0.5901A2B0_DP1
   (18:55:05) aero.csh done
 o case M0.5901A2B0_DP1, averaging data over 1 cycle(s)
&gt;&gt;&gt; CL2 [0.01631562]  CL 0.12773309
----------------------------------------
----------------------------------------
&gt;&gt;&gt; alpha [2.]
&gt;&gt;&gt; CL2 [0.01631562]  CL 0.12773309
----------------------------------------
========================================
 o Evaluating Cart3D functionals and/or gradients
   ATTENTION: using static geometry ../inputs/Components.i.tri
   (18:55:06) Running aero.csh on 2 core(s) in M0.5901A2B0_DP1
   (18:55:07) aero.csh done
              Max memory allowed:       32 GB
              Flow hexes:               2188
              Estimated cutter memory:  0.000219 GB / DV
              Estimated xsensit memory: 0.004157 GB / DV
              Available threads:        2
              # DVs:                    1
   o Number of simultaneous cutter jobs:   1
   (18:55:08) Linearizing cut-cells
   (18:55:08) ... done
   o Number of simultaneous xsensit jobs:  1
   (18:55:08) Computing gradients
   (18:55:12) ... done
 o case M0.5901A2B0_DP1, averaging data over 1 cycle(s)
&gt;&gt;&gt; CL2_alpha [[0.01572627]]
========================================
RUNNING THE L-BFGS-B CODE

           * * *

Machine precision = 2.220D-16
 N =            1     M =           10

At X0         0 variables are exactly at the bounds

At iterate    0    f=  1.63156D-02    |proj g|=  1.57263D-02
----------------------------------------
&gt;&gt;&gt; alpha [1.98427373]
 o Evaluating Cart3D functionals and/or gradients
   ATTENTION: using static geometry ../inputs/Components.i.tri
   (18:55:12) Running aero.csh on 2 core(s) in M0.5901A1.98427B0_DP1
   (18:55:14) aero.csh done
 o case M0.5901A1.98427B0_DP1, averaging data over 1 cycle(s)
&gt;&gt;&gt; CL2 [0.01606724]  CL 0.12675617
----------------------------------------
========================================
 o Evaluating Cart3D functionals and/or gradients
   ATTENTION: using static geometry ../inputs/Components.i.tri
   (18:55:14) Running aero.csh on 2 core(s) in M0.5901A1.98427B0_DP1
   (18:55:16) aero.csh done
              Max memory allowed:       32 GB
              Flow hexes:               2188
              Estimated cutter memory:  0.000219 GB / DV
              Estimated xsensit memory: 0.004157 GB / DV
              Available threads:        2
              # DVs:                    1
   o Number of simultaneous cutter jobs:   1
   (18:55:16) Linearizing cut-cells
   (18:55:16) ... done
   o Number of simultaneous xsensit jobs:  1
   (18:55:16) Computing gradients
   (18:55:20) ... done
 o case M0.5901A1.98427B0_DP1, averaging data over 1 cycle(s)
&gt;&gt;&gt; CL2_alpha [[0.01560329]]
========================================

At iterate    1    f=  1.60672D-02    |proj g|=  1.56033D-02
----------------------------------------
&gt;&gt;&gt; alpha [-0.01099175]
 o Evaluating Cart3D functionals and/or gradients
   ATTENTION: using static geometry ../inputs/Components.i.tri
   (18:55:21) Running aero.csh on 2 core(s) in M0.5901A-0.0109917B0_DP1
   (18:55:23) aero.csh done
 o case M0.5901A-0.0109917B0_DP1, averaging data over 1 cycle(s)
&gt;&gt;&gt; CL2 [6.05653711e-06]  CL 0.00246101
----------------------------------------
========================================
 o Evaluating Cart3D functionals and/or gradients
   ATTENTION: using static geometry ../inputs/Components.i.tri
   (18:55:23) Running aero.csh on 2 core(s) in M0.5901A-0.0109917B0_DP1
   (18:55:25) aero.csh done
              Max memory allowed:       32 GB
              Flow hexes:               2188
              Estimated cutter memory:  0.000219 GB / DV
              Estimated xsensit memory: 0.004157 GB / DV
              Available threads:        2
              # DVs:                    1
   o Number of simultaneous cutter jobs:   1
   (18:55:25) Linearizing cut-cells
   (18:55:25) ... done
   o Number of simultaneous xsensit jobs:  1
   (18:55:25) Computing gradients
   (18:55:29) ... done
 o case M0.5901A-0.0109917B0_DP1, averaging data over 1 cycle(s)
&gt;&gt;&gt; CL2_alpha [[0.00031042]]
========================================

At iterate    2    f=  6.05654D-06    |proj g|=  3.10424D-04
----------------------------------------
&gt;&gt;&gt; alpha [-0.05149286]
 o Evaluating Cart3D functionals and/or gradients
   ATTENTION: using static geometry ../inputs/Components.i.tri
   (18:55:30) Running aero.csh on 2 core(s) in M0.5901A-0.0514929B0_DP1
   (18:55:32) aero.csh done
 o case M0.5901A-0.0514929B0_DP1, averaging data over 1 cycle(s)
&gt;&gt;&gt; CL2 [2.59817062e-10]  CL 1.612e-05
----------------------------------------
========================================
 o Evaluating Cart3D functionals and/or gradients
   ATTENTION: using static geometry ../inputs/Components.i.tri
   (18:55:32) Running aero.csh on 2 core(s) in M0.5901A-0.0514929B0_DP1
   (18:55:34) aero.csh done
              Max memory allowed:       32 GB
              Flow hexes:               2188
              Estimated cutter memory:  0.000219 GB / DV
              Estimated xsensit memory: 0.004157 GB / DV
              Available threads:        2
              # DVs:                    1
   o Number of simultaneous cutter jobs:   1
   (18:55:34) Linearizing cut-cells
   (18:55:34) ... done
   o Number of simultaneous xsensit jobs:  1
   (18:55:34) Computing gradients
   (18:55:38) ... done
 o case M0.5901A-0.0514929B0_DP1, averaging data over 1 cycle(s)
&gt;&gt;&gt; CL2_alpha [[2.03612433e-06]]
========================================

At iterate    3    f=  2.59817D-10    |proj g|=  2.03612D-06
----------------------------------------
&gt;&gt;&gt; alpha [-0.05176027]
 o Evaluating Cart3D functionals and/or gradients
   ATTENTION: using static geometry ../inputs/Components.i.tri
   (18:55:39) Running aero.csh on 2 core(s) in M0.5901A-0.0517603B0_DP1
   (18:55:40) aero.csh done
 o case M0.5901A-0.0517603B0_DP1, averaging data over 1 cycle(s)
&gt;&gt;&gt; CL2 [9.25766089e-15]  CL 1e-07
----------------------------------------
========================================
 o Evaluating Cart3D functionals and/or gradients
   ATTENTION: using static geometry ../inputs/Components.i.tri
   (18:55:41) Running aero.csh on 2 core(s) in M0.5901A-0.0517603B0_DP1
   (18:55:43) aero.csh done
              Max memory allowed:       32 GB
              Flow hexes:               2188
              Estimated cutter memory:  0.000219 GB / DV
              Estimated xsensit memory: 0.004157 GB / DV
              Available threads:        2
              # DVs:                    1
   o Number of simultaneous cutter jobs:   1
   (18:55:43) Linearizing cut-cells
   (18:55:43) ... done
   o Number of simultaneous xsensit jobs:  1
   (18:55:43) Computing gradients
   (18:55:47) ... done
 o case M0.5901A-0.0517603B0_DP1, averaging data over 1 cycle(s)
&gt;&gt;&gt; CL2_alpha [[1.21372408e-08]]
========================================

At iterate    4    f=  9.25766D-15    |proj g|=  1.21372D-08

           * * *

Tit   = total number of iterations
Tnf   = total number of function evaluations
Tnint = total number of segments explored during Cauchy searches
Skip  = number of BFGS updates skipped
Nact  = number of active bounds at final generalized Cauchy point
Projg = norm of the final projected gradient
F     = final function value

           * * *

   N    Tit     Tnf  Tnint  Skip  Nact     Projg        F
    1      4      5      4     0     0   1.214D-08   9.258D-15
  F =   9.2576608860000000E-015

CONVERGENCE: NORM_OF_PROJECTED_GRADIENT_&lt;=_PGTOL            
Optimization Complete
-----------------------------------
Optimized value: [-0.05176027]

real	0m45.211s
user	0m30.674s
sys	0m4.329s
+ status=0
+ set +x

=================================================
CAPS verification (using pyCAPS) case cart3d_OpenMDAO_3_alpha_PyTest.py passed (as expected)
=================================================


=================================================
+ echo 'cart3d_OpenMDAO_3_twist_PyTest.py test;'
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESP126/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
cart3d_OpenMDAO_3_twist_PyTest.py test;
+ python -u cart3d_OpenMDAO_3_twist_PyTest.py -outLevel=0
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESP126/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
----------------------------------------
&gt;&gt;&gt; twist [4.]
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = Wing, index = 1

Getting CFD design variables.......
	Number of design variables - 1
	Design Variable name - twist
	Done getting CFD design variables
Getting CFD functional.......
	Number of design variables - 1
	Objective name - CL2
	Done getting CFD functional
 Body size = 3.630958
 Tessellating body 1 with  MaxEdge = 0.018155  Sag = 0.000908  Angle = 10.000000
 Executing: autoInputs -r 5.123450 -nDiv 5 -maxR 7  -symmY -halfBody &gt; autoInputs.out
 o Evaluating Cart3D functionals and/or gradients
   ATTENTION: using static geometry ../inputs/Components.i.tri
   (18:55:49) Running aero.csh on 2 core(s) in M0.5901A0B0_DP1
   (18:55:57) aero.csh done
 o case M0.5901A0B0_DP1, averaging data over 1 cycle(s)
&gt;&gt;&gt; CL2 [0.00411365]  CL 0.0641354
----------------------------------------
----------------------------------------
&gt;&gt;&gt; twist [4.]
&gt;&gt;&gt; CL2 [0.00411365]  CL 0.0641354
----------------------------------------
========================================
 o Evaluating Cart3D functionals and/or gradients
   ATTENTION: using static geometry ../inputs/Components.i.tri
   (18:55:57) Running aero.csh on 2 core(s) in M0.5901A0B0_DP1
   (18:56:08) aero.csh done
              Max memory allowed:       32 GB
              Flow hexes:               37528
              Estimated cutter memory:  0.003753 GB / DV
              Estimated xsensit memory: 0.071303 GB / DV
              Available threads:        2
              # DVs:                    1
   o Number of simultaneous cutter jobs:   1
   (18:56:08) Linearizing cut-cells
   (18:56:10) ... done
   o Number of simultaneous xsensit jobs:  1
   (18:56:10) Computing gradients
   (18:56:14) ... done
 o case M0.5901A0B0_DP1, averaging data over 1 cycle(s)
&gt;&gt;&gt; CL2_twist [[0.00210056]]
========================================
RUNNING THE L-BFGS-B CODE

           * * *

Machine precision = 2.220D-16
 N =            1     M =           10

At X0         0 variables are exactly at the bounds

At iterate    0    f=  4.11365D-03    |proj g|=  2.10056D-03
----------------------------------------
&gt;&gt;&gt; twist [3.99789944]
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = Wing, index = 1
 Body size = 3.630955
 Tessellating body 1 with  MaxEdge = 0.018155  Sag = 0.000908  Angle = 10.000000
 Executing: autoInputs -r 5.123450 -nDiv 5 -maxR 7  -symmY -halfBody &gt; autoInputs.out
 o Evaluating Cart3D functionals and/or gradients
   ATTENTION: using static geometry ../inputs/Components.i.tri
   (18:56:15) Running aero.csh on 2 core(s) in M0.5901A0B0_DP1
   (18:56:23) aero.csh done
 o case M0.5901A0B0_DP1, averaging data over 1 cycle(s)
&gt;&gt;&gt; CL2 [0.0041123]  CL 0.0641197
----------------------------------------
========================================
 o Evaluating Cart3D functionals and/or gradients
   ATTENTION: using static geometry ../inputs/Components.i.tri
   (18:56:24) Running aero.csh on 2 core(s) in M0.5901A0B0_DP1
   (18:56:34) aero.csh done
              Max memory allowed:       32 GB
              Flow hexes:               37527
              Estimated cutter memory:  0.003753 GB / DV
              Estimated xsensit memory: 0.071301 GB / DV
              Available threads:        2
              # DVs:                    1
   o Number of simultaneous cutter jobs:   1
   (18:56:34) Linearizing cut-cells
   (18:56:36) ... done
   o Number of simultaneous xsensit jobs:  1
   (18:56:37) Computing gradients
   (18:56:41) ... done
 o case M0.5901A0B0_DP1, averaging data over 1 cycle(s)
&gt;&gt;&gt; CL2_twist [[0.00210014]]
========================================

At iterate    1    f=  4.11230D-03    |proj g|=  2.10014D-03
----------------------------------------
&gt;&gt;&gt; twist [-6.51746279]
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = Wing, index = 1
 Body size = 3.635732
 Tessellating body 1 with  MaxEdge = 0.018179  Sag = 0.000909  Angle = 10.000000
 Executing: autoInputs -r 5.123450 -nDiv 5 -maxR 7  -symmY -halfBody &gt; autoInputs.out
 o Evaluating Cart3D functionals and/or gradients
   ATTENTION: using static geometry ../inputs/Components.i.tri
   (18:56:42) Running aero.csh on 2 core(s) in M0.5901A0B0_DP1
   (18:56:49) aero.csh done
 o case M0.5901A0B0_DP1, averaging data over 1 cycle(s)
&gt;&gt;&gt; CL2 [0.00998113]  CL -0.0999038
----------------------------------------
========================================
 o Evaluating Cart3D functionals and/or gradients
   ATTENTION: using static geometry ../inputs/Components.i.tri
   (18:56:50) Running aero.csh on 2 core(s) in M0.5901A0B0_DP1
   (18:57:01) aero.csh done
              Max memory allowed:       32 GB
              Flow hexes:               37089
              Estimated cutter memory:  0.003709 GB / DV
              Estimated xsensit memory: 0.070469 GB / DV
              Available threads:        2
              # DVs:                    1
   o Number of simultaneous cutter jobs:   1
   (18:57:01) Linearizing cut-cells
   (18:57:03) ... done
   o Number of simultaneous xsensit jobs:  1
   (18:57:03) Computing gradients
   (18:57:07) ... done
 o case M0.5901A0B0_DP1, averaging data over 1 cycle(s)
&gt;&gt;&gt; CL2_twist [[-0.00319688]]
========================================
----------------------------------------
&gt;&gt;&gt; twist [-0.14346249]
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = Wing, index = 1
 Body size = 3.625762
 Tessellating body 1 with  MaxEdge = 0.018129  Sag = 0.000906  Angle = 10.000000
 Executing: autoInputs -r 5.123450 -nDiv 5 -maxR 7  -symmY -halfBody &gt; autoInputs.out
 o Evaluating Cart3D functionals and/or gradients
   ATTENTION: using static geometry ../inputs/Components.i.tri
   (18:57:08) Running aero.csh on 2 core(s) in M0.5901A0B0_DP1
   (18:57:16) aero.csh done
 o case M0.5901A0B0_DP1, averaging data over 1 cycle(s)
&gt;&gt;&gt; CL2 [4.79392926e-08]  CL -0.00022338
----------------------------------------
========================================
 o Evaluating Cart3D functionals and/or gradients
   ATTENTION: using static geometry ../inputs/Components.i.tri
   (18:57:16) Running aero.csh on 2 core(s) in M0.5901A0B0_DP1
   (18:57:27) aero.csh done
              Max memory allowed:       32 GB
              Flow hexes:               37755
              Estimated cutter memory:  0.003776 GB / DV
              Estimated xsensit memory: 0.071735 GB / DV
              Available threads:        2
              # DVs:                    1
   o Number of simultaneous cutter jobs:   1
   (18:57:27) Linearizing cut-cells
   (18:57:29) ... done
   o Number of simultaneous xsensit jobs:  1
   (18:57:29) Computing gradients
   (18:57:33) ... done
 o case M0.5901A0B0_DP1, averaging data over 1 cycle(s)
&gt;&gt;&gt; CL2_twist [[-7.2473947e-06]]
========================================

At iterate    2    f=  4.79393D-08    |proj g|=  7.24739D-06
----------------------------------------
&gt;&gt;&gt; twist [-0.12922018]
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = Wing, index = 1
 Body size = 3.625747
 Tessellating body 1 with  MaxEdge = 0.018129  Sag = 0.000906  Angle = 10.000000
 Executing: autoInputs -r 5.123450 -nDiv 5 -maxR 7  -symmY -halfBody &gt; autoInputs.out
 o Evaluating Cart3D functionals and/or gradients
   ATTENTION: using static geometry ../inputs/Components.i.tri
   (18:57:34) Running aero.csh on 2 core(s) in M0.5901A0B0_DP1
   (18:57:42) aero.csh done
 o case M0.5901A0B0_DP1, averaging data over 1 cycle(s)
&gt;&gt;&gt; CL2 [2.18169714e-08]  CL 0.00015117
----------------------------------------
========================================
 o Evaluating Cart3D functionals and/or gradients
   ATTENTION: using static geometry ../inputs/Components.i.tri
   (18:57:42) Running aero.csh on 2 core(s) in M0.5901A0B0_DP1
   (18:57:53) aero.csh done
              Max memory allowed:       32 GB
              Flow hexes:               37755
              Estimated cutter memory:  0.003776 GB / DV
              Estimated xsensit memory: 0.071735 GB / DV
              Available threads:        2
              # DVs:                    1
   o Number of simultaneous cutter jobs:   1
   (18:57:53) Linearizing cut-cells
   (18:57:55) ... done
   o Number of simultaneous xsensit jobs:  1
   (18:57:55) Computing gradients
   (18:57:59) ... done
 o case M0.5901A0B0_DP1, averaging data over 1 cycle(s)
&gt;&gt;&gt; CL2_twist [[4.89190887e-06]]
========================================

At iterate    3    f=  2.18170D-08    |proj g|=  4.89191D-06

           * * *

Tit   = total number of iterations
Tnf   = total number of function evaluations
Tnint = total number of segments explored during Cauchy searches
Skip  = number of BFGS updates skipped
Nact  = number of active bounds at final generalized Cauchy point
Projg = norm of the final projected gradient
F     = final function value

           * * *

   N    Tit     Tnf  Tnint  Skip  Nact     Projg        F
    1      3      5      3     0     0   4.892D-06   2.182D-08
  F =   2.1816971420000000E-008

CONVERGENCE: REL_REDUCTION_OF_F_&lt;=_FACTR*EPSMCH             
Optimization Complete
-----------------------------------
Optimized values: [-0.12922018]

real	2m12.390s
user	2m58.637s
sys	0m4.883s
+ status=0
+ set +x

=================================================
CAPS verification (using pyCAPS) case cart3d_OpenMDAO_3_twist_PyTest.py passed (as expected)
=================================================


=================================================
+ echo 'fun3d_Morph_PyTest.py test;'
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESP126/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
fun3d_Morph_PyTest.py test;
+ python -u fun3d_Morph_PyTest.py -outLevel=0 -noAnalysis
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESP126/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 3
	Name = Wing1, index = 1
	Name = Wing2, index = 2
	Name = Farfield, index = 3
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 3
	Name = Wing1, index = 1
	Name = Wing2, index = 2
	Name = Farfield, index = 3
AFLR4    : Proximity BG Surface Grid Generation Skipped
AFLR4    : No Modifications Required

Writing Tecplot file ....
Finished writing Tecplot file

Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 3
	Name = Wing1, index = 1
	Name = Wing2, index = 2
	Name = Farfield, index = 3
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 3
	Name = Wing1, index = 1
	Name = Wing2, index = 2
	Name = Farfield, index = 3
Getting volume mesh
 
AFLR2    : ---------------------------------------
AFLR2    : AFLR2 LIBRARY
AFLR2    : ADVANCING-FRONT/LOCAL-RECONNECTION
AFLR2    : TRIA/QUAD GRID GENERATOR
AFLR2    : Version Number 9.18.1
AFLR2    : Version Date   06/11/24 @ 05:52PM
AFLR2    : Compile OS     Darwin 23.5.0 arm64
AFLR2    : Compile Date   06/11/24 @ 05:52PM
AFLR2    : Copyright 1994-2021, D.L. Marcum
AFLR2    : ---------------------------------------
 
AFLR4    : ---------------------------------------
AFLR4    : AFLR4 LIBRARY
AFLR4    : ADVANCING-FRONT/LOCAL-RECONNECTION
AFLR4    : TRIA/QUAD SURFACE GRID GENERATOR
AFLR4    : Version Number 11.5.15
AFLR4    : Version Date   07/19/24 @ 07:04PM
AFLR4    : Compile OS     Darwin 23.5.0 arm64
AFLR4    : Compile Date   07/19/24 @ 07:06PM
AFLR4    : Copyright 1994-2021, D.L. Marcum
AFLR4    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.8.1
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.8.1
EGADS    : ---------------------------------------
Volume mesh:
	Number of nodes          = 82829
	Number of elements       = 483649
	Number of triangles      = 15680
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 467969
	Number of pyramids       = 0
	Number of prisms         = 0
	Number of hexahedrals    = 0

Writing Tecplot file ....
Finished writing Tecplot file

Getting CFD boundary conditions
	Boundary condition name - Farfield
	Boundary condition name - Wing1
	Boundary condition name - Wing2
	Done getting CFD boundary conditions

Getting CFD design variables.......
	Number of design variables - 2
	Design Variable name - Alpha
	Design Variable name - twist
	Done getting CFD design variables
Getting CFD functional.......
	Number of design variables - 2
	Objective name - Cd2
	Objective name - Const
	Done getting CFD functional
Python library was linked, but will not be used!
Creating FUN3D directory tree
DesignVariable = Alpha
DesignVariable = twist
Writing sensitivity file for body 1, File - Rubberize/model.tec.1.sd1
Writing sensitivity file for body 2, File - Rubberize/model.tec.2.sd1
Writing sensitivity file for body 3, File - Rubberize/model.tec.3.sd1
Writing rubber.data 
Writing surface file for 1 (of 3) in body 1 File - Flow/fun3dAFLRTest_body1.dat
Writing surface file for 1 (of 3) in body 1 File - Flow/fun3dAFLRTest_body1.dat
Writing surface file for 1 (of 3) in body 1 File - Flow/fun3dAFLRTest_body1.dat

Writing MAPBC file ....
Finished writing MAPBC file

Warning: The fun3d.nml file will be overwritten!
Writing fun3d.nml
Info: No recognized data transfer names found.
Reading rubber.data 
Projecting tessellation 1 (of 3) on to new body
Projecting tessellation 2 (of 3) on to new body
Projecting tessellation 3 (of 3) on to new body
Python library was linked, but will not be used!
Creating FUN3D directory tree
DesignVariable = Alpha
DesignVariable = twist
Writing sensitivity file for body 1, File - Rubberize/model.tec.1.sd1
Writing sensitivity file for body 2, File - Rubberize/model.tec.2.sd1
Writing sensitivity file for body 3, File - Rubberize/model.tec.3.sd1
Writing surface file for 1 (of 3) in body 1 File - Flow/fun3dAFLRTest_body1.dat
Writing surface file for 1 (of 3) in body 1 File - Flow/fun3dAFLRTest_body1.dat
Writing surface file for 1 (of 3) in body 1 File - Flow/fun3dAFLRTest_body1.dat

Writing MAPBC file ....
Finished writing MAPBC file

Warning: The fun3d.nml file will be overwritten!
Writing fun3d.nml
Info: No recognized data transfer names found.
Reading rubber.data 

real	0m5.359s
user	0m5.300s
sys	0m0.339s
+ status=0
+ set +x

=================================================
CAPS verification (using pyCAPS) case fun3d_Morph_PyTest.py passed (as expected)
=================================================

Running.... STRUCTURE PyTests


=================================================
+ echo 'masstran_PyTest.py test;'
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESP126/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
masstran_PyTest.py test;
+ python -u masstran_PyTest.py -outLevel=0
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESP126/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt

Getting results mass properties.....

Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = Ribs_and_Spars, index = 1
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 0
Getting surface mesh for body 1 (of 1)
Body 1 (of 1)
Number of nodes    = 1159
Number of elements = 798
Number of triangle elements      = 0
Number of quadrilateral elements = 798
----------------------------
Total number of nodes    = 1159
Total number of elements = 798
Mapping Csys attributes ................
	Number of unique Csys attributes = 0

Getting FEA coordinate systems.......
	Number of coordinate systems - 0
	No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
	Number of unique capsConstraint attributes = 1
	Name = Rib_Constraint, index = 1
Mapping capsLoad attributes ................
	Number of unique capsLoad attributes = 0
Mapping capsBound attributes ................
	Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
	Number of unique capsConnect attributes = 0
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = Ribs_and_Spars, index = 1
Setting FEA Data
	Mesh for body = 0
	Number of nodal coordinates = 1159
	Number of elements = 798
	Elemental Nodes = 0
	Elemental Rods  = 0
	Elemental Tria3 = 0
	Elemental Quad4 = 798

Getting FEA materials.......
	Number of materials - 2
	Material name - Madeupium
	Material name - Unobtainium
	No "materialType" specified for Material tuple Unobtainium, defaulting to "Isotropic"
	Done getting FEA materials

Getting FEA properties.......
	Number of properties - 1
	Property name - Ribs_and_Spars
	No "material" specified for Property tuple Ribs_and_Spars, defaulting to an index of 1
	Done getting FEA properties
Updating mesh element types based on properties input
Area      3.428666259749
Mass      5383.006027806
Centroid  [1.222256036872, 0.1634981473779, -4.647736192456e-11]
CG        [1.222256036872, 0.1634981473779, -4.647907951721e-11]
Ixx       22133.97306031
Iyy       23448.30046704
Izz       1389.213122564
Ixy       164.2055275655
Ixz       -7.485782319314e-06
Iyz       1.710545499156e-06
I         [22133.97306031, 23448.30046704, 1389.213122564, 164.2055275655, -7.485782319314e-06, 1.710545499156e-06]
II        [[22133.97306031, -164.2055275655, 7.485782319314e-06], [-164.2055275655, 23448.30046704, -1.710545499156e-06], [7.485782319314e-06, -1.710545499156e-06, 1389.213122564]]

real	0m3.046s
user	0m4.639s
sys	0m5.834s
+ status=0
+ set +x

=================================================
CAPS verification (using pyCAPS) case masstran_PyTest.py passed (as expected)
=================================================


=================================================
+ echo 'masstran_AGARD445_PyTest.py test;'
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESP126/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
masstran_AGARD445_PyTest.py test;
+ python -u masstran_AGARD445_PyTest.py -outLevel=0
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESP126/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt

Getting results mass properties.....

Mapping Csys attributes ................
	Number of unique Csys attributes = 0

Getting FEA coordinate systems.......
	Number of coordinate systems - 0
	No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
	Number of unique capsConstraint attributes = 1
	Name = constEdge, index = 1
Mapping capsLoad attributes ................
	Number of unique capsLoad attributes = 1
	Name = force, index = 1
Mapping capsBound attributes ................
	Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
	Number of unique capsConnect attributes = 0
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = yatesPlate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
	Mesh for body = 0
	Number of nodal coordinates = 36
	Number of elements = 25
	Elemental Nodes = 0
	Elemental Rods  = 0
	Elemental Tria3 = 0
	Elemental Quad4 = 25

Getting FEA materials.......
	Number of materials - 1
	Material name - Mahogany
	Done getting FEA materials

Getting FEA properties.......
	Number of properties - 1
	Property name - yatesPlate
	Done getting FEA properties
Updating mesh element types based on properties input
Area      547.7004
Mass      0.01605224431138
Centroid  [20.03586282449, 14.01686746988, 0.0]
CG        [20.03586282449, 14.01686746988, 0.0]
Ixx       1.140246300554
Iyy       0.919317482675
Izz       2.059563783229
Ixy       0.7352134614013
Ixz       0.0
Iyz       0.0
I         [1.140246300554, 0.919317482675, 2.059563783229, 0.7352134614013, 0.0, 0.0]
II        [[1.140246300554, -0.7352134614013, -0.0], [-0.7352134614013, 0.919317482675, -0.0], [-0.0, -0.0, 2.059563783229]]

real	0m0.241s
user	0m0.298s
sys	0m0.071s
+ status=0
+ set +x

=================================================
CAPS verification (using pyCAPS) case masstran_AGARD445_PyTest.py passed (as expected)
=================================================


=================================================
+ echo 'hsm_SingleLoadCase_PyTest.py test;'
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESP126/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
hsm_SingleLoadCase_PyTest.py test;
+ python -u hsm_SingleLoadCase_PyTest.py -outLevel=0
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESP126/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
Mapping Csys attributes ................
	Number of unique Csys attributes = 0

Getting FEA coordinate systems.......
	Number of coordinate systems - 0
	No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
	Number of unique capsConstraint attributes = 1
	Name = plateEdge, index = 1
Mapping capsLoad attributes ................
	Number of unique capsLoad attributes = 1
	Name = plate, index = 1
Mapping capsBound attributes ................
	Number of unique capsBound attributes = 0
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = plate, index = 1
Creating HSM BEM
	Getting quads for BEM!
	Number of nodal coordinates = 81
	Number of elements = 96
	Elemental Tria3 = 0
	Elemental Quad4 = 64

Getting FEA materials.......
	Number of materials - 1
	Material name - Madeupium
	Done getting FEA materials

Getting FEA properties.......
	Number of properties - 1
	Property name - plate
	Done getting FEA properties

Getting FEA constraints.......
	Number of constraints - 1
	Constraint name - edgeConstraint
	No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement"
	Done getting FEA constraints

Getting FEA loads.......
	Number of loads - 1
	Load name - appliedPressure
	Done getting FEA loads

Writing Nastran grid and connectivity file (in small field format) ....
Finished writing Nastran grid file

Max Adjacency set to = 9
MaxDim = 32, numBCEdge = 0, numBCNode = 32, numJoint = 0
NEED TO ADD MORE CODE TO hsm_setGlobalParameter
NEED TO ADD MORE CODE TO hsm_setNodeBCParameter
NumBCNode = 32
-&gt;HSMSOL
 Matrix Non-zero Entries = 5741

 Converging HSM equation system ...
  iter     dr         dd         dp         rlx   max
   1    0.130E-01  0.165E+00  0.153E-04    1.000  ddy @ (   0.25   0.06   0.00)
   1*   0.260E-03  0.000E+00  0.000E+00    1.000  drz @ (   0.25   0.12   0.00)
   1*   0.240E-05  0.000E+00  0.000E+00    1.000  drz @ (   0.25   0.09   0.00)
   2    0.379E-02  0.505E-01  0.750E-04    1.000  ddy @ (   0.25   0.19   0.00)
   2*   0.420E-04  0.000E+00  0.000E+00    1.000  drz @ (   0.25   0.12   0.00)
   3    0.168E-02  0.225E-01  0.208E-04    1.000  ddy @ (   0.25   0.06   0.00)
   4    0.325E-03  0.427E-02  0.250E-05    1.000  ddy @ (   0.25   0.19   0.00)
   5    0.794E-05  0.112E-03  0.170E-06    1.000  ddy @ (   0.25   0.19   0.00)
   6    0.387E-08  0.598E-07  0.197E-09    1.000  ddy @ (   0.25   0.06   0.00)
   7    0.848E-15  0.147E-13  0.924E-15    1.000  ddy @ (   0.25   0.19   0.00)

 Converging n vectors ...
 it =  1    dn =  0.788E-01   rlx = 1.000  (  59 )
 it =  2    dn =  0.566E-16   rlx = 1.000  (  35 )

 Converging e1,e2 vectors ...
 it =  1    de =  0.691E-03   rlx = 1.000  (  45 )
 it =  2    de =  0.404E-04   rlx = 1.000  (   9 )
 it =  3    de =  0.142E-07   rlx = 1.000  (  46 )
 it =  4    de =  0.521E-11   rlx = 1.000  (  62 )

 Calculating  strains, stress resultants ...
Writing HSM solution to Tecplot File - HSMSingleLoadPlate.dat

real	0m0.381s
user	0m0.601s
sys	0m0.048s
+ status=0
+ set +x

=================================================
CAPS verification (using pyCAPS) case hsm_SingleLoadCase_PyTest.py passed (as expected)
=================================================


=================================================
+ echo 'hsm_CantileverPlate_PyTest.py test;'
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESP126/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
hsm_CantileverPlate_PyTest.py test;
+ python -u hsm_CantileverPlate_PyTest.py -outLevel=0
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESP126/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
Mapping Csys attributes ................
	Number of unique Csys attributes = 1
	Name = plate, index = 1

Getting FEA coordinate systems.......
	Number of coordinate systems - 1
	Coordinate system name - plate
Mapping capsConstraint attributes ................
	Number of unique capsConstraint attributes = 1
	Name = plateEdge, index = 1
Mapping capsLoad attributes ................
	Number of unique capsLoad attributes = 1
	Name = plateTip, index = 1
Mapping capsBound attributes ................
	Number of unique capsBound attributes = 0
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = plate, index = 1
Creating HSM BEM
	Getting quads for BEM!
	Number of nodal coordinates = 40
	Number of elements = 51
	Elemental Tria3 = 0
	Elemental Quad4 = 27

Getting FEA materials.......
	Number of materials - 1
	Material name - Madeupium
	Done getting FEA materials

Getting FEA properties.......
	Number of properties - 1
	Property name - plate
	Done getting FEA properties

Getting FEA constraints.......
	Number of constraints - 1
	Constraint name - edgeConstraint
	No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement"
	Done getting FEA constraints

Getting FEA loads.......
	Number of loads - 1
	Load name - appliedLoad
	Done getting FEA loads

Writing Nastran grid and connectivity file (in small field format) ....
Finished writing Nastran grid file

Max Adjacency set to = 9
MaxDim = 4, numBCEdge = 3, numBCNode = 4, numJoint = 0
NEED TO ADD MORE CODE TO hsm_setGlobalParameter
NEED TO ADD MORE CODE TO hsm_setNodeBCParameter
NumBCNode = 4
-&gt;HSMSOL
 Matrix Non-zero Entries = 1313

 Converging HSM equation system ...
  iter     dr         dd         dp         rlx   max
   1    0.314E+01  0.628E+01  0.000E+00    0.080  ddx @ (   1.00   0.00   0.00)
   1*   0.341E-01  0.000E+00  0.000E+00    1.000  drx @ (   1.00   0.10   0.00)
   1*   0.326E-02  0.000E+00  0.000E+00    1.000  drx @ (   1.00   0.10   0.00)
   1*   0.438E-04  0.000E+00  0.000E+00    1.000  drx @ (   1.00   0.10   0.00)
   2    0.274E+01  0.521E+01  0.106E-07    0.096  ddx @ (   1.00   0.03   0.00)
   2*   0.321E-01  0.000E+00  0.000E+00    1.000  drx @ (   1.00   0.00   0.00)
   2*   0.373E-02  0.000E+00  0.000E+00    1.000  drz @ (   1.00   0.03   0.00)
   2*   0.777E-04  0.000E+00  0.000E+00    1.000  drz @ (   1.00   0.03   0.00)
   3    0.202E+01  0.439E+01  0.928E-07    0.114  ddz @ (   1.00   0.03   0.00)
   3*   0.442E-01  0.000E+00  0.000E+00    1.000  drz @ (   1.00   0.03   0.00)
   3*   0.623E-02  0.000E+00  0.000E+00    1.000  drz @ (   1.00   0.03   0.00)
   3*   0.163E-03  0.000E+00  0.000E+00    1.000  drz @ (   1.00   0.07   0.00)
   3*   0.167E-06  0.000E+00  0.000E+00    1.000  drz @ (   1.00   0.03   0.00)
   4    0.192E+01  0.476E+01  0.126E-07    0.105  ddz @ (   1.00   0.03   0.00)
   4*   0.335E-01  0.000E+00  0.000E+00    1.000  drz @ (   1.00   0.10   0.00)
   4*   0.332E-02  0.000E+00  0.000E+00    1.000  drz @ (   1.00   0.10   0.00)
   4*   0.451E-04  0.000E+00  0.000E+00    1.000  drz @ (   1.00   0.10   0.00)
   5    0.187E+01  0.394E+01  0.254E-07    0.127  ddz @ (   1.00   0.07   0.00)
   5*   0.353E-01  0.000E+00  0.000E+00    1.000  drz @ (   1.00   0.00   0.00)
   5*   0.379E-02  0.000E+00  0.000E+00    1.000  drz @ (   1.00   0.00   0.00)
   5*   0.638E-04  0.000E+00  0.000E+00    1.000  drz @ (   1.00   0.00   0.00)
   6    0.156E+01  0.300E+01  0.112E-06    0.166  ddx @ (   1.00   0.07   0.00)
   6*   0.326E-01  0.000E+00  0.000E+00    1.000  drz @ (   1.00   0.00   0.00)
   6*   0.575E-02  0.000E+00  0.000E+00    1.000  drx @ (   1.00   0.00   0.00)
   6*   0.193E-03  0.000E+00  0.000E+00    1.000  drx @ (   1.00   0.00   0.00)
   6*   0.272E-06  0.000E+00  0.000E+00    1.000  drx @ (   1.00   0.00   0.00)
   7    0.103E+01  0.323E+01  0.345E-07    0.155  ddx @ (   1.00   0.07   0.00)
   7*   0.259E-01  0.000E+00  0.000E+00    1.000  drx @ (   1.00   0.00   0.00)
   7*   0.297E-02  0.000E+00  0.000E+00    1.000  drx @ (   1.00   0.00   0.00)
   7*   0.435E-04  0.000E+00  0.000E+00    1.000  drx @ (   1.00   0.00   0.00)
   8    0.756E+00  0.259E+01  0.139E-07    0.193  ddx @ (   1.00   0.03   0.00)
   8*   0.295E-01  0.000E+00  0.000E+00    1.000  drx @ (   1.00   0.10   0.00)
   8*   0.350E-02  0.000E+00  0.000E+00    1.000  drx @ (   1.00   0.00   0.00)
   8*   0.587E-04  0.000E+00  0.000E+00    1.000  drx @ (   1.00   0.00   0.00)
   9    0.678E+00  0.179E+01  0.639E-07    0.279  ddx @ (   0.89   0.00   0.00)
   9*   0.330E-01  0.000E+00  0.000E+00    1.000  drx @ (   1.00   0.10   0.00)
   9*   0.457E-02  0.000E+00  0.000E+00    1.000  drx @ (   1.00   0.00   0.00)
   9*   0.167E-03  0.000E+00  0.000E+00    1.000  drz @ (   1.00   0.00   0.00)
   9*   0.264E-06  0.000E+00  0.000E+00    1.000  drz @ (   1.00   0.00   0.00)
  10    0.452E+00  0.171E+01  0.499E-07    0.292  ddz @ (   1.00   0.10   0.00)
  10*   0.166E-01  0.000E+00  0.000E+00    1.000  drz @ (   1.00   0.00   0.00)
  10*   0.239E-02  0.000E+00  0.000E+00    1.000  drz @ (   1.00   0.00   0.00)
  10*   0.393E-04  0.000E+00  0.000E+00    1.000  drz @ (   1.00   0.00   0.00)
  iter     dr         dd         dp         rlx   max
  11    0.257E+00  0.120E+01  0.614E-08    0.417  ddz @ (   1.00   0.00   0.00)
  11*   0.206E-01  0.000E+00  0.000E+00    1.000  drz @ (   1.00   0.10   0.00)
  11*   0.283E-02  0.000E+00  0.000E+00    1.000  drz @ (   1.00   0.10   0.00)
  11*   0.488E-04  0.000E+00  0.000E+00    1.000  drz @ (   1.00   0.10   0.00)
  12    0.131E+00  0.647E+00  0.288E-08    0.772  ddz @ (   0.89   0.00   0.00)
  12*   0.238E-01  0.000E+00  0.000E+00    1.000  drz @ (   1.00   0.10   0.00)
  12*   0.357E-02  0.000E+00  0.000E+00    1.000  drz @ (   1.00   0.10   0.00)
  12*   0.849E-04  0.000E+00  0.000E+00    1.000  drx @ (   1.00   0.10   0.00)
  13    0.393E-01  0.238E+00  0.325E-07    1.000  ddx @ (   1.00   0.07   0.00)
  13*   0.336E-02  0.000E+00  0.000E+00    1.000  drz @ (   1.00   0.00   0.00)
  13*   0.936E-04  0.000E+00  0.000E+00    1.000  drx @ (   1.00   0.10   0.00)
  14    0.475E-03  0.514E-02  0.635E-07    1.000  ddx @ (   1.00   0.10   0.00)
  15    0.893E-06  0.651E-06  0.135E-08    1.000  drx @ (   1.00   0.00   0.00)
  16    0.574E-10  0.216E-09  0.140E-11    1.000  ddx @ (   0.44   0.00   0.00)
  17    0.148E-15  0.575E-15  0.104E-14    1.000  dps @ (   1.00   0.10   0.00)

 Converging n vectors ...
 it =  1    dn =  0.193E+01   rlx = 1.000  (   9 )
 it =  2    dn =  0.423E-15   rlx = 1.000  (  31 )

 Converging e1,e2 vectors ...
 it =  1    de =  0.285E+01   rlx = 0.351  (  24 )
 it =  2    de =  0.269E+01   rlx = 0.372  (  14 )
 it =  3    de =  0.202E+01   rlx = 0.494  (  40 )
 it =  4    de =  0.122E+01   rlx = 0.820  (  40 )
 it =  5    de =  0.378E+00   rlx = 1.000  (  40 )
 it =  6    de =  0.127E-01   rlx = 1.000  (  14 )
 it =  7    de =  0.524E-06   rlx = 1.000  (  40 )
 it =  8    de =  0.938E-16   rlx = 1.000  (  22 )

 Calculating  strains, stress resultants ...
Writing HSM solution to Tecplot File - HSMCantileverPlate.dat

real	0m0.317s
user	0m0.474s
sys	0m0.047s
+ status=0
+ set +x

=================================================
CAPS verification (using pyCAPS) case hsm_CantileverPlate_PyTest.py passed (as expected)
=================================================

ASTROS_ROOT: /Users/jenkins/util/astros/Astros/Darwin-64bit

=================================================
+ echo 'astros_Aeroelastic_PyTest.py test;'
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESP126/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
astros_Aeroelastic_PyTest.py test;
+ python -u astros_Aeroelastic_PyTest.py -outLevel=0
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESP126/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
Mapping Csys attributes ................
	Number of unique Csys attributes = 0

Getting FEA coordinate systems.......
	Number of coordinate systems - 0
	No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
	Number of unique capsConstraint attributes = 1
	Name = Rib_Root_Point, index = 1
Mapping capsLoad attributes ................
	Number of unique capsLoad attributes = 0
Mapping capsBound attributes ................
	Number of unique capsBound attributes = 1
	Name = Skin_Top, index = 1
Mapping capsConnect attributes ................
	Number of unique capsConnect attributes = 1
	Name = Rib_Root, index = 1
Mapping capsResponse attributes ................
	Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
	Number of unique capsReference attributes = 1
	Name = Rib_Root_Point, index = 1
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 7
	Name = Ribs, index = 1
	Name = Skin, index = 2
	Name = Spar1, index = 3
	Name = Rib_Root, index = 4
	Name = Spar2, index = 5
	Name = Rib_Root_Point, index = 6
	Name = Wing, index = 7
Setting FEA Data
	Mesh for body = 0
	Number of nodal coordinates = 366
	Number of elements = 523
	Elemental Nodes = 0
	Elemental Rods  = 0
	Elemental Tria3 = 190
	Elemental Quad4 = 333
Setting FEA Data
	Mesh for body = 1
	Number of nodal coordinates = 1
	Number of elements = 1
	Elemental Nodes = 1
	Elemental Rods  = 0
	Elemental Tria3 = 0
	Elemental Quad4 = 0
Combining multiple FEA meshes!
	Combined Number of nodal coordinates = 367
	Combined Number of elements = 524
	Combined Elemental Nodes = 1
	Combined Elemental Rods  = 0
	Combined Elemental Tria3 = 190
	Combined Elemental Quad4 = 333
Getting vortex lattice surface data
	VLM surface name - Skin_Top
	Done getting vortex lattice surface data
Getting vortex lattice control surface data
	VLM control surface name - CntrlLE
	VLM control surface name - CntrlTE
	Done getting vortex lattice control surface data

Getting FEA vortex lattice mesh
	Surface 1: Number of points found for aero-spline = 48
	(Re-)Combining all aerodynamic surfaces into a 'Wing', 'Canard', and/or  'Fin' single surfaces !

Getting Aero Reference Parameters.......

Getting FEA materials.......
	Number of materials - 1
	Material name - Unobtainium
	No "materialType" specified for Material tuple Unobtainium, defaulting to "Isotropic"
	Done getting FEA materials

Getting FEA properties.......
	Number of properties - 5
	Property name - Rib_Root
	No "material" specified for Property tuple Rib_Root, defaulting to an index of 1
	Property name - Ribs
	No "material" specified for Property tuple Ribs, defaulting to an index of 1
	Property name - Skin
	No "material" specified for Property tuple Skin, defaulting to an index of 1
	Property name - Spar1
	No "material" specified for Property tuple Spar1, defaulting to an index of 1
	Property name - Spar2
	No "material" specified for Property tuple Spar2, defaulting to an index of 1
	Done getting FEA properties
Updating mesh element types based on properties input

Getting FEA constraints.......
	Number of constraints - 1
	Constraint name - ribConstraint
	No "constraintType" specified for Constraint tuple ribConstraint, defaulting to "ZeroDisplacement"
	Done getting FEA constraints

Getting FEA supports.......
	Number of supports - 1
	Support name - ribSupport
	Done getting FEA supports

Getting FEA connections.......
	Number of connection tuples - 1
	Connection name - Rib_Root
	No "groupName" specified for Connection tuple Rib_Root!
	Looking for automatic connections from the use of capsConnectLink for Rib_Root
	43 automatic connections were made for capsConnect Rib_Root (node id 367)
	Done getting FEA connections
Load tuple is NULL - No loads applied
Optimization Control tuple is NULL - Default optimization control is used

Getting FEA optimization control.......
Done getting FEA Optimization Control
Design_Variable tuple is NULL - No design variables applied
Design_Constraint tuple is NULL - No design constraints applied

Getting FEA analyses.......
	Number of analyses - 1
	Analysis name - Trim1
	Done getting FEA analyses

Writing Astros grid and connectivity file (in free field format) ....
Finished writing Astros grid file

Writing subElement types (if any) - appending mesh file
Writing connection cards - appending mesh file

Writing Astros instruction file....
	Writing aeros card
	Writing analysis cards
	Writing constraint cards--each subcase individually
	Writing support cards
	Writing material cards
	Writing property cards
	Writing aeroelastic cards
Note: The following floating-point exceptions are signalling: IEEE_UNDERFLOW_FLAG

real	0m6.355s
user	0m12.508s
sys	0m4.649s
+ status=0
+ set +x

=================================================
CAPS verification (using pyCAPS) case astros_Aeroelastic_PyTest.py passed (as expected)
=================================================


=================================================
+ echo 'astros_AGARD445_PyTest.py test;'
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESP126/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
astros_AGARD445_PyTest.py test;
+ python -u astros_AGARD445_PyTest.py -outLevel=0
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESP126/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt

Getting results natural frequencies.....
Mapping Csys attributes ................
	Number of unique Csys attributes = 0

Getting FEA coordinate systems.......
	Number of coordinate systems - 0
	No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
	Number of unique capsConstraint attributes = 1
	Name = constEdge, index = 1
Mapping capsLoad attributes ................
	Number of unique capsLoad attributes = 1
	Name = force, index = 1
Mapping capsBound attributes ................
	Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
	Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
	Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
	Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = yatesPlate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
	Mesh for body = 0
	Number of nodal coordinates = 36
	Number of elements = 25
	Elemental Nodes = 0
	Elemental Rods  = 0
	Elemental Tria3 = 0
	Elemental Quad4 = 25
Aero_Reference value is NULL - No aero reference parameters set

Getting FEA materials.......
	Number of materials - 1
	Material name - Mahogany
	Done getting FEA materials

Getting FEA properties.......
	Number of properties - 1
	Property name - yatesPlate
	Done getting FEA properties
Updating mesh element types based on properties input

Getting FEA constraints.......
	Number of constraints - 1
	Constraint name - edgeConstraint
	No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement"
	Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults
Load tuple is NULL - No loads applied
Optimization Control tuple is NULL - Default optimization control is used

Getting FEA optimization control.......
Done getting FEA Optimization Control
Design_Variable tuple is NULL - No design variables applied
Design_Constraint tuple is NULL - No design constraints applied

Getting FEA analyses.......
	Number of analyses - 1
	Analysis name - EigenAnalysis
	No "analysisType" specified for Analysis tuple EigenAnalysis, defaulting to "Modal"
	Done getting FEA analyses

Writing Astros grid and connectivity file (in free field format) ....
Finished writing Astros grid file

Writing subElement types (if any) - appending mesh file

Writing Astros instruction file....
	Warning: No constraints specified for case EigenAnalysis, assuming all constraints are applied!!!!
	Writing analysis cards
	Writing constraint cards--all constraints for each subcase
	Writing material cards
	Writing property cards
Reading Astros OUT file - extracting Eigen-Values!
	Number of Eigen-Values = 2
	Loading Eigen-Value = 1
	Loading Eigen-Value = 2
Natural freq (Mode 1) = 5.78 (Hz)
Natural freq (Mode 2) = 30.66 (Hz)

real	0m0.355s
user	0m0.492s
sys	0m0.100s
+ status=0
+ set +x

=================================================
CAPS verification (using pyCAPS) case astros_AGARD445_PyTest.py passed (as expected)
=================================================


=================================================
+ echo 'astros_Composite_PyTest.py test;'
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESP126/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
astros_Composite_PyTest.py test;
+ python -u astros_Composite_PyTest.py -outLevel=0
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESP126/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
Mapping Csys attributes ................
	Number of unique Csys attributes = 1
	Name = plate, index = 1

Getting FEA coordinate systems.......
	Number of coordinate systems - 1
	Coordinate system name - plate
Mapping capsConstraint attributes ................
	Number of unique capsConstraint attributes = 1
	Name = plateEdge, index = 1
Mapping capsLoad attributes ................
	Number of unique capsLoad attributes = 1
	Name = plateTip, index = 1
Mapping capsBound attributes ................
	Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
	Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
	Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
	Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
	Mesh for body = 0
	Number of nodal coordinates = 15
	Number of elements = 8
	Elemental Nodes = 0
	Elemental Rods  = 0
	Elemental Tria3 = 0
	Elemental Quad4 = 8
Aero_Reference value is NULL - No aero reference parameters set

Getting FEA materials.......
	Number of materials - 2
	Material name - Madeupium
	Material name - Unobtainium
	No "materialType" specified for Material tuple Unobtainium, defaulting to "Isotropic"
	Done getting FEA materials

Getting FEA properties.......
	Number of properties - 1
	Property name - plate
	Done getting FEA properties
Updating mesh element types based on properties input

Getting FEA constraints.......
	Number of constraints - 1
	Constraint name - cantilever
	No "constraintType" specified for Constraint tuple cantilever, defaulting to "ZeroDisplacement"
	Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults
Load tuple is NULL - No loads applied
Optimization Control tuple is NULL - Default optimization control is used

Getting FEA optimization control.......
Done getting FEA Optimization Control
Design_Variable tuple is NULL - No design variables applied
Design_Constraint tuple is NULL - No design constraints applied

Getting FEA analyses.......
	Number of analyses - 1
	Analysis name - EigenAnalysis
	No "analysisType" specified for Analysis tuple EigenAnalysis, defaulting to "Modal"
	Done getting FEA analyses

Writing Astros grid and connectivity file (in large field format) ....
Finished writing Astros grid file

Writing subElement types (if any) - appending mesh file

Writing Astros instruction file....
	Warning: No constraints specified for case EigenAnalysis, assuming all constraints are applied!!!!
	Writing analysis cards
	Writing constraint cards--all constraints for each subcase
	Writing material cards
	Writing property cards
	Writing coordinate system cards

real	0m0.449s
user	0m0.653s
sys	0m0.099s
+ status=0
+ set +x

=================================================
CAPS verification (using pyCAPS) case astros_Composite_PyTest.py passed (as expected)
=================================================


=================================================
+ echo 'astros_CompositeWingFreq_PyTest.py test;'
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESP126/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
astros_CompositeWingFreq_PyTest.py test;
+ python -u astros_CompositeWingFreq_PyTest.py -outLevel=0
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESP126/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt

Getting results for natural frequencies.....
Mapping Csys attributes ................
	Number of unique Csys attributes = 1
	Name = wing, index = 1

Getting FEA coordinate systems.......
	Number of coordinate systems - 1
	Coordinate system name - wing
Mapping capsConstraint attributes ................
	Number of unique capsConstraint attributes = 1
	Name = root, index = 1
Mapping capsLoad attributes ................
	Number of unique capsLoad attributes = 1
	Name = wing, index = 1
Mapping capsBound attributes ................
	Number of unique capsBound attributes = 1
	Name = wing, index = 1
Mapping capsConnect attributes ................
	Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
	Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
	Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = wing, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 5 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 6 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 7 of face 1, unable to assign a boundary index value
Setting FEA Data
	Mesh for body = 0
	Number of nodal coordinates = 443
	Number of elements = 845
	Elemental Nodes = 0
	Elemental Rods  = 0
	Elemental Tria3 = 845
	Elemental Quad4 = 0
Aero_Reference value is NULL - No aero reference parameters set

Getting FEA materials.......
	Number of materials - 2
	Material name - Aluminum
	No "materialType" specified for Material tuple Aluminum, defaulting to "Isotropic"
	Material name - Graphite_epoxy
	Done getting FEA materials

Getting FEA properties.......
	Number of properties - 1
	Property name - wing
	Done getting FEA properties
Updating mesh element types based on properties input

Getting FEA constraints.......
	Number of constraints - 1
	Constraint name - root
	No "constraintType" specified for Constraint tuple root, defaulting to "ZeroDisplacement"
	Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults
Load tuple is NULL - No loads applied
Optimization Control tuple is NULL - Default optimization control is used

Getting FEA optimization control.......
Done getting FEA Optimization Control
Design_Variable tuple is NULL - No design variables applied
Design_Constraint tuple is NULL - No design constraints applied

Getting FEA analyses.......
	Number of analyses - 1
	Analysis name - EigenAnalysis
	No "analysisType" specified for Analysis tuple EigenAnalysis, defaulting to "Modal"
	Done getting FEA analyses

Writing Astros grid and connectivity file (in large field format) ....
Finished writing Astros grid file

Writing subElement types (if any) - appending mesh file

Writing Astros instruction file....
	Warning: No constraints specified for case EigenAnalysis, assuming all constraints are applied!!!!
	Writing analysis cards
	Writing constraint cards--all constraints for each subcase
	Writing material cards
	Writing property cards
	Writing coordinate system cards
Reading Astros OUT file - extracting Eigen-Values!
	Number of Eigen-Values = 10
	Loading Eigen-Value = 1
	Loading Eigen-Value = 2
	Loading Eigen-Value = 3
	Loading Eigen-Value = 4
	Loading Eigen-Value = 5
	Loading Eigen-Value = 6
	Loading Eigen-Value = 7
	Loading Eigen-Value = 8
	Loading Eigen-Value = 9
	Loading Eigen-Value = 10
Natural freq (Mode 1) = 5.90553 (Hz)
Natural freq (Mode 2) = 29.72860 (Hz)
Natural freq (Mode 3) = 39.11840 (Hz)
Natural freq (Mode 4) = 77.46400 (Hz)
Natural freq (Mode 5) = 99.53050 (Hz)
Natural freq (Mode 6) = 146.35200 (Hz)
Natural freq (Mode 7) = 178.74700 (Hz)
Natural freq (Mode 8) = 234.29900 (Hz)
Natural freq (Mode 9) = 278.97300 (Hz)
Natural freq (Mode 10) = 313.52300 (Hz)
Reading Astros OUT file - extracting Eigen-Vectors!
	Number of Eigen-Vectors = 10
	Number of Grid Points = 443 for each Eigen-Vector
	Loading Eigen-Vector = 1
	Loading Eigen-Vector = 2
	Loading Eigen-Vector = 3
	Loading Eigen-Vector = 4
	Loading Eigen-Vector = 5
	Loading Eigen-Vector = 6
	Loading Eigen-Vector = 7
	Loading Eigen-Vector = 8
	Loading Eigen-Vector = 9
	Loading Eigen-Vector = 10
Reading Astros OUT file - extracting Eigen-Vectors!
	Number of Eigen-Vectors = 10
	Number of Grid Points = 443 for each Eigen-Vector
	Loading Eigen-Vector = 1
	Loading Eigen-Vector = 2
	Loading Eigen-Vector = 3
	Loading Eigen-Vector = 4
	Loading Eigen-Vector = 5
	Loading Eigen-Vector = 6
	Loading Eigen-Vector = 7
	Loading Eigen-Vector = 8
	Loading Eigen-Vector = 9
	Loading Eigen-Vector = 10
Reading Astros OUT file - extracting Eigen-Vectors!
	Number of Eigen-Vectors = 10
	Number of Grid Points = 443 for each Eigen-Vector
	Loading Eigen-Vector = 1
	Loading Eigen-Vector = 2
	Loading Eigen-Vector = 3
	Loading Eigen-Vector = 4
	Loading Eigen-Vector = 5
	Loading Eigen-Vector = 6
	Loading Eigen-Vector = 7
	Loading Eigen-Vector = 8
	Loading Eigen-Vector = 9
	Loading Eigen-Vector = 10
Reading Astros OUT file - extracting Eigen-Vectors!
	Number of Eigen-Vectors = 10
	Number of Grid Points = 443 for each Eigen-Vector
	Loading Eigen-Vector = 1
	Loading Eigen-Vector = 2
	Loading Eigen-Vector = 3
	Loading Eigen-Vector = 4
	Loading Eigen-Vector = 5
	Loading Eigen-Vector = 6
	Loading Eigen-Vector = 7
	Loading Eigen-Vector = 8
	Loading Eigen-Vector = 9
	Loading Eigen-Vector = 10
Reading Astros OUT file - extracting Eigen-Vectors!
	Number of Eigen-Vectors = 10
	Number of Grid Points = 443 for each Eigen-Vector
	Loading Eigen-Vector = 1
	Loading Eigen-Vector = 2
	Loading Eigen-Vector = 3
	Loading Eigen-Vector = 4
	Loading Eigen-Vector = 5
	Loading Eigen-Vector = 6
	Loading Eigen-Vector = 7
	Loading Eigen-Vector = 8
	Loading Eigen-Vector = 9
	Loading Eigen-Vector = 10

real	0m21.418s
user	0m21.269s
sys	0m0.399s
+ status=0
+ set +x

=================================================
CAPS verification (using pyCAPS) case astros_CompositeWingFreq_PyTest.py passed (as expected)
=================================================


=================================================
+ echo 'astros_Flutter_15degree.py test;'
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESP126/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
astros_Flutter_15degree.py test;
+ python -u astros_Flutter_15degree.py -outLevel=0
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESP126/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
Mapping Csys attributes ................
	Number of unique Csys attributes = 0

Getting FEA coordinate systems.......
	Number of coordinate systems - 0
	No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
	Number of unique capsConstraint attributes = 1
	Name = Root_Point, index = 1
Mapping capsLoad attributes ................
	Number of unique capsLoad attributes = 1
	Name = Root_Point, index = 1
Mapping capsBound attributes ................
	Number of unique capsBound attributes = 1
	Name = WingSurface, index = 1
Mapping capsConnect attributes ................
	Number of unique capsConnect attributes = 1
	Name = Root, index = 1
Mapping capsResponse attributes ................
	Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
	Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 4
	Name = Edge, index = 1
	Name = Body, index = 2
	Name = Root, index = 3
	Name = Wing, index = 4
Setting FEA Data
	Mesh for body = 0
	Number of nodal coordinates = 96
	Number of elements = 77
	Elemental Nodes = 0
	Elemental Rods  = 0
	Elemental Tria3 = 0
	Elemental Quad4 = 77
Setting FEA Data
	Mesh for body = 1
	Number of nodal coordinates = 1
	Number of elements = 1
	Elemental Nodes = 1
	Elemental Rods  = 0
	Elemental Tria3 = 0
	Elemental Quad4 = 0
Combining multiple FEA meshes!
	Combined Number of nodal coordinates = 97
	Combined Number of elements = 78
	Combined Elemental Nodes = 1
	Combined Elemental Rods  = 0
	Combined Elemental Tria3 = 0
	Combined Elemental Quad4 = 77
Getting vortex lattice surface data
	VLM surface name - WingSurface
	Done getting vortex lattice surface data

Getting FEA vortex lattice mesh
	Surface 1: Number of points found for aero-spline = 96
	(Re-)Combining all aerodynamic surfaces into a 'Wing', 'Canard', and/or  'Fin' single surfaces !
Aero_Reference value is NULL - No aero reference parameters set

Getting FEA materials.......
	Number of materials - 1
	Material name - aluminum
	No "materialType" specified for Material tuple aluminum, defaulting to "Isotropic"
	Done getting FEA materials

Getting FEA properties.......
	Number of properties - 2
	Property name - Body
	Property name - Edge
	Done getting FEA properties
Updating mesh element types based on properties input

Getting FEA constraints.......
	Number of constraints - 1
	Constraint name - PointConstraint
	No "constraintType" specified for Constraint tuple PointConstraint, defaulting to "ZeroDisplacement"
	Done getting FEA constraints
Support tuple is NULL - No supports applied

Getting FEA connections.......
	Number of connection tuples - 1
	Connection name - Root
	No "groupName" specified for Connection tuple Root!
	Looking for automatic connections from the use of capsConnectLink for Root
	8 automatic connections were made for capsConnect Root (node id 97)
	Done getting FEA connections
Load tuple is NULL - No loads applied
Optimization Control tuple is NULL - Default optimization control is used

Getting FEA optimization control.......
Done getting FEA Optimization Control
Design_Variable tuple is NULL - No design variables applied
Design_Constraint tuple is NULL - No design constraints applied

Getting FEA analyses.......
	Number of analyses - 1
	Analysis name - Flutter
	Done getting FEA analyses

Writing Astros grid and connectivity file (in free field format) ....
Finished writing Astros grid file

Writing subElement types (if any) - appending mesh file
Writing connection cards - appending mesh file

Writing Astros instruction file....
	Writing aero card
	Writing analysis cards
	Writing constraint cards--each subcase individually
	Writing material cards
	Writing property cards
	Writing unsteady aeroelastic cards
Note: The following floating-point exceptions are signalling: IEEE_UNDERFLOW_FLAG

real	0m0.666s
user	0m0.789s
sys	0m0.182s
+ status=0
+ set +x

=================================================
CAPS verification (using pyCAPS) case astros_Flutter_15degree.py passed (as expected)
=================================================


=================================================
+ echo 'astros_MultipleLoadCase_PyTest.py test;'
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESP126/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
astros_MultipleLoadCase_PyTest.py test;
+ python -u astros_MultipleLoadCase_PyTest.py -outLevel=0
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESP126/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
Mapping Csys attributes ................
	Number of unique Csys attributes = 0

Getting FEA coordinate systems.......
	Number of coordinate systems - 0
	No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
	Number of unique capsConstraint attributes = 1
	Name = plateEdge, index = 1
Mapping capsLoad attributes ................
	Number of unique capsLoad attributes = 1
	Name = plate, index = 1
Mapping capsBound attributes ................
	Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
	Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
	Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
	Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
	Mesh for body = 0
	Number of nodal coordinates = 16
	Number of elements = 9
	Elemental Nodes = 0
	Elemental Rods  = 0
	Elemental Tria3 = 0
	Elemental Quad4 = 9
Aero_Reference value is NULL - No aero reference parameters set

Getting FEA materials.......
	Number of materials - 1
	Material name - Madeupium
	Done getting FEA materials

Getting FEA properties.......
	Number of properties - 1
	Property name - plate
	Done getting FEA properties
Updating mesh element types based on properties input

Getting FEA constraints.......
	Number of constraints - 1
	Constraint name - edgeConstraint
	No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement"
	Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults

Getting FEA loads.......
	Number of loads - 5
	Load name - load_0
	Load name - load_1
	Load name - load_2
	Load name - load_3
	Load name - load_4
	Done getting FEA loads
Optimization Control tuple is NULL - Default optimization control is used

Getting FEA optimization control.......
Done getting FEA Optimization Control
Design_Variable tuple is NULL - No design variables applied
Design_Constraint tuple is NULL - No design constraints applied

Getting FEA analyses.......
	Number of analyses - 5
	Analysis name - load_0
	Analysis name - load_1
	Analysis name - load_2
	Analysis name - load_3
	Analysis name - load_4
	Done getting FEA analyses

Writing Astros grid and connectivity file (in free field format) ....
Finished writing Astros grid file

Writing subElement types (if any) - appending mesh file

Writing Astros instruction file....
	Warning: No constraints specified for case load_0, assuming all constraints are applied!!!!
	Warning: No constraints specified for case load_1, assuming all constraints are applied!!!!
	Warning: No constraints specified for case load_2, assuming all constraints are applied!!!!
	Warning: No constraints specified for case load_3, assuming all constraints are applied!!!!
	Warning: No constraints specified for case load_4, assuming all constraints are applied!!!!
	Writing analysis cards
	Writing load ADD cards
	Writing constraint cards--all constraints for each subcase
	Writing load ADD cards
	Writing constraint cards--all constraints for each subcase
	Writing load ADD cards
	Writing constraint cards--all constraints for each subcase
	Writing load ADD cards
	Writing constraint cards--all constraints for each subcase
	Writing load ADD cards
	Writing constraint cards--all constraints for each subcase
	Writing load cards
	Writing material cards
	Writing property cards
Note: The following floating-point exceptions are signalling: IEEE_UNDERFLOW_FLAG

real	0m0.538s
user	0m0.733s
sys	0m0.108s
+ status=0
+ set +x

=================================================
CAPS verification (using pyCAPS) case astros_MultipleLoadCase_PyTest.py passed (as expected)
=================================================


=================================================
+ echo 'astros_PyTest.py test;'
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESP126/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
astros_PyTest.py test;
+ python -u astros_PyTest.py -outLevel=0
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESP126/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt

Getting results for natural frequencies.....
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = Ribs_and_Spars, index = 1
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 0
Getting surface mesh for body 1 (of 1)
Body 1 (of 1)
Number of nodes    = 293
Number of elements = 217
Number of triangle elements      = 0
Number of quadrilateral elements = 217
----------------------------
Total number of nodes    = 293
Total number of elements = 217
Mapping Csys attributes ................
	Number of unique Csys attributes = 0

Getting FEA coordinate systems.......
	Number of coordinate systems - 0
	No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
	Number of unique capsConstraint attributes = 1
	Name = Rib_Constraint, index = 1
Mapping capsLoad attributes ................
	Number of unique capsLoad attributes = 0
Mapping capsBound attributes ................
	Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
	Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
	Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
	Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = Ribs_and_Spars, index = 1
Setting FEA Data
	Mesh for body = 0
	Number of nodal coordinates = 293
	Number of elements = 217
	Elemental Nodes = 0
	Elemental Rods  = 0
	Elemental Tria3 = 0
	Elemental Quad4 = 217
Aero_Reference value is NULL - No aero reference parameters set

Getting FEA materials.......
	Number of materials - 2
	Material name - Madeupium
	Material name - Unobtainium
	No "materialType" specified for Material tuple Unobtainium, defaulting to "Isotropic"
	Done getting FEA materials

Getting FEA properties.......
	Number of properties - 1
	Property name - Ribs_and_Spars
	Done getting FEA properties
Updating mesh element types based on properties input

Getting FEA constraints.......
	Number of constraints - 1
	Constraint name - ribConstraint
	No "constraintType" specified for Constraint tuple ribConstraint, defaulting to "ZeroDisplacement"
	Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults
Load tuple is NULL - No loads applied
Optimization Control tuple is NULL - Default optimization control is used

Getting FEA optimization control.......
Done getting FEA Optimization Control
Design_Variable tuple is NULL - No design variables applied
Design_Constraint tuple is NULL - No design constraints applied

Getting FEA analyses.......
	Number of analyses - 1
	Analysis name - EigenAnalysis
	No "analysisType" specified for Analysis tuple EigenAnalysis, defaulting to "Modal"
	Done getting FEA analyses

Writing Astros grid and connectivity file (in large field format) ....
Finished writing Astros grid file

Writing subElement types (if any) - appending mesh file

Writing Astros instruction file....
	Warning: No constraints specified for case EigenAnalysis, assuming all constraints are applied!!!!
	Writing analysis cards
	Writing constraint cards--all constraints for each subcase
	Writing material cards
	Writing property cards
Reading Astros OUT file - extracting Eigen-Values!
	Number of Eigen-Values = 10
	Loading Eigen-Value = 1
	Loading Eigen-Value = 2
	Loading Eigen-Value = 3
	Loading Eigen-Value = 4
	Loading Eigen-Value = 5
	Loading Eigen-Value = 6
	Loading Eigen-Value = 7
	Loading Eigen-Value = 8
	Loading Eigen-Value = 9
	Loading Eigen-Value = 10
Natural freq (Mode 1) = 0.02335 (Hz)
Natural freq (Mode 2) = 0.02335 (Hz)
Natural freq (Mode 3) = 0.11619 (Hz)
Natural freq (Mode 4) = 0.11619 (Hz)
Natural freq (Mode 5) = 0.14468 (Hz)
Natural freq (Mode 6) = 0.14468 (Hz)
Natural freq (Mode 7) = 0.23352 (Hz)
Natural freq (Mode 8) = 0.23352 (Hz)
Natural freq (Mode 9) = 0.30497 (Hz)
Natural freq (Mode 10) = 0.30497 (Hz)

real	0m8.300s
user	0m9.439s
sys	0m7.758s
+ status=0
+ set +x

=================================================
CAPS verification (using pyCAPS) case astros_PyTest.py passed (as expected)
=================================================


=================================================
+ echo 'astros_SingleLoadCase_PyTest.py test;'
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESP126/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
astros_SingleLoadCase_PyTest.py test;
+ python -u astros_SingleLoadCase_PyTest.py -outLevel=0
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESP126/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
Mapping Csys attributes ................
	Number of unique Csys attributes = 0

Getting FEA coordinate systems.......
	Number of coordinate systems - 0
	No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
	Number of unique capsConstraint attributes = 1
	Name = plateEdge, index = 1
Mapping capsLoad attributes ................
	Number of unique capsLoad attributes = 1
	Name = plate, index = 1
Mapping capsBound attributes ................
	Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
	Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
	Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
	Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
	Mesh for body = 0
	Number of nodal coordinates = 12
	Number of elements = 6
	Elemental Nodes = 0
	Elemental Rods  = 0
	Elemental Tria3 = 0
	Elemental Quad4 = 6
Aero_Reference value is NULL - No aero reference parameters set

Getting FEA materials.......
	Number of materials - 1
	Material name - Madeupium
	Done getting FEA materials

Getting FEA properties.......
	Number of properties - 1
	Property name - plate
	Done getting FEA properties
Updating mesh element types based on properties input

Getting FEA constraints.......
	Number of constraints - 1
	Constraint name - edgeConstraint
	No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement"
	Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults

Getting FEA loads.......
	Number of loads - 1
	Load name - appliedPressure
	Done getting FEA loads
Optimization Control tuple is NULL - Default optimization control is used

Getting FEA optimization control.......
Done getting FEA Optimization Control
Design_Variable tuple is NULL - No design variables applied
Design_Constraint tuple is NULL - No design constraints applied
Analysis tuple is NULL

Getting FEA analyses.......
	Number of analyses - 1
	Analysis name - Default
	Done getting FEA analyses

Writing Astros grid and connectivity file (in free field format) ....
Finished writing Astros grid file

Writing subElement types (if any) - appending mesh file

Writing Astros instruction file....
	Writing analysis cards
	Writing load ADD cards
	Writing constraint cards--each subcase individually
	Writing load cards
	Writing material cards
	Writing property cards
Note: The following floating-point exceptions are signalling: IEEE_UNDERFLOW_FLAG

real	0m0.447s
user	0m0.652s
sys	0m0.099s
+ status=0
+ set +x

=================================================
CAPS verification (using pyCAPS) case astros_SingleLoadCase_PyTest.py passed (as expected)
=================================================


=================================================
+ echo 'astros_ThreeBarFreq_PyTest.py test;'
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESP126/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
astros_ThreeBarFreq_PyTest.py test;
+ python -u astros_ThreeBarFreq_PyTest.py -outLevel=0
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESP126/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt

Getting results for natural frequencies.....
WARNING:: WireBody is non-manifold
Mapping Csys attributes ................
	Number of unique Csys attributes = 0

Getting FEA coordinate systems.......
	Number of coordinate systems - 0
	No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
	Number of unique capsConstraint attributes = 1
	Name = boundary, index = 1
Mapping capsLoad attributes ................
	Number of unique capsLoad attributes = 1
	Name = force, index = 1
Mapping capsBound attributes ................
	Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
	Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
	Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
	Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 3
	Name = bar1, index = 1
	Name = bar2, index = 2
	Name = bar3, index = 3
	capsIgnore attribute found for edge - 3!!
capsIgnore attribute found. Removing unneeded nodes and elements from mesh!
Removing unused nodes...
	Removed 0 (out of 4) unused nodes!
Setting FEA Data
	Mesh for body = 0
	Number of nodal coordinates = 4
	Number of elements = 3
	Elemental Nodes = 0
	Elemental Rods  = 3
	Elemental Tria3 = 0
	Elemental Quad4 = 0
Aero_Reference value is NULL - No aero reference parameters set

Getting FEA materials.......
	Number of materials - 1
	Material name - Madeupium
	Done getting FEA materials

Getting FEA properties.......
	Number of properties - 3
	Property name - bar1
	Property name - bar2
	Property name - bar3
	Done getting FEA properties
Updating mesh element types based on properties input

Getting FEA constraints.......
	Number of constraints - 1
	Constraint name - BoundaryCondition
	No "constraintType" specified for Constraint tuple BoundaryCondition, defaulting to "ZeroDisplacement"
	Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults
Load tuple is NULL - No loads applied
Optimization Control tuple is NULL - Default optimization control is used

Getting FEA optimization control.......
Done getting FEA Optimization Control
Design_Variable tuple is NULL - No design variables applied
Design_Constraint tuple is NULL - No design constraints applied

Getting FEA analyses.......
	Number of analyses - 1
	Analysis name - EigenAnalysis
	No "analysisType" specified for Analysis tuple EigenAnalysis, defaulting to "Modal"
	Done getting FEA analyses

Writing Astros grid and connectivity file (in large field format) ....
Finished writing Astros grid file

Writing subElement types (if any) - appending mesh file

Writing Astros instruction file....
	Warning: No constraints specified for case EigenAnalysis, assuming all constraints are applied!!!!
	Writing analysis cards
	Writing constraint cards--all constraints for each subcase
	Writing material cards
	Writing property cards
Reading Astros OUT file - extracting Eigen-Values!
	Number of Eigen-Values = 2
	Loading Eigen-Value = 1
	Loading Eigen-Value = 2
Natural freq (Mode 1) = 86.13400 (Hz)
Natural freq (Mode 2) = 168.53300 (Hz)

real	0m0.439s
user	0m0.643s
sys	0m0.100s
+ status=0
+ set +x

=================================================
CAPS verification (using pyCAPS) case astros_ThreeBarFreq_PyTest.py passed (as expected)
=================================================


=================================================
+ echo 'astros_ThreeBarLinkDesign_PyTest.py test;'
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESP126/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
astros_ThreeBarLinkDesign_PyTest.py test;
+ python -u astros_ThreeBarLinkDesign_PyTest.py -outLevel=0
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESP126/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
WARNING:: WireBody is non-manifold
Mapping Csys attributes ................
	Number of unique Csys attributes = 0

Getting FEA coordinate systems.......
	Number of coordinate systems - 0
	No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
	Number of unique capsConstraint attributes = 1
	Name = boundary, index = 1
Mapping capsLoad attributes ................
	Number of unique capsLoad attributes = 1
	Name = force, index = 1
Mapping capsBound attributes ................
	Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
	Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
	Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
	Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 3
	Name = bar1, index = 1
	Name = bar2, index = 2
	Name = bar3, index = 3
	capsIgnore attribute found for edge - 3!!
capsIgnore attribute found. Removing unneeded nodes and elements from mesh!
Removing unused nodes...
	Removed 0 (out of 4) unused nodes!
Setting FEA Data
	Mesh for body = 0
	Number of nodal coordinates = 4
	Number of elements = 3
	Elemental Nodes = 0
	Elemental Rods  = 3
	Elemental Tria3 = 0
	Elemental Quad4 = 0
Aero_Reference value is NULL - No aero reference parameters set

Getting FEA materials.......
	Number of materials - 1
	Material name - Madeupium
	Done getting FEA materials

Getting FEA properties.......
	Number of properties - 3
	Property name - bar1
	Property name - bar2
	Property name - bar3
	Done getting FEA properties
Updating mesh element types based on properties input

Getting FEA constraints.......
	Number of constraints - 1
	Constraint name - BoundaryCondition
	No "constraintType" specified for Constraint tuple BoundaryCondition, defaulting to "ZeroDisplacement"
	Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults

Getting FEA loads.......
	Number of loads - 1
	Load name - appliedForce
	Done getting FEA loads
Optimization Control tuple is NULL - Default optimization control is used

Getting FEA optimization control.......
Done getting FEA Optimization Control

Getting FEA design variables.......
	Number of design variables          - 3
	Design_Variable name - Bar1A
	Design_Variable name - Bar2A
	Design_Variable name - Bar3A
	Design_Variable_Relation name - Bar1A
	Design_Variable_Relation name - Bar2A
	Design_Variable_Relation name - Bar3A
	Number of design variable relations - 3
	Done getting FEA design variables

Getting FEA design constraints.......
	Number of design constraints - 3
	Design_Constraint name - stress1
	Design_Constraint name - stress2
	Design_Constraint name - stress3
Done getting FEA design constraints

Getting FEA analyses.......
	Number of analyses - 1
	Analysis name - SingleLoadCase
	Done getting FEA analyses

Writing Astros grid and connectivity file (in large field format) ....
Finished writing Astros grid file

Writing subElement types (if any) - appending mesh file

Writing Astros instruction file....
	Writing analysis cards
	Writing load ADD cards
	Writing constraint cards--each subcase individually
	Writing design constraint cards
	Writing load cards
	Writing material cards
	Writing property cards
	Writing design variable cards


Running Astros......
Done running Astros!

real	0m0.536s
user	0m0.736s
sys	0m0.104s
+ status=0
+ set +x

=================================================
CAPS verification (using pyCAPS) case astros_ThreeBarLinkDesign_PyTest.py passed (as expected)
=================================================


=================================================
+ echo 'astros_ThreeBarMultiLoad_PyTest.py test;'
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESP126/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
astros_ThreeBarMultiLoad_PyTest.py test;
+ python -u astros_ThreeBarMultiLoad_PyTest.py -outLevel=0
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESP126/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
WARNING:: WireBody is non-manifold
Mapping Csys attributes ................
	Number of unique Csys attributes = 0

Getting FEA coordinate systems.......
	Number of coordinate systems - 0
	No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
	Number of unique capsConstraint attributes = 1
	Name = boundary, index = 1
Mapping capsLoad attributes ................
	Number of unique capsLoad attributes = 1
	Name = force, index = 1
Mapping capsBound attributes ................
	Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
	Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
	Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
	Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 3
	Name = bar1, index = 1
	Name = bar2, index = 2
	Name = bar3, index = 3
	capsIgnore attribute found for edge - 3!!
capsIgnore attribute found. Removing unneeded nodes and elements from mesh!
Removing unused nodes...
	Removed 0 (out of 4) unused nodes!
Setting FEA Data
	Mesh for body = 0
	Number of nodal coordinates = 4
	Number of elements = 3
	Elemental Nodes = 0
	Elemental Rods  = 3
	Elemental Tria3 = 0
	Elemental Quad4 = 0
Aero_Reference value is NULL - No aero reference parameters set

Getting FEA materials.......
	Number of materials - 1
	Material name - Madeupium
	Done getting FEA materials

Getting FEA properties.......
	Number of properties - 3
	Property name - bar1
	Property name - bar2
	Property name - bar3
	Done getting FEA properties
Updating mesh element types based on properties input

Getting FEA constraints.......
	Number of constraints - 2
	Constraint name - conOne
	No "constraintType" specified for Constraint tuple conOne, defaulting to "ZeroDisplacement"
	Constraint name - conTwo
	No "constraintType" specified for Constraint tuple conTwo, defaulting to "ZeroDisplacement"
	Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults

Getting FEA loads.......
	Number of loads - 2
	Load name - loadOne
	Load name - loadTwo
	Done getting FEA loads
Optimization Control tuple is NULL - Default optimization control is used

Getting FEA optimization control.......
Done getting FEA Optimization Control
Design_Variable tuple is NULL - No design variables applied
Design_Constraint tuple is NULL - No design constraints applied

Getting FEA analyses.......
	Number of analyses - 2
	Analysis name - analysisOne
	Analysis name - analysisTwo
	Done getting FEA analyses

Writing Astros grid and connectivity file (in large field format) ....
Finished writing Astros grid file

Writing subElement types (if any) - appending mesh file

Writing Astros instruction file....
	Writing analysis cards
	Writing load ADD cards
	Writing constraint cards--each subcase individually
	Writing load ADD cards
	Writing constraint cards--each subcase individually
	Writing load cards
	Writing material cards
	Writing property cards

real	0m0.458s
user	0m0.660s
sys	0m0.101s
+ status=0
+ set +x

=================================================
CAPS verification (using pyCAPS) case astros_ThreeBarMultiLoad_PyTest.py passed (as expected)
=================================================


=================================================
+ echo 'astros_ThreeBar_PyTest.py test;'
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESP126/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
astros_ThreeBar_PyTest.py test;
+ python -u astros_ThreeBar_PyTest.py -outLevel=0
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESP126/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
WARNING:: WireBody is non-manifold
Mapping Csys attributes ................
	Number of unique Csys attributes = 0

Getting FEA coordinate systems.......
	Number of coordinate systems - 0
	No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
	Number of unique capsConstraint attributes = 1
	Name = boundary, index = 1
Mapping capsLoad attributes ................
	Number of unique capsLoad attributes = 1
	Name = force, index = 1
Mapping capsBound attributes ................
	Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
	Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
	Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
	Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 3
	Name = bar1, index = 1
	Name = bar2, index = 2
	Name = bar3, index = 3
	capsIgnore attribute found for edge - 3!!
capsIgnore attribute found. Removing unneeded nodes and elements from mesh!
Removing unused nodes...
	Removed 0 (out of 4) unused nodes!
Setting FEA Data
	Mesh for body = 0
	Number of nodal coordinates = 4
	Number of elements = 3
	Elemental Nodes = 0
	Elemental Rods  = 3
	Elemental Tria3 = 0
	Elemental Quad4 = 0
Aero_Reference value is NULL - No aero reference parameters set

Getting FEA materials.......
	Number of materials - 1
	Material name - Madeupium
	Done getting FEA materials

Getting FEA properties.......
	Number of properties - 3
	Property name - bar1
	Property name - bar2
	Property name - bar3
	Done getting FEA properties
Updating mesh element types based on properties input

Getting FEA constraints.......
	Number of constraints - 1
	Constraint name - BoundaryCondition
	No "constraintType" specified for Constraint tuple BoundaryCondition, defaulting to "ZeroDisplacement"
	Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults

Getting FEA loads.......
	Number of loads - 1
	Load name - appliedForce
	Done getting FEA loads
Optimization Control tuple is NULL - Default optimization control is used

Getting FEA optimization control.......
Done getting FEA Optimization Control
Design_Variable tuple is NULL - No design variables applied
Design_Constraint tuple is NULL - No design constraints applied

Getting FEA analyses.......
	Number of analyses - 1
	Analysis name - SingleLoadCase
	Done getting FEA analyses

Writing Astros grid and connectivity file (in free field format) ....
Finished writing Astros grid file

Writing subElement types (if any) - appending mesh file

Writing Astros instruction file....
	Writing analysis cards
	Writing load ADD cards
	Writing constraint cards--each subcase individually
	Writing load cards
	Writing material cards
	Writing property cards

real	0m0.441s
user	0m0.644s
sys	0m0.100s
+ status=0
+ set +x

=================================================
CAPS verification (using pyCAPS) case astros_ThreeBar_PyTest.py passed (as expected)
=================================================


=================================================
+ echo 'astros_Trim_15degree.py test;'
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESP126/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
astros_Trim_15degree.py test;
+ python -u astros_Trim_15degree.py -outLevel=0
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESP126/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
Mapping Csys attributes ................
	Number of unique Csys attributes = 0

Getting FEA coordinate systems.......
	Number of coordinate systems - 0
	No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
	Number of unique capsConstraint attributes = 1
	Name = Root_Point, index = 1
Mapping capsLoad attributes ................
	Number of unique capsLoad attributes = 1
	Name = Root_Point, index = 1
Mapping capsBound attributes ................
	Number of unique capsBound attributes = 1
	Name = WingSurface, index = 1
Mapping capsConnect attributes ................
	Number of unique capsConnect attributes = 1
	Name = Root, index = 1
Mapping capsResponse attributes ................
	Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
	Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 4
	Name = Edge, index = 1
	Name = Body, index = 2
	Name = Root, index = 3
	Name = Wing, index = 4
Setting FEA Data
	Mesh for body = 0
	Number of nodal coordinates = 96
	Number of elements = 77
	Elemental Nodes = 0
	Elemental Rods  = 0
	Elemental Tria3 = 0
	Elemental Quad4 = 77
Setting FEA Data
	Mesh for body = 1
	Number of nodal coordinates = 1
	Number of elements = 1
	Elemental Nodes = 1
	Elemental Rods  = 0
	Elemental Tria3 = 0
	Elemental Quad4 = 0
Combining multiple FEA meshes!
	Combined Number of nodal coordinates = 97
	Combined Number of elements = 78
	Combined Elemental Nodes = 1
	Combined Elemental Rods  = 0
	Combined Elemental Tria3 = 0
	Combined Elemental Quad4 = 77
Getting vortex lattice surface data
	VLM surface name - WingSurface
	Done getting vortex lattice surface data

Getting FEA vortex lattice mesh
	Surface 1: Number of points found for aero-spline = 96
	(Re-)Combining all aerodynamic surfaces into a 'Wing', 'Canard', and/or  'Fin' single surfaces !
Aero_Reference value is NULL - No aero reference parameters set

Getting FEA materials.......
	Number of materials - 1
	Material name - aluminum
	No "materialType" specified for Material tuple aluminum, defaulting to "Isotropic"
	Done getting FEA materials

Getting FEA properties.......
	Number of properties - 3
	Property name - Body
	Property name - Edge
	Property name - Root
	Done getting FEA properties
Updating mesh element types based on properties input

Getting FEA constraints.......
	Number of constraints - 1
	Constraint name - PointConstraint
	No "constraintType" specified for Constraint tuple PointConstraint, defaulting to "ZeroDisplacement"
	Done getting FEA constraints

Getting FEA supports.......
	Number of supports - 1
	Support name - PointSupport
	Done getting FEA supports

Getting FEA connections.......
	Number of connection tuples - 1
	Connection name - Root
	No "groupName" specified for Connection tuple Root!
	Looking for automatic connections from the use of capsConnectLink for Root
	8 automatic connections were made for capsConnect Root (node id 97)
	Done getting FEA connections

Getting FEA loads.......
	Number of loads - 2
	Load name - GravityLoad
	No "groupName" specified for Load tuple GravityLoad, going to use load name
	Load name - PointLoad
	Done getting FEA loads
Optimization Control tuple is NULL - Default optimization control is used

Getting FEA optimization control.......
Done getting FEA Optimization Control
Design_Variable tuple is NULL - No design variables applied
Design_Constraint tuple is NULL - No design constraints applied

Getting FEA analyses.......
	Number of analyses - 1
	Analysis name - Trim
	Done getting FEA analyses

Writing Astros grid and connectivity file (in free field format) ....
Finished writing Astros grid file

Writing subElement types (if any) - appending mesh file
Writing connection cards - appending mesh file

Writing Astros instruction file....
	Writing aeros card
	Writing analysis cards
	Writing load ADD cards
	Writing constraint cards--each subcase individually
	Writing load cards
	Writing support cards
	Writing material cards
	Writing property cards
	Writing aeroelastic cards
Note: The following floating-point exceptions are signalling: IEEE_UNDERFLOW_FLAG

real	0m0.645s
user	0m0.790s
sys	0m0.160s
+ status=0
+ set +x

=================================================
CAPS verification (using pyCAPS) case astros_Trim_15degree.py passed (as expected)
=================================================


=================================================
+ echo 'nastran_AGARD445_PyTest.py test;'
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESP126/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
nastran_AGARD445_PyTest.py test;
+ python -u nastran_AGARD445_PyTest.py -outLevel=0 -noAnalysis
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESP126/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = yatesPlate, index = 1
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 0
Getting surface mesh for body 1 (of 1)
Body 1 (of 1)
Number of nodes    = 49
Number of elements = 36
Number of triangle elements      = 0
Number of quadrilateral elements = 36
----------------------------
Total number of nodes    = 49
Total number of elements = 36
Mapping Csys attributes ................
	Number of unique Csys attributes = 0

Getting FEA coordinate systems.......
	Number of coordinate systems - 0
	No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
	Number of unique capsConstraint attributes = 1
	Name = constEdge, index = 1
Mapping capsLoad attributes ................
	Number of unique capsLoad attributes = 1
	Name = force, index = 1
Mapping capsBound attributes ................
	Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
	Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
	Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
	Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = yatesPlate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
	Mesh for body = 0
	Number of nodal coordinates = 49
	Number of elements = 36
	Elemental Nodes = 0
	Elemental Rods  = 0
	Elemental Tria3 = 0
	Elemental Quad4 = 36
Aero_Reference value is NULL - No aero reference parameters set

Getting FEA materials.......
	Number of materials - 1
	Material name - Mahogany
	Done getting FEA materials

Getting FEA properties.......
	Number of properties - 1
	Property name - yatesPlate
	Done getting FEA properties
Updating mesh element types based on properties input

Getting FEA constraints.......
	Number of constraints - 1
	Constraint name - edgeConstraint
	No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement"
	Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults
Load tuple is NULL - No loads applied
Design_Variable tuple is NULL - No design variables applied
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Mass_Increment tuple is NULL - No mass increments applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied

Getting FEA analyses.......
	Number of analyses - 1
	Analysis name - EigenAnalysis
	No "analysisType" specified for Analysis tuple EigenAnalysis, defaulting to "Modal"
	Done getting FEA analyses

Writing Nastran grid and connectivity file (in free field format) ....
Finished writing Nastran grid file

Writing subElement types (if any) - appending mesh file
	Writing mass increment set

Writing Nastran instruction file....
	Warning: No constraints specified for case EigenAnalysis, assuming all constraints are applied!!!!
	Warning: No loads specified for case EigenAnalysis!!!!
	Writing mass increment cards
	Writing analysis cards, 0
	Writing combined constraint cards
	Writing constraint cards
	Writing material cards
	Writing property cards
	Done writing aeroelastic cards
	Done writing files


Running Nastran......
Done running Nastran!

Getting results natural frequencies.....
Reading Nastran FO6 file - extracting Eigen-Values!
	Number of Eigen-Values = 132
	Loading Eigen-Value = 1
	Loading Eigen-Value = 2
	Loading Eigen-Value = 3
	Loading Eigen-Value = 4
	Loading Eigen-Value = 5
	Loading Eigen-Value = 6
	Loading Eigen-Value = 7
	Loading Eigen-Value = 8
	Loading Eigen-Value = 9
	Loading Eigen-Value = 10
	Loading Eigen-Value = 11
	Loading Eigen-Value = 12
	Loading Eigen-Value = 13
	Loading Eigen-Value = 14
	Loading Eigen-Value = 15
	Loading Eigen-Value = 16
	Loading Eigen-Value = 17
	Loading Eigen-Value = 18
	Loading Eigen-Value = 19
	Loading Eigen-Value = 20
	Loading Eigen-Value = 21
	Loading Eigen-Value = 22
	Loading Eigen-Value = 23
	Loading Eigen-Value = 24
	Loading Eigen-Value = 25
	Loading Eigen-Value = 26
	Loading Eigen-Value = 27
	Loading Eigen-Value = 28
	Loading Eigen-Value = 29
	Loading Eigen-Value = 30
	Loading Eigen-Value = 31
	Loading Eigen-Value = 32
	Loading Eigen-Value = 33
	Loading Eigen-Value = 34
	Loading Eigen-Value = 35
	Loading Eigen-Value = 36
	Loading Eigen-Value = 37
	Loading Eigen-Value = 38
	Loading Eigen-Value = 39
	Loading Eigen-Value = 40
	Loading Eigen-Value = 41
	Loading Eigen-Value = 42
	Loading Eigen-Value = 43
	Loading Eigen-Value = 44
	Loading Eigen-Value = 45
	Loading Eigen-Value = 46
	Loading Eigen-Value = 47
	Loading Eigen-Value = 48
	Loading Eigen-Value = 49
	Loading Eigen-Value = 50
	Loading Eigen-Value = 51
	Loading Eigen-Value = 52
	Loading Eigen-Value = 53
	Loading Eigen-Value = 54
	Loading Eigen-Value = 55
	Loading Eigen-Value = 56
	Loading Eigen-Value = 57
	Loading Eigen-Value = 58
	Loading Eigen-Value = 59
	Loading Eigen-Value = 60
	Loading Eigen-Value = 61
	Loading Eigen-Value = 62
	Loading Eigen-Value = 63
	Loading Eigen-Value = 64
	Loading Eigen-Value = 65
	Loading Eigen-Value = 66
	Loading Eigen-Value = 67
	Loading Eigen-Value = 68
	Loading Eigen-Value = 69
	Loading Eigen-Value = 70
	Loading Eigen-Value = 71
	Loading Eigen-Value = 72
	Loading Eigen-Value = 73
	Loading Eigen-Value = 74
	Loading Eigen-Value = 75
	Loading Eigen-Value = 76
	Loading Eigen-Value = 77
	Loading Eigen-Value = 78
	Loading Eigen-Value = 79
	Loading Eigen-Value = 80
	Loading Eigen-Value = 81
	Loading Eigen-Value = 82
	Loading Eigen-Value = 83
	Loading Eigen-Value = 84
	Loading Eigen-Value = 85
	Loading Eigen-Value = 86
	Loading Eigen-Value = 87
	Loading Eigen-Value = 88
	Loading Eigen-Value = 89
	Loading Eigen-Value = 90
	Loading Eigen-Value = 91
	Loading Eigen-Value = 92
	Loading Eigen-Value = 93
	Loading Eigen-Value = 94
	Loading Eigen-Value = 95
	Loading Eigen-Value = 96
	Loading Eigen-Value = 97
	Loading Eigen-Value = 98
	Loading Eigen-Value = 99
	Loading Eigen-Value = 100
	Loading Eigen-Value = 101
	Loading Eigen-Value = 102
	Loading Eigen-Value = 103
	Loading Eigen-Value = 104
	Loading Eigen-Value = 105
	Loading Eigen-Value = 106
	Loading Eigen-Value = 107
	Loading Eigen-Value = 108
	Loading Eigen-Value = 109
	Loading Eigen-Value = 110
	Loading Eigen-Value = 111
	Loading Eigen-Value = 112
	Loading Eigen-Value = 113
	Loading Eigen-Value = 114
	Loading Eigen-Value = 115
	Loading Eigen-Value = 116
	Loading Eigen-Value = 117
	Loading Eigen-Value = 118
	Loading Eigen-Value = 119
	Loading Eigen-Value = 120
	Loading Eigen-Value = 121
	Loading Eigen-Value = 122
	Loading Eigen-Value = 123
	Loading Eigen-Value = 124
	Loading Eigen-Value = 125
	Loading Eigen-Value = 126
	Loading Eigen-Value = 127
	Loading Eigen-Value = 128
	Loading Eigen-Value = 129
	Loading Eigen-Value = 130
	Loading Eigen-Value = 131
	Loading Eigen-Value = 132
Natural freq (Mode 0) = 9.44 (Hz)
Natural freq (Mode 1) = 35.99 (Hz)
Natural freq (Mode 2) = 50.58 (Hz)
Natural freq (Mode 3) = 93.48 (Hz)
Natural freq (Mode 4) = 122.58 (Hz)
Natural freq (Mode 5) = 142.96 (Hz)
Natural freq (Mode 6) = 153.81 (Hz)
Natural freq (Mode 7) = 201.18 (Hz)
Natural freq (Mode 8) = 203.69 (Hz)
Natural freq (Mode 9) = 218.54 (Hz)
Natural freq (Mode 10) = 244.49 (Hz)
Natural freq (Mode 11) = 267.52 (Hz)
Natural freq (Mode 12) = 282.33 (Hz)
Natural freq (Mode 13) = 284.46 (Hz)
Natural freq (Mode 14) = 311.84 (Hz)
Natural freq (Mode 15) = 328.87 (Hz)
Natural freq (Mode 16) = 334.68 (Hz)
Natural freq (Mode 17) = 346.25 (Hz)
Natural freq (Mode 18) = 362.24 (Hz)
Natural freq (Mode 19) = 368.68 (Hz)
Natural freq (Mode 20) = 377.76 (Hz)
Natural freq (Mode 21) = 393.48 (Hz)
Natural freq (Mode 22) = 403.01 (Hz)
Natural freq (Mode 23) = 415.98 (Hz)
Natural freq (Mode 24) = 430.66 (Hz)
Natural freq (Mode 25) = 456.25 (Hz)
Natural freq (Mode 26) = 460.70 (Hz)
Natural freq (Mode 27) = 478.12 (Hz)
Natural freq (Mode 28) = 500.39 (Hz)
Natural freq (Mode 29) = 510.45 (Hz)
Natural freq (Mode 30) = 514.48 (Hz)
Natural freq (Mode 31) = 519.72 (Hz)
Natural freq (Mode 32) = 531.28 (Hz)
Natural freq (Mode 33) = 553.76 (Hz)
Natural freq (Mode 34) = 566.65 (Hz)
Natural freq (Mode 35) = 591.27 (Hz)
Natural freq (Mode 36) = 611.71 (Hz)
Natural freq (Mode 37) = 612.08 (Hz)
Natural freq (Mode 38) = 624.35 (Hz)
Natural freq (Mode 39) = 650.56 (Hz)
Natural freq (Mode 40) = 670.08 (Hz)
Natural freq (Mode 41) = 721.11 (Hz)
Natural freq (Mode 42) = 732.49 (Hz)
Natural freq (Mode 43) = 751.28 (Hz)
Natural freq (Mode 44) = 814.54 (Hz)
Natural freq (Mode 45) = 883.96 (Hz)
Natural freq (Mode 46) = 951.75 (Hz)
Natural freq (Mode 47) = 975.90 (Hz)
Natural freq (Mode 48) = 1290.98 (Hz)
Natural freq (Mode 49) = 1356.05 (Hz)
Natural freq (Mode 50) = 1506.01 (Hz)
Natural freq (Mode 51) = 1619.60 (Hz)
Natural freq (Mode 52) = 1631.13 (Hz)
Natural freq (Mode 53) = 1745.44 (Hz)
Natural freq (Mode 54) = 1904.47 (Hz)
Natural freq (Mode 55) = 2010.78 (Hz)
Natural freq (Mode 56) = 2031.59 (Hz)
Natural freq (Mode 57) = 2108.70 (Hz)
Natural freq (Mode 58) = 2215.97 (Hz)
Natural freq (Mode 59) = 2306.66 (Hz)
Natural freq (Mode 60) = 2320.15 (Hz)
Natural freq (Mode 61) = 2390.78 (Hz)
Natural freq (Mode 62) = 2494.64 (Hz)
Natural freq (Mode 63) = 2560.50 (Hz)
Natural freq (Mode 64) = 2584.60 (Hz)
Natural freq (Mode 65) = 2587.28 (Hz)
Natural freq (Mode 66) = 2659.52 (Hz)
Natural freq (Mode 67) = 2737.71 (Hz)
Natural freq (Mode 68) = 2789.18 (Hz)
Natural freq (Mode 69) = 2840.95 (Hz)
Natural freq (Mode 70) = 2888.34 (Hz)
Natural freq (Mode 71) = 2967.46 (Hz)
Natural freq (Mode 72) = 3051.49 (Hz)
Natural freq (Mode 73) = 3112.98 (Hz)
Natural freq (Mode 74) = 3139.85 (Hz)
Natural freq (Mode 75) = 3247.88 (Hz)
Natural freq (Mode 76) = 3303.45 (Hz)
Natural freq (Mode 77) = 3344.57 (Hz)
Natural freq (Mode 78) = 3466.41 (Hz)
Natural freq (Mode 79) = 3489.29 (Hz)
Natural freq (Mode 80) = 3562.75 (Hz)
Natural freq (Mode 81) = 3651.56 (Hz)
Natural freq (Mode 82) = 3712.84 (Hz)
Natural freq (Mode 83) = 3761.27 (Hz)
Natural freq (Mode 84) = 3806.30 (Hz)
Natural freq (Mode 85) = 3902.83 (Hz)
Natural freq (Mode 86) = 3961.00 (Hz)
Natural freq (Mode 87) = 4028.45 (Hz)
Natural freq (Mode 88) = 4110.02 (Hz)
Natural freq (Mode 89) = 4191.05 (Hz)
Natural freq (Mode 90) = 4202.44 (Hz)
Natural freq (Mode 91) = 4299.35 (Hz)
Natural freq (Mode 92) = 4376.59 (Hz)
Natural freq (Mode 93) = 4425.85 (Hz)
Natural freq (Mode 94) = 4501.49 (Hz)
Natural freq (Mode 95) = 4518.77 (Hz)
Natural freq (Mode 96) = 4586.52 (Hz)
Natural freq (Mode 97) = 4621.28 (Hz)
Natural freq (Mode 98) = 4678.52 (Hz)
Natural freq (Mode 99) = 4733.41 (Hz)
Natural freq (Mode 100) = 4788.76 (Hz)
Natural freq (Mode 101) = 4816.52 (Hz)
Natural freq (Mode 102) = 4942.47 (Hz)
Natural freq (Mode 103) = 4997.55 (Hz)
Natural freq (Mode 104) = 5045.56 (Hz)
Natural freq (Mode 105) = 5120.59 (Hz)
Natural freq (Mode 106) = 5155.17 (Hz)
Natural freq (Mode 107) = 5325.08 (Hz)
Natural freq (Mode 108) = 5474.54 (Hz)
Natural freq (Mode 109) = 5512.48 (Hz)
Natural freq (Mode 110) = 5525.67 (Hz)
Natural freq (Mode 111) = 5576.25 (Hz)
Natural freq (Mode 112) = 5647.01 (Hz)
Natural freq (Mode 113) = 5841.96 (Hz)
Natural freq (Mode 114) = 6096.57 (Hz)
Natural freq (Mode 115) = 6188.63 (Hz)
Natural freq (Mode 116) = 6328.76 (Hz)
Natural freq (Mode 117) = 6428.94 (Hz)
Natural freq (Mode 118) = 6468.91 (Hz)
Natural freq (Mode 119) = 6958.88 (Hz)
Natural freq (Mode 120) = 7050.41 (Hz)
Natural freq (Mode 121) = 7389.46 (Hz)
Natural freq (Mode 122) = 7464.28 (Hz)
Natural freq (Mode 123) = 7559.48 (Hz)
Natural freq (Mode 124) = 8076.62 (Hz)
Natural freq (Mode 125) = 8344.67 (Hz)
Natural freq (Mode 126) = 8685.13 (Hz)
Natural freq (Mode 127) = 9093.83 (Hz)
Natural freq (Mode 128) = 9351.46 (Hz)
Natural freq (Mode 129) = 10123.65 (Hz)
Natural freq (Mode 130) = 10828.55 (Hz)
Natural freq (Mode 131) = 11674.11 (Hz)

real	0m0.317s
user	0m0.381s
sys	0m0.131s
+ status=0
+ set +x

=================================================
CAPS verification (using pyCAPS) case nastran_AGARD445_PyTest.py passed (as expected)
=================================================


=================================================
+ echo 'nastran_Aeroelastic_PyTest.py test;'
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESP126/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
nastran_Aeroelastic_PyTest.py test;
+ python -u nastran_Aeroelastic_PyTest.py -outLevel=0 -noAnalysis
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESP126/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 7
	Name = Ribs, index = 1
	Name = Skin, index = 2
	Name = Spar1, index = 3
	Name = Rib_Root, index = 4
	Name = Spar2, index = 5
	Name = Rib_Root_Point, index = 6
	Name = Wing, index = 7
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 2
	Name = LeadingEdge, index = 1
	Name = TrailingEdge, index = 2
Getting surface mesh for body 1 (of 4)
Getting surface mesh for body 2 (of 4)
Getting surface mesh for body 3 (of 4)
Getting surface mesh for body 4 (of 4)
Body 1 (of 4)
Number of nodes    = 1373
Number of elements = 1510
Number of triangle elements      = 0
Number of quadrilateral elements = 1510
Body 2 (of 4)
Number of nodes    = 1
Number of elements = 0
Number of triangle elements      = 0
Number of quadrilateral elements = 0
Body 3 (of 4)
Number of nodes    = 17
Number of elements = 10
Number of triangle elements      = 0
Number of quadrilateral elements = 10
Body 4 (of 4)
Number of nodes    = 17
Number of elements = 10
Number of triangle elements      = 0
Number of quadrilateral elements = 10
----------------------------
Total number of nodes    = 1408
Total number of elements = 1530
Mapping Csys attributes ................
	Number of unique Csys attributes = 0

Getting FEA coordinate systems.......
	Number of coordinate systems - 0
	No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
	Number of unique capsConstraint attributes = 1
	Name = Rib_Root_Point, index = 1
Mapping capsLoad attributes ................
	Number of unique capsLoad attributes = 0
Mapping capsBound attributes ................
	Number of unique capsBound attributes = 1
	Name = Skin_Top, index = 1
Mapping capsConnect attributes ................
	Number of unique capsConnect attributes = 1
	Name = Rib_Root, index = 1
Mapping capsResponse attributes ................
	Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
	Number of unique capsReference attributes = 1
	Name = Rib_Root_Point, index = 1
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 7
	Name = Ribs, index = 1
	Name = Skin, index = 2
	Name = Spar1, index = 3
	Name = Rib_Root, index = 4
	Name = Spar2, index = 5
	Name = Rib_Root_Point, index = 6
	Name = Wing, index = 7
Setting FEA Data
	Mesh for body = 0
	Number of nodal coordinates = 1373
	Number of elements = 1510
	Elemental Nodes = 0
	Elemental Rods  = 0
	Elemental Tria3 = 0
	Elemental Quad4 = 1510
Setting FEA Data
	Mesh for body = 1
	Number of nodal coordinates = 1
	Number of elements = 1
	Elemental Nodes = 1
	Elemental Rods  = 0
	Elemental Tria3 = 0
	Elemental Quad4 = 0
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Setting FEA Data
	Mesh for body = 2
	Number of nodal coordinates = 17
	Number of elements = 10
	Elemental Nodes = 0
	Elemental Rods  = 0
	Elemental Tria3 = 0
	Elemental Quad4 = 10
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Setting FEA Data
	Mesh for body = 3
	Number of nodal coordinates = 17
	Number of elements = 10
	Elemental Nodes = 0
	Elemental Rods  = 0
	Elemental Tria3 = 0
	Elemental Quad4 = 10
Combining multiple FEA meshes!
	Combined Number of nodal coordinates = 1408
	Combined Number of elements = 1531
	Combined Elemental Nodes = 1
	Combined Elemental Rods  = 0
	Combined Elemental Tria3 = 0
	Combined Elemental Quad4 = 1530
Getting vortex lattice surface data
	VLM surface name - Skin_Top
	Done getting vortex lattice surface data

Getting FEA vortex lattice mesh
	Surface 1: Number of points found for aero-spline = 300
Aero_Reference value is NULL - No aero reference parameters set

Getting FEA materials.......
	Number of materials - 1
	Material name - Unobtainium
	No "materialType" specified for Material tuple Unobtainium, defaulting to "Isotropic"
	Done getting FEA materials

Getting FEA properties.......
	Number of properties - 5
	Property name - Rib_Root
	No "material" specified for Property tuple Rib_Root, defaulting to an index of 1
	Property name - Ribs
	No "material" specified for Property tuple Ribs, defaulting to an index of 1
	Property name - Skin
	No "material" specified for Property tuple Skin, defaulting to an index of 1
	Property name - Spar1
	No "material" specified for Property tuple Spar1, defaulting to an index of 1
	Property name - Spar2
	No "material" specified for Property tuple Spar2, defaulting to an index of 1
	Done getting FEA properties
Updating mesh element types based on properties input

Getting FEA constraints.......
	Number of constraints - 1
	Constraint name - ribConstraint
	No "constraintType" specified for Constraint tuple ribConstraint, defaulting to "ZeroDisplacement"
	Done getting FEA constraints

Getting FEA supports.......
	Number of supports - 1
	Support name - ribSupport
	Done getting FEA supports

Getting FEA connections.......
	Number of connection tuples - 1
	Connection name - Rib_Root
	No "groupName" specified for Connection tuple Rib_Root!
	Looking for automatic connections from the use of capsConnectLink for Rib_Root
	93 automatic connections were made for capsConnect Rib_Root (node id 1374)
	Done getting FEA connections
Load tuple is NULL - No loads applied
Design_Variable tuple is NULL - No design variables applied
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Mass_Increment tuple is NULL - No mass increments applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied

Getting FEA analyses.......
	Number of analyses - 1
	Analysis name - Trim1
	Done getting FEA analyses

Writing Nastran grid and connectivity file (in free field format) ....
Finished writing Nastran grid file

Writing subElement types (if any) - appending mesh file
Writing connection cards - appending mesh file
	Writing mass increment set

Writing Nastran instruction file....
	Warning: No loads specified for case Trim1!!!!
	Writing mass increment cards
	Writing aeros card
	Writing aestat cards
	Writing analysis cards, 0
	Writing constraint ADD cards
	Writing constraint cards
	Writing support cards
	Writing material cards
	Writing property cards
	Writing aeroelastic cards
	Done writing aeroelastic cards
	Done writing files


Running Nastran......
Done running Nastran!

real	0m3.527s
user	0m9.958s
sys	0m4.714s
+ status=0
+ set +x

=================================================
CAPS verification (using pyCAPS) case nastran_Aeroelastic_PyTest.py passed (as expected)
=================================================


=================================================
+ echo 'nastran_CompositeWingDesign_PyTest.py test;'
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESP126/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
nastran_CompositeWingDesign_PyTest.py test;
+ python -u nastran_CompositeWingDesign_PyTest.py -outLevel=0 -noAnalysis
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESP126/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = wing, index = 1
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 0
Getting surface mesh for body 1 (of 1)
Body 1 (of 1)
Number of nodes    = 323
Number of elements = 262
Number of triangle elements      = 0
Number of quadrilateral elements = 262
----------------------------
Total number of nodes    = 323
Total number of elements = 262
Mapping Csys attributes ................
	Number of unique Csys attributes = 1
	Name = wing, index = 1

Getting FEA coordinate systems.......
	Number of coordinate systems - 1
	Coordinate system name - wing
Mapping capsConstraint attributes ................
	Number of unique capsConstraint attributes = 1
	Name = root, index = 1
Mapping capsLoad attributes ................
	Number of unique capsLoad attributes = 1
	Name = wing, index = 1
Mapping capsBound attributes ................
	Number of unique capsBound attributes = 1
	Name = wing, index = 1
Mapping capsConnect attributes ................
	Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
	Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
	Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = wing, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 5 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 6 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 7 of face 1, unable to assign a boundary index value
Setting FEA Data
	Mesh for body = 0
	Number of nodal coordinates = 323
	Number of elements = 262
	Elemental Nodes = 0
	Elemental Rods  = 0
	Elemental Tria3 = 0
	Elemental Quad4 = 262
Aero_Reference value is NULL - No aero reference parameters set

Getting FEA materials.......
	Number of materials - 2
	Material name - Aluminum
	No "materialType" specified for Material tuple Aluminum, defaulting to "Isotropic"
	Material name - Graphite_epoxy
	Done getting FEA materials

Getting FEA properties.......
	Number of properties - 1
	Property name - wing
	Done getting FEA properties
Updating mesh element types based on properties input

Getting FEA constraints.......
	Number of constraints - 1
	Constraint name - BoundaryCondition
	No "constraintType" specified for Constraint tuple BoundaryCondition, defaulting to "ZeroDisplacement"
	Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults

Getting FEA loads.......
	Number of loads - 1
	Load name - appliedPressure
	Done getting FEA loads

Getting FEA design variables.......
	Number of design variables          - 8
	Design_Variable name - L1
	Design_Variable name - L2
	Design_Variable name - L3
	Design_Variable name - L4
	Design_Variable name - L5
	Design_Variable name - L6
	Design_Variable name - L7
	Design_Variable name - L8
	Design_Variable_Relation name - L1R
	Design_Variable_Relation name - L2R
	Design_Variable_Relation name - L3R
	Design_Variable_Relation name - L4R
	Design_Variable_Relation name - L5R
	Design_Variable_Relation name - L6R
	Design_Variable_Relation name - L7R
	Design_Variable_Relation name - L8R
	Number of design variable relations - 8
	Done getting FEA design variables

Getting FEA design constraints.......
	Number of design constraints - 8
	Design_Constraint name - stress1
	Design_Constraint name - stress2
	Design_Constraint name - stress3
	Design_Constraint name - stress4
	Design_Constraint name - stress5
	Design_Constraint name - stress6
	Design_Constraint name - stress7
	Design_Constraint name - stress8
Done getting FEA design constraints
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Mass_Increment tuple is NULL - No mass increments applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied

Getting FEA analyses.......
	Number of analyses - 1
	Analysis name - StaticAnalysis
	Done getting FEA analyses

Writing Nastran grid and connectivity file (in large field format) ....
Finished writing Nastran grid file

Writing subElement types (if any) - appending mesh file
	Writing mass increment set

Writing Nastran instruction file....
	Writing mass increment cards
	Writing analysis cards, 0
	Writing load ADD cards
	Writing constraint ADD cards
	Writing design constraint ADD cards
	Writing load cards
	Writing constraint cards
	Writing material cards
	Writing property cards
	Writing coordinate system cards
	Writing design variable cards
	Writing design variable relation cards
	Writing design constraints and responses cards
	Done writing aeroelastic cards
	Done writing files


Running Nastran......
Done running Nastran!

real	0m0.548s
user	0m0.740s
sys	0m0.115s
+ status=0
+ set +x

=================================================
CAPS verification (using pyCAPS) case nastran_CompositeWingDesign_PyTest.py passed (as expected)
=================================================


=================================================
+ echo 'nastran_CompositeWingFreq_PyTest.py test;'
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESP126/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
nastran_CompositeWingFreq_PyTest.py test;
+ python -u nastran_CompositeWingFreq_PyTest.py -outLevel=0 -noAnalysis
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESP126/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = wing, index = 1
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 0
Getting surface mesh for body 1 (of 1)
Body 1 (of 1)
Number of nodes    = 323
Number of elements = 262
Number of triangle elements      = 0
Number of quadrilateral elements = 262
----------------------------
Total number of nodes    = 323
Total number of elements = 262
Mapping Csys attributes ................
	Number of unique Csys attributes = 1
	Name = wing, index = 1

Getting FEA coordinate systems.......
	Number of coordinate systems - 1
	Coordinate system name - wing
Mapping capsConstraint attributes ................
	Number of unique capsConstraint attributes = 1
	Name = root, index = 1
Mapping capsLoad attributes ................
	Number of unique capsLoad attributes = 1
	Name = wing, index = 1
Mapping capsBound attributes ................
	Number of unique capsBound attributes = 1
	Name = wing, index = 1
Mapping capsConnect attributes ................
	Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
	Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
	Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = wing, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 5 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 6 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 7 of face 1, unable to assign a boundary index value
Setting FEA Data
	Mesh for body = 0
	Number of nodal coordinates = 323
	Number of elements = 262
	Elemental Nodes = 0
	Elemental Rods  = 0
	Elemental Tria3 = 0
	Elemental Quad4 = 262
Aero_Reference value is NULL - No aero reference parameters set

Getting FEA materials.......
	Number of materials - 2
	Material name - Aluminum
	No "materialType" specified for Material tuple Aluminum, defaulting to "Isotropic"
	Material name - Graphite_epoxy
	Done getting FEA materials

Getting FEA properties.......
	Number of properties - 1
	Property name - wing
	Done getting FEA properties
Updating mesh element types based on properties input

Getting FEA constraints.......
	Number of constraints - 1
	Constraint name - root
	No "constraintType" specified for Constraint tuple root, defaulting to "ZeroDisplacement"
	Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults
Load tuple is NULL - No loads applied
Design_Variable tuple is NULL - No design variables applied
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Mass_Increment tuple is NULL - No mass increments applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied

Getting FEA analyses.......
	Number of analyses - 1
	Analysis name - EigenAnalysis
	No "analysisType" specified for Analysis tuple EigenAnalysis, defaulting to "Modal"
	Done getting FEA analyses

Writing Nastran grid and connectivity file (in large field format) ....
Finished writing Nastran grid file

Writing subElement types (if any) - appending mesh file
	Writing mass increment set

Writing Nastran instruction file....
	Warning: No constraints specified for case EigenAnalysis, assuming all constraints are applied!!!!
	Warning: No loads specified for case EigenAnalysis!!!!
	Writing mass increment cards
	Writing analysis cards, 0
	Writing combined constraint cards
	Writing constraint cards
	Writing material cards
	Writing property cards
	Writing coordinate system cards
	Done writing aeroelastic cards
	Done writing files


Running Nastran......
Done running Nastran!

Getting results for natural frequencies.....
Reading Nastran FO6 file - extracting Eigen-Values!
	Number of Eigen-Values = 1779
	Loading Eigen-Value = 1
	Loading Eigen-Value = 2
	Loading Eigen-Value = 3
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	Loading Eigen-Value = 1107
	Loading Eigen-Value = 1108
	Loading Eigen-Value = 1109
	Loading Eigen-Value = 1110
	Loading Eigen-Value = 1111
	Loading Eigen-Value = 1112
	Loading Eigen-Value = 1113
	Loading Eigen-Value = 1114
	Loading Eigen-Value = 1115
	Loading Eigen-Value = 1116
	Loading Eigen-Value = 1117
	Loading Eigen-Value = 1118
	Loading Eigen-Value = 1119
	Loading Eigen-Value = 1120
	Loading Eigen-Value = 1121
	Loading Eigen-Value = 1122
	Loading Eigen-Value = 1123
	Loading Eigen-Value = 1124
	Loading Eigen-Value = 1125
	Loading Eigen-Value = 1126
	Loading Eigen-Value = 1127
	Loading Eigen-Value = 1128
	Loading Eigen-Value = 1129
	Loading Eigen-Value = 1130
	Loading Eigen-Value = 1131
	Loading Eigen-Value = 1132
	Loading Eigen-Value = 1133
	Loading Eigen-Value = 1134
	Loading Eigen-Value = 1135
	Loading Eigen-Value = 1136
	Loading Eigen-Value = 1137
	Loading Eigen-Value = 1138
	Loading Eigen-Value = 1139
	Loading Eigen-Value = 1140
	Loading Eigen-Value = 1141
	Loading Eigen-Value = 1142
	Loading Eigen-Value = 1143
	Loading Eigen-Value = 1144
	Loading Eigen-Value = 1145
	Loading Eigen-Value = 1146
	Loading Eigen-Value = 1147
	Loading Eigen-Value = 1148
	Loading Eigen-Value = 1149
	Loading Eigen-Value = 1150
	Loading Eigen-Value = 1151
	Loading Eigen-Value = 1152
	Loading Eigen-Value = 1153
	Loading Eigen-Value = 1154
	Loading Eigen-Value = 1155
	Loading Eigen-Value = 1156
	Loading Eigen-Value = 1157
	Loading Eigen-Value = 1158
	Loading Eigen-Value = 1159
	Loading Eigen-Value = 1160
	Loading Eigen-Value = 1161
	Loading Eigen-Value = 1162
	Loading Eigen-Value = 1163
	Loading Eigen-Value = 1164
	Loading Eigen-Value = 1165
	Loading Eigen-Value = 1166
	Loading Eigen-Value = 1167
	Loading Eigen-Value = 1168
	Loading Eigen-Value = 1169
	Loading Eigen-Value = 1170
	Loading Eigen-Value = 1171
	Loading Eigen-Value = 1172
	Loading Eigen-Value = 1173
	Loading Eigen-Value = 1174
	Loading Eigen-Value = 1175
	Loading Eigen-Value = 1176
	Loading Eigen-Value = 1177
	Loading Eigen-Value = 1178
	Loading Eigen-Value = 1179
	Loading Eigen-Value = 1180
	Loading Eigen-Value = 1181
	Loading Eigen-Value = 1182
	Loading Eigen-Value = 1183
	Loading Eigen-Value = 1184
	Loading Eigen-Value = 1185
	Loading Eigen-Value = 1186
	Loading Eigen-Value = 1187
	Loading Eigen-Value = 1188
	Loading Eigen-Value = 1189
	Loading Eigen-Value = 1190
	Loading Eigen-Value = 1191
	Loading Eigen-Value = 1192
	Loading Eigen-Value = 1193
	Loading Eigen-Value = 1194
	Loading Eigen-Value = 1195
	Loading Eigen-Value = 1196
	Loading Eigen-Value = 1197
	Loading Eigen-Value = 1198
	Loading Eigen-Value = 1199
	Loading Eigen-Value = 1200
	Loading Eigen-Value = 1201
	Loading Eigen-Value = 1202
	Loading Eigen-Value = 1203
	Loading Eigen-Value = 1204
	Loading Eigen-Value = 1205
	Loading Eigen-Value = 1206
	Loading Eigen-Value = 1207
	Loading Eigen-Value = 1208
	Loading Eigen-Value = 1209
	Loading Eigen-Value = 1210
	Loading Eigen-Value = 1211
	Loading Eigen-Value = 1212
	Loading Eigen-Value = 1213
	Loading Eigen-Value = 1214
	Loading Eigen-Value = 1215
	Loading Eigen-Value = 1216
	Loading Eigen-Value = 1217
	Loading Eigen-Value = 1218
	Loading Eigen-Value = 1219
	Loading Eigen-Value = 1220
	Loading Eigen-Value = 1221
	Loading Eigen-Value = 1222
	Loading Eigen-Value = 1223
	Loading Eigen-Value = 1224
	Loading Eigen-Value = 1225
	Loading Eigen-Value = 1226
	Loading Eigen-Value = 1227
	Loading Eigen-Value = 1228
	Loading Eigen-Value = 1229
	Loading Eigen-Value = 1230
	Loading Eigen-Value = 1231
	Loading Eigen-Value = 1232
	Loading Eigen-Value = 1233
	Loading Eigen-Value = 1234
	Loading Eigen-Value = 1235
	Loading Eigen-Value = 1236
	Loading Eigen-Value = 1237
	Loading Eigen-Value = 1238
	Loading Eigen-Value = 1239
	Loading Eigen-Value = 1240
	Loading Eigen-Value = 1241
	Loading Eigen-Value = 1242
	Loading Eigen-Value = 1243
	Loading Eigen-Value = 1244
	Loading Eigen-Value = 1245
	Loading Eigen-Value = 1246
	Loading Eigen-Value = 1247
	Loading Eigen-Value = 1248
	Loading Eigen-Value = 1249
	Loading Eigen-Value = 1250
	Loading Eigen-Value = 1251
	Loading Eigen-Value = 1252
	Loading Eigen-Value = 1253
	Loading Eigen-Value = 1254
	Loading Eigen-Value = 1255
	Loading Eigen-Value = 1256
	Loading Eigen-Value = 1257
	Loading Eigen-Value = 1258
	Loading Eigen-Value = 1259
	Loading Eigen-Value = 1260
	Loading Eigen-Value = 1261
	Loading Eigen-Value = 1262
	Loading Eigen-Value = 1263
	Loading Eigen-Value = 1264
	Loading Eigen-Value = 1265
	Loading Eigen-Value = 1266
	Loading Eigen-Value = 1267
	Loading Eigen-Value = 1268
	Loading Eigen-Value = 1269
	Loading Eigen-Value = 1270
	Loading Eigen-Value = 1271
	Loading Eigen-Value = 1272
	Loading Eigen-Value = 1273
	Loading Eigen-Value = 1274
	Loading Eigen-Value = 1275
	Loading Eigen-Value = 1276
	Loading Eigen-Value = 1277
	Loading Eigen-Value = 1278
	Loading Eigen-Value = 1279
	Loading Eigen-Value = 1280
	Loading Eigen-Value = 1281
	Loading Eigen-Value = 1282
	Loading Eigen-Value = 1283
	Loading Eigen-Value = 1284
	Loading Eigen-Value = 1285
	Loading Eigen-Value = 1286
	Loading Eigen-Value = 1287
	Loading Eigen-Value = 1288
	Loading Eigen-Value = 1289
	Loading Eigen-Value = 1290
	Loading Eigen-Value = 1291
	Loading Eigen-Value = 1292
	Loading Eigen-Value = 1293
	Loading Eigen-Value = 1294
	Loading Eigen-Value = 1295
	Loading Eigen-Value = 1296
	Loading Eigen-Value = 1297
	Loading Eigen-Value = 1298
	Loading Eigen-Value = 1299
	Loading Eigen-Value = 1300
	Loading Eigen-Value = 1301
	Loading Eigen-Value = 1302
	Loading Eigen-Value = 1303
	Loading Eigen-Value = 1304
	Loading Eigen-Value = 1305
	Loading Eigen-Value = 1306
	Loading Eigen-Value = 1307
	Loading Eigen-Value = 1308
	Loading Eigen-Value = 1309
	Loading Eigen-Value = 1310
	Loading Eigen-Value = 1311
	Loading Eigen-Value = 1312
	Loading Eigen-Value = 1313
	Loading Eigen-Value = 1314
	Loading Eigen-Value = 1315
	Loading Eigen-Value = 1316
	Loading Eigen-Value = 1317
	Loading Eigen-Value = 1318
	Loading Eigen-Value = 1319
	Loading Eigen-Value = 1320
	Loading Eigen-Value = 1321
	Loading Eigen-Value = 1322
	Loading Eigen-Value = 1323
	Loading Eigen-Value = 1324
	Loading Eigen-Value = 1325
	Loading Eigen-Value = 1326
	Loading Eigen-Value = 1327
	Loading Eigen-Value = 1328
	Loading Eigen-Value = 1329
	Loading Eigen-Value = 1330
	Loading Eigen-Value = 1331
	Loading Eigen-Value = 1332
	Loading Eigen-Value = 1333
	Loading Eigen-Value = 1334
	Loading Eigen-Value = 1335
	Loading Eigen-Value = 1336
	Loading Eigen-Value = 1337
	Loading Eigen-Value = 1338
	Loading Eigen-Value = 1339
	Loading Eigen-Value = 1340
	Loading Eigen-Value = 1341
	Loading Eigen-Value = 1342
	Loading Eigen-Value = 1343
	Loading Eigen-Value = 1344
	Loading Eigen-Value = 1345
	Loading Eigen-Value = 1346
	Loading Eigen-Value = 1347
	Loading Eigen-Value = 1348
	Loading Eigen-Value = 1349
	Loading Eigen-Value = 1350
	Loading Eigen-Value = 1351
	Loading Eigen-Value = 1352
	Loading Eigen-Value = 1353
	Loading Eigen-Value = 1354
	Loading Eigen-Value = 1355
	Loading Eigen-Value = 1356
	Loading Eigen-Value = 1357
	Loading Eigen-Value = 1358
	Loading Eigen-Value = 1359
	Loading Eigen-Value = 1360
	Loading Eigen-Value = 1361
	Loading Eigen-Value = 1362
	Loading Eigen-Value = 1363
	Loading Eigen-Value = 1364
	Loading Eigen-Value = 1365
	Loading Eigen-Value = 1366
	Loading Eigen-Value = 1367
	Loading Eigen-Value = 1368
	Loading Eigen-Value = 1369
	Loading Eigen-Value = 1370
	Loading Eigen-Value = 1371
	Loading Eigen-Value = 1372
	Loading Eigen-Value = 1373
	Loading Eigen-Value = 1374
	Loading Eigen-Value = 1375
	Loading Eigen-Value = 1376
	Loading Eigen-Value = 1377
	Loading Eigen-Value = 1378
	Loading Eigen-Value = 1379
	Loading Eigen-Value = 1380
	Loading Eigen-Value = 1381
	Loading Eigen-Value = 1382
	Loading Eigen-Value = 1383
	Loading Eigen-Value = 1384
	Loading Eigen-Value = 1385
	Loading Eigen-Value = 1386
	Loading Eigen-Value = 1387
	Loading Eigen-Value = 1388
	Loading Eigen-Value = 1389
	Loading Eigen-Value = 1390
	Loading Eigen-Value = 1391
	Loading Eigen-Value = 1392
	Loading Eigen-Value = 1393
	Loading Eigen-Value = 1394
	Loading Eigen-Value = 1395
	Loading Eigen-Value = 1396
	Loading Eigen-Value = 1397
	Loading Eigen-Value = 1398
	Loading Eigen-Value = 1399
	Loading Eigen-Value = 1400
	Loading Eigen-Value = 1401
	Loading Eigen-Value = 1402
	Loading Eigen-Value = 1403
	Loading Eigen-Value = 1404
	Loading Eigen-Value = 1405
	Loading Eigen-Value = 1406
	Loading Eigen-Value = 1407
	Loading Eigen-Value = 1408
	Loading Eigen-Value = 1409
	Loading Eigen-Value = 1410
	Loading Eigen-Value = 1411
	Loading Eigen-Value = 1412
	Loading Eigen-Value = 1413
	Loading Eigen-Value = 1414
	Loading Eigen-Value = 1415
	Loading Eigen-Value = 1416
	Loading Eigen-Value = 1417
	Loading Eigen-Value = 1418
	Loading Eigen-Value = 1419
	Loading Eigen-Value = 1420
	Loading Eigen-Value = 1421
	Loading Eigen-Value = 1422
	Loading Eigen-Value = 1423
	Loading Eigen-Value = 1424
	Loading Eigen-Value = 1425
	Loading Eigen-Value = 1426
	Loading Eigen-Value = 1427
	Loading Eigen-Value = 1428
	Loading Eigen-Value = 1429
	Loading Eigen-Value = 1430
	Loading Eigen-Value = 1431
	Loading Eigen-Value = 1432
	Loading Eigen-Value = 1433
	Loading Eigen-Value = 1434
	Loading Eigen-Value = 1435
	Loading Eigen-Value = 1436
	Loading Eigen-Value = 1437
	Loading Eigen-Value = 1438
	Loading Eigen-Value = 1439
	Loading Eigen-Value = 1440
	Loading Eigen-Value = 1441
	Loading Eigen-Value = 1442
	Loading Eigen-Value = 1443
	Loading Eigen-Value = 1444
	Loading Eigen-Value = 1445
	Loading Eigen-Value = 1446
	Loading Eigen-Value = 1447
	Loading Eigen-Value = 1448
	Loading Eigen-Value = 1449
	Loading Eigen-Value = 1450
	Loading Eigen-Value = 1451
	Loading Eigen-Value = 1452
	Loading Eigen-Value = 1453
	Loading Eigen-Value = 1454
	Loading Eigen-Value = 1455
	Loading Eigen-Value = 1456
	Loading Eigen-Value = 1457
	Loading Eigen-Value = 1458
	Loading Eigen-Value = 1459
	Loading Eigen-Value = 1460
	Loading Eigen-Value = 1461
	Loading Eigen-Value = 1462
	Loading Eigen-Value = 1463
	Loading Eigen-Value = 1464
	Loading Eigen-Value = 1465
	Loading Eigen-Value = 1466
	Loading Eigen-Value = 1467
	Loading Eigen-Value = 1468
	Loading Eigen-Value = 1469
	Loading Eigen-Value = 1470
	Loading Eigen-Value = 1471
	Loading Eigen-Value = 1472
	Loading Eigen-Value = 1473
	Loading Eigen-Value = 1474
	Loading Eigen-Value = 1475
	Loading Eigen-Value = 1476
	Loading Eigen-Value = 1477
	Loading Eigen-Value = 1478
	Loading Eigen-Value = 1479
	Loading Eigen-Value = 1480
	Loading Eigen-Value = 1481
	Loading Eigen-Value = 1482
	Loading Eigen-Value = 1483
	Loading Eigen-Value = 1484
	Loading Eigen-Value = 1485
	Loading Eigen-Value = 1486
	Loading Eigen-Value = 1487
	Loading Eigen-Value = 1488
	Loading Eigen-Value = 1489
	Loading Eigen-Value = 1490
	Loading Eigen-Value = 1491
	Loading Eigen-Value = 1492
	Loading Eigen-Value = 1493
	Loading Eigen-Value = 1494
	Loading Eigen-Value = 1495
	Loading Eigen-Value = 1496
	Loading Eigen-Value = 1497
	Loading Eigen-Value = 1498
	Loading Eigen-Value = 1499
	Loading Eigen-Value = 1500
	Loading Eigen-Value = 1501
	Loading Eigen-Value = 1502
	Loading Eigen-Value = 1503
	Loading Eigen-Value = 1504
	Loading Eigen-Value = 1505
	Loading Eigen-Value = 1506
	Loading Eigen-Value = 1507
	Loading Eigen-Value = 1508
	Loading Eigen-Value = 1509
	Loading Eigen-Value = 1510
	Loading Eigen-Value = 1511
	Loading Eigen-Value = 1512
	Loading Eigen-Value = 1513
	Loading Eigen-Value = 1514
	Loading Eigen-Value = 1515
	Loading Eigen-Value = 1516
	Loading Eigen-Value = 1517
	Loading Eigen-Value = 1518
	Loading Eigen-Value = 1519
	Loading Eigen-Value = 1520
	Loading Eigen-Value = 1521
	Loading Eigen-Value = 1522
	Loading Eigen-Value = 1523
	Loading Eigen-Value = 1524
	Loading Eigen-Value = 1525
	Loading Eigen-Value = 1526
	Loading Eigen-Value = 1527
	Loading Eigen-Value = 1528
	Loading Eigen-Value = 1529
	Loading Eigen-Value = 1530
	Loading Eigen-Value = 1531
	Loading Eigen-Value = 1532
	Loading Eigen-Value = 1533
	Loading Eigen-Value = 1534
	Loading Eigen-Value = 1535
	Loading Eigen-Value = 1536
	Loading Eigen-Value = 1537
	Loading Eigen-Value = 1538
	Loading Eigen-Value = 1539
	Loading Eigen-Value = 1540
	Loading Eigen-Value = 1541
	Loading Eigen-Value = 1542
	Loading Eigen-Value = 1543
	Loading Eigen-Value = 1544
	Loading Eigen-Value = 1545
	Loading Eigen-Value = 1546
	Loading Eigen-Value = 1547
	Loading Eigen-Value = 1548
	Loading Eigen-Value = 1549
	Loading Eigen-Value = 1550
	Loading Eigen-Value = 1551
	Loading Eigen-Value = 1552
	Loading Eigen-Value = 1553
	Loading Eigen-Value = 1554
	Loading Eigen-Value = 1555
	Loading Eigen-Value = 1556
	Loading Eigen-Value = 1557
	Loading Eigen-Value = 1558
	Loading Eigen-Value = 1559
	Loading Eigen-Value = 1560
	Loading Eigen-Value = 1561
	Loading Eigen-Value = 1562
	Loading Eigen-Value = 1563
	Loading Eigen-Value = 1564
	Loading Eigen-Value = 1565
	Loading Eigen-Value = 1566
	Loading Eigen-Value = 1567
	Loading Eigen-Value = 1568
	Loading Eigen-Value = 1569
	Loading Eigen-Value = 1570
	Loading Eigen-Value = 1571
	Loading Eigen-Value = 1572
	Loading Eigen-Value = 1573
	Loading Eigen-Value = 1574
	Loading Eigen-Value = 1575
	Loading Eigen-Value = 1576
	Loading Eigen-Value = 1577
	Loading Eigen-Value = 1578
	Loading Eigen-Value = 1579
	Loading Eigen-Value = 1580
	Loading Eigen-Value = 1581
	Loading Eigen-Value = 1582
	Loading Eigen-Value = 1583
	Loading Eigen-Value = 1584
	Loading Eigen-Value = 1585
	Loading Eigen-Value = 1586
	Loading Eigen-Value = 1587
	Loading Eigen-Value = 1588
	Loading Eigen-Value = 1589
	Loading Eigen-Value = 1590
	Loading Eigen-Value = 1591
	Loading Eigen-Value = 1592
	Loading Eigen-Value = 1593
	Loading Eigen-Value = 1594
	Loading Eigen-Value = 1595
	Loading Eigen-Value = 1596
	Loading Eigen-Value = 1597
	Loading Eigen-Value = 1598
	Loading Eigen-Value = 1599
	Loading Eigen-Value = 1600
	Loading Eigen-Value = 1601
	Loading Eigen-Value = 1602
	Loading Eigen-Value = 1603
	Loading Eigen-Value = 1604
	Loading Eigen-Value = 1605
	Loading Eigen-Value = 1606
	Loading Eigen-Value = 1607
	Loading Eigen-Value = 1608
	Loading Eigen-Value = 1609
	Loading Eigen-Value = 1610
	Loading Eigen-Value = 1611
	Loading Eigen-Value = 1612
	Loading Eigen-Value = 1613
	Loading Eigen-Value = 1614
	Loading Eigen-Value = 1615
	Loading Eigen-Value = 1616
	Loading Eigen-Value = 1617
	Loading Eigen-Value = 1618
	Loading Eigen-Value = 1619
	Loading Eigen-Value = 1620
	Loading Eigen-Value = 1621
	Loading Eigen-Value = 1622
	Loading Eigen-Value = 1623
	Loading Eigen-Value = 1624
	Loading Eigen-Value = 1625
	Loading Eigen-Value = 1626
	Loading Eigen-Value = 1627
	Loading Eigen-Value = 1628
	Loading Eigen-Value = 1629
	Loading Eigen-Value = 1630
	Loading Eigen-Value = 1631
	Loading Eigen-Value = 1632
	Loading Eigen-Value = 1633
	Loading Eigen-Value = 1634
	Loading Eigen-Value = 1635
	Loading Eigen-Value = 1636
	Loading Eigen-Value = 1637
	Loading Eigen-Value = 1638
	Loading Eigen-Value = 1639
	Loading Eigen-Value = 1640
	Loading Eigen-Value = 1641
	Loading Eigen-Value = 1642
	Loading Eigen-Value = 1643
	Loading Eigen-Value = 1644
	Loading Eigen-Value = 1645
	Loading Eigen-Value = 1646
	Loading Eigen-Value = 1647
	Loading Eigen-Value = 1648
	Loading Eigen-Value = 1649
	Loading Eigen-Value = 1650
	Loading Eigen-Value = 1651
	Loading Eigen-Value = 1652
	Loading Eigen-Value = 1653
	Loading Eigen-Value = 1654
	Loading Eigen-Value = 1655
	Loading Eigen-Value = 1656
	Loading Eigen-Value = 1657
	Loading Eigen-Value = 1658
	Loading Eigen-Value = 1659
	Loading Eigen-Value = 1660
	Loading Eigen-Value = 1661
	Loading Eigen-Value = 1662
	Loading Eigen-Value = 1663
	Loading Eigen-Value = 1664
	Loading Eigen-Value = 1665
	Loading Eigen-Value = 1666
	Loading Eigen-Value = 1667
	Loading Eigen-Value = 1668
	Loading Eigen-Value = 1669
	Loading Eigen-Value = 1670
	Loading Eigen-Value = 1671
	Loading Eigen-Value = 1672
	Loading Eigen-Value = 1673
	Loading Eigen-Value = 1674
	Loading Eigen-Value = 1675
	Loading Eigen-Value = 1676
	Loading Eigen-Value = 1677
	Loading Eigen-Value = 1678
	Loading Eigen-Value = 1679
	Loading Eigen-Value = 1680
	Loading Eigen-Value = 1681
	Loading Eigen-Value = 1682
	Loading Eigen-Value = 1683
	Loading Eigen-Value = 1684
	Loading Eigen-Value = 1685
	Loading Eigen-Value = 1686
	Loading Eigen-Value = 1687
	Loading Eigen-Value = 1688
	Loading Eigen-Value = 1689
	Loading Eigen-Value = 1690
	Loading Eigen-Value = 1691
	Loading Eigen-Value = 1692
	Loading Eigen-Value = 1693
	Loading Eigen-Value = 1694
	Loading Eigen-Value = 1695
	Loading Eigen-Value = 1696
	Loading Eigen-Value = 1697
	Loading Eigen-Value = 1698
	Loading Eigen-Value = 1699
	Loading Eigen-Value = 1700
	Loading Eigen-Value = 1701
	Loading Eigen-Value = 1702
	Loading Eigen-Value = 1703
	Loading Eigen-Value = 1704
	Loading Eigen-Value = 1705
	Loading Eigen-Value = 1706
	Loading Eigen-Value = 1707
	Loading Eigen-Value = 1708
	Loading Eigen-Value = 1709
	Loading Eigen-Value = 1710
	Loading Eigen-Value = 1711
	Loading Eigen-Value = 1712
	Loading Eigen-Value = 1713
	Loading Eigen-Value = 1714
	Loading Eigen-Value = 1715
	Loading Eigen-Value = 1716
	Loading Eigen-Value = 1717
	Loading Eigen-Value = 1718
	Loading Eigen-Value = 1719
	Loading Eigen-Value = 1720
	Loading Eigen-Value = 1721
	Loading Eigen-Value = 1722
	Loading Eigen-Value = 1723
	Loading Eigen-Value = 1724
	Loading Eigen-Value = 1725
	Loading Eigen-Value = 1726
	Loading Eigen-Value = 1727
	Loading Eigen-Value = 1728
	Loading Eigen-Value = 1729
	Loading Eigen-Value = 1730
	Loading Eigen-Value = 1731
	Loading Eigen-Value = 1732
	Loading Eigen-Value = 1733
	Loading Eigen-Value = 1734
	Loading Eigen-Value = 1735
	Loading Eigen-Value = 1736
	Loading Eigen-Value = 1737
	Loading Eigen-Value = 1738
	Loading Eigen-Value = 1739
	Loading Eigen-Value = 1740
	Loading Eigen-Value = 1741
	Loading Eigen-Value = 1742
	Loading Eigen-Value = 1743
	Loading Eigen-Value = 1744
	Loading Eigen-Value = 1745
	Loading Eigen-Value = 1746
	Loading Eigen-Value = 1747
	Loading Eigen-Value = 1748
	Loading Eigen-Value = 1749
	Loading Eigen-Value = 1750
	Loading Eigen-Value = 1751
	Loading Eigen-Value = 1752
	Loading Eigen-Value = 1753
	Loading Eigen-Value = 1754
	Loading Eigen-Value = 1755
	Loading Eigen-Value = 1756
	Loading Eigen-Value = 1757
	Loading Eigen-Value = 1758
	Loading Eigen-Value = 1759
	Loading Eigen-Value = 1760
	Loading Eigen-Value = 1761
	Loading Eigen-Value = 1762
	Loading Eigen-Value = 1763
	Loading Eigen-Value = 1764
	Loading Eigen-Value = 1765
	Loading Eigen-Value = 1766
	Loading Eigen-Value = 1767
	Loading Eigen-Value = 1768
	Loading Eigen-Value = 1769
	Loading Eigen-Value = 1770
	Loading Eigen-Value = 1771
	Loading Eigen-Value = 1772
	Loading Eigen-Value = 1773
	Loading Eigen-Value = 1774
	Loading Eigen-Value = 1775
	Loading Eigen-Value = 1776
	Loading Eigen-Value = 1777
	Loading Eigen-Value = 1778
	Loading Eigen-Value = 1779
Natural freq (Mode 1) = 5.91752 (Hz)
Natural freq (Mode 2) = 29.92398 (Hz)
Natural freq (Mode 3) = 40.01939 (Hz)
Natural freq (Mode 4) = 78.26336 (Hz)
Natural freq (Mode 5) = 102.48770 (Hz)
Natural freq (Mode 6) = 148.28700 (Hz)
Natural freq (Mode 7) = 182.97520 (Hz)
Natural freq (Mode 8) = 238.39370 (Hz)
Natural freq (Mode 9) = 285.36330 (Hz)
Natural freq (Mode 10) = 321.90370 (Hz)
Natural freq (Mode 11) = 338.36210 (Hz)
Natural freq (Mode 12) = 347.87480 (Hz)
Natural freq (Mode 13) = 412.76490 (Hz)
Natural freq (Mode 14) = 446.89790 (Hz)
Natural freq (Mode 15) = 477.26050 (Hz)
Natural freq (Mode 16) = 556.73130 (Hz)
Natural freq (Mode 17) = 582.55570 (Hz)
Natural freq (Mode 18) = 627.20430 (Hz)
Natural freq (Mode 19) = 696.67300 (Hz)
Natural freq (Mode 20) = 750.94670 (Hz)
Natural freq (Mode 21) = 757.10910 (Hz)
Natural freq (Mode 22) = 797.86110 (Hz)
Natural freq (Mode 23) = 847.03330 (Hz)
Natural freq (Mode 24) = 944.72760 (Hz)
Natural freq (Mode 25) = 956.33970 (Hz)
Natural freq (Mode 26) = 978.56320 (Hz)
Natural freq (Mode 27) = 1011.29500 (Hz)
Natural freq (Mode 28) = 1121.40300 (Hz)
Natural freq (Mode 29) = 1155.17800 (Hz)
Natural freq (Mode 30) = 1174.22000 (Hz)
Natural freq (Mode 31) = 1218.32400 (Hz)
Natural freq (Mode 32) = 1289.59300 (Hz)
Natural freq (Mode 33) = 1300.85200 (Hz)
Natural freq (Mode 34) = 1332.20600 (Hz)
Natural freq (Mode 35) = 1359.39700 (Hz)
Natural freq (Mode 36) = 1412.35900 (Hz)
Natural freq (Mode 37) = 1457.87000 (Hz)
Natural freq (Mode 38) = 1504.80200 (Hz)
Natural freq (Mode 39) = 1555.90000 (Hz)
Natural freq (Mode 40) = 1607.07800 (Hz)
Natural freq (Mode 41) = 1655.47400 (Hz)
Natural freq (Mode 42) = 1717.08000 (Hz)
Natural freq (Mode 43) = 1741.97300 (Hz)
Natural freq (Mode 44) = 1801.38700 (Hz)
Natural freq (Mode 45) = 1873.31100 (Hz)
Natural freq (Mode 46) = 1913.09800 (Hz)
Natural freq (Mode 47) = 1980.26900 (Hz)
Natural freq (Mode 48) = 1991.99800 (Hz)
Natural freq (Mode 49) = 2069.91300 (Hz)
Natural freq (Mode 50) = 2113.76400 (Hz)
Natural freq (Mode 51) = 2145.78500 (Hz)
Natural freq (Mode 52) = 2175.50900 (Hz)
Natural freq (Mode 53) = 2224.13400 (Hz)
Natural freq (Mode 54) = 2298.75800 (Hz)
Natural freq (Mode 55) = 2349.76500 (Hz)
Natural freq (Mode 56) = 2413.31600 (Hz)
Natural freq (Mode 57) = 2439.34000 (Hz)
Natural freq (Mode 58) = 2497.21500 (Hz)
Natural freq (Mode 59) = 2499.99000 (Hz)
Natural freq (Mode 60) = 2549.47200 (Hz)
Natural freq (Mode 61) = 2608.88800 (Hz)
Natural freq (Mode 62) = 2632.75600 (Hz)
Natural freq (Mode 63) = 2710.43000 (Hz)
Natural freq (Mode 64) = 2747.45500 (Hz)
Natural freq (Mode 65) = 2787.56600 (Hz)
Natural freq (Mode 66) = 2804.88200 (Hz)
Natural freq (Mode 67) = 2828.01000 (Hz)
Natural freq (Mode 68) = 2891.33900 (Hz)
Natural freq (Mode 69) = 2943.88700 (Hz)
Natural freq (Mode 70) = 2996.34500 (Hz)
Natural freq (Mode 71) = 3038.47900 (Hz)
Natural freq (Mode 72) = 3110.97300 (Hz)
Natural freq (Mode 73) = 3155.74800 (Hz)
Natural freq (Mode 74) = 3171.54500 (Hz)
Natural freq (Mode 75) = 3208.80000 (Hz)
Natural freq (Mode 76) = 3270.76600 (Hz)
Natural freq (Mode 77) = 3337.48000 (Hz)
Natural freq (Mode 78) = 3397.62800 (Hz)
Natural freq (Mode 79) = 3430.15700 (Hz)
Natural freq (Mode 80) = 3486.27900 (Hz)
Natural freq (Mode 81) = 3519.90500 (Hz)
Natural freq (Mode 82) = 3582.41700 (Hz)
Natural freq (Mode 83) = 3644.34000 (Hz)
Natural freq (Mode 84) = 3690.50500 (Hz)
Natural freq (Mode 85) = 3709.94700 (Hz)
Natural freq (Mode 86) = 3751.86800 (Hz)
Natural freq (Mode 87) = 3847.60300 (Hz)
Natural freq (Mode 88) = 3881.69700 (Hz)
Natural freq (Mode 89) = 3929.56900 (Hz)
Natural freq (Mode 90) = 4030.33000 (Hz)
Natural freq (Mode 91) = 4075.24600 (Hz)
Natural freq (Mode 92) = 4112.23100 (Hz)
Natural freq (Mode 93) = 4125.08800 (Hz)
Natural freq (Mode 94) = 4175.94300 (Hz)
Natural freq (Mode 95) = 4249.31900 (Hz)
Natural freq (Mode 96) = 4326.93400 (Hz)
Natural freq (Mode 97) = 4350.07800 (Hz)
Natural freq (Mode 98) = 4422.66200 (Hz)
Natural freq (Mode 99) = 4433.83300 (Hz)
Natural freq (Mode 100) = 4490.80200 (Hz)
Natural freq (Mode 101) = 4533.85600 (Hz)
Natural freq (Mode 102) = 4575.81800 (Hz)
Natural freq (Mode 103) = 4650.17200 (Hz)
Natural freq (Mode 104) = 4653.01800 (Hz)
Natural freq (Mode 105) = 4762.06400 (Hz)
Natural freq (Mode 106) = 4783.26800 (Hz)
Natural freq (Mode 107) = 4833.77500 (Hz)
Natural freq (Mode 108) = 4859.19300 (Hz)
Natural freq (Mode 109) = 4906.46000 (Hz)
Natural freq (Mode 110) = 4983.49100 (Hz)
Natural freq (Mode 111) = 5036.52400 (Hz)
Natural freq (Mode 112) = 5088.89300 (Hz)
Natural freq (Mode 113) = 5131.49800 (Hz)
Natural freq (Mode 114) = 5189.45600 (Hz)
Natural freq (Mode 115) = 5226.69000 (Hz)
Natural freq (Mode 116) = 5312.39900 (Hz)
Natural freq (Mode 117) = 5337.54300 (Hz)
Natural freq (Mode 118) = 5412.15200 (Hz)
Natural freq (Mode 119) = 5468.34800 (Hz)
Natural freq (Mode 120) = 5515.48600 (Hz)
Natural freq (Mode 121) = 5524.08000 (Hz)
Natural freq (Mode 122) = 5619.29500 (Hz)
Natural freq (Mode 123) = 5653.70400 (Hz)
Natural freq (Mode 124) = 5733.63600 (Hz)
Natural freq (Mode 125) = 5773.94900 (Hz)
Natural freq (Mode 126) = 5844.35200 (Hz)
Natural freq (Mode 127) = 5867.65000 (Hz)
Natural freq (Mode 128) = 5906.70100 (Hz)
Natural freq (Mode 129) = 5971.92900 (Hz)
Natural freq (Mode 130) = 6009.02100 (Hz)
Natural freq (Mode 131) = 6072.23100 (Hz)
Natural freq (Mode 132) = 6114.32400 (Hz)
Natural freq (Mode 133) = 6217.45300 (Hz)
Natural freq (Mode 134) = 6258.33500 (Hz)
Natural freq (Mode 135) = 6280.35900 (Hz)
Natural freq (Mode 136) = 6328.06800 (Hz)
Natural freq (Mode 137) = 6380.03600 (Hz)
Natural freq (Mode 138) = 6420.51900 (Hz)
Natural freq (Mode 139) = 6443.62300 (Hz)
Natural freq (Mode 140) = 6482.95600 (Hz)
Natural freq (Mode 141) = 6556.30700 (Hz)
Natural freq (Mode 142) = 6581.93700 (Hz)
Natural freq (Mode 143) = 6681.89000 (Hz)
Natural freq (Mode 144) = 6710.49400 (Hz)
Natural freq (Mode 145) = 6712.56300 (Hz)
Natural freq (Mode 146) = 6757.85200 (Hz)
Natural freq (Mode 147) = 6773.85300 (Hz)
Natural freq (Mode 148) = 6855.24800 (Hz)
Natural freq (Mode 149) = 6906.85000 (Hz)
Natural freq (Mode 150) = 6964.86500 (Hz)
Natural freq (Mode 151) = 7005.47200 (Hz)
Natural freq (Mode 152) = 7093.12700 (Hz)
Natural freq (Mode 153) = 7172.58500 (Hz)
Natural freq (Mode 154) = 7235.36700 (Hz)
Natural freq (Mode 155) = 7284.38800 (Hz)
Natural freq (Mode 156) = 7339.50900 (Hz)
Natural freq (Mode 157) = 7387.76000 (Hz)
Natural freq (Mode 158) = 7432.07800 (Hz)
Natural freq (Mode 159) = 7484.19100 (Hz)
Natural freq (Mode 160) = 7505.65500 (Hz)
Natural freq (Mode 161) = 7575.40800 (Hz)
Natural freq (Mode 162) = 7619.31300 (Hz)
Natural freq (Mode 163) = 7645.70400 (Hz)
Natural freq (Mode 164) = 7763.99600 (Hz)
Natural freq (Mode 165) = 7804.56500 (Hz)
Natural freq (Mode 166) = 7847.62900 (Hz)
Natural freq (Mode 167) = 7884.94000 (Hz)
Natural freq (Mode 168) = 7971.14100 (Hz)
Natural freq (Mode 169) = 7981.26000 (Hz)
Natural freq (Mode 170) = 8018.25500 (Hz)
Natural freq (Mode 171) = 8065.35200 (Hz)
Natural freq (Mode 172) = 8190.58300 (Hz)
Natural freq (Mode 173) = 8219.15300 (Hz)
Natural freq (Mode 174) = 8242.49900 (Hz)
Natural freq (Mode 175) = 8305.01600 (Hz)
Natural freq (Mode 176) = 8338.74300 (Hz)
Natural freq (Mode 177) = 8449.34200 (Hz)
Natural freq (Mode 178) = 8515.47200 (Hz)
Natural freq (Mode 179) = 8589.43700 (Hz)
Natural freq (Mode 180) = 8616.56100 (Hz)
Natural freq (Mode 181) = 8640.13700 (Hz)
Natural freq (Mode 182) = 8712.28800 (Hz)
Natural freq (Mode 183) = 8716.81500 (Hz)
Natural freq (Mode 184) = 8787.58300 (Hz)
Natural freq (Mode 185) = 8846.56900 (Hz)
Natural freq (Mode 186) = 8875.50500 (Hz)
Natural freq (Mode 187) = 8964.94700 (Hz)
Natural freq (Mode 188) = 8992.86500 (Hz)
Natural freq (Mode 189) = 9077.22400 (Hz)
Natural freq (Mode 190) = 9096.26100 (Hz)
Natural freq (Mode 191) = 9145.99500 (Hz)
Natural freq (Mode 192) = 9199.71100 (Hz)
Natural freq (Mode 193) = 9239.19700 (Hz)
Natural freq (Mode 194) = 9335.28900 (Hz)
Natural freq (Mode 195) = 9367.16700 (Hz)
Natural freq (Mode 196) = 9496.20700 (Hz)
Natural freq (Mode 197) = 9506.20900 (Hz)
Natural freq (Mode 198) = 9530.04800 (Hz)
Natural freq (Mode 199) = 9569.59000 (Hz)
Natural freq (Mode 200) = 9612.48400 (Hz)
Natural freq (Mode 201) = 9670.18300 (Hz)
Natural freq (Mode 202) = 9702.23300 (Hz)
Natural freq (Mode 203) = 9772.30000 (Hz)
Natural freq (Mode 204) = 9825.17600 (Hz)
Natural freq (Mode 205) = 9883.47700 (Hz)
Natural freq (Mode 206) = 9901.35100 (Hz)
Natural freq (Mode 207) = 9952.14500 (Hz)
Natural freq (Mode 208) = 10096.61000 (Hz)
Natural freq (Mode 209) = 10117.51000 (Hz)
Natural freq (Mode 210) = 10152.60000 (Hz)
Natural freq (Mode 211) = 10241.89000 (Hz)
Natural freq (Mode 212) = 10283.19000 (Hz)
Natural freq (Mode 213) = 10290.01000 (Hz)
Natural freq (Mode 214) = 10313.76000 (Hz)
Natural freq (Mode 215) = 10380.63000 (Hz)
Natural freq (Mode 216) = 10423.29000 (Hz)
Natural freq (Mode 217) = 10489.16000 (Hz)
Natural freq (Mode 218) = 10534.94000 (Hz)
Natural freq (Mode 219) = 10617.34000 (Hz)
Natural freq (Mode 220) = 10692.66000 (Hz)
Natural freq (Mode 221) = 10724.57000 (Hz)
Natural freq (Mode 222) = 10783.30000 (Hz)
Natural freq (Mode 223) = 10796.14000 (Hz)
Natural freq (Mode 224) = 10837.42000 (Hz)
Natural freq (Mode 225) = 10917.22000 (Hz)
Natural freq (Mode 226) = 10990.39000 (Hz)
Natural freq (Mode 227) = 11032.01000 (Hz)
Natural freq (Mode 228) = 11066.56000 (Hz)
Natural freq (Mode 229) = 11107.64000 (Hz)
Natural freq (Mode 230) = 11181.18000 (Hz)
Natural freq (Mode 231) = 11203.75000 (Hz)
Natural freq (Mode 232) = 11301.06000 (Hz)
Natural freq (Mode 233) = 11368.84000 (Hz)
Natural freq (Mode 234) = 11405.65000 (Hz)
Natural freq (Mode 235) = 11479.89000 (Hz)
Natural freq (Mode 236) = 11556.38000 (Hz)
Natural freq (Mode 237) = 11582.24000 (Hz)
Natural freq (Mode 238) = 11608.71000 (Hz)
Natural freq (Mode 239) = 11663.11000 (Hz)
Natural freq (Mode 240) = 11767.24000 (Hz)
Natural freq (Mode 241) = 11809.88000 (Hz)
Natural freq (Mode 242) = 11869.78000 (Hz)
Natural freq (Mode 243) = 11968.82000 (Hz)
Natural freq (Mode 244) = 11983.42000 (Hz)
Natural freq (Mode 245) = 12042.58000 (Hz)
Natural freq (Mode 246) = 12116.63000 (Hz)
Natural freq (Mode 247) = 12143.37000 (Hz)
Natural freq (Mode 248) = 12143.61000 (Hz)
Natural freq (Mode 249) = 12189.26000 (Hz)
Natural freq (Mode 250) = 12256.66000 (Hz)
Natural freq (Mode 251) = 12310.75000 (Hz)
Natural freq (Mode 252) = 12364.03000 (Hz)
Natural freq (Mode 253) = 12370.65000 (Hz)
Natural freq (Mode 254) = 12548.26000 (Hz)
Natural freq (Mode 255) = 12565.68000 (Hz)
Natural freq (Mode 256) = 12594.88000 (Hz)
Natural freq (Mode 257) = 12712.07000 (Hz)
Natural freq (Mode 258) = 12770.17000 (Hz)
Natural freq (Mode 259) = 12775.62000 (Hz)
Natural freq (Mode 260) = 12825.19000 (Hz)
Natural freq (Mode 261) = 12905.15000 (Hz)
Natural freq (Mode 262) = 12955.70000 (Hz)
Natural freq (Mode 263) = 13036.73000 (Hz)
Natural freq (Mode 264) = 13054.72000 (Hz)
Natural freq (Mode 265) = 13161.42000 (Hz)
Natural freq (Mode 266) = 13192.61000 (Hz)
Natural freq (Mode 267) = 13239.57000 (Hz)
Natural freq (Mode 268) = 13284.37000 (Hz)
Natural freq (Mode 269) = 13384.14000 (Hz)
Natural freq (Mode 270) = 13408.39000 (Hz)
Natural freq (Mode 271) = 13456.16000 (Hz)
Natural freq (Mode 272) = 13472.22000 (Hz)
Natural freq (Mode 273) = 13530.73000 (Hz)
Natural freq (Mode 274) = 13593.85000 (Hz)
Natural freq (Mode 275) = 13760.49000 (Hz)
Natural freq (Mode 276) = 13785.68000 (Hz)
Natural freq (Mode 277) = 13876.39000 (Hz)
Natural freq (Mode 278) = 13897.87000 (Hz)
Natural freq (Mode 279) = 13949.89000 (Hz)
Natural freq (Mode 280) = 13982.83000 (Hz)
Natural freq (Mode 281) = 14036.06000 (Hz)
Natural freq (Mode 282) = 14061.26000 (Hz)
Natural freq (Mode 283) = 14126.31000 (Hz)
Natural freq (Mode 284) = 14289.37000 (Hz)
Natural freq (Mode 285) = 14326.99000 (Hz)
Natural freq (Mode 286) = 14398.55000 (Hz)
Natural freq (Mode 287) = 14484.76000 (Hz)
Natural freq (Mode 288) = 14489.28000 (Hz)
Natural freq (Mode 289) = 14522.37000 (Hz)
Natural freq (Mode 290) = 14565.89000 (Hz)
Natural freq (Mode 291) = 14606.46000 (Hz)
Natural freq (Mode 292) = 14649.44000 (Hz)
Natural freq (Mode 293) = 14786.59000 (Hz)
Natural freq (Mode 294) = 14893.02000 (Hz)
Natural freq (Mode 295) = 14975.89000 (Hz)
Natural freq (Mode 296) = 14990.37000 (Hz)
Natural freq (Mode 297) = 15048.04000 (Hz)
Natural freq (Mode 298) = 15137.92000 (Hz)
Natural freq (Mode 299) = 15180.15000 (Hz)
Natural freq (Mode 300) = 15208.71000 (Hz)
Natural freq (Mode 301) = 15324.33000 (Hz)
Natural freq (Mode 302) = 15358.41000 (Hz)
Natural freq (Mode 303) = 15371.80000 (Hz)
Natural freq (Mode 304) = 15469.29000 (Hz)
Natural freq (Mode 305) = 15502.22000 (Hz)
Natural freq (Mode 306) = 15582.06000 (Hz)
Natural freq (Mode 307) = 15697.16000 (Hz)
Natural freq (Mode 308) = 15716.81000 (Hz)
Natural freq (Mode 309) = 15838.63000 (Hz)
Natural freq (Mode 310) = 15881.20000 (Hz)
Natural freq (Mode 311) = 15983.89000 (Hz)
Natural freq (Mode 312) = 15994.51000 (Hz)
Natural freq (Mode 313) = 16002.53000 (Hz)
Natural freq (Mode 314) = 16137.48000 (Hz)
Natural freq (Mode 315) = 16143.49000 (Hz)
Natural freq (Mode 316) = 16191.25000 (Hz)
Natural freq (Mode 317) = 16444.55000 (Hz)
Natural freq (Mode 318) = 16465.20000 (Hz)
Natural freq (Mode 319) = 16540.14000 (Hz)
Natural freq (Mode 320) = 16545.05000 (Hz)
Natural freq (Mode 321) = 16607.63000 (Hz)
Natural freq (Mode 322) = 16787.41000 (Hz)
Natural freq (Mode 323) = 16809.01000 (Hz)
Natural freq (Mode 324) = 16854.44000 (Hz)
Natural freq (Mode 325) = 16898.50000 (Hz)
Natural freq (Mode 326) = 16931.53000 (Hz)
Natural freq (Mode 327) = 16952.62000 (Hz)
Natural freq (Mode 328) = 17074.71000 (Hz)
Natural freq (Mode 329) = 17099.57000 (Hz)
Natural freq (Mode 330) = 17119.86000 (Hz)
Natural freq (Mode 331) = 17222.80000 (Hz)
Natural freq (Mode 332) = 17266.61000 (Hz)
Natural freq (Mode 333) = 17383.30000 (Hz)
Natural freq (Mode 334) = 17418.65000 (Hz)
Natural freq (Mode 335) = 17488.28000 (Hz)
Natural freq (Mode 336) = 17541.06000 (Hz)
Natural freq (Mode 337) = 17694.88000 (Hz)
Natural freq (Mode 338) = 17700.81000 (Hz)
Natural freq (Mode 339) = 17741.71000 (Hz)
Natural freq (Mode 340) = 17800.10000 (Hz)
Natural freq (Mode 341) = 17816.33000 (Hz)
Natural freq (Mode 342) = 17925.23000 (Hz)
Natural freq (Mode 343) = 17964.70000 (Hz)
Natural freq (Mode 344) = 18050.17000 (Hz)
Natural freq (Mode 345) = 18098.53000 (Hz)
Natural freq (Mode 346) = 18131.22000 (Hz)
Natural freq (Mode 347) = 18183.38000 (Hz)
Natural freq (Mode 348) = 18215.32000 (Hz)
Natural freq (Mode 349) = 18334.29000 (Hz)
Natural freq (Mode 350) = 18362.53000 (Hz)
Natural freq (Mode 351) = 18486.87000 (Hz)
Natural freq (Mode 352) = 18591.83000 (Hz)
Natural freq (Mode 353) = 18709.08000 (Hz)
Natural freq (Mode 354) = 18712.34000 (Hz)
Natural freq (Mode 355) = 18799.42000 (Hz)
Natural freq (Mode 356) = 18829.22000 (Hz)
Natural freq (Mode 357) = 18853.39000 (Hz)
Natural freq (Mode 358) = 18976.00000 (Hz)
Natural freq (Mode 359) = 19059.20000 (Hz)
Natural freq (Mode 360) = 19125.02000 (Hz)
Natural freq (Mode 361) = 19157.08000 (Hz)
Natural freq (Mode 362) = 19255.37000 (Hz)
Natural freq (Mode 363) = 19304.60000 (Hz)
Natural freq (Mode 364) = 19419.35000 (Hz)
Natural freq (Mode 365) = 19455.45000 (Hz)
Natural freq (Mode 366) = 19511.95000 (Hz)
Natural freq (Mode 367) = 19591.56000 (Hz)
Natural freq (Mode 368) = 19646.65000 (Hz)
Natural freq (Mode 369) = 19757.04000 (Hz)
Natural freq (Mode 370) = 19782.00000 (Hz)
Natural freq (Mode 371) = 19921.47000 (Hz)
Natural freq (Mode 372) = 20038.24000 (Hz)
Natural freq (Mode 373) = 20087.59000 (Hz)
Natural freq (Mode 374) = 20247.26000 (Hz)
Natural freq (Mode 375) = 20314.55000 (Hz)
Natural freq (Mode 376) = 20347.61000 (Hz)
Natural freq (Mode 377) = 20409.15000 (Hz)
Natural freq (Mode 378) = 20555.38000 (Hz)
Natural freq (Mode 379) = 20745.27000 (Hz)
Natural freq (Mode 380) = 20826.08000 (Hz)
Natural freq (Mode 381) = 20926.47000 (Hz)
Natural freq (Mode 382) = 20927.93000 (Hz)
Natural freq (Mode 383) = 20961.74000 (Hz)
Natural freq (Mode 384) = 21049.74000 (Hz)
Natural freq (Mode 385) = 21086.09000 (Hz)
Natural freq (Mode 386) = 21226.15000 (Hz)
Natural freq (Mode 387) = 21285.19000 (Hz)
Natural freq (Mode 388) = 21322.08000 (Hz)
Natural freq (Mode 389) = 21443.02000 (Hz)
Natural freq (Mode 390) = 21485.59000 (Hz)
Natural freq (Mode 391) = 21498.71000 (Hz)
Natural freq (Mode 392) = 21600.59000 (Hz)
Natural freq (Mode 393) = 21699.40000 (Hz)
Natural freq (Mode 394) = 21749.01000 (Hz)
Natural freq (Mode 395) = 21760.19000 (Hz)
Natural freq (Mode 396) = 21871.83000 (Hz)
Natural freq (Mode 397) = 21968.82000 (Hz)
Natural freq (Mode 398) = 22004.93000 (Hz)
Natural freq (Mode 399) = 22037.06000 (Hz)
Natural freq (Mode 400) = 22132.05000 (Hz)
Natural freq (Mode 401) = 22272.75000 (Hz)
Natural freq (Mode 402) = 22284.71000 (Hz)
Natural freq (Mode 403) = 22343.19000 (Hz)
Natural freq (Mode 404) = 22492.85000 (Hz)
Natural freq (Mode 405) = 22675.22000 (Hz)
Natural freq (Mode 406) = 22726.67000 (Hz)
Natural freq (Mode 407) = 22795.38000 (Hz)
Natural freq (Mode 408) = 22847.12000 (Hz)
Natural freq (Mode 409) = 23027.21000 (Hz)
Natural freq (Mode 410) = 23066.16000 (Hz)
Natural freq (Mode 411) = 23111.55000 (Hz)
Natural freq (Mode 412) = 23264.07000 (Hz)
Natural freq (Mode 413) = 23277.39000 (Hz)
Natural freq (Mode 414) = 23280.87000 (Hz)
Natural freq (Mode 415) = 23489.27000 (Hz)
Natural freq (Mode 416) = 23508.29000 (Hz)
Natural freq (Mode 417) = 23538.90000 (Hz)
Natural freq (Mode 418) = 23734.87000 (Hz)
Natural freq (Mode 419) = 23748.21000 (Hz)
Natural freq (Mode 420) = 23776.47000 (Hz)
Natural freq (Mode 421) = 23836.88000 (Hz)
Natural freq (Mode 422) = 23851.33000 (Hz)
Natural freq (Mode 423) = 23996.21000 (Hz)
Natural freq (Mode 424) = 24072.71000 (Hz)
Natural freq (Mode 425) = 24231.38000 (Hz)
Natural freq (Mode 426) = 24326.89000 (Hz)
Natural freq (Mode 427) = 24335.46000 (Hz)
Natural freq (Mode 428) = 24378.13000 (Hz)
Natural freq (Mode 429) = 24422.91000 (Hz)
Natural freq (Mode 430) = 24535.55000 (Hz)
Natural freq (Mode 431) = 24612.28000 (Hz)
Natural freq (Mode 432) = 24749.69000 (Hz)
Natural freq (Mode 433) = 24864.25000 (Hz)
Natural freq (Mode 434) = 25020.23000 (Hz)
Natural freq (Mode 435) = 25036.26000 (Hz)
Natural freq (Mode 436) = 25255.07000 (Hz)
Natural freq (Mode 437) = 25348.07000 (Hz)
Natural freq (Mode 438) = 25376.09000 (Hz)
Natural freq (Mode 439) = 25408.28000 (Hz)
Natural freq (Mode 440) = 25484.80000 (Hz)
Natural freq (Mode 441) = 25615.76000 (Hz)
Natural freq (Mode 442) = 25669.87000 (Hz)
Natural freq (Mode 443) = 25819.13000 (Hz)
Natural freq (Mode 444) = 25981.25000 (Hz)
Natural freq (Mode 445) = 25999.63000 (Hz)
Natural freq (Mode 446) = 26070.56000 (Hz)
Natural freq (Mode 447) = 26145.77000 (Hz)
Natural freq (Mode 448) = 26279.59000 (Hz)
Natural freq (Mode 449) = 26351.51000 (Hz)
Natural freq (Mode 450) = 26395.38000 (Hz)
Natural freq (Mode 451) = 26502.02000 (Hz)
Natural freq (Mode 452) = 26532.53000 (Hz)
Natural freq (Mode 453) = 26637.85000 (Hz)
Natural freq (Mode 454) = 26643.48000 (Hz)
Natural freq (Mode 455) = 26745.91000 (Hz)
Natural freq (Mode 456) = 26934.27000 (Hz)
Natural freq (Mode 457) = 27070.38000 (Hz)
Natural freq (Mode 458) = 27164.86000 (Hz)
Natural freq (Mode 459) = 27237.99000 (Hz)
Natural freq (Mode 460) = 27380.39000 (Hz)
Natural freq (Mode 461) = 27500.71000 (Hz)
Natural freq (Mode 462) = 27556.49000 (Hz)
Natural freq (Mode 463) = 27702.19000 (Hz)
Natural freq (Mode 464) = 27702.94000 (Hz)
Natural freq (Mode 465) = 27916.39000 (Hz)
Natural freq (Mode 466) = 28012.95000 (Hz)
Natural freq (Mode 467) = 28161.58000 (Hz)
Natural freq (Mode 468) = 28179.12000 (Hz)
Natural freq (Mode 469) = 28422.62000 (Hz)
Natural freq (Mode 470) = 28474.77000 (Hz)
Natural freq (Mode 471) = 28560.92000 (Hz)
Natural freq (Mode 472) = 28566.15000 (Hz)
Natural freq (Mode 473) = 28710.87000 (Hz)
Natural freq (Mode 474) = 28781.45000 (Hz)
Natural freq (Mode 475) = 28999.03000 (Hz)
Natural freq (Mode 476) = 29078.86000 (Hz)
Natural freq (Mode 477) = 29154.48000 (Hz)
Natural freq (Mode 478) = 29296.92000 (Hz)
Natural freq (Mode 479) = 29356.81000 (Hz)
Natural freq (Mode 480) = 29380.71000 (Hz)
Natural freq (Mode 481) = 29478.38000 (Hz)
Natural freq (Mode 482) = 29553.13000 (Hz)
Natural freq (Mode 483) = 29622.04000 (Hz)
Natural freq (Mode 484) = 29712.53000 (Hz)
Natural freq (Mode 485) = 30011.06000 (Hz)
Natural freq (Mode 486) = 30035.66000 (Hz)
Natural freq (Mode 487) = 30102.46000 (Hz)
Natural freq (Mode 488) = 30209.47000 (Hz)
Natural freq (Mode 489) = 30280.31000 (Hz)
Natural freq (Mode 490) = 30323.96000 (Hz)
Natural freq (Mode 491) = 30365.31000 (Hz)
Natural freq (Mode 492) = 30520.68000 (Hz)
Natural freq (Mode 493) = 30541.57000 (Hz)
Natural freq (Mode 494) = 30606.26000 (Hz)
Natural freq (Mode 495) = 30742.72000 (Hz)
Natural freq (Mode 496) = 30869.45000 (Hz)
Natural freq (Mode 497) = 30969.95000 (Hz)
Natural freq (Mode 498) = 31100.58000 (Hz)
Natural freq (Mode 499) = 31169.65000 (Hz)
Natural freq (Mode 500) = 31244.07000 (Hz)
Natural freq (Mode 501) = 31425.86000 (Hz)
Natural freq (Mode 502) = 31537.51000 (Hz)
Natural freq (Mode 503) = 31639.96000 (Hz)
Natural freq (Mode 504) = 31754.34000 (Hz)
Natural freq (Mode 505) = 31760.84000 (Hz)
Natural freq (Mode 506) = 31883.20000 (Hz)
Natural freq (Mode 507) = 32002.92000 (Hz)
Natural freq (Mode 508) = 32220.74000 (Hz)
Natural freq (Mode 509) = 32290.88000 (Hz)
Natural freq (Mode 510) = 32391.40000 (Hz)
Natural freq (Mode 511) = 32608.03000 (Hz)
Natural freq (Mode 512) = 32647.91000 (Hz)
Natural freq (Mode 513) = 32720.89000 (Hz)
Natural freq (Mode 514) = 32949.41000 (Hz)
Natural freq (Mode 515) = 32988.75000 (Hz)
Natural freq (Mode 516) = 33115.60000 (Hz)
Natural freq (Mode 517) = 33200.03000 (Hz)
Natural freq (Mode 518) = 33318.92000 (Hz)
Natural freq (Mode 519) = 33330.25000 (Hz)
Natural freq (Mode 520) = 33333.78000 (Hz)
Natural freq (Mode 521) = 33486.56000 (Hz)
Natural freq (Mode 522) = 33531.17000 (Hz)
Natural freq (Mode 523) = 33683.28000 (Hz)
Natural freq (Mode 524) = 33797.57000 (Hz)
Natural freq (Mode 525) = 33906.94000 (Hz)
Natural freq (Mode 526) = 33914.80000 (Hz)
Natural freq (Mode 527) = 33989.41000 (Hz)
Natural freq (Mode 528) = 34210.63000 (Hz)
Natural freq (Mode 529) = 34378.73000 (Hz)
Natural freq (Mode 530) = 34494.40000 (Hz)
Natural freq (Mode 531) = 34582.28000 (Hz)
Natural freq (Mode 532) = 34836.82000 (Hz)
Natural freq (Mode 533) = 34902.17000 (Hz)
Natural freq (Mode 534) = 34987.61000 (Hz)
Natural freq (Mode 535) = 35067.79000 (Hz)
Natural freq (Mode 536) = 35153.96000 (Hz)
Natural freq (Mode 537) = 35173.18000 (Hz)
Natural freq (Mode 538) = 35315.79000 (Hz)
Natural freq (Mode 539) = 35452.04000 (Hz)
Natural freq (Mode 540) = 35564.39000 (Hz)
Natural freq (Mode 541) = 35577.60000 (Hz)
Natural freq (Mode 542) = 35671.63000 (Hz)
Natural freq (Mode 543) = 35764.36000 (Hz)
Natural freq (Mode 544) = 35817.39000 (Hz)
Natural freq (Mode 545) = 35987.39000 (Hz)
Natural freq (Mode 546) = 35988.65000 (Hz)
Natural freq (Mode 547) = 36149.87000 (Hz)
Natural freq (Mode 548) = 36216.11000 (Hz)
Natural freq (Mode 549) = 36374.59000 (Hz)
Natural freq (Mode 550) = 36456.40000 (Hz)
Natural freq (Mode 551) = 36643.81000 (Hz)
Natural freq (Mode 552) = 36841.90000 (Hz)
Natural freq (Mode 553) = 36898.49000 (Hz)
Natural freq (Mode 554) = 36940.48000 (Hz)
Natural freq (Mode 555) = 37109.42000 (Hz)
Natural freq (Mode 556) = 37109.45000 (Hz)
Natural freq (Mode 557) = 37157.88000 (Hz)
Natural freq (Mode 558) = 37177.07000 (Hz)
Natural freq (Mode 559) = 37287.62000 (Hz)
Natural freq (Mode 560) = 37387.53000 (Hz)
Natural freq (Mode 561) = 37522.76000 (Hz)
Natural freq (Mode 562) = 37628.77000 (Hz)
Natural freq (Mode 563) = 37734.15000 (Hz)
Natural freq (Mode 564) = 37824.32000 (Hz)
Natural freq (Mode 565) = 37936.66000 (Hz)
Natural freq (Mode 566) = 38054.42000 (Hz)
Natural freq (Mode 567) = 38287.95000 (Hz)
Natural freq (Mode 568) = 38432.25000 (Hz)
Natural freq (Mode 569) = 38489.84000 (Hz)
Natural freq (Mode 570) = 38652.49000 (Hz)
Natural freq (Mode 571) = 38702.59000 (Hz)
Natural freq (Mode 572) = 38877.29000 (Hz)
Natural freq (Mode 573) = 39004.32000 (Hz)
Natural freq (Mode 574) = 39191.21000 (Hz)
Natural freq (Mode 575) = 39286.07000 (Hz)
Natural freq (Mode 576) = 39329.37000 (Hz)
Natural freq (Mode 577) = 39574.73000 (Hz)
Natural freq (Mode 578) = 39720.89000 (Hz)
Natural freq (Mode 579) = 40162.23000 (Hz)
Natural freq (Mode 580) = 40253.22000 (Hz)
Natural freq (Mode 581) = 40293.79000 (Hz)
Natural freq (Mode 582) = 40337.32000 (Hz)
Natural freq (Mode 583) = 40474.10000 (Hz)
Natural freq (Mode 584) = 40602.31000 (Hz)
Natural freq (Mode 585) = 40635.95000 (Hz)
Natural freq (Mode 586) = 40660.85000 (Hz)
Natural freq (Mode 587) = 40743.75000 (Hz)
Natural freq (Mode 588) = 40756.84000 (Hz)
Natural freq (Mode 589) = 40949.57000 (Hz)
Natural freq (Mode 590) = 40995.24000 (Hz)
Natural freq (Mode 591) = 41223.55000 (Hz)
Natural freq (Mode 592) = 41359.39000 (Hz)
Natural freq (Mode 593) = 41528.88000 (Hz)
Natural freq (Mode 594) = 41791.72000 (Hz)
Natural freq (Mode 595) = 41887.48000 (Hz)
Natural freq (Mode 596) = 42118.45000 (Hz)
Natural freq (Mode 597) = 42198.64000 (Hz)
Natural freq (Mode 598) = 42348.55000 (Hz)
Natural freq (Mode 599) = 42370.13000 (Hz)
Natural freq (Mode 600) = 42416.97000 (Hz)
Natural freq (Mode 601) = 42462.20000 (Hz)
Natural freq (Mode 602) = 42642.21000 (Hz)
Natural freq (Mode 603) = 42726.17000 (Hz)
Natural freq (Mode 604) = 42854.97000 (Hz)
Natural freq (Mode 605) = 42962.25000 (Hz)
Natural freq (Mode 606) = 43123.13000 (Hz)
Natural freq (Mode 607) = 43203.68000 (Hz)
Natural freq (Mode 608) = 43400.77000 (Hz)
Natural freq (Mode 609) = 43508.95000 (Hz)
Natural freq (Mode 610) = 43597.38000 (Hz)
Natural freq (Mode 611) = 43700.77000 (Hz)
Natural freq (Mode 612) = 43704.76000 (Hz)
Natural freq (Mode 613) = 43877.68000 (Hz)
Natural freq (Mode 614) = 44012.25000 (Hz)
Natural freq (Mode 615) = 44106.74000 (Hz)
Natural freq (Mode 616) = 44292.90000 (Hz)
Natural freq (Mode 617) = 44314.06000 (Hz)
Natural freq (Mode 618) = 44374.05000 (Hz)
Natural freq (Mode 619) = 44397.46000 (Hz)
Natural freq (Mode 620) = 44586.68000 (Hz)
Natural freq (Mode 621) = 44696.46000 (Hz)
Natural freq (Mode 622) = 44741.60000 (Hz)
Natural freq (Mode 623) = 45054.47000 (Hz)
Natural freq (Mode 624) = 45140.14000 (Hz)
Natural freq (Mode 625) = 45249.72000 (Hz)
Natural freq (Mode 626) = 45385.59000 (Hz)
Natural freq (Mode 627) = 45567.35000 (Hz)
Natural freq (Mode 628) = 45605.37000 (Hz)
Natural freq (Mode 629) = 45735.81000 (Hz)
Natural freq (Mode 630) = 45752.43000 (Hz)
Natural freq (Mode 631) = 46051.15000 (Hz)
Natural freq (Mode 632) = 46420.19000 (Hz)
Natural freq (Mode 633) = 46488.60000 (Hz)
Natural freq (Mode 634) = 46552.35000 (Hz)
Natural freq (Mode 635) = 46577.11000 (Hz)
Natural freq (Mode 636) = 46578.90000 (Hz)
Natural freq (Mode 637) = 46694.76000 (Hz)
Natural freq (Mode 638) = 46912.64000 (Hz)
Natural freq (Mode 639) = 46981.14000 (Hz)
Natural freq (Mode 640) = 47193.58000 (Hz)
Natural freq (Mode 641) = 47238.25000 (Hz)
Natural freq (Mode 642) = 47338.20000 (Hz)
Natural freq (Mode 643) = 47429.59000 (Hz)
Natural freq (Mode 644) = 47576.44000 (Hz)
Natural freq (Mode 645) = 47611.71000 (Hz)
Natural freq (Mode 646) = 47691.93000 (Hz)
Natural freq (Mode 647) = 47807.08000 (Hz)
Natural freq (Mode 648) = 47890.22000 (Hz)
Natural freq (Mode 649) = 47917.94000 (Hz)
Natural freq (Mode 650) = 48003.06000 (Hz)
Natural freq (Mode 651) = 48405.16000 (Hz)
Natural freq (Mode 652) = 48501.56000 (Hz)
Natural freq (Mode 653) = 48589.31000 (Hz)
Natural freq (Mode 654) = 48598.45000 (Hz)
Natural freq (Mode 655) = 48779.29000 (Hz)
Natural freq (Mode 656) = 48883.09000 (Hz)
Natural freq (Mode 657) = 48930.20000 (Hz)
Natural freq (Mode 658) = 49088.71000 (Hz)
Natural freq (Mode 659) = 49207.57000 (Hz)
Natural freq (Mode 660) = 49256.51000 (Hz)
Natural freq (Mode 661) = 49376.35000 (Hz)
Natural freq (Mode 662) = 49480.93000 (Hz)
Natural freq (Mode 663) = 49565.85000 (Hz)
Natural freq (Mode 664) = 49718.37000 (Hz)
Natural freq (Mode 665) = 49722.37000 (Hz)
Natural freq (Mode 666) = 49790.09000 (Hz)
Natural freq (Mode 667) = 49897.80000 (Hz)
Natural freq (Mode 668) = 50054.08000 (Hz)
Natural freq (Mode 669) = 50090.88000 (Hz)
Natural freq (Mode 670) = 50160.08000 (Hz)
Natural freq (Mode 671) = 50228.52000 (Hz)
Natural freq (Mode 672) = 50465.21000 (Hz)
Natural freq (Mode 673) = 50484.11000 (Hz)
Natural freq (Mode 674) = 50692.21000 (Hz)
Natural freq (Mode 675) = 50853.68000 (Hz)
Natural freq (Mode 676) = 50857.21000 (Hz)
Natural freq (Mode 677) = 50936.92000 (Hz)
Natural freq (Mode 678) = 51135.05000 (Hz)
Natural freq (Mode 679) = 51171.95000 (Hz)
Natural freq (Mode 680) = 51382.60000 (Hz)
Natural freq (Mode 681) = 51500.84000 (Hz)
Natural freq (Mode 682) = 51551.45000 (Hz)
Natural freq (Mode 683) = 51604.40000 (Hz)
Natural freq (Mode 684) = 51794.87000 (Hz)
Natural freq (Mode 685) = 51921.50000 (Hz)
Natural freq (Mode 686) = 52077.61000 (Hz)
Natural freq (Mode 687) = 52106.14000 (Hz)
Natural freq (Mode 688) = 52156.48000 (Hz)
Natural freq (Mode 689) = 52196.38000 (Hz)
Natural freq (Mode 690) = 52375.95000 (Hz)
Natural freq (Mode 691) = 52511.88000 (Hz)
Natural freq (Mode 692) = 52690.02000 (Hz)
Natural freq (Mode 693) = 52760.29000 (Hz)
Natural freq (Mode 694) = 52983.51000 (Hz)
Natural freq (Mode 695) = 53151.14000 (Hz)
Natural freq (Mode 696) = 53168.78000 (Hz)
Natural freq (Mode 697) = 53351.66000 (Hz)
Natural freq (Mode 698) = 53457.94000 (Hz)
Natural freq (Mode 699) = 53501.50000 (Hz)
Natural freq (Mode 700) = 53568.66000 (Hz)
Natural freq (Mode 701) = 53771.08000 (Hz)
Natural freq (Mode 702) = 53815.28000 (Hz)
Natural freq (Mode 703) = 53819.51000 (Hz)
Natural freq (Mode 704) = 54018.69000 (Hz)
Natural freq (Mode 705) = 54206.11000 (Hz)
Natural freq (Mode 706) = 54242.44000 (Hz)
Natural freq (Mode 707) = 54451.73000 (Hz)
Natural freq (Mode 708) = 54504.73000 (Hz)
Natural freq (Mode 709) = 54515.07000 (Hz)
Natural freq (Mode 710) = 54603.34000 (Hz)
Natural freq (Mode 711) = 54798.02000 (Hz)
Natural freq (Mode 712) = 54826.34000 (Hz)
Natural freq (Mode 713) = 54976.60000 (Hz)
Natural freq (Mode 714) = 55099.90000 (Hz)
Natural freq (Mode 715) = 55233.76000 (Hz)
Natural freq (Mode 716) = 55312.55000 (Hz)
Natural freq (Mode 717) = 55359.35000 (Hz)
Natural freq (Mode 718) = 55622.14000 (Hz)
Natural freq (Mode 719) = 55794.26000 (Hz)
Natural freq (Mode 720) = 55892.18000 (Hz)
Natural freq (Mode 721) = 56015.41000 (Hz)
Natural freq (Mode 722) = 56088.41000 (Hz)
Natural freq (Mode 723) = 56115.56000 (Hz)
Natural freq (Mode 724) = 56334.32000 (Hz)
Natural freq (Mode 725) = 56351.92000 (Hz)
Natural freq (Mode 726) = 56609.43000 (Hz)
Natural freq (Mode 727) = 56690.62000 (Hz)
Natural freq (Mode 728) = 56781.62000 (Hz)
Natural freq (Mode 729) = 56865.87000 (Hz)
Natural freq (Mode 730) = 56948.31000 (Hz)
Natural freq (Mode 731) = 57119.90000 (Hz)
Natural freq (Mode 732) = 57228.48000 (Hz)
Natural freq (Mode 733) = 57330.72000 (Hz)
Natural freq (Mode 734) = 57473.44000 (Hz)
Natural freq (Mode 735) = 57547.01000 (Hz)
Natural freq (Mode 736) = 57627.58000 (Hz)
Natural freq (Mode 737) = 57732.92000 (Hz)
Natural freq (Mode 738) = 57822.45000 (Hz)
Natural freq (Mode 739) = 57992.67000 (Hz)
Natural freq (Mode 740) = 58178.70000 (Hz)
Natural freq (Mode 741) = 58235.37000 (Hz)
Natural freq (Mode 742) = 58342.95000 (Hz)
Natural freq (Mode 743) = 58393.04000 (Hz)
Natural freq (Mode 744) = 58548.01000 (Hz)
Natural freq (Mode 745) = 58743.37000 (Hz)
Natural freq (Mode 746) = 58747.77000 (Hz)
Natural freq (Mode 747) = 58763.92000 (Hz)
Natural freq (Mode 748) = 58967.43000 (Hz)
Natural freq (Mode 749) = 59096.52000 (Hz)
Natural freq (Mode 750) = 59102.65000 (Hz)
Natural freq (Mode 751) = 59219.30000 (Hz)
Natural freq (Mode 752) = 59386.15000 (Hz)
Natural freq (Mode 753) = 59562.50000 (Hz)
Natural freq (Mode 754) = 59631.56000 (Hz)
Natural freq (Mode 755) = 59639.75000 (Hz)
Natural freq (Mode 756) = 59712.64000 (Hz)
Natural freq (Mode 757) = 59838.64000 (Hz)
Natural freq (Mode 758) = 59903.59000 (Hz)
Natural freq (Mode 759) = 60006.47000 (Hz)
Natural freq (Mode 760) = 60127.36000 (Hz)
Natural freq (Mode 761) = 60224.49000 (Hz)
Natural freq (Mode 762) = 60294.48000 (Hz)
Natural freq (Mode 763) = 60324.69000 (Hz)
Natural freq (Mode 764) = 60396.43000 (Hz)
Natural freq (Mode 765) = 60515.33000 (Hz)
Natural freq (Mode 766) = 60559.32000 (Hz)
Natural freq (Mode 767) = 60678.05000 (Hz)
Natural freq (Mode 768) = 60828.19000 (Hz)
Natural freq (Mode 769) = 60907.92000 (Hz)
Natural freq (Mode 770) = 61254.36000 (Hz)
Natural freq (Mode 771) = 61307.17000 (Hz)
Natural freq (Mode 772) = 61381.37000 (Hz)
Natural freq (Mode 773) = 61481.29000 (Hz)
Natural freq (Mode 774) = 61562.68000 (Hz)
Natural freq (Mode 775) = 61716.24000 (Hz)
Natural freq (Mode 776) = 61781.28000 (Hz)
Natural freq (Mode 777) = 61795.57000 (Hz)
Natural freq (Mode 778) = 61994.89000 (Hz)
Natural freq (Mode 779) = 62094.15000 (Hz)
Natural freq (Mode 780) = 62113.02000 (Hz)
Natural freq (Mode 781) = 62222.04000 (Hz)
Natural freq (Mode 782) = 62288.52000 (Hz)
Natural freq (Mode 783) = 62385.94000 (Hz)
Natural freq (Mode 784) = 62396.24000 (Hz)
Natural freq (Mode 785) = 62527.74000 (Hz)
Natural freq (Mode 786) = 62579.81000 (Hz)
Natural freq (Mode 787) = 62721.25000 (Hz)
Natural freq (Mode 788) = 62738.94000 (Hz)
Natural freq (Mode 789) = 62865.63000 (Hz)
Natural freq (Mode 790) = 62948.16000 (Hz)
Natural freq (Mode 791) = 63042.76000 (Hz)
Natural freq (Mode 792) = 63143.53000 (Hz)
Natural freq (Mode 793) = 63170.49000 (Hz)
Natural freq (Mode 794) = 63233.18000 (Hz)
Natural freq (Mode 795) = 63391.41000 (Hz)
Natural freq (Mode 796) = 63540.32000 (Hz)
Natural freq (Mode 797) = 63602.34000 (Hz)
Natural freq (Mode 798) = 63750.55000 (Hz)
Natural freq (Mode 799) = 63885.63000 (Hz)
Natural freq (Mode 800) = 63965.49000 (Hz)
Natural freq (Mode 801) = 64042.26000 (Hz)
Natural freq (Mode 802) = 64146.40000 (Hz)
Natural freq (Mode 803) = 64163.32000 (Hz)
Natural freq (Mode 804) = 64321.53000 (Hz)
Natural freq (Mode 805) = 64416.47000 (Hz)
Natural freq (Mode 806) = 64596.16000 (Hz)
Natural freq (Mode 807) = 64668.98000 (Hz)
Natural freq (Mode 808) = 64816.43000 (Hz)
Natural freq (Mode 809) = 64962.29000 (Hz)
Natural freq (Mode 810) = 65109.30000 (Hz)
Natural freq (Mode 811) = 65160.50000 (Hz)
Natural freq (Mode 812) = 65187.46000 (Hz)
Natural freq (Mode 813) = 65332.37000 (Hz)
Natural freq (Mode 814) = 65388.61000 (Hz)
Natural freq (Mode 815) = 65410.63000 (Hz)
Natural freq (Mode 816) = 65475.19000 (Hz)
Natural freq (Mode 817) = 65597.51000 (Hz)
Natural freq (Mode 818) = 65661.34000 (Hz)
Natural freq (Mode 819) = 65720.16000 (Hz)
Natural freq (Mode 820) = 65867.98000 (Hz)
Natural freq (Mode 821) = 66059.62000 (Hz)
Natural freq (Mode 822) = 66131.58000 (Hz)
Natural freq (Mode 823) = 66322.35000 (Hz)
Natural freq (Mode 824) = 66464.03000 (Hz)
Natural freq (Mode 825) = 66530.87000 (Hz)
Natural freq (Mode 826) = 66564.12000 (Hz)
Natural freq (Mode 827) = 66605.34000 (Hz)
Natural freq (Mode 828) = 66789.47000 (Hz)
Natural freq (Mode 829) = 66945.90000 (Hz)
Natural freq (Mode 830) = 66998.07000 (Hz)
Natural freq (Mode 831) = 67080.26000 (Hz)
Natural freq (Mode 832) = 67189.01000 (Hz)
Natural freq (Mode 833) = 67243.66000 (Hz)
Natural freq (Mode 834) = 67296.74000 (Hz)
Natural freq (Mode 835) = 67376.41000 (Hz)
Natural freq (Mode 836) = 67513.82000 (Hz)
Natural freq (Mode 837) = 67567.81000 (Hz)
Natural freq (Mode 838) = 67666.32000 (Hz)
Natural freq (Mode 839) = 67841.24000 (Hz)
Natural freq (Mode 840) = 67908.45000 (Hz)
Natural freq (Mode 841) = 68016.58000 (Hz)
Natural freq (Mode 842) = 68079.98000 (Hz)
Natural freq (Mode 843) = 68176.81000 (Hz)
Natural freq (Mode 844) = 68460.19000 (Hz)
Natural freq (Mode 845) = 68554.47000 (Hz)
Natural freq (Mode 846) = 68590.22000 (Hz)
Natural freq (Mode 847) = 68651.88000 (Hz)
Natural freq (Mode 848) = 68687.21000 (Hz)
Natural freq (Mode 849) = 68786.12000 (Hz)
Natural freq (Mode 850) = 68856.07000 (Hz)
Natural freq (Mode 851) = 68911.45000 (Hz)
Natural freq (Mode 852) = 68921.30000 (Hz)
Natural freq (Mode 853) = 69021.59000 (Hz)
Natural freq (Mode 854) = 69065.40000 (Hz)
Natural freq (Mode 855) = 69205.85000 (Hz)
Natural freq (Mode 856) = 69252.89000 (Hz)
Natural freq (Mode 857) = 69340.47000 (Hz)
Natural freq (Mode 858) = 69375.84000 (Hz)
Natural freq (Mode 859) = 69440.12000 (Hz)
Natural freq (Mode 860) = 69512.06000 (Hz)
Natural freq (Mode 861) = 69654.96000 (Hz)
Natural freq (Mode 862) = 69777.94000 (Hz)
Natural freq (Mode 863) = 69802.79000 (Hz)
Natural freq (Mode 864) = 69841.16000 (Hz)
Natural freq (Mode 865) = 69862.84000 (Hz)
Natural freq (Mode 866) = 70097.50000 (Hz)
Natural freq (Mode 867) = 70162.36000 (Hz)
Natural freq (Mode 868) = 70263.24000 (Hz)
Natural freq (Mode 869) = 70382.94000 (Hz)
Natural freq (Mode 870) = 70458.26000 (Hz)
Natural freq (Mode 871) = 70518.42000 (Hz)
Natural freq (Mode 872) = 70586.77000 (Hz)
Natural freq (Mode 873) = 70696.01000 (Hz)
Natural freq (Mode 874) = 70815.79000 (Hz)
Natural freq (Mode 875) = 70909.97000 (Hz)
Natural freq (Mode 876) = 70983.21000 (Hz)
Natural freq (Mode 877) = 71056.86000 (Hz)
Natural freq (Mode 878) = 71154.90000 (Hz)
Natural freq (Mode 879) = 71186.77000 (Hz)
Natural freq (Mode 880) = 71297.27000 (Hz)
Natural freq (Mode 881) = 71311.62000 (Hz)
Natural freq (Mode 882) = 71367.08000 (Hz)
Natural freq (Mode 883) = 71546.12000 (Hz)
Natural freq (Mode 884) = 71616.69000 (Hz)
Natural freq (Mode 885) = 71716.84000 (Hz)
Natural freq (Mode 886) = 71918.26000 (Hz)
Natural freq (Mode 887) = 72018.71000 (Hz)
Natural freq (Mode 888) = 72140.89000 (Hz)
Natural freq (Mode 889) = 72189.70000 (Hz)
Natural freq (Mode 890) = 72303.92000 (Hz)
Natural freq (Mode 891) = 72392.19000 (Hz)
Natural freq (Mode 892) = 72479.59000 (Hz)
Natural freq (Mode 893) = 72685.64000 (Hz)
Natural freq (Mode 894) = 72758.08000 (Hz)
Natural freq (Mode 895) = 72772.19000 (Hz)
Natural freq (Mode 896) = 72899.19000 (Hz)
Natural freq (Mode 897) = 73060.15000 (Hz)
Natural freq (Mode 898) = 73133.38000 (Hz)
Natural freq (Mode 899) = 73302.51000 (Hz)
Natural freq (Mode 900) = 73340.19000 (Hz)
Natural freq (Mode 901) = 73393.19000 (Hz)
Natural freq (Mode 902) = 73522.47000 (Hz)
Natural freq (Mode 903) = 73626.04000 (Hz)
Natural freq (Mode 904) = 73721.49000 (Hz)
Natural freq (Mode 905) = 73739.77000 (Hz)
Natural freq (Mode 906) = 73766.51000 (Hz)
Natural freq (Mode 907) = 73944.32000 (Hz)
Natural freq (Mode 908) = 74006.82000 (Hz)
Natural freq (Mode 909) = 74121.25000 (Hz)
Natural freq (Mode 910) = 74153.07000 (Hz)
Natural freq (Mode 911) = 74175.30000 (Hz)
Natural freq (Mode 912) = 74249.00000 (Hz)
Natural freq (Mode 913) = 74364.63000 (Hz)
Natural freq (Mode 914) = 74494.14000 (Hz)
Natural freq (Mode 915) = 74538.38000 (Hz)
Natural freq (Mode 916) = 74634.16000 (Hz)
Natural freq (Mode 917) = 74679.94000 (Hz)
Natural freq (Mode 918) = 74739.85000 (Hz)
Natural freq (Mode 919) = 74803.58000 (Hz)
Natural freq (Mode 920) = 74993.28000 (Hz)
Natural freq (Mode 921) = 75053.98000 (Hz)
Natural freq (Mode 922) = 75093.93000 (Hz)
Natural freq (Mode 923) = 75299.71000 (Hz)
Natural freq (Mode 924) = 75358.80000 (Hz)
Natural freq (Mode 925) = 75425.58000 (Hz)
Natural freq (Mode 926) = 75536.12000 (Hz)
Natural freq (Mode 927) = 75713.14000 (Hz)
Natural freq (Mode 928) = 75834.39000 (Hz)
Natural freq (Mode 929) = 75884.56000 (Hz)
Natural freq (Mode 930) = 76007.14000 (Hz)
Natural freq (Mode 931) = 76120.42000 (Hz)
Natural freq (Mode 932) = 76225.74000 (Hz)
Natural freq (Mode 933) = 76255.57000 (Hz)
Natural freq (Mode 934) = 76430.79000 (Hz)
Natural freq (Mode 935) = 76638.92000 (Hz)
Natural freq (Mode 936) = 76687.01000 (Hz)
Natural freq (Mode 937) = 76810.80000 (Hz)
Natural freq (Mode 938) = 76828.09000 (Hz)
Natural freq (Mode 939) = 76925.01000 (Hz)
Natural freq (Mode 940) = 77008.94000 (Hz)
Natural freq (Mode 941) = 77102.92000 (Hz)
Natural freq (Mode 942) = 77151.28000 (Hz)
Natural freq (Mode 943) = 77289.38000 (Hz)
Natural freq (Mode 944) = 77372.04000 (Hz)
Natural freq (Mode 945) = 77376.51000 (Hz)
Natural freq (Mode 946) = 77440.76000 (Hz)
Natural freq (Mode 947) = 77523.43000 (Hz)
Natural freq (Mode 948) = 77561.89000 (Hz)
Natural freq (Mode 949) = 77587.38000 (Hz)
Natural freq (Mode 950) = 77748.95000 (Hz)
Natural freq (Mode 951) = 77853.38000 (Hz)
Natural freq (Mode 952) = 77858.82000 (Hz)
Natural freq (Mode 953) = 77953.25000 (Hz)
Natural freq (Mode 954) = 78000.41000 (Hz)
Natural freq (Mode 955) = 78099.35000 (Hz)
Natural freq (Mode 956) = 78253.68000 (Hz)
Natural freq (Mode 957) = 78382.22000 (Hz)
Natural freq (Mode 958) = 78418.48000 (Hz)
Natural freq (Mode 959) = 78515.48000 (Hz)
Natural freq (Mode 960) = 78610.92000 (Hz)
Natural freq (Mode 961) = 78645.10000 (Hz)
Natural freq (Mode 962) = 78727.57000 (Hz)
Natural freq (Mode 963) = 78863.91000 (Hz)
Natural freq (Mode 964) = 78937.32000 (Hz)
Natural freq (Mode 965) = 79053.58000 (Hz)
Natural freq (Mode 966) = 79077.26000 (Hz)
Natural freq (Mode 967) = 79215.24000 (Hz)
Natural freq (Mode 968) = 79294.12000 (Hz)
Natural freq (Mode 969) = 79324.82000 (Hz)
Natural freq (Mode 970) = 79362.91000 (Hz)
Natural freq (Mode 971) = 79527.23000 (Hz)
Natural freq (Mode 972) = 79611.69000 (Hz)
Natural freq (Mode 973) = 79647.10000 (Hz)
Natural freq (Mode 974) = 79832.89000 (Hz)
Natural freq (Mode 975) = 79866.64000 (Hz)
Natural freq (Mode 976) = 79970.43000 (Hz)
Natural freq (Mode 977) = 80030.32000 (Hz)
Natural freq (Mode 978) = 80104.74000 (Hz)
Natural freq (Mode 979) = 80123.64000 (Hz)
Natural freq (Mode 980) = 80182.67000 (Hz)
Natural freq (Mode 981) = 80321.53000 (Hz)
Natural freq (Mode 982) = 80385.61000 (Hz)
Natural freq (Mode 983) = 80444.38000 (Hz)
Natural freq (Mode 984) = 80581.53000 (Hz)
Natural freq (Mode 985) = 80665.28000 (Hz)
Natural freq (Mode 986) = 80757.29000 (Hz)
Natural freq (Mode 987) = 80846.96000 (Hz)
Natural freq (Mode 988) = 81004.13000 (Hz)
Natural freq (Mode 989) = 81044.79000 (Hz)
Natural freq (Mode 990) = 81140.53000 (Hz)
Natural freq (Mode 991) = 81244.66000 (Hz)
Natural freq (Mode 992) = 81434.94000 (Hz)
Natural freq (Mode 993) = 81460.92000 (Hz)
Natural freq (Mode 994) = 81502.50000 (Hz)
Natural freq (Mode 995) = 81572.23000 (Hz)
Natural freq (Mode 996) = 81703.12000 (Hz)
Natural freq (Mode 997) = 81809.87000 (Hz)
Natural freq (Mode 998) = 81917.77000 (Hz)
Natural freq (Mode 999) = 81922.97000 (Hz)
Natural freq (Mode 1000) = 82100.35000 (Hz)
Natural freq (Mode 1001) = 82120.03000 (Hz)
Natural freq (Mode 1002) = 82160.63000 (Hz)
Natural freq (Mode 1003) = 82272.67000 (Hz)
Natural freq (Mode 1004) = 82375.92000 (Hz)
Natural freq (Mode 1005) = 82426.08000 (Hz)
Natural freq (Mode 1006) = 82607.53000 (Hz)
Natural freq (Mode 1007) = 82667.54000 (Hz)
Natural freq (Mode 1008) = 82795.73000 (Hz)
Natural freq (Mode 1009) = 82830.25000 (Hz)
Natural freq (Mode 1010) = 82913.56000 (Hz)
Natural freq (Mode 1011) = 83117.39000 (Hz)
Natural freq (Mode 1012) = 83264.48000 (Hz)
Natural freq (Mode 1013) = 83303.87000 (Hz)
Natural freq (Mode 1014) = 83383.77000 (Hz)
Natural freq (Mode 1015) = 83474.57000 (Hz)
Natural freq (Mode 1016) = 83564.55000 (Hz)
Natural freq (Mode 1017) = 83612.36000 (Hz)
Natural freq (Mode 1018) = 83635.59000 (Hz)
Natural freq (Mode 1019) = 83660.44000 (Hz)
Natural freq (Mode 1020) = 83784.58000 (Hz)
Natural freq (Mode 1021) = 83861.33000 (Hz)
Natural freq (Mode 1022) = 83937.67000 (Hz)
Natural freq (Mode 1023) = 84023.90000 (Hz)
Natural freq (Mode 1024) = 84139.57000 (Hz)
Natural freq (Mode 1025) = 84188.86000 (Hz)
Natural freq (Mode 1026) = 84266.69000 (Hz)
Natural freq (Mode 1027) = 84269.75000 (Hz)
Natural freq (Mode 1028) = 84309.34000 (Hz)
Natural freq (Mode 1029) = 84427.03000 (Hz)
Natural freq (Mode 1030) = 84673.20000 (Hz)
Natural freq (Mode 1031) = 84725.60000 (Hz)
Natural freq (Mode 1032) = 84802.77000 (Hz)
Natural freq (Mode 1033) = 84921.77000 (Hz)
Natural freq (Mode 1034) = 84960.34000 (Hz)
Natural freq (Mode 1035) = 85091.32000 (Hz)
Natural freq (Mode 1036) = 85116.43000 (Hz)
Natural freq (Mode 1037) = 85264.96000 (Hz)
Natural freq (Mode 1038) = 85286.54000 (Hz)
Natural freq (Mode 1039) = 85306.32000 (Hz)
Natural freq (Mode 1040) = 85421.91000 (Hz)
Natural freq (Mode 1041) = 85547.09000 (Hz)
Natural freq (Mode 1042) = 85661.92000 (Hz)
Natural freq (Mode 1043) = 85719.86000 (Hz)
Natural freq (Mode 1044) = 85749.15000 (Hz)
Natural freq (Mode 1045) = 85924.99000 (Hz)
Natural freq (Mode 1046) = 86089.57000 (Hz)
Natural freq (Mode 1047) = 86148.53000 (Hz)
Natural freq (Mode 1048) = 86302.17000 (Hz)
Natural freq (Mode 1049) = 86373.30000 (Hz)
Natural freq (Mode 1050) = 86491.27000 (Hz)
Natural freq (Mode 1051) = 86624.46000 (Hz)
Natural freq (Mode 1052) = 86658.50000 (Hz)
Natural freq (Mode 1053) = 86688.69000 (Hz)
Natural freq (Mode 1054) = 86846.44000 (Hz)
Natural freq (Mode 1055) = 86952.64000 (Hz)
Natural freq (Mode 1056) = 87074.96000 (Hz)
Natural freq (Mode 1057) = 87237.35000 (Hz)
Natural freq (Mode 1058) = 87398.33000 (Hz)
Natural freq (Mode 1059) = 87464.73000 (Hz)
Natural freq (Mode 1060) = 87561.27000 (Hz)
Natural freq (Mode 1061) = 87628.88000 (Hz)
Natural freq (Mode 1062) = 87672.54000 (Hz)
Natural freq (Mode 1063) = 87868.90000 (Hz)
Natural freq (Mode 1064) = 87909.61000 (Hz)
Natural freq (Mode 1065) = 87948.39000 (Hz)
Natural freq (Mode 1066) = 88031.61000 (Hz)
Natural freq (Mode 1067) = 88056.46000 (Hz)
Natural freq (Mode 1068) = 88172.09000 (Hz)
Natural freq (Mode 1069) = 88206.87000 (Hz)
Natural freq (Mode 1070) = 88308.04000 (Hz)
Natural freq (Mode 1071) = 88352.02000 (Hz)
Natural freq (Mode 1072) = 88465.10000 (Hz)
Natural freq (Mode 1073) = 88565.23000 (Hz)
Natural freq (Mode 1074) = 88657.34000 (Hz)
Natural freq (Mode 1075) = 88700.26000 (Hz)
Natural freq (Mode 1076) = 88709.47000 (Hz)
Natural freq (Mode 1077) = 88724.85000 (Hz)
Natural freq (Mode 1078) = 88816.78000 (Hz)
Natural freq (Mode 1079) = 88873.34000 (Hz)
Natural freq (Mode 1080) = 89020.17000 (Hz)
Natural freq (Mode 1081) = 89078.82000 (Hz)
Natural freq (Mode 1082) = 89146.32000 (Hz)
Natural freq (Mode 1083) = 89216.51000 (Hz)
Natural freq (Mode 1084) = 89285.04000 (Hz)
Natural freq (Mode 1085) = 89306.96000 (Hz)
Natural freq (Mode 1086) = 89439.18000 (Hz)
Natural freq (Mode 1087) = 89528.18000 (Hz)
Natural freq (Mode 1088) = 89620.32000 (Hz)
Natural freq (Mode 1089) = 89716.06000 (Hz)
Natural freq (Mode 1090) = 89813.61000 (Hz)
Natural freq (Mode 1091) = 89915.21000 (Hz)
Natural freq (Mode 1092) = 89957.09000 (Hz)
Natural freq (Mode 1093) = 90076.36000 (Hz)
Natural freq (Mode 1094) = 90217.64000 (Hz)
Natural freq (Mode 1095) = 90281.78000 (Hz)
Natural freq (Mode 1096) = 90337.50000 (Hz)
Natural freq (Mode 1097) = 90383.03000 (Hz)
Natural freq (Mode 1098) = 90467.45000 (Hz)
Natural freq (Mode 1099) = 90504.77000 (Hz)
Natural freq (Mode 1100) = 90625.35000 (Hz)
Natural freq (Mode 1101) = 90713.12000 (Hz)
Natural freq (Mode 1102) = 90740.85000 (Hz)
Natural freq (Mode 1103) = 90752.30000 (Hz)
Natural freq (Mode 1104) = 90845.66000 (Hz)
Natural freq (Mode 1105) = 90901.66000 (Hz)
Natural freq (Mode 1106) = 91071.76000 (Hz)
Natural freq (Mode 1107) = 91110.43000 (Hz)
Natural freq (Mode 1108) = 91256.23000 (Hz)
Natural freq (Mode 1109) = 91418.58000 (Hz)
Natural freq (Mode 1110) = 91547.07000 (Hz)
Natural freq (Mode 1111) = 91607.19000 (Hz)
Natural freq (Mode 1112) = 91650.98000 (Hz)
Natural freq (Mode 1113) = 91713.15000 (Hz)
Natural freq (Mode 1114) = 91833.30000 (Hz)
Natural freq (Mode 1115) = 91977.28000 (Hz)
Natural freq (Mode 1116) = 92097.01000 (Hz)
Natural freq (Mode 1117) = 92197.90000 (Hz)
Natural freq (Mode 1118) = 92227.72000 (Hz)
Natural freq (Mode 1119) = 92254.49000 (Hz)
Natural freq (Mode 1120) = 92434.76000 (Hz)
Natural freq (Mode 1121) = 92530.93000 (Hz)
Natural freq (Mode 1122) = 92547.32000 (Hz)
Natural freq (Mode 1123) = 92617.38000 (Hz)
Natural freq (Mode 1124) = 92860.10000 (Hz)
Natural freq (Mode 1125) = 92989.60000 (Hz)
Natural freq (Mode 1126) = 93070.57000 (Hz)
Natural freq (Mode 1127) = 93135.01000 (Hz)
Natural freq (Mode 1128) = 93268.29000 (Hz)
Natural freq (Mode 1129) = 93358.34000 (Hz)
Natural freq (Mode 1130) = 93369.00000 (Hz)
Natural freq (Mode 1131) = 93384.06000 (Hz)
Natural freq (Mode 1132) = 93491.51000 (Hz)
Natural freq (Mode 1133) = 93537.09000 (Hz)
Natural freq (Mode 1134) = 93562.33000 (Hz)
Natural freq (Mode 1135) = 93754.73000 (Hz)
Natural freq (Mode 1136) = 93814.21000 (Hz)
Natural freq (Mode 1137) = 93871.80000 (Hz)
Natural freq (Mode 1138) = 93938.57000 (Hz)
Natural freq (Mode 1139) = 94024.20000 (Hz)
Natural freq (Mode 1140) = 94128.21000 (Hz)
Natural freq (Mode 1141) = 94232.26000 (Hz)
Natural freq (Mode 1142) = 94351.51000 (Hz)
Natural freq (Mode 1143) = 94409.17000 (Hz)
Natural freq (Mode 1144) = 94558.20000 (Hz)
Natural freq (Mode 1145) = 94631.15000 (Hz)
Natural freq (Mode 1146) = 94732.62000 (Hz)
Natural freq (Mode 1147) = 94826.06000 (Hz)
Natural freq (Mode 1148) = 94976.99000 (Hz)
Natural freq (Mode 1149) = 95048.56000 (Hz)
Natural freq (Mode 1150) = 95181.86000 (Hz)
Natural freq (Mode 1151) = 95192.30000 (Hz)
Natural freq (Mode 1152) = 95297.16000 (Hz)
Natural freq (Mode 1153) = 95436.33000 (Hz)
Natural freq (Mode 1154) = 95618.01000 (Hz)
Natural freq (Mode 1155) = 95702.23000 (Hz)
Natural freq (Mode 1156) = 95750.83000 (Hz)
Natural freq (Mode 1157) = 95867.23000 (Hz)
Natural freq (Mode 1158) = 95962.79000 (Hz)
Natural freq (Mode 1159) = 96041.91000 (Hz)
Natural freq (Mode 1160) = 96091.17000 (Hz)
Natural freq (Mode 1161) = 96284.30000 (Hz)
Natural freq (Mode 1162) = 96348.77000 (Hz)
Natural freq (Mode 1163) = 96411.30000 (Hz)
Natural freq (Mode 1164) = 96457.12000 (Hz)
Natural freq (Mode 1165) = 96570.81000 (Hz)
Natural freq (Mode 1166) = 96623.90000 (Hz)
Natural freq (Mode 1167) = 96696.38000 (Hz)
Natural freq (Mode 1168) = 96737.32000 (Hz)
Natural freq (Mode 1169) = 96846.65000 (Hz)
Natural freq (Mode 1170) = 97008.36000 (Hz)
Natural freq (Mode 1171) = 97119.42000 (Hz)
Natural freq (Mode 1172) = 97233.69000 (Hz)
Natural freq (Mode 1173) = 97270.07000 (Hz)
Natural freq (Mode 1174) = 97447.92000 (Hz)
Natural freq (Mode 1175) = 97506.07000 (Hz)
Natural freq (Mode 1176) = 97594.28000 (Hz)
Natural freq (Mode 1177) = 97805.04000 (Hz)
Natural freq (Mode 1178) = 97894.72000 (Hz)
Natural freq (Mode 1179) = 97928.87000 (Hz)
Natural freq (Mode 1180) = 97981.40000 (Hz)
Natural freq (Mode 1181) = 98086.96000 (Hz)
Natural freq (Mode 1182) = 98117.62000 (Hz)
Natural freq (Mode 1183) = 98245.71000 (Hz)
Natural freq (Mode 1184) = 98360.74000 (Hz)
Natural freq (Mode 1185) = 98519.72000 (Hz)
Natural freq (Mode 1186) = 98691.42000 (Hz)
Natural freq (Mode 1187) = 98754.68000 (Hz)
Natural freq (Mode 1188) = 98877.99000 (Hz)
Natural freq (Mode 1189) = 98986.09000 (Hz)
Natural freq (Mode 1190) = 99067.69000 (Hz)
Natural freq (Mode 1191) = 99222.21000 (Hz)
Natural freq (Mode 1192) = 99324.10000 (Hz)
Natural freq (Mode 1193) = 99363.49000 (Hz)
Natural freq (Mode 1194) = 99552.85000 (Hz)
Natural freq (Mode 1195) = 99565.86000 (Hz)
Natural freq (Mode 1196) = 99651.71000 (Hz)
Natural freq (Mode 1197) = 99914.16000 (Hz)
Natural freq (Mode 1198) = 99997.05000 (Hz)
Natural freq (Mode 1199) = 100086.10000 (Hz)
Natural freq (Mode 1200) = 100112.50000 (Hz)
Natural freq (Mode 1201) = 100320.50000 (Hz)
Natural freq (Mode 1202) = 100334.10000 (Hz)
Natural freq (Mode 1203) = 100410.10000 (Hz)
Natural freq (Mode 1204) = 100520.60000 (Hz)
Natural freq (Mode 1205) = 100611.10000 (Hz)
Natural freq (Mode 1206) = 100756.50000 (Hz)
Natural freq (Mode 1207) = 100857.90000 (Hz)
Natural freq (Mode 1208) = 100906.60000 (Hz)
Natural freq (Mode 1209) = 101024.70000 (Hz)
Natural freq (Mode 1210) = 101217.30000 (Hz)
Natural freq (Mode 1211) = 101378.20000 (Hz)
Natural freq (Mode 1212) = 101425.90000 (Hz)
Natural freq (Mode 1213) = 101568.40000 (Hz)
Natural freq (Mode 1214) = 101649.20000 (Hz)
Natural freq (Mode 1215) = 101854.50000 (Hz)
Natural freq (Mode 1216) = 101859.60000 (Hz)
Natural freq (Mode 1217) = 102032.30000 (Hz)
Natural freq (Mode 1218) = 102118.70000 (Hz)
Natural freq (Mode 1219) = 102163.20000 (Hz)
Natural freq (Mode 1220) = 102309.80000 (Hz)
Natural freq (Mode 1221) = 102376.90000 (Hz)
Natural freq (Mode 1222) = 102475.10000 (Hz)
Natural freq (Mode 1223) = 102587.10000 (Hz)
Natural freq (Mode 1224) = 102626.40000 (Hz)
Natural freq (Mode 1225) = 102808.10000 (Hz)
Natural freq (Mode 1226) = 102999.10000 (Hz)
Natural freq (Mode 1227) = 103055.40000 (Hz)
Natural freq (Mode 1228) = 103153.30000 (Hz)
Natural freq (Mode 1229) = 103210.50000 (Hz)
Natural freq (Mode 1230) = 103389.80000 (Hz)
Natural freq (Mode 1231) = 103567.90000 (Hz)
Natural freq (Mode 1232) = 103741.10000 (Hz)
Natural freq (Mode 1233) = 103800.40000 (Hz)
Natural freq (Mode 1234) = 103844.10000 (Hz)
Natural freq (Mode 1235) = 103957.40000 (Hz)
Natural freq (Mode 1236) = 104142.80000 (Hz)
Natural freq (Mode 1237) = 104186.80000 (Hz)
Natural freq (Mode 1238) = 104368.90000 (Hz)
Natural freq (Mode 1239) = 104521.90000 (Hz)
Natural freq (Mode 1240) = 104605.60000 (Hz)
Natural freq (Mode 1241) = 104640.40000 (Hz)
Natural freq (Mode 1242) = 104752.90000 (Hz)
Natural freq (Mode 1243) = 104877.60000 (Hz)
Natural freq (Mode 1244) = 104974.20000 (Hz)
Natural freq (Mode 1245) = 105069.10000 (Hz)
Natural freq (Mode 1246) = 105261.70000 (Hz)
Natural freq (Mode 1247) = 105316.40000 (Hz)
Natural freq (Mode 1248) = 105535.40000 (Hz)
Natural freq (Mode 1249) = 105616.20000 (Hz)
Natural freq (Mode 1250) = 105792.20000 (Hz)
Natural freq (Mode 1251) = 105817.40000 (Hz)
Natural freq (Mode 1252) = 105974.60000 (Hz)
Natural freq (Mode 1253) = 106104.30000 (Hz)
Natural freq (Mode 1254) = 106143.00000 (Hz)
Natural freq (Mode 1255) = 106291.00000 (Hz)
Natural freq (Mode 1256) = 106393.00000 (Hz)
Natural freq (Mode 1257) = 106517.20000 (Hz)
Natural freq (Mode 1258) = 106601.60000 (Hz)
Natural freq (Mode 1259) = 106776.20000 (Hz)
Natural freq (Mode 1260) = 106847.60000 (Hz)
Natural freq (Mode 1261) = 106928.10000 (Hz)
Natural freq (Mode 1262) = 107010.40000 (Hz)
Natural freq (Mode 1263) = 107146.40000 (Hz)
Natural freq (Mode 1264) = 107311.10000 (Hz)
Natural freq (Mode 1265) = 107361.80000 (Hz)
Natural freq (Mode 1266) = 107415.20000 (Hz)
Natural freq (Mode 1267) = 107609.10000 (Hz)
Natural freq (Mode 1268) = 107719.30000 (Hz)
Natural freq (Mode 1269) = 108001.00000 (Hz)
Natural freq (Mode 1270) = 108061.80000 (Hz)
Natural freq (Mode 1271) = 108076.50000 (Hz)
Natural freq (Mode 1272) = 108252.70000 (Hz)
Natural freq (Mode 1273) = 108325.20000 (Hz)
Natural freq (Mode 1274) = 108375.60000 (Hz)
Natural freq (Mode 1275) = 108506.50000 (Hz)
Natural freq (Mode 1276) = 108549.10000 (Hz)
Natural freq (Mode 1277) = 108709.70000 (Hz)
Natural freq (Mode 1278) = 108776.70000 (Hz)
Natural freq (Mode 1279) = 108840.10000 (Hz)
Natural freq (Mode 1280) = 109176.60000 (Hz)
Natural freq (Mode 1281) = 109253.60000 (Hz)
Natural freq (Mode 1282) = 109305.80000 (Hz)
Natural freq (Mode 1283) = 109383.00000 (Hz)
Natural freq (Mode 1284) = 109470.60000 (Hz)
Natural freq (Mode 1285) = 109580.90000 (Hz)
Natural freq (Mode 1286) = 109637.50000 (Hz)
Natural freq (Mode 1287) = 109903.10000 (Hz)
Natural freq (Mode 1288) = 109941.40000 (Hz)
Natural freq (Mode 1289) = 109970.10000 (Hz)
Natural freq (Mode 1290) = 110176.20000 (Hz)
Natural freq (Mode 1291) = 110262.20000 (Hz)
Natural freq (Mode 1292) = 110397.60000 (Hz)
Natural freq (Mode 1293) = 110469.50000 (Hz)
Natural freq (Mode 1294) = 110498.80000 (Hz)
Natural freq (Mode 1295) = 110660.80000 (Hz)
Natural freq (Mode 1296) = 110709.90000 (Hz)
Natural freq (Mode 1297) = 110855.40000 (Hz)
Natural freq (Mode 1298) = 111003.50000 (Hz)
Natural freq (Mode 1299) = 111108.40000 (Hz)
Natural freq (Mode 1300) = 111239.20000 (Hz)
Natural freq (Mode 1301) = 111263.50000 (Hz)
Natural freq (Mode 1302) = 111446.80000 (Hz)
Natural freq (Mode 1303) = 111644.50000 (Hz)
Natural freq (Mode 1304) = 111765.20000 (Hz)
Natural freq (Mode 1305) = 111843.10000 (Hz)
Natural freq (Mode 1306) = 111987.60000 (Hz)
Natural freq (Mode 1307) = 112035.40000 (Hz)
Natural freq (Mode 1308) = 112128.30000 (Hz)
Natural freq (Mode 1309) = 112392.30000 (Hz)
Natural freq (Mode 1310) = 112433.70000 (Hz)
Natural freq (Mode 1311) = 112461.80000 (Hz)
Natural freq (Mode 1312) = 112598.60000 (Hz)
Natural freq (Mode 1313) = 112674.70000 (Hz)
Natural freq (Mode 1314) = 112785.90000 (Hz)
Natural freq (Mode 1315) = 112877.40000 (Hz)
Natural freq (Mode 1316) = 112951.70000 (Hz)
Natural freq (Mode 1317) = 113078.10000 (Hz)
Natural freq (Mode 1318) = 113182.60000 (Hz)
Natural freq (Mode 1319) = 113251.80000 (Hz)
Natural freq (Mode 1320) = 113572.60000 (Hz)
Natural freq (Mode 1321) = 113614.80000 (Hz)
Natural freq (Mode 1322) = 113655.60000 (Hz)
Natural freq (Mode 1323) = 114032.30000 (Hz)
Natural freq (Mode 1324) = 114186.80000 (Hz)
Natural freq (Mode 1325) = 114294.00000 (Hz)
Natural freq (Mode 1326) = 114354.20000 (Hz)
Natural freq (Mode 1327) = 114521.20000 (Hz)
Natural freq (Mode 1328) = 114551.30000 (Hz)
Natural freq (Mode 1329) = 114600.10000 (Hz)
Natural freq (Mode 1330) = 114716.60000 (Hz)
Natural freq (Mode 1331) = 114808.50000 (Hz)
Natural freq (Mode 1332) = 114961.50000 (Hz)
Natural freq (Mode 1333) = 115052.60000 (Hz)
Natural freq (Mode 1334) = 115156.20000 (Hz)
Natural freq (Mode 1335) = 115377.20000 (Hz)
Natural freq (Mode 1336) = 115484.80000 (Hz)
Natural freq (Mode 1337) = 115597.90000 (Hz)
Natural freq (Mode 1338) = 115718.90000 (Hz)
Natural freq (Mode 1339) = 115960.20000 (Hz)
Natural freq (Mode 1340) = 116114.10000 (Hz)
Natural freq (Mode 1341) = 116243.00000 (Hz)
Natural freq (Mode 1342) = 116262.40000 (Hz)
Natural freq (Mode 1343) = 116413.40000 (Hz)
Natural freq (Mode 1344) = 116477.70000 (Hz)
Natural freq (Mode 1345) = 116555.20000 (Hz)
Natural freq (Mode 1346) = 116672.70000 (Hz)
Natural freq (Mode 1347) = 116713.00000 (Hz)
Natural freq (Mode 1348) = 116874.30000 (Hz)
Natural freq (Mode 1349) = 117031.80000 (Hz)
Natural freq (Mode 1350) = 117183.70000 (Hz)
Natural freq (Mode 1351) = 117264.80000 (Hz)
Natural freq (Mode 1352) = 117412.80000 (Hz)
Natural freq (Mode 1353) = 117527.50000 (Hz)
Natural freq (Mode 1354) = 117697.90000 (Hz)
Natural freq (Mode 1355) = 117771.70000 (Hz)
Natural freq (Mode 1356) = 117868.10000 (Hz)
Natural freq (Mode 1357) = 117969.50000 (Hz)
Natural freq (Mode 1358) = 118129.50000 (Hz)
Natural freq (Mode 1359) = 118302.40000 (Hz)
Natural freq (Mode 1360) = 118370.90000 (Hz)
Natural freq (Mode 1361) = 118419.00000 (Hz)
Natural freq (Mode 1362) = 118571.50000 (Hz)
Natural freq (Mode 1363) = 118877.20000 (Hz)
Natural freq (Mode 1364) = 118947.70000 (Hz)
Natural freq (Mode 1365) = 118997.70000 (Hz)
Natural freq (Mode 1366) = 119126.20000 (Hz)
Natural freq (Mode 1367) = 119270.50000 (Hz)
Natural freq (Mode 1368) = 119406.20000 (Hz)
Natural freq (Mode 1369) = 119511.30000 (Hz)
Natural freq (Mode 1370) = 119574.30000 (Hz)
Natural freq (Mode 1371) = 119781.00000 (Hz)
Natural freq (Mode 1372) = 119933.60000 (Hz)
Natural freq (Mode 1373) = 120145.60000 (Hz)
Natural freq (Mode 1374) = 120190.00000 (Hz)
Natural freq (Mode 1375) = 120321.80000 (Hz)
Natural freq (Mode 1376) = 120353.10000 (Hz)
Natural freq (Mode 1377) = 120597.80000 (Hz)
Natural freq (Mode 1378) = 120644.50000 (Hz)
Natural freq (Mode 1379) = 120725.60000 (Hz)
Natural freq (Mode 1380) = 120837.90000 (Hz)
Natural freq (Mode 1381) = 120870.10000 (Hz)
Natural freq (Mode 1382) = 121080.50000 (Hz)
Natural freq (Mode 1383) = 121177.30000 (Hz)
Natural freq (Mode 1384) = 121278.30000 (Hz)
Natural freq (Mode 1385) = 121504.70000 (Hz)
Natural freq (Mode 1386) = 121567.70000 (Hz)
Natural freq (Mode 1387) = 121628.50000 (Hz)
Natural freq (Mode 1388) = 121743.40000 (Hz)
Natural freq (Mode 1389) = 121787.00000 (Hz)
Natural freq (Mode 1390) = 122020.70000 (Hz)
Natural freq (Mode 1391) = 122085.30000 (Hz)
Natural freq (Mode 1392) = 122227.70000 (Hz)
Natural freq (Mode 1393) = 122430.00000 (Hz)
Natural freq (Mode 1394) = 122517.90000 (Hz)
Natural freq (Mode 1395) = 122566.40000 (Hz)
Natural freq (Mode 1396) = 122794.80000 (Hz)
Natural freq (Mode 1397) = 122905.20000 (Hz)
Natural freq (Mode 1398) = 123064.90000 (Hz)
Natural freq (Mode 1399) = 123171.70000 (Hz)
Natural freq (Mode 1400) = 123264.40000 (Hz)
Natural freq (Mode 1401) = 123359.30000 (Hz)
Natural freq (Mode 1402) = 123494.90000 (Hz)
Natural freq (Mode 1403) = 123758.80000 (Hz)
Natural freq (Mode 1404) = 123897.70000 (Hz)
Natural freq (Mode 1405) = 124106.20000 (Hz)
Natural freq (Mode 1406) = 124163.70000 (Hz)
Natural freq (Mode 1407) = 124297.60000 (Hz)
Natural freq (Mode 1408) = 124377.30000 (Hz)
Natural freq (Mode 1409) = 124544.60000 (Hz)
Natural freq (Mode 1410) = 124658.30000 (Hz)
Natural freq (Mode 1411) = 124674.60000 (Hz)
Natural freq (Mode 1412) = 124969.70000 (Hz)
Natural freq (Mode 1413) = 125010.20000 (Hz)
Natural freq (Mode 1414) = 125106.50000 (Hz)
Natural freq (Mode 1415) = 125287.30000 (Hz)
Natural freq (Mode 1416) = 125364.30000 (Hz)
Natural freq (Mode 1417) = 125496.00000 (Hz)
Natural freq (Mode 1418) = 125668.20000 (Hz)
Natural freq (Mode 1419) = 125806.90000 (Hz)
Natural freq (Mode 1420) = 125859.20000 (Hz)
Natural freq (Mode 1421) = 126124.10000 (Hz)
Natural freq (Mode 1422) = 126336.10000 (Hz)
Natural freq (Mode 1423) = 126512.70000 (Hz)
Natural freq (Mode 1424) = 126539.10000 (Hz)
Natural freq (Mode 1425) = 126620.50000 (Hz)
Natural freq (Mode 1426) = 126877.60000 (Hz)
Natural freq (Mode 1427) = 126962.30000 (Hz)
Natural freq (Mode 1428) = 127132.20000 (Hz)
Natural freq (Mode 1429) = 127254.70000 (Hz)
Natural freq (Mode 1430) = 127477.10000 (Hz)
Natural freq (Mode 1431) = 127659.30000 (Hz)
Natural freq (Mode 1432) = 127893.90000 (Hz)
Natural freq (Mode 1433) = 127957.60000 (Hz)
Natural freq (Mode 1434) = 128099.20000 (Hz)
Natural freq (Mode 1435) = 128180.30000 (Hz)
Natural freq (Mode 1436) = 128320.40000 (Hz)
Natural freq (Mode 1437) = 128363.50000 (Hz)
Natural freq (Mode 1438) = 128546.60000 (Hz)
Natural freq (Mode 1439) = 128764.90000 (Hz)
Natural freq (Mode 1440) = 128804.00000 (Hz)
Natural freq (Mode 1441) = 128925.30000 (Hz)
Natural freq (Mode 1442) = 128959.00000 (Hz)
Natural freq (Mode 1443) = 128969.90000 (Hz)
Natural freq (Mode 1444) = 129220.00000 (Hz)
Natural freq (Mode 1445) = 129323.20000 (Hz)
Natural freq (Mode 1446) = 129474.70000 (Hz)
Natural freq (Mode 1447) = 129675.90000 (Hz)
Natural freq (Mode 1448) = 129703.10000 (Hz)
Natural freq (Mode 1449) = 130113.10000 (Hz)
Natural freq (Mode 1450) = 130185.80000 (Hz)
Natural freq (Mode 1451) = 130348.10000 (Hz)
Natural freq (Mode 1452) = 130578.30000 (Hz)
Natural freq (Mode 1453) = 130708.50000 (Hz)
Natural freq (Mode 1454) = 130869.20000 (Hz)
Natural freq (Mode 1455) = 130922.50000 (Hz)
Natural freq (Mode 1456) = 131020.90000 (Hz)
Natural freq (Mode 1457) = 131122.90000 (Hz)
Natural freq (Mode 1458) = 131424.50000 (Hz)
Natural freq (Mode 1459) = 131584.80000 (Hz)
Natural freq (Mode 1460) = 131684.30000 (Hz)
Natural freq (Mode 1461) = 131809.90000 (Hz)
Natural freq (Mode 1462) = 131858.60000 (Hz)
Natural freq (Mode 1463) = 131958.50000 (Hz)
Natural freq (Mode 1464) = 132233.70000 (Hz)
Natural freq (Mode 1465) = 132449.40000 (Hz)
Natural freq (Mode 1466) = 132607.40000 (Hz)
Natural freq (Mode 1467) = 132729.70000 (Hz)
Natural freq (Mode 1468) = 132880.40000 (Hz)
Natural freq (Mode 1469) = 133046.80000 (Hz)
Natural freq (Mode 1470) = 133201.30000 (Hz)
Natural freq (Mode 1471) = 133234.10000 (Hz)
Natural freq (Mode 1472) = 133629.50000 (Hz)
Natural freq (Mode 1473) = 133796.90000 (Hz)
Natural freq (Mode 1474) = 133948.40000 (Hz)
Natural freq (Mode 1475) = 134006.30000 (Hz)
Natural freq (Mode 1476) = 134324.40000 (Hz)
Natural freq (Mode 1477) = 134507.70000 (Hz)
Natural freq (Mode 1478) = 134620.10000 (Hz)
Natural freq (Mode 1479) = 134837.70000 (Hz)
Natural freq (Mode 1480) = 134916.50000 (Hz)
Natural freq (Mode 1481) = 135097.00000 (Hz)
Natural freq (Mode 1482) = 135137.40000 (Hz)
Natural freq (Mode 1483) = 135476.30000 (Hz)
Natural freq (Mode 1484) = 135553.40000 (Hz)
Natural freq (Mode 1485) = 135680.90000 (Hz)
Natural freq (Mode 1486) = 135723.70000 (Hz)
Natural freq (Mode 1487) = 136137.20000 (Hz)
Natural freq (Mode 1488) = 136254.00000 (Hz)
Natural freq (Mode 1489) = 136531.70000 (Hz)
Natural freq (Mode 1490) = 136629.60000 (Hz)
Natural freq (Mode 1491) = 136739.30000 (Hz)
Natural freq (Mode 1492) = 136927.00000 (Hz)
Natural freq (Mode 1493) = 136989.70000 (Hz)
Natural freq (Mode 1494) = 137183.70000 (Hz)
Natural freq (Mode 1495) = 137230.00000 (Hz)
Natural freq (Mode 1496) = 137313.30000 (Hz)
Natural freq (Mode 1497) = 137520.90000 (Hz)
Natural freq (Mode 1498) = 137639.00000 (Hz)
Natural freq (Mode 1499) = 138090.60000 (Hz)
Natural freq (Mode 1500) = 138387.40000 (Hz)
Natural freq (Mode 1501) = 138465.10000 (Hz)
Natural freq (Mode 1502) = 138815.80000 (Hz)
Natural freq (Mode 1503) = 138915.10000 (Hz)
Natural freq (Mode 1504) = 138942.60000 (Hz)
Natural freq (Mode 1505) = 139174.70000 (Hz)
Natural freq (Mode 1506) = 139199.90000 (Hz)
Natural freq (Mode 1507) = 139357.90000 (Hz)
Natural freq (Mode 1508) = 139425.70000 (Hz)
Natural freq (Mode 1509) = 139577.30000 (Hz)
Natural freq (Mode 1510) = 139690.00000 (Hz)
Natural freq (Mode 1511) = 139888.50000 (Hz)
Natural freq (Mode 1512) = 140098.70000 (Hz)
Natural freq (Mode 1513) = 140249.80000 (Hz)
Natural freq (Mode 1514) = 140367.30000 (Hz)
Natural freq (Mode 1515) = 140657.00000 (Hz)
Natural freq (Mode 1516) = 140786.00000 (Hz)
Natural freq (Mode 1517) = 141026.50000 (Hz)
Natural freq (Mode 1518) = 141186.20000 (Hz)
Natural freq (Mode 1519) = 141405.70000 (Hz)
Natural freq (Mode 1520) = 141619.60000 (Hz)
Natural freq (Mode 1521) = 141793.30000 (Hz)
Natural freq (Mode 1522) = 142003.20000 (Hz)
Natural freq (Mode 1523) = 142060.70000 (Hz)
Natural freq (Mode 1524) = 142212.40000 (Hz)
Natural freq (Mode 1525) = 142235.00000 (Hz)
Natural freq (Mode 1526) = 142422.80000 (Hz)
Natural freq (Mode 1527) = 142663.20000 (Hz)
Natural freq (Mode 1528) = 143052.20000 (Hz)
Natural freq (Mode 1529) = 143084.90000 (Hz)
Natural freq (Mode 1530) = 143132.30000 (Hz)
Natural freq (Mode 1531) = 143274.40000 (Hz)
Natural freq (Mode 1532) = 143396.20000 (Hz)
Natural freq (Mode 1533) = 143756.70000 (Hz)
Natural freq (Mode 1534) = 143943.30000 (Hz)
Natural freq (Mode 1535) = 144127.80000 (Hz)
Natural freq (Mode 1536) = 144235.40000 (Hz)
Natural freq (Mode 1537) = 144542.10000 (Hz)
Natural freq (Mode 1538) = 144662.30000 (Hz)
Natural freq (Mode 1539) = 144690.70000 (Hz)
Natural freq (Mode 1540) = 144771.30000 (Hz)
Natural freq (Mode 1541) = 145039.90000 (Hz)
Natural freq (Mode 1542) = 145151.10000 (Hz)
Natural freq (Mode 1543) = 145284.10000 (Hz)
Natural freq (Mode 1544) = 145642.50000 (Hz)
Natural freq (Mode 1545) = 146249.40000 (Hz)
Natural freq (Mode 1546) = 146402.00000 (Hz)
Natural freq (Mode 1547) = 146685.30000 (Hz)
Natural freq (Mode 1548) = 146725.90000 (Hz)
Natural freq (Mode 1549) = 146784.20000 (Hz)
Natural freq (Mode 1550) = 146916.60000 (Hz)
Natural freq (Mode 1551) = 147213.30000 (Hz)
Natural freq (Mode 1552) = 147379.50000 (Hz)
Natural freq (Mode 1553) = 147702.80000 (Hz)
Natural freq (Mode 1554) = 148135.00000 (Hz)
Natural freq (Mode 1555) = 148211.80000 (Hz)
Natural freq (Mode 1556) = 148385.40000 (Hz)
Natural freq (Mode 1557) = 148579.80000 (Hz)
Natural freq (Mode 1558) = 148840.20000 (Hz)
Natural freq (Mode 1559) = 148989.20000 (Hz)
Natural freq (Mode 1560) = 149117.70000 (Hz)
Natural freq (Mode 1561) = 149384.50000 (Hz)
Natural freq (Mode 1562) = 149901.10000 (Hz)
Natural freq (Mode 1563) = 150012.00000 (Hz)
Natural freq (Mode 1564) = 150026.60000 (Hz)
Natural freq (Mode 1565) = 150123.80000 (Hz)
Natural freq (Mode 1566) = 150212.80000 (Hz)
Natural freq (Mode 1567) = 150535.40000 (Hz)
Natural freq (Mode 1568) = 150791.90000 (Hz)
Natural freq (Mode 1569) = 151291.00000 (Hz)
Natural freq (Mode 1570) = 151469.60000 (Hz)
Natural freq (Mode 1571) = 151604.60000 (Hz)
Natural freq (Mode 1572) = 151672.40000 (Hz)
Natural freq (Mode 1573) = 151822.30000 (Hz)
Natural freq (Mode 1574) = 152226.20000 (Hz)
Natural freq (Mode 1575) = 152338.60000 (Hz)
Natural freq (Mode 1576) = 152687.80000 (Hz)
Natural freq (Mode 1577) = 152820.80000 (Hz)
Natural freq (Mode 1578) = 153515.50000 (Hz)
Natural freq (Mode 1579) = 153649.70000 (Hz)
Natural freq (Mode 1580) = 153716.80000 (Hz)
Natural freq (Mode 1581) = 154080.40000 (Hz)
Natural freq (Mode 1582) = 154227.00000 (Hz)
Natural freq (Mode 1583) = 154281.30000 (Hz)
Natural freq (Mode 1584) = 154350.30000 (Hz)
Natural freq (Mode 1585) = 154510.10000 (Hz)
Natural freq (Mode 1586) = 154829.60000 (Hz)
Natural freq (Mode 1587) = 155355.80000 (Hz)
Natural freq (Mode 1588) = 155436.70000 (Hz)
Natural freq (Mode 1589) = 155641.50000 (Hz)
Natural freq (Mode 1590) = 155881.40000 (Hz)
Natural freq (Mode 1591) = 155898.70000 (Hz)
Natural freq (Mode 1592) = 156045.80000 (Hz)
Natural freq (Mode 1593) = 156632.20000 (Hz)
Natural freq (Mode 1594) = 156715.70000 (Hz)
Natural freq (Mode 1595) = 156944.30000 (Hz)
Natural freq (Mode 1596) = 156959.70000 (Hz)
Natural freq (Mode 1597) = 157074.30000 (Hz)
Natural freq (Mode 1598) = 157281.40000 (Hz)
Natural freq (Mode 1599) = 157509.00000 (Hz)
Natural freq (Mode 1600) = 157672.90000 (Hz)
Natural freq (Mode 1601) = 157765.50000 (Hz)
Natural freq (Mode 1602) = 157847.60000 (Hz)
Natural freq (Mode 1603) = 157987.50000 (Hz)
Natural freq (Mode 1604) = 158062.80000 (Hz)
Natural freq (Mode 1605) = 158390.60000 (Hz)
Natural freq (Mode 1606) = 158600.10000 (Hz)
Natural freq (Mode 1607) = 158957.10000 (Hz)
Natural freq (Mode 1608) = 159008.80000 (Hz)
Natural freq (Mode 1609) = 159347.70000 (Hz)
Natural freq (Mode 1610) = 159448.00000 (Hz)
Natural freq (Mode 1611) = 160017.90000 (Hz)
Natural freq (Mode 1612) = 160125.80000 (Hz)
Natural freq (Mode 1613) = 160197.70000 (Hz)
Natural freq (Mode 1614) = 160403.10000 (Hz)
Natural freq (Mode 1615) = 160624.50000 (Hz)
Natural freq (Mode 1616) = 160755.70000 (Hz)
Natural freq (Mode 1617) = 160803.50000 (Hz)
Natural freq (Mode 1618) = 160976.60000 (Hz)
Natural freq (Mode 1619) = 161448.10000 (Hz)
Natural freq (Mode 1620) = 161586.90000 (Hz)
Natural freq (Mode 1621) = 161815.20000 (Hz)
Natural freq (Mode 1622) = 161986.90000 (Hz)
Natural freq (Mode 1623) = 162466.80000 (Hz)
Natural freq (Mode 1624) = 162566.50000 (Hz)
Natural freq (Mode 1625) = 162608.40000 (Hz)
Natural freq (Mode 1626) = 162717.60000 (Hz)
Natural freq (Mode 1627) = 162844.00000 (Hz)
Natural freq (Mode 1628) = 163278.60000 (Hz)
Natural freq (Mode 1629) = 163309.40000 (Hz)
Natural freq (Mode 1630) = 163964.70000 (Hz)
Natural freq (Mode 1631) = 164005.10000 (Hz)
Natural freq (Mode 1632) = 164261.60000 (Hz)
Natural freq (Mode 1633) = 164326.10000 (Hz)
Natural freq (Mode 1634) = 164590.90000 (Hz)
Natural freq (Mode 1635) = 164656.90000 (Hz)
Natural freq (Mode 1636) = 165096.90000 (Hz)
Natural freq (Mode 1637) = 165297.50000 (Hz)
Natural freq (Mode 1638) = 165804.30000 (Hz)
Natural freq (Mode 1639) = 166068.20000 (Hz)
Natural freq (Mode 1640) = 166457.30000 (Hz)
Natural freq (Mode 1641) = 166514.40000 (Hz)
Natural freq (Mode 1642) = 166618.00000 (Hz)
Natural freq (Mode 1643) = 167181.10000 (Hz)
Natural freq (Mode 1644) = 167769.30000 (Hz)
Natural freq (Mode 1645) = 167803.40000 (Hz)
Natural freq (Mode 1646) = 167887.70000 (Hz)
Natural freq (Mode 1647) = 167937.00000 (Hz)
Natural freq (Mode 1648) = 168171.80000 (Hz)
Natural freq (Mode 1649) = 168637.70000 (Hz)
Natural freq (Mode 1650) = 168827.00000 (Hz)
Natural freq (Mode 1651) = 168918.90000 (Hz)
Natural freq (Mode 1652) = 169013.80000 (Hz)
Natural freq (Mode 1653) = 169143.70000 (Hz)
Natural freq (Mode 1654) = 169595.50000 (Hz)
Natural freq (Mode 1655) = 169874.10000 (Hz)
Natural freq (Mode 1656) = 169886.40000 (Hz)
Natural freq (Mode 1657) = 169891.20000 (Hz)
Natural freq (Mode 1658) = 169934.80000 (Hz)
Natural freq (Mode 1659) = 170188.10000 (Hz)
Natural freq (Mode 1660) = 170651.40000 (Hz)
Natural freq (Mode 1661) = 170659.80000 (Hz)
Natural freq (Mode 1662) = 171236.50000 (Hz)
Natural freq (Mode 1663) = 171387.80000 (Hz)
Natural freq (Mode 1664) = 171667.50000 (Hz)
Natural freq (Mode 1665) = 171785.20000 (Hz)
Natural freq (Mode 1666) = 172104.00000 (Hz)
Natural freq (Mode 1667) = 172379.30000 (Hz)
Natural freq (Mode 1668) = 172531.20000 (Hz)
Natural freq (Mode 1669) = 173061.80000 (Hz)
Natural freq (Mode 1670) = 173218.80000 (Hz)
Natural freq (Mode 1671) = 173992.60000 (Hz)
Natural freq (Mode 1672) = 174199.60000 (Hz)
Natural freq (Mode 1673) = 174311.20000 (Hz)
Natural freq (Mode 1674) = 174609.30000 (Hz)
Natural freq (Mode 1675) = 174851.40000 (Hz)
Natural freq (Mode 1676) = 175088.40000 (Hz)
Natural freq (Mode 1677) = 175104.80000 (Hz)
Natural freq (Mode 1678) = 175240.60000 (Hz)
Natural freq (Mode 1679) = 175725.80000 (Hz)
Natural freq (Mode 1680) = 175958.00000 (Hz)
Natural freq (Mode 1681) = 176785.50000 (Hz)
Natural freq (Mode 1682) = 176887.90000 (Hz)
Natural freq (Mode 1683) = 176960.70000 (Hz)
Natural freq (Mode 1684) = 177004.30000 (Hz)
Natural freq (Mode 1685) = 177410.10000 (Hz)
Natural freq (Mode 1686) = 177613.00000 (Hz)
Natural freq (Mode 1687) = 177999.40000 (Hz)
Natural freq (Mode 1688) = 178203.10000 (Hz)
Natural freq (Mode 1689) = 178443.20000 (Hz)
Natural freq (Mode 1690) = 179265.20000 (Hz)
Natural freq (Mode 1691) = 179577.40000 (Hz)
Natural freq (Mode 1692) = 179735.20000 (Hz)
Natural freq (Mode 1693) = 179903.20000 (Hz)
Natural freq (Mode 1694) = 180130.10000 (Hz)
Natural freq (Mode 1695) = 180359.50000 (Hz)
Natural freq (Mode 1696) = 180434.90000 (Hz)
Natural freq (Mode 1697) = 181385.00000 (Hz)
Natural freq (Mode 1698) = 181992.60000 (Hz)
Natural freq (Mode 1699) = 182050.10000 (Hz)
Natural freq (Mode 1700) = 182062.40000 (Hz)
Natural freq (Mode 1701) = 183019.60000 (Hz)
Natural freq (Mode 1702) = 183208.80000 (Hz)
Natural freq (Mode 1703) = 183609.70000 (Hz)
Natural freq (Mode 1704) = 184158.80000 (Hz)
Natural freq (Mode 1705) = 184251.30000 (Hz)
Natural freq (Mode 1706) = 184789.50000 (Hz)
Natural freq (Mode 1707) = 184832.80000 (Hz)
Natural freq (Mode 1708) = 185132.10000 (Hz)
Natural freq (Mode 1709) = 185327.30000 (Hz)
Natural freq (Mode 1710) = 185472.20000 (Hz)
Natural freq (Mode 1711) = 185901.70000 (Hz)
Natural freq (Mode 1712) = 186622.70000 (Hz)
Natural freq (Mode 1713) = 187198.40000 (Hz)
Natural freq (Mode 1714) = 187443.40000 (Hz)
Natural freq (Mode 1715) = 187507.80000 (Hz)
Natural freq (Mode 1716) = 187872.30000 (Hz)
Natural freq (Mode 1717) = 188187.00000 (Hz)
Natural freq (Mode 1718) = 188741.90000 (Hz)
Natural freq (Mode 1719) = 188959.60000 (Hz)
Natural freq (Mode 1720) = 189275.20000 (Hz)
Natural freq (Mode 1721) = 190410.90000 (Hz)
Natural freq (Mode 1722) = 190828.60000 (Hz)
Natural freq (Mode 1723) = 191294.90000 (Hz)
Natural freq (Mode 1724) = 191352.10000 (Hz)
Natural freq (Mode 1725) = 191490.70000 (Hz)
Natural freq (Mode 1726) = 191801.40000 (Hz)
Natural freq (Mode 1727) = 192067.80000 (Hz)
Natural freq (Mode 1728) = 192128.50000 (Hz)
Natural freq (Mode 1729) = 192910.30000 (Hz)
Natural freq (Mode 1730) = 193493.10000 (Hz)
Natural freq (Mode 1731) = 193667.50000 (Hz)
Natural freq (Mode 1732) = 193707.10000 (Hz)
Natural freq (Mode 1733) = 194562.50000 (Hz)
Natural freq (Mode 1734) = 194671.90000 (Hz)
Natural freq (Mode 1735) = 194895.90000 (Hz)
Natural freq (Mode 1736) = 195986.20000 (Hz)
Natural freq (Mode 1737) = 196046.40000 (Hz)
Natural freq (Mode 1738) = 196164.80000 (Hz)
Natural freq (Mode 1739) = 196916.80000 (Hz)
Natural freq (Mode 1740) = 196945.90000 (Hz)
Natural freq (Mode 1741) = 196963.30000 (Hz)
Natural freq (Mode 1742) = 198742.00000 (Hz)
Natural freq (Mode 1743) = 198832.90000 (Hz)
Natural freq (Mode 1744) = 199305.40000 (Hz)
Natural freq (Mode 1745) = 200294.70000 (Hz)
Natural freq (Mode 1746) = 200419.80000 (Hz)
Natural freq (Mode 1747) = 201244.20000 (Hz)
Natural freq (Mode 1748) = 201284.70000 (Hz)
Natural freq (Mode 1749) = 201362.20000 (Hz)
Natural freq (Mode 1750) = 201875.70000 (Hz)
Natural freq (Mode 1751) = 202090.90000 (Hz)
Natural freq (Mode 1752) = 202691.80000 (Hz)
Natural freq (Mode 1753) = 203016.30000 (Hz)
Natural freq (Mode 1754) = 204512.00000 (Hz)
Natural freq (Mode 1755) = 205046.80000 (Hz)
Natural freq (Mode 1756) = 205539.70000 (Hz)
Natural freq (Mode 1757) = 206255.10000 (Hz)
Natural freq (Mode 1758) = 209931.40000 (Hz)
Natural freq (Mode 1759) = 210310.70000 (Hz)
Natural freq (Mode 1760) = 211454.20000 (Hz)
Natural freq (Mode 1761) = 211898.10000 (Hz)
Natural freq (Mode 1762) = 212483.80000 (Hz)
Natural freq (Mode 1763) = 213805.00000 (Hz)
Natural freq (Mode 1764) = 215284.00000 (Hz)
Natural freq (Mode 1765) = 216529.80000 (Hz)
Natural freq (Mode 1766) = 217898.60000 (Hz)
Natural freq (Mode 1767) = 219200.70000 (Hz)
Natural freq (Mode 1768) = 220852.30000 (Hz)
Natural freq (Mode 1769) = 222877.80000 (Hz)
Natural freq (Mode 1770) = 223804.40000 (Hz)
Natural freq (Mode 1771) = 230522.70000 (Hz)
Natural freq (Mode 1772) = 231395.10000 (Hz)
Natural freq (Mode 1773) = 234055.50000 (Hz)
Natural freq (Mode 1774) = 237433.60000 (Hz)
Natural freq (Mode 1775) = 240144.30000 (Hz)
Natural freq (Mode 1776) = 240535.30000 (Hz)
Natural freq (Mode 1777) = 243767.00000 (Hz)
Natural freq (Mode 1778) = 253575.70000 (Hz)
Natural freq (Mode 1779) = 267124.30000 (Hz)

real	0m0.561s
user	0m0.744s
sys	0m0.126s
+ status=0
+ set +x

=================================================
CAPS verification (using pyCAPS) case nastran_CompositeWingFreq_PyTest.py passed (as expected)
=================================================


=================================================
+ echo 'nastran_Composite_PyTest.py test;'
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESP126/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
nastran_Composite_PyTest.py test;
+ python -u nastran_Composite_PyTest.py -outLevel=0 -noAnalysis
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESP126/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = plate, index = 1
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 0
Getting surface mesh for body 1 (of 1)
Body 1 (of 1)
Number of nodes    = 49
Number of elements = 36
Number of triangle elements      = 0
Number of quadrilateral elements = 36
----------------------------
Total number of nodes    = 49
Total number of elements = 36
Mapping Csys attributes ................
	Number of unique Csys attributes = 1
	Name = plate, index = 1

Getting FEA coordinate systems.......
	Number of coordinate systems - 1
	Coordinate system name - plate
Mapping capsConstraint attributes ................
	Number of unique capsConstraint attributes = 1
	Name = plateEdge, index = 1
Mapping capsLoad attributes ................
	Number of unique capsLoad attributes = 1
	Name = plateTip, index = 1
Mapping capsBound attributes ................
	Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
	Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
	Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
	Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
	Mesh for body = 0
	Number of nodal coordinates = 49
	Number of elements = 36
	Elemental Nodes = 0
	Elemental Rods  = 0
	Elemental Tria3 = 0
	Elemental Quad4 = 36
Aero_Reference value is NULL - No aero reference parameters set

Getting FEA materials.......
	Number of materials - 2
	Material name - Madeupium
	Material name - Unobtainium
	No "materialType" specified for Material tuple Unobtainium, defaulting to "Isotropic"
	Done getting FEA materials

Getting FEA properties.......
	Number of properties - 1
	Property name - plate
	Done getting FEA properties
Updating mesh element types based on properties input

Getting FEA constraints.......
	Number of constraints - 1
	Constraint name - cantilever
	No "constraintType" specified for Constraint tuple cantilever, defaulting to "ZeroDisplacement"
	Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults
Load tuple is NULL - No loads applied
Design_Variable tuple is NULL - No design variables applied
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Mass_Increment tuple is NULL - No mass increments applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied

Getting FEA analyses.......
	Number of analyses - 1
	Analysis name - EigenAnalysis
	No "analysisType" specified for Analysis tuple EigenAnalysis, defaulting to "Modal"
	Done getting FEA analyses

Writing Nastran grid and connectivity file (in large field format) ....
Finished writing Nastran grid file

Writing subElement types (if any) - appending mesh file
	Writing mass increment set

Writing Nastran instruction file....
	Warning: No constraints specified for case EigenAnalysis, assuming all constraints are applied!!!!
	Warning: No loads specified for case EigenAnalysis!!!!
	Writing mass increment cards
	Writing analysis cards, 0
	Writing combined constraint cards
	Writing constraint cards
	Writing material cards
	Writing property cards
	Writing coordinate system cards
	Done writing aeroelastic cards
	Done writing files


Running Nastran......
Done running Nastran!

real	0m0.310s
user	0m0.369s
sys	0m0.121s
+ status=0
+ set +x

=================================================
CAPS verification (using pyCAPS) case nastran_Composite_PyTest.py passed (as expected)
=================================================


=================================================
+ echo 'nastran_Flutter_15degree.py test;'
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESP126/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
nastran_Flutter_15degree.py test;
+ python -u nastran_Flutter_15degree.py -outLevel=0 -noAnalysis
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESP126/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 3
	Name = Edge, index = 1
	Name = Body, index = 2
	Name = Root, index = 3
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 0
Getting surface mesh for body 1 (of 2)
Getting surface mesh for body 2 (of 2)
Body 1 (of 2)
Number of nodes    = 133
Number of elements = 108
Number of triangle elements      = 0
Number of quadrilateral elements = 108
Body 2 (of 2)
Number of nodes    = 1
Number of elements = 0
Number of triangle elements      = 0
Number of quadrilateral elements = 0
----------------------------
Total number of nodes    = 134
Total number of elements = 108
Mapping Csys attributes ................
	Number of unique Csys attributes = 0

Getting FEA coordinate systems.......
	Number of coordinate systems - 0
	No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
	Number of unique capsConstraint attributes = 1
	Name = Root_Point, index = 1
Mapping capsLoad attributes ................
	Number of unique capsLoad attributes = 1
	Name = Root_Point, index = 1
Mapping capsBound attributes ................
	Number of unique capsBound attributes = 1
	Name = WingSurface, index = 1
Mapping capsConnect attributes ................
	Number of unique capsConnect attributes = 1
	Name = Root, index = 1
Mapping capsResponse attributes ................
	Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
	Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 4
	Name = Edge, index = 1
	Name = Body, index = 2
	Name = Root, index = 3
	Name = Wing, index = 4
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 4
	Name = Edge, index = 1
	Name = Body, index = 2
	Name = Root, index = 3
	Name = Wing, index = 4
Setting FEA Data
	Mesh for body = 0
	Number of nodal coordinates = 133
	Number of elements = 108
	Elemental Nodes = 0
	Elemental Rods  = 0
	Elemental Tria3 = 0
	Elemental Quad4 = 108
Setting FEA Data
	Mesh for body = 1
	Number of nodal coordinates = 1
	Number of elements = 1
	Elemental Nodes = 1
	Elemental Rods  = 0
	Elemental Tria3 = 0
	Elemental Quad4 = 0
Combining multiple FEA meshes!
	Combined Number of nodal coordinates = 134
	Combined Number of elements = 109
	Combined Elemental Nodes = 1
	Combined Elemental Rods  = 0
	Combined Elemental Tria3 = 0
	Combined Elemental Quad4 = 108
Getting vortex lattice surface data
	VLM surface name - WingSurface
	Done getting vortex lattice surface data

Getting FEA vortex lattice mesh
	Surface 1: Number of points found for aero-spline = 133
Aero_Reference value is NULL - No aero reference parameters set

Getting FEA materials.......
	Number of materials - 1
	Material name - aluminum
	No "materialType" specified for Material tuple aluminum, defaulting to "Isotropic"
	Done getting FEA materials

Getting FEA properties.......
	Number of properties - 2
	Property name - Body
	Property name - Edge
	Done getting FEA properties
Updating mesh element types based on properties input

Getting FEA constraints.......
	Number of constraints - 1
	Constraint name - PointConstraint
	No "constraintType" specified for Constraint tuple PointConstraint, defaulting to "ZeroDisplacement"
	Done getting FEA constraints
Support tuple is NULL - No supports applied

Getting FEA connections.......
	Number of connection tuples - 1
	Connection name - Root
	No "groupName" specified for Connection tuple Root!
	Looking for automatic connections from the use of capsConnectLink for Root
	7 automatic connections were made for capsConnect Root (node id 134)
	Done getting FEA connections
Load tuple is NULL - No loads applied
Design_Variable tuple is NULL - No design variables applied
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Mass_Increment tuple is NULL - No mass increments applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied

Getting FEA analyses.......
	Number of analyses - 1
	Analysis name - Flutter
	Done getting FEA analyses

Writing Nastran grid and connectivity file (in free field format) ....
Finished writing Nastran grid file

Writing subElement types (if any) - appending mesh file
Writing connection cards - appending mesh file
	Writing mass increment set

Writing Nastran instruction file....
	Warning: No loads specified for case Flutter!!!!
	Writing mass increment cards
	Writing aero card
	Writing analysis cards, 0
	Writing constraint ADD cards
	Writing constraint cards
	Writing material cards
	Writing property cards
	Writing aeroelastic cards
	Done writing aeroelastic cards
	Done writing files


Running Nastran......
Done running Nastran!

real	0m0.301s
user	0m0.371s
sys	0m0.116s
+ status=0
+ set +x

=================================================
CAPS verification (using pyCAPS) case nastran_Flutter_15degree.py passed (as expected)
=================================================


=================================================
+ echo 'nastran_MultiLoadCase_PyTest.py test;'
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESP126/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
nastran_MultiLoadCase_PyTest.py test;
+ python -u nastran_MultiLoadCase_PyTest.py -outLevel=0 -noAnalysis
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESP126/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = plate, index = 1
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 0
Getting surface mesh for body 1 (of 1)
Body 1 (of 1)
Number of nodes    = 49
Number of elements = 36
Number of triangle elements      = 0
Number of quadrilateral elements = 36
----------------------------
Total number of nodes    = 49
Total number of elements = 36
Mapping Csys attributes ................
	Number of unique Csys attributes = 0

Getting FEA coordinate systems.......
	Number of coordinate systems - 0
	No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
	Number of unique capsConstraint attributes = 1
	Name = plateEdge, index = 1
Mapping capsLoad attributes ................
	Number of unique capsLoad attributes = 1
	Name = plate, index = 1
Mapping capsBound attributes ................
	Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
	Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
	Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
	Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
	Mesh for body = 0
	Number of nodal coordinates = 49
	Number of elements = 36
	Elemental Nodes = 0
	Elemental Rods  = 0
	Elemental Tria3 = 0
	Elemental Quad4 = 36
Aero_Reference value is NULL - No aero reference parameters set

Getting FEA materials.......
	Number of materials - 1
	Material name - Madeupium
	Done getting FEA materials

Getting FEA properties.......
	Number of properties - 1
	Property name - plate
	Done getting FEA properties
Updating mesh element types based on properties input

Getting FEA constraints.......
	Number of constraints - 1
	Constraint name - edgeConstraint
	No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement"
	Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults

Getting FEA loads.......
	Number of loads - 5
	Load name - load_0
	Load name - load_1
	Load name - load_2
	Load name - load_3
	Load name - load_4
	Done getting FEA loads
Design_Variable tuple is NULL - No design variables applied
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Mass_Increment tuple is NULL - No mass increments applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied

Getting FEA analyses.......
	Number of analyses - 5
	Analysis name - load_0
	Analysis name - load_1
	Analysis name - load_2
	Analysis name - load_3
	Analysis name - load_4
	Done getting FEA analyses

Writing Nastran grid and connectivity file (in free field format) ....
Finished writing Nastran grid file

Writing subElement types (if any) - appending mesh file
	Writing mass increment set

Writing Nastran instruction file....
	Warning: No constraints specified for case load_0, assuming all constraints are applied!!!!
	Warning: No constraints specified for case load_1, assuming all constraints are applied!!!!
	Warning: No constraints specified for case load_2, assuming all constraints are applied!!!!
	Warning: No constraints specified for case load_3, assuming all constraints are applied!!!!
	Warning: No constraints specified for case load_4, assuming all constraints are applied!!!!
	Writing mass increment cards
	Writing analysis cards, 0
	Writing load ADD cards
	Writing combined constraint cards
	Writing load ADD cards
	Writing combined constraint cards
	Writing load ADD cards
	Writing combined constraint cards
	Writing load ADD cards
	Writing combined constraint cards
	Writing load ADD cards
	Writing combined constraint cards
	Writing load cards
	Writing constraint cards
	Writing material cards
	Writing property cards
	Done writing aeroelastic cards
	Done writing files


Running Nastran......
Done running Nastran!

real	0m0.298s
user	0m0.360s
sys	0m0.120s
+ status=0
+ set +x

=================================================
CAPS verification (using pyCAPS) case nastran_MultiLoadCase_PyTest.py passed (as expected)
=================================================


=================================================
+ echo 'nastran_OptimizationMultiLoad_PyTest.py test;'
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESP126/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
nastran_OptimizationMultiLoad_PyTest.py test;
+ python -u nastran_OptimizationMultiLoad_PyTest.py -outLevel=0 -noAnalysis
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESP126/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = plate, index = 1
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 0
Getting surface mesh for body 1 (of 1)
Body 1 (of 1)
Number of nodes    = 49
Number of elements = 36
Number of triangle elements      = 0
Number of quadrilateral elements = 36
----------------------------
Total number of nodes    = 49
Total number of elements = 36
Mapping Csys attributes ................
	Number of unique Csys attributes = 0

Getting FEA coordinate systems.......
	Number of coordinate systems - 0
	No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
	Number of unique capsConstraint attributes = 1
	Name = plateEdge, index = 1
Mapping capsLoad attributes ................
	Number of unique capsLoad attributes = 1
	Name = plate, index = 1
Mapping capsBound attributes ................
	Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
	Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
	Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
	Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
	Mesh for body = 0
	Number of nodal coordinates = 49
	Number of elements = 36
	Elemental Nodes = 0
	Elemental Rods  = 0
	Elemental Tria3 = 0
	Elemental Quad4 = 36
Aero_Reference value is NULL - No aero reference parameters set

Getting FEA materials.......
	Number of materials - 1
	Material name - Madeupium
	Done getting FEA materials

Getting FEA properties.......
	Number of properties - 1
	Property name - plate
	Done getting FEA properties
Updating mesh element types based on properties input

Getting FEA constraints.......
	Number of constraints - 1
	Constraint name - edgeConstraint
	No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement"
	Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults

Getting FEA loads.......
	Number of loads - 2
	Load name - load_0
	Load name - load_1
	Done getting FEA loads

Getting FEA design variables.......
	Number of design variables          - 2
	Design_Variable name - materialDV
	Design_Variable name - propertyDV
	Design_Variable_Relation name - materialDVR
	Name madeupium not found in attribute map!!!!
	Design_Variable_Relation name - propertyDVR
	Number of design variable relations - 2
	Done getting FEA design variables

Getting FEA design constraints.......
	Number of design constraints - 2
	Design_Constraint name - stress1
	Design_Constraint name - stress2
Done getting FEA design constraints
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Mass_Increment tuple is NULL - No mass increments applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied

Getting FEA analyses.......
	Number of analyses - 2
	Analysis name - load_0
	Analysis name - load_1
	Done getting FEA analyses

Writing Nastran grid and connectivity file (in large field format) ....
Finished writing Nastran grid file

Writing subElement types (if any) - appending mesh file
	Writing mass increment set

Writing Nastran instruction file....
	Warning: No constraints specified for case load_0, assuming all constraints are applied!!!!
	Warning: No constraints specified for case load_1, assuming all constraints are applied!!!!
	Writing mass increment cards
	Writing analysis cards, 0
	Writing load ADD cards
	Writing combined constraint cards
	Writing design constraint ADD cards
	Writing load ADD cards
	Writing combined constraint cards
	Writing design constraint ADD cards
	Writing load cards
	Writing constraint cards
	Writing material cards
	Writing property cards
	Writing design variable cards
	Writing design variable relation cards
	Writing design constraints and responses cards
	Done writing aeroelastic cards
	Done writing files


Running Nastran......
Done running NASTRAN!

real	0m0.303s
user	0m0.365s
sys	0m0.123s
+ status=0
+ set +x

=================================================
CAPS verification (using pyCAPS) case nastran_OptimizationMultiLoad_PyTest.py passed (as expected)
=================================================


=================================================
+ echo 'nastran_PlateMisc_PyTest.py test;'
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESP126/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
nastran_PlateMisc_PyTest.py test;
+ python -u nastran_PlateMisc_PyTest.py -outLevel=0 -noAnalysis
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESP126/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = plate, index = 1
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 0
Getting surface mesh for body 1 (of 1)
Body 1 (of 1)
Number of nodes    = 49
Number of elements = 36
Number of triangle elements      = 0
Number of quadrilateral elements = 36
----------------------------
Total number of nodes    = 49
Total number of elements = 36
Mapping Csys attributes ................
	Number of unique Csys attributes = 0

Getting FEA coordinate systems.......
	Number of coordinate systems - 0
	No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
	Number of unique capsConstraint attributes = 1
	Name = plateEdge, index = 1
Mapping capsLoad attributes ................
	Number of unique capsLoad attributes = 1
	Name = plate, index = 1
Mapping capsBound attributes ................
	Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
	Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
	Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
	Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
	Mesh for body = 0
	Number of nodal coordinates = 49
	Number of elements = 36
	Elemental Nodes = 0
	Elemental Rods  = 0
	Elemental Tria3 = 0
	Elemental Quad4 = 36
Aero_Reference value is NULL - No aero reference parameters set

Getting FEA materials.......
	Number of materials - 1
	Material name - Madeupium
	Done getting FEA materials

Getting FEA properties.......
	Number of properties - 1
	Property name - plate
	Done getting FEA properties
Updating mesh element types based on properties input

Getting FEA constraints.......
	Number of constraints - 1
	Constraint name - edgeConstraint
	No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement"
	Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults

Getting FEA loads.......
	Number of loads - 3
	Load name - moment
	Load name - pressure
	Load name - thermal
	Done getting FEA loads

Getting FEA design variables.......
	Number of design variables          - 1
	Design_Variable name - pltvar
	Number of design variable relations - 0
	Done getting FEA design variables

Getting FEA design constraints.......
	Number of design constraints - 1
	Design_Constraint name - pltcon
Done getting FEA design constraints
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Mass_Increment tuple is NULL - No mass increments applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL

Getting FEA analyses.......
	Number of analyses - 1
	Analysis name - Default
	Done getting FEA analyses

Writing Nastran grid and connectivity file (in free field format) ....
Finished writing Nastran grid file

Writing subElement types (if any) - appending mesh file
	Writing mass increment set

Writing Nastran instruction file....
	Writing mass increment cards
	Writing analysis cards, 0
	Writing load ADD cards
	Writing constraint ADD cards
	Writing design constraint ADD cards
	Writing load cards
	Writing constraint cards
	Writing material cards
	Writing property cards
	Writing design variable cards
	Writing design constraints and responses cards
	Done writing aeroelastic cards
	Done writing files


Running Nastran......
Done running Nastran!

real	0m0.300s
user	0m0.362s
sys	0m0.121s
+ status=0
+ set +x

=================================================
CAPS verification (using pyCAPS) case nastran_PlateMisc_PyTest.py passed (as expected)
=================================================


=================================================
+ echo 'nastran_PyTest.py test;'
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESP126/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
nastran_PyTest.py test;
+ python -u nastran_PyTest.py -outLevel=0 -noAnalysis
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESP126/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = Ribs_and_Spars, index = 1
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 0
Getting surface mesh for body 1 (of 1)
Body 1 (of 1)
Number of nodes    = 2099
Number of elements = 1853
Number of triangle elements      = 0
Number of quadrilateral elements = 1853
----------------------------
Total number of nodes    = 2099
Total number of elements = 1853
Mapping Csys attributes ................
	Number of unique Csys attributes = 0

Getting FEA coordinate systems.......
	Number of coordinate systems - 0
	No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
	Number of unique capsConstraint attributes = 1
	Name = Rib_Constraint, index = 1
Mapping capsLoad attributes ................
	Number of unique capsLoad attributes = 0
Mapping capsBound attributes ................
	Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
	Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
	Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
	Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = Ribs_and_Spars, index = 1
Setting FEA Data
	Mesh for body = 0
	Number of nodal coordinates = 2099
	Number of elements = 1853
	Elemental Nodes = 0
	Elemental Rods  = 0
	Elemental Tria3 = 0
	Elemental Quad4 = 1853
Aero_Reference value is NULL - No aero reference parameters set

Getting FEA materials.......
	Number of materials - 2
	Material name - Madeupium
	Material name - Unobtainium
	No "materialType" specified for Material tuple Unobtainium, defaulting to "Isotropic"
	Done getting FEA materials

Getting FEA properties.......
	Number of properties - 1
	Property name - Ribs_and_Spars
	Done getting FEA properties
Updating mesh element types based on properties input

Getting FEA constraints.......
	Number of constraints - 1
	Constraint name - ribConstraint
	No "constraintType" specified for Constraint tuple ribConstraint, defaulting to "ZeroDisplacement"
	Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults
Load tuple is NULL - No loads applied
Design_Variable tuple is NULL - No design variables applied
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Mass_Increment tuple is NULL - No mass increments applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied

Getting FEA analyses.......
	Number of analyses - 1
	Analysis name - EigenAnalysis
	No "analysisType" specified for Analysis tuple EigenAnalysis, defaulting to "Modal"
	Done getting FEA analyses

Writing Nastran grid and connectivity file (in large field format) ....
Finished writing Nastran grid file

Writing subElement types (if any) - appending mesh file
	Writing mass increment set

Writing Nastran instruction file....
	Warning: No constraints specified for case EigenAnalysis, assuming all constraints are applied!!!!
	Warning: No loads specified for case EigenAnalysis!!!!
	Writing mass increment cards
	Writing analysis cards, 0
	Writing combined constraint cards
	Writing constraint cards
	Writing material cards
	Writing property cards
	Done writing aeroelastic cards
	Done writing files


Running Nastran......
Done running Nastran!

Getting results for natural frequencies.....
Reading Nastran FO6 file - extracting Eigen-Values!
	Number of Eigen-Values = 10
	Loading Eigen-Value = 1
	Loading Eigen-Value = 2
	Loading Eigen-Value = 3
	Loading Eigen-Value = 4
	Loading Eigen-Value = 5
	Loading Eigen-Value = 6
	Loading Eigen-Value = 7
	Loading Eigen-Value = 8
	Loading Eigen-Value = 9
	Loading Eigen-Value = 10
Natural freq (Mode 1) = 0.02165 (Hz)
Natural freq (Mode 2) = 0.02165 (Hz)
Natural freq (Mode 3) = 0.10665 (Hz)
Natural freq (Mode 4) = 0.10665 (Hz)
Natural freq (Mode 5) = 0.13547 (Hz)
Natural freq (Mode 6) = 0.13547 (Hz)
Natural freq (Mode 7) = 0.23092 (Hz)
Natural freq (Mode 8) = 0.23092 (Hz)
Natural freq (Mode 9) = 0.27609 (Hz)
Natural freq (Mode 10) = 0.27609 (Hz)

real	0m3.130s
user	0m4.624s
sys	0m6.303s
+ status=0
+ set +x

=================================================
CAPS verification (using pyCAPS) case nastran_PyTest.py passed (as expected)
=================================================


=================================================
+ echo 'nastran_SingleLoadCase_PyTest.py test;'
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESP126/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
nastran_SingleLoadCase_PyTest.py test;
+ python -u nastran_SingleLoadCase_PyTest.py -outLevel=0 -noAnalysis
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESP126/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = plate, index = 1
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 0
Getting surface mesh for body 1 (of 1)
Body 1 (of 1)
Number of nodes    = 25
Number of elements = 16
Number of triangle elements      = 0
Number of quadrilateral elements = 16
----------------------------
Total number of nodes    = 25
Total number of elements = 16
Mapping Csys attributes ................
	Number of unique Csys attributes = 0

Getting FEA coordinate systems.......
	Number of coordinate systems - 0
	No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
	Number of unique capsConstraint attributes = 1
	Name = plateEdge, index = 1
Mapping capsLoad attributes ................
	Number of unique capsLoad attributes = 1
	Name = plate, index = 1
Mapping capsBound attributes ................
	Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
	Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
	Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
	Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
	Mesh for body = 0
	Number of nodal coordinates = 25
	Number of elements = 16
	Elemental Nodes = 0
	Elemental Rods  = 0
	Elemental Tria3 = 0
	Elemental Quad4 = 16
Aero_Reference value is NULL - No aero reference parameters set

Getting FEA materials.......
	Number of materials - 1
	Material name - Madeupium
	Done getting FEA materials

Getting FEA properties.......
	Number of properties - 1
	Property name - plate
	Done getting FEA properties
Updating mesh element types based on properties input

Getting FEA constraints.......
	Number of constraints - 1
	Constraint name - edgeConstraint
	No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement"
	Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults

Getting FEA loads.......
	Number of loads - 1
	Load name - appliedPressure
	Done getting FEA loads
Design_Variable tuple is NULL - No design variables applied
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Mass_Increment tuple is NULL - No mass increments applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL

Getting FEA analyses.......
	Number of analyses - 1
	Analysis name - Default
	Done getting FEA analyses

Writing Nastran grid and connectivity file (in free field format) ....
Finished writing Nastran grid file

Writing subElement types (if any) - appending mesh file
	Writing mass increment set

Writing Nastran instruction file....
	Writing mass increment cards
	Writing analysis cards, 0
	Writing load ADD cards
	Writing constraint ADD cards
	Writing load cards
	Writing constraint cards
	Writing material cards
	Writing property cards
	Done writing aeroelastic cards
	Done writing files


Running Nastran......
Done running Nastran!

real	0m0.298s
user	0m0.360s
sys	0m0.121s
+ status=0
+ set +x

=================================================
CAPS verification (using pyCAPS) case nastran_SingleLoadCase_PyTest.py passed (as expected)
=================================================


=================================================
+ echo 'nastran_ThreeBarDesign_PyTest.py test;'
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESP126/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
nastran_ThreeBarDesign_PyTest.py test;
+ python -u nastran_ThreeBarDesign_PyTest.py -outLevel=0 -noAnalysis
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESP126/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
WARNING:: WireBody is non-manifold
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 3
	Name = bar1, index = 1
	Name = bar2, index = 2
	Name = bar3, index = 3
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 0
Getting surface mesh for body 1 (of 1)
Body 1 (of 1)
Number of nodes    = 4
Number of elements = 0
Number of triangle elements      = 0
Number of quadrilateral elements = 0
----------------------------
Total number of nodes    = 4
Total number of elements = 0
Mapping Csys attributes ................
	Number of unique Csys attributes = 0

Getting FEA coordinate systems.......
	Number of coordinate systems - 0
	No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
	Number of unique capsConstraint attributes = 1
	Name = boundary, index = 1
Mapping capsLoad attributes ................
	Number of unique capsLoad attributes = 1
	Name = force, index = 1
Mapping capsBound attributes ................
	Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
	Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
	Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
	Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 3
	Name = bar1, index = 1
	Name = bar2, index = 2
	Name = bar3, index = 3
	capsIgnore attribute found for edge - 3!!
capsIgnore attribute found. Removing unneeded nodes and elements from mesh!
Removing unused nodes...
	Removed 0 (out of 4) unused nodes!
Setting FEA Data
	Mesh for body = 0
	Number of nodal coordinates = 4
	Number of elements = 3
	Elemental Nodes = 0
	Elemental Rods  = 3
	Elemental Tria3 = 0
	Elemental Quad4 = 0
Aero_Reference value is NULL - No aero reference parameters set

Getting FEA materials.......
	Number of materials - 1
	Material name - Madeupium
	Done getting FEA materials

Getting FEA properties.......
	Number of properties - 3
	Property name - bar1
	Property name - bar2
	Property name - bar3
	Done getting FEA properties
Updating mesh element types based on properties input

Getting FEA constraints.......
	Number of constraints - 1
	Constraint name - BoundaryCondition
	No "constraintType" specified for Constraint tuple BoundaryCondition, defaulting to "ZeroDisplacement"
	Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults

Getting FEA loads.......
	Number of loads - 1
	Load name - appliedForce
	Done getting FEA loads

Getting FEA design variables.......
	Number of design variables          - 3
	Design_Variable name - Bar1A
	Design_Variable name - Bar2A
	Design_Variable name - Bar3A
	Design_Variable_Relation name - Bar1A
	Design_Variable_Relation name - Bar2A
	Design_Variable_Relation name - Bar3A
	Number of design variable relations - 3
	Done getting FEA design variables

Getting FEA design constraints.......
	Number of design constraints - 3
	Design_Constraint name - stress1
	Design_Constraint name - stress2
	Design_Constraint name - stress3
Done getting FEA design constraints
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Mass_Increment tuple is NULL - No mass increments applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied

Getting FEA analyses.......
	Number of analyses - 1
	Analysis name - SingleLoadCase
	Done getting FEA analyses

Writing Nastran grid and connectivity file (in large field format) ....
Finished writing Nastran grid file

Writing subElement types (if any) - appending mesh file
	Writing mass increment set

Writing Nastran instruction file....
	Writing mass increment cards
	Writing analysis cards, 0
	Writing load ADD cards
	Writing constraint ADD cards
	Writing design constraint ADD cards
	Writing load cards
	Writing constraint cards
	Writing material cards
	Writing property cards
	Writing design variable cards
	Writing design variable relation cards
	Writing design constraints and responses cards
	Done writing aeroelastic cards
	Done writing files


Running Nastran......
Done running Nastran!

real	0m0.302s
user	0m0.364s
sys	0m0.124s
+ status=0
+ set +x

=================================================
CAPS verification (using pyCAPS) case nastran_ThreeBarDesign_PyTest.py passed (as expected)
=================================================


=================================================
+ echo 'nastran_ThreeBarFreq_PyTest.py test;'
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESP126/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
nastran_ThreeBarFreq_PyTest.py test;
+ python -u nastran_ThreeBarFreq_PyTest.py -outLevel=0 -noAnalysis
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESP126/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
WARNING:: WireBody is non-manifold
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 3
	Name = bar1, index = 1
	Name = bar2, index = 2
	Name = bar3, index = 3
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 0
Getting surface mesh for body 1 (of 1)
Body 1 (of 1)
Number of nodes    = 4
Number of elements = 0
Number of triangle elements      = 0
Number of quadrilateral elements = 0
----------------------------
Total number of nodes    = 4
Total number of elements = 0
Mapping Csys attributes ................
	Number of unique Csys attributes = 0

Getting FEA coordinate systems.......
	Number of coordinate systems - 0
	No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
	Number of unique capsConstraint attributes = 1
	Name = boundary, index = 1
Mapping capsLoad attributes ................
	Number of unique capsLoad attributes = 1
	Name = force, index = 1
Mapping capsBound attributes ................
	Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
	Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
	Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
	Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 3
	Name = bar1, index = 1
	Name = bar2, index = 2
	Name = bar3, index = 3
	capsIgnore attribute found for edge - 3!!
capsIgnore attribute found. Removing unneeded nodes and elements from mesh!
Removing unused nodes...
	Removed 0 (out of 4) unused nodes!
Setting FEA Data
	Mesh for body = 0
	Number of nodal coordinates = 4
	Number of elements = 3
	Elemental Nodes = 0
	Elemental Rods  = 3
	Elemental Tria3 = 0
	Elemental Quad4 = 0
Aero_Reference value is NULL - No aero reference parameters set

Getting FEA materials.......
	Number of materials - 1
	Material name - Madeupium
	Done getting FEA materials

Getting FEA properties.......
	Number of properties - 3
	Property name - bar1
	Property name - bar2
	Property name - bar3
	Done getting FEA properties
Updating mesh element types based on properties input

Getting FEA constraints.......
	Number of constraints - 1
	Constraint name - BoundaryCondition
	No "constraintType" specified for Constraint tuple BoundaryCondition, defaulting to "ZeroDisplacement"
	Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults
Load tuple is NULL - No loads applied
Design_Variable tuple is NULL - No design variables applied
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Mass_Increment tuple is NULL - No mass increments applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied

Getting FEA analyses.......
	Number of analyses - 1
	Analysis name - EigenAnalysis
	No "analysisType" specified for Analysis tuple EigenAnalysis, defaulting to "Modal"
	Done getting FEA analyses

Writing Nastran grid and connectivity file (in large field format) ....
Finished writing Nastran grid file

Writing subElement types (if any) - appending mesh file
	Writing mass increment set

Writing Nastran instruction file....
	Warning: No constraints specified for case EigenAnalysis, assuming all constraints are applied!!!!
	Warning: No loads specified for case EigenAnalysis!!!!
	Writing mass increment cards
	Writing analysis cards, 0
	Writing combined constraint cards
	Writing constraint cards
	Writing material cards
	Writing property cards
	Done writing aeroelastic cards
	Done writing files


Running Nastran......
Done running Nastran!

real	0m0.301s
user	0m0.362s
sys	0m0.123s
+ status=0
+ set +x

=================================================
CAPS verification (using pyCAPS) case nastran_ThreeBarFreq_PyTest.py passed (as expected)
=================================================


=================================================
+ echo 'nastran_ThreeBarLinkDesign_PyTest.py test;'
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESP126/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
nastran_ThreeBarLinkDesign_PyTest.py test;
+ python -u nastran_ThreeBarLinkDesign_PyTest.py -outLevel=0 -noAnalysis
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESP126/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
WARNING:: WireBody is non-manifold
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 3
	Name = bar1, index = 1
	Name = bar2, index = 2
	Name = bar3, index = 3
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 0
Getting surface mesh for body 1 (of 1)
Body 1 (of 1)
Number of nodes    = 4
Number of elements = 0
Number of triangle elements      = 0
Number of quadrilateral elements = 0
----------------------------
Total number of nodes    = 4
Total number of elements = 0
Mapping Csys attributes ................
	Number of unique Csys attributes = 0

Getting FEA coordinate systems.......
	Number of coordinate systems - 0
	No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
	Number of unique capsConstraint attributes = 1
	Name = boundary, index = 1
Mapping capsLoad attributes ................
	Number of unique capsLoad attributes = 1
	Name = force, index = 1
Mapping capsBound attributes ................
	Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
	Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
	Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
	Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 3
	Name = bar1, index = 1
	Name = bar2, index = 2
	Name = bar3, index = 3
	capsIgnore attribute found for edge - 3!!
capsIgnore attribute found. Removing unneeded nodes and elements from mesh!
Removing unused nodes...
	Removed 0 (out of 4) unused nodes!
Setting FEA Data
	Mesh for body = 0
	Number of nodal coordinates = 4
	Number of elements = 3
	Elemental Nodes = 0
	Elemental Rods  = 3
	Elemental Tria3 = 0
	Elemental Quad4 = 0
Aero_Reference value is NULL - No aero reference parameters set

Getting FEA materials.......
	Number of materials - 1
	Material name - Madeupium
	Done getting FEA materials

Getting FEA properties.......
	Number of properties - 3
	Property name - bar1
	Property name - bar2
	Property name - bar3
	Done getting FEA properties
Updating mesh element types based on properties input

Getting FEA constraints.......
	Number of constraints - 1
	Constraint name - BoundaryCondition
	No "constraintType" specified for Constraint tuple BoundaryCondition, defaulting to "ZeroDisplacement"
	Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults

Getting FEA loads.......
	Number of loads - 1
	Load name - appliedForce
	Done getting FEA loads

Getting FEA design variables.......
	Number of design variables          - 3
	Design_Variable name - Bar1A
	Design_Variable name - Bar2A
	Design_Variable name - Bar3A
	Design_Variable_Relation name - Bar1A
	Design_Variable_Relation name - Bar2A
	Design_Variable_Relation name - Bar3A
	Number of design variable relations - 3
	Done getting FEA design variables

Getting FEA design constraints.......
	Number of design constraints - 3
	Design_Constraint name - stress1
	Design_Constraint name - stress2
	Design_Constraint name - stress3
Done getting FEA design constraints
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Mass_Increment tuple is NULL - No mass increments applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied

Getting FEA analyses.......
	Number of analyses - 1
	Analysis name - SingleLoadCase
	Done getting FEA analyses

Writing Nastran grid and connectivity file (in large field format) ....
Finished writing Nastran grid file

Writing subElement types (if any) - appending mesh file
	Writing mass increment set

Writing Nastran instruction file....
	Writing mass increment cards
	Writing analysis cards, 0
	Writing load ADD cards
	Writing constraint ADD cards
	Writing design constraint ADD cards
	Writing load cards
	Writing constraint cards
	Writing material cards
	Writing property cards
	Writing design variable cards
	Writing design variable relation cards
	Writing design constraints and responses cards
	Done writing aeroelastic cards
	Done writing files


Running Nastran......
Done running Nastran!

real	0m0.303s
user	0m0.365s
sys	0m0.125s
+ status=0
+ set +x

=================================================
CAPS verification (using pyCAPS) case nastran_ThreeBarLinkDesign_PyTest.py passed (as expected)
=================================================


=================================================
+ echo 'nastran_ThreeBarMultiLoad_PyTest.py test;'
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESP126/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
nastran_ThreeBarMultiLoad_PyTest.py test;
+ python -u nastran_ThreeBarMultiLoad_PyTest.py -outLevel=0 -noAnalysis
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESP126/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
WARNING:: WireBody is non-manifold
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 3
	Name = bar1, index = 1
	Name = bar2, index = 2
	Name = bar3, index = 3
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 0
Getting surface mesh for body 1 (of 1)
Body 1 (of 1)
Number of nodes    = 4
Number of elements = 0
Number of triangle elements      = 0
Number of quadrilateral elements = 0
----------------------------
Total number of nodes    = 4
Total number of elements = 0
Mapping Csys attributes ................
	Number of unique Csys attributes = 0

Getting FEA coordinate systems.......
	Number of coordinate systems - 0
	No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
	Number of unique capsConstraint attributes = 1
	Name = boundary, index = 1
Mapping capsLoad attributes ................
	Number of unique capsLoad attributes = 1
	Name = force, index = 1
Mapping capsBound attributes ................
	Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
	Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
	Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
	Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 3
	Name = bar1, index = 1
	Name = bar2, index = 2
	Name = bar3, index = 3
	capsIgnore attribute found for edge - 3!!
capsIgnore attribute found. Removing unneeded nodes and elements from mesh!
Removing unused nodes...
	Removed 0 (out of 4) unused nodes!
Setting FEA Data
	Mesh for body = 0
	Number of nodal coordinates = 4
	Number of elements = 3
	Elemental Nodes = 0
	Elemental Rods  = 3
	Elemental Tria3 = 0
	Elemental Quad4 = 0
Aero_Reference value is NULL - No aero reference parameters set

Getting FEA materials.......
	Number of materials - 1
	Material name - Madeupium
	Done getting FEA materials

Getting FEA properties.......
	Number of properties - 3
	Property name - bar1
	Property name - bar2
	Property name - bar3
	Done getting FEA properties
Updating mesh element types based on properties input

Getting FEA constraints.......
	Number of constraints - 2
	Constraint name - conOne
	No "constraintType" specified for Constraint tuple conOne, defaulting to "ZeroDisplacement"
	Constraint name - conTwo
	No "constraintType" specified for Constraint tuple conTwo, defaulting to "ZeroDisplacement"
	Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults

Getting FEA loads.......
	Number of loads - 2
	Load name - loadOne
	Load name - loadTwo
	Done getting FEA loads
Design_Variable tuple is NULL - No design variables applied
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Mass_Increment tuple is NULL - No mass increments applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied

Getting FEA analyses.......
	Number of analyses - 2
	Analysis name - caseOne
	Analysis name - caseTwo
	Done getting FEA analyses

Writing Nastran grid and connectivity file (in large field format) ....
Finished writing Nastran grid file

Writing subElement types (if any) - appending mesh file
	Writing mass increment set

Writing Nastran instruction file....
	Writing mass increment cards
	Writing analysis cards, 0
	Writing load ADD cards
	Writing constraint ADD cards
	Writing load ADD cards
	Writing constraint ADD cards
	Writing load cards
	Writing constraint cards
	Writing material cards
	Writing property cards
	Done writing aeroelastic cards
	Done writing files


Running Nastran......
Done running Nastran!

real	0m0.308s
user	0m0.366s
sys	0m0.124s
+ status=0
+ set +x

=================================================
CAPS verification (using pyCAPS) case nastran_ThreeBarMultiLoad_PyTest.py passed (as expected)
=================================================


=================================================
+ echo 'nastran_ThreeBar_PyTest.py test;'
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESP126/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
nastran_ThreeBar_PyTest.py test;
+ python -u nastran_ThreeBar_PyTest.py -outLevel=0 -noAnalysis
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESP126/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
WARNING:: WireBody is non-manifold
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 3
	Name = bar1, index = 1
	Name = bar2, index = 2
	Name = bar3, index = 3
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 0
Getting surface mesh for body 1 (of 1)
Body 1 (of 1)
Number of nodes    = 4
Number of elements = 0
Number of triangle elements      = 0
Number of quadrilateral elements = 0
----------------------------
Total number of nodes    = 4
Total number of elements = 0
Mapping Csys attributes ................
	Number of unique Csys attributes = 0

Getting FEA coordinate systems.......
	Number of coordinate systems - 0
	No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
	Number of unique capsConstraint attributes = 1
	Name = boundary, index = 1
Mapping capsLoad attributes ................
	Number of unique capsLoad attributes = 1
	Name = force, index = 1
Mapping capsBound attributes ................
	Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
	Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
	Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
	Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 3
	Name = bar1, index = 1
	Name = bar2, index = 2
	Name = bar3, index = 3
	capsIgnore attribute found for edge - 3!!
capsIgnore attribute found. Removing unneeded nodes and elements from mesh!
Removing unused nodes...
	Removed 0 (out of 4) unused nodes!
Setting FEA Data
	Mesh for body = 0
	Number of nodal coordinates = 4
	Number of elements = 3
	Elemental Nodes = 0
	Elemental Rods  = 3
	Elemental Tria3 = 0
	Elemental Quad4 = 0
Aero_Reference value is NULL - No aero reference parameters set

Getting FEA materials.......
	Number of materials - 1
	Material name - Madeupium
	Done getting FEA materials

Getting FEA properties.......
	Number of properties - 3
	Property name - bar1
	Property name - bar2
	Property name - bar3
	Done getting FEA properties
Updating mesh element types based on properties input

Getting FEA constraints.......
	Number of constraints - 1
	Constraint name - BoundaryCondition
	No "constraintType" specified for Constraint tuple BoundaryCondition, defaulting to "ZeroDisplacement"
	Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults

Getting FEA loads.......
	Number of loads - 1
	Load name - appliedForce
	Done getting FEA loads
Design_Variable tuple is NULL - No design variables applied
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Mass_Increment tuple is NULL - No mass increments applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied

Getting FEA analyses.......
	Number of analyses - 1
	Analysis name - SingleLoadCase
	Done getting FEA analyses

Writing Nastran grid and connectivity file (in large field format) ....
Finished writing Nastran grid file

Writing subElement types (if any) - appending mesh file
	Writing mass increment set

Writing Nastran instruction file....
	Writing mass increment cards
	Writing analysis cards, 0
	Writing load ADD cards
	Writing constraint ADD cards
	Writing load cards
	Writing constraint cards
	Writing material cards
	Writing property cards
	Done writing aeroelastic cards
	Done writing files


Running Nastran......
Done running Nastran!

real	0m0.301s
user	0m0.363s
sys	0m0.123s
+ status=0
+ set +x

=================================================
CAPS verification (using pyCAPS) case nastran_ThreeBar_PyTest.py passed (as expected)
=================================================


=================================================
+ echo 'nastran_Trim_15degree.py test;'
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESP126/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
nastran_Trim_15degree.py test;
+ python -u nastran_Trim_15degree.py -outLevel=0 -noAnalysis
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESP126/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 3
	Name = Edge, index = 1
	Name = Body, index = 2
	Name = Root, index = 3
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 0
Getting surface mesh for body 1 (of 2)
Getting surface mesh for body 2 (of 2)
Body 1 (of 2)
Number of nodes    = 117
Number of elements = 96
Number of triangle elements      = 0
Number of quadrilateral elements = 96
Body 2 (of 2)
Number of nodes    = 1
Number of elements = 0
Number of triangle elements      = 0
Number of quadrilateral elements = 0
----------------------------
Total number of nodes    = 118
Total number of elements = 96
Mapping Csys attributes ................
	Number of unique Csys attributes = 0

Getting FEA coordinate systems.......
	Number of coordinate systems - 0
	No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
	Number of unique capsConstraint attributes = 1
	Name = Root_Point, index = 1
Mapping capsLoad attributes ................
	Number of unique capsLoad attributes = 1
	Name = Root_Point, index = 1
Mapping capsBound attributes ................
	Number of unique capsBound attributes = 1
	Name = WingSurface, index = 1
Mapping capsConnect attributes ................
	Number of unique capsConnect attributes = 1
	Name = Root, index = 1
Mapping capsResponse attributes ................
	Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
	Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 4
	Name = Edge, index = 1
	Name = Body, index = 2
	Name = Root, index = 3
	Name = Wing, index = 4
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 4
	Name = Edge, index = 1
	Name = Body, index = 2
	Name = Root, index = 3
	Name = Wing, index = 4
Setting FEA Data
	Mesh for body = 0
	Number of nodal coordinates = 117
	Number of elements = 96
	Elemental Nodes = 0
	Elemental Rods  = 0
	Elemental Tria3 = 0
	Elemental Quad4 = 96
Setting FEA Data
	Mesh for body = 1
	Number of nodal coordinates = 1
	Number of elements = 1
	Elemental Nodes = 1
	Elemental Rods  = 0
	Elemental Tria3 = 0
	Elemental Quad4 = 0
Combining multiple FEA meshes!
	Combined Number of nodal coordinates = 118
	Combined Number of elements = 97
	Combined Elemental Nodes = 1
	Combined Elemental Rods  = 0
	Combined Elemental Tria3 = 0
	Combined Elemental Quad4 = 96
Getting vortex lattice surface data
	VLM surface name - WingSurface
	Done getting vortex lattice surface data

Getting FEA vortex lattice mesh
	Surface 1: Number of points found for aero-spline = 117
Aero_Reference value is NULL - No aero reference parameters set

Getting FEA materials.......
	Number of materials - 1
	Material name - aluminum
	No "materialType" specified for Material tuple aluminum, defaulting to "Isotropic"
	Done getting FEA materials

Getting FEA properties.......
	Number of properties - 3
	Property name - Body
	Property name - Edge
	Property name - Root
	Done getting FEA properties
Updating mesh element types based on properties input

Getting FEA constraints.......
	Number of constraints - 1
	Constraint name - PointConstraint
	No "constraintType" specified for Constraint tuple PointConstraint, defaulting to "ZeroDisplacement"
	Done getting FEA constraints

Getting FEA supports.......
	Number of supports - 1
	Support name - PointSupport
	Done getting FEA supports

Getting FEA connections.......
	Number of connection tuples - 1
	Connection name - Root
	No "groupName" specified for Connection tuple Root!
	Looking for automatic connections from the use of capsConnectLink for Root
	9 automatic connections were made for capsConnect Root (node id 118)
	Done getting FEA connections

Getting FEA loads.......
	Number of loads - 2
	Load name - GravityLoad
	No "groupName" specified for Load tuple GravityLoad, going to use load name
	Load name - PointLoad
	Done getting FEA loads
Design_Variable tuple is NULL - No design variables applied
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Mass_Increment tuple is NULL - No mass increments applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied

Getting FEA analyses.......
	Number of analyses - 1
	Analysis name - Trim
	Done getting FEA analyses

Writing Nastran grid and connectivity file (in free field format) ....
Finished writing Nastran grid file

Writing subElement types (if any) - appending mesh file
Writing connection cards - appending mesh file
	Writing mass increment set

Writing Nastran instruction file....
	Warning: No loads specified for case Trim, assuming all loads are applied!!!!
	Writing mass increment cards
	Writing aeros card
	Writing aestat cards
	Writing analysis cards, 0
	Writing load ADD cards
	Writing constraint ADD cards
	Writing load cards
	Writing constraint cards
	Writing support cards
	Writing material cards
	Writing property cards
	Writing aeroelastic cards
	Done writing aeroelastic cards
	Done writing files


Running Nastran......
Done running Nastran!

real	0m0.299s
user	0m0.369s
sys	0m0.114s
+ status=0
+ set +x

=================================================
CAPS verification (using pyCAPS) case nastran_Trim_15degree.py passed (as expected)
=================================================

Running.... AEROELASTIC PyTests


=================================================
+ echo 'aeroelasticSimple_Pressure_SU2_and_Astros.py test;'
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESP126/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
aeroelasticSimple_Pressure_SU2_and_Astros.py test;
+ python -u aeroelasticSimple_Pressure_SU2_and_Astros.py -outLevel=0 -noPlotData
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESP126/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt

Running PreAnalysis ...... su2
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 3
	Name = Farfield, index = 1
	Name = SymmPlane, index = 2
	Name = Skin, index = 3
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 0
 
AFLR2    : ---------------------------------------
AFLR2    : AFLR2 LIBRARY
AFLR2    : ADVANCING-FRONT/LOCAL-RECONNECTION
AFLR2    : TRIA/QUAD GRID GENERATOR
AFLR2    : Version Number 9.18.1
AFLR2    : Version Date   06/11/24 @ 05:52PM
AFLR2    : Compile OS     Darwin 23.5.0 arm64
AFLR2    : Compile Date   06/11/24 @ 05:52PM
AFLR2    : Copyright 1994-2021, D.L. Marcum
AFLR2    : ---------------------------------------
 
AFLR4    : ---------------------------------------
AFLR4    : AFLR4 LIBRARY
AFLR4    : ADVANCING-FRONT/LOCAL-RECONNECTION
AFLR4    : TRIA/QUAD SURFACE GRID GENERATOR
AFLR4    : Version Number 11.5.15
AFLR4    : Version Date   07/19/24 @ 07:04PM
AFLR4    : Compile OS     Darwin 23.5.0 arm64
AFLR4    : Compile Date   07/19/24 @ 07:06PM
AFLR4    : Copyright 1994-2021, D.L. Marcum
AFLR4    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.8.1
EGADS    : ---------------------------------------

EGADS    : EGADS CAD Geometry Setup

EGADS    : Model has 1 Active Bodies

EGADS    : Body 0 is a SolidBody
EGADS    : Body 0 has 1 Shells
EGADS    : Body 0 has 9 Faces
EGADS    : Body 0 has 18 Edges
EGADS    : Body 0 has 10 Loops
EGADS    : Body 0 has 12 Nodes

EGADS    : Check Grid BCs

EGADS    : Grid BCs are OK

EGADS    : Face Neighbor-Faces Information

EGADS    : QC  = Face Quad Combination Flag
EGADS    : IER = Face Isolated Edge Refinement Flag
EGADS    : ER  = Face Edge Refinement Factor
EGADS    :       Not applicable for Faces with a FarField Grid BC.
EGADS    : SF  = Face Scale Factor
EGADS    :       Not applicable for Faces with a FarField Grid BC.

EGADS    :   Face          Body    QC   IER       ER    Scale   Neighbor
EGADS    :     ID  Active    ID  Flag  Flag   Weight   Factor   Faces
EGADS    :      1     Yes     0     0     1        0        1   2 3 4 5
EGADS    :      2     Yes     0     0     1        0        1   1 3 5 6
EGADS    :      3     Yes     0     0     1        0        1   1 2 4 6 7 8
EGADS    :      4     Yes     0     0     1        0        1   1 3 5 6
EGADS    :      5     Yes     0     0     1        0        1   1 2 4 6
EGADS    :      6     Yes     0     0     1        0        1   2 3 4 5
EGADS    :      7     Yes     0     0     1        0        1   3 8 9
EGADS    :      8     Yes     0     0     1        0        1   3 7 9
EGADS    :      9     Yes     0     0     1        0        1   7 8

EGADS    : Face Edges Information

EGADS    :   Face   Edges
EGADS    :      1   1 2 -3 -4
EGADS    :      2   5 6 -7 -1
EGADS    :      3   -2 7 9 -8 -10 -11
EGADS    :      4   -12 3 8 -13
EGADS    :      5   4 12 -14 -5
EGADS    :      6   -6 14 13 -9
EGADS    :      7   15 10 -17 -16
EGADS    :      8   17 11 -15 -18
EGADS    :      9   16 18

EGADS    : Face Loops Information

EGADS    :   Face   Loops
EGADS    :      1   1
EGADS    :      2   2
EGADS    :      3   3 4
EGADS    :      4   5
EGADS    :      5   6
EGADS    :      6   7
EGADS    :      7   8
EGADS    :      8   9
EGADS    :      9   10

EGADS    : Loop Edges Information

EGADS    :   Loop  Active   Edges
EGADS    :      1     Yes   1 2 -3 -4
EGADS    :      2     Yes   5 6 -7 -1
EGADS    :      3     Yes   -2 7 9 -8
EGADS    :      4     Yes   -10 -11
EGADS    :      5     Yes   -12 3 8 -13
EGADS    :      6     Yes   4 12 -14 -5
EGADS    :      7     Yes   -6 14 13 -9
EGADS    :      8     Yes   15 10 -17 -16
EGADS    :      9     Yes   17 11 -15 -18
EGADS    :     10     Yes   16 18

EGADS    : Edge Node, Scale Factor, and Neighbor-Faces Information

EGADS    : ESF = Edge Scale Factor
EGADS    :       Not applicable for DEGENERATE Edges or Edges with a FarField
EGADS    :       Grid BC Neighbor Face.

EGADS    :                                             Neighbor
EGADS    :   Edge  Body  Active Node1 Node2      ESF   Faces
EGADS    :      1     0     Yes     2     1        1   1 2
EGADS    :      2     0     Yes     1     3        1   1 3
EGADS    :      3     0     Yes     4     3        1   1 4
EGADS    :      4     0     Yes     2     4        1   1 5
EGADS    :      5     0     Yes     2     5        1   2 5
EGADS    :      6     0     Yes     5     6        1   2 6
EGADS    :      7     0     Yes     1     6        1   2 3
EGADS    :      8     0     Yes     3     7        1   3 4
EGADS    :      9     0     Yes     6     7        1   3 6
EGADS    :     10     0     Yes     8     9        1   3 7
EGADS    :     11     0     Yes     9     8        1   3 8
EGADS    :     12     0     Yes     4    10        1   4 5
EGADS    :     13     0     Yes    10     7        1   4 6
EGADS    :     14     0     Yes     5    10        1   5 6
EGADS    :     15     0     Yes    11     8        1   7 8
EGADS    :     16     0     Yes    11    12        1   7 9
EGADS    :     17     0     Yes    12     9        1   7 8
EGADS    :     18     0     Yes    12    11        1   8 9

EGADS    : Node Information

EGADS    :   Node  Active      Coordinates
EGADS    :      1     Yes                0                0                0
EGADS    :      2     Yes                0               40                0
EGADS    :      3     Yes                0                0               20
EGADS    :      4     Yes                0               40               20
EGADS    :      5     Yes               20               40                0
EGADS    :      6     Yes               20                0                0
EGADS    :      7     Yes               20                0               20
EGADS    :      8     Yes       1.61374306                0                0
EGADS    :      9     Yes                0                0                0
EGADS    :     10     Yes               20               40               20
EGADS    :     11     Yes       2.53650745       3.87298335      0.334116517
EGADS    :     12     Yes       1.57194608       3.87298335      0.249728332

EGADS    : Face and Edge Match Information

EGADS    : No Face Matches Found

AFLR4    : Surface Mesh Spacing Setup

AFLR4    : Max Bounding Box Length     = 40
AFLR4    : Min Bounding Box Length     = 40
AFLR4    : Max Ref Bounding Box Length = 40
AFLR4    : Min Ref Bounding Box Length = 40
AFLR4    : Reference Length            = 1.61374
AFLR4    : BL Thickness                = 0
AFLR4    : Abs Min Surf Spacing        = 0.00403436
AFLR4    : Min Surf Spacing            = 0.161374
AFLR4    : Max Surf Spacing            = 1.21031
AFLR4    : Global Scale Factor         = 1

AFLR4    : Geometry Definition Information

AFLR4    : Definition              Definition   Composite             Grid BC
AFLR4    :         ID                    Type          ID                Type
AFLR4    :          0     glue-only composite           -                   -
AFLR4    :          1            CAD geometry           0            STD w/BL
AFLR4    :          2            CAD geometry           0            STD w/BL
AFLR4    :          3            CAD geometry           0            STD w/BL
AFLR4    :          4            CAD geometry           0            STD w/BL
AFLR4    :          5            CAD geometry           0            STD w/BL
AFLR4    :          6            CAD geometry           0            STD w/BL
AFLR4    :          7            CAD geometry           0            STD w/BL
AFLR4    :          8            CAD geometry           0            STD w/BL
AFLR4    :          9            CAD geometry           0            STD w/BL

AFLR4    : Define CAD surface definition 1
AFLR4    : Define CAD surface definition 2
AFLR4    : Define CAD surface definition 3
AFLR4    : Define CAD surface definition 4
AFLR4    : Define CAD surface definition 5
AFLR4    : Define CAD surface definition 6
AFLR4    : Define CAD surface definition 7
AFLR4    : Define CAD surface definition 8
AFLR4    : Define CAD surface definition 9

AFLR4    : Surface Grid Generation

AFLR4    : Generate optimal mesh on surface definition 1
AFLR2    : Nodes, Trias,Quads=      1318      2502         0
AFLR4    : Nodes, Trias,Quads=      1293      2452         0

AFLR4    : Generate optimal mesh on surface definition 2
AFLR2    : Nodes, Trias,Quads=      1318      2502         0
AFLR4    : Nodes, Trias,Quads=      1298      2462         0

AFLR4    : Generate optimal mesh on surface definition 3
AFLR2    : Nodes, Trias,Quads=      3418      6687         0
AFLR4    : Nodes, Trias,Quads=      3008      5867         0

AFLR4    : Generate optimal mesh on surface definition 4
AFLR2    : Nodes, Trias,Quads=      1316      2498         0
AFLR4    : Nodes, Trias,Quads=      1297      2460         0

AFLR4    : Generate optimal mesh on surface definition 5
AFLR2    : Nodes, Trias,Quads=      1318      2502         0
AFLR4    : Nodes, Trias,Quads=      1297      2460         0

AFLR4    : Generate optimal mesh on surface definition 6
AFLR2    : Nodes, Trias,Quads=      1319      2504         0
AFLR4    : Nodes, Trias,Quads=      1294      2454         0

AFLR4    : Generate optimal mesh on surface definition 7
AFLR2    : Nodes, Trias,Quads=       200       344         0
AFLR4    : Nodes, Trias,Quads=       160       264         0

AFLR4    : Generate optimal mesh on surface definition 8
AFLR2    : Nodes, Trias,Quads=       193       330         0
AFLR4    : Nodes, Trias,Quads=       155       254         0

AFLR4    : Generate optimal mesh on surface definition 9
AFLR2    : Nodes, Trias,Quads=        17        21         0
AFLR4    : Nodes, Trias,Quads=        11         9         0

DGEOM    : Add surface definitions to composite definition 0
DGEOM    : Glue composite surface definition 0
DGEOM    : Nodes,Faces,BEdges=      9343     18682       928

AFLR4    : Curvature BG Surface Grid Generation

AFLR4    : Nodes, Faces      =      9343     18682

AFLR4    : Surface Grid Generation

AFLR4    : Generate optimal mesh on surface definition 1
AFLR2    : Nodes, Trias,Quads=      1337      2540         0
AFLR4    : Nodes, Trias,Quads=      1321      2508         0

AFLR4    : Generate optimal mesh on surface definition 2
AFLR2    : Nodes, Trias,Quads=      1339      2544         0
AFLR4    : Nodes, Trias,Quads=      1318      2502         0

AFLR4    : Generate optimal mesh on surface definition 3
AFLR2    : Nodes, Trias,Quads=      3782      7410         0
AFLR4    : Nodes, Trias,Quads=      2950      5746         0

AFLR4    : Generate optimal mesh on surface definition 4
AFLR2    : Nodes, Trias,Quads=      1339      2544         0
AFLR4    : Nodes, Trias,Quads=      1318      2502         0

AFLR4    : Generate optimal mesh on surface definition 5
AFLR2    : Nodes, Trias,Quads=      1338      2542         0
AFLR4    : Nodes, Trias,Quads=      1322      2510         0

AFLR4    : Generate optimal mesh on surface definition 6
AFLR2    : Nodes, Trias,Quads=      1340      2546         0
AFLR4    : Nodes, Trias,Quads=      1321      2508         0

AFLR4    : Generate optimal mesh on surface definition 7
AFLR2    : Nodes, Trias,Quads=       233       404         0
AFLR4    : Nodes, Trias,Quads=       210       358         0

AFLR4    : Generate optimal mesh on surface definition 8
AFLR2    : Nodes, Trias,Quads=       224       386         0
AFLR4    : Nodes, Trias,Quads=       196       330         0

AFLR4    : Generate optimal mesh on surface definition 9
AFLR2    : Nodes, Trias,Quads=        18        22         0
AFLR4    : Nodes, Trias,Quads=        12        10         0

DGEOM    : Add surface definitions to composite definition 0
DGEOM    : Glue composite surface definition 0
DGEOM    : Nodes,Faces,BEdges=      9489     18974       946

OVERALL  : CPU Time          =     0.151   seconds
Body 1 (of 1)
Number of nodes    = 9489
Number of elements = 18974
Number of triangle elements      = 18974
Number of quadrilateral elements = 0
----------------------------
Total number of nodes    = 9489
Total number of elements = 18974
Total number of triangle elements      = 18974
Total number of quadrilateral elements = 0
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 0
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 3
	Name = Farfield, index = 1
	Name = SymmPlane, index = 2
	Name = Skin, index = 3
Getting volume mesh
 
AFLR2    : ---------------------------------------
AFLR2    : AFLR2 LIBRARY
AFLR2    : ADVANCING-FRONT/LOCAL-RECONNECTION
AFLR2    : TRIA/QUAD GRID GENERATOR
AFLR2    : Version Number 9.18.1
AFLR2    : Version Date   06/11/24 @ 05:52PM
AFLR2    : Compile OS     Darwin 23.5.0 arm64
AFLR2    : Compile Date   06/11/24 @ 05:52PM
AFLR2    : Copyright 1994-2021, D.L. Marcum
AFLR2    : ---------------------------------------
 
AFLR4    : ---------------------------------------
AFLR4    : AFLR4 LIBRARY
AFLR4    : ADVANCING-FRONT/LOCAL-RECONNECTION
AFLR4    : TRIA/QUAD SURFACE GRID GENERATOR
AFLR4    : Version Number 11.5.15
AFLR4    : Version Date   07/19/24 @ 07:04PM
AFLR4    : Compile OS     Darwin 23.5.0 arm64
AFLR4    : Compile Date   07/19/24 @ 07:06PM
AFLR4    : Copyright 1994-2021, D.L. Marcum
AFLR4    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.8.1
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.8.1
EGADS    : ---------------------------------------
Volume mesh:
	Number of nodes          = 60093
	Number of elements       = 345939
	Number of triangles      = 18974
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 326965
	Number of pyramids       = 0
	Number of prisms         = 0
	Number of hexahedrals    = 0

Writing SU2 file ....
Finished writing SU2 file

Getting CFD boundary conditions
	Boundary condition name - Farfield
	Boundary condition name - Skin
	Boundary condition name - SymmPlane
	Done getting CFD boundary conditions
Info: No recognized data transfer names found.
Warning: The su2 cfg file will be overwritten!
Write SU2 configuration file for version "Harrier (8.0.1)"


Running SU2......

-------------------------------------------------------------------------
|    ___ _   _ ___                                                      |
|   / __| | | |_  )   Release 8.0.0 "Harrier"                           |
|   \__ \ |_| |/ /                                                      |
|   |___/\___//___|   Suite (Computational Fluid Dynamics Code)         |
|                                                                       |
-------------------------------------------------------------------------
| SU2 Project Website: <a href='https://su2code.github.io'>https://su2code.github.io</a>                        |
|                                                                       |
| The SU2 Project is maintained by the SU2 Foundation                   |
| (<a href='http://su2foundation.org'>http://su2foundation.org</a>)                                            |
-------------------------------------------------------------------------
| Copyright 2012-2023, SU2 Contributors                                 |
|                                                                       |
| SU2 is free software; you can redistribute it and/or                  |
| modify it under the terms of the GNU Lesser General Public            |
| License as published by the Free Software Foundation; either          |
| version 2.1 of the License, or (at your option) any later version.    |
|                                                                       |
| SU2 is distributed in the hope that it will be useful,                |
| but WITHOUT ANY WARRANTY; without even the implied warranty of        |
| MERCHANTABILITY or FITNESS FOR A PARTICULAR PURPOSE. See the GNU      |
| Lesser General Public License for more details.                       |
|                                                                       |
| You should have received a copy of the GNU Lesser General Public      |
| License along with SU2. If not, see &lt;<a href='http://www.gnu.org/licenses/'>http://www.gnu.org/licenses/</a>&gt;.   |
-------------------------------------------------------------------------

Parsing config file for zone 0

----------------- Physical Case Definition ( Zone 0 ) -------------------
Compressible Euler equations.
Mach number: 0.294118.
Angle of attack (AoA): 0 deg, and angle of sideslip (AoS): 0 deg.
No restart solution, use the values at infinity (freestream).
Dimensional simulation.
The reference area is 1 m^2.
The semi-span will be computed using the max y(3D) value.
The reference length is 1 m.
Reference origin for moment evaluation is (0, 0, 0).
Surface(s) where the force coefficients are evaluated: BC_3.

Surface(s) plotted in the output file: BC_3.
Surface(s) affected by the design variables: BC_3.
Input mesh file name: ../aflr3/aflr3_CAPS.su2

--------------- Space Numerical Integration ( Zone 0 ) ------------------
Roe (with entropy fix = 0.001) solver for the flow inviscid terms.
Standard Roe without low-dissipation function.
Second order integration in space, with slope limiter.
Venkatakrishnan slope-limiting method, with constant: 0.05.
The reference element size is: 1. 
Gradient for upwind reconstruction: inverse-distance weighted Least-Squares.
Gradient for viscous and source terms: inverse-distance weighted Least-Squares.

--------------- Time Numerical Integration  ( Zone 0 ) ------------------
Local time stepping (steady state simulation).
Euler implicit method for the flow equations.
FGMRES is used for solving the linear system.
Using a ILU(0) preconditioning.
Convergence criteria of the linear solver: 1e-06.
Max number of linear iterations: 10.
V Multigrid Cycle, with 2 multigrid levels.
Damping factor for the residual restriction: 0.75.
Damping factor for the correction prolongation: 0.75.
No CFL adaptation.
+-------------------------------------------+
|  MG Level| Presmooth|PostSmooth|CorrectSmo|
+-------------------------------------------+
|         0|         1|         0|         0|
|         1|         2|         0|         0|
|         2|         3|         0|         0|
+-------------------------------------------+
Courant-Friedrichs-Lewy number:       10

------------------ Convergence Criteria  ( Zone 0 ) ---------------------
Maximum number of solver subiterations: 3.
Begin convergence monitoring at iteration 5.
Residual minimum value: 1e-14.
Cauchy series min. value: 1e-10.
Number of Cauchy elements: 100.
Begin windowed time average at iteration 0.

-------------------- Output Information ( Zone 0 ) ----------------------
File writing frequency: 
+------------------------------------+
|                     File| Frequency|
+------------------------------------+
|                  RESTART|       250|
|              SURFACE_CSV|       250|
|                  TECPLOT|       250|
|          SURFACE_TECPLOT|       250|
+------------------------------------+
Writing the convergence history file every 1 inner iterations.
Writing the screen convergence history every 1 inner iterations.
The tabular file format is CSV (.csv).
Convergence history file name: history.
Forces breakdown file name: forces_breakdown_aeroelasticSimple_Pressure_SA.dat.
Surface file name: surface_flow_aeroelasticSimple_Pressure_SA.
Volume file name: flow_aeroelasticSimple_Pressure_SA.
Restart file name: restart_flow_aeroelasticSimple_Pressure_SA.dat.

------------- Config File Boundary Information ( Zone 0 ) ---------------
+-----------------------------------------------------------------------+
|                        Marker Type|                        Marker Name|
+-----------------------------------------------------------------------+
|                         Euler wall|                               BC_3|
+-----------------------------------------------------------------------+
|                          Far-field|                               BC_1|
+-----------------------------------------------------------------------+
|                     Symmetry plane|                               BC_2|
+-----------------------------------------------------------------------+

-------------------- Output Preprocessing ( Zone 0 ) --------------------

WARNING: SURFACE_PRESSURE_DROP can only be computed for at least 2 surfaces (outlet, inlet, ...)

Screen output fields: TIME_ITER, OUTER_ITER, INNER_ITER, CUR_TIME, TIME_STEP, WALL_TIME, RMS_DENSITY, RMS_MOMENTUM-X, RMS_MOMENTUM-Y, RMS_ENERGY, EFFICIENCY
History output group(s): ITER, TIME_DOMAIN, WALL_TIME, RMS_RES, AERO_COEFF
Convergence field(s): RMS_DENSITY
Warning: No (valid) fields chosen for time convergence monitoring. Time convergence monitoring inactive.
Volume output fields: COORDINATES, SOLUTION, PRIMITIVE

------------------- Geometry Preprocessing ( Zone 0 ) -------------------
Three dimensional problem.
60093 grid points.
326965 volume elements.
3 surface markers.
12530 boundary elements in index 0 (Marker = BC_1).
5746 boundary elements in index 1 (Marker = BC_2).
698 boundary elements in index 2 (Marker = BC_3).
326965 tetrahedra.
Setting point connectivity.
Renumbering points (Reverse Cuthill McKee Ordering).
Recomputing point connectivity.
Setting element connectivity.
Checking the numerical grid orientation.
All volume elements are correctly orientend.
All surface elements are correctly orientend.
Identifying edges and vertices.
Setting the control volume structure.
Volume of the computational grid: 63999.5.
Searching for the closest normal neighbors to the surfaces.
Storing a mapping from global to local point index.
Compute the surface curvature.
Max K: 83.4538. Mean K: 0.86237. Standard deviation K: 5.00385.
Checking for periodicity.
Computing mesh quality statistics for the dual control volumes.
+--------------------------------------------------------------+
|           Mesh Quality Metric|        Minimum|        Maximum|
+--------------------------------------------------------------+
|    Orthogonality Angle (deg.)|        54.7348|        86.8035|
|     CV Face Area Aspect Ratio|        1.06478|        21.5651|
|           CV Sub-Volume Ratio|              1|        8.64744|
+--------------------------------------------------------------+
Setting the multigrid structure.
+-------------------------------------------+
|  MG Level|       CVs|Aggl. Rate|       CFL|
+-------------------------------------------+
|         0|     60093|    1/1.00|        10|
|         1|     10214|    1/5.88|     8.309|
|         2|      1799|    1/5.68|   6.98637|
+-------------------------------------------+
Finding max control volume width.
Semi-span length = 3.87298 m.
Wetted area = 9.2451 m^2.
Area projection in the x-plane = 0.651846 m^2, y-plane = 0.30478 m^2, z-plane = 4.4157 m^2.
Max. coordinate in the x-direction = 2.53651 m, y-direction = 3.87298 m, z-direction = 0.38 m.
Min. coordinate in the x-direction = 0 m, y-direction = -2.86329e-18 m, z-direction = -0.0467611 m.
Checking if Euler &amp; Symmetry markers are straight/plane:
Boundary marker BC_3 is NOT a single plane.
Boundary marker BC_2 is a single plane.
Computing wall distances.

-------------------- Solver Preprocessing ( Zone 0 ) --------------------
Inviscid flow: Computing density based on free-stream
temperature and pressure using the ideal gas law.
Force coefficients computed using free-stream values.

-- Models:
+------------------------------------------------------------------------------+
|          Viscosity Model|        Conductivity Model|              Fluid Model|
+------------------------------------------------------------------------------+
|                        -|                         -|             STANDARD_AIR|
+------------------------------------------------------------------------------+
-- Fluid properties:
+------------------------------------------------------------------------------+
|                  Name|    Dim. value|    Ref. value|      Unit|Non-dim. value|
+------------------------------------------------------------------------------+
|          Gas Constant|       287.058|             1|  N.m/kg.K|       287.058|
|      Spec. Heat Ratio|             -|             -|         -|           1.4|
+------------------------------------------------------------------------------+
-- Initial and free-stream conditions:
+------------------------------------------------------------------------------+
|                  Name|    Dim. value|    Ref. value|      Unit|Non-dim. value|
+------------------------------------------------------------------------------+
|       Static Pressure|        101325|             1|        Pa|        101325|
|               Density|       1.22498|             1|    kg/m^3|       1.22498|
|           Temperature|        288.15|             1|         K|        288.15|
|          Total Energy|        211798|             1|   m^2/s^2|        211798|
|            Velocity-X|       100.087|             1|       m/s|       100.087|
|            Velocity-Y|             0|             1|       m/s|             0|
|            Velocity-Z|             0|             1|       m/s|             0|
|    Velocity Magnitude|       100.087|             1|       m/s|       100.087|
+------------------------------------------------------------------------------+
|           Mach Number|             -|             -|         -|      0.294118|
+------------------------------------------------------------------------------+
Initialize Jacobian structure (Euler). MG level: 0.
Initialize Jacobian structure (Euler). MG level: 1.
Initialize Jacobian structure (Euler). MG level: 2.

------------------- Numerics Preprocessing ( Zone 0 ) -------------------

----------------- Integration Preprocessing ( Zone 0 ) ------------------

------------------- Iteration Preprocessing ( Zone 0 ) ------------------
Euler/Navier-Stokes/RANS fluid iteration.

------------------------------ Begin Solver -----------------------------

Simulation Run using the Single-zone Driver
WARNING: SU2 was not compiled for an AVX-capable architecture. Performance could be better,
         see <a href='https://su2code.github.io/docs_v7/Build-SU2-Linux-MacOS/#compiler-optimizations'>https://su2code.github.io/docs_v7/Build-SU2-Linux-MacOS/#compiler-optimizations</a>
WARNING: SU2 was not compiled for an AVX-capable architecture. Performance could be better,
         see <a href='https://su2code.github.io/docs_v7/Build-SU2-Linux-MacOS/#compiler-optimizations'>https://su2code.github.io/docs_v7/Build-SU2-Linux-MacOS/#compiler-optimizations</a>
WARNING: SU2 was not compiled for an AVX-capable architecture. Performance could be better,
         see <a href='https://su2code.github.io/docs_v7/Build-SU2-Linux-MacOS/#compiler-optimizations'>https://su2code.github.io/docs_v7/Build-SU2-Linux-MacOS/#compiler-optimizations</a>
+----------------------------------------------------------------------------------------------------------------------------------------------+
|   Time_Iter|  Outer_Iter|  Inner_Iter|    Cur_Time|   Time_Step|   Time(sec)|    rms[Rho]|   rms[RhoU]|   rms[RhoV]|   rms[RhoE]|        CEff|
+----------------------------------------------------------------------------------------------------------------------------------------------+
|           0|           0|           0|  0.0000e+00|  0.0000e+00|  9.9137e-01|   -1.355330|    0.925001|    0.586785|    4.113776|   -0.972828|
|           0|           0|           1|  0.0000e+00|  0.0000e+00|  9.8294e-01|   -1.745808|    0.767133|    0.413608|    3.711112|   -0.534020|
|           0|           0|           2|  0.0000e+00|  0.0000e+00|  9.8109e-01|   -1.758263|    0.583631|    0.231030|    3.699433|    1.633106|

----------------------------- Solver Exit -------------------------------

Maximum number of iterations reached (ITER = 3) before convergence.
+-----------------------------------------------------------------------+
|      Convergence Field     |     Value    |   Criterion  |  Converged |
+-----------------------------------------------------------------------+
|                    rms[Rho]|      -1.75826|         &lt; -14|          No|
+-----------------------------------------------------------------------+
-------------------------------------------------------------------------
+-----------------------------------------------------------------------+
|        File Writing Summary       |              Filename             |
+-----------------------------------------------------------------------+
|SU2 binary restart                 |restart_flow_aeroelasticSimple_Pressure_SA.dat|

Writing the forces breakdown file (forces_breakdown_aeroelasticSimple_Pressure_SA.dat).
|CSV file                           |surface_flow_aeroelasticSimple_Pressure_SA.csv|

Writing the forces breakdown file (forces_breakdown_aeroelasticSimple_Pressure_SA.dat).
|Tecplot binary                     |flow_aeroelasticSimple_Pressure_SA.szplt|

Writing the forces breakdown file (forces_breakdown_aeroelasticSimple_Pressure_SA.dat).
|Tecplot binary surface             |surface_flow_aeroelasticSimple_Pressure_SA.szplt|

Writing the forces breakdown file (forces_breakdown_aeroelasticSimple_Pressure_SA.dat).
+-----------------------------------------------------------------------+

--------------------------- Finalizing Solver ---------------------------
Deleted CNumerics container.
Deleted CIntegration container.
Deleted CSolver container.
Deleted CIteration container.
Deleted CInterface container.
Deleted CGeometry container.
Deleted CFreeFormDefBox class.
Deleted CSurfaceMovement class.
Deleted CVolumetricMovement class.
Deleted CConfig container.
Deleted nInst container.
Deleted COutput class.
-------------------------------------------------------------------------

------------------------- Exit Success (SU2_CFD) ------------------------


Running PostAnalysis ...... su2

Running ...... astros
Mapping Csys attributes ................
	Number of unique Csys attributes = 0

Getting FEA coordinate systems.......
	Number of coordinate systems - 0
	No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
	Number of unique capsConstraint attributes = 1
	Name = Rib_Root, index = 1
Mapping capsLoad attributes ................
	Number of unique capsLoad attributes = 1
	Name = Skin, index = 1
Mapping capsBound attributes ................
	Number of unique capsBound attributes = 3
	Name = Skin_Top, index = 1
	Name = Skin_Bottom, index = 2
	Name = Skin_Tip, index = 3
Mapping capsConnect attributes ................
	Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
	Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
	Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 2
	Name = Skin, index = 1
	Name = Rib_Root, index = 2
Setting FEA Data
	Mesh for body = 0
	Number of nodal coordinates = 180
	Number of elements = 194
	Elemental Nodes = 0
	Elemental Rods  = 0
	Elemental Tria3 = 32
	Elemental Quad4 = 162
Aero_Reference value is NULL - No aero reference parameters set

Getting FEA materials.......
	Number of materials - 1
	Material name - Madeupium
	Done getting FEA materials

Getting FEA properties.......
	Number of properties - 2
	Property name - Rib_Root
	Property name - Skin
	Done getting FEA properties
Updating mesh element types based on properties input

Getting FEA constraints.......
	Number of constraints - 1
	Constraint name - edgeConstraint
	No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement"
	Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults

Getting FEA loads.......
	Number of loads - 1
	Load name - pressureAero
	No "groupName" specified for Load tuple pressureAero, going to use load name
	Done getting FEA loads
Optimization Control tuple is NULL - Default optimization control is used

Getting FEA optimization control.......
Done getting FEA Optimization Control
Design_Variable tuple is NULL - No design variables applied
Design_Constraint tuple is NULL - No design constraints applied
Analysis tuple is NULL

Getting FEA analyses.......
	Number of analyses - 1
	Analysis name - Default
	Done getting FEA analyses
Reading SU2 AeroLoad File - surface_flow_aeroelasticSimple_Pressure_SA.csv
	Number of variables = 16
	Number of data points = 361
 CAPS Info: Bound 'Skin_Top' Normalized Integrated 'Pressure'
            Rank 0: src = 3.101730e+09, tgt = 3.101730e+09, diff = 3.131247e+02
Reading SU2 AeroLoad File - surface_flow_aeroelasticSimple_Pressure_SA.csv
	Number of variables = 16
	Number of data points = 361
 CAPS Info: Bound 'Skin_Bottom' Normalized Integrated 'Pressure'
            Rank 0: src = 3.017948e+09, tgt = 3.017948e+09, diff = 2.034838e+02
Reading SU2 AeroLoad File - surface_flow_aeroelasticSimple_Pressure_SA.csv
	Number of variables = 16
	Number of data points = 361
 CAPS Info: Bound 'Skin_Tip' Normalized Integrated 'Pressure'
            Rank 0: src = 4.372770e+07, tgt = 4.372770e+07, diff = 1.404514e-02
Extracting external pressure loads from data transfer....
	TransferName = Skin_Top
	Number of Elements = 81 (total = 81)
Extracting external pressure loads from data transfer....
	TransferName = Skin_Bottom
	Number of Elements = 81 (total = 162)
Extracting external pressure loads from data transfer....
	TransferName = Skin_Tip
	Number of Elements = 16 (total = 178)

Writing Astros grid and connectivity file (in free field format) ....
Finished writing Astros grid file

Writing subElement types (if any) - appending mesh file

Writing Astros instruction file....
	Writing analysis cards
	Writing load ADD cards
	Writing constraint cards--each subcase individually
	Writing load cards
	Writing material cards
	Writing property cards
Note: The following floating-point exceptions are signalling: IEEE_UNDERFLOW_FLAG

real	0m10.310s
user	0m10.517s
sys	0m0.865s
+ status=0
+ set +x

=================================================
CAPS verification (using pyCAPS) case aeroelasticSimple_Pressure_SU2_and_Astros.py passed (as expected)
=================================================


=================================================
+ echo 'aeroelasticSimple_Displacement_SU2_and_Astros.py test;'
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESP126/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
aeroelasticSimple_Displacement_SU2_and_Astros.py test;
+ python -u aeroelasticSimple_Displacement_SU2_and_Astros.py -outLevel=0 -noPlotData
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESP126/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt

Running PreAnalysis ...... astros
Mapping Csys attributes ................
	Number of unique Csys attributes = 0

Getting FEA coordinate systems.......
	Number of coordinate systems - 0
	No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
	Number of unique capsConstraint attributes = 1
	Name = Rib_Root, index = 1
Mapping capsLoad attributes ................
	Number of unique capsLoad attributes = 1
	Name = Skin, index = 1
Mapping capsBound attributes ................
	Number of unique capsBound attributes = 3
	Name = Skin_Top, index = 1
	Name = Skin_Bottom, index = 2
	Name = Skin_Tip, index = 3
Mapping capsConnect attributes ................
	Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
	Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
	Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 2
	Name = Skin, index = 1
	Name = Rib_Root, index = 2
Setting FEA Data
	Mesh for body = 0
	Number of nodal coordinates = 180
	Number of elements = 194
	Elemental Nodes = 0
	Elemental Rods  = 0
	Elemental Tria3 = 32
	Elemental Quad4 = 162
Aero_Reference value is NULL - No aero reference parameters set

Getting FEA materials.......
	Number of materials - 1
	Material name - Madeupium
	Done getting FEA materials

Getting FEA properties.......
	Number of properties - 2
	Property name - Rib_Root
	Property name - Skin
	Done getting FEA properties
Updating mesh element types based on properties input

Getting FEA constraints.......
	Number of constraints - 1
	Constraint name - edgeConstraint
	No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement"
	Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults

Getting FEA loads.......
	Number of loads - 1
	Load name - pressureInternal
	Done getting FEA loads
Optimization Control tuple is NULL - Default optimization control is used

Getting FEA optimization control.......
Done getting FEA Optimization Control
Design_Variable tuple is NULL - No design variables applied
Design_Constraint tuple is NULL - No design constraints applied
Analysis tuple is NULL

Getting FEA analyses.......
	Number of analyses - 1
	Analysis name - Default
	Done getting FEA analyses

Writing Astros grid and connectivity file (in free field format) ....
Finished writing Astros grid file

Writing subElement types (if any) - appending mesh file

Writing Astros instruction file....
	Writing analysis cards
	Writing load ADD cards
	Writing constraint cards--each subcase individually
	Writing load cards
	Writing material cards
	Writing property cards


Running Astros......
Note: The following floating-point exceptions are signalling: IEEE_UNDERFLOW_FLAG

Running PostAnalysis ...... astros

Running PreAnalysis ...... su2
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 3
	Name = Farfield, index = 1
	Name = SymmPlane, index = 2
	Name = Skin, index = 3
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 0
 
AFLR2    : ---------------------------------------
AFLR2    : AFLR2 LIBRARY
AFLR2    : ADVANCING-FRONT/LOCAL-RECONNECTION
AFLR2    : TRIA/QUAD GRID GENERATOR
AFLR2    : Version Number 9.18.1
AFLR2    : Version Date   06/11/24 @ 05:52PM
AFLR2    : Compile OS     Darwin 23.5.0 arm64
AFLR2    : Compile Date   06/11/24 @ 05:52PM
AFLR2    : Copyright 1994-2021, D.L. Marcum
AFLR2    : ---------------------------------------
 
AFLR4    : ---------------------------------------
AFLR4    : AFLR4 LIBRARY
AFLR4    : ADVANCING-FRONT/LOCAL-RECONNECTION
AFLR4    : TRIA/QUAD SURFACE GRID GENERATOR
AFLR4    : Version Number 11.5.15
AFLR4    : Version Date   07/19/24 @ 07:04PM
AFLR4    : Compile OS     Darwin 23.5.0 arm64
AFLR4    : Compile Date   07/19/24 @ 07:06PM
AFLR4    : Copyright 1994-2021, D.L. Marcum
AFLR4    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.8.1
EGADS    : ---------------------------------------

EGADS    : EGADS CAD Geometry Setup

EGADS    : Model has 1 Active Bodies

EGADS    : Body 0 is a SolidBody
EGADS    : Body 0 has 1 Shells
EGADS    : Body 0 has 9 Faces
EGADS    : Body 0 has 18 Edges
EGADS    : Body 0 has 10 Loops
EGADS    : Body 0 has 12 Nodes

EGADS    : Check Grid BCs

EGADS    : Grid BCs are OK

EGADS    : Face Neighbor-Faces Information

EGADS    : QC  = Face Quad Combination Flag
EGADS    : IER = Face Isolated Edge Refinement Flag
EGADS    : ER  = Face Edge Refinement Factor
EGADS    :       Not applicable for Faces with a FarField Grid BC.
EGADS    : SF  = Face Scale Factor
EGADS    :       Not applicable for Faces with a FarField Grid BC.

EGADS    :   Face          Body    QC   IER       ER    Scale   Neighbor
EGADS    :     ID  Active    ID  Flag  Flag   Weight   Factor   Faces
EGADS    :      1     Yes     0     0     1        0        1   2 3 4 5
EGADS    :      2     Yes     0     0     1        0        1   1 3 5 6
EGADS    :      3     Yes     0     0     1        0        1   1 2 4 6 7 8
EGADS    :      4     Yes     0     0     1        0        1   1 3 5 6
EGADS    :      5     Yes     0     0     1        0        1   1 2 4 6
EGADS    :      6     Yes     0     0     1        0        1   2 3 4 5
EGADS    :      7     Yes     0     0     1        0        1   3 8 9
EGADS    :      8     Yes     0     0     1        0        1   3 7 9
EGADS    :      9     Yes     0     0     1        0        1   7 8

EGADS    : Face Edges Information

EGADS    :   Face   Edges
EGADS    :      1   1 2 -3 -4
EGADS    :      2   5 6 -7 -1
EGADS    :      3   -2 7 9 -8 -10 -11
EGADS    :      4   -12 3 8 -13
EGADS    :      5   4 12 -14 -5
EGADS    :      6   -6 14 13 -9
EGADS    :      7   15 10 -17 -16
EGADS    :      8   17 11 -15 -18
EGADS    :      9   16 18

EGADS    : Face Loops Information

EGADS    :   Face   Loops
EGADS    :      1   1
EGADS    :      2   2
EGADS    :      3   3 4
EGADS    :      4   5
EGADS    :      5   6
EGADS    :      6   7
EGADS    :      7   8
EGADS    :      8   9
EGADS    :      9   10

EGADS    : Loop Edges Information

EGADS    :   Loop  Active   Edges
EGADS    :      1     Yes   1 2 -3 -4
EGADS    :      2     Yes   5 6 -7 -1
EGADS    :      3     Yes   -2 7 9 -8
EGADS    :      4     Yes   -10 -11
EGADS    :      5     Yes   -12 3 8 -13
EGADS    :      6     Yes   4 12 -14 -5
EGADS    :      7     Yes   -6 14 13 -9
EGADS    :      8     Yes   15 10 -17 -16
EGADS    :      9     Yes   17 11 -15 -18
EGADS    :     10     Yes   16 18

EGADS    : Edge Node, Scale Factor, and Neighbor-Faces Information

EGADS    : ESF = Edge Scale Factor
EGADS    :       Not applicable for DEGENERATE Edges or Edges with a FarField
EGADS    :       Grid BC Neighbor Face.

EGADS    :                                             Neighbor
EGADS    :   Edge  Body  Active Node1 Node2      ESF   Faces
EGADS    :      1     0     Yes     2     1        1   1 2
EGADS    :      2     0     Yes     1     3        1   1 3
EGADS    :      3     0     Yes     4     3        1   1 4
EGADS    :      4     0     Yes     2     4        1   1 5
EGADS    :      5     0     Yes     2     5        1   2 5
EGADS    :      6     0     Yes     5     6        1   2 6
EGADS    :      7     0     Yes     1     6        1   2 3
EGADS    :      8     0     Yes     3     7        1   3 4
EGADS    :      9     0     Yes     6     7        1   3 6
EGADS    :     10     0     Yes     8     9        1   3 7
EGADS    :     11     0     Yes     9     8        1   3 8
EGADS    :     12     0     Yes     4    10        1   4 5
EGADS    :     13     0     Yes    10     7        1   4 6
EGADS    :     14     0     Yes     5    10        1   5 6
EGADS    :     15     0     Yes    11     8        1   7 8
EGADS    :     16     0     Yes    11    12        1   7 9
EGADS    :     17     0     Yes    12     9        1   7 8
EGADS    :     18     0     Yes    12    11        1   8 9

EGADS    : Node Information

EGADS    :   Node  Active      Coordinates
EGADS    :      1     Yes                0                0                0
EGADS    :      2     Yes                0               40                0
EGADS    :      3     Yes                0                0               20
EGADS    :      4     Yes                0               40               20
EGADS    :      5     Yes               20               40                0
EGADS    :      6     Yes               20                0                0
EGADS    :      7     Yes               20                0               20
EGADS    :      8     Yes       1.61374306                0                0
EGADS    :      9     Yes                0                0                0
EGADS    :     10     Yes               20               40               20
EGADS    :     11     Yes       2.53650745       3.87298335      0.334116517
EGADS    :     12     Yes       1.57194608       3.87298335      0.249728332

EGADS    : Face and Edge Match Information

EGADS    : No Face Matches Found

AFLR4    : Surface Mesh Spacing Setup

AFLR4    : Max Bounding Box Length     = 40
AFLR4    : Min Bounding Box Length     = 40
AFLR4    : Max Ref Bounding Box Length = 40
AFLR4    : Min Ref Bounding Box Length = 40
AFLR4    : Reference Length            = 1.61374
AFLR4    : BL Thickness                = 0
AFLR4    : Abs Min Surf Spacing        = 0.00403436
AFLR4    : Min Surf Spacing            = 0.161374
AFLR4    : Max Surf Spacing            = 1.21031
AFLR4    : Global Scale Factor         = 1

AFLR4    : Geometry Definition Information

AFLR4    : Definition              Definition   Composite             Grid BC
AFLR4    :         ID                    Type          ID                Type
AFLR4    :          0     glue-only composite           -                   -
AFLR4    :          1            CAD geometry           0            STD w/BL
AFLR4    :          2            CAD geometry           0            STD w/BL
AFLR4    :          3            CAD geometry           0            STD w/BL
AFLR4    :          4            CAD geometry           0            STD w/BL
AFLR4    :          5            CAD geometry           0            STD w/BL
AFLR4    :          6            CAD geometry           0            STD w/BL
AFLR4    :          7            CAD geometry           0            STD w/BL
AFLR4    :          8            CAD geometry           0            STD w/BL
AFLR4    :          9            CAD geometry           0            STD w/BL

AFLR4    : Define CAD surface definition 1
AFLR4    : Define CAD surface definition 2
AFLR4    : Define CAD surface definition 3
AFLR4    : Define CAD surface definition 4
AFLR4    : Define CAD surface definition 5
AFLR4    : Define CAD surface definition 6
AFLR4    : Define CAD surface definition 7
AFLR4    : Define CAD surface definition 8
AFLR4    : Define CAD surface definition 9

AFLR4    : Surface Grid Generation

AFLR4    : Generate optimal mesh on surface definition 1
AFLR2    : Nodes, Trias,Quads=      1318      2502         0
AFLR4    : Nodes, Trias,Quads=      1293      2452         0

AFLR4    : Generate optimal mesh on surface definition 2
AFLR2    : Nodes, Trias,Quads=      1318      2502         0
AFLR4    : Nodes, Trias,Quads=      1298      2462         0

AFLR4    : Generate optimal mesh on surface definition 3
AFLR2    : Nodes, Trias,Quads=      3418      6687         0
AFLR4    : Nodes, Trias,Quads=      3008      5867         0

AFLR4    : Generate optimal mesh on surface definition 4
AFLR2    : Nodes, Trias,Quads=      1316      2498         0
AFLR4    : Nodes, Trias,Quads=      1297      2460         0

AFLR4    : Generate optimal mesh on surface definition 5
AFLR2    : Nodes, Trias,Quads=      1318      2502         0
AFLR4    : Nodes, Trias,Quads=      1297      2460         0

AFLR4    : Generate optimal mesh on surface definition 6
AFLR2    : Nodes, Trias,Quads=      1319      2504         0
AFLR4    : Nodes, Trias,Quads=      1294      2454         0

AFLR4    : Generate optimal mesh on surface definition 7
AFLR2    : Nodes, Trias,Quads=       200       344         0
AFLR4    : Nodes, Trias,Quads=       160       264         0

AFLR4    : Generate optimal mesh on surface definition 8
AFLR2    : Nodes, Trias,Quads=       193       330         0
AFLR4    : Nodes, Trias,Quads=       155       254         0

AFLR4    : Generate optimal mesh on surface definition 9
AFLR2    : Nodes, Trias,Quads=        17        21         0
AFLR4    : Nodes, Trias,Quads=        11         9         0

DGEOM    : Add surface definitions to composite definition 0
DGEOM    : Glue composite surface definition 0
DGEOM    : Nodes,Faces,BEdges=      9343     18682       928

AFLR4    : Curvature BG Surface Grid Generation

AFLR4    : Nodes, Faces      =      9343     18682

AFLR4    : Surface Grid Generation

AFLR4    : Generate optimal mesh on surface definition 1
AFLR2    : Nodes, Trias,Quads=      1337      2540         0
AFLR4    : Nodes, Trias,Quads=      1321      2508         0

AFLR4    : Generate optimal mesh on surface definition 2
AFLR2    : Nodes, Trias,Quads=      1339      2544         0
AFLR4    : Nodes, Trias,Quads=      1318      2502         0

AFLR4    : Generate optimal mesh on surface definition 3
AFLR2    : Nodes, Trias,Quads=      3782      7410         0
AFLR4    : Nodes, Trias,Quads=      2950      5746         0

AFLR4    : Generate optimal mesh on surface definition 4
AFLR2    : Nodes, Trias,Quads=      1339      2544         0
AFLR4    : Nodes, Trias,Quads=      1318      2502         0

AFLR4    : Generate optimal mesh on surface definition 5
AFLR2    : Nodes, Trias,Quads=      1338      2542         0
AFLR4    : Nodes, Trias,Quads=      1322      2510         0

AFLR4    : Generate optimal mesh on surface definition 6
AFLR2    : Nodes, Trias,Quads=      1340      2546         0
AFLR4    : Nodes, Trias,Quads=      1321      2508         0

AFLR4    : Generate optimal mesh on surface definition 7
AFLR2    : Nodes, Trias,Quads=       233       404         0
AFLR4    : Nodes, Trias,Quads=       210       358         0

AFLR4    : Generate optimal mesh on surface definition 8
AFLR2    : Nodes, Trias,Quads=       224       386         0
AFLR4    : Nodes, Trias,Quads=       196       330         0

AFLR4    : Generate optimal mesh on surface definition 9
AFLR2    : Nodes, Trias,Quads=        18        22         0
AFLR4    : Nodes, Trias,Quads=        12        10         0

DGEOM    : Add surface definitions to composite definition 0
DGEOM    : Glue composite surface definition 0
DGEOM    : Nodes,Faces,BEdges=      9489     18974       946

OVERALL  : CPU Time          =     0.138   seconds
Body 1 (of 1)
Number of nodes    = 9489
Number of elements = 18974
Number of triangle elements      = 18974
Number of quadrilateral elements = 0
----------------------------
Total number of nodes    = 9489
Total number of elements = 18974
Total number of triangle elements      = 18974
Total number of quadrilateral elements = 0
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 0
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 3
	Name = Farfield, index = 1
	Name = SymmPlane, index = 2
	Name = Skin, index = 3
Getting volume mesh
 
AFLR2    : ---------------------------------------
AFLR2    : AFLR2 LIBRARY
AFLR2    : ADVANCING-FRONT/LOCAL-RECONNECTION
AFLR2    : TRIA/QUAD GRID GENERATOR
AFLR2    : Version Number 9.18.1
AFLR2    : Version Date   06/11/24 @ 05:52PM
AFLR2    : Compile OS     Darwin 23.5.0 arm64
AFLR2    : Compile Date   06/11/24 @ 05:52PM
AFLR2    : Copyright 1994-2021, D.L. Marcum
AFLR2    : ---------------------------------------
 
AFLR4    : ---------------------------------------
AFLR4    : AFLR4 LIBRARY
AFLR4    : ADVANCING-FRONT/LOCAL-RECONNECTION
AFLR4    : TRIA/QUAD SURFACE GRID GENERATOR
AFLR4    : Version Number 11.5.15
AFLR4    : Version Date   07/19/24 @ 07:04PM
AFLR4    : Compile OS     Darwin 23.5.0 arm64
AFLR4    : Compile Date   07/19/24 @ 07:06PM
AFLR4    : Copyright 1994-2021, D.L. Marcum
AFLR4    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.8.1
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.8.1
EGADS    : ---------------------------------------
Volume mesh:
	Number of nodes          = 60093
	Number of elements       = 345939
	Number of triangles      = 18974
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 326965
	Number of pyramids       = 0
	Number of prisms         = 0
	Number of hexahedrals    = 0

Writing SU2 file ....
Finished writing SU2 file

Getting CFD boundary conditions
	Boundary condition name - Farfield
	Boundary condition name - Skin
	Boundary condition name - SymmPlane
	Done getting CFD boundary conditions
Writing SU2 data transfer files
Writing SU2 Motion File - aeroelasticSimple_Displacement_SA_motion.dat
Warning: The su2 cfg file will be overwritten!
Write SU2 configuration file for version "Harrier (8.0.1)"


Running SU2......

-------------------------------------------------------------------------
|    ___ _   _ ___                                                      |
|   / __| | | |_  )   Release 8.0.0 "Harrier"                           |
|   \__ \ |_| |/ /                                                      |
|   |___/\___//___|   Suite (Mesh Deformation Code)                     |
|                                                                       |
-------------------------------------------------------------------------
| SU2 Project Website: <a href='https://su2code.github.io'>https://su2code.github.io</a>                        |
|                                                                       |
| The SU2 Project is maintained by the SU2 Foundation                   |
| (<a href='http://su2foundation.org'>http://su2foundation.org</a>)                                            |
-------------------------------------------------------------------------
| Copyright 2012-2023, SU2 Contributors                                 |
|                                                                       |
| SU2 is free software; you can redistribute it and/or                  |
| modify it under the terms of the GNU Lesser General Public            |
| License as published by the Free Software Foundation; either          |
| version 2.1 of the License, or (at your option) any later version.    |
|                                                                       |
| SU2 is distributed in the hope that it will be useful,                |
| but WITHOUT ANY WARRANTY; without even the implied warranty of        |
| MERCHANTABILITY or FITNESS FOR A PARTICULAR PURPOSE. See the GNU      |
| Lesser General Public License for more details.                       |
|                                                                       |
| You should have received a copy of the GNU Lesser General Public      |
| License along with SU2. If not, see &lt;<a href='http://www.gnu.org/licenses/'>http://www.gnu.org/licenses/</a>&gt;.   |
-------------------------------------------------------------------------

----------------- Physical Case Definition ( Zone 0 ) -------------------
Input mesh file name: ../aflr3/aflr3_CAPS.su2

---------------- Grid deformation parameters ( Zone 0 )  ----------------
Grid deformation using a linear elasticity method.


-------------------- Output Information ( Zone 0 ) ----------------------
Output mesh file name: ../aflr3/aflr3_CAPS.su2. 
Cell stiffness scaled by distance to nearest solid surface.

------------- Config File Boundary Information ( Zone 0 ) ---------------
+-----------------------------------------------------------------------+
|                        Marker Type|                        Marker Name|
+-----------------------------------------------------------------------+
|                         Euler wall|                               BC_3|
+-----------------------------------------------------------------------+
|                          Far-field|                               BC_1|
+-----------------------------------------------------------------------+
|                     Symmetry plane|                               BC_2|
+-----------------------------------------------------------------------+
Three dimensional problem.
60093 grid points.
326965 volume elements.
3 surface markers.
12530 boundary elements in index 0 (Marker = BC_1).
5746 boundary elements in index 1 (Marker = BC_2).
698 boundary elements in index 2 (Marker = BC_3).
326965 tetrahedra.

----------------------- Preprocessing computations ----------------------
Setting local point connectivity.
Checking the numerical grid orientation of the interior elements.
All volume elements are correctly orientend.
All surface elements are correctly orientend.
Identify edges and vertices.
Setting the bound control volume structure.
Volume of the computational grid: 63999.5.
  Info: Ignoring the following volume output fields/groups:
  SOLUTION
Volume output fields: COORDINATES
  Info: Ignoring the following screen output fields:
  RMS_DENSITY, RMS_MOMENTUM-X, RMS_MOMENTUM-Y, RMS_ENERGY, EFFICIENCY
Screen output fields: TIME_ITER, OUTER_ITER, INNER_ITER, CUR_TIME, TIME_STEP, WALL_TIME
  Info: Ignoring the following history output groups:
  RMS_RES, AERO_COEFF
History output group(s): ITER, TIME_DOMAIN, WALL_TIME
Warning: No (valid) fields chosen for convergence monitoring. Convergence monitoring inactive.
Warning: No (valid) fields chosen for time convergence monitoring. Time convergence monitoring inactive.

--------------------- Surface grid deformation (ZONE 0) -----------------
Performing the deformation of the surface grid.
Updating the surface coordinates from the input file.

------------------- Volumetric grid deformation (ZONE 0) ----------------
Performing the deformation of the volumetric grid.

WARNING: Convexity is not checked for 3D elements (issue #1171).


Completed in 9.779935 seconds on 1 core.

----------------------- Write deformed grid files -----------------------
|SU2 mesh                           |../aflr3/aflr3_CAPS.su2            |
|CSV file                           |surface_deformed.csv               |
|Tecplot binary                     |volume_deformed.szplt              |
|Tecplot binary surface             |surface_deformed.szplt             |
Adding any FFD information to the SU2 file.

------------------------- Finalize Solver -------------------------
Deleted CNumerics container.
Deleted CSolver container.
Deleted CGeometry container.
Deleted CSurfaceMovement class.
Deleted CVolumetricMovement class.
Deleted CConfig container.
Deleted COutput class.

------------------------- Exit Success (SU2_DEF) ------------------------


-------------------------------------------------------------------------
|    ___ _   _ ___                                                      |
|   / __| | | |_  )   Release 8.0.0 "Harrier"                           |
|   \__ \ |_| |/ /                                                      |
|   |___/\___//___|   Suite (Computational Fluid Dynamics Code)         |
|                                                                       |
-------------------------------------------------------------------------
| SU2 Project Website: <a href='https://su2code.github.io'>https://su2code.github.io</a>                        |
|                                                                       |
| The SU2 Project is maintained by the SU2 Foundation                   |
| (<a href='http://su2foundation.org'>http://su2foundation.org</a>)                                            |
-------------------------------------------------------------------------
| Copyright 2012-2023, SU2 Contributors                                 |
|                                                                       |
| SU2 is free software; you can redistribute it and/or                  |
| modify it under the terms of the GNU Lesser General Public            |
| License as published by the Free Software Foundation; either          |
| version 2.1 of the License, or (at your option) any later version.    |
|                                                                       |
| SU2 is distributed in the hope that it will be useful,                |
| but WITHOUT ANY WARRANTY; without even the implied warranty of        |
| MERCHANTABILITY or FITNESS FOR A PARTICULAR PURPOSE. See the GNU      |
| Lesser General Public License for more details.                       |
|                                                                       |
| You should have received a copy of the GNU Lesser General Public      |
| License along with SU2. If not, see &lt;<a href='http://www.gnu.org/licenses/'>http://www.gnu.org/licenses/</a>&gt;.   |
-------------------------------------------------------------------------

Parsing config file for zone 0

----------------- Physical Case Definition ( Zone 0 ) -------------------
Compressible Euler equations.
Mach number: 0.294118.
Angle of attack (AoA): 0 deg, and angle of sideslip (AoS): 0 deg.
No restart solution, use the values at infinity (freestream).
Dimensional simulation.
The reference area is 1 m^2.
The semi-span will be computed using the max y(3D) value.
The reference length is 1 m.
Reference origin for moment evaluation is (0, 0, 0).
Surface(s) where the force coefficients are evaluated: BC_3.

Surface(s) plotted in the output file: BC_3.
Surface(s) affected by the design variables: BC_3.
Input mesh file name: ../aflr3/aflr3_CAPS.su2

--------------- Space Numerical Integration ( Zone 0 ) ------------------
Roe (with entropy fix = 0.001) solver for the flow inviscid terms.
Standard Roe without low-dissipation function.
Second order integration in space, with slope limiter.
Venkatakrishnan slope-limiting method, with constant: 0.05.
The reference element size is: 1. 
Gradient for upwind reconstruction: inverse-distance weighted Least-Squares.
Gradient for viscous and source terms: inverse-distance weighted Least-Squares.

--------------- Time Numerical Integration  ( Zone 0 ) ------------------
Local time stepping (steady state simulation).
Euler implicit method for the flow equations.
FGMRES is used for solving the linear system.
Using a ILU(0) preconditioning.
Convergence criteria of the linear solver: 1e-06.
Max number of linear iterations: 10.
V Multigrid Cycle, with 2 multigrid levels.
Damping factor for the residual restriction: 0.75.
Damping factor for the correction prolongation: 0.75.
No CFL adaptation.
+-------------------------------------------+
|  MG Level| Presmooth|PostSmooth|CorrectSmo|
+-------------------------------------------+
|         0|         1|         0|         0|
|         1|         2|         0|         0|
|         2|         3|         0|         0|
+-------------------------------------------+
Courant-Friedrichs-Lewy number:       10

------------------ Convergence Criteria  ( Zone 0 ) ---------------------
Maximum number of solver subiterations: 3.
Begin convergence monitoring at iteration 5.
Residual minimum value: 1e-14.
Cauchy series min. value: 1e-10.
Number of Cauchy elements: 100.
Begin windowed time average at iteration 0.

-------------------- Output Information ( Zone 0 ) ----------------------
File writing frequency: 
+------------------------------------+
|                     File| Frequency|
+------------------------------------+
|                  RESTART|       250|
|              SURFACE_CSV|       250|
|                  TECPLOT|       250|
|          SURFACE_TECPLOT|       250|
+------------------------------------+
Writing the convergence history file every 1 inner iterations.
Writing the screen convergence history every 1 inner iterations.
The tabular file format is CSV (.csv).
Convergence history file name: history.
Forces breakdown file name: forces_breakdown_aeroelasticSimple_Displacement_SA.dat.
Surface file name: surface_flow_aeroelasticSimple_Displacement_SA.
Volume file name: flow_aeroelasticSimple_Displacement_SA.
Restart file name: restart_flow_aeroelasticSimple_Displacement_SA.dat.

------------- Config File Boundary Information ( Zone 0 ) ---------------
+-----------------------------------------------------------------------+
|                        Marker Type|                        Marker Name|
+-----------------------------------------------------------------------+
|                         Euler wall|                               BC_3|
+-----------------------------------------------------------------------+
|                          Far-field|                               BC_1|
+-----------------------------------------------------------------------+
|                     Symmetry plane|                               BC_2|
+-----------------------------------------------------------------------+

-------------------- Output Preprocessing ( Zone 0 ) --------------------

WARNING: SURFACE_PRESSURE_DROP can only be computed for at least 2 surfaces (outlet, inlet, ...)

Screen output fields: TIME_ITER, OUTER_ITER, INNER_ITER, CUR_TIME, TIME_STEP, WALL_TIME, RMS_DENSITY, RMS_MOMENTUM-X, RMS_MOMENTUM-Y, RMS_ENERGY, EFFICIENCY
History output group(s): ITER, TIME_DOMAIN, WALL_TIME, RMS_RES, AERO_COEFF
Convergence field(s): RMS_DENSITY
Warning: No (valid) fields chosen for time convergence monitoring. Time convergence monitoring inactive.
Volume output fields: COORDINATES, SOLUTION, PRIMITIVE

------------------- Geometry Preprocessing ( Zone 0 ) -------------------
Three dimensional problem.
60093 grid points.
326965 volume elements.
3 surface markers.
12530 boundary elements in index 0 (Marker = BC_1).
5746 boundary elements in index 1 (Marker = BC_2).
698 boundary elements in index 2 (Marker = BC_3).
326965 tetrahedra.
Setting point connectivity.
Renumbering points (Reverse Cuthill McKee Ordering).
Recomputing point connectivity.
Setting element connectivity.
Checking the numerical grid orientation.
There has been a re-orientation of 3 TETRAHEDRON volume elements.
All surface elements are correctly orientend.
Identifying edges and vertices.
Setting the control volume structure.
Volume of the computational grid: 63997.8.
Searching for the closest normal neighbors to the surfaces.
Storing a mapping from global to local point index.
Compute the surface curvature.
Max K: 83.9101. Mean K: 0.902367. Standard deviation K: 4.47382.
Checking for periodicity.
Computing mesh quality statistics for the dual control volumes.
+--------------------------------------------------------------+
|           Mesh Quality Metric|        Minimum|        Maximum|
+--------------------------------------------------------------+
|    Orthogonality Angle (deg.)|        42.5942|        86.8036|
|     CV Face Area Aspect Ratio|        1.05478|        23.5105|
|           CV Sub-Volume Ratio|              1|        134.901|
+--------------------------------------------------------------+
Setting the multigrid structure.
+-------------------------------------------+
|  MG Level|       CVs|Aggl. Rate|       CFL|
+-------------------------------------------+
|         0|     60093|    1/1.00|        10|
|         1|     10214|    1/5.88|     8.309|
|         2|      1799|    1/5.68|   6.98637|
+-------------------------------------------+
Finding max control volume width.
Semi-span length = 3.89892 m.
Wetted area = 11.6151 m^2.
Area projection in the x-plane = 2.90002 m^2, y-plane = 1.28883 m^2, z-plane = 4.27937 m^2.
Max. coordinate in the x-direction = 2.53729 m, y-direction = 3.89892 m, z-direction = 0.526515 m.
Min. coordinate in the x-direction = 0.000170858 m, y-direction = -2.86329e-18 m, z-direction = -0.706552 m.
Checking if Euler &amp; Symmetry markers are straight/plane:
Boundary marker BC_3 is NOT a single plane.
Boundary marker BC_2 is a single plane.
Computing wall distances.

-------------------- Solver Preprocessing ( Zone 0 ) --------------------
Inviscid flow: Computing density based on free-stream
temperature and pressure using the ideal gas law.
Force coefficients computed using free-stream values.

-- Models:
+------------------------------------------------------------------------------+
|          Viscosity Model|        Conductivity Model|              Fluid Model|
+------------------------------------------------------------------------------+
|                        -|                         -|             STANDARD_AIR|
+------------------------------------------------------------------------------+
-- Fluid properties:
+------------------------------------------------------------------------------+
|                  Name|    Dim. value|    Ref. value|      Unit|Non-dim. value|
+------------------------------------------------------------------------------+
|          Gas Constant|       287.058|             1|  N.m/kg.K|       287.058|
|      Spec. Heat Ratio|             -|             -|         -|           1.4|
+------------------------------------------------------------------------------+
-- Initial and free-stream conditions:
+------------------------------------------------------------------------------+
|                  Name|    Dim. value|    Ref. value|      Unit|Non-dim. value|
+------------------------------------------------------------------------------+
|       Static Pressure|        101325|             1|        Pa|        101325|
|               Density|       1.22498|             1|    kg/m^3|       1.22498|
|           Temperature|        288.15|             1|         K|        288.15|
|          Total Energy|        211798|             1|   m^2/s^2|        211798|
|            Velocity-X|       100.087|             1|       m/s|       100.087|
|            Velocity-Y|             0|             1|       m/s|             0|
|            Velocity-Z|             0|             1|       m/s|             0|
|    Velocity Magnitude|       100.087|             1|       m/s|       100.087|
+------------------------------------------------------------------------------+
|           Mach Number|             -|             -|         -|      0.294118|
+------------------------------------------------------------------------------+
Initialize Jacobian structure (Euler). MG level: 0.
Initialize Jacobian structure (Euler). MG level: 1.
Initialize Jacobian structure (Euler). MG level: 2.

------------------- Numerics Preprocessing ( Zone 0 ) -------------------

----------------- Integration Preprocessing ( Zone 0 ) ------------------

------------------- Iteration Preprocessing ( Zone 0 ) ------------------
Euler/Navier-Stokes/RANS fluid iteration.

------------------------------ Begin Solver -----------------------------

Simulation Run using the Single-zone Driver
WARNING: SU2 was not compiled for an AVX-capable architecture. Performance could be better,
         see <a href='https://su2code.github.io/docs_v7/Build-SU2-Linux-MacOS/#compiler-optimizations'>https://su2code.github.io/docs_v7/Build-SU2-Linux-MacOS/#compiler-optimizations</a>
WARNING: SU2 was not compiled for an AVX-capable architecture. Performance could be better,
         see <a href='https://su2code.github.io/docs_v7/Build-SU2-Linux-MacOS/#compiler-optimizations'>https://su2code.github.io/docs_v7/Build-SU2-Linux-MacOS/#compiler-optimizations</a>
WARNING: SU2 was not compiled for an AVX-capable architecture. Performance could be better,
         see <a href='https://su2code.github.io/docs_v7/Build-SU2-Linux-MacOS/#compiler-optimizations'>https://su2code.github.io/docs_v7/Build-SU2-Linux-MacOS/#compiler-optimizations</a>
+----------------------------------------------------------------------------------------------------------------------------------------------+
|   Time_Iter|  Outer_Iter|  Inner_Iter|    Cur_Time|   Time_Step|   Time(sec)|    rms[Rho]|   rms[RhoU]|   rms[RhoV]|   rms[RhoE]|        CEff|
+----------------------------------------------------------------------------------------------------------------------------------------------+
|           0|           0|           0|  0.0000e+00|  0.0000e+00|  9.9354e-01|   -0.685108|    1.753422|    1.256019|    4.783998|    0.049188|
|           0|           0|           1|  0.0000e+00|  0.0000e+00|  9.8857e-01|   -1.120721|    1.479573|    1.113372|    4.351408|    0.028658|
|           0|           0|           2|  0.0000e+00|  0.0000e+00|  9.8363e-01|   -1.141622|    1.261036|    0.931565|    4.324727|    0.031964|

----------------------------- Solver Exit -------------------------------

Maximum number of iterations reached (ITER = 3) before convergence.
+-----------------------------------------------------------------------+
|      Convergence Field     |     Value    |   Criterion  |  Converged |
+-----------------------------------------------------------------------+
|                    rms[Rho]|      -1.14162|         &lt; -14|          No|
+-----------------------------------------------------------------------+
-------------------------------------------------------------------------
+-----------------------------------------------------------------------+
|        File Writing Summary       |              Filename             |
+-----------------------------------------------------------------------+
|SU2 binary restart                 |restart_flow_aeroelasticSimple_Displacement_SA.dat|

Writing the forces breakdown file (forces_breakdown_aeroelasticSimple_Displacement_SA.dat).
|CSV file                           |surface_flow_aeroelasticSimple_Displacement_SA.csv|

Writing the forces breakdown file (forces_breakdown_aeroelasticSimple_Displacement_SA.dat).
|Tecplot binary                     |flow_aeroelasticSimple_Displacement_SA.szplt|

Writing the forces breakdown file (forces_breakdown_aeroelasticSimple_Displacement_SA.dat).
|Tecplot binary surface             |surface_flow_aeroelasticSimple_Displacement_SA.szplt|

Writing the forces breakdown file (forces_breakdown_aeroelasticSimple_Displacement_SA.dat).
+-----------------------------------------------------------------------+

--------------------------- Finalizing Solver ---------------------------
Deleted CNumerics container.
Deleted CIntegration container.
Deleted CSolver container.
Deleted CIteration container.
Deleted CInterface container.
Deleted CGeometry container.
Deleted CFreeFormDefBox class.
Deleted CSurfaceMovement class.
Deleted CVolumetricMovement class.
Deleted CConfig container.
Deleted nInst container.
Deleted COutput class.
-------------------------------------------------------------------------

------------------------- Exit Success (SU2_CFD) ------------------------


Running PostAnalysis ...... su2

real	0m24.357s
user	0m24.081s
sys	0m1.502s
+ status=0
+ set +x

=================================================
CAPS verification (using pyCAPS) case aeroelasticSimple_Displacement_SU2_and_Astros.py passed (as expected)
=================================================


=================================================
+ echo 'aeroelasticSimple_Iterative_SU2_and_Astros.py test;'
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESP126/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
aeroelasticSimple_Iterative_SU2_and_Astros.py test;
+ python -u aeroelasticSimple_Iterative_SU2_and_Astros.py -outLevel=0
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESP126/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt

Running PreAnalysis ...... su2
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 3
	Name = Farfield, index = 1
	Name = SymmPlane, index = 2
	Name = Skin, index = 3
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 0
 
AFLR2    : ---------------------------------------
AFLR2    : AFLR2 LIBRARY
AFLR2    : ADVANCING-FRONT/LOCAL-RECONNECTION
AFLR2    : TRIA/QUAD GRID GENERATOR
AFLR2    : Version Number 9.18.1
AFLR2    : Version Date   06/11/24 @ 05:52PM
AFLR2    : Compile OS     Darwin 23.5.0 arm64
AFLR2    : Compile Date   06/11/24 @ 05:52PM
AFLR2    : Copyright 1994-2021, D.L. Marcum
AFLR2    : ---------------------------------------
 
AFLR4    : ---------------------------------------
AFLR4    : AFLR4 LIBRARY
AFLR4    : ADVANCING-FRONT/LOCAL-RECONNECTION
AFLR4    : TRIA/QUAD SURFACE GRID GENERATOR
AFLR4    : Version Number 11.5.15
AFLR4    : Version Date   07/19/24 @ 07:04PM
AFLR4    : Compile OS     Darwin 23.5.0 arm64
AFLR4    : Compile Date   07/19/24 @ 07:06PM
AFLR4    : Copyright 1994-2021, D.L. Marcum
AFLR4    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.8.1
EGADS    : ---------------------------------------

EGADS    : EGADS CAD Geometry Setup

EGADS    : Model has 1 Active Bodies

EGADS    : Body 0 is a SolidBody
EGADS    : Body 0 has 1 Shells
EGADS    : Body 0 has 9 Faces
EGADS    : Body 0 has 18 Edges
EGADS    : Body 0 has 10 Loops
EGADS    : Body 0 has 12 Nodes

EGADS    : Check Grid BCs

EGADS    : Grid BCs are OK

EGADS    : Face Neighbor-Faces Information

EGADS    : QC  = Face Quad Combination Flag
EGADS    : IER = Face Isolated Edge Refinement Flag
EGADS    : ER  = Face Edge Refinement Factor
EGADS    :       Not applicable for Faces with a FarField Grid BC.
EGADS    : SF  = Face Scale Factor
EGADS    :       Not applicable for Faces with a FarField Grid BC.

EGADS    :   Face          Body    QC   IER       ER    Scale   Neighbor
EGADS    :     ID  Active    ID  Flag  Flag   Weight   Factor   Faces
EGADS    :      1     Yes     0     0     1        0        1   2 3 4 5
EGADS    :      2     Yes     0     0     1        0        1   1 3 5 6
EGADS    :      3     Yes     0     0     1        0        1   1 2 4 6 7 8
EGADS    :      4     Yes     0     0     1        0        1   1 3 5 6
EGADS    :      5     Yes     0     0     1        0        1   1 2 4 6
EGADS    :      6     Yes     0     0     1        0        1   2 3 4 5
EGADS    :      7     Yes     0     0     1        0        1   3 8 9
EGADS    :      8     Yes     0     0     1        0        1   3 7 9
EGADS    :      9     Yes     0     0     1        0        1   7 8

EGADS    : Face Edges Information

EGADS    :   Face   Edges
EGADS    :      1   1 2 -3 -4
EGADS    :      2   5 6 -7 -1
EGADS    :      3   -2 7 9 -8 -10 -11
EGADS    :      4   -12 3 8 -13
EGADS    :      5   4 12 -14 -5
EGADS    :      6   -6 14 13 -9
EGADS    :      7   15 10 -17 -16
EGADS    :      8   17 11 -15 -18
EGADS    :      9   16 18

EGADS    : Face Loops Information

EGADS    :   Face   Loops
EGADS    :      1   1
EGADS    :      2   2
EGADS    :      3   3 4
EGADS    :      4   5
EGADS    :      5   6
EGADS    :      6   7
EGADS    :      7   8
EGADS    :      8   9
EGADS    :      9   10

EGADS    : Loop Edges Information

EGADS    :   Loop  Active   Edges
EGADS    :      1     Yes   1 2 -3 -4
EGADS    :      2     Yes   5 6 -7 -1
EGADS    :      3     Yes   -2 7 9 -8
EGADS    :      4     Yes   -10 -11
EGADS    :      5     Yes   -12 3 8 -13
EGADS    :      6     Yes   4 12 -14 -5
EGADS    :      7     Yes   -6 14 13 -9
EGADS    :      8     Yes   15 10 -17 -16
EGADS    :      9     Yes   17 11 -15 -18
EGADS    :     10     Yes   16 18

EGADS    : Edge Node, Scale Factor, and Neighbor-Faces Information

EGADS    : ESF = Edge Scale Factor
EGADS    :       Not applicable for DEGENERATE Edges or Edges with a FarField
EGADS    :       Grid BC Neighbor Face.

EGADS    :                                             Neighbor
EGADS    :   Edge  Body  Active Node1 Node2      ESF   Faces
EGADS    :      1     0     Yes     2     1        1   1 2
EGADS    :      2     0     Yes     1     3        1   1 3
EGADS    :      3     0     Yes     4     3        1   1 4
EGADS    :      4     0     Yes     2     4        1   1 5
EGADS    :      5     0     Yes     2     5        1   2 5
EGADS    :      6     0     Yes     5     6        1   2 6
EGADS    :      7     0     Yes     1     6        1   2 3
EGADS    :      8     0     Yes     3     7        1   3 4
EGADS    :      9     0     Yes     6     7        1   3 6
EGADS    :     10     0     Yes     8     9        1   3 7
EGADS    :     11     0     Yes     9     8        1   3 8
EGADS    :     12     0     Yes     4    10        1   4 5
EGADS    :     13     0     Yes    10     7        1   4 6
EGADS    :     14     0     Yes     5    10        1   5 6
EGADS    :     15     0     Yes    11     8        1   7 8
EGADS    :     16     0     Yes    11    12        1   7 9
EGADS    :     17     0     Yes    12     9        1   7 8
EGADS    :     18     0     Yes    12    11        1   8 9

EGADS    : Node Information

EGADS    :   Node  Active      Coordinates
EGADS    :      1     Yes                0                0                0
EGADS    :      2     Yes                0               40                0
EGADS    :      3     Yes                0                0               20
EGADS    :      4     Yes                0               40               20
EGADS    :      5     Yes               20               40                0
EGADS    :      6     Yes               20                0                0
EGADS    :      7     Yes               20                0               20
EGADS    :      8     Yes       1.61374306                0                0
EGADS    :      9     Yes                0                0                0
EGADS    :     10     Yes               20               40               20
EGADS    :     11     Yes       2.53650745       3.87298335      0.334116517
EGADS    :     12     Yes       1.57194608       3.87298335      0.249728332

EGADS    : Face and Edge Match Information

EGADS    : No Face Matches Found

AFLR4    : Surface Mesh Spacing Setup

AFLR4    : Max Bounding Box Length     = 40
AFLR4    : Min Bounding Box Length     = 40
AFLR4    : Max Ref Bounding Box Length = 40
AFLR4    : Min Ref Bounding Box Length = 40
AFLR4    : Reference Length            = 1.61374
AFLR4    : BL Thickness                = 0
AFLR4    : Abs Min Surf Spacing        = 0.00403436
AFLR4    : Min Surf Spacing            = 0.161374
AFLR4    : Max Surf Spacing            = 1.21031
AFLR4    : Global Scale Factor         = 2

AFLR4    : Geometry Definition Information

AFLR4    : Definition              Definition   Composite             Grid BC
AFLR4    :         ID                    Type          ID                Type
AFLR4    :          0     glue-only composite           -                   -
AFLR4    :          1            CAD geometry           0            STD w/BL
AFLR4    :          2            CAD geometry           0            STD w/BL
AFLR4    :          3            CAD geometry           0            STD w/BL
AFLR4    :          4            CAD geometry           0            STD w/BL
AFLR4    :          5            CAD geometry           0            STD w/BL
AFLR4    :          6            CAD geometry           0            STD w/BL
AFLR4    :          7            CAD geometry           0            STD w/BL
AFLR4    :          8            CAD geometry           0            STD w/BL
AFLR4    :          9            CAD geometry           0            STD w/BL

AFLR4    : Define CAD surface definition 1
AFLR4    : Define CAD surface definition 2
AFLR4    : Define CAD surface definition 3
AFLR4    : Define CAD surface definition 4
AFLR4    : Define CAD surface definition 5
AFLR4    : Define CAD surface definition 6
AFLR4    : Define CAD surface definition 7
AFLR4    : Define CAD surface definition 8
AFLR4    : Define CAD surface definition 9

AFLR4    : Surface Grid Generation

AFLR4    : Generate optimal mesh on surface definition 1
AFLR2    : Nodes, Trias,Quads=       376       682         0
AFLR4    : Nodes, Trias,Quads=       381       692         0

AFLR4    : Generate optimal mesh on surface definition 2
AFLR2    : Nodes, Trias,Quads=       374       678         0
AFLR4    : Nodes, Trias,Quads=       380       690         0

AFLR4    : Generate optimal mesh on surface definition 3
AFLR2    : Nodes, Trias,Quads=       927      1777         0
AFLR4    : Nodes, Trias,Quads=       821      1565         0

AFLR4    : Generate optimal mesh on surface definition 4
AFLR2    : Nodes, Trias,Quads=       376       682         0
AFLR4    : Nodes, Trias,Quads=       380       690         0

AFLR4    : Generate optimal mesh on surface definition 5
AFLR2    : Nodes, Trias,Quads=       374       678         0
AFLR4    : Nodes, Trias,Quads=       380       690         0

AFLR4    : Generate optimal mesh on surface definition 6
AFLR2    : Nodes, Trias,Quads=       376       682         0
AFLR4    : Nodes, Trias,Quads=       378       686         0

AFLR4    : Generate optimal mesh on surface definition 7
AFLR2    : Nodes, Trias,Quads=        63        96         0
AFLR4    : Nodes, Trias,Quads=        55        80         0

AFLR4    : Generate optimal mesh on surface definition 8
AFLR2    : Nodes, Trias,Quads=        64        96         0
AFLR4    : Nodes, Trias,Quads=        57        82         0

AFLR4    : Generate optimal mesh on surface definition 9
AFLR2    : Nodes, Trias,Quads=        11        13         0
AFLR4    : Nodes, Trias,Quads=         7         5         0

DGEOM    : Add surface definitions to composite definition 0
DGEOM    : Glue composite surface definition 0
DGEOM    : Nodes,Faces,BEdges=      2592      5180       482

AFLR4    : Curvature BG Surface Grid Generation

AFLR4    : Nodes, Faces      =      2592      5180

AFLR4    : Surface Grid Generation

AFLR4    : Generate optimal mesh on surface definition 1
AFLR2    : Nodes, Trias,Quads=       385       700         0
AFLR4    : Nodes, Trias,Quads=       380       690         0

AFLR4    : Generate optimal mesh on surface definition 2
AFLR2    : Nodes, Trias,Quads=       385       700         0
AFLR4    : Nodes, Trias,Quads=       381       692         0

AFLR4    : Generate optimal mesh on surface definition 3
AFLR2    : Nodes, Trias,Quads=      1009      1939         0
AFLR4    : Nodes, Trias,Quads=       953      1827         0

AFLR4    : Generate optimal mesh on surface definition 4
AFLR2    : Nodes, Trias,Quads=       383       696         0
AFLR4    : Nodes, Trias,Quads=       378       686         0

AFLR4    : Generate optimal mesh on surface definition 5
AFLR2    : Nodes, Trias,Quads=       383       696         0
AFLR4    : Nodes, Trias,Quads=       382       694         0

AFLR4    : Generate optimal mesh on surface definition 6
AFLR2    : Nodes, Trias,Quads=       381       692         0
AFLR4    : Nodes, Trias,Quads=       380       690         0

AFLR4    : Generate optimal mesh on surface definition 7
AFLR2    : Nodes, Trias,Quads=        74       115         0
AFLR4    : Nodes, Trias,Quads=        65        97         0

AFLR4    : Generate optimal mesh on surface definition 8
AFLR2    : Nodes, Trias,Quads=        75       116         0
AFLR4    : Nodes, Trias,Quads=        63        92         0

AFLR4    : Generate optimal mesh on surface definition 9
AFLR2    : Nodes, Trias,Quads=        12        14         0
AFLR4    : Nodes, Trias,Quads=         8         6         0

DGEOM    : Add surface definitions to composite definition 0
DGEOM    : Glue composite surface definition 0
DGEOM    : Nodes,Faces,BEdges=      2739      5474       490

OVERALL  : CPU Time          =     0.061   seconds
Body 1 (of 1)
Number of nodes    = 2739
Number of elements = 5474
Number of triangle elements      = 5474
Number of quadrilateral elements = 0
----------------------------
Total number of nodes    = 2739
Total number of elements = 5474
Total number of triangle elements      = 5474
Total number of quadrilateral elements = 0
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 0
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 3
	Name = Farfield, index = 1
	Name = SymmPlane, index = 2
	Name = Skin, index = 3
Getting volume mesh
 
AFLR2    : ---------------------------------------
AFLR2    : AFLR2 LIBRARY
AFLR2    : ADVANCING-FRONT/LOCAL-RECONNECTION
AFLR2    : TRIA/QUAD GRID GENERATOR
AFLR2    : Version Number 9.18.1
AFLR2    : Version Date   06/11/24 @ 05:52PM
AFLR2    : Compile OS     Darwin 23.5.0 arm64
AFLR2    : Compile Date   06/11/24 @ 05:52PM
AFLR2    : Copyright 1994-2021, D.L. Marcum
AFLR2    : ---------------------------------------
 
AFLR4    : ---------------------------------------
AFLR4    : AFLR4 LIBRARY
AFLR4    : ADVANCING-FRONT/LOCAL-RECONNECTION
AFLR4    : TRIA/QUAD SURFACE GRID GENERATOR
AFLR4    : Version Number 11.5.15
AFLR4    : Version Date   07/19/24 @ 07:04PM
AFLR4    : Compile OS     Darwin 23.5.0 arm64
AFLR4    : Compile Date   07/19/24 @ 07:06PM
AFLR4    : Copyright 1994-2021, D.L. Marcum
AFLR4    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.8.1
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.8.1
EGADS    : ---------------------------------------
Volume mesh:
	Number of nodes          = 11301
	Number of elements       = 64025
	Number of triangles      = 5474
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 58551
	Number of pyramids       = 0
	Number of prisms         = 0
	Number of hexahedrals    = 0

Writing SU2 file ....
Finished writing SU2 file

Getting CFD boundary conditions
	Boundary condition name - Farfield
	Boundary condition name - Skin
	Boundary condition name - SymmPlane
	Done getting CFD boundary conditions
Writing SU2 data transfer files
Writing SU2 Motion File - aeroelasticSimple_Iterative_motion.dat
Warning: The su2 cfg file will be overwritten!
Write SU2 configuration file for version "Harrier (8.0.1)"


Running SU2......

-------------------------------------------------------------------------
|    ___ _   _ ___                                                      |
|   / __| | | |_  )   Release 8.0.0 "Harrier"                           |
|   \__ \ |_| |/ /                                                      |
|   |___/\___//___|   Suite (Computational Fluid Dynamics Code)         |
|                                                                       |
-------------------------------------------------------------------------
| SU2 Project Website: <a href='https://su2code.github.io'>https://su2code.github.io</a>                        |
|                                                                       |
| The SU2 Project is maintained by the SU2 Foundation                   |
| (<a href='http://su2foundation.org'>http://su2foundation.org</a>)                                            |
-------------------------------------------------------------------------
| Copyright 2012-2023, SU2 Contributors                                 |
|                                                                       |
| SU2 is free software; you can redistribute it and/or                  |
| modify it under the terms of the GNU Lesser General Public            |
| License as published by the Free Software Foundation; either          |
| version 2.1 of the License, or (at your option) any later version.    |
|                                                                       |
| SU2 is distributed in the hope that it will be useful,                |
| but WITHOUT ANY WARRANTY; without even the implied warranty of        |
| MERCHANTABILITY or FITNESS FOR A PARTICULAR PURPOSE. See the GNU      |
| Lesser General Public License for more details.                       |
|                                                                       |
| You should have received a copy of the GNU Lesser General Public      |
| License along with SU2. If not, see &lt;<a href='http://www.gnu.org/licenses/'>http://www.gnu.org/licenses/</a>&gt;.   |
-------------------------------------------------------------------------

Parsing config file for zone 0

----------------- Physical Case Definition ( Zone 0 ) -------------------
Compressible Euler equations.
Mach number: 0.294118.
Angle of attack (AoA): 0 deg, and angle of sideslip (AoS): 0 deg.
No restart solution, use the values at infinity (freestream).
Dimensional simulation.
The reference area is 1 m^2.
The semi-span will be computed using the max y(3D) value.
The reference length is 1 m.
Reference origin for moment evaluation is (0, 0, 0).
Surface(s) where the force coefficients are evaluated: BC_3.

Surface(s) plotted in the output file: BC_3.
Surface(s) affected by the design variables: BC_3.
Input mesh file name: ../aflr3/aflr3_CAPS.su2

--------------- Space Numerical Integration ( Zone 0 ) ------------------
Roe (with entropy fix = 0.001) solver for the flow inviscid terms.
Standard Roe without low-dissipation function.
Second order integration in space, with slope limiter.
Venkatakrishnan slope-limiting method, with constant: 0.05.
The reference element size is: 1. 
Gradient for upwind reconstruction: inverse-distance weighted Least-Squares.
Gradient for viscous and source terms: inverse-distance weighted Least-Squares.

--------------- Time Numerical Integration  ( Zone 0 ) ------------------
Local time stepping (steady state simulation).
Euler implicit method for the flow equations.
FGMRES is used for solving the linear system.
Using a ILU(0) preconditioning.
Convergence criteria of the linear solver: 1e-06.
Max number of linear iterations: 10.
V Multigrid Cycle, with 2 multigrid levels.
Damping factor for the residual restriction: 0.75.
Damping factor for the correction prolongation: 0.75.
No CFL adaptation.
+-------------------------------------------+
|  MG Level| Presmooth|PostSmooth|CorrectSmo|
+-------------------------------------------+
|         0|         1|         0|         0|
|         1|         2|         0|         0|
|         2|         3|         0|         0|
+-------------------------------------------+
Courant-Friedrichs-Lewy number:       10

------------------ Convergence Criteria  ( Zone 0 ) ---------------------
Maximum number of solver subiterations: 3.
Begin convergence monitoring at iteration 5.
Residual minimum value: 1e-14.
Cauchy series min. value: 1e-10.
Number of Cauchy elements: 100.
Begin windowed time average at iteration 0.

-------------------- Output Information ( Zone 0 ) ----------------------
File writing frequency: 
+------------------------------------+
|                     File| Frequency|
+------------------------------------+
|                  RESTART|       250|
|              SURFACE_CSV|       250|
|                  TECPLOT|       250|
|          SURFACE_TECPLOT|       250|
+------------------------------------+
Writing the convergence history file every 1 inner iterations.
Writing the screen convergence history every 1 inner iterations.
The tabular file format is CSV (.csv).
Convergence history file name: history.
Forces breakdown file name: forces_breakdown_aeroelasticSimple_Iterative.dat.
Surface file name: surface_flow_aeroelasticSimple_Iterative.
Volume file name: flow_aeroelasticSimple_Iterative.
Restart file name: restart_flow_aeroelasticSimple_Iterative.dat.

------------- Config File Boundary Information ( Zone 0 ) ---------------
+-----------------------------------------------------------------------+
|                        Marker Type|                        Marker Name|
+-----------------------------------------------------------------------+
|                         Euler wall|                               BC_3|
+-----------------------------------------------------------------------+
|                          Far-field|                               BC_1|
+-----------------------------------------------------------------------+
|                     Symmetry plane|                               BC_2|
+-----------------------------------------------------------------------+

-------------------- Output Preprocessing ( Zone 0 ) --------------------

WARNING: SURFACE_PRESSURE_DROP can only be computed for at least 2 surfaces (outlet, inlet, ...)

Screen output fields: TIME_ITER, OUTER_ITER, INNER_ITER, CUR_TIME, TIME_STEP, WALL_TIME, RMS_DENSITY, RMS_MOMENTUM-X, RMS_MOMENTUM-Y, RMS_ENERGY, EFFICIENCY
History output group(s): ITER, TIME_DOMAIN, WALL_TIME, RMS_RES, AERO_COEFF
Convergence field(s): RMS_DENSITY
Warning: No (valid) fields chosen for time convergence monitoring. Time convergence monitoring inactive.
Volume output fields: COORDINATES, SOLUTION, PRIMITIVE

------------------- Geometry Preprocessing ( Zone 0 ) -------------------
Three dimensional problem.
11301 grid points.
58551 volume elements.
3 surface markers.
3452 boundary elements in index 0 (Marker = BC_1).
1827 boundary elements in index 1 (Marker = BC_2).
195 boundary elements in index 2 (Marker = BC_3).
58551 tetrahedra.
Setting point connectivity.
Renumbering points (Reverse Cuthill McKee Ordering).
Recomputing point connectivity.
Setting element connectivity.
Checking the numerical grid orientation.
All volume elements are correctly orientend.
All surface elements are correctly orientend.
Identifying edges and vertices.
Setting the control volume structure.
Volume of the computational grid: 63999.5.
Searching for the closest normal neighbors to the surfaces.
Storing a mapping from global to local point index.
Compute the surface curvature.
Max K: 47.1143. Mean K: 0.755059. Standard deviation K: 3.51124.
Checking for periodicity.
Computing mesh quality statistics for the dual control volumes.
+--------------------------------------------------------------+
|           Mesh Quality Metric|        Minimum|        Maximum|
+--------------------------------------------------------------+
|    Orthogonality Angle (deg.)|        54.7348|        85.4032|
|     CV Face Area Aspect Ratio|        1.05389|        21.5536|
|           CV Sub-Volume Ratio|              1|        13.9349|
+--------------------------------------------------------------+
Setting the multigrid structure.
+-------------------------------------------+
|  MG Level|       CVs|Aggl. Rate|       CFL|
+-------------------------------------------+
|         0|     11301|    1/1.00|        10|
|         1|      2021|    1/5.59|   8.45099|
|         2|       414|    1/4.88|   7.47269|
+-------------------------------------------+
Finding max control volume width.
Semi-span length = 3.87298 m.
Wetted area = 8.08979 m^2.
Area projection in the x-plane = 0.572014 m^2, y-plane = 0.261888 m^2, z-plane = 3.84035 m^2.
Max. coordinate in the x-direction = 2.53651 m, y-direction = 3.87298 m, z-direction = 0.380358 m.
Min. coordinate in the x-direction = 0 m, y-direction = -2.8602e-18 m, z-direction = -0.0467106 m.
Checking if Euler &amp; Symmetry markers are straight/plane:
Boundary marker BC_3 is NOT a single plane.
Boundary marker BC_2 is a single plane.
Computing wall distances.

-------------------- Solver Preprocessing ( Zone 0 ) --------------------
Inviscid flow: Computing density based on free-stream
temperature and pressure using the ideal gas law.
Force coefficients computed using free-stream values.

-- Models:
+------------------------------------------------------------------------------+
|          Viscosity Model|        Conductivity Model|              Fluid Model|
+------------------------------------------------------------------------------+
|                        -|                         -|             STANDARD_AIR|
+------------------------------------------------------------------------------+
-- Fluid properties:
+------------------------------------------------------------------------------+
|                  Name|    Dim. value|    Ref. value|      Unit|Non-dim. value|
+------------------------------------------------------------------------------+
|          Gas Constant|       287.058|             1|  N.m/kg.K|       287.058|
|      Spec. Heat Ratio|             -|             -|         -|           1.4|
+------------------------------------------------------------------------------+
-- Initial and free-stream conditions:
+------------------------------------------------------------------------------+
|                  Name|    Dim. value|    Ref. value|      Unit|Non-dim. value|
+------------------------------------------------------------------------------+
|       Static Pressure|        101325|             1|        Pa|        101325|
|               Density|       1.22498|             1|    kg/m^3|       1.22498|
|           Temperature|        288.15|             1|         K|        288.15|
|          Total Energy|        211798|             1|   m^2/s^2|        211798|
|            Velocity-X|       100.087|             1|       m/s|       100.087|
|            Velocity-Y|             0|             1|       m/s|             0|
|            Velocity-Z|             0|             1|       m/s|             0|
|    Velocity Magnitude|       100.087|             1|       m/s|       100.087|
+------------------------------------------------------------------------------+
|           Mach Number|             -|             -|         -|      0.294118|
+------------------------------------------------------------------------------+
Initialize Jacobian structure (Euler). MG level: 0.
Initialize Jacobian structure (Euler). MG level: 1.
Initialize Jacobian structure (Euler). MG level: 2.

------------------- Numerics Preprocessing ( Zone 0 ) -------------------

----------------- Integration Preprocessing ( Zone 0 ) ------------------

------------------- Iteration Preprocessing ( Zone 0 ) ------------------
Euler/Navier-Stokes/RANS fluid iteration.

------------------------------ Begin Solver -----------------------------

Simulation Run using the Single-zone Driver
WARNING: SU2 was not compiled for an AVX-capable architecture. Performance could be better,
         see <a href='https://su2code.github.io/docs_v7/Build-SU2-Linux-MacOS/#compiler-optimizations'>https://su2code.github.io/docs_v7/Build-SU2-Linux-MacOS/#compiler-optimizations</a>
WARNING: SU2 was not compiled for an AVX-capable architecture. Performance could be better,
         see <a href='https://su2code.github.io/docs_v7/Build-SU2-Linux-MacOS/#compiler-optimizations'>https://su2code.github.io/docs_v7/Build-SU2-Linux-MacOS/#compiler-optimizations</a>
WARNING: SU2 was not compiled for an AVX-capable architecture. Performance could be better,
         see <a href='https://su2code.github.io/docs_v7/Build-SU2-Linux-MacOS/#compiler-optimizations'>https://su2code.github.io/docs_v7/Build-SU2-Linux-MacOS/#compiler-optimizations</a>
+----------------------------------------------------------------------------------------------------------------------------------------------+
|   Time_Iter|  Outer_Iter|  Inner_Iter|    Cur_Time|   Time_Step|   Time(sec)|    rms[Rho]|   rms[RhoU]|   rms[RhoV]|   rms[RhoE]|        CEff|
+----------------------------------------------------------------------------------------------------------------------------------------------+
|           0|           0|           0|  0.0000e+00|  0.0000e+00|  1.6740e-01|   -0.790402|    1.509543|    1.185099|    4.678704|   -1.072828|
|           0|           0|           1|  0.0000e+00|  0.0000e+00|  1.6616e-01|   -1.125423|    1.402824|    1.016209|    4.328795|   -0.842279|
|           0|           0|           2|  0.0000e+00|  0.0000e+00|  1.6537e-01|   -1.188494|    1.266186|    0.868459|    4.264282|   -0.355290|

----------------------------- Solver Exit -------------------------------

Maximum number of iterations reached (ITER = 3) before convergence.
+-----------------------------------------------------------------------+
|      Convergence Field     |     Value    |   Criterion  |  Converged |
+-----------------------------------------------------------------------+
|                    rms[Rho]|      -1.18849|         &lt; -14|          No|
+-----------------------------------------------------------------------+
-------------------------------------------------------------------------
+-----------------------------------------------------------------------+
|        File Writing Summary       |              Filename             |
+-----------------------------------------------------------------------+
|SU2 binary restart                 |restart_flow_aeroelasticSimple_Iterative.dat|

Writing the forces breakdown file (forces_breakdown_aeroelasticSimple_Iterative.dat).
|CSV file                           |surface_flow_aeroelasticSimple_Iterative.csv|

Writing the forces breakdown file (forces_breakdown_aeroelasticSimple_Iterative.dat).
|Tecplot binary                     |flow_aeroelasticSimple_Iterative.szplt|

Writing the forces breakdown file (forces_breakdown_aeroelasticSimple_Iterative.dat).
|Tecplot binary surface             |surface_flow_aeroelasticSimple_Iterative.szplt|

Writing the forces breakdown file (forces_breakdown_aeroelasticSimple_Iterative.dat).
+-----------------------------------------------------------------------+

--------------------------- Finalizing Solver ---------------------------
Deleted CNumerics container.
Deleted CIntegration container.
Deleted CSolver container.
Deleted CIteration container.
Deleted CInterface container.
Deleted CGeometry container.
Deleted CFreeFormDefBox class.
Deleted CSurfaceMovement class.
Deleted CVolumetricMovement class.
Deleted CConfig container.
Deleted nInst container.
Deleted COutput class.
-------------------------------------------------------------------------

------------------------- Exit Success (SU2_CFD) ------------------------


Running PostAnalysis ...... su2

Running PreAnalysis ...... su2
Mapping Csys attributes ................
	Number of unique Csys attributes = 0

Getting FEA coordinate systems.......
	Number of coordinate systems - 0
	No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
	Number of unique capsConstraint attributes = 1
	Name = Rib_Root, index = 1
Mapping capsLoad attributes ................
	Number of unique capsLoad attributes = 1
	Name = Skin, index = 1
Mapping capsBound attributes ................
	Number of unique capsBound attributes = 3
	Name = Skin_Top, index = 1
	Name = Skin_Bottom, index = 2
	Name = Skin_Tip, index = 3
Mapping capsConnect attributes ................
	Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
	Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
	Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 2
	Name = Skin, index = 1
	Name = Rib_Root, index = 2
Setting FEA Data
	Mesh for body = 0
	Number of nodal coordinates = 180
	Number of elements = 194
	Elemental Nodes = 0
	Elemental Rods  = 0
	Elemental Tria3 = 32
	Elemental Quad4 = 162
Aero_Reference value is NULL - No aero reference parameters set

Getting FEA materials.......
	Number of materials - 1
	Material name - Madeupium
	Done getting FEA materials

Getting FEA properties.......
	Number of properties - 2
	Property name - Rib_Root
	Property name - Skin
	Done getting FEA properties
Updating mesh element types based on properties input

Getting FEA constraints.......
	Number of constraints - 1
	Constraint name - edgeConstraint
	No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement"
	Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults

Getting FEA loads.......
	Number of loads - 1
	Load name - pressureAero
	No "groupName" specified for Load tuple pressureAero, going to use load name
	Done getting FEA loads
Optimization Control tuple is NULL - Default optimization control is used

Getting FEA optimization control.......
Done getting FEA Optimization Control
Design_Variable tuple is NULL - No design variables applied
Design_Constraint tuple is NULL - No design constraints applied
Analysis tuple is NULL

Getting FEA analyses.......
	Number of analyses - 1
	Analysis name - Default
	Done getting FEA analyses
Reading SU2 AeroLoad File - surface_flow_aeroelasticSimple_Iterative.csv
	Number of variables = 16
	Number of data points = 104
 CAPS Info: Bound 'Skin_Top' Normalized Integrated 'Pressure'
            Rank 0: src = 3.095468e+09, tgt = 3.095467e+09, diff = 1.346687e+02
Reading SU2 AeroLoad File - surface_flow_aeroelasticSimple_Iterative.csv
	Number of variables = 16
	Number of data points = 104
 CAPS Info: Bound 'Skin_Bottom' Normalized Integrated 'Pressure'
            Rank 0: src = 3.008438e+09, tgt = 3.008438e+09, diff = 1.930931e+02
Reading SU2 AeroLoad File - surface_flow_aeroelasticSimple_Iterative.csv
	Number of variables = 16
	Number of data points = 104
 CAPS Info: Bound 'Skin_Tip' Normalized Integrated 'Pressure'
            Rank 0: src = 4.099882e+07, tgt = 4.099882e+07, diff = 3.402070e-02
Extracting external pressure loads from data transfer....
	TransferName = Skin_Top
	Number of Elements = 81 (total = 81)
Extracting external pressure loads from data transfer....
	TransferName = Skin_Bottom
	Number of Elements = 81 (total = 162)
Extracting external pressure loads from data transfer....
	TransferName = Skin_Tip
	Number of Elements = 16 (total = 178)

Writing Astros grid and connectivity file (in free field format) ....
Finished writing Astros grid file

Writing subElement types (if any) - appending mesh file

Writing Astros instruction file....
	Writing analysis cards
	Writing load ADD cards
	Writing constraint cards--each subcase individually
	Writing load cards
	Writing material cards
	Writing property cards
Note: The following floating-point exceptions are signalling: IEEE_UNDERFLOW_FLAG
Writing SU2 data transfer files
Writing SU2 Motion File - aeroelasticSimple_Iterative_motion.dat
Warning: The su2 cfg file will be overwritten!
Write SU2 configuration file for version "Harrier (8.0.1)"


Running SU2......

-------------------------------------------------------------------------
|    ___ _   _ ___                                                      |
|   / __| | | |_  )   Release 8.0.0 "Harrier"                           |
|   \__ \ |_| |/ /                                                      |
|   |___/\___//___|   Suite (Mesh Deformation Code)                     |
|                                                                       |
-------------------------------------------------------------------------
| SU2 Project Website: <a href='https://su2code.github.io'>https://su2code.github.io</a>                        |
|                                                                       |
| The SU2 Project is maintained by the SU2 Foundation                   |
| (<a href='http://su2foundation.org'>http://su2foundation.org</a>)                                            |
-------------------------------------------------------------------------
| Copyright 2012-2023, SU2 Contributors                                 |
|                                                                       |
| SU2 is free software; you can redistribute it and/or                  |
| modify it under the terms of the GNU Lesser General Public            |
| License as published by the Free Software Foundation; either          |
| version 2.1 of the License, or (at your option) any later version.    |
|                                                                       |
| SU2 is distributed in the hope that it will be useful,                |
| but WITHOUT ANY WARRANTY; without even the implied warranty of        |
| MERCHANTABILITY or FITNESS FOR A PARTICULAR PURPOSE. See the GNU      |
| Lesser General Public License for more details.                       |
|                                                                       |
| You should have received a copy of the GNU Lesser General Public      |
| License along with SU2. If not, see &lt;<a href='http://www.gnu.org/licenses/'>http://www.gnu.org/licenses/</a>&gt;.   |
-------------------------------------------------------------------------

----------------- Physical Case Definition ( Zone 0 ) -------------------
Input mesh file name: ../aflr3/aflr3_CAPS.su2

---------------- Grid deformation parameters ( Zone 0 )  ----------------
Grid deformation using a linear elasticity method.


-------------------- Output Information ( Zone 0 ) ----------------------
Output mesh file name: ../aflr3/aflr3_CAPS.su2. 
Cell stiffness scaled by distance to nearest solid surface.

------------- Config File Boundary Information ( Zone 0 ) ---------------
+-----------------------------------------------------------------------+
|                        Marker Type|                        Marker Name|
+-----------------------------------------------------------------------+
|                         Euler wall|                               BC_3|
+-----------------------------------------------------------------------+
|                          Far-field|                               BC_1|
+-----------------------------------------------------------------------+
|                     Symmetry plane|                               BC_2|
+-----------------------------------------------------------------------+
Three dimensional problem.
11301 grid points.
58551 volume elements.
3 surface markers.
3452 boundary elements in index 0 (Marker = BC_1).
1827 boundary elements in index 1 (Marker = BC_2).
195 boundary elements in index 2 (Marker = BC_3).
58551 tetrahedra.

----------------------- Preprocessing computations ----------------------
Setting local point connectivity.
Checking the numerical grid orientation of the interior elements.
All volume elements are correctly orientend.
All surface elements are correctly orientend.
Identify edges and vertices.
Setting the bound control volume structure.
Volume of the computational grid: 63999.5.
  Info: Ignoring the following volume output fields/groups:
  SOLUTION
Volume output fields: COORDINATES
  Info: Ignoring the following screen output fields:
  RMS_DENSITY, RMS_MOMENTUM-X, RMS_MOMENTUM-Y, RMS_ENERGY, EFFICIENCY
Screen output fields: TIME_ITER, OUTER_ITER, INNER_ITER, CUR_TIME, TIME_STEP, WALL_TIME
  Info: Ignoring the following history output groups:
  RMS_RES, AERO_COEFF
History output group(s): ITER, TIME_DOMAIN, WALL_TIME
Warning: No (valid) fields chosen for convergence monitoring. Convergence monitoring inactive.
Warning: No (valid) fields chosen for time convergence monitoring. Time convergence monitoring inactive.

--------------------- Surface grid deformation (ZONE 0) -----------------
Performing the deformation of the surface grid.
Updating the surface coordinates from the input file.

------------------- Volumetric grid deformation (ZONE 0) ----------------
Performing the deformation of the volumetric grid.

WARNING: Convexity is not checked for 3D elements (issue #1171).


Completed in 0.614413 seconds on 1 core.

----------------------- Write deformed grid files -----------------------
|SU2 mesh                           |../aflr3/aflr3_CAPS.su2            |
|CSV file                           |surface_deformed.csv               |
|Tecplot binary                     |volume_deformed.szplt              |
|Tecplot binary surface             |surface_deformed.szplt             |
Adding any FFD information to the SU2 file.

------------------------- Finalize Solver -------------------------
Deleted CNumerics container.
Deleted CSolver container.
Deleted CGeometry container.
Deleted CSurfaceMovement class.
Deleted CVolumetricMovement class.
Deleted CConfig container.
Deleted COutput class.

------------------------- Exit Success (SU2_DEF) ------------------------


-------------------------------------------------------------------------
|    ___ _   _ ___                                                      |
|   / __| | | |_  )   Release 8.0.0 "Harrier"                           |
|   \__ \ |_| |/ /                                                      |
|   |___/\___//___|   Suite (Computational Fluid Dynamics Code)         |
|                                                                       |
-------------------------------------------------------------------------
| SU2 Project Website: <a href='https://su2code.github.io'>https://su2code.github.io</a>                        |
|                                                                       |
| The SU2 Project is maintained by the SU2 Foundation                   |
| (<a href='http://su2foundation.org'>http://su2foundation.org</a>)                                            |
-------------------------------------------------------------------------
| Copyright 2012-2023, SU2 Contributors                                 |
|                                                                       |
| SU2 is free software; you can redistribute it and/or                  |
| modify it under the terms of the GNU Lesser General Public            |
| License as published by the Free Software Foundation; either          |
| version 2.1 of the License, or (at your option) any later version.    |
|                                                                       |
| SU2 is distributed in the hope that it will be useful,                |
| but WITHOUT ANY WARRANTY; without even the implied warranty of        |
| MERCHANTABILITY or FITNESS FOR A PARTICULAR PURPOSE. See the GNU      |
| Lesser General Public License for more details.                       |
|                                                                       |
| You should have received a copy of the GNU Lesser General Public      |
| License along with SU2. If not, see &lt;<a href='http://www.gnu.org/licenses/'>http://www.gnu.org/licenses/</a>&gt;.   |
-------------------------------------------------------------------------

Parsing config file for zone 0

----------------- Physical Case Definition ( Zone 0 ) -------------------
Compressible Euler equations.
Mach number: 0.294118.
Angle of attack (AoA): 0 deg, and angle of sideslip (AoS): 0 deg.
No restart solution, use the values at infinity (freestream).
Dimensional simulation.
The reference area is 1 m^2.
The semi-span will be computed using the max y(3D) value.
The reference length is 1 m.
Reference origin for moment evaluation is (0, 0, 0).
Surface(s) where the force coefficients are evaluated: BC_3.

Surface(s) plotted in the output file: BC_3.
Surface(s) affected by the design variables: BC_3.
Input mesh file name: ../aflr3/aflr3_CAPS.su2

--------------- Space Numerical Integration ( Zone 0 ) ------------------
Roe (with entropy fix = 0.001) solver for the flow inviscid terms.
Standard Roe without low-dissipation function.
Second order integration in space, with slope limiter.
Venkatakrishnan slope-limiting method, with constant: 0.05.
The reference element size is: 1. 
Gradient for upwind reconstruction: inverse-distance weighted Least-Squares.
Gradient for viscous and source terms: inverse-distance weighted Least-Squares.

--------------- Time Numerical Integration  ( Zone 0 ) ------------------
Local time stepping (steady state simulation).
Euler implicit method for the flow equations.
FGMRES is used for solving the linear system.
Using a ILU(0) preconditioning.
Convergence criteria of the linear solver: 1e-06.
Max number of linear iterations: 10.
V Multigrid Cycle, with 2 multigrid levels.
Damping factor for the residual restriction: 0.75.
Damping factor for the correction prolongation: 0.75.
No CFL adaptation.
+-------------------------------------------+
|  MG Level| Presmooth|PostSmooth|CorrectSmo|
+-------------------------------------------+
|         0|         1|         0|         0|
|         1|         2|         0|         0|
|         2|         3|         0|         0|
+-------------------------------------------+
Courant-Friedrichs-Lewy number:       10

------------------ Convergence Criteria  ( Zone 0 ) ---------------------
Maximum number of solver subiterations: 3.
Begin convergence monitoring at iteration 5.
Residual minimum value: 1e-14.
Cauchy series min. value: 1e-10.
Number of Cauchy elements: 100.
Begin windowed time average at iteration 0.

-------------------- Output Information ( Zone 0 ) ----------------------
File writing frequency: 
+------------------------------------+
|                     File| Frequency|
+------------------------------------+
|                  RESTART|       250|
|              SURFACE_CSV|       250|
|                  TECPLOT|       250|
|          SURFACE_TECPLOT|       250|
+------------------------------------+
Writing the convergence history file every 1 inner iterations.
Writing the screen convergence history every 1 inner iterations.
The tabular file format is CSV (.csv).
Convergence history file name: history.
Forces breakdown file name: forces_breakdown_aeroelasticSimple_Iterative.dat.
Surface file name: surface_flow_aeroelasticSimple_Iterative.
Volume file name: flow_aeroelasticSimple_Iterative.
Restart file name: restart_flow_aeroelasticSimple_Iterative.dat.

------------- Config File Boundary Information ( Zone 0 ) ---------------
+-----------------------------------------------------------------------+
|                        Marker Type|                        Marker Name|
+-----------------------------------------------------------------------+
|                         Euler wall|                               BC_3|
+-----------------------------------------------------------------------+
|                          Far-field|                               BC_1|
+-----------------------------------------------------------------------+
|                     Symmetry plane|                               BC_2|
+-----------------------------------------------------------------------+

-------------------- Output Preprocessing ( Zone 0 ) --------------------

WARNING: SURFACE_PRESSURE_DROP can only be computed for at least 2 surfaces (outlet, inlet, ...)

Screen output fields: TIME_ITER, OUTER_ITER, INNER_ITER, CUR_TIME, TIME_STEP, WALL_TIME, RMS_DENSITY, RMS_MOMENTUM-X, RMS_MOMENTUM-Y, RMS_ENERGY, EFFICIENCY
History output group(s): ITER, TIME_DOMAIN, WALL_TIME, RMS_RES, AERO_COEFF
Convergence field(s): RMS_DENSITY
Warning: No (valid) fields chosen for time convergence monitoring. Time convergence monitoring inactive.
Volume output fields: COORDINATES, SOLUTION, PRIMITIVE

------------------- Geometry Preprocessing ( Zone 0 ) -------------------
Three dimensional problem.
11301 grid points.
58551 volume elements.
3 surface markers.
3452 boundary elements in index 0 (Marker = BC_1).
1827 boundary elements in index 1 (Marker = BC_2).
195 boundary elements in index 2 (Marker = BC_3).
58551 tetrahedra.
Setting point connectivity.
Renumbering points (Reverse Cuthill McKee Ordering).
Recomputing point connectivity.
Setting element connectivity.
Checking the numerical grid orientation.
There has been a re-orientation of 1059 TETRAHEDRON volume elements.
There has been a re-orientation of 43 TRIANGLE surface elements.
Identifying edges and vertices.
Setting the control volume structure.
Volume of the computational grid: 64515.
Searching for the closest normal neighbors to the surfaces.
Storing a mapping from global to local point index.
Compute the surface curvature.
Max K: 33.5988. Mean K: 0.526022. Standard deviation K: 1.77961.
Checking for periodicity.
Computing mesh quality statistics for the dual control volumes.
+--------------------------------------------------------------+
|           Mesh Quality Metric|        Minimum|        Maximum|
+--------------------------------------------------------------+
|    Orthogonality Angle (deg.)|        3.57195|        85.5935|
|     CV Face Area Aspect Ratio|        1.16408|        159.268|
|           CV Sub-Volume Ratio|              1|        6410.87|
+--------------------------------------------------------------+
Setting the multigrid structure.
+-------------------------------------------+
|  MG Level|       CVs|Aggl. Rate|       CFL|
+-------------------------------------------+
|         0|     11301|    1/1.00|        10|
|         1|      2022|    1/5.59|   8.45239|
|         2|       415|    1/4.87|    7.4787|
+-------------------------------------------+
Finding max control volume width.
Semi-span length = 4.34904 m.
Wetted area = 166.087 m^2.
Area projection in the x-plane = 64.7975 m^2, y-plane = 37.3137 m^2, z-plane = 5.27348 m^2.
Max. coordinate in the x-direction = 2.74566 m, y-direction = 4.34904 m, z-direction = 19.6307 m.
Min. coordinate in the x-direction = -0.647511 m, y-direction = -0.0653684 m, z-direction = -18.9106 m.
Checking if Euler &amp; Symmetry markers are straight/plane:
Boundary marker BC_3 is NOT a single plane.
Boundary marker BC_2 is NOT a single plane.
Computing wall distances.

-------------------- Solver Preprocessing ( Zone 0 ) --------------------
Inviscid flow: Computing density based on free-stream
temperature and pressure using the ideal gas law.
Force coefficients computed using free-stream values.

-- Models:
+------------------------------------------------------------------------------+
|          Viscosity Model|        Conductivity Model|              Fluid Model|
+------------------------------------------------------------------------------+
|                        -|                         -|             STANDARD_AIR|
+------------------------------------------------------------------------------+
-- Fluid properties:
+------------------------------------------------------------------------------+
|                  Name|    Dim. value|    Ref. value|      Unit|Non-dim. value|
+------------------------------------------------------------------------------+
|          Gas Constant|       287.058|             1|  N.m/kg.K|       287.058|
|      Spec. Heat Ratio|             -|             -|         -|           1.4|
+------------------------------------------------------------------------------+
-- Initial and free-stream conditions:
+------------------------------------------------------------------------------+
|                  Name|    Dim. value|    Ref. value|      Unit|Non-dim. value|
+------------------------------------------------------------------------------+
|       Static Pressure|        101325|             1|        Pa|        101325|
|               Density|       1.22498|             1|    kg/m^3|       1.22498|
|           Temperature|        288.15|             1|         K|        288.15|
|          Total Energy|        211798|             1|   m^2/s^2|        211798|
|            Velocity-X|       100.087|             1|       m/s|       100.087|
|            Velocity-Y|             0|             1|       m/s|             0|
|            Velocity-Z|             0|             1|       m/s|             0|
|    Velocity Magnitude|       100.087|             1|       m/s|       100.087|
+------------------------------------------------------------------------------+
|           Mach Number|             -|             -|         -|      0.294118|
+------------------------------------------------------------------------------+
Initialize Jacobian structure (Euler). MG level: 0.
Initialize Jacobian structure (Euler). MG level: 1.
Initialize Jacobian structure (Euler). MG level: 2.

------------------- Numerics Preprocessing ( Zone 0 ) -------------------

----------------- Integration Preprocessing ( Zone 0 ) ------------------

------------------- Iteration Preprocessing ( Zone 0 ) ------------------
Euler/Navier-Stokes/RANS fluid iteration.

------------------------------ Begin Solver -----------------------------

Simulation Run using the Single-zone Driver
WARNING: SU2 was not compiled for an AVX-capable architecture. Performance could be better,
         see <a href='https://su2code.github.io/docs_v7/Build-SU2-Linux-MacOS/#compiler-optimizations'>https://su2code.github.io/docs_v7/Build-SU2-Linux-MacOS/#compiler-optimizations</a>
WARNING: SU2 was not compiled for an AVX-capable architecture. Performance could be better,
         see <a href='https://su2code.github.io/docs_v7/Build-SU2-Linux-MacOS/#compiler-optimizations'>https://su2code.github.io/docs_v7/Build-SU2-Linux-MacOS/#compiler-optimizations</a>
WARNING: SU2 was not compiled for an AVX-capable architecture. Performance could be better,
         see <a href='https://su2code.github.io/docs_v7/Build-SU2-Linux-MacOS/#compiler-optimizations'>https://su2code.github.io/docs_v7/Build-SU2-Linux-MacOS/#compiler-optimizations</a>
+----------------------------------------------------------------------------------------------------------------------------------------------+
|   Time_Iter|  Outer_Iter|  Inner_Iter|    Cur_Time|   Time_Step|   Time(sec)|    rms[Rho]|   rms[RhoU]|   rms[RhoV]|   rms[RhoE]|        CEff|
+----------------------------------------------------------------------------------------------------------------------------------------------+
|           0|           0|           0|  0.0000e+00|  0.0000e+00|  1.7618e-01|    1.834424|    4.789528|    4.866267|    7.303530|   -0.031030|
|           0|           0|           1|  0.0000e+00|  0.0000e+00|  1.8053e-01|    2.279632|    4.832406|    4.888836|    7.690003|   -0.045547|
|           0|           0|           2|  0.0000e+00|  0.0000e+00|  1.8165e-01|    2.326325|    4.844282|    4.900460|    7.711785|   -0.025198|

----------------------------- Solver Exit -------------------------------

Maximum number of iterations reached (ITER = 3) before convergence.
+-----------------------------------------------------------------------+
|      Convergence Field     |     Value    |   Criterion  |  Converged |
+-----------------------------------------------------------------------+
|                    rms[Rho]|       2.32633|         &lt; -14|          No|
+-----------------------------------------------------------------------+
-------------------------------------------------------------------------
+-----------------------------------------------------------------------+
|        File Writing Summary       |              Filename             |
+-----------------------------------------------------------------------+
|SU2 binary restart                 |restart_flow_aeroelasticSimple_Iterative.dat|

Writing the forces breakdown file (forces_breakdown_aeroelasticSimple_Iterative.dat).
|CSV file                           |surface_flow_aeroelasticSimple_Iterative.csv|

Writing the forces breakdown file (forces_breakdown_aeroelasticSimple_Iterative.dat).
|Tecplot binary                     |flow_aeroelasticSimple_Iterative.szplt|

Writing the forces breakdown file (forces_breakdown_aeroelasticSimple_Iterative.dat).
|Tecplot binary surface             |surface_flow_aeroelasticSimple_Iterative.szplt|

Writing the forces breakdown file (forces_breakdown_aeroelasticSimple_Iterative.dat).
+-----------------------------------------------------------------------+
Warning: there are 59 non-physical points in the solution.
Warning: 2 reconstructed states for upwinding are non-physical.

--------------------------- Finalizing Solver ---------------------------
Deleted CNumerics container.
Deleted CIntegration container.
Deleted CSolver container.
Deleted CIteration container.
Deleted CInterface container.
Deleted CGeometry container.
Deleted CFreeFormDefBox class.
Deleted CSurfaceMovement class.
Deleted CVolumetricMovement class.
Deleted CConfig container.
Deleted nInst container.
Deleted COutput class.
-------------------------------------------------------------------------

------------------------- Exit Success (SU2_CFD) ------------------------


Running PostAnalysis ...... su2

Running PreAnalysis ...... su2
Reading SU2 AeroLoad File - surface_flow_aeroelasticSimple_Iterative.csv
	Number of variables = 16
	Number of data points = 104
 CAPS Info: Bound 'Skin_Top' Normalized Integrated 'Pressure'
            Rank 0: src = 1.889013e+09, tgt = 1.889013e+09, diff = 1.783712e+02
Reading SU2 AeroLoad File - surface_flow_aeroelasticSimple_Iterative.csv
	Number of variables = 16
	Number of data points = 104
 CAPS Info: Bound 'Skin_Bottom' Normalized Integrated 'Pressure'
            Rank 0: src = 1.356764e+09, tgt = 1.356764e+09, diff = 2.847698e+02
Reading SU2 AeroLoad File - surface_flow_aeroelasticSimple_Iterative.csv
	Number of variables = 16
	Number of data points = 104
 CAPS Info: Bound 'Skin_Tip' Normalized Integrated 'Pressure'
            Rank 0: src = 1.544678e+07, tgt = 1.544678e+07, diff = 5.994724e-02
Extracting external pressure loads from data transfer....
	TransferName = Skin_Top
	Number of Elements = 81 (total = 81)
Extracting external pressure loads from data transfer....
	TransferName = Skin_Bottom
	Number of Elements = 81 (total = 162)
Extracting external pressure loads from data transfer....
	TransferName = Skin_Tip
	Number of Elements = 16 (total = 178)

Writing Astros grid and connectivity file (in free field format) ....
Finished writing Astros grid file

Writing subElement types (if any) - appending mesh file

Writing Astros instruction file....
	Writing analysis cards
	Writing load ADD cards
	Writing constraint cards--each subcase individually
	Writing load cards
	Writing material cards
	Writing property cards
Note: The following floating-point exceptions are signalling: IEEE_UNDERFLOW_FLAG
Writing SU2 data transfer files
Writing SU2 Motion File - aeroelasticSimple_Iterative_motion.dat
Warning: The su2 cfg file will be overwritten!
Write SU2 configuration file for version "Harrier (8.0.1)"


Running SU2......

-------------------------------------------------------------------------
|    ___ _   _ ___                                                      |
|   / __| | | |_  )   Release 8.0.0 "Harrier"                           |
|   \__ \ |_| |/ /                                                      |
|   |___/\___//___|   Suite (Mesh Deformation Code)                     |
|                                                                       |
-------------------------------------------------------------------------
| SU2 Project Website: <a href='https://su2code.github.io'>https://su2code.github.io</a>                        |
|                                                                       |
| The SU2 Project is maintained by the SU2 Foundation                   |
| (<a href='http://su2foundation.org'>http://su2foundation.org</a>)                                            |
-------------------------------------------------------------------------
| Copyright 2012-2023, SU2 Contributors                                 |
|                                                                       |
| SU2 is free software; you can redistribute it and/or                  |
| modify it under the terms of the GNU Lesser General Public            |
| License as published by the Free Software Foundation; either          |
| version 2.1 of the License, or (at your option) any later version.    |
|                                                                       |
| SU2 is distributed in the hope that it will be useful,                |
| but WITHOUT ANY WARRANTY; without even the implied warranty of        |
| MERCHANTABILITY or FITNESS FOR A PARTICULAR PURPOSE. See the GNU      |
| Lesser General Public License for more details.                       |
|                                                                       |
| You should have received a copy of the GNU Lesser General Public      |
| License along with SU2. If not, see &lt;<a href='http://www.gnu.org/licenses/'>http://www.gnu.org/licenses/</a>&gt;.   |
-------------------------------------------------------------------------

----------------- Physical Case Definition ( Zone 0 ) -------------------
Input mesh file name: ../aflr3/aflr3_CAPS.su2

---------------- Grid deformation parameters ( Zone 0 )  ----------------
Grid deformation using a linear elasticity method.


-------------------- Output Information ( Zone 0 ) ----------------------
Output mesh file name: ../aflr3/aflr3_CAPS.su2. 
Cell stiffness scaled by distance to nearest solid surface.

------------- Config File Boundary Information ( Zone 0 ) ---------------
+-----------------------------------------------------------------------+
|                        Marker Type|                        Marker Name|
+-----------------------------------------------------------------------+
|                         Euler wall|                               BC_3|
+-----------------------------------------------------------------------+
|                          Far-field|                               BC_1|
+-----------------------------------------------------------------------+
|                     Symmetry plane|                               BC_2|
+-----------------------------------------------------------------------+
Three dimensional problem.
11301 grid points.
58551 volume elements.
3 surface markers.
3452 boundary elements in index 0 (Marker = BC_1).
1827 boundary elements in index 1 (Marker = BC_2).
195 boundary elements in index 2 (Marker = BC_3).
58551 tetrahedra.

----------------------- Preprocessing computations ----------------------
Setting local point connectivity.
Checking the numerical grid orientation of the interior elements.
There has been a re-orientation of 1059 TETRAHEDRON volume elements.
There has been a re-orientation of 43 TRIANGLE surface elements.
Identify edges and vertices.
Setting the bound control volume structure.
Volume of the computational grid: 64515.
  Info: Ignoring the following volume output fields/groups:
  SOLUTION
Volume output fields: COORDINATES
  Info: Ignoring the following screen output fields:
  RMS_DENSITY, RMS_MOMENTUM-X, RMS_MOMENTUM-Y, RMS_ENERGY, EFFICIENCY
Screen output fields: TIME_ITER, OUTER_ITER, INNER_ITER, CUR_TIME, TIME_STEP, WALL_TIME
  Info: Ignoring the following history output groups:
  RMS_RES, AERO_COEFF
History output group(s): ITER, TIME_DOMAIN, WALL_TIME
Warning: No (valid) fields chosen for convergence monitoring. Convergence monitoring inactive.
Warning: No (valid) fields chosen for time convergence monitoring. Time convergence monitoring inactive.

--------------------- Surface grid deformation (ZONE 0) -----------------
Performing the deformation of the surface grid.
Updating the surface coordinates from the input file.

------------------- Volumetric grid deformation (ZONE 0) ----------------
Performing the deformation of the volumetric grid.

WARNING: Convexity is not checked for 3D elements (issue #1171).


Completed in 3.387828 seconds on 1 core.

----------------------- Write deformed grid files -----------------------
|SU2 mesh                           |../aflr3/aflr3_CAPS.su2            |
|CSV file                           |surface_deformed.csv               |
|Tecplot binary                     |volume_deformed.szplt              |
|Tecplot binary surface             |surface_deformed.szplt             |
Adding any FFD information to the SU2 file.

------------------------- Finalize Solver -------------------------
Deleted CNumerics container.
Deleted CSolver container.
Deleted CGeometry container.
Deleted CSurfaceMovement class.
Deleted CVolumetricMovement class.
Deleted CConfig container.
Deleted COutput class.

------------------------- Exit Success (SU2_DEF) ------------------------


-------------------------------------------------------------------------
|    ___ _   _ ___                                                      |
|   / __| | | |_  )   Release 8.0.0 "Harrier"                           |
|   \__ \ |_| |/ /                                                      |
|   |___/\___//___|   Suite (Computational Fluid Dynamics Code)         |
|                                                                       |
-------------------------------------------------------------------------
| SU2 Project Website: <a href='https://su2code.github.io'>https://su2code.github.io</a>                        |
|                                                                       |
| The SU2 Project is maintained by the SU2 Foundation                   |
| (<a href='http://su2foundation.org'>http://su2foundation.org</a>)                                            |
-------------------------------------------------------------------------
| Copyright 2012-2023, SU2 Contributors                                 |
|                                                                       |
| SU2 is free software; you can redistribute it and/or                  |
| modify it under the terms of the GNU Lesser General Public            |
| License as published by the Free Software Foundation; either          |
| version 2.1 of the License, or (at your option) any later version.    |
|                                                                       |
| SU2 is distributed in the hope that it will be useful,                |
| but WITHOUT ANY WARRANTY; without even the implied warranty of        |
| MERCHANTABILITY or FITNESS FOR A PARTICULAR PURPOSE. See the GNU      |
| Lesser General Public License for more details.                       |
|                                                                       |
| You should have received a copy of the GNU Lesser General Public      |
| License along with SU2. If not, see &lt;<a href='http://www.gnu.org/licenses/'>http://www.gnu.org/licenses/</a>&gt;.   |
-------------------------------------------------------------------------

Parsing config file for zone 0

----------------- Physical Case Definition ( Zone 0 ) -------------------
Compressible Euler equations.
Mach number: 0.294118.
Angle of attack (AoA): 0 deg, and angle of sideslip (AoS): 0 deg.
No restart solution, use the values at infinity (freestream).
Dimensional simulation.
The reference area is 1 m^2.
The semi-span will be computed using the max y(3D) value.
The reference length is 1 m.
Reference origin for moment evaluation is (0, 0, 0).
Surface(s) where the force coefficients are evaluated: BC_3.

Surface(s) plotted in the output file: BC_3.
Surface(s) affected by the design variables: BC_3.
Input mesh file name: ../aflr3/aflr3_CAPS.su2

--------------- Space Numerical Integration ( Zone 0 ) ------------------
Roe (with entropy fix = 0.001) solver for the flow inviscid terms.
Standard Roe without low-dissipation function.
Second order integration in space, with slope limiter.
Venkatakrishnan slope-limiting method, with constant: 0.05.
The reference element size is: 1. 
Gradient for upwind reconstruction: inverse-distance weighted Least-Squares.
Gradient for viscous and source terms: inverse-distance weighted Least-Squares.

--------------- Time Numerical Integration  ( Zone 0 ) ------------------
Local time stepping (steady state simulation).
Euler implicit method for the flow equations.
FGMRES is used for solving the linear system.
Using a ILU(0) preconditioning.
Convergence criteria of the linear solver: 1e-06.
Max number of linear iterations: 10.
V Multigrid Cycle, with 2 multigrid levels.
Damping factor for the residual restriction: 0.75.
Damping factor for the correction prolongation: 0.75.
No CFL adaptation.
+-------------------------------------------+
|  MG Level| Presmooth|PostSmooth|CorrectSmo|
+-------------------------------------------+
|         0|         1|         0|         0|
|         1|         2|         0|         0|
|         2|         3|         0|         0|
+-------------------------------------------+
Courant-Friedrichs-Lewy number:       10

------------------ Convergence Criteria  ( Zone 0 ) ---------------------
Maximum number of solver subiterations: 3.
Begin convergence monitoring at iteration 5.
Residual minimum value: 1e-14.
Cauchy series min. value: 1e-10.
Number of Cauchy elements: 100.
Begin windowed time average at iteration 0.

-------------------- Output Information ( Zone 0 ) ----------------------
File writing frequency: 
+------------------------------------+
|                     File| Frequency|
+------------------------------------+
|                  RESTART|       250|
|              SURFACE_CSV|       250|
|                  TECPLOT|       250|
|          SURFACE_TECPLOT|       250|
+------------------------------------+
Writing the convergence history file every 1 inner iterations.
Writing the screen convergence history every 1 inner iterations.
The tabular file format is CSV (.csv).
Convergence history file name: history.
Forces breakdown file name: forces_breakdown_aeroelasticSimple_Iterative.dat.
Surface file name: surface_flow_aeroelasticSimple_Iterative.
Volume file name: flow_aeroelasticSimple_Iterative.
Restart file name: restart_flow_aeroelasticSimple_Iterative.dat.

------------- Config File Boundary Information ( Zone 0 ) ---------------
+-----------------------------------------------------------------------+
|                        Marker Type|                        Marker Name|
+-----------------------------------------------------------------------+
|                         Euler wall|                               BC_3|
+-----------------------------------------------------------------------+
|                          Far-field|                               BC_1|
+-----------------------------------------------------------------------+
|                     Symmetry plane|                               BC_2|
+-----------------------------------------------------------------------+

-------------------- Output Preprocessing ( Zone 0 ) --------------------

WARNING: SURFACE_PRESSURE_DROP can only be computed for at least 2 surfaces (outlet, inlet, ...)

Screen output fields: TIME_ITER, OUTER_ITER, INNER_ITER, CUR_TIME, TIME_STEP, WALL_TIME, RMS_DENSITY, RMS_MOMENTUM-X, RMS_MOMENTUM-Y, RMS_ENERGY, EFFICIENCY
History output group(s): ITER, TIME_DOMAIN, WALL_TIME, RMS_RES, AERO_COEFF
Convergence field(s): RMS_DENSITY
Warning: No (valid) fields chosen for time convergence monitoring. Time convergence monitoring inactive.
Volume output fields: COORDINATES, SOLUTION, PRIMITIVE

------------------- Geometry Preprocessing ( Zone 0 ) -------------------
Three dimensional problem.
11301 grid points.
58551 volume elements.
3 surface markers.
3452 boundary elements in index 0 (Marker = BC_1).
1827 boundary elements in index 1 (Marker = BC_2).
195 boundary elements in index 2 (Marker = BC_3).
58551 tetrahedra.
Setting point connectivity.
Renumbering points (Reverse Cuthill McKee Ordering).
Recomputing point connectivity.
Setting element connectivity.
Checking the numerical grid orientation.
There has been a re-orientation of 27048 TETRAHEDRON volume elements.
There has been a re-orientation of 1531 TRIANGLE surface elements.
Identifying edges and vertices.
Setting the control volume structure.
Volume of the computational grid: 567481.
Searching for the closest normal neighbors to the surfaces.
Storing a mapping from global to local point index.
Compute the surface curvature.
Max K: 105.217. Mean K: 1.32211. Standard deviation K: 5.15455.
Checking for periodicity.
Computing mesh quality statistics for the dual control volumes.
+--------------------------------------------------------------+
|           Mesh Quality Metric|        Minimum|        Maximum|
+--------------------------------------------------------------+
|    Orthogonality Angle (deg.)|       0.800934|        81.1446|
|     CV Face Area Aspect Ratio|        1.53152|        961.841|
|           CV Sub-Volume Ratio|              1|         103390|
+--------------------------------------------------------------+
Setting the multigrid structure.
+-------------------------------------------+
|  MG Level|       CVs|Aggl. Rate|       CFL|
+-------------------------------------------+
|         0|     11301|    1/1.00|        10|
|         1|      2018|     1/5.6|   8.44681|
|         2|       413|    1/4.89|   7.46667|
+-------------------------------------------+
Finding max control volume width.
Semi-span length = 1.38253 m.
Wetted area = 1283.54 m^2.
Area projection in the x-plane = 312.855 m^2, y-plane = 448.481 m^2, z-plane = 63.5159 m^2.
Max. coordinate in the x-direction = 13.9358 m, y-direction = 1.38253 m, z-direction = 228.447 m.
Min. coordinate in the x-direction = 0.0404474 m, y-direction = -18.09 m, z-direction = -0.0756566 m.
Checking if Euler &amp; Symmetry markers are straight/plane:
Boundary marker BC_3 is NOT a single plane.
Boundary marker BC_2 is NOT a single plane.
Computing wall distances.

-------------------- Solver Preprocessing ( Zone 0 ) --------------------
Inviscid flow: Computing density based on free-stream
temperature and pressure using the ideal gas law.
Force coefficients computed using free-stream values.

-- Models:
+------------------------------------------------------------------------------+
|          Viscosity Model|        Conductivity Model|              Fluid Model|
+------------------------------------------------------------------------------+
|                        -|                         -|             STANDARD_AIR|
+------------------------------------------------------------------------------+
-- Fluid properties:
+------------------------------------------------------------------------------+
|                  Name|    Dim. value|    Ref. value|      Unit|Non-dim. value|
+------------------------------------------------------------------------------+
|          Gas Constant|       287.058|             1|  N.m/kg.K|       287.058|
|      Spec. Heat Ratio|             -|             -|         -|           1.4|
+------------------------------------------------------------------------------+
-- Initial and free-stream conditions:
+------------------------------------------------------------------------------+
|                  Name|    Dim. value|    Ref. value|      Unit|Non-dim. value|
+------------------------------------------------------------------------------+
|       Static Pressure|        101325|             1|        Pa|        101325|
|               Density|       1.22498|             1|    kg/m^3|       1.22498|
|           Temperature|        288.15|             1|         K|        288.15|
|          Total Energy|        211798|             1|   m^2/s^2|        211798|
|            Velocity-X|       100.087|             1|       m/s|       100.087|
|            Velocity-Y|             0|             1|       m/s|             0|
|            Velocity-Z|             0|             1|       m/s|             0|
|    Velocity Magnitude|       100.087|             1|       m/s|       100.087|
+------------------------------------------------------------------------------+
|           Mach Number|             -|             -|         -|      0.294118|
+------------------------------------------------------------------------------+
Initialize Jacobian structure (Euler). MG level: 0.
Initialize Jacobian structure (Euler). MG level: 1.
Initialize Jacobian structure (Euler). MG level: 2.

------------------- Numerics Preprocessing ( Zone 0 ) -------------------

----------------- Integration Preprocessing ( Zone 0 ) ------------------

------------------- Iteration Preprocessing ( Zone 0 ) ------------------
Euler/Navier-Stokes/RANS fluid iteration.

------------------------------ Begin Solver -----------------------------

Simulation Run using the Single-zone Driver
WARNING: SU2 was not compiled for an AVX-capable architecture. Performance could be better,
         see <a href='https://su2code.github.io/docs_v7/Build-SU2-Linux-MacOS/#compiler-optimizations'>https://su2code.github.io/docs_v7/Build-SU2-Linux-MacOS/#compiler-optimizations</a>
WARNING: SU2 was not compiled for an AVX-capable architecture. Performance could be better,
         see <a href='https://su2code.github.io/docs_v7/Build-SU2-Linux-MacOS/#compiler-optimizations'>https://su2code.github.io/docs_v7/Build-SU2-Linux-MacOS/#compiler-optimizations</a>
WARNING: SU2 was not compiled for an AVX-capable architecture. Performance could be better,
         see <a href='https://su2code.github.io/docs_v7/Build-SU2-Linux-MacOS/#compiler-optimizations'>https://su2code.github.io/docs_v7/Build-SU2-Linux-MacOS/#compiler-optimizations</a>
+----------------------------------------------------------------------------------------------------------------------------------------------+
|   Time_Iter|  Outer_Iter|  Inner_Iter|    Cur_Time|   Time_Step|   Time(sec)|    rms[Rho]|   rms[RhoU]|   rms[RhoV]|   rms[RhoE]|        CEff|
+----------------------------------------------------------------------------------------------------------------------------------------------+
|           0|           0|           0|  0.0000e+00|  0.0000e+00|  1.7192e-01|    3.680103|    6.645738|    6.490933|    9.149209|   -0.074394|
|           0|           0|           1|  0.0000e+00|  0.0000e+00|  1.7964e-01|    3.953727|    6.601837|    6.531704|    9.385408|   -0.068059|
|           0|           0|           2|  0.0000e+00|  0.0000e+00|  1.8165e-01|    4.102420|    6.694617|    6.667295|    9.479603|   -0.082163|

----------------------------- Solver Exit -------------------------------

Maximum number of iterations reached (ITER = 3) before convergence.
+-----------------------------------------------------------------------+
|      Convergence Field     |     Value    |   Criterion  |  Converged |
+-----------------------------------------------------------------------+
|                    rms[Rho]|       4.10242|         &lt; -14|          No|
+-----------------------------------------------------------------------+
-------------------------------------------------------------------------
+-----------------------------------------------------------------------+
|        File Writing Summary       |              Filename             |
+-----------------------------------------------------------------------+
|SU2 binary restart                 |restart_flow_aeroelasticSimple_Iterative.dat|

Writing the forces breakdown file (forces_breakdown_aeroelasticSimple_Iterative.dat).
|CSV file                           |surface_flow_aeroelasticSimple_Iterative.csv|

Writing the forces breakdown file (forces_breakdown_aeroelasticSimple_Iterative.dat).
|Tecplot binary                     |flow_aeroelasticSimple_Iterative.szplt|

Writing the forces breakdown file (forces_breakdown_aeroelasticSimple_Iterative.dat).
|Tecplot binary surface             |surface_flow_aeroelasticSimple_Iterative.szplt|

Writing the forces breakdown file (forces_breakdown_aeroelasticSimple_Iterative.dat).
+-----------------------------------------------------------------------+
Warning: there are 411 non-physical points in the solution.
Warning: 28 reconstructed states for upwinding are non-physical.

--------------------------- Finalizing Solver ---------------------------
Deleted CNumerics container.
Deleted CIntegration container.
Deleted CSolver container.
Deleted CIteration container.
Deleted CInterface container.
Deleted CGeometry container.
Deleted CFreeFormDefBox class.
Deleted CSurfaceMovement class.
Deleted CVolumetricMovement class.
Deleted CConfig container.
Deleted nInst container.
Deleted COutput class.
-------------------------------------------------------------------------

------------------------- Exit Success (SU2_CFD) ------------------------


Running PostAnalysis ...... su2

Running PreAnalysis ...... su2
Reading SU2 AeroLoad File - surface_flow_aeroelasticSimple_Iterative.csv
	Number of variables = 16
	Number of data points = 104
 CAPS Info: Bound 'Skin_Top' Normalized Integrated 'Pressure'
            Rank 0: src = 1.300681e+09, tgt = 1.300681e+09, diff = 5.065727e+01
Reading SU2 AeroLoad File - surface_flow_aeroelasticSimple_Iterative.csv
	Number of variables = 16
	Number of data points = 104
 CAPS Info: Bound 'Skin_Bottom' Normalized Integrated 'Pressure'
            Rank 0: src = 1.188523e+09, tgt = 1.188523e+09, diff = 5.800187e+01
Reading SU2 AeroLoad File - surface_flow_aeroelasticSimple_Iterative.csv
	Number of variables = 16
	Number of data points = 104
 CAPS Info: Bound 'Skin_Tip' Normalized Integrated 'Pressure'
            Rank 0: src = 1.304642e+07, tgt = 1.304642e+07, diff = 7.784819e-03
Extracting external pressure loads from data transfer....
	TransferName = Skin_Top
	Number of Elements = 81 (total = 81)
Extracting external pressure loads from data transfer....
	TransferName = Skin_Bottom
	Number of Elements = 81 (total = 162)
Extracting external pressure loads from data transfer....
	TransferName = Skin_Tip
	Number of Elements = 16 (total = 178)

Writing Astros grid and connectivity file (in free field format) ....
Finished writing Astros grid file

Writing subElement types (if any) - appending mesh file

Writing Astros instruction file....
	Writing analysis cards
	Writing load ADD cards
	Writing constraint cards--each subcase individually
	Writing load cards
	Writing material cards
	Writing property cards
Note: The following floating-point exceptions are signalling: IEEE_UNDERFLOW_FLAG
Writing SU2 data transfer files
Writing SU2 Motion File - aeroelasticSimple_Iterative_motion.dat
Warning: The su2 cfg file will be overwritten!
Write SU2 configuration file for version "Harrier (8.0.1)"


Running SU2......

-------------------------------------------------------------------------
|    ___ _   _ ___                                                      |
|   / __| | | |_  )   Release 8.0.0 "Harrier"                           |
|   \__ \ |_| |/ /                                                      |
|   |___/\___//___|   Suite (Mesh Deformation Code)                     |
|                                                                       |
-------------------------------------------------------------------------
| SU2 Project Website: <a href='https://su2code.github.io'>https://su2code.github.io</a>                        |
|                                                                       |
| The SU2 Project is maintained by the SU2 Foundation                   |
| (<a href='http://su2foundation.org'>http://su2foundation.org</a>)                                            |
-------------------------------------------------------------------------
| Copyright 2012-2023, SU2 Contributors                                 |
|                                                                       |
| SU2 is free software; you can redistribute it and/or                  |
| modify it under the terms of the GNU Lesser General Public            |
| License as published by the Free Software Foundation; either          |
| version 2.1 of the License, or (at your option) any later version.    |
|                                                                       |
| SU2 is distributed in the hope that it will be useful,                |
| but WITHOUT ANY WARRANTY; without even the implied warranty of        |
| MERCHANTABILITY or FITNESS FOR A PARTICULAR PURPOSE. See the GNU      |
| Lesser General Public License for more details.                       |
|                                                                       |
| You should have received a copy of the GNU Lesser General Public      |
| License along with SU2. If not, see &lt;<a href='http://www.gnu.org/licenses/'>http://www.gnu.org/licenses/</a>&gt;.   |
-------------------------------------------------------------------------

----------------- Physical Case Definition ( Zone 0 ) -------------------
Input mesh file name: ../aflr3/aflr3_CAPS.su2

---------------- Grid deformation parameters ( Zone 0 )  ----------------
Grid deformation using a linear elasticity method.


-------------------- Output Information ( Zone 0 ) ----------------------
Output mesh file name: ../aflr3/aflr3_CAPS.su2. 
Cell stiffness scaled by distance to nearest solid surface.

------------- Config File Boundary Information ( Zone 0 ) ---------------
+-----------------------------------------------------------------------+
|                        Marker Type|                        Marker Name|
+-----------------------------------------------------------------------+
|                         Euler wall|                               BC_3|
+-----------------------------------------------------------------------+
|                          Far-field|                               BC_1|
+-----------------------------------------------------------------------+
|                     Symmetry plane|                               BC_2|
+-----------------------------------------------------------------------+
Three dimensional problem.
11301 grid points.
58551 volume elements.
3 surface markers.
3452 boundary elements in index 0 (Marker = BC_1).
1827 boundary elements in index 1 (Marker = BC_2).
195 boundary elements in index 2 (Marker = BC_3).
58551 tetrahedra.

----------------------- Preprocessing computations ----------------------
Setting local point connectivity.
Checking the numerical grid orientation of the interior elements.
There has been a re-orientation of 27048 TETRAHEDRON volume elements.
There has been a re-orientation of 1531 TRIANGLE surface elements.
Identify edges and vertices.
Setting the bound control volume structure.
Volume of the computational grid: 567481.
  Info: Ignoring the following volume output fields/groups:
  SOLUTION
Volume output fields: COORDINATES
  Info: Ignoring the following screen output fields:
  RMS_DENSITY, RMS_MOMENTUM-X, RMS_MOMENTUM-Y, RMS_ENERGY, EFFICIENCY
Screen output fields: TIME_ITER, OUTER_ITER, INNER_ITER, CUR_TIME, TIME_STEP, WALL_TIME
  Info: Ignoring the following history output groups:
  RMS_RES, AERO_COEFF
History output group(s): ITER, TIME_DOMAIN, WALL_TIME
Warning: No (valid) fields chosen for convergence monitoring. Convergence monitoring inactive.
Warning: No (valid) fields chosen for time convergence monitoring. Time convergence monitoring inactive.

--------------------- Surface grid deformation (ZONE 0) -----------------
Performing the deformation of the surface grid.
Updating the surface coordinates from the input file.

------------------- Volumetric grid deformation (ZONE 0) ----------------
Performing the deformation of the volumetric grid.

WARNING: Convexity is not checked for 3D elements (issue #1171).


Completed in 23.532696 seconds on 1 core.

----------------------- Write deformed grid files -----------------------
|SU2 mesh                           |../aflr3/aflr3_CAPS.su2            |
|CSV file                           |surface_deformed.csv               |
|Tecplot binary                     |volume_deformed.szplt              |
|Tecplot binary surface             |surface_deformed.szplt             |
Adding any FFD information to the SU2 file.

------------------------- Finalize Solver -------------------------
Deleted CNumerics container.
Deleted CSolver container.
Deleted CGeometry container.
Deleted CSurfaceMovement class.
Deleted CVolumetricMovement class.
Deleted CConfig container.
Deleted COutput class.

------------------------- Exit Success (SU2_DEF) ------------------------


-------------------------------------------------------------------------
|    ___ _   _ ___                                                      |
|   / __| | | |_  )   Release 8.0.0 "Harrier"                           |
|   \__ \ |_| |/ /                                                      |
|   |___/\___//___|   Suite (Computational Fluid Dynamics Code)         |
|                                                                       |
-------------------------------------------------------------------------
| SU2 Project Website: <a href='https://su2code.github.io'>https://su2code.github.io</a>                        |
|                                                                       |
| The SU2 Project is maintained by the SU2 Foundation                   |
| (<a href='http://su2foundation.org'>http://su2foundation.org</a>)                                            |
-------------------------------------------------------------------------
| Copyright 2012-2023, SU2 Contributors                                 |
|                                                                       |
| SU2 is free software; you can redistribute it and/or                  |
| modify it under the terms of the GNU Lesser General Public            |
| License as published by the Free Software Foundation; either          |
| version 2.1 of the License, or (at your option) any later version.    |
|                                                                       |
| SU2 is distributed in the hope that it will be useful,                |
| but WITHOUT ANY WARRANTY; without even the implied warranty of        |
| MERCHANTABILITY or FITNESS FOR A PARTICULAR PURPOSE. See the GNU      |
| Lesser General Public License for more details.                       |
|                                                                       |
| You should have received a copy of the GNU Lesser General Public      |
| License along with SU2. If not, see &lt;<a href='http://www.gnu.org/licenses/'>http://www.gnu.org/licenses/</a>&gt;.   |
-------------------------------------------------------------------------

Parsing config file for zone 0

----------------- Physical Case Definition ( Zone 0 ) -------------------
Compressible Euler equations.
Mach number: 0.294118.
Angle of attack (AoA): 0 deg, and angle of sideslip (AoS): 0 deg.
No restart solution, use the values at infinity (freestream).
Dimensional simulation.
The reference area is 1 m^2.
The semi-span will be computed using the max y(3D) value.
The reference length is 1 m.
Reference origin for moment evaluation is (0, 0, 0).
Surface(s) where the force coefficients are evaluated: BC_3.

Surface(s) plotted in the output file: BC_3.
Surface(s) affected by the design variables: BC_3.
Input mesh file name: ../aflr3/aflr3_CAPS.su2

--------------- Space Numerical Integration ( Zone 0 ) ------------------
Roe (with entropy fix = 0.001) solver for the flow inviscid terms.
Standard Roe without low-dissipation function.
Second order integration in space, with slope limiter.
Venkatakrishnan slope-limiting method, with constant: 0.05.
The reference element size is: 1. 
Gradient for upwind reconstruction: inverse-distance weighted Least-Squares.
Gradient for viscous and source terms: inverse-distance weighted Least-Squares.

--------------- Time Numerical Integration  ( Zone 0 ) ------------------
Local time stepping (steady state simulation).
Euler implicit method for the flow equations.
FGMRES is used for solving the linear system.
Using a ILU(0) preconditioning.
Convergence criteria of the linear solver: 1e-06.
Max number of linear iterations: 10.
V Multigrid Cycle, with 2 multigrid levels.
Damping factor for the residual restriction: 0.75.
Damping factor for the correction prolongation: 0.75.
No CFL adaptation.
+-------------------------------------------+
|  MG Level| Presmooth|PostSmooth|CorrectSmo|
+-------------------------------------------+
|         0|         1|         0|         0|
|         1|         2|         0|         0|
|         2|         3|         0|         0|
+-------------------------------------------+
Courant-Friedrichs-Lewy number:       10

------------------ Convergence Criteria  ( Zone 0 ) ---------------------
Maximum number of solver subiterations: 3.
Begin convergence monitoring at iteration 5.
Residual minimum value: 1e-14.
Cauchy series min. value: 1e-10.
Number of Cauchy elements: 100.
Begin windowed time average at iteration 0.

-------------------- Output Information ( Zone 0 ) ----------------------
File writing frequency: 
+------------------------------------+
|                     File| Frequency|
+------------------------------------+
|                  RESTART|       250|
|              SURFACE_CSV|       250|
|                  TECPLOT|       250|
|          SURFACE_TECPLOT|       250|
+------------------------------------+
Writing the convergence history file every 1 inner iterations.
Writing the screen convergence history every 1 inner iterations.
The tabular file format is CSV (.csv).
Convergence history file name: history.
Forces breakdown file name: forces_breakdown_aeroelasticSimple_Iterative.dat.
Surface file name: surface_flow_aeroelasticSimple_Iterative.
Volume file name: flow_aeroelasticSimple_Iterative.
Restart file name: restart_flow_aeroelasticSimple_Iterative.dat.

------------- Config File Boundary Information ( Zone 0 ) ---------------
+-----------------------------------------------------------------------+
|                        Marker Type|                        Marker Name|
+-----------------------------------------------------------------------+
|                         Euler wall|                               BC_3|
+-----------------------------------------------------------------------+
|                          Far-field|                               BC_1|
+-----------------------------------------------------------------------+
|                     Symmetry plane|                               BC_2|
+-----------------------------------------------------------------------+

-------------------- Output Preprocessing ( Zone 0 ) --------------------

WARNING: SURFACE_PRESSURE_DROP can only be computed for at least 2 surfaces (outlet, inlet, ...)

Screen output fields: TIME_ITER, OUTER_ITER, INNER_ITER, CUR_TIME, TIME_STEP, WALL_TIME, RMS_DENSITY, RMS_MOMENTUM-X, RMS_MOMENTUM-Y, RMS_ENERGY, EFFICIENCY
History output group(s): ITER, TIME_DOMAIN, WALL_TIME, RMS_RES, AERO_COEFF
Convergence field(s): RMS_DENSITY
Warning: No (valid) fields chosen for time convergence monitoring. Time convergence monitoring inactive.
Volume output fields: COORDINATES, SOLUTION, PRIMITIVE

------------------- Geometry Preprocessing ( Zone 0 ) -------------------
Three dimensional problem.
11301 grid points.
58551 volume elements.
3 surface markers.
3452 boundary elements in index 0 (Marker = BC_1).
1827 boundary elements in index 1 (Marker = BC_2).
195 boundary elements in index 2 (Marker = BC_3).
58551 tetrahedra.
Setting point connectivity.
Renumbering points (Reverse Cuthill McKee Ordering).
Recomputing point connectivity.
Setting element connectivity.
Checking the numerical grid orientation.
There has been a re-orientation of 27100 TETRAHEDRON volume elements.
There has been a re-orientation of 3235 TRIANGLE surface elements.
Identifying edges and vertices.
Setting the control volume structure.
Volume of the computational grid: 4.1102e+09.
Searching for the closest normal neighbors to the surfaces.
Storing a mapping from global to local point index.
Compute the surface curvature.
Max K: 42.3079. Mean K: 0.547697. Standard deviation K: 2.0063.
Checking for periodicity.
Computing mesh quality statistics for the dual control volumes.
+--------------------------------------------------------------+
|           Mesh Quality Metric|        Minimum|        Maximum|
+--------------------------------------------------------------+
|    Orthogonality Angle (deg.)|       0.627985|        85.0642|
|     CV Face Area Aspect Ratio|        1.44985|          34677|
|           CV Sub-Volume Ratio|              1|    5.46302e+06|
+--------------------------------------------------------------+
Setting the multigrid structure.
+-------------------------------------------+
|  MG Level|       CVs|Aggl. Rate|       CFL|
+-------------------------------------------+
|         0|     11301|    1/1.00|        10|
|         1|      1998|    1/5.66|   8.41881|
|         2|       411|    1/4.86|    7.4546|
+-------------------------------------------+
Finding max control volume width.
Semi-span length = 1.89763 m.
Wetted area = 5762.5 m^2.
Area projection in the x-plane = 1473.21 m^2, y-plane = 1717.92 m^2, z-plane = 123.508 m^2.
Max. coordinate in the x-direction = 6.80902 m, y-direction = 1.89763 m, z-direction = 474.436 m.
Min. coordinate in the x-direction = 0.0324872 m, y-direction = -32.3124 m, z-direction = -1.31748 m.
Checking if Euler &amp; Symmetry markers are straight/plane:
Boundary marker BC_3 is NOT a single plane.
Boundary marker BC_2 is NOT a single plane.
Computing wall distances.

-------------------- Solver Preprocessing ( Zone 0 ) --------------------
Inviscid flow: Computing density based on free-stream
temperature and pressure using the ideal gas law.
Force coefficients computed using free-stream values.

-- Models:
+------------------------------------------------------------------------------+
|          Viscosity Model|        Conductivity Model|              Fluid Model|
+------------------------------------------------------------------------------+
|                        -|                         -|             STANDARD_AIR|
+------------------------------------------------------------------------------+
-- Fluid properties:
+------------------------------------------------------------------------------+
|                  Name|    Dim. value|    Ref. value|      Unit|Non-dim. value|
+------------------------------------------------------------------------------+
|          Gas Constant|       287.058|             1|  N.m/kg.K|       287.058|
|      Spec. Heat Ratio|             -|             -|         -|           1.4|
+------------------------------------------------------------------------------+
-- Initial and free-stream conditions:
+------------------------------------------------------------------------------+
|                  Name|    Dim. value|    Ref. value|      Unit|Non-dim. value|
+------------------------------------------------------------------------------+
|       Static Pressure|        101325|             1|        Pa|        101325|
|               Density|       1.22498|             1|    kg/m^3|       1.22498|
|           Temperature|        288.15|             1|         K|        288.15|
|          Total Energy|        211798|             1|   m^2/s^2|        211798|
|            Velocity-X|       100.087|             1|       m/s|       100.087|
|            Velocity-Y|             0|             1|       m/s|             0|
|            Velocity-Z|             0|             1|       m/s|             0|
|    Velocity Magnitude|       100.087|             1|       m/s|       100.087|
+------------------------------------------------------------------------------+
|           Mach Number|             -|             -|         -|      0.294118|
+------------------------------------------------------------------------------+
Initialize Jacobian structure (Euler). MG level: 0.
Initialize Jacobian structure (Euler). MG level: 1.
Initialize Jacobian structure (Euler). MG level: 2.

------------------- Numerics Preprocessing ( Zone 0 ) -------------------

----------------- Integration Preprocessing ( Zone 0 ) ------------------

------------------- Iteration Preprocessing ( Zone 0 ) ------------------
Euler/Navier-Stokes/RANS fluid iteration.

------------------------------ Begin Solver -----------------------------

Simulation Run using the Single-zone Driver
WARNING: SU2 was not compiled for an AVX-capable architecture. Performance could be better,
         see <a href='https://su2code.github.io/docs_v7/Build-SU2-Linux-MacOS/#compiler-optimizations'>https://su2code.github.io/docs_v7/Build-SU2-Linux-MacOS/#compiler-optimizations</a>
WARNING: SU2 was not compiled for an AVX-capable architecture. Performance could be better,
         see <a href='https://su2code.github.io/docs_v7/Build-SU2-Linux-MacOS/#compiler-optimizations'>https://su2code.github.io/docs_v7/Build-SU2-Linux-MacOS/#compiler-optimizations</a>
WARNING: SU2 was not compiled for an AVX-capable architecture. Performance could be better,
         see <a href='https://su2code.github.io/docs_v7/Build-SU2-Linux-MacOS/#compiler-optimizations'>https://su2code.github.io/docs_v7/Build-SU2-Linux-MacOS/#compiler-optimizations</a>
+----------------------------------------------------------------------------------------------------------------------------------------------+
|   Time_Iter|  Outer_Iter|  Inner_Iter|    Cur_Time|   Time_Step|   Time(sec)|    rms[Rho]|   rms[RhoU]|   rms[RhoV]|   rms[RhoE]|        CEff|
+----------------------------------------------------------------------------------------------------------------------------------------------+
|           0|           0|           0|  0.0000e+00|  0.0000e+00|  1.7328e-01|    5.976390|    8.943243|    8.907682|   11.445496|   -0.033796|
|           0|           0|           1|  0.0000e+00|  0.0000e+00|  1.7946e-01|    6.427253|    8.962699|    8.955813|   11.829598|   -0.032181|
|           0|           0|           2|  0.0000e+00|  0.0000e+00|  1.8119e-01|    6.584833|    9.029467|    9.074330|   11.957314|   -0.030968|

----------------------------- Solver Exit -------------------------------

Maximum number of iterations reached (ITER = 3) before convergence.
+-----------------------------------------------------------------------+
|      Convergence Field     |     Value    |   Criterion  |  Converged |
+-----------------------------------------------------------------------+
|                    rms[Rho]|       6.58483|         &lt; -14|          No|
+-----------------------------------------------------------------------+
-------------------------------------------------------------------------
+-----------------------------------------------------------------------+
|        File Writing Summary       |              Filename             |
+-----------------------------------------------------------------------+
|SU2 binary restart                 |restart_flow_aeroelasticSimple_Iterative.dat|

Writing the forces breakdown file (forces_breakdown_aeroelasticSimple_Iterative.dat).
|CSV file                           |surface_flow_aeroelasticSimple_Iterative.csv|

Writing the forces breakdown file (forces_breakdown_aeroelasticSimple_Iterative.dat).
|Tecplot binary                     |flow_aeroelasticSimple_Iterative.szplt|

Writing the forces breakdown file (forces_breakdown_aeroelasticSimple_Iterative.dat).
|Tecplot binary surface             |surface_flow_aeroelasticSimple_Iterative.szplt|

Writing the forces breakdown file (forces_breakdown_aeroelasticSimple_Iterative.dat).
+-----------------------------------------------------------------------+
Warning: there are 598 non-physical points in the solution.
Warning: 38 reconstructed states for upwinding are non-physical.

--------------------------- Finalizing Solver ---------------------------
Deleted CNumerics container.
Deleted CIntegration container.
Deleted CSolver container.
Deleted CIteration container.
Deleted CInterface container.
Deleted CGeometry container.
Deleted CFreeFormDefBox class.
Deleted CSurfaceMovement class.
Deleted CVolumetricMovement class.
Deleted CConfig container.
Deleted nInst container.
Deleted COutput class.
-------------------------------------------------------------------------

------------------------- Exit Success (SU2_CFD) ------------------------


Running PostAnalysis ...... su2
Cl =  -751.30915
Cd =  24260.68865

real	0m38.045s
user	0m37.347s
sys	0m1.626s
+ status=0
+ set +x

=================================================
CAPS verification (using pyCAPS) case aeroelasticSimple_Iterative_SU2_and_Astros.py passed (as expected)
=================================================


=================================================
+ echo 'aeroelastic_Iterative_SU2_and_Astros.py test;'
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESP126/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
aeroelastic_Iterative_SU2_and_Astros.py test;
+ python -u aeroelastic_Iterative_SU2_and_Astros.py -outLevel=0
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESP126/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt

Running PreAnalysis ...... su2
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 3
	Name = Farfield, index = 1
	Name = SymmPlane, index = 2
	Name = Skin, index = 3
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 0
 
AFLR2    : ---------------------------------------
AFLR2    : AFLR2 LIBRARY
AFLR2    : ADVANCING-FRONT/LOCAL-RECONNECTION
AFLR2    : TRIA/QUAD GRID GENERATOR
AFLR2    : Version Number 9.18.1
AFLR2    : Version Date   06/11/24 @ 05:52PM
AFLR2    : Compile OS     Darwin 23.5.0 arm64
AFLR2    : Compile Date   06/11/24 @ 05:52PM
AFLR2    : Copyright 1994-2021, D.L. Marcum
AFLR2    : ---------------------------------------
 
AFLR4    : ---------------------------------------
AFLR4    : AFLR4 LIBRARY
AFLR4    : ADVANCING-FRONT/LOCAL-RECONNECTION
AFLR4    : TRIA/QUAD SURFACE GRID GENERATOR
AFLR4    : Version Number 11.5.15
AFLR4    : Version Date   07/19/24 @ 07:04PM
AFLR4    : Compile OS     Darwin 23.5.0 arm64
AFLR4    : Compile Date   07/19/24 @ 07:06PM
AFLR4    : Copyright 1994-2021, D.L. Marcum
AFLR4    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.8.1
EGADS    : ---------------------------------------

EGADS    : EGADS CAD Geometry Setup

EGADS    : Model has 1 Active Bodies

EGADS    : Body 0 is a SolidBody
EGADS    : Body 0 has 1 Shells
EGADS    : Body 0 has 9 Faces
EGADS    : Body 0 has 18 Edges
EGADS    : Body 0 has 10 Loops
EGADS    : Body 0 has 12 Nodes

EGADS    : Check Grid BCs

EGADS    : Grid BCs are OK

EGADS    : Face Neighbor-Faces Information

EGADS    : QC  = Face Quad Combination Flag
EGADS    : IER = Face Isolated Edge Refinement Flag
EGADS    : ER  = Face Edge Refinement Factor
EGADS    :       Not applicable for Faces with a FarField Grid BC.
EGADS    : SF  = Face Scale Factor
EGADS    :       Not applicable for Faces with a FarField Grid BC.

EGADS    :   Face          Body    QC   IER       ER    Scale   Neighbor
EGADS    :     ID  Active    ID  Flag  Flag   Weight   Factor   Faces
EGADS    :      1     Yes     0     0     1        0        1   2 3 4 5
EGADS    :      2     Yes     0     0     1        0        1   1 3 5 6
EGADS    :      3     Yes     0     0     1        0        1   1 2 4 6 7 8
EGADS    :      4     Yes     0     0     1        0        1   1 3 5 6
EGADS    :      5     Yes     0     0     1        0        1   1 2 4 6
EGADS    :      6     Yes     0     0     1        0        1   2 3 4 5
EGADS    :      7     Yes     0     0     1        0        1   3 8 9
EGADS    :      8     Yes     0     0     1        0        1   3 7 9
EGADS    :      9     Yes     0     0     1        0        1   7 8

EGADS    : Face Edges Information

EGADS    :   Face   Edges
EGADS    :      1   1 2 -3 -4
EGADS    :      2   5 6 -7 -1
EGADS    :      3   -2 7 9 -8 -10 -11
EGADS    :      4   -12 3 8 -13
EGADS    :      5   4 12 -14 -5
EGADS    :      6   -6 14 13 -9
EGADS    :      7   15 10 -17 -16
EGADS    :      8   17 11 -15 -18
EGADS    :      9   16 18

EGADS    : Face Loops Information

EGADS    :   Face   Loops
EGADS    :      1   1
EGADS    :      2   2
EGADS    :      3   3 4
EGADS    :      4   5
EGADS    :      5   6
EGADS    :      6   7
EGADS    :      7   8
EGADS    :      8   9
EGADS    :      9   10

EGADS    : Loop Edges Information

EGADS    :   Loop  Active   Edges
EGADS    :      1     Yes   1 2 -3 -4
EGADS    :      2     Yes   5 6 -7 -1
EGADS    :      3     Yes   -2 7 9 -8
EGADS    :      4     Yes   -10 -11
EGADS    :      5     Yes   -12 3 8 -13
EGADS    :      6     Yes   4 12 -14 -5
EGADS    :      7     Yes   -6 14 13 -9
EGADS    :      8     Yes   15 10 -17 -16
EGADS    :      9     Yes   17 11 -15 -18
EGADS    :     10     Yes   16 18

EGADS    : Edge Node, Scale Factor, and Neighbor-Faces Information

EGADS    : ESF = Edge Scale Factor
EGADS    :       Not applicable for DEGENERATE Edges or Edges with a FarField
EGADS    :       Grid BC Neighbor Face.

EGADS    :                                             Neighbor
EGADS    :   Edge  Body  Active Node1 Node2      ESF   Faces
EGADS    :      1     0     Yes     2     1        1   1 2
EGADS    :      2     0     Yes     1     3        1   1 3
EGADS    :      3     0     Yes     4     3        1   1 4
EGADS    :      4     0     Yes     2     4        1   1 5
EGADS    :      5     0     Yes     2     5        1   2 5
EGADS    :      6     0     Yes     5     6        1   2 6
EGADS    :      7     0     Yes     1     6        1   2 3
EGADS    :      8     0     Yes     3     7        1   3 4
EGADS    :      9     0     Yes     6     7        1   3 6
EGADS    :     10     0     Yes     8     9        1   3 7
EGADS    :     11     0     Yes     9     8        1   3 8
EGADS    :     12     0     Yes     4    10        1   4 5
EGADS    :     13     0     Yes    10     7        1   4 6
EGADS    :     14     0     Yes     5    10        1   5 6
EGADS    :     15     0     Yes    11     8        1   7 8
EGADS    :     16     0     Yes    11    12        1   7 9
EGADS    :     17     0     Yes    12     9        1   7 8
EGADS    :     18     0     Yes    12    11        1   8 9

EGADS    : Node Information

EGADS    :   Node  Active      Coordinates
EGADS    :      1     Yes                0                0                0
EGADS    :      2     Yes                0               40                0
EGADS    :      3     Yes                0                0               20
EGADS    :      4     Yes                0               40               20
EGADS    :      5     Yes               20               40                0
EGADS    :      6     Yes               20                0                0
EGADS    :      7     Yes               20                0               20
EGADS    :      8     Yes       1.61374306                0                0
EGADS    :      9     Yes                0                0                0
EGADS    :     10     Yes               20               40               20
EGADS    :     11     Yes       2.53650745       3.87298335      0.334116517
EGADS    :     12     Yes       1.57194608       3.87298335      0.249728332

EGADS    : Face and Edge Match Information

EGADS    : No Face Matches Found

AFLR4    : Surface Mesh Spacing Setup

AFLR4    : Max Bounding Box Length     = 40
AFLR4    : Min Bounding Box Length     = 40
AFLR4    : Max Ref Bounding Box Length = 40
AFLR4    : Min Ref Bounding Box Length = 40
AFLR4    : Reference Length            = 1.61374
AFLR4    : BL Thickness                = 0
AFLR4    : Abs Min Surf Spacing        = 0.00403436
AFLR4    : Min Surf Spacing            = 0.161374
AFLR4    : Max Surf Spacing            = 1.21031
AFLR4    : Global Scale Factor         = 2

AFLR4    : Geometry Definition Information

AFLR4    : Definition              Definition   Composite             Grid BC
AFLR4    :         ID                    Type          ID                Type
AFLR4    :          0     glue-only composite           -                   -
AFLR4    :          1            CAD geometry           0            STD w/BL
AFLR4    :          2            CAD geometry           0            STD w/BL
AFLR4    :          3            CAD geometry           0            STD w/BL
AFLR4    :          4            CAD geometry           0            STD w/BL
AFLR4    :          5            CAD geometry           0            STD w/BL
AFLR4    :          6            CAD geometry           0            STD w/BL
AFLR4    :          7            CAD geometry           0            STD w/BL
AFLR4    :          8            CAD geometry           0            STD w/BL
AFLR4    :          9            CAD geometry           0            STD w/BL

AFLR4    : Define CAD surface definition 1
AFLR4    : Define CAD surface definition 2
AFLR4    : Define CAD surface definition 3
AFLR4    : Define CAD surface definition 4
AFLR4    : Define CAD surface definition 5
AFLR4    : Define CAD surface definition 6
AFLR4    : Define CAD surface definition 7
AFLR4    : Define CAD surface definition 8
AFLR4    : Define CAD surface definition 9

AFLR4    : Surface Grid Generation

AFLR4    : Generate optimal mesh on surface definition 1
AFLR2    : Nodes, Trias,Quads=       376       682         0
AFLR4    : Nodes, Trias,Quads=       381       692         0

AFLR4    : Generate optimal mesh on surface definition 2
AFLR2    : Nodes, Trias,Quads=       374       678         0
AFLR4    : Nodes, Trias,Quads=       380       690         0

AFLR4    : Generate optimal mesh on surface definition 3
AFLR2    : Nodes, Trias,Quads=       927      1777         0
AFLR4    : Nodes, Trias,Quads=       821      1565         0

AFLR4    : Generate optimal mesh on surface definition 4
AFLR2    : Nodes, Trias,Quads=       376       682         0
AFLR4    : Nodes, Trias,Quads=       380       690         0

AFLR4    : Generate optimal mesh on surface definition 5
AFLR2    : Nodes, Trias,Quads=       374       678         0
AFLR4    : Nodes, Trias,Quads=       380       690         0

AFLR4    : Generate optimal mesh on surface definition 6
AFLR2    : Nodes, Trias,Quads=       376       682         0
AFLR4    : Nodes, Trias,Quads=       378       686         0

AFLR4    : Generate optimal mesh on surface definition 7
AFLR2    : Nodes, Trias,Quads=        63        96         0
AFLR4    : Nodes, Trias,Quads=        55        80         0

AFLR4    : Generate optimal mesh on surface definition 8
AFLR2    : Nodes, Trias,Quads=        64        96         0
AFLR4    : Nodes, Trias,Quads=        57        82         0

AFLR4    : Generate optimal mesh on surface definition 9
AFLR2    : Nodes, Trias,Quads=        11        13         0
AFLR4    : Nodes, Trias,Quads=         7         5         0

DGEOM    : Add surface definitions to composite definition 0
DGEOM    : Glue composite surface definition 0
DGEOM    : Nodes,Faces,BEdges=      2592      5180       482

AFLR4    : Curvature BG Surface Grid Generation

AFLR4    : Nodes, Faces      =      2592      5180

AFLR4    : Surface Grid Generation

AFLR4    : Generate optimal mesh on surface definition 1
AFLR2    : Nodes, Trias,Quads=       385       700         0
AFLR4    : Nodes, Trias,Quads=       380       690         0

AFLR4    : Generate optimal mesh on surface definition 2
AFLR2    : Nodes, Trias,Quads=       385       700         0
AFLR4    : Nodes, Trias,Quads=       381       692         0

AFLR4    : Generate optimal mesh on surface definition 3
AFLR2    : Nodes, Trias,Quads=      1009      1939         0
AFLR4    : Nodes, Trias,Quads=       953      1827         0

AFLR4    : Generate optimal mesh on surface definition 4
AFLR2    : Nodes, Trias,Quads=       383       696         0
AFLR4    : Nodes, Trias,Quads=       378       686         0

AFLR4    : Generate optimal mesh on surface definition 5
AFLR2    : Nodes, Trias,Quads=       383       696         0
AFLR4    : Nodes, Trias,Quads=       382       694         0

AFLR4    : Generate optimal mesh on surface definition 6
AFLR2    : Nodes, Trias,Quads=       381       692         0
AFLR4    : Nodes, Trias,Quads=       380       690         0

AFLR4    : Generate optimal mesh on surface definition 7
AFLR2    : Nodes, Trias,Quads=        74       115         0
AFLR4    : Nodes, Trias,Quads=        65        97         0

AFLR4    : Generate optimal mesh on surface definition 8
AFLR2    : Nodes, Trias,Quads=        75       116         0
AFLR4    : Nodes, Trias,Quads=        63        92         0

AFLR4    : Generate optimal mesh on surface definition 9
AFLR2    : Nodes, Trias,Quads=        12        14         0
AFLR4    : Nodes, Trias,Quads=         8         6         0

DGEOM    : Add surface definitions to composite definition 0
DGEOM    : Glue composite surface definition 0
DGEOM    : Nodes,Faces,BEdges=      2739      5474       490

OVERALL  : CPU Time          =     0.061   seconds
Body 1 (of 1)
Number of nodes    = 2739
Number of elements = 5474
Number of triangle elements      = 5474
Number of quadrilateral elements = 0
----------------------------
Total number of nodes    = 2739
Total number of elements = 5474
Total number of triangle elements      = 5474
Total number of quadrilateral elements = 0
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 0
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 3
	Name = Farfield, index = 1
	Name = SymmPlane, index = 2
	Name = Skin, index = 3
Getting volume mesh
 
AFLR2    : ---------------------------------------
AFLR2    : AFLR2 LIBRARY
AFLR2    : ADVANCING-FRONT/LOCAL-RECONNECTION
AFLR2    : TRIA/QUAD GRID GENERATOR
AFLR2    : Version Number 9.18.1
AFLR2    : Version Date   06/11/24 @ 05:52PM
AFLR2    : Compile OS     Darwin 23.5.0 arm64
AFLR2    : Compile Date   06/11/24 @ 05:52PM
AFLR2    : Copyright 1994-2021, D.L. Marcum
AFLR2    : ---------------------------------------
 
AFLR4    : ---------------------------------------
AFLR4    : AFLR4 LIBRARY
AFLR4    : ADVANCING-FRONT/LOCAL-RECONNECTION
AFLR4    : TRIA/QUAD SURFACE GRID GENERATOR
AFLR4    : Version Number 11.5.15
AFLR4    : Version Date   07/19/24 @ 07:04PM
AFLR4    : Compile OS     Darwin 23.5.0 arm64
AFLR4    : Compile Date   07/19/24 @ 07:06PM
AFLR4    : Copyright 1994-2021, D.L. Marcum
AFLR4    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.8.1
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.8.1
EGADS    : ---------------------------------------
Volume mesh:
	Number of nodes          = 11301
	Number of elements       = 64025
	Number of triangles      = 5474
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 58551
	Number of pyramids       = 0
	Number of prisms         = 0
	Number of hexahedrals    = 0

Writing SU2 file ....
Finished writing SU2 file

Getting CFD boundary conditions
	Boundary condition name - Farfield
	Boundary condition name - Skin
	Boundary condition name - SymmPlane
	Done getting CFD boundary conditions
Writing SU2 data transfer files
Writing SU2 Motion File - aeroelastic_Iterative_motion.dat
Warning: The su2 cfg file will be overwritten!
Write SU2 configuration file for version "Harrier (8.0.1)"


Running SU2......

-------------------------------------------------------------------------
|    ___ _   _ ___                                                      |
|   / __| | | |_  )   Release 8.0.0 "Harrier"                           |
|   \__ \ |_| |/ /                                                      |
|   |___/\___//___|   Suite (Computational Fluid Dynamics Code)         |
|                                                                       |
-------------------------------------------------------------------------
| SU2 Project Website: <a href='https://su2code.github.io'>https://su2code.github.io</a>                        |
|                                                                       |
| The SU2 Project is maintained by the SU2 Foundation                   |
| (<a href='http://su2foundation.org'>http://su2foundation.org</a>)                                            |
-------------------------------------------------------------------------
| Copyright 2012-2023, SU2 Contributors                                 |
|                                                                       |
| SU2 is free software; you can redistribute it and/or                  |
| modify it under the terms of the GNU Lesser General Public            |
| License as published by the Free Software Foundation; either          |
| version 2.1 of the License, or (at your option) any later version.    |
|                                                                       |
| SU2 is distributed in the hope that it will be useful,                |
| but WITHOUT ANY WARRANTY; without even the implied warranty of        |
| MERCHANTABILITY or FITNESS FOR A PARTICULAR PURPOSE. See the GNU      |
| Lesser General Public License for more details.                       |
|                                                                       |
| You should have received a copy of the GNU Lesser General Public      |
| License along with SU2. If not, see &lt;<a href='http://www.gnu.org/licenses/'>http://www.gnu.org/licenses/</a>&gt;.   |
-------------------------------------------------------------------------

Parsing config file for zone 0

----------------- Physical Case Definition ( Zone 0 ) -------------------
Compressible Euler equations.
Mach number: 0.294118.
Angle of attack (AoA): 0 deg, and angle of sideslip (AoS): 0 deg.
No restart solution, use the values at infinity (freestream).
Dimensional simulation.
The reference area is 1 m^2.
The semi-span will be computed using the max y(3D) value.
The reference length is 1 m.
Reference origin for moment evaluation is (0, 0, 0).
Surface(s) where the force coefficients are evaluated: BC_3.

Surface(s) plotted in the output file: BC_3.
Surface(s) affected by the design variables: BC_3.
Input mesh file name: ../aflr3/aflr3_CAPS.su2

--------------- Space Numerical Integration ( Zone 0 ) ------------------
Roe (with entropy fix = 0.001) solver for the flow inviscid terms.
Standard Roe without low-dissipation function.
Second order integration in space, with slope limiter.
Venkatakrishnan slope-limiting method, with constant: 0.05.
The reference element size is: 1. 
Gradient for upwind reconstruction: inverse-distance weighted Least-Squares.
Gradient for viscous and source terms: inverse-distance weighted Least-Squares.

--------------- Time Numerical Integration  ( Zone 0 ) ------------------
Local time stepping (steady state simulation).
Euler implicit method for the flow equations.
FGMRES is used for solving the linear system.
Using a ILU(0) preconditioning.
Convergence criteria of the linear solver: 1e-06.
Max number of linear iterations: 10.
V Multigrid Cycle, with 2 multigrid levels.
Damping factor for the residual restriction: 0.75.
Damping factor for the correction prolongation: 0.75.
No CFL adaptation.
+-------------------------------------------+
|  MG Level| Presmooth|PostSmooth|CorrectSmo|
+-------------------------------------------+
|         0|         1|         0|         0|
|         1|         2|         0|         0|
|         2|         3|         0|         0|
+-------------------------------------------+
Courant-Friedrichs-Lewy number:       10

------------------ Convergence Criteria  ( Zone 0 ) ---------------------
Maximum number of solver subiterations: 3.
Begin convergence monitoring at iteration 5.
Residual minimum value: 1e-14.
Cauchy series min. value: 1e-10.
Number of Cauchy elements: 100.
Begin windowed time average at iteration 0.

-------------------- Output Information ( Zone 0 ) ----------------------
File writing frequency: 
+------------------------------------+
|                     File| Frequency|
+------------------------------------+
|                  RESTART|       250|
|              SURFACE_CSV|       250|
|                  TECPLOT|       250|
|          SURFACE_TECPLOT|       250|
+------------------------------------+
Writing the convergence history file every 1 inner iterations.
Writing the screen convergence history every 1 inner iterations.
The tabular file format is CSV (.csv).
Convergence history file name: history.
Forces breakdown file name: forces_breakdown_aeroelastic_Iterative.dat.
Surface file name: surface_flow_aeroelastic_Iterative.
Volume file name: flow_aeroelastic_Iterative.
Restart file name: restart_flow_aeroelastic_Iterative.dat.

------------- Config File Boundary Information ( Zone 0 ) ---------------
+-----------------------------------------------------------------------+
|                        Marker Type|                        Marker Name|
+-----------------------------------------------------------------------+
|                         Euler wall|                               BC_3|
+-----------------------------------------------------------------------+
|                          Far-field|                               BC_1|
+-----------------------------------------------------------------------+
|                     Symmetry plane|                               BC_2|
+-----------------------------------------------------------------------+

-------------------- Output Preprocessing ( Zone 0 ) --------------------

WARNING: SURFACE_PRESSURE_DROP can only be computed for at least 2 surfaces (outlet, inlet, ...)

Screen output fields: TIME_ITER, OUTER_ITER, INNER_ITER, CUR_TIME, TIME_STEP, WALL_TIME, RMS_DENSITY, RMS_MOMENTUM-X, RMS_MOMENTUM-Y, RMS_ENERGY, EFFICIENCY
History output group(s): ITER, TIME_DOMAIN, WALL_TIME, RMS_RES, AERO_COEFF
Convergence field(s): RMS_DENSITY
Warning: No (valid) fields chosen for time convergence monitoring. Time convergence monitoring inactive.
Volume output fields: COORDINATES, SOLUTION, PRIMITIVE

------------------- Geometry Preprocessing ( Zone 0 ) -------------------
Three dimensional problem.
11301 grid points.
58551 volume elements.
3 surface markers.
3452 boundary elements in index 0 (Marker = BC_1).
1827 boundary elements in index 1 (Marker = BC_2).
195 boundary elements in index 2 (Marker = BC_3).
58551 tetrahedra.
Setting point connectivity.
Renumbering points (Reverse Cuthill McKee Ordering).
Recomputing point connectivity.
Setting element connectivity.
Checking the numerical grid orientation.
All volume elements are correctly orientend.
All surface elements are correctly orientend.
Identifying edges and vertices.
Setting the control volume structure.
Volume of the computational grid: 63999.5.
Searching for the closest normal neighbors to the surfaces.
Storing a mapping from global to local point index.
Compute the surface curvature.
Max K: 47.1143. Mean K: 0.755059. Standard deviation K: 3.51124.
Checking for periodicity.
Computing mesh quality statistics for the dual control volumes.
+--------------------------------------------------------------+
|           Mesh Quality Metric|        Minimum|        Maximum|
+--------------------------------------------------------------+
|    Orthogonality Angle (deg.)|        54.7348|        85.4032|
|     CV Face Area Aspect Ratio|        1.05389|        21.5536|
|           CV Sub-Volume Ratio|              1|        13.9349|
+--------------------------------------------------------------+
Setting the multigrid structure.
+-------------------------------------------+
|  MG Level|       CVs|Aggl. Rate|       CFL|
+-------------------------------------------+
|         0|     11301|    1/1.00|        10|
|         1|      2021|    1/5.59|   8.45099|
|         2|       414|    1/4.88|   7.47269|
+-------------------------------------------+
Finding max control volume width.
Semi-span length = 3.87298 m.
Wetted area = 8.08979 m^2.
Area projection in the x-plane = 0.572014 m^2, y-plane = 0.261888 m^2, z-plane = 3.84035 m^2.
Max. coordinate in the x-direction = 2.53651 m, y-direction = 3.87298 m, z-direction = 0.380358 m.
Min. coordinate in the x-direction = 0 m, y-direction = -2.8602e-18 m, z-direction = -0.0467106 m.
Checking if Euler &amp; Symmetry markers are straight/plane:
Boundary marker BC_3 is NOT a single plane.
Boundary marker BC_2 is a single plane.
Computing wall distances.

-------------------- Solver Preprocessing ( Zone 0 ) --------------------
Inviscid flow: Computing density based on free-stream
temperature and pressure using the ideal gas law.
Force coefficients computed using free-stream values.

-- Models:
+------------------------------------------------------------------------------+
|          Viscosity Model|        Conductivity Model|              Fluid Model|
+------------------------------------------------------------------------------+
|                        -|                         -|             STANDARD_AIR|
+------------------------------------------------------------------------------+
-- Fluid properties:
+------------------------------------------------------------------------------+
|                  Name|    Dim. value|    Ref. value|      Unit|Non-dim. value|
+------------------------------------------------------------------------------+
|          Gas Constant|       287.058|             1|  N.m/kg.K|       287.058|
|      Spec. Heat Ratio|             -|             -|         -|           1.4|
+------------------------------------------------------------------------------+
-- Initial and free-stream conditions:
+------------------------------------------------------------------------------+
|                  Name|    Dim. value|    Ref. value|      Unit|Non-dim. value|
+------------------------------------------------------------------------------+
|       Static Pressure|        101325|             1|        Pa|        101325|
|               Density|       1.22498|             1|    kg/m^3|       1.22498|
|           Temperature|        288.15|             1|         K|        288.15|
|          Total Energy|        211798|             1|   m^2/s^2|        211798|
|            Velocity-X|       100.087|             1|       m/s|       100.087|
|            Velocity-Y|             0|             1|       m/s|             0|
|            Velocity-Z|             0|             1|       m/s|             0|
|    Velocity Magnitude|       100.087|             1|       m/s|       100.087|
+------------------------------------------------------------------------------+
|           Mach Number|             -|             -|         -|      0.294118|
+------------------------------------------------------------------------------+
Initialize Jacobian structure (Euler). MG level: 0.
Initialize Jacobian structure (Euler). MG level: 1.
Initialize Jacobian structure (Euler). MG level: 2.

------------------- Numerics Preprocessing ( Zone 0 ) -------------------

----------------- Integration Preprocessing ( Zone 0 ) ------------------

------------------- Iteration Preprocessing ( Zone 0 ) ------------------
Euler/Navier-Stokes/RANS fluid iteration.

------------------------------ Begin Solver -----------------------------

Simulation Run using the Single-zone Driver
WARNING: SU2 was not compiled for an AVX-capable architecture. Performance could be better,
         see <a href='https://su2code.github.io/docs_v7/Build-SU2-Linux-MacOS/#compiler-optimizations'>https://su2code.github.io/docs_v7/Build-SU2-Linux-MacOS/#compiler-optimizations</a>
WARNING: SU2 was not compiled for an AVX-capable architecture. Performance could be better,
         see <a href='https://su2code.github.io/docs_v7/Build-SU2-Linux-MacOS/#compiler-optimizations'>https://su2code.github.io/docs_v7/Build-SU2-Linux-MacOS/#compiler-optimizations</a>
WARNING: SU2 was not compiled for an AVX-capable architecture. Performance could be better,
         see <a href='https://su2code.github.io/docs_v7/Build-SU2-Linux-MacOS/#compiler-optimizations'>https://su2code.github.io/docs_v7/Build-SU2-Linux-MacOS/#compiler-optimizations</a>
+----------------------------------------------------------------------------------------------------------------------------------------------+
|   Time_Iter|  Outer_Iter|  Inner_Iter|    Cur_Time|   Time_Step|   Time(sec)|    rms[Rho]|   rms[RhoU]|   rms[RhoV]|   rms[RhoE]|        CEff|
+----------------------------------------------------------------------------------------------------------------------------------------------+
|           0|           0|           0|  0.0000e+00|  0.0000e+00|  1.6728e-01|   -0.790402|    1.509543|    1.185099|    4.678704|   -1.072828|
|           0|           0|           1|  0.0000e+00|  0.0000e+00|  1.6617e-01|   -1.125423|    1.402824|    1.016209|    4.328795|   -0.842279|
|           0|           0|           2|  0.0000e+00|  0.0000e+00|  1.6532e-01|   -1.188494|    1.266186|    0.868459|    4.264282|   -0.355290|

----------------------------- Solver Exit -------------------------------

Maximum number of iterations reached (ITER = 3) before convergence.
+-----------------------------------------------------------------------+
|      Convergence Field     |     Value    |   Criterion  |  Converged |
+-----------------------------------------------------------------------+
|                    rms[Rho]|      -1.18849|         &lt; -14|          No|
+-----------------------------------------------------------------------+
-------------------------------------------------------------------------
+-----------------------------------------------------------------------+
|        File Writing Summary       |              Filename             |
+-----------------------------------------------------------------------+
|SU2 binary restart                 |restart_flow_aeroelastic_Iterative.dat|

Writing the forces breakdown file (forces_breakdown_aeroelastic_Iterative.dat).
|CSV file                           |surface_flow_aeroelastic_Iterative.csv|

Writing the forces breakdown file (forces_breakdown_aeroelastic_Iterative.dat).
|Tecplot binary                     |flow_aeroelastic_Iterative.szplt   |

Writing the forces breakdown file (forces_breakdown_aeroelastic_Iterative.dat).
|Tecplot binary surface             |surface_flow_aeroelastic_Iterative.szplt|

Writing the forces breakdown file (forces_breakdown_aeroelastic_Iterative.dat).
+-----------------------------------------------------------------------+

--------------------------- Finalizing Solver ---------------------------
Deleted CNumerics container.
Deleted CIntegration container.
Deleted CSolver container.
Deleted CIteration container.
Deleted CInterface container.
Deleted CGeometry container.
Deleted CFreeFormDefBox class.
Deleted CSurfaceMovement class.
Deleted CVolumetricMovement class.
Deleted CConfig container.
Deleted nInst container.
Deleted COutput class.
-------------------------------------------------------------------------

------------------------- Exit Success (SU2_CFD) ------------------------


Running PostAnalysis ...... su2

Running PreAnalysis ...... su2
Mapping Csys attributes ................
	Number of unique Csys attributes = 0

Getting FEA coordinate systems.......
	Number of coordinate systems - 0
	No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
	Number of unique capsConstraint attributes = 1
	Name = Rib_Root, index = 1
Mapping capsLoad attributes ................
	Number of unique capsLoad attributes = 0
Mapping capsBound attributes ................
	Number of unique capsBound attributes = 3
	Name = Skin_Top, index = 1
	Name = Skin_Bottom, index = 2
	Name = Skin_Tip, index = 3
Mapping capsConnect attributes ................
	Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
	Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
	Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 3
	Name = Ribs_and_Spars, index = 1
	Name = Skin, index = 2
	Name = Rib_Root, index = 3
Setting FEA Data
	Mesh for body = 0
	Number of nodal coordinates = 746
	Number of elements = 898
	Elemental Nodes = 0
	Elemental Rods  = 0
	Elemental Tria3 = 120
	Elemental Quad4 = 778
Aero_Reference value is NULL - No aero reference parameters set

Getting FEA materials.......
	Number of materials - 2
	Material name - Madeupium
	Material name - Unobtainium
	Done getting FEA materials

Getting FEA properties.......
	Number of properties - 3
	Property name - Rib_Root
	Property name - Ribs_and_Spars
	Property name - Skin
	Done getting FEA properties
Updating mesh element types based on properties input

Getting FEA constraints.......
	Number of constraints - 1
	Constraint name - edgeConstraint
	No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement"
	Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults

Getting FEA loads.......
	Number of loads - 1
	Load name - pressureAero
	No "groupName" specified for Load tuple pressureAero, going to use load name
	Done getting FEA loads
Optimization Control tuple is NULL - Default optimization control is used

Getting FEA optimization control.......
Done getting FEA Optimization Control
Design_Variable tuple is NULL - No design variables applied
Design_Constraint tuple is NULL - No design constraints applied
Analysis tuple is NULL

Getting FEA analyses.......
	Number of analyses - 1
	Analysis name - Default
	Done getting FEA analyses
Reading SU2 AeroLoad File - surface_flow_aeroelastic_Iterative.csv
	Number of variables = 16
	Number of data points = 104
 CAPS Info: Bound 'Skin_Top' Normalized Integrated 'Pressure'
            Rank 0: src = 3.095468e+09, tgt = 3.095468e+09, diff = 6.724647e+01
Reading SU2 AeroLoad File - surface_flow_aeroelastic_Iterative.csv
	Number of variables = 16
	Number of data points = 104
 CAPS Info: Bound 'Skin_Bottom' Normalized Integrated 'Pressure'
            Rank 0: src = 3.008438e+09, tgt = 3.008438e+09, diff = 7.140274e+01
Reading SU2 AeroLoad File - surface_flow_aeroelastic_Iterative.csv
	Number of variables = 16
	Number of data points = 104
 CAPS Info: Bound 'Skin_Tip' Normalized Integrated 'Pressure'
            Rank 0: src = 4.099882e+07, tgt = 4.099881e+07, diff = 2.658112e+00
Extracting external pressure loads from data transfer....
	TransferName = Skin_Top
	Number of Elements = 330 (total = 330)
Extracting external pressure loads from data transfer....
	TransferName = Skin_Bottom
	Number of Elements = 330 (total = 660)
Extracting external pressure loads from data transfer....
	TransferName = Skin_Tip
	Number of Elements = 30 (total = 690)

Writing Astros grid and connectivity file (in free field format) ....
Finished writing Astros grid file

Writing subElement types (if any) - appending mesh file

Writing Astros instruction file....
	Writing analysis cards
	Writing load ADD cards
	Writing constraint cards--each subcase individually
	Writing load cards
	Writing material cards
	Writing property cards
Note: The following floating-point exceptions are signalling: IEEE_UNDERFLOW_FLAG
Writing SU2 data transfer files
Writing SU2 Motion File - aeroelastic_Iterative_motion.dat
Warning: The su2 cfg file will be overwritten!
Write SU2 configuration file for version "Harrier (8.0.1)"


Running SU2......

-------------------------------------------------------------------------
|    ___ _   _ ___                                                      |
|   / __| | | |_  )   Release 8.0.0 "Harrier"                           |
|   \__ \ |_| |/ /                                                      |
|   |___/\___//___|   Suite (Mesh Deformation Code)                     |
|                                                                       |
-------------------------------------------------------------------------
| SU2 Project Website: <a href='https://su2code.github.io'>https://su2code.github.io</a>                        |
|                                                                       |
| The SU2 Project is maintained by the SU2 Foundation                   |
| (<a href='http://su2foundation.org'>http://su2foundation.org</a>)                                            |
-------------------------------------------------------------------------
| Copyright 2012-2023, SU2 Contributors                                 |
|                                                                       |
| SU2 is free software; you can redistribute it and/or                  |
| modify it under the terms of the GNU Lesser General Public            |
| License as published by the Free Software Foundation; either          |
| version 2.1 of the License, or (at your option) any later version.    |
|                                                                       |
| SU2 is distributed in the hope that it will be useful,                |
| but WITHOUT ANY WARRANTY; without even the implied warranty of        |
| MERCHANTABILITY or FITNESS FOR A PARTICULAR PURPOSE. See the GNU      |
| Lesser General Public License for more details.                       |
|                                                                       |
| You should have received a copy of the GNU Lesser General Public      |
| License along with SU2. If not, see &lt;<a href='http://www.gnu.org/licenses/'>http://www.gnu.org/licenses/</a>&gt;.   |
-------------------------------------------------------------------------

----------------- Physical Case Definition ( Zone 0 ) -------------------
Input mesh file name: ../aflr3/aflr3_CAPS.su2

---------------- Grid deformation parameters ( Zone 0 )  ----------------
Grid deformation using a linear elasticity method.


-------------------- Output Information ( Zone 0 ) ----------------------
Output mesh file name: ../aflr3/aflr3_CAPS.su2. 
Cell stiffness scaled by distance to nearest solid surface.

------------- Config File Boundary Information ( Zone 0 ) ---------------
+-----------------------------------------------------------------------+
|                        Marker Type|                        Marker Name|
+-----------------------------------------------------------------------+
|                         Euler wall|                               BC_3|
+-----------------------------------------------------------------------+
|                          Far-field|                               BC_1|
+-----------------------------------------------------------------------+
|                     Symmetry plane|                               BC_2|
+-----------------------------------------------------------------------+
Three dimensional problem.
11301 grid points.
58551 volume elements.
3 surface markers.
3452 boundary elements in index 0 (Marker = BC_1).
1827 boundary elements in index 1 (Marker = BC_2).
195 boundary elements in index 2 (Marker = BC_3).
58551 tetrahedra.

----------------------- Preprocessing computations ----------------------
Setting local point connectivity.
Checking the numerical grid orientation of the interior elements.
All volume elements are correctly orientend.
All surface elements are correctly orientend.
Identify edges and vertices.
Setting the bound control volume structure.
Volume of the computational grid: 63999.5.
  Info: Ignoring the following volume output fields/groups:
  SOLUTION
Volume output fields: COORDINATES
  Info: Ignoring the following screen output fields:
  RMS_DENSITY, RMS_MOMENTUM-X, RMS_MOMENTUM-Y, RMS_ENERGY, EFFICIENCY
Screen output fields: TIME_ITER, OUTER_ITER, INNER_ITER, CUR_TIME, TIME_STEP, WALL_TIME
  Info: Ignoring the following history output groups:
  RMS_RES, AERO_COEFF
History output group(s): ITER, TIME_DOMAIN, WALL_TIME
Warning: No (valid) fields chosen for convergence monitoring. Convergence monitoring inactive.
Warning: No (valid) fields chosen for time convergence monitoring. Time convergence monitoring inactive.

--------------------- Surface grid deformation (ZONE 0) -----------------
Performing the deformation of the surface grid.
Updating the surface coordinates from the input file.

------------------- Volumetric grid deformation (ZONE 0) ----------------
Performing the deformation of the volumetric grid.

WARNING: Convexity is not checked for 3D elements (issue #1171).


Completed in 0.952518 seconds on 1 core.

----------------------- Write deformed grid files -----------------------
|SU2 mesh                           |../aflr3/aflr3_CAPS.su2            |
|CSV file                           |surface_deformed.csv               |
|Tecplot binary                     |volume_deformed.szplt              |
|Tecplot binary surface             |surface_deformed.szplt             |
Adding any FFD information to the SU2 file.

------------------------- Finalize Solver -------------------------
Deleted CNumerics container.
Deleted CSolver container.
Deleted CGeometry container.
Deleted CSurfaceMovement class.
Deleted CVolumetricMovement class.
Deleted CConfig container.
Deleted COutput class.

------------------------- Exit Success (SU2_DEF) ------------------------


-------------------------------------------------------------------------
|    ___ _   _ ___                                                      |
|   / __| | | |_  )   Release 8.0.0 "Harrier"                           |
|   \__ \ |_| |/ /                                                      |
|   |___/\___//___|   Suite (Computational Fluid Dynamics Code)         |
|                                                                       |
-------------------------------------------------------------------------
| SU2 Project Website: <a href='https://su2code.github.io'>https://su2code.github.io</a>                        |
|                                                                       |
| The SU2 Project is maintained by the SU2 Foundation                   |
| (<a href='http://su2foundation.org'>http://su2foundation.org</a>)                                            |
-------------------------------------------------------------------------
| Copyright 2012-2023, SU2 Contributors                                 |
|                                                                       |
| SU2 is free software; you can redistribute it and/or                  |
| modify it under the terms of the GNU Lesser General Public            |
| License as published by the Free Software Foundation; either          |
| version 2.1 of the License, or (at your option) any later version.    |
|                                                                       |
| SU2 is distributed in the hope that it will be useful,                |
| but WITHOUT ANY WARRANTY; without even the implied warranty of        |
| MERCHANTABILITY or FITNESS FOR A PARTICULAR PURPOSE. See the GNU      |
| Lesser General Public License for more details.                       |
|                                                                       |
| You should have received a copy of the GNU Lesser General Public      |
| License along with SU2. If not, see &lt;<a href='http://www.gnu.org/licenses/'>http://www.gnu.org/licenses/</a>&gt;.   |
-------------------------------------------------------------------------

Parsing config file for zone 0

----------------- Physical Case Definition ( Zone 0 ) -------------------
Compressible Euler equations.
Mach number: 0.294118.
Angle of attack (AoA): 0 deg, and angle of sideslip (AoS): 0 deg.
No restart solution, use the values at infinity (freestream).
Dimensional simulation.
The reference area is 1 m^2.
The semi-span will be computed using the max y(3D) value.
The reference length is 1 m.
Reference origin for moment evaluation is (0, 0, 0).
Surface(s) where the force coefficients are evaluated: BC_3.

Surface(s) plotted in the output file: BC_3.
Surface(s) affected by the design variables: BC_3.
Input mesh file name: ../aflr3/aflr3_CAPS.su2

--------------- Space Numerical Integration ( Zone 0 ) ------------------
Roe (with entropy fix = 0.001) solver for the flow inviscid terms.
Standard Roe without low-dissipation function.
Second order integration in space, with slope limiter.
Venkatakrishnan slope-limiting method, with constant: 0.05.
The reference element size is: 1. 
Gradient for upwind reconstruction: inverse-distance weighted Least-Squares.
Gradient for viscous and source terms: inverse-distance weighted Least-Squares.

--------------- Time Numerical Integration  ( Zone 0 ) ------------------
Local time stepping (steady state simulation).
Euler implicit method for the flow equations.
FGMRES is used for solving the linear system.
Using a ILU(0) preconditioning.
Convergence criteria of the linear solver: 1e-06.
Max number of linear iterations: 10.
V Multigrid Cycle, with 2 multigrid levels.
Damping factor for the residual restriction: 0.75.
Damping factor for the correction prolongation: 0.75.
No CFL adaptation.
+-------------------------------------------+
|  MG Level| Presmooth|PostSmooth|CorrectSmo|
+-------------------------------------------+
|         0|         1|         0|         0|
|         1|         2|         0|         0|
|         2|         3|         0|         0|
+-------------------------------------------+
Courant-Friedrichs-Lewy number:       10

------------------ Convergence Criteria  ( Zone 0 ) ---------------------
Maximum number of solver subiterations: 3.
Begin convergence monitoring at iteration 5.
Residual minimum value: 1e-14.
Cauchy series min. value: 1e-10.
Number of Cauchy elements: 100.
Begin windowed time average at iteration 0.

-------------------- Output Information ( Zone 0 ) ----------------------
File writing frequency: 
+------------------------------------+
|                     File| Frequency|
+------------------------------------+
|                  RESTART|       250|
|              SURFACE_CSV|       250|
|                  TECPLOT|       250|
|          SURFACE_TECPLOT|       250|
+------------------------------------+
Writing the convergence history file every 1 inner iterations.
Writing the screen convergence history every 1 inner iterations.
The tabular file format is CSV (.csv).
Convergence history file name: history.
Forces breakdown file name: forces_breakdown_aeroelastic_Iterative.dat.
Surface file name: surface_flow_aeroelastic_Iterative.
Volume file name: flow_aeroelastic_Iterative.
Restart file name: restart_flow_aeroelastic_Iterative.dat.

------------- Config File Boundary Information ( Zone 0 ) ---------------
+-----------------------------------------------------------------------+
|                        Marker Type|                        Marker Name|
+-----------------------------------------------------------------------+
|                         Euler wall|                               BC_3|
+-----------------------------------------------------------------------+
|                          Far-field|                               BC_1|
+-----------------------------------------------------------------------+
|                     Symmetry plane|                               BC_2|
+-----------------------------------------------------------------------+

-------------------- Output Preprocessing ( Zone 0 ) --------------------

WARNING: SURFACE_PRESSURE_DROP can only be computed for at least 2 surfaces (outlet, inlet, ...)

Screen output fields: TIME_ITER, OUTER_ITER, INNER_ITER, CUR_TIME, TIME_STEP, WALL_TIME, RMS_DENSITY, RMS_MOMENTUM-X, RMS_MOMENTUM-Y, RMS_ENERGY, EFFICIENCY
History output group(s): ITER, TIME_DOMAIN, WALL_TIME, RMS_RES, AERO_COEFF
Convergence field(s): RMS_DENSITY
Warning: No (valid) fields chosen for time convergence monitoring. Time convergence monitoring inactive.
Volume output fields: COORDINATES, SOLUTION, PRIMITIVE

------------------- Geometry Preprocessing ( Zone 0 ) -------------------
Three dimensional problem.
11301 grid points.
58551 volume elements.
3 surface markers.
3452 boundary elements in index 0 (Marker = BC_1).
1827 boundary elements in index 1 (Marker = BC_2).
195 boundary elements in index 2 (Marker = BC_3).
58551 tetrahedra.
Setting point connectivity.
Renumbering points (Reverse Cuthill McKee Ordering).
Recomputing point connectivity.
Setting element connectivity.
Checking the numerical grid orientation.
There has been a re-orientation of 14459 TETRAHEDRON volume elements.
There has been a re-orientation of 682 TRIANGLE surface elements.
Identifying edges and vertices.
Setting the control volume structure.
Volume of the computational grid: 111778.
Searching for the closest normal neighbors to the surfaces.
Storing a mapping from global to local point index.
Compute the surface curvature.
Max K: 331.173. Mean K: 2.9916. Standard deviation K: 14.8257.
Checking for periodicity.
Computing mesh quality statistics for the dual control volumes.
+--------------------------------------------------------------+
|           Mesh Quality Metric|        Minimum|        Maximum|
+--------------------------------------------------------------+
|    Orthogonality Angle (deg.)|        3.40837|        84.3565|
|     CV Face Area Aspect Ratio|        1.28265|         2842.4|
|           CV Sub-Volume Ratio|              1|         163626|
+--------------------------------------------------------------+
Setting the multigrid structure.
+-------------------------------------------+
|  MG Level|       CVs|Aggl. Rate|       CFL|
+-------------------------------------------+
|         0|     11301|    1/1.00|        10|
|         1|      2017|     1/5.6|   8.44541|
|         2|       417|    1/4.84|    7.4907|
+-------------------------------------------+
Finding max control volume width.
Semi-span length = 11.7588 m.
Wetted area = 1396.25 m^2.
Area projection in the x-plane = 460.266 m^2, y-plane = 458.805 m^2, z-plane = 57.6887 m^2.
Max. coordinate in the x-direction = 3.70785 m, y-direction = 11.7588 m, z-direction = 39.9754 m.
Min. coordinate in the x-direction = -12.9853 m, y-direction = -0.927282 m, z-direction = -70.3501 m.
Checking if Euler &amp; Symmetry markers are straight/plane:
Boundary marker BC_3 is NOT a single plane.
Boundary marker BC_2 is NOT a single plane.
Computing wall distances.

-------------------- Solver Preprocessing ( Zone 0 ) --------------------
Inviscid flow: Computing density based on free-stream
temperature and pressure using the ideal gas law.
Force coefficients computed using free-stream values.

-- Models:
+------------------------------------------------------------------------------+
|          Viscosity Model|        Conductivity Model|              Fluid Model|
+------------------------------------------------------------------------------+
|                        -|                         -|             STANDARD_AIR|
+------------------------------------------------------------------------------+
-- Fluid properties:
+------------------------------------------------------------------------------+
|                  Name|    Dim. value|    Ref. value|      Unit|Non-dim. value|
+------------------------------------------------------------------------------+
|          Gas Constant|       287.058|             1|  N.m/kg.K|       287.058|
|      Spec. Heat Ratio|             -|             -|         -|           1.4|
+------------------------------------------------------------------------------+
-- Initial and free-stream conditions:
+------------------------------------------------------------------------------+
|                  Name|    Dim. value|    Ref. value|      Unit|Non-dim. value|
+------------------------------------------------------------------------------+
|       Static Pressure|        101325|             1|        Pa|        101325|
|               Density|       1.22498|             1|    kg/m^3|       1.22498|
|           Temperature|        288.15|             1|         K|        288.15|
|          Total Energy|        211798|             1|   m^2/s^2|        211798|
|            Velocity-X|       100.087|             1|       m/s|       100.087|
|            Velocity-Y|             0|             1|       m/s|             0|
|            Velocity-Z|             0|             1|       m/s|             0|
|    Velocity Magnitude|       100.087|             1|       m/s|       100.087|
+------------------------------------------------------------------------------+
|           Mach Number|             -|             -|         -|      0.294118|
+------------------------------------------------------------------------------+
Initialize Jacobian structure (Euler). MG level: 0.
Initialize Jacobian structure (Euler). MG level: 1.
Initialize Jacobian structure (Euler). MG level: 2.

------------------- Numerics Preprocessing ( Zone 0 ) -------------------

----------------- Integration Preprocessing ( Zone 0 ) ------------------

------------------- Iteration Preprocessing ( Zone 0 ) ------------------
Euler/Navier-Stokes/RANS fluid iteration.

------------------------------ Begin Solver -----------------------------

Simulation Run using the Single-zone Driver
WARNING: SU2 was not compiled for an AVX-capable architecture. Performance could be better,
         see <a href='https://su2code.github.io/docs_v7/Build-SU2-Linux-MacOS/#compiler-optimizations'>https://su2code.github.io/docs_v7/Build-SU2-Linux-MacOS/#compiler-optimizations</a>
WARNING: SU2 was not compiled for an AVX-capable architecture. Performance could be better,
         see <a href='https://su2code.github.io/docs_v7/Build-SU2-Linux-MacOS/#compiler-optimizations'>https://su2code.github.io/docs_v7/Build-SU2-Linux-MacOS/#compiler-optimizations</a>
WARNING: SU2 was not compiled for an AVX-capable architecture. Performance could be better,
         see <a href='https://su2code.github.io/docs_v7/Build-SU2-Linux-MacOS/#compiler-optimizations'>https://su2code.github.io/docs_v7/Build-SU2-Linux-MacOS/#compiler-optimizations</a>
+----------------------------------------------------------------------------------------------------------------------------------------------+
|   Time_Iter|  Outer_Iter|  Inner_Iter|    Cur_Time|   Time_Step|   Time(sec)|    rms[Rho]|   rms[RhoU]|   rms[RhoV]|   rms[RhoE]|        CEff|
+----------------------------------------------------------------------------------------------------------------------------------------------+
|           0|           0|           0|  0.0000e+00|  0.0000e+00|  1.7901e-01|    2.914707|    5.875636|    6.265734|    8.383813|    0.209002|
|           0|           0|           1|  0.0000e+00|  0.0000e+00|  1.8277e-01|    3.316493|    5.858698|    6.095228|    8.744846|    0.234611|
|           0|           0|           2|  0.0000e+00|  0.0000e+00|  1.8369e-01|    3.407997|    5.867221|    6.069520|    8.809945|    0.177305|

----------------------------- Solver Exit -------------------------------

Maximum number of iterations reached (ITER = 3) before convergence.
+-----------------------------------------------------------------------+
|      Convergence Field     |     Value    |   Criterion  |  Converged |
+-----------------------------------------------------------------------+
|                    rms[Rho]|         3.408|         &lt; -14|          No|
+-----------------------------------------------------------------------+
-------------------------------------------------------------------------
+-----------------------------------------------------------------------+
|        File Writing Summary       |              Filename             |
+-----------------------------------------------------------------------+
|SU2 binary restart                 |restart_flow_aeroelastic_Iterative.dat|

Writing the forces breakdown file (forces_breakdown_aeroelastic_Iterative.dat).
|CSV file                           |surface_flow_aeroelastic_Iterative.csv|

Writing the forces breakdown file (forces_breakdown_aeroelastic_Iterative.dat).
|Tecplot binary                     |flow_aeroelastic_Iterative.szplt   |

Writing the forces breakdown file (forces_breakdown_aeroelastic_Iterative.dat).
|Tecplot binary surface             |surface_flow_aeroelastic_Iterative.szplt|

Writing the forces breakdown file (forces_breakdown_aeroelastic_Iterative.dat).
+-----------------------------------------------------------------------+
Warning: there are 199 non-physical points in the solution.
Warning: 20 reconstructed states for upwinding are non-physical.

--------------------------- Finalizing Solver ---------------------------
Deleted CNumerics container.
Deleted CIntegration container.
Deleted CSolver container.
Deleted CIteration container.
Deleted CInterface container.
Deleted CGeometry container.
Deleted CFreeFormDefBox class.
Deleted CSurfaceMovement class.
Deleted CVolumetricMovement class.
Deleted CConfig container.
Deleted nInst container.
Deleted COutput class.
-------------------------------------------------------------------------

------------------------- Exit Success (SU2_CFD) ------------------------


Running PostAnalysis ...... su2

Running PreAnalysis ...... su2
Reading SU2 AeroLoad File - surface_flow_aeroelastic_Iterative.csv
	Number of variables = 16
	Number of data points = 104
 CAPS Info: Bound 'Skin_Top' Normalized Integrated 'Pressure'
            Rank 0: src = 8.819257e+08, tgt = 8.819253e+08, diff = 3.923236e+02
Reading SU2 AeroLoad File - surface_flow_aeroelastic_Iterative.csv
	Number of variables = 16
	Number of data points = 104
 CAPS Info: Bound 'Skin_Bottom' Normalized Integrated 'Pressure'
            Rank 0: src = 1.207830e+09, tgt = 1.207830e+09, diff = 2.597151e+02
Reading SU2 AeroLoad File - surface_flow_aeroelastic_Iterative.csv
	Number of variables = 16
	Number of data points = 104
 CAPS Info: Bound 'Skin_Tip' Normalized Integrated 'Pressure'
            Rank 0: src = 1.219268e+07, tgt = 1.219271e+07, diff = 2.880687e+01
Extracting external pressure loads from data transfer....
	TransferName = Skin_Top
	Number of Elements = 330 (total = 330)
Extracting external pressure loads from data transfer....
	TransferName = Skin_Bottom
	Number of Elements = 330 (total = 660)
Extracting external pressure loads from data transfer....
	TransferName = Skin_Tip
	Number of Elements = 30 (total = 690)

Writing Astros grid and connectivity file (in free field format) ....
Finished writing Astros grid file

Writing subElement types (if any) - appending mesh file

Writing Astros instruction file....
	Writing analysis cards
	Writing load ADD cards
	Writing constraint cards--each subcase individually
	Writing load cards
	Writing material cards
	Writing property cards
Note: The following floating-point exceptions are signalling: IEEE_UNDERFLOW_FLAG
Writing SU2 data transfer files
Writing SU2 Motion File - aeroelastic_Iterative_motion.dat
Warning: The su2 cfg file will be overwritten!
Write SU2 configuration file for version "Harrier (8.0.1)"


Running SU2......

-------------------------------------------------------------------------
|    ___ _   _ ___                                                      |
|   / __| | | |_  )   Release 8.0.0 "Harrier"                           |
|   \__ \ |_| |/ /                                                      |
|   |___/\___//___|   Suite (Mesh Deformation Code)                     |
|                                                                       |
-------------------------------------------------------------------------
| SU2 Project Website: <a href='https://su2code.github.io'>https://su2code.github.io</a>                        |
|                                                                       |
| The SU2 Project is maintained by the SU2 Foundation                   |
| (<a href='http://su2foundation.org'>http://su2foundation.org</a>)                                            |
-------------------------------------------------------------------------
| Copyright 2012-2023, SU2 Contributors                                 |
|                                                                       |
| SU2 is free software; you can redistribute it and/or                  |
| modify it under the terms of the GNU Lesser General Public            |
| License as published by the Free Software Foundation; either          |
| version 2.1 of the License, or (at your option) any later version.    |
|                                                                       |
| SU2 is distributed in the hope that it will be useful,                |
| but WITHOUT ANY WARRANTY; without even the implied warranty of        |
| MERCHANTABILITY or FITNESS FOR A PARTICULAR PURPOSE. See the GNU      |
| Lesser General Public License for more details.                       |
|                                                                       |
| You should have received a copy of the GNU Lesser General Public      |
| License along with SU2. If not, see &lt;<a href='http://www.gnu.org/licenses/'>http://www.gnu.org/licenses/</a>&gt;.   |
-------------------------------------------------------------------------

----------------- Physical Case Definition ( Zone 0 ) -------------------
Input mesh file name: ../aflr3/aflr3_CAPS.su2

---------------- Grid deformation parameters ( Zone 0 )  ----------------
Grid deformation using a linear elasticity method.


-------------------- Output Information ( Zone 0 ) ----------------------
Output mesh file name: ../aflr3/aflr3_CAPS.su2. 
Cell stiffness scaled by distance to nearest solid surface.

------------- Config File Boundary Information ( Zone 0 ) ---------------
+-----------------------------------------------------------------------+
|                        Marker Type|                        Marker Name|
+-----------------------------------------------------------------------+
|                         Euler wall|                               BC_3|
+-----------------------------------------------------------------------+
|                          Far-field|                               BC_1|
+-----------------------------------------------------------------------+
|                     Symmetry plane|                               BC_2|
+-----------------------------------------------------------------------+
Three dimensional problem.
11301 grid points.
58551 volume elements.
3 surface markers.
3452 boundary elements in index 0 (Marker = BC_1).
1827 boundary elements in index 1 (Marker = BC_2).
195 boundary elements in index 2 (Marker = BC_3).
58551 tetrahedra.

----------------------- Preprocessing computations ----------------------
Setting local point connectivity.
Checking the numerical grid orientation of the interior elements.
There has been a re-orientation of 14459 TETRAHEDRON volume elements.
There has been a re-orientation of 682 TRIANGLE surface elements.
Identify edges and vertices.
Setting the bound control volume structure.
Volume of the computational grid: 111778.
  Info: Ignoring the following volume output fields/groups:
  SOLUTION
Volume output fields: COORDINATES
  Info: Ignoring the following screen output fields:
  RMS_DENSITY, RMS_MOMENTUM-X, RMS_MOMENTUM-Y, RMS_ENERGY, EFFICIENCY
Screen output fields: TIME_ITER, OUTER_ITER, INNER_ITER, CUR_TIME, TIME_STEP, WALL_TIME
  Info: Ignoring the following history output groups:
  RMS_RES, AERO_COEFF
History output group(s): ITER, TIME_DOMAIN, WALL_TIME
Warning: No (valid) fields chosen for convergence monitoring. Convergence monitoring inactive.
Warning: No (valid) fields chosen for time convergence monitoring. Time convergence monitoring inactive.

--------------------- Surface grid deformation (ZONE 0) -----------------
Performing the deformation of the surface grid.
Updating the surface coordinates from the input file.

------------------- Volumetric grid deformation (ZONE 0) ----------------
Performing the deformation of the volumetric grid.

WARNING: Convexity is not checked for 3D elements (issue #1171).


Completed in 14.979367 seconds on 1 core.

----------------------- Write deformed grid files -----------------------
|SU2 mesh                           |../aflr3/aflr3_CAPS.su2            |
|CSV file                           |surface_deformed.csv               |
|Tecplot binary                     |volume_deformed.szplt              |
|Tecplot binary surface             |surface_deformed.szplt             |
Adding any FFD information to the SU2 file.

------------------------- Finalize Solver -------------------------
Deleted CNumerics container.
Deleted CSolver container.
Deleted CGeometry container.
Deleted CSurfaceMovement class.
Deleted CVolumetricMovement class.
Deleted CConfig container.
Deleted COutput class.

------------------------- Exit Success (SU2_DEF) ------------------------


-------------------------------------------------------------------------
|    ___ _   _ ___                                                      |
|   / __| | | |_  )   Release 8.0.0 "Harrier"                           |
|   \__ \ |_| |/ /                                                      |
|   |___/\___//___|   Suite (Computational Fluid Dynamics Code)         |
|                                                                       |
-------------------------------------------------------------------------
| SU2 Project Website: <a href='https://su2code.github.io'>https://su2code.github.io</a>                        |
|                                                                       |
| The SU2 Project is maintained by the SU2 Foundation                   |
| (<a href='http://su2foundation.org'>http://su2foundation.org</a>)                                            |
-------------------------------------------------------------------------
| Copyright 2012-2023, SU2 Contributors                                 |
|                                                                       |
| SU2 is free software; you can redistribute it and/or                  |
| modify it under the terms of the GNU Lesser General Public            |
| License as published by the Free Software Foundation; either          |
| version 2.1 of the License, or (at your option) any later version.    |
|                                                                       |
| SU2 is distributed in the hope that it will be useful,                |
| but WITHOUT ANY WARRANTY; without even the implied warranty of        |
| MERCHANTABILITY or FITNESS FOR A PARTICULAR PURPOSE. See the GNU      |
| Lesser General Public License for more details.                       |
|                                                                       |
| You should have received a copy of the GNU Lesser General Public      |
| License along with SU2. If not, see &lt;<a href='http://www.gnu.org/licenses/'>http://www.gnu.org/licenses/</a>&gt;.   |
-------------------------------------------------------------------------

Parsing config file for zone 0

----------------- Physical Case Definition ( Zone 0 ) -------------------
Compressible Euler equations.
Mach number: 0.294118.
Angle of attack (AoA): 0 deg, and angle of sideslip (AoS): 0 deg.
No restart solution, use the values at infinity (freestream).
Dimensional simulation.
The reference area is 1 m^2.
The semi-span will be computed using the max y(3D) value.
The reference length is 1 m.
Reference origin for moment evaluation is (0, 0, 0).
Surface(s) where the force coefficients are evaluated: BC_3.

Surface(s) plotted in the output file: BC_3.
Surface(s) affected by the design variables: BC_3.
Input mesh file name: ../aflr3/aflr3_CAPS.su2

--------------- Space Numerical Integration ( Zone 0 ) ------------------
Roe (with entropy fix = 0.001) solver for the flow inviscid terms.
Standard Roe without low-dissipation function.
Second order integration in space, with slope limiter.
Venkatakrishnan slope-limiting method, with constant: 0.05.
The reference element size is: 1. 
Gradient for upwind reconstruction: inverse-distance weighted Least-Squares.
Gradient for viscous and source terms: inverse-distance weighted Least-Squares.

--------------- Time Numerical Integration  ( Zone 0 ) ------------------
Local time stepping (steady state simulation).
Euler implicit method for the flow equations.
FGMRES is used for solving the linear system.
Using a ILU(0) preconditioning.
Convergence criteria of the linear solver: 1e-06.
Max number of linear iterations: 10.
V Multigrid Cycle, with 2 multigrid levels.
Damping factor for the residual restriction: 0.75.
Damping factor for the correction prolongation: 0.75.
No CFL adaptation.
+-------------------------------------------+
|  MG Level| Presmooth|PostSmooth|CorrectSmo|
+-------------------------------------------+
|         0|         1|         0|         0|
|         1|         2|         0|         0|
|         2|         3|         0|         0|
+-------------------------------------------+
Courant-Friedrichs-Lewy number:       10

------------------ Convergence Criteria  ( Zone 0 ) ---------------------
Maximum number of solver subiterations: 3.
Begin convergence monitoring at iteration 5.
Residual minimum value: 1e-14.
Cauchy series min. value: 1e-10.
Number of Cauchy elements: 100.
Begin windowed time average at iteration 0.

-------------------- Output Information ( Zone 0 ) ----------------------
File writing frequency: 
+------------------------------------+
|                     File| Frequency|
+------------------------------------+
|                  RESTART|       250|
|              SURFACE_CSV|       250|
|                  TECPLOT|       250|
|          SURFACE_TECPLOT|       250|
+------------------------------------+
Writing the convergence history file every 1 inner iterations.
Writing the screen convergence history every 1 inner iterations.
The tabular file format is CSV (.csv).
Convergence history file name: history.
Forces breakdown file name: forces_breakdown_aeroelastic_Iterative.dat.
Surface file name: surface_flow_aeroelastic_Iterative.
Volume file name: flow_aeroelastic_Iterative.
Restart file name: restart_flow_aeroelastic_Iterative.dat.

------------- Config File Boundary Information ( Zone 0 ) ---------------
+-----------------------------------------------------------------------+
|                        Marker Type|                        Marker Name|
+-----------------------------------------------------------------------+
|                         Euler wall|                               BC_3|
+-----------------------------------------------------------------------+
|                          Far-field|                               BC_1|
+-----------------------------------------------------------------------+
|                     Symmetry plane|                               BC_2|
+-----------------------------------------------------------------------+

-------------------- Output Preprocessing ( Zone 0 ) --------------------

WARNING: SURFACE_PRESSURE_DROP can only be computed for at least 2 surfaces (outlet, inlet, ...)

Screen output fields: TIME_ITER, OUTER_ITER, INNER_ITER, CUR_TIME, TIME_STEP, WALL_TIME, RMS_DENSITY, RMS_MOMENTUM-X, RMS_MOMENTUM-Y, RMS_ENERGY, EFFICIENCY
History output group(s): ITER, TIME_DOMAIN, WALL_TIME, RMS_RES, AERO_COEFF
Convergence field(s): RMS_DENSITY
Warning: No (valid) fields chosen for time convergence monitoring. Time convergence monitoring inactive.
Volume output fields: COORDINATES, SOLUTION, PRIMITIVE

------------------- Geometry Preprocessing ( Zone 0 ) -------------------
Three dimensional problem.
11301 grid points.
58551 volume elements.
3 surface markers.
3452 boundary elements in index 0 (Marker = BC_1).
1827 boundary elements in index 1 (Marker = BC_2).
195 boundary elements in index 2 (Marker = BC_3).
58551 tetrahedra.
Setting point connectivity.
Renumbering points (Reverse Cuthill McKee Ordering).
Recomputing point connectivity.
Setting element connectivity.
Checking the numerical grid orientation.
There has been a re-orientation of 31311 TETRAHEDRON volume elements.
There has been a re-orientation of 3369 TRIANGLE surface elements.
Identifying edges and vertices.
Setting the control volume structure.
Volume of the computational grid: 1.16776e+11.
Searching for the closest normal neighbors to the surfaces.
Storing a mapping from global to local point index.
Compute the surface curvature.
Max K: 21.0169. Mean K: 0.354492. Standard deviation K: 1.30595.
Checking for periodicity.
Computing mesh quality statistics for the dual control volumes.
+--------------------------------------------------------------+
|           Mesh Quality Metric|        Minimum|        Maximum|
+--------------------------------------------------------------+
|    Orthogonality Angle (deg.)|       0.453746|        85.8506|
|     CV Face Area Aspect Ratio|         1.5343|         899846|
|           CV Sub-Volume Ratio|              1|    6.31279e+06|
+--------------------------------------------------------------+
Setting the multigrid structure.
+-------------------------------------------+
|  MG Level|       CVs|Aggl. Rate|       CFL|
+-------------------------------------------+
|         0|     11301|    1/1.00|        10|
|         1|      1992|    1/5.67|   8.41038|
|         2|       421|    1/4.73|   7.51457|
+-------------------------------------------+
Finding max control volume width.
Semi-span length = 397.143 m.
Wetted area = 881016 m^2.
Area projection in the x-plane = 445045 m^2, y-plane = 151377 m^2, z-plane = 8426.75 m^2.
Max. coordinate in the x-direction = 50.0167 m, y-direction = 397.143 m, z-direction = 0.159487 m.
Min. coordinate in the x-direction = -18.3734 m, y-direction = -10.3349 m, z-direction = -5468.94 m.
Checking if Euler &amp; Symmetry markers are straight/plane:
Boundary marker BC_3 is NOT a single plane.
Boundary marker BC_2 is NOT a single plane.
Computing wall distances.

-------------------- Solver Preprocessing ( Zone 0 ) --------------------
Inviscid flow: Computing density based on free-stream
temperature and pressure using the ideal gas law.
Force coefficients computed using free-stream values.

-- Models:
+------------------------------------------------------------------------------+
|          Viscosity Model|        Conductivity Model|              Fluid Model|
+------------------------------------------------------------------------------+
|                        -|                         -|             STANDARD_AIR|
+------------------------------------------------------------------------------+
-- Fluid properties:
+------------------------------------------------------------------------------+
|                  Name|    Dim. value|    Ref. value|      Unit|Non-dim. value|
+------------------------------------------------------------------------------+
|          Gas Constant|       287.058|             1|  N.m/kg.K|       287.058|
|      Spec. Heat Ratio|             -|             -|         -|           1.4|
+------------------------------------------------------------------------------+
-- Initial and free-stream conditions:
+------------------------------------------------------------------------------+
|                  Name|    Dim. value|    Ref. value|      Unit|Non-dim. value|
+------------------------------------------------------------------------------+
|       Static Pressure|        101325|             1|        Pa|        101325|
|               Density|       1.22498|             1|    kg/m^3|       1.22498|
|           Temperature|        288.15|             1|         K|        288.15|
|          Total Energy|        211798|             1|   m^2/s^2|        211798|
|            Velocity-X|       100.087|             1|       m/s|       100.087|
|            Velocity-Y|             0|             1|       m/s|             0|
|            Velocity-Z|             0|             1|       m/s|             0|
|    Velocity Magnitude|       100.087|             1|       m/s|       100.087|
+------------------------------------------------------------------------------+
|           Mach Number|             -|             -|         -|      0.294118|
+------------------------------------------------------------------------------+
Initialize Jacobian structure (Euler). MG level: 0.
Initialize Jacobian structure (Euler). MG level: 1.
Initialize Jacobian structure (Euler). MG level: 2.

------------------- Numerics Preprocessing ( Zone 0 ) -------------------

----------------- Integration Preprocessing ( Zone 0 ) ------------------

------------------- Iteration Preprocessing ( Zone 0 ) ------------------
Euler/Navier-Stokes/RANS fluid iteration.

------------------------------ Begin Solver -----------------------------

Simulation Run using the Single-zone Driver
WARNING: SU2 was not compiled for an AVX-capable architecture. Performance could be better,
         see <a href='https://su2code.github.io/docs_v7/Build-SU2-Linux-MacOS/#compiler-optimizations'>https://su2code.github.io/docs_v7/Build-SU2-Linux-MacOS/#compiler-optimizations</a>
WARNING: SU2 was not compiled for an AVX-capable architecture. Performance could be better,
         see <a href='https://su2code.github.io/docs_v7/Build-SU2-Linux-MacOS/#compiler-optimizations'>https://su2code.github.io/docs_v7/Build-SU2-Linux-MacOS/#compiler-optimizations</a>
WARNING: SU2 was not compiled for an AVX-capable architecture. Performance could be better,
         see <a href='https://su2code.github.io/docs_v7/Build-SU2-Linux-MacOS/#compiler-optimizations'>https://su2code.github.io/docs_v7/Build-SU2-Linux-MacOS/#compiler-optimizations</a>
+----------------------------------------------------------------------------------------------------------------------------------------------+
|   Time_Iter|  Outer_Iter|  Inner_Iter|    Cur_Time|   Time_Step|   Time(sec)|    rms[Rho]|   rms[RhoU]|   rms[RhoV]|   rms[RhoE]|        CEff|
+----------------------------------------------------------------------------------------------------------------------------------------------+
|           0|           0|           0|  0.0000e+00|  0.0000e+00|  1.7812e-01|    7.276733|   10.242971|   10.238844|   12.745838|    0.089051|
|           0|           0|           1|  0.0000e+00|  0.0000e+00|  1.8184e-01|    7.638465|   10.267040|   10.181291|   13.033584|    0.027721|
|           0|           0|           2|  0.0000e+00|  0.0000e+00|  1.8287e-01|    7.779909|   10.393368|   10.306450|   13.183336|   -0.089022|

----------------------------- Solver Exit -------------------------------

Maximum number of iterations reached (ITER = 3) before convergence.
+-----------------------------------------------------------------------+
|      Convergence Field     |     Value    |   Criterion  |  Converged |
+-----------------------------------------------------------------------+
|                    rms[Rho]|       7.77991|         &lt; -14|          No|
+-----------------------------------------------------------------------+
-------------------------------------------------------------------------
+-----------------------------------------------------------------------+
|        File Writing Summary       |              Filename             |
+-----------------------------------------------------------------------+
|SU2 binary restart                 |restart_flow_aeroelastic_Iterative.dat|

Writing the forces breakdown file (forces_breakdown_aeroelastic_Iterative.dat).
|CSV file                           |surface_flow_aeroelastic_Iterative.csv|

Writing the forces breakdown file (forces_breakdown_aeroelastic_Iterative.dat).
|Tecplot binary                     |flow_aeroelastic_Iterative.szplt   |

Writing the forces breakdown file (forces_breakdown_aeroelastic_Iterative.dat).
|Tecplot binary surface             |surface_flow_aeroelastic_Iterative.szplt|

Writing the forces breakdown file (forces_breakdown_aeroelastic_Iterative.dat).
+-----------------------------------------------------------------------+
Warning: there are 552 non-physical points in the solution.
Warning: 55 reconstructed states for upwinding are non-physical.

--------------------------- Finalizing Solver ---------------------------
Deleted CNumerics container.
Deleted CIntegration container.
Deleted CSolver container.
Deleted CIteration container.
Deleted CInterface container.
Deleted CGeometry container.
Deleted CFreeFormDefBox class.
Deleted CSurfaceMovement class.
Deleted CVolumetricMovement class.
Deleted CConfig container.
Deleted nInst container.
Deleted COutput class.
-------------------------------------------------------------------------

------------------------- Exit Success (SU2_CFD) ------------------------


Running PostAnalysis ...... su2

Running PreAnalysis ...... su2
Reading SU2 AeroLoad File - surface_flow_aeroelastic_Iterative.csv
	Number of variables = 16
	Number of data points = 104
 CAPS Info: Bound 'Skin_Top' Normalized Integrated 'Pressure'
            Rank 0: src = 1.076975e+09, tgt = 1.076975e+09, diff = 3.649154e+02
Reading SU2 AeroLoad File - surface_flow_aeroelastic_Iterative.csv
	Number of variables = 16
	Number of data points = 104
 CAPS Info: Bound 'Skin_Bottom' Normalized Integrated 'Pressure'
            Rank 0: src = 1.571003e+09, tgt = 1.571004e+09, diff = 1.719102e+02
Reading SU2 AeroLoad File - surface_flow_aeroelastic_Iterative.csv
	Number of variables = 16
	Number of data points = 104
 CAPS Info: Bound 'Skin_Tip' Normalized Integrated 'Pressure'
            Rank 0: src = 1.913889e+07, tgt = 1.913886e+07, diff = 2.267927e+01
Extracting external pressure loads from data transfer....
	TransferName = Skin_Top
	Number of Elements = 330 (total = 330)
Extracting external pressure loads from data transfer....
	TransferName = Skin_Bottom
	Number of Elements = 330 (total = 660)
Extracting external pressure loads from data transfer....
	TransferName = Skin_Tip
	Number of Elements = 30 (total = 690)

Writing Astros grid and connectivity file (in free field format) ....
Finished writing Astros grid file

Writing subElement types (if any) - appending mesh file

Writing Astros instruction file....
	Writing analysis cards
	Writing load ADD cards
	Writing constraint cards--each subcase individually
	Writing load cards
	Writing material cards
	Writing property cards
Note: The following floating-point exceptions are signalling: IEEE_UNDERFLOW_FLAG
Writing SU2 data transfer files
Writing SU2 Motion File - aeroelastic_Iterative_motion.dat
Warning: The su2 cfg file will be overwritten!
Write SU2 configuration file for version "Harrier (8.0.1)"


Running SU2......

-------------------------------------------------------------------------
|    ___ _   _ ___                                                      |
|   / __| | | |_  )   Release 8.0.0 "Harrier"                           |
|   \__ \ |_| |/ /                                                      |
|   |___/\___//___|   Suite (Mesh Deformation Code)                     |
|                                                                       |
-------------------------------------------------------------------------
| SU2 Project Website: <a href='https://su2code.github.io'>https://su2code.github.io</a>                        |
|                                                                       |
| The SU2 Project is maintained by the SU2 Foundation                   |
| (<a href='http://su2foundation.org'>http://su2foundation.org</a>)                                            |
-------------------------------------------------------------------------
| Copyright 2012-2023, SU2 Contributors                                 |
|                                                                       |
| SU2 is free software; you can redistribute it and/or                  |
| modify it under the terms of the GNU Lesser General Public            |
| License as published by the Free Software Foundation; either          |
| version 2.1 of the License, or (at your option) any later version.    |
|                                                                       |
| SU2 is distributed in the hope that it will be useful,                |
| but WITHOUT ANY WARRANTY; without even the implied warranty of        |
| MERCHANTABILITY or FITNESS FOR A PARTICULAR PURPOSE. See the GNU      |
| Lesser General Public License for more details.                       |
|                                                                       |
| You should have received a copy of the GNU Lesser General Public      |
| License along with SU2. If not, see &lt;<a href='http://www.gnu.org/licenses/'>http://www.gnu.org/licenses/</a>&gt;.   |
-------------------------------------------------------------------------

----------------- Physical Case Definition ( Zone 0 ) -------------------
Input mesh file name: ../aflr3/aflr3_CAPS.su2

---------------- Grid deformation parameters ( Zone 0 )  ----------------
Grid deformation using a linear elasticity method.


-------------------- Output Information ( Zone 0 ) ----------------------
Output mesh file name: ../aflr3/aflr3_CAPS.su2. 
Cell stiffness scaled by distance to nearest solid surface.

------------- Config File Boundary Information ( Zone 0 ) ---------------
+-----------------------------------------------------------------------+
|                        Marker Type|                        Marker Name|
+-----------------------------------------------------------------------+
|                         Euler wall|                               BC_3|
+-----------------------------------------------------------------------+
|                          Far-field|                               BC_1|
+-----------------------------------------------------------------------+
|                     Symmetry plane|                               BC_2|
+-----------------------------------------------------------------------+
Three dimensional problem.
11301 grid points.
58551 volume elements.
3 surface markers.
3452 boundary elements in index 0 (Marker = BC_1).
1827 boundary elements in index 1 (Marker = BC_2).
195 boundary elements in index 2 (Marker = BC_3).
58551 tetrahedra.

----------------------- Preprocessing computations ----------------------
Setting local point connectivity.
Checking the numerical grid orientation of the interior elements.
There has been a re-orientation of 31311 TETRAHEDRON volume elements.
There has been a re-orientation of 3369 TRIANGLE surface elements.
Identify edges and vertices.
Setting the bound control volume structure.
Volume of the computational grid: 1.16776e+11.
  Info: Ignoring the following volume output fields/groups:
  SOLUTION
Volume output fields: COORDINATES
  Info: Ignoring the following screen output fields:
  RMS_DENSITY, RMS_MOMENTUM-X, RMS_MOMENTUM-Y, RMS_ENERGY, EFFICIENCY
Screen output fields: TIME_ITER, OUTER_ITER, INNER_ITER, CUR_TIME, TIME_STEP, WALL_TIME
  Info: Ignoring the following history output groups:
  RMS_RES, AERO_COEFF
History output group(s): ITER, TIME_DOMAIN, WALL_TIME
Warning: No (valid) fields chosen for convergence monitoring. Convergence monitoring inactive.
Warning: No (valid) fields chosen for time convergence monitoring. Time convergence monitoring inactive.

--------------------- Surface grid deformation (ZONE 0) -----------------
Performing the deformation of the surface grid.
Updating the surface coordinates from the input file.

------------------- Volumetric grid deformation (ZONE 0) ----------------
Performing the deformation of the volumetric grid.

WARNING: Convexity is not checked for 3D elements (issue #1171).


Completed in 23.541524 seconds on 1 core.

----------------------- Write deformed grid files -----------------------
|SU2 mesh                           |../aflr3/aflr3_CAPS.su2            |
|CSV file                           |surface_deformed.csv               |
|Tecplot binary                     |volume_deformed.szplt              |
|Tecplot binary surface             |surface_deformed.szplt             |
Adding any FFD information to the SU2 file.

------------------------- Finalize Solver -------------------------
Deleted CNumerics container.
Deleted CSolver container.
Deleted CGeometry container.
Deleted CSurfaceMovement class.
Deleted CVolumetricMovement class.
Deleted CConfig container.
Deleted COutput class.

------------------------- Exit Success (SU2_DEF) ------------------------


-------------------------------------------------------------------------
|    ___ _   _ ___                                                      |
|   / __| | | |_  )   Release 8.0.0 "Harrier"                           |
|   \__ \ |_| |/ /                                                      |
|   |___/\___//___|   Suite (Computational Fluid Dynamics Code)         |
|                                                                       |
-------------------------------------------------------------------------
| SU2 Project Website: <a href='https://su2code.github.io'>https://su2code.github.io</a>                        |
|                                                                       |
| The SU2 Project is maintained by the SU2 Foundation                   |
| (<a href='http://su2foundation.org'>http://su2foundation.org</a>)                                            |
-------------------------------------------------------------------------
| Copyright 2012-2023, SU2 Contributors                                 |
|                                                                       |
| SU2 is free software; you can redistribute it and/or                  |
| modify it under the terms of the GNU Lesser General Public            |
| License as published by the Free Software Foundation; either          |
| version 2.1 of the License, or (at your option) any later version.    |
|                                                                       |
| SU2 is distributed in the hope that it will be useful,                |
| but WITHOUT ANY WARRANTY; without even the implied warranty of        |
| MERCHANTABILITY or FITNESS FOR A PARTICULAR PURPOSE. See the GNU      |
| Lesser General Public License for more details.                       |
|                                                                       |
| You should have received a copy of the GNU Lesser General Public      |
| License along with SU2. If not, see &lt;<a href='http://www.gnu.org/licenses/'>http://www.gnu.org/licenses/</a>&gt;.   |
-------------------------------------------------------------------------

Parsing config file for zone 0

----------------- Physical Case Definition ( Zone 0 ) -------------------
Compressible Euler equations.
Mach number: 0.294118.
Angle of attack (AoA): 0 deg, and angle of sideslip (AoS): 0 deg.
No restart solution, use the values at infinity (freestream).
Dimensional simulation.
The reference area is 1 m^2.
The semi-span will be computed using the max y(3D) value.
The reference length is 1 m.
Reference origin for moment evaluation is (0, 0, 0).
Surface(s) where the force coefficients are evaluated: BC_3.

Surface(s) plotted in the output file: BC_3.
Surface(s) affected by the design variables: BC_3.
Input mesh file name: ../aflr3/aflr3_CAPS.su2

--------------- Space Numerical Integration ( Zone 0 ) ------------------
Roe (with entropy fix = 0.001) solver for the flow inviscid terms.
Standard Roe without low-dissipation function.
Second order integration in space, with slope limiter.
Venkatakrishnan slope-limiting method, with constant: 0.05.
The reference element size is: 1. 
Gradient for upwind reconstruction: inverse-distance weighted Least-Squares.
Gradient for viscous and source terms: inverse-distance weighted Least-Squares.

--------------- Time Numerical Integration  ( Zone 0 ) ------------------
Local time stepping (steady state simulation).
Euler implicit method for the flow equations.
FGMRES is used for solving the linear system.
Using a ILU(0) preconditioning.
Convergence criteria of the linear solver: 1e-06.
Max number of linear iterations: 10.
V Multigrid Cycle, with 2 multigrid levels.
Damping factor for the residual restriction: 0.75.
Damping factor for the correction prolongation: 0.75.
No CFL adaptation.
+-------------------------------------------+
|  MG Level| Presmooth|PostSmooth|CorrectSmo|
+-------------------------------------------+
|         0|         1|         0|         0|
|         1|         2|         0|         0|
|         2|         3|         0|         0|
+-------------------------------------------+
Courant-Friedrichs-Lewy number:       10

------------------ Convergence Criteria  ( Zone 0 ) ---------------------
Maximum number of solver subiterations: 3.
Begin convergence monitoring at iteration 5.
Residual minimum value: 1e-14.
Cauchy series min. value: 1e-10.
Number of Cauchy elements: 100.
Begin windowed time average at iteration 0.

-------------------- Output Information ( Zone 0 ) ----------------------
File writing frequency: 
+------------------------------------+
|                     File| Frequency|
+------------------------------------+
|                  RESTART|       250|
|              SURFACE_CSV|       250|
|                  TECPLOT|       250|
|          SURFACE_TECPLOT|       250|
+------------------------------------+
Writing the convergence history file every 1 inner iterations.
Writing the screen convergence history every 1 inner iterations.
The tabular file format is CSV (.csv).
Convergence history file name: history.
Forces breakdown file name: forces_breakdown_aeroelastic_Iterative.dat.
Surface file name: surface_flow_aeroelastic_Iterative.
Volume file name: flow_aeroelastic_Iterative.
Restart file name: restart_flow_aeroelastic_Iterative.dat.

------------- Config File Boundary Information ( Zone 0 ) ---------------
+-----------------------------------------------------------------------+
|                        Marker Type|                        Marker Name|
+-----------------------------------------------------------------------+
|                         Euler wall|                               BC_3|
+-----------------------------------------------------------------------+
|                          Far-field|                               BC_1|
+-----------------------------------------------------------------------+
|                     Symmetry plane|                               BC_2|
+-----------------------------------------------------------------------+

-------------------- Output Preprocessing ( Zone 0 ) --------------------

WARNING: SURFACE_PRESSURE_DROP can only be computed for at least 2 surfaces (outlet, inlet, ...)

Screen output fields: TIME_ITER, OUTER_ITER, INNER_ITER, CUR_TIME, TIME_STEP, WALL_TIME, RMS_DENSITY, RMS_MOMENTUM-X, RMS_MOMENTUM-Y, RMS_ENERGY, EFFICIENCY
History output group(s): ITER, TIME_DOMAIN, WALL_TIME, RMS_RES, AERO_COEFF
Convergence field(s): RMS_DENSITY
Warning: No (valid) fields chosen for time convergence monitoring. Time convergence monitoring inactive.
Volume output fields: COORDINATES, SOLUTION, PRIMITIVE

------------------- Geometry Preprocessing ( Zone 0 ) -------------------
Three dimensional problem.
11301 grid points.
58551 volume elements.
3 surface markers.
3452 boundary elements in index 0 (Marker = BC_1).
1827 boundary elements in index 1 (Marker = BC_2).
195 boundary elements in index 2 (Marker = BC_3).
58551 tetrahedra.
Setting point connectivity.
Renumbering points (Reverse Cuthill McKee Ordering).
Recomputing point connectivity.
Setting element connectivity.
Checking the numerical grid orientation.
There has been a re-orientation of 12469 TETRAHEDRON volume elements.
There has been a re-orientation of 3032 TRIANGLE surface elements.
Identifying edges and vertices.
Setting the control volume structure.
Volume of the computational grid: 1.4591e+13.
Searching for the closest normal neighbors to the surfaces.
Storing a mapping from global to local point index.
Compute the surface curvature.
Max K: 17.5858. Mean K: 0.217072. Standard deviation K: 0.879795.
Checking for periodicity.
Computing mesh quality statistics for the dual control volumes.
+--------------------------------------------------------------+
|           Mesh Quality Metric|        Minimum|        Maximum|
+--------------------------------------------------------------+
|    Orthogonality Angle (deg.)|       0.577466|        85.1191|
|     CV Face Area Aspect Ratio|        1.70706|    2.96442e+07|
|           CV Sub-Volume Ratio|              1|    1.37716e+09|
+--------------------------------------------------------------+
Setting the multigrid structure.
+-------------------------------------------+
|  MG Level|       CVs|Aggl. Rate|       CFL|
+-------------------------------------------+
|         0|     11301|    1/1.00|        10|
|         1|      1992|    1/5.67|   8.41038|
|         2|       413|    1/4.82|   7.46667|
+-------------------------------------------+
Finding max control volume width.
Semi-span length = 993.177 m.
Wetted area = 4.88018e+06 m^2.
Area projection in the x-plane = 1.61503e+06 m^2, y-plane = 1.25948e+06 m^2, z-plane = 71304.9 m^2.
Max. coordinate in the x-direction = 127.282 m, y-direction = 993.177 m, z-direction = 0.159487 m.
Min. coordinate in the x-direction = -60.3931 m, y-direction = -24.6094 m, z-direction = -13719 m.
Checking if Euler &amp; Symmetry markers are straight/plane:
Boundary marker BC_3 is NOT a single plane.
Boundary marker BC_2 is NOT a single plane.
Computing wall distances.

-------------------- Solver Preprocessing ( Zone 0 ) --------------------
Inviscid flow: Computing density based on free-stream
temperature and pressure using the ideal gas law.
Force coefficients computed using free-stream values.

-- Models:
+------------------------------------------------------------------------------+
|          Viscosity Model|        Conductivity Model|              Fluid Model|
+------------------------------------------------------------------------------+
|                        -|                         -|             STANDARD_AIR|
+------------------------------------------------------------------------------+
-- Fluid properties:
+------------------------------------------------------------------------------+
|                  Name|    Dim. value|    Ref. value|      Unit|Non-dim. value|
+------------------------------------------------------------------------------+
|          Gas Constant|       287.058|             1|  N.m/kg.K|       287.058|
|      Spec. Heat Ratio|             -|             -|         -|           1.4|
+------------------------------------------------------------------------------+
-- Initial and free-stream conditions:
+------------------------------------------------------------------------------+
|                  Name|    Dim. value|    Ref. value|      Unit|Non-dim. value|
+------------------------------------------------------------------------------+
|       Static Pressure|        101325|             1|        Pa|        101325|
|               Density|       1.22498|             1|    kg/m^3|       1.22498|
|           Temperature|        288.15|             1|         K|        288.15|
|          Total Energy|        211798|             1|   m^2/s^2|        211798|
|            Velocity-X|       100.087|             1|       m/s|       100.087|
|            Velocity-Y|             0|             1|       m/s|             0|
|            Velocity-Z|             0|             1|       m/s|             0|
|    Velocity Magnitude|       100.087|             1|       m/s|       100.087|
+------------------------------------------------------------------------------+
|           Mach Number|             -|             -|         -|      0.294118|
+------------------------------------------------------------------------------+
Initialize Jacobian structure (Euler). MG level: 0.
Initialize Jacobian structure (Euler). MG level: 1.
Initialize Jacobian structure (Euler). MG level: 2.

------------------- Numerics Preprocessing ( Zone 0 ) -------------------

----------------- Integration Preprocessing ( Zone 0 ) ------------------

------------------- Iteration Preprocessing ( Zone 0 ) ------------------
Euler/Navier-Stokes/RANS fluid iteration.

------------------------------ Begin Solver -----------------------------

Simulation Run using the Single-zone Driver
WARNING: SU2 was not compiled for an AVX-capable architecture. Performance could be better,
         see <a href='https://su2code.github.io/docs_v7/Build-SU2-Linux-MacOS/#compiler-optimizations'>https://su2code.github.io/docs_v7/Build-SU2-Linux-MacOS/#compiler-optimizations</a>
WARNING: SU2 was not compiled for an AVX-capable architecture. Performance could be better,
         see <a href='https://su2code.github.io/docs_v7/Build-SU2-Linux-MacOS/#compiler-optimizations'>https://su2code.github.io/docs_v7/Build-SU2-Linux-MacOS/#compiler-optimizations</a>
WARNING: SU2 was not compiled for an AVX-capable architecture. Performance could be better,
         see <a href='https://su2code.github.io/docs_v7/Build-SU2-Linux-MacOS/#compiler-optimizations'>https://su2code.github.io/docs_v7/Build-SU2-Linux-MacOS/#compiler-optimizations</a>
+----------------------------------------------------------------------------------------------------------------------------------------------+
|   Time_Iter|  Outer_Iter|  Inner_Iter|    Cur_Time|   Time_Step|   Time(sec)|    rms[Rho]|   rms[RhoU]|   rms[RhoV]|   rms[RhoE]|        CEff|
+----------------------------------------------------------------------------------------------------------------------------------------------+
|           0|           0|           0|  0.0000e+00|  0.0000e+00|  1.7462e-01|    8.373383|   11.340190|   11.408519|   13.842489|    0.034826|
|           0|           0|           1|  0.0000e+00|  0.0000e+00|  1.8052e-01|    8.825382|   11.415919|   11.390647|   14.294942|   -0.015998|
|           0|           0|           2|  0.0000e+00|  0.0000e+00|  1.8202e-01|    8.879168|   11.426477|   11.408611|   14.320373|   -0.006719|

----------------------------- Solver Exit -------------------------------

Maximum number of iterations reached (ITER = 3) before convergence.
+-----------------------------------------------------------------------+
|      Convergence Field     |     Value    |   Criterion  |  Converged |
+-----------------------------------------------------------------------+
|                    rms[Rho]|       8.87917|         &lt; -14|          No|
+-----------------------------------------------------------------------+
-------------------------------------------------------------------------
+-----------------------------------------------------------------------+
|        File Writing Summary       |              Filename             |
+-----------------------------------------------------------------------+
|SU2 binary restart                 |restart_flow_aeroelastic_Iterative.dat|

Writing the forces breakdown file (forces_breakdown_aeroelastic_Iterative.dat).
|CSV file                           |surface_flow_aeroelastic_Iterative.csv|

Writing the forces breakdown file (forces_breakdown_aeroelastic_Iterative.dat).
|Tecplot binary                     |flow_aeroelastic_Iterative.szplt   |

Writing the forces breakdown file (forces_breakdown_aeroelastic_Iterative.dat).
|Tecplot binary surface             |surface_flow_aeroelastic_Iterative.szplt|

Writing the forces breakdown file (forces_breakdown_aeroelastic_Iterative.dat).
+-----------------------------------------------------------------------+
Warning: there are 476 non-physical points in the solution.
Warning: 51 reconstructed states for upwinding are non-physical.

--------------------------- Finalizing Solver ---------------------------
Deleted CNumerics container.
Deleted CIntegration container.
Deleted CSolver container.
Deleted CIteration container.
Deleted CInterface container.
Deleted CGeometry container.
Deleted CFreeFormDefBox class.
Deleted CSurfaceMovement class.
Deleted CVolumetricMovement class.
Deleted CConfig container.
Deleted nInst container.
Deleted COutput class.
-------------------------------------------------------------------------

------------------------- Exit Success (SU2_CFD) ------------------------


Running PostAnalysis ...... su2

real	1m10.991s
user	1m15.951s
sys	0m6.607s
+ status=0
+ set +x

=================================================
CAPS verification (using pyCAPS) case aeroelastic_Iterative_SU2_and_Astros.py passed (as expected)
=================================================


=================================================
+ echo 'aeroelasticSimple_Temperature_SU2_and_TACS.py test;'
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESP126/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
aeroelasticSimple_Temperature_SU2_and_TACS.py test;
+ python -u aeroelasticSimple_Temperature_SU2_and_TACS.py -outLevel=0 -noPlotData
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESP126/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt

Running PreAnalysis ...... su2
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 3
	Name = Farfield, index = 1
	Name = SymmPlane, index = 2
	Name = Skin, index = 3
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 0
 
AFLR2    : ---------------------------------------
AFLR2    : AFLR2 LIBRARY
AFLR2    : ADVANCING-FRONT/LOCAL-RECONNECTION
AFLR2    : TRIA/QUAD GRID GENERATOR
AFLR2    : Version Number 9.18.1
AFLR2    : Version Date   06/11/24 @ 05:52PM
AFLR2    : Compile OS     Darwin 23.5.0 arm64
AFLR2    : Compile Date   06/11/24 @ 05:52PM
AFLR2    : Copyright 1994-2021, D.L. Marcum
AFLR2    : ---------------------------------------
 
AFLR4    : ---------------------------------------
AFLR4    : AFLR4 LIBRARY
AFLR4    : ADVANCING-FRONT/LOCAL-RECONNECTION
AFLR4    : TRIA/QUAD SURFACE GRID GENERATOR
AFLR4    : Version Number 11.5.15
AFLR4    : Version Date   07/19/24 @ 07:04PM
AFLR4    : Compile OS     Darwin 23.5.0 arm64
AFLR4    : Compile Date   07/19/24 @ 07:06PM
AFLR4    : Copyright 1994-2021, D.L. Marcum
AFLR4    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.8.1
EGADS    : ---------------------------------------

EGADS    : EGADS CAD Geometry Setup

EGADS    : Model has 1 Active Bodies

EGADS    : Body 0 is a SolidBody
EGADS    : Body 0 has 1 Shells
EGADS    : Body 0 has 9 Faces
EGADS    : Body 0 has 18 Edges
EGADS    : Body 0 has 10 Loops
EGADS    : Body 0 has 12 Nodes

EGADS    : Check Grid BCs

EGADS    : Grid BCs are OK

EGADS    : Face Neighbor-Faces Information

EGADS    : QC  = Face Quad Combination Flag
EGADS    : IER = Face Isolated Edge Refinement Flag
EGADS    : ER  = Face Edge Refinement Factor
EGADS    :       Not applicable for Faces with a FarField Grid BC.
EGADS    : SF  = Face Scale Factor
EGADS    :       Not applicable for Faces with a FarField Grid BC.

EGADS    :   Face          Body    QC   IER       ER    Scale   Neighbor
EGADS    :     ID  Active    ID  Flag  Flag   Weight   Factor   Faces
EGADS    :      1     Yes     0     0     1        0        1   2 3 4 5
EGADS    :      2     Yes     0     0     1        0        1   1 3 5 6
EGADS    :      3     Yes     0     0     1        0        1   1 2 4 6 7 8
EGADS    :      4     Yes     0     0     1        0        1   1 3 5 6
EGADS    :      5     Yes     0     0     1        0        1   1 2 4 6
EGADS    :      6     Yes     0     0     1        0        1   2 3 4 5
EGADS    :      7     Yes     0     0     1        0        1   3 8 9
EGADS    :      8     Yes     0     0     1        0        1   3 7 9
EGADS    :      9     Yes     0     0     1        0        1   7 8

EGADS    : Face Edges Information

EGADS    :   Face   Edges
EGADS    :      1   1 2 -3 -4
EGADS    :      2   5 6 -7 -1
EGADS    :      3   -2 7 9 -8 -10 -11
EGADS    :      4   -12 3 8 -13
EGADS    :      5   4 12 -14 -5
EGADS    :      6   -6 14 13 -9
EGADS    :      7   15 10 -17 -16
EGADS    :      8   17 11 -15 -18
EGADS    :      9   16 18

EGADS    : Face Loops Information

EGADS    :   Face   Loops
EGADS    :      1   1
EGADS    :      2   2
EGADS    :      3   3 4
EGADS    :      4   5
EGADS    :      5   6
EGADS    :      6   7
EGADS    :      7   8
EGADS    :      8   9
EGADS    :      9   10

EGADS    : Loop Edges Information

EGADS    :   Loop  Active   Edges
EGADS    :      1     Yes   1 2 -3 -4
EGADS    :      2     Yes   5 6 -7 -1
EGADS    :      3     Yes   -2 7 9 -8
EGADS    :      4     Yes   -10 -11
EGADS    :      5     Yes   -12 3 8 -13
EGADS    :      6     Yes   4 12 -14 -5
EGADS    :      7     Yes   -6 14 13 -9
EGADS    :      8     Yes   15 10 -17 -16
EGADS    :      9     Yes   17 11 -15 -18
EGADS    :     10     Yes   16 18

EGADS    : Edge Node, Scale Factor, and Neighbor-Faces Information

EGADS    : ESF = Edge Scale Factor
EGADS    :       Not applicable for DEGENERATE Edges or Edges with a FarField
EGADS    :       Grid BC Neighbor Face.

EGADS    :                                             Neighbor
EGADS    :   Edge  Body  Active Node1 Node2      ESF   Faces
EGADS    :      1     0     Yes     2     1        1   1 2
EGADS    :      2     0     Yes     1     3        1   1 3
EGADS    :      3     0     Yes     4     3        1   1 4
EGADS    :      4     0     Yes     2     4        1   1 5
EGADS    :      5     0     Yes     2     5        1   2 5
EGADS    :      6     0     Yes     5     6        1   2 6
EGADS    :      7     0     Yes     1     6        1   2 3
EGADS    :      8     0     Yes     3     7        1   3 4
EGADS    :      9     0     Yes     6     7        1   3 6
EGADS    :     10     0     Yes     8     9        1   3 7
EGADS    :     11     0     Yes     9     8        1   3 8
EGADS    :     12     0     Yes     4    10        1   4 5
EGADS    :     13     0     Yes    10     7        1   4 6
EGADS    :     14     0     Yes     5    10        1   5 6
EGADS    :     15     0     Yes    11     8        1   7 8
EGADS    :     16     0     Yes    11    12        1   7 9
EGADS    :     17     0     Yes    12     9        1   7 8
EGADS    :     18     0     Yes    12    11        1   8 9

EGADS    : Node Information

EGADS    :   Node  Active      Coordinates
EGADS    :      1     Yes                0                0                0
EGADS    :      2     Yes                0               40                0
EGADS    :      3     Yes                0                0               20
EGADS    :      4     Yes                0               40               20
EGADS    :      5     Yes               20               40                0
EGADS    :      6     Yes               20                0                0
EGADS    :      7     Yes               20                0               20
EGADS    :      8     Yes       1.61374306                0                0
EGADS    :      9     Yes                0                0                0
EGADS    :     10     Yes               20               40               20
EGADS    :     11     Yes       2.53650745       3.87298335      0.334116517
EGADS    :     12     Yes       1.57194608       3.87298335      0.249728332

EGADS    : Face and Edge Match Information

EGADS    : No Face Matches Found

AFLR4    : Surface Mesh Spacing Setup

AFLR4    : Max Bounding Box Length     = 40
AFLR4    : Min Bounding Box Length     = 40
AFLR4    : Max Ref Bounding Box Length = 40
AFLR4    : Min Ref Bounding Box Length = 40
AFLR4    : Reference Length            = 1.61374
AFLR4    : BL Thickness                = 0
AFLR4    : Abs Min Surf Spacing        = 0.00403436
AFLR4    : Min Surf Spacing            = 0.161374
AFLR4    : Max Surf Spacing            = 1.21031
AFLR4    : Global Scale Factor         = 1

AFLR4    : Geometry Definition Information

AFLR4    : Definition              Definition   Composite             Grid BC
AFLR4    :         ID                    Type          ID                Type
AFLR4    :          0     glue-only composite           -                   -
AFLR4    :          1            CAD geometry           0            STD w/BL
AFLR4    :          2            CAD geometry           0            STD w/BL
AFLR4    :          3            CAD geometry           0            STD w/BL
AFLR4    :          4            CAD geometry           0            STD w/BL
AFLR4    :          5            CAD geometry           0            STD w/BL
AFLR4    :          6            CAD geometry           0            STD w/BL
AFLR4    :          7            CAD geometry           0            STD w/BL
AFLR4    :          8            CAD geometry           0            STD w/BL
AFLR4    :          9            CAD geometry           0            STD w/BL

AFLR4    : Define CAD surface definition 1
AFLR4    : Define CAD surface definition 2
AFLR4    : Define CAD surface definition 3
AFLR4    : Define CAD surface definition 4
AFLR4    : Define CAD surface definition 5
AFLR4    : Define CAD surface definition 6
AFLR4    : Define CAD surface definition 7
AFLR4    : Define CAD surface definition 8
AFLR4    : Define CAD surface definition 9

AFLR4    : Surface Grid Generation

AFLR4    : Generate optimal mesh on surface definition 1
AFLR2    : Nodes, Trias,Quads=      1318      2502         0
AFLR4    : Nodes, Trias,Quads=      1293      2452         0

AFLR4    : Generate optimal mesh on surface definition 2
AFLR2    : Nodes, Trias,Quads=      1318      2502         0
AFLR4    : Nodes, Trias,Quads=      1298      2462         0

AFLR4    : Generate optimal mesh on surface definition 3
AFLR2    : Nodes, Trias,Quads=      3418      6687         0
AFLR4    : Nodes, Trias,Quads=      3008      5867         0

AFLR4    : Generate optimal mesh on surface definition 4
AFLR2    : Nodes, Trias,Quads=      1316      2498         0
AFLR4    : Nodes, Trias,Quads=      1297      2460         0

AFLR4    : Generate optimal mesh on surface definition 5
AFLR2    : Nodes, Trias,Quads=      1318      2502         0
AFLR4    : Nodes, Trias,Quads=      1297      2460         0

AFLR4    : Generate optimal mesh on surface definition 6
AFLR2    : Nodes, Trias,Quads=      1319      2504         0
AFLR4    : Nodes, Trias,Quads=      1294      2454         0

AFLR4    : Generate optimal mesh on surface definition 7
AFLR2    : Nodes, Trias,Quads=       200       344         0
AFLR4    : Nodes, Trias,Quads=       160       264         0

AFLR4    : Generate optimal mesh on surface definition 8
AFLR2    : Nodes, Trias,Quads=       193       330         0
AFLR4    : Nodes, Trias,Quads=       155       254         0

AFLR4    : Generate optimal mesh on surface definition 9
AFLR2    : Nodes, Trias,Quads=        17        21         0
AFLR4    : Nodes, Trias,Quads=        11         9         0

DGEOM    : Add surface definitions to composite definition 0
DGEOM    : Glue composite surface definition 0
DGEOM    : Nodes,Faces,BEdges=      9343     18682       928

AFLR4    : Curvature BG Surface Grid Generation

AFLR4    : Nodes, Faces      =      9343     18682

AFLR4    : Surface Grid Generation

AFLR4    : Generate optimal mesh on surface definition 1
AFLR2    : Nodes, Trias,Quads=      1337      2540         0
AFLR4    : Nodes, Trias,Quads=      1321      2508         0

AFLR4    : Generate optimal mesh on surface definition 2
AFLR2    : Nodes, Trias,Quads=      1339      2544         0
AFLR4    : Nodes, Trias,Quads=      1318      2502         0

AFLR4    : Generate optimal mesh on surface definition 3
AFLR2    : Nodes, Trias,Quads=      3782      7410         0
AFLR4    : Nodes, Trias,Quads=      2950      5746         0

AFLR4    : Generate optimal mesh on surface definition 4
AFLR2    : Nodes, Trias,Quads=      1339      2544         0
AFLR4    : Nodes, Trias,Quads=      1318      2502         0

AFLR4    : Generate optimal mesh on surface definition 5
AFLR2    : Nodes, Trias,Quads=      1338      2542         0
AFLR4    : Nodes, Trias,Quads=      1322      2510         0

AFLR4    : Generate optimal mesh on surface definition 6
AFLR2    : Nodes, Trias,Quads=      1340      2546         0
AFLR4    : Nodes, Trias,Quads=      1321      2508         0

AFLR4    : Generate optimal mesh on surface definition 7
AFLR2    : Nodes, Trias,Quads=       233       404         0
AFLR4    : Nodes, Trias,Quads=       210       358         0

AFLR4    : Generate optimal mesh on surface definition 8
AFLR2    : Nodes, Trias,Quads=       224       386         0
AFLR4    : Nodes, Trias,Quads=       196       330         0

AFLR4    : Generate optimal mesh on surface definition 9
AFLR2    : Nodes, Trias,Quads=        18        22         0
AFLR4    : Nodes, Trias,Quads=        12        10         0

DGEOM    : Add surface definitions to composite definition 0
DGEOM    : Glue composite surface definition 0
DGEOM    : Nodes,Faces,BEdges=      9489     18974       946

OVERALL  : CPU Time          =     0.138   seconds
Body 1 (of 1)
Number of nodes    = 9489
Number of elements = 18974
Number of triangle elements      = 18974
Number of quadrilateral elements = 0
----------------------------
Total number of nodes    = 9489
Total number of elements = 18974
Total number of triangle elements      = 18974
Total number of quadrilateral elements = 0
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 0
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 3
	Name = Farfield, index = 1
	Name = SymmPlane, index = 2
	Name = Skin, index = 3
Getting volume mesh
 
AFLR2    : ---------------------------------------
AFLR2    : AFLR2 LIBRARY
AFLR2    : ADVANCING-FRONT/LOCAL-RECONNECTION
AFLR2    : TRIA/QUAD GRID GENERATOR
AFLR2    : Version Number 9.18.1
AFLR2    : Version Date   06/11/24 @ 05:52PM
AFLR2    : Compile OS     Darwin 23.5.0 arm64
AFLR2    : Compile Date   06/11/24 @ 05:52PM
AFLR2    : Copyright 1994-2021, D.L. Marcum
AFLR2    : ---------------------------------------
 
AFLR4    : ---------------------------------------
AFLR4    : AFLR4 LIBRARY
AFLR4    : ADVANCING-FRONT/LOCAL-RECONNECTION
AFLR4    : TRIA/QUAD SURFACE GRID GENERATOR
AFLR4    : Version Number 11.5.15
AFLR4    : Version Date   07/19/24 @ 07:04PM
AFLR4    : Compile OS     Darwin 23.5.0 arm64
AFLR4    : Compile Date   07/19/24 @ 07:06PM
AFLR4    : Copyright 1994-2021, D.L. Marcum
AFLR4    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.8.1
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.8.1
EGADS    : ---------------------------------------
Volume mesh:
	Number of nodes          = 60093
	Number of elements       = 345939
	Number of triangles      = 18974
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 326965
	Number of pyramids       = 0
	Number of prisms         = 0
	Number of hexahedrals    = 0

Writing SU2 file ....
Finished writing SU2 file

Getting CFD boundary conditions
	Boundary condition name - Farfield
	Boundary condition name - Skin
	Boundary condition name - SymmPlane
	Done getting CFD boundary conditions
Info: No recognized data transfer names found.
Warning: The su2 cfg file will be overwritten!
Write SU2 configuration file for version "BlackBird (7.5.1) "


Running SU2......

-------------------------------------------------------------------------
|    ___ _   _ ___                                                      |
|   / __| | | |_  )   Release 8.0.0 "Harrier"                           |
|   \__ \ |_| |/ /                                                      |
|   |___/\___//___|   Suite (Computational Fluid Dynamics Code)         |
|                                                                       |
-------------------------------------------------------------------------
| SU2 Project Website: <a href='https://su2code.github.io'>https://su2code.github.io</a>                        |
|                                                                       |
| The SU2 Project is maintained by the SU2 Foundation                   |
| (<a href='http://su2foundation.org'>http://su2foundation.org</a>)                                            |
-------------------------------------------------------------------------
| Copyright 2012-2023, SU2 Contributors                                 |
|                                                                       |
| SU2 is free software; you can redistribute it and/or                  |
| modify it under the terms of the GNU Lesser General Public            |
| License as published by the Free Software Foundation; either          |
| version 2.1 of the License, or (at your option) any later version.    |
|                                                                       |
| SU2 is distributed in the hope that it will be useful,                |
| but WITHOUT ANY WARRANTY; without even the implied warranty of        |
| MERCHANTABILITY or FITNESS FOR A PARTICULAR PURPOSE. See the GNU      |
| Lesser General Public License for more details.                       |
|                                                                       |
| You should have received a copy of the GNU Lesser General Public      |
| License along with SU2. If not, see &lt;<a href='http://www.gnu.org/licenses/'>http://www.gnu.org/licenses/</a>&gt;.   |
-------------------------------------------------------------------------

Parsing config file for zone 0

----------------- Physical Case Definition ( Zone 0 ) -------------------
Compressible Euler equations.
Mach number: 0.294118.
Angle of attack (AoA): 0 deg, and angle of sideslip (AoS): 0 deg.
No restart solution, use the values at infinity (freestream).
Dimensional simulation.
The reference area is 1 m^2.
The semi-span will be computed using the max y(3D) value.
The reference length is 1 m.
Reference origin for moment evaluation is (0, 0, 0).
Surface(s) where the force coefficients are evaluated: BC_3.

Surface(s) plotted in the output file: BC_3.
Surface(s) affected by the design variables: BC_3.
Input mesh file name: ../aflr3/aflr3_CAPS.su2

--------------- Space Numerical Integration ( Zone 0 ) ------------------
Roe (with entropy fix = 0.001) solver for the flow inviscid terms.
Standard Roe without low-dissipation function.
Second order integration in space, with slope limiter.
Venkatakrishnan slope-limiting method, with constant: 0.05.
The reference element size is: 1. 
Gradient for upwind reconstruction: inverse-distance weighted Least-Squares.
Gradient for viscous and source terms: inverse-distance weighted Least-Squares.

--------------- Time Numerical Integration  ( Zone 0 ) ------------------
Local time stepping (steady state simulation).
Euler implicit method for the flow equations.
FGMRES is used for solving the linear system.
Using a ILU(0) preconditioning.
Convergence criteria of the linear solver: 1e-06.
Max number of linear iterations: 10.
V Multigrid Cycle, with 2 multigrid levels.
Damping factor for the residual restriction: 0.75.
Damping factor for the correction prolongation: 0.75.
No CFL adaptation.
+-------------------------------------------+
|  MG Level| Presmooth|PostSmooth|CorrectSmo|
+-------------------------------------------+
|         0|         1|         0|         0|
|         1|         2|         0|         0|
|         2|         3|         0|         0|
+-------------------------------------------+
Courant-Friedrichs-Lewy number:       10

------------------ Convergence Criteria  ( Zone 0 ) ---------------------
Maximum number of solver subiterations: 3.
Begin convergence monitoring at iteration 5.
Residual minimum value: 1e-14.
Cauchy series min. value: 1e-10.
Number of Cauchy elements: 100.
Begin windowed time average at iteration 0.

-------------------- Output Information ( Zone 0 ) ----------------------
File writing frequency: 
+------------------------------------+
|                     File| Frequency|
+------------------------------------+
|                  RESTART|       250|
|              SURFACE_CSV|       250|
|                  TECPLOT|       250|
|          SURFACE_TECPLOT|       250|
+------------------------------------+
Writing the convergence history file every 1 inner iterations.
Writing the screen convergence history every 1 inner iterations.
The tabular file format is CSV (.csv).
Convergence history file name: history.
Forces breakdown file name: forces_breakdown_aeroelasticSimple_Temperature_SM.dat.
Surface file name: surface_flow_aeroelasticSimple_Temperature_SM.
Volume file name: flow_aeroelasticSimple_Temperature_SM.
Restart file name: restart_flow_aeroelasticSimple_Temperature_SM.dat.

------------- Config File Boundary Information ( Zone 0 ) ---------------
+-----------------------------------------------------------------------+
|                        Marker Type|                        Marker Name|
+-----------------------------------------------------------------------+
|                         Euler wall|                               BC_3|
+-----------------------------------------------------------------------+
|                          Far-field|                               BC_1|
+-----------------------------------------------------------------------+
|                     Symmetry plane|                               BC_2|
+-----------------------------------------------------------------------+

-------------------- Output Preprocessing ( Zone 0 ) --------------------

WARNING: SURFACE_PRESSURE_DROP can only be computed for at least 2 surfaces (outlet, inlet, ...)

Screen output fields: TIME_ITER, OUTER_ITER, INNER_ITER, CUR_TIME, TIME_STEP, WALL_TIME, RMS_DENSITY, RMS_MOMENTUM-X, RMS_MOMENTUM-Y, RMS_ENERGY, EFFICIENCY
History output group(s): ITER, TIME_DOMAIN, WALL_TIME, RMS_RES, AERO_COEFF
Convergence field(s): RMS_DENSITY
Warning: No (valid) fields chosen for time convergence monitoring. Time convergence monitoring inactive.
Volume output fields: COORDINATES, SOLUTION, PRIMITIVE

------------------- Geometry Preprocessing ( Zone 0 ) -------------------
Three dimensional problem.
60093 grid points.
326965 volume elements.
3 surface markers.
12530 boundary elements in index 0 (Marker = BC_1).
5746 boundary elements in index 1 (Marker = BC_2).
698 boundary elements in index 2 (Marker = BC_3).
326965 tetrahedra.
Setting point connectivity.
Renumbering points (Reverse Cuthill McKee Ordering).
Recomputing point connectivity.
Setting element connectivity.
Checking the numerical grid orientation.
All volume elements are correctly orientend.
All surface elements are correctly orientend.
Identifying edges and vertices.
Setting the control volume structure.
Volume of the computational grid: 63999.5.
Searching for the closest normal neighbors to the surfaces.
Storing a mapping from global to local point index.
Compute the surface curvature.
Max K: 83.4538. Mean K: 0.86237. Standard deviation K: 5.00385.
Checking for periodicity.
Computing mesh quality statistics for the dual control volumes.
+--------------------------------------------------------------+
|           Mesh Quality Metric|        Minimum|        Maximum|
+--------------------------------------------------------------+
|    Orthogonality Angle (deg.)|        54.7348|        86.8035|
|     CV Face Area Aspect Ratio|        1.06478|        21.5651|
|           CV Sub-Volume Ratio|              1|        8.64744|
+--------------------------------------------------------------+
Setting the multigrid structure.
+-------------------------------------------+
|  MG Level|       CVs|Aggl. Rate|       CFL|
+-------------------------------------------+
|         0|     60093|    1/1.00|        10|
|         1|     10214|    1/5.88|     8.309|
|         2|      1799|    1/5.68|   6.98637|
+-------------------------------------------+
Finding max control volume width.
Semi-span length = 3.87298 m.
Wetted area = 9.2451 m^2.
Area projection in the x-plane = 0.651846 m^2, y-plane = 0.30478 m^2, z-plane = 4.4157 m^2.
Max. coordinate in the x-direction = 2.53651 m, y-direction = 3.87298 m, z-direction = 0.38 m.
Min. coordinate in the x-direction = 0 m, y-direction = -2.86329e-18 m, z-direction = -0.0467611 m.
Checking if Euler &amp; Symmetry markers are straight/plane:
Boundary marker BC_3 is NOT a single plane.
Boundary marker BC_2 is a single plane.
Computing wall distances.

-------------------- Solver Preprocessing ( Zone 0 ) --------------------
Inviscid flow: Computing density based on free-stream
temperature and pressure using the ideal gas law.
Force coefficients computed using free-stream values.

-- Models:
+------------------------------------------------------------------------------+
|          Viscosity Model|        Conductivity Model|              Fluid Model|
+------------------------------------------------------------------------------+
|                        -|                         -|             STANDARD_AIR|
+------------------------------------------------------------------------------+
-- Fluid properties:
+------------------------------------------------------------------------------+
|                  Name|    Dim. value|    Ref. value|      Unit|Non-dim. value|
+------------------------------------------------------------------------------+
|          Gas Constant|       287.058|             1|  N.m/kg.K|       287.058|
|      Spec. Heat Ratio|             -|             -|         -|           1.4|
+------------------------------------------------------------------------------+
-- Initial and free-stream conditions:
+------------------------------------------------------------------------------+
|                  Name|    Dim. value|    Ref. value|      Unit|Non-dim. value|
+------------------------------------------------------------------------------+
|       Static Pressure|        101325|             1|        Pa|        101325|
|               Density|       1.22498|             1|    kg/m^3|       1.22498|
|           Temperature|        288.15|             1|         K|        288.15|
|          Total Energy|        211798|             1|   m^2/s^2|        211798|
|            Velocity-X|       100.087|             1|       m/s|       100.087|
|            Velocity-Y|             0|             1|       m/s|             0|
|            Velocity-Z|             0|             1|       m/s|             0|
|    Velocity Magnitude|       100.087|             1|       m/s|       100.087|
+------------------------------------------------------------------------------+
|           Mach Number|             -|             -|         -|      0.294118|
+------------------------------------------------------------------------------+
Initialize Jacobian structure (Euler). MG level: 0.
Initialize Jacobian structure (Euler). MG level: 1.
Initialize Jacobian structure (Euler). MG level: 2.

------------------- Numerics Preprocessing ( Zone 0 ) -------------------

----------------- Integration Preprocessing ( Zone 0 ) ------------------

------------------- Iteration Preprocessing ( Zone 0 ) ------------------
Euler/Navier-Stokes/RANS fluid iteration.

------------------------------ Begin Solver -----------------------------

Simulation Run using the Single-zone Driver
WARNING: SU2 was not compiled for an AVX-capable architecture. Performance could be better,
         see <a href='https://su2code.github.io/docs_v7/Build-SU2-Linux-MacOS/#compiler-optimizations'>https://su2code.github.io/docs_v7/Build-SU2-Linux-MacOS/#compiler-optimizations</a>
WARNING: SU2 was not compiled for an AVX-capable architecture. Performance could be better,
         see <a href='https://su2code.github.io/docs_v7/Build-SU2-Linux-MacOS/#compiler-optimizations'>https://su2code.github.io/docs_v7/Build-SU2-Linux-MacOS/#compiler-optimizations</a>
WARNING: SU2 was not compiled for an AVX-capable architecture. Performance could be better,
         see <a href='https://su2code.github.io/docs_v7/Build-SU2-Linux-MacOS/#compiler-optimizations'>https://su2code.github.io/docs_v7/Build-SU2-Linux-MacOS/#compiler-optimizations</a>
+----------------------------------------------------------------------------------------------------------------------------------------------+
|   Time_Iter|  Outer_Iter|  Inner_Iter|    Cur_Time|   Time_Step|   Time(sec)|    rms[Rho]|   rms[RhoU]|   rms[RhoV]|   rms[RhoE]|        CEff|
+----------------------------------------------------------------------------------------------------------------------------------------------+
|           0|           0|           0|  0.0000e+00|  0.0000e+00|  1.0022e+00|   -1.355330|    0.925001|    0.586785|    4.113776|   -0.972828|
|           0|           0|           1|  0.0000e+00|  0.0000e+00|  9.9292e-01|   -1.745808|    0.767133|    0.413608|    3.711112|   -0.534020|
|           0|           0|           2|  0.0000e+00|  0.0000e+00|  9.8809e-01|   -1.758263|    0.583631|    0.231030|    3.699433|    1.633106|

----------------------------- Solver Exit -------------------------------

Maximum number of iterations reached (ITER = 3) before convergence.
+-----------------------------------------------------------------------+
|      Convergence Field     |     Value    |   Criterion  |  Converged |
+-----------------------------------------------------------------------+
|                    rms[Rho]|      -1.75826|         &lt; -14|          No|
+-----------------------------------------------------------------------+
-------------------------------------------------------------------------
+-----------------------------------------------------------------------+
|        File Writing Summary       |              Filename             |
+-----------------------------------------------------------------------+
|SU2 binary restart                 |restart_flow_aeroelasticSimple_Temperature_SM.dat|

Writing the forces breakdown file (forces_breakdown_aeroelasticSimple_Temperature_SM.dat).
|CSV file                           |surface_flow_aeroelasticSimple_Temperature_SM.csv|

Writing the forces breakdown file (forces_breakdown_aeroelasticSimple_Temperature_SM.dat).
|Tecplot binary                     |flow_aeroelasticSimple_Temperature_SM.szplt|

Writing the forces breakdown file (forces_breakdown_aeroelasticSimple_Temperature_SM.dat).
|Tecplot binary surface             |surface_flow_aeroelasticSimple_Temperature_SM.szplt|

Writing the forces breakdown file (forces_breakdown_aeroelasticSimple_Temperature_SM.dat).
+-----------------------------------------------------------------------+

--------------------------- Finalizing Solver ---------------------------
Deleted CNumerics container.
Deleted CIntegration container.
Deleted CSolver container.
Deleted CIteration container.
Deleted CInterface container.
Deleted CGeometry container.
Deleted CFreeFormDefBox class.
Deleted CSurfaceMovement class.
Deleted CVolumetricMovement class.
Deleted CConfig container.
Deleted nInst container.
Deleted COutput class.
-------------------------------------------------------------------------

------------------------- Exit Success (SU2_CFD) ------------------------


Running PostAnalysis ...... su2

Running PreAnalysis ...... tacs
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 2
	Name = Skin, index = 1
	Name = Rib_Root, index = 2
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 0
Getting surface mesh for body 1 (of 1)
Body 1 (of 1)
Number of nodes    = 12
Number of elements = 12
Number of triangle elements      = 4
Number of quadrilateral elements = 8
----------------------------
Total number of nodes    = 12
Total number of elements = 12
Mapping Csys attributes ................
	Number of unique Csys attributes = 0

Getting FEA coordinate systems.......
	Number of coordinate systems - 0
	No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
	Number of unique capsConstraint attributes = 1
	Name = Rib_Root, index = 1
Mapping capsLoad attributes ................
	Number of unique capsLoad attributes = 1
	Name = Skin, index = 1
Mapping capsBound attributes ................
	Number of unique capsBound attributes = 3
	Name = Skin_Top, index = 1
	Name = Skin_Bottom, index = 2
	Name = Skin_Tip, index = 3
Mapping capsConnect attributes ................
	Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
	Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
	Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 2
	Name = Skin, index = 1
	Name = Rib_Root, index = 2
Setting FEA Data
	Mesh for body = 0
	Number of nodal coordinates = 12
	Number of elements = 12
	Elemental Nodes = 0
	Elemental Rods  = 0
	Elemental Tria3 = 4
	Elemental Quad4 = 8

Getting FEA materials.......
	Number of materials - 1
	Material name - Madeupium
	Done getting FEA materials

Getting FEA properties.......
	Number of properties - 2
	Property name - Rib_Root
	Property name - Skin
	Done getting FEA properties
Updating mesh element types based on properties input

Getting FEA constraints.......
	Number of constraints - 1
	Constraint name - edgeConstraint
	No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement"
	Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults

Getting FEA loads.......
	Number of loads - 1
	Load name - Skin
	No "groupName" specified for Load tuple Skin, going to use load name
	Done getting FEA loads
Design_Variable tuple is NULL - No design variables applied
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL

Getting FEA analyses.......
	Number of analyses - 1
	Analysis name - Default
	Done getting FEA analyses
Mapping Csys attributes ................
	Number of unique Csys attributes = 0

Getting FEA coordinate systems.......
	Number of coordinate systems - 0
	No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
	Number of unique capsConstraint attributes = 1
	Name = Rib_Root, index = 1
Mapping capsLoad attributes ................
	Number of unique capsLoad attributes = 1
	Name = Skin, index = 1
Mapping capsBound attributes ................
	Number of unique capsBound attributes = 3
	Name = Skin_Top, index = 1
	Name = Skin_Bottom, index = 2
	Name = Skin_Tip, index = 3
Mapping capsConnect attributes ................
	Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
	Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
	Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 2
	Name = Skin, index = 1
	Name = Rib_Root, index = 2
Setting FEA Data
	Mesh for body = 0
	Number of nodal coordinates = 12
	Number of elements = 12
	Elemental Nodes = 0
	Elemental Rods  = 0
	Elemental Tria3 = 4
	Elemental Quad4 = 8
Reading SU2 AeroLoad File - surface_flow_aeroelasticSimple_Temperature_SM.csv
	Number of variables = 16
	Number of data points = 361
 CAPS Info: Bound 'Skin_Top' Normalized Integrated 'Temperature'
            Rank 0: src = 1.497275e+03, tgt = 1.497275e+03, diff = 8.156515e-06
Mapping Csys attributes ................
	Number of unique Csys attributes = 0

Getting FEA coordinate systems.......
	Number of coordinate systems - 0
	No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
	Number of unique capsConstraint attributes = 1
	Name = Rib_Root, index = 1
Mapping capsLoad attributes ................
	Number of unique capsLoad attributes = 1
	Name = Skin, index = 1
Mapping capsBound attributes ................
	Number of unique capsBound attributes = 3
	Name = Skin_Top, index = 1
	Name = Skin_Bottom, index = 2
	Name = Skin_Tip, index = 3
Mapping capsConnect attributes ................
	Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
	Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
	Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 2
	Name = Skin, index = 1
	Name = Rib_Root, index = 2
Setting FEA Data
	Mesh for body = 0
	Number of nodal coordinates = 12
	Number of elements = 12
	Elemental Nodes = 0
	Elemental Rods  = 0
	Elemental Tria3 = 4
	Elemental Quad4 = 8
Reading SU2 AeroLoad File - surface_flow_aeroelasticSimple_Temperature_SM.csv
	Number of variables = 16
	Number of data points = 361
 CAPS Info: Bound 'Skin_Bottom' Normalized Integrated 'Temperature'
            Rank 0: src = 1.453270e+03, tgt = 1.453270e+03, diff = 4.021617e-06
Mapping Csys attributes ................
	Number of unique Csys attributes = 0

Getting FEA coordinate systems.......
	Number of coordinate systems - 0
	No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
	Number of unique capsConstraint attributes = 1
	Name = Rib_Root, index = 1
Mapping capsLoad attributes ................
	Number of unique capsLoad attributes = 1
	Name = Skin, index = 1
Mapping capsBound attributes ................
	Number of unique capsBound attributes = 3
	Name = Skin_Top, index = 1
	Name = Skin_Bottom, index = 2
	Name = Skin_Tip, index = 3
Mapping capsConnect attributes ................
	Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
	Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
	Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 2
	Name = Skin, index = 1
	Name = Rib_Root, index = 2
Setting FEA Data
	Mesh for body = 0
	Number of nodal coordinates = 12
	Number of elements = 12
	Elemental Nodes = 0
	Elemental Rods  = 0
	Elemental Tria3 = 4
	Elemental Quad4 = 8
Reading SU2 AeroLoad File - surface_flow_aeroelasticSimple_Temperature_SM.csv
	Number of variables = 16
	Number of data points = 361
 CAPS Info: Bound 'Skin_Tip' Normalized Integrated 'Temperature'
            Rank 0: src = 2.098244e+01, tgt = 2.098244e+01, diff = 1.101341e-13
Extracting external thermal loads from data transfer....
	TransferName = Skin_Top
	Number of Nodes = 9 (total = 9)
Extracting external thermal loads from data transfer....
	TransferName = Skin_Bottom
	Number of Nodes = 9 (total = 18)
Extracting external thermal loads from data transfer....
	TransferName = Skin_Tip
	Number of Nodes = 4 (total = 16)

Writing Nastran grid and connectivity file (in free field format) ....
Finished writing Nastran grid file

Writing subElement types (if any) - appending mesh file

Writing TACS instruction file....
	Writing analysis cards
	Writing load ADD cards
	Writing constraint ADD cards
	Writing load cards
	Writing constraint cards
	Writing material cards
	Writing property cards

Running PostAnalysis ...... tacs

real	0m10.084s
user	0m10.540s
sys	0m0.831s
+ status=0
+ set +x

=================================================
CAPS verification (using pyCAPS) case aeroelasticSimple_Temperature_SU2_and_TACS.py passed (as expected)
=================================================

Running.... CORSAIRLITE PyTests


=================================================
+ echo 'gp.py test;'
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESP126/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
gp.py test;
+ python -u gp.py -outLevel=0
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESP126/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt

Objective
---------
   0.00713 dimensionless

Variables
---------
   x  :   3.00000   [-]   The X variable
   y  :  81.00008   [-]   The Y variable
   z  :   0.19245   [-]   The Z variable

Sensitivities
-------------
   No Constants in the Formulation

Solve Report
------------
   Solve Method           :  Geometric Program 
   Classification         :  Convex 
   Solver                 :  cvxopt 


real	0m3.343s
user	0m1.355s
sys	0m0.097s
+ status=0
+ set +x

=================================================
CAPS verification (using pyCAPS) case gp.py passed (as expected)
=================================================


=================================================
+ echo 'qp.py test;'
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESP126/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
qp.py test;
+ python -u qp.py -outLevel=0
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESP126/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt

Objective
---------
   -21.56250 dimensionless

Variables
---------
   x  :  1.62500   [-]   The X variable
   y  :  1.37500   [-]   The Y variable

Constants
---------
   c   :  3         [-]   A constant
   c2  :  2         [-]   A constant

Sensitivities
-------------
   c   :  + 0.46957   A constant
   c2  :  - 0.22338   A constant

Solve Report
------------
   Solve Method           :  Quadratic Program 
   Classification         :  Convex 
   Solver                 :  cvxopt 


real	0m0.689s
user	0m1.220s
sys	0m0.044s
+ status=0
+ set +x

=================================================
CAPS verification (using pyCAPS) case qp.py passed (as expected)
=================================================


=================================================
+ echo 'sp.py test;'
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESP126/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
sp.py test;
+ python -u sp.py -outLevel=0
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESP126/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt

Objective
---------
   0.45721 dimensionless

Variables
---------
   x  :  2.56155   [-]   The X variable
   y  :  6.56155   [-]   The Y variable
   z  :  1.17116   [-]   The Z variable

Constants
---------
   c  :  2         [-]   A constant

Sensitivities
-------------
   Sensitivities not computed

Solve Report
------------
   Solve Method           :  Signomial Program--Standard 
   Classification         :  Iterative 
   Solver                 :  cvxopt 
   Number of Iterations   :  3 
   Termination Status     :  Converged, relative error (3.15e-04) is less than specified tolerance (1.00e-03) 


real	0m0.679s
user	0m1.207s
sys	0m0.046s
+ status=0
+ set +x

=================================================
CAPS verification (using pyCAPS) case sp.py passed (as expected)
=================================================


=================================================
+ echo 'boydBox.py test;'
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESP126/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
boydBox.py test;
+ python -u boydBox.py -outLevel=0
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESP126/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt

Objective
---------
   0.00520 1 / meter ** 3

Variables
---------
   d  :  11.26658   meter   The Z variable
   h  :   2.92246   meter   The Y variable
   w  :   5.84486   meter   The X variable

Constants
---------
   Aflr   :  1000         meter ** 2   Area of floor          
   Awall  :   100         meter ** 2   Area of wall           
   alpha  :     0.50000      [-]       Aspect Ratio Constraint
   beta   :     2            [-]       Aspect Ratio Constraint
   delta  :     2            [-]       Aspect Ratio Constraint
   gamma  :     0.50000      [-]       Aspect Ratio Constraint

Sensitivities
-------------
   Sensitivities not computed

Solve Report
------------
   Solve Method           :  Geometric Program 
   Classification         :  Convex 
   Solver                 :  cvxopt 


real	0m0.604s
user	0m1.134s
sys	0m0.044s
+ status=0
+ set +x

=================================================
CAPS verification (using pyCAPS) case boydBox.py passed (as expected)
=================================================


=================================================
+ echo 'hoburg_gp.py test;'
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESP126/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
hoburg_gp.py test;
+ python -u hoburg_gp.py -outLevel=0
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESP126/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt

Objective
---------
   5905.58568 newton

Variables
---------
   AR          :       20.36983        [-]         aspect ratio                                                            
   C_D_0       :        0.01271        [-]         Drag Coefficient, segment 0                                             
   C_D_1       :        0.01273        [-]         Drag Coefficient, segment 1                                             
   C_D_2       :        0.00778        [-]         Drag Coefficient, segment 2                                             
   C_Dfuse_0   :        0.00180        [-]         Fuselage Drag Coefficient, segment 0                                    
   C_Dfuse_1   :        0.00180        [-]         Fuselage Drag Coefficient, segment 1                                    
   C_Dfuse_2   :        0.00180        [-]         Fuselage Drag Coefficient, segment 2                                    
   C_Di_0      :        0.00542        [-]         Induced Drag Coefficient, segment 0                                     
   C_Di_1      :        0.00542        [-]         Induced Drag Coefficient, segment 1                                     
   C_Di_2      :        0.00023        [-]         Induced Drag Coefficient, segment 2                                     
   C_Dp_0      :        0.00549        [-]         Wing Profile Drag Coefficient, segment 0                                
   C_Dp_1      :        0.00551        [-]         Wing Profile Drag Coefficient, segment 1                                
   C_Dp_2      :        0.00575        [-]         Wing Profile Drag Coefficient, segment 2                                
   C_L_0       :        0.57420        [-]         Lift Coefficient, segment 0                                             
   C_L_1       :        0.57421        [-]         Lift Coefficient, segment 1                                             
   C_L_2       :        0.11881        [-]         Lift Coefficient, segment 2                                             
   I_cap_bar   :        0.00002        [-]         Area moment of inertia of cap on 2D cross section, normalized by chord^4
   M_r_bar     :    36139.20785       newton       Root Bending unit per unit chord                                        
   P_max       :  1185884.98442        watt        Maximum Engine Power                                                    
   R           :     4999.98983     kilometer      Single Segment range                                                    
   Re_0        :  4232645.50367        [-]         Reynolds Number, segment 0                                              
   Re_1        :  4051247.93913        [-]         Reynolds Number, segment 1                                              
   Re_2        :  9305153.26607        [-]         Reynolds Number, segment 2                                              
   S           :       27.73109     meter ** 2     total wing area                                                         
   T_0         :      746.21338       newton       Thrust, segment 0                                                       
   T_1         :      684.51827       newton       Thrust, segment 1                                                       
   T_2         :     2208.51611       newton       Thrust, segment 2                                                       
   V_0         :       68.23357   meter / second   Velocity, segment 0                                                     
   V_1         :       65.30930   meter / second   Velocity, segment 1                                                     
   V_2         :      150.00638   meter / second   Velocity, segment 2                                                     
   V_stall     :       37.99896   meter / second   stall speed                                                             
   W_0         :    33698.97702       newton       Weight, segment 0                                                       
   W_1         :    30873.13301       newton       Weight, segment 1                                                       
   W_2         :    33698.96566       newton       Weight, segment 2                                                       
   W_MTO       :    36788.13387       newton       Maximum Takeoff Weight                                                  
   W_cap       :     4091.65066       newton       Weight of Wing Spar Cap                                                 
   W_eng       :     2806.10727       newton       Engine Weight                                                           
   W_fuel_out  :     3079.86524       newton       Weight of fuel, outbound                                                
   W_fuel_ret  :     2825.71897       newton       Weight of fuel, return                                                  
   W_pay       :     4905.15902       newton       Payload Weight                                                          
   W_tilde     :    22409.98513       newton       Dry Weight, no wing                                                     
   W_web       :      139.91823       newton       Weight of Wing Spar Shear Web                                           
   W_wing      :     8462.91404       newton       wing weight                                                             
   W_zfw       :    30872.92436       newton       Zero Fuel Weight                                                        
   eta_0_0     :        0.26999        [-]         Overall Efficiency, segment 0                                           
   eta_0_1     :        0.26996        [-]         Overall Efficiency, segment 1                                           
   eta_0_2     :        0.27945        [-]         Overall Efficiency, segment 2                                           
   eta_i_0     :        0.90752        [-]         Inviscid Propeller Efficiency, segment 0                                
   eta_i_1     :        0.90742        [-]         Inviscid Propeller Efficiency, segment 1                                
   eta_i_2     :        0.93932        [-]         Inviscid Propeller Efficiency, segment 2                                
   eta_prop_0  :        0.77139        [-]         Propeller Efficiency, segment 0                                         
   eta_prop_1  :        0.77131        [-]         Propeller Efficiency, segment 1                                         
   eta_prop_2  :        0.79842        [-]         Propeller Efficiency, segment 2                                         
   nu          :        0.78603        [-]         Placeholder, (1+lam_w+lam_w**2)/(1+lam_w)**2                            
   p           :        1.90003        [-]         Dummy Variable (1+2*lam_w)                                              
   q           :        1.45002        [-]         Dummy Variable (1+lam_w)                                                
   t_cap_bar   :        0.00456        [-]         Spar cap thickness per unit chord                                       
   t_web_bar   :        0.00069        [-]         Spar web thickness per unit chord                                       
   tau         :        0.15000        [-]         airfoil thickness to chord ratio                                        
   z_bre_0     :        0.08745        [-]         Breguet Range Factor, segment 0                                         
   z_bre_1     :        0.08758        [-]         Breguet Range Factor, segment 1                                         

Constants
---------
   A_prop           :         0.78500           meter ** 2          Disk area of propeller                             
   CDA0             :         0.05000           meter ** 2          fuselage drag area                                 
   C_Lmax           :         1.50000              [-]              max CL with flaps down                             
   N_lift           :         6                    [-]              Ultimate Load Factor                               
   W_fixed          :     14700                   newton            fixed weight                                       
   e                :         0.95000              [-]              Oswald efficiency factor                           
   eta_eng          :         0.35000              [-]              Engine Efficiency                                  
   eta_v            :         0.85000              [-]              Propeller Viscous Efficiency                       
   f_wadd           :         2                    [-]              Added Weight Fraction                              
   g                :         9.81000      meter / second ** 2      Gravitational constant                             
   h_fuel           :  46000000              joule / kilogram       Fuel Specific energy density                       
   k_ew             :         0.03720     newton / watt ** 0.803    Constant for engine weight                         
   mu               :         0.00002   kilogram / meter / second   viscosity of air                                   
   r_h              :         0.75000              [-]              Ratio of height at rear spar to maximum wing height
   rho              :         0.90912     kilogram / meter ** 3     density of air                                     
   rho_SL           :         1.22500     kilogram / meter ** 3     density of air, sea level                          
   rho_cap          :      2700           kilogram / meter ** 3     Density of wing cap material (aluminum)            
   rho_web          :      2700           kilogram / meter ** 3     Density of wing web material (aluminum)            
   sigma_max        :       310                 megapascal          Allowable tensile stress of aluminum               
   sigma_max_shear  :       167                 megapascal          Allowable shear stress of aluminum                 
   w_bar            :         0.50000              [-]              Ratio of spar box width to chord length            

Sensitivities
-------------
   Sensitivities not computed

Solve Report
------------
   Solve Method           :  Geometric Program 
   Classification         :  Convex 
   Solver                 :  cvxopt 


real	0m4.527s
user	0m5.032s
sys	0m0.048s
+ status=0
+ set +x

=================================================
CAPS verification (using pyCAPS) case hoburg_gp.py passed (as expected)
=================================================


=================================================
+ echo 'hoburg_blackbox.py test;'
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESP126/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
hoburg_blackbox.py test;
+ python -u hoburg_blackbox.py -outLevel=0
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESP126/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt

Objective
---------
   5905.2294 newton

Variables
---------
   AR          :       20.3737        [-]         aspect ratio                                                            
   C_D_0       :        0.0127        [-]         Drag Coefficient, segment 0                                             
   C_D_1       :        0.0127        [-]         Drag Coefficient, segment 1                                             
   C_D_2       :        0.0078        [-]         Drag Coefficient, segment 2                                             
   C_Dfuse_0   :        0.0018        [-]         Fuselage Drag Coefficient, segment 0                                    
   C_Dfuse_1   :        0.0018        [-]         Fuselage Drag Coefficient, segment 1                                    
   C_Dfuse_2   :        0.0018        [-]         Fuselage Drag Coefficient, segment 2                                    
   C_Di_0      :        0.0054        [-]         Induced Drag Coefficient, segment 0                                     
   C_Di_1      :        0.0054        [-]         Induced Drag Coefficient, segment 1                                     
   C_Di_2      :        0.0002        [-]         Induced Drag Coefficient, segment 2                                     
   C_Dp_0      :        0.0055        [-]         Wing Profile Drag Coefficient, segment 0                                
   C_Dp_1      :        0.0055        [-]         Wing Profile Drag Coefficient, segment 1                                
   C_Dp_2      :        0.0057        [-]         Wing Profile Drag Coefficient, segment 2                                
   C_L_0       :        0.5743        [-]         Lift Coefficient, segment 0                                             
   C_L_1       :        0.5743        [-]         Lift Coefficient, segment 1                                             
   C_L_2       :        0.1189        [-]         Lift Coefficient, segment 2                                             
   I_cap_bar   :        0.0000        [-]         Area moment of inertia of cap on 2D cross section, normalized by chord^4
   M_r_bar     :    36141.5015       newton       Root Bending unit per unit chord                                        
   P_max       :  1184357.7686        watt        Maximum Engine Power                                                    
   R           :     5000.0000     kilometer      Single Segment range                                                    
   Re_0        :  4231748.4657        [-]         Reynolds Number, segment 0                                              
   Re_1        :  4050340.4368        [-]         Reynolds Number, segment 1                                              
   Re_2        :  9301869.2068        [-]         Reynolds Number, segment 2                                              
   S           :       27.7189     meter ** 2     total wing area                                                         
   T_0         :      746.1648       newton       Thrust, segment 0                                                       
   T_1         :      684.5072       newton       Thrust, segment 1                                                       
   T_2         :     2206.5587       newton       Thrust, segment 2                                                       
   V_0         :       68.2403   meter / second   Velocity, segment 0                                                     
   V_1         :       65.3149   meter / second   Velocity, segment 1                                                     
   V_2         :      150.0000   meter / second   Velocity, segment 2                                                     
   V_stall     :       38.0000   meter / second   stall speed                                                             
   W_0         :    33694.3546       newton       Weight, segment 0                                                       
   W_1         :    30868.7209       newton       Weight, segment 1                                                       
   W_2         :    33694.3546       newton       Weight, segment 2                                                       
   W_MTO       :    36773.9503       newton       Maximum Takeoff Weight                                                  
   W_cap       :     4091.0280       newton       Weight of Wing Spar Cap                                                 
   W_eng       :     2802.5264       newton       Engine Weight                                                           
   W_fuel_out  :     3079.5957       newton       Weight of fuel, outbound                                                
   W_fuel_ret  :     2825.6337       newton       Weight of fuel, return                                                  
   W_pay       :     4905.0000       newton       Payload Weight                                                          
   W_tilde     :    22407.5264       newton       Dry Weight, no wing                                                     
   W_web       :      139.5692       newton       Weight of Wing Spar Shear Web                                           
   W_wing      :     8461.1945       newton       wing weight                                                             
   W_zfw       :    30868.7209       newton       Zero Fuel Weight                                                        
   eta_0_0     :        0.2700        [-]         Overall Efficiency, segment 0                                           
   eta_0_1     :        0.2700        [-]         Overall Efficiency, segment 1                                           
   eta_0_2     :        0.2795        [-]         Overall Efficiency, segment 2                                           
   eta_i_0     :        0.9075        [-]         Inviscid Propeller Efficiency, segment 0                                
   eta_i_1     :        0.9074        [-]         Inviscid Propeller Efficiency, segment 1                                
   eta_i_2     :        0.9394        [-]         Inviscid Propeller Efficiency, segment 2                                
   eta_prop_0  :        0.7714        [-]         Propeller Efficiency, segment 0                                         
   eta_prop_1  :        0.7713        [-]         Propeller Efficiency, segment 1                                         
   eta_prop_2  :        0.7985        [-]         Propeller Efficiency, segment 2                                         
   nu          :        0.7860        [-]         Placeholder, (1+lam_w+lam_w**2)/(1+lam_w)**2                            
   p           :        1.9000        [-]         Dummy Variable (1+2*lam_w)                                              
   q           :        1.4500        [-]         Dummy Variable (1+lam_w)                                                
   t_cap_bar   :        0.0046        [-]         Spar cap thickness per unit chord                                       
   t_web_bar   :        0.0007        [-]         Spar web thickness per unit chord                                       
   tau         :        0.1500        [-]         airfoil thickness to chord ratio                                        
   z_bre_0     :        0.0875        [-]         Breguet Range Factor, segment 0                                         
   z_bre_1     :        0.0876        [-]         Breguet Range Factor, segment 1                                         

Constants
---------
   A_prop           :         0.7850           meter ** 2          Disk area of propeller                             
   CDA0             :         0.0500           meter ** 2          fuselage drag area                                 
   C_Lmax           :         1.5000              [-]              max CL with flaps down                             
   N_lift           :         6                   [-]              Ultimate Load Factor                               
   W_fixed          :     14700                  newton            fixed weight                                       
   e                :         0.9500              [-]              Oswald efficiency factor                           
   eta_eng          :         0.3500              [-]              Engine Efficiency                                  
   eta_v            :         0.8500              [-]              Propeller Viscous Efficiency                       
   f_wadd           :         2                   [-]              Added Weight Fraction                              
   g                :         9.8100      meter / second ** 2      Gravitational constant                             
   h_fuel           :  46000000             joule / kilogram       Fuel Specific energy density                       
   k_ew             :         0.0372     newton / watt ** 0.803    Constant for engine weight                         
   mu               :         0.0000   kilogram / meter / second   viscosity of air                                   
   r_h              :         0.7500              [-]              Ratio of height at rear spar to maximum wing height
   rho              :         0.9091     kilogram / meter ** 3     density of air                                     
   rho_SL           :         1.2250     kilogram / meter ** 3     density of air, sea level                          
   rho_cap          :      2700          kilogram / meter ** 3     Density of wing cap material (aluminum)            
   rho_web          :      2700          kilogram / meter ** 3     Density of wing web material (aluminum)            
   sigma_max        :       310                megapascal          Ultimate tensile stress of aluminum                
   sigma_max_shear  :       167                megapascal          Ultimate shear stress of aluminum                  
   w_bar            :         0.5000              [-]              Ratio of spar box width to chord length            

Sensitivities
-------------
   Sensitivities not currently implemented for optimization type Logspace Sequential Quadratic Program 

Solve Report
------------
   Solve Method           :  Logspace Sequential Quadratic Program 
   Classification         :  Iterative 
   Solver                 :  cvxopt 
   Number of Iterations   :  7 
   Termination Status     :  Converged, gradient of Lagrangian (9.636631e-07) within tolerance (1.000000e-06)  

Messages
--------
   1. Wolfe Condition 1 failed at iteration 5 (Step 5).  Watchdog counter is 1
   2. Wolfe Condition 1 failed at iteration 6 (Step 6).  Watchdog counter is 2


real	0m18.214s
user	0m18.685s
sys	0m0.071s
+ status=0
+ set +x

=================================================
CAPS verification (using pyCAPS) case hoburg_blackbox.py passed (as expected)
=================================================


=================================================
+ echo 'pyCAPS/sizeWing.py test;'
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESP126/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
pyCAPS/sizeWing.py test;
+ python -u pyCAPS/sizeWing.py -outLevel=0
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESP126/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
nrock 2

Objective
---------
   0.075 dimensionless

Variables
---------
   AR     :  10.000        [-]         Wing aspect ratio
   CD     :   0.075        [-]         Drag Coefficient 
   CL     :   0.999        [-]         Lift Coefficient 
   S      :   2.642     meter ** 2     Wing area        
   V      :   2.722   meter / second   Airspeed         
   W      :  11.979       newton       Aircraft weight  
   Wwing  :   1.598       newton       Wing weight      

Constants
---------
   ARmax     :  10                [-]            Max AR                                         
   CD0       :   0.040            [-]            Profile drag                                   
   CLmax     :   1                [-]            Max CL                                         
   E0        :  10               joule           Maximum elastic potential energy in rubber band
   Wfixed    :   0.100           newton          Weight of fixed components                     
   Wrock     :   2               newton          Weight of each rock                            
   e         :   0.900            [-]            Oswawld efficiency factor                      
   g         :   9.810    meter / second ** 2    Gravitational constant                         
   nrock     :   2                [-]            Number of rocks to carry                       
   rho       :   1.225   kilogram / meter ** 3   Density of air                                 
   rho_wing  :   1       kilogram / meter ** 3   Weight density of wing                         
   tau       :   0.120            [-]            Airfoil thickness as t/c                       

Sensitivities
-------------
   Sensitivities not computed

Solve Report
------------
   Solve Method           :  Geometric Program 
   Classification         :  Convex 
   Solver                 :  cvxopt 

Optimized L/D: 13.267784561972137
 EGADS Info: 0 Objects, 0 Reference in Use (of 0) at Close!

real	0m0.828s
user	0m1.333s
sys	0m0.071s
+ status=0
+ set +x

=================================================
CAPS verification (using pyCAPS) case pyCAPS/sizeWing.py passed (as expected)
=================================================

avl: /Users/jenkins/workspace/ESP_bPreBuilt/ESP126/EngSketchPad/bin/avl

=================================================
+ echo 'pyCAPS/optTaperAvl.py test;'
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESP126/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
pyCAPS/optTaperAvl.py test;
+ python -u pyCAPS/optTaperAvl.py -outLevel=0
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESP126/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = wing, index = 1
Getting vortex lattice surface data
	VLM surface name - wing
	No "groupName" variable provided or no matches found, going to use tuple name
	Done getting vortex lattice surface data
Writing surface - wing (ID = 0)
	Section 1 of 3 (ID = 0)
	Section 2 of 3 (ID = 1)
	Section 3 of 3 (ID = 2)
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = wing, index = 1
Getting vortex lattice surface data
	VLM surface name - wing
	No "groupName" variable provided or no matches found, going to use tuple name
	Done getting vortex lattice surface data
Writing surface - wing (ID = 0)
	Section 1 of 3 (ID = 0)
	Section 2 of 3 (ID = 1)
	Section 3 of 3 (ID = 2)
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = wing, index = 1
Getting vortex lattice surface data
	VLM surface name - wing
	No "groupName" variable provided or no matches found, going to use tuple name
	Done getting vortex lattice surface data
Writing surface - wing (ID = 0)
	Section 1 of 3 (ID = 0)
	Section 2 of 3 (ID = 1)
	Section 3 of 3 (ID = 2)
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = wing, index = 1
Getting vortex lattice surface data
	VLM surface name - wing
	No "groupName" variable provided or no matches found, going to use tuple name
	Done getting vortex lattice surface data
Writing surface - wing (ID = 0)
	Section 1 of 3 (ID = 0)
	Section 2 of 3 (ID = 1)
	Section 3 of 3 (ID = 2)
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = wing, index = 1
Getting vortex lattice surface data
	VLM surface name - wing
	No "groupName" variable provided or no matches found, going to use tuple name
	Done getting vortex lattice surface data
Writing surface - wing (ID = 0)
	Section 1 of 3 (ID = 0)
	Section 2 of 3 (ID = 1)
	Section 3 of 3 (ID = 2)
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = wing, index = 1
Getting vortex lattice surface data
	VLM surface name - wing
	No "groupName" variable provided or no matches found, going to use tuple name
	Done getting vortex lattice surface data
Writing surface - wing (ID = 0)
	Section 1 of 3 (ID = 0)
	Section 2 of 3 (ID = 1)
	Section 3 of 3 (ID = 2)
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = wing, index = 1
Getting vortex lattice surface data
	VLM surface name - wing
	No "groupName" variable provided or no matches found, going to use tuple name
	Done getting vortex lattice surface data
Writing surface - wing (ID = 0)
	Section 1 of 3 (ID = 0)
	Section 2 of 3 (ID = 1)
	Section 3 of 3 (ID = 2)
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = wing, index = 1
Getting vortex lattice surface data
	VLM surface name - wing
	No "groupName" variable provided or no matches found, going to use tuple name
	Done getting vortex lattice surface data
Writing surface - wing (ID = 0)
	Section 1 of 3 (ID = 0)
	Section 2 of 3 (ID = 1)
	Section 3 of 3 (ID = 2)
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = wing, index = 1
Getting vortex lattice surface data
	VLM surface name - wing
	No "groupName" variable provided or no matches found, going to use tuple name
	Done getting vortex lattice surface data
Writing surface - wing (ID = 0)
	Section 1 of 3 (ID = 0)
	Section 2 of 3 (ID = 1)
	Section 3 of 3 (ID = 2)
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = wing, index = 1
Getting vortex lattice surface data
	VLM surface name - wing
	No "groupName" variable provided or no matches found, going to use tuple name
	Done getting vortex lattice surface data
Writing surface - wing (ID = 0)
	Section 1 of 3 (ID = 0)
	Section 2 of 3 (ID = 1)
	Section 3 of 3 (ID = 2)
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = wing, index = 1
Getting vortex lattice surface data
	VLM surface name - wing
	No "groupName" variable provided or no matches found, going to use tuple name
	Done getting vortex lattice surface data
Writing surface - wing (ID = 0)
	Section 1 of 3 (ID = 0)
	Section 2 of 3 (ID = 1)
	Section 3 of 3 (ID = 2)
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = wing, index = 1
Getting vortex lattice surface data
	VLM surface name - wing
	No "groupName" variable provided or no matches found, going to use tuple name
	Done getting vortex lattice surface data
Writing surface - wing (ID = 0)
	Section 1 of 3 (ID = 0)
	Section 2 of 3 (ID = 1)
	Section 3 of 3 (ID = 2)
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = wing, index = 1
Getting vortex lattice surface data
	VLM surface name - wing
	No "groupName" variable provided or no matches found, going to use tuple name
	Done getting vortex lattice surface data
Writing surface - wing (ID = 0)
	Section 1 of 3 (ID = 0)
	Section 2 of 3 (ID = 1)
	Section 3 of 3 (ID = 2)
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = wing, index = 1
Getting vortex lattice surface data
	VLM surface name - wing
	No "groupName" variable provided or no matches found, going to use tuple name
	Done getting vortex lattice surface data
Writing surface - wing (ID = 0)
	Section 1 of 3 (ID = 0)
	Section 2 of 3 (ID = 1)
	Section 3 of 3 (ID = 2)
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = wing, index = 1
Getting vortex lattice surface data
	VLM surface name - wing
	No "groupName" variable provided or no matches found, going to use tuple name
	Done getting vortex lattice surface data
Writing surface - wing (ID = 0)
	Section 1 of 3 (ID = 0)
	Section 2 of 3 (ID = 1)
	Section 3 of 3 (ID = 2)
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = wing, index = 1
Getting vortex lattice surface data
	VLM surface name - wing
	No "groupName" variable provided or no matches found, going to use tuple name
	Done getting vortex lattice surface data
Writing surface - wing (ID = 0)
	Section 1 of 3 (ID = 0)
	Section 2 of 3 (ID = 1)
	Section 3 of 3 (ID = 2)
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = wing, index = 1
Getting vortex lattice surface data
	VLM surface name - wing
	No "groupName" variable provided or no matches found, going to use tuple name
	Done getting vortex lattice surface data
Writing surface - wing (ID = 0)
	Section 1 of 3 (ID = 0)
	Section 2 of 3 (ID = 1)
	Section 3 of 3 (ID = 2)
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = wing, index = 1
Getting vortex lattice surface data
	VLM surface name - wing
	No "groupName" variable provided or no matches found, going to use tuple name
	Done getting vortex lattice surface data
Writing surface - wing (ID = 0)
	Section 1 of 3 (ID = 0)
	Section 2 of 3 (ID = 1)
	Section 3 of 3 (ID = 2)
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = wing, index = 1
Getting vortex lattice surface data
	VLM surface name - wing
	No "groupName" variable provided or no matches found, going to use tuple name
	Done getting vortex lattice surface data
Writing surface - wing (ID = 0)
	Section 1 of 3 (ID = 0)
	Section 2 of 3 (ID = 1)
	Section 3 of 3 (ID = 2)
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = wing, index = 1
Getting vortex lattice surface data
	VLM surface name - wing
	No "groupName" variable provided or no matches found, going to use tuple name
	Done getting vortex lattice surface data
Writing surface - wing (ID = 0)
	Section 1 of 3 (ID = 0)
	Section 2 of 3 (ID = 1)
	Section 3 of 3 (ID = 2)
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = wing, index = 1
Getting vortex lattice surface data
	VLM surface name - wing
	No "groupName" variable provided or no matches found, going to use tuple name
	Done getting vortex lattice surface data
Writing surface - wing (ID = 0)
	Section 1 of 3 (ID = 0)
	Section 2 of 3 (ID = 1)
	Section 3 of 3 (ID = 2)

Objective
---------
   1.00805 dimensionless

Variables
---------
   e    :  0.99202   [-]   Oswald efficiency factor
   lam  :  0.39881   [-]   Wing taper ratio        

Sensitivities
-------------
   Sensitivities not available for optimizations of type Sequential Log Convex Program 

Solve Report
------------
   Solve Method           :  Sequential Log Convex Program 
   Classification         :  Iterative 
   Solver                 :  cvxopt 
   Number of Iterations   :  6 
   Termination Status     :  Converged, gradient of Lagrangian (5.888774e-08) within tolerance (1.000000e-06)  

Messages
--------
   1. Wolfe Condition 1 failed at iteration 5 (Step 5).  Watchdog counter is 1


real	0m3.141s
user	0m2.579s
sys	0m1.072s
+ status=0
+ set +x

=================================================
CAPS verification (using pyCAPS) case pyCAPS/optTaperAvl.py passed (as expected)
=================================================


=================================================
+ echo 'pyCAPS/optWingAvl.py test;'
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESP126/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
pyCAPS/optWingAvl.py test;
+ python -u pyCAPS/optWingAvl.py -outLevel=0
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESP126/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
nrock 2
Starting iteration 0 at 0.1442 seconds
AR : 9.0 dimensionless
CD : 0.1 dimensionless
CL : 1.0 dimensionless
S : 1.0 meter ** 2
V : 1.0 meter / second
W : 10.0 newton
Wwing : 0.1 newton
e : 1.0 dimensionless
lam : 0.3 dimensionless
AVL run case - lam, AR: 0.3 9.0
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = wing, index = 1
Getting vortex lattice surface data
	VLM surface name - wing
	No "groupName" variable provided or no matches found, going to use tuple name
	Done getting vortex lattice surface data
Writing surface - wing (ID = 0)
	Section 1 of 3 (ID = 0)
	Section 2 of 3 (ID = 1)
	Section 3 of 3 (ID = 2)
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = wing, index = 1
Getting vortex lattice surface data
	VLM surface name - wing
	No "groupName" variable provided or no matches found, going to use tuple name
	Done getting vortex lattice surface data
Writing surface - wing (ID = 0)
	Section 1 of 3 (ID = 0)
	Section 2 of 3 (ID = 1)
	Section 3 of 3 (ID = 2)
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = wing, index = 1
Getting vortex lattice surface data
	VLM surface name - wing
	No "groupName" variable provided or no matches found, going to use tuple name
	Done getting vortex lattice surface data
Writing surface - wing (ID = 0)
	Section 1 of 3 (ID = 0)
	Section 2 of 3 (ID = 1)
	Section 3 of 3 (ID = 2)
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = wing, index = 1
Getting vortex lattice surface data
	VLM surface name - wing
	No "groupName" variable provided or no matches found, going to use tuple name
	Done getting vortex lattice surface data
Writing surface - wing (ID = 0)
	Section 1 of 3 (ID = 0)
	Section 2 of 3 (ID = 1)
	Section 3 of 3 (ID = 2)
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = wing, index = 1
Getting vortex lattice surface data
	VLM surface name - wing
	No "groupName" variable provided or no matches found, going to use tuple name
	Done getting vortex lattice surface data
Writing surface - wing (ID = 0)
	Section 1 of 3 (ID = 0)
	Section 2 of 3 (ID = 1)
	Section 3 of 3 (ID = 2)
y: 0.990550414371373 dimensionless
dydx: [&lt;Quantity(0.060834734963571835, 'dimensionless')&gt;, &lt;Quantity(-0.0014769756679916535, 'dimensionless')&gt;]
Calling cvxopt.solvers.cp at 0.7067 seconds
Got sol from cvxopt at 0.7155 seconds
status optimal
x [ 1.05e-01]
[-3.26e-01]
[-1.49e-11]
[-4.10e-01]
[ 1.28e+00]
[-6.40e-01]
[ 7.00e-01]
[-1.08e-02]
[ 5.73e-03]
[-3.20e-16]
[ 3.50e-16]
[ 1.56e-16]
[ 5.20e-16]
[ 2.70e-16]
[ 4.16e-27]
[ 3.37e-16]
[ 2.07e-23]

y [-6.40e-01]
[ 7.00e-01]
[ 3.11e-01]

znl [ 6.74e-01]
[ 4.14e-08]

zl [ 1.04e+00]
[ 5.41e-01]
[ 8.31e-12]

snl [ 8.55e-11]
[ 2.03e-01]

sl [ 1.49e-11]
[ 4.30e-10]
[ 8.74e-01]

gap 8.743959706200045e-09
relative gap 7.1941976174589016e-09
primal objective -1.2154183372694929
dual objective -1.2154183416834794
primal slack 1.3843122277340912e-11
dual slack 8.310943825855639e-12
primal infeasibility 1.13903462789848e-09
dual infeasibility 2.3823418495103618e-11
AVL run case - lam, AR: 0.3017253411787602 9.999999995701312
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = wing, index = 1
Getting vortex lattice surface data
	VLM surface name - wing
	No "groupName" variable provided or no matches found, going to use tuple name
	Done getting vortex lattice surface data
Writing surface - wing (ID = 0)
	Section 1 of 3 (ID = 0)
	Section 2 of 3 (ID = 1)
	Section 3 of 3 (ID = 2)
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = wing, index = 1
Getting vortex lattice surface data
	VLM surface name - wing
	No "groupName" variable provided or no matches found, going to use tuple name
	Done getting vortex lattice surface data
Writing surface - wing (ID = 0)
	Section 1 of 3 (ID = 0)
	Section 2 of 3 (ID = 1)
	Section 3 of 3 (ID = 2)
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = wing, index = 1
Getting vortex lattice surface data
	VLM surface name - wing
	No "groupName" variable provided or no matches found, going to use tuple name
	Done getting vortex lattice surface data
Writing surface - wing (ID = 0)
	Section 1 of 3 (ID = 0)
	Section 2 of 3 (ID = 1)
	Section 3 of 3 (ID = 2)
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = wing, index = 1
Getting vortex lattice surface data
	VLM surface name - wing
	No "groupName" variable provided or no matches found, going to use tuple name
	Done getting vortex lattice surface data
Writing surface - wing (ID = 0)
	Section 1 of 3 (ID = 0)
	Section 2 of 3 (ID = 1)
	Section 3 of 3 (ID = 2)
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = wing, index = 1
Getting vortex lattice surface data
	VLM surface name - wing
	No "groupName" variable provided or no matches found, going to use tuple name
	Done getting vortex lattice surface data
Writing surface - wing (ID = 0)
	Section 1 of 3 (ID = 0)
	Section 2 of 3 (ID = 1)
	Section 3 of 3 (ID = 2)
y: 0.9892210301573232 dimensionless
dydx: [&lt;Quantity(0.06359341837018917, 'dimensionless')&gt;, &lt;Quantity(-0.0014812479862164052, 'dimensionless')&gt;]
logspace stuff at 1.2899 seconds
Starting iteration 1 at 1.3042 seconds
AR : 9.999999995701312 dimensionless
CD : 0.07217671497330859 dimensionless
CL : 0.9999999999851361 dimensionless
S : 0.6639217992634345 meter ** 2
V : 3.600068783658014 meter / second
W : 5.270412635736404 newton
Wwing : 0.20138431695627712 newton
e : 0.9892553874046033 dimensionless
lam : 0.3017253411787602 dimensionless
Calling cvxopt.solvers.cp at 1.3079 seconds
Got sol from cvxopt at 1.3154 seconds
status optimal
x [ 3.90e-10]
[-5.94e-05]
[-1.96e-07]
[ 1.14e-08]
[ 7.38e-08]
[-3.68e-08]
[ 1.70e-08]
[ 1.33e-04]
[ 8.64e-03]
[ 6.35e-21]
[-6.95e-21]
[ 2.23e-16]
[ 5.42e-17]
[ 2.20e-16]
[ 1.27e-26]
[ 5.00e-16]
[ 6.63e-26]

y [ 1.27e-05]
[-1.39e-05]
[ 4.46e-01]

znl [ 1.00e+00]
[ 1.33e-10]

zl [ 1.08e-01]
[ 4.39e-01]
[ 2.53e-11]

snl [ 2.06e-11]
[ 2.03e-01]

sl [ 1.96e-07]
[ 4.02e-11]
[ 8.74e-01]

gap 2.1363031593454878e-08
relative gap 8.126967446080017e-09
primal objective -2.628659673511942
dual objective -2.628659684337833
primal slack 2.0577846480825846e-11
dual slack 2.53050406780468e-11
primal infeasibility 3.085803284597273e-09
dual infeasibility 3.13391320011975e-09
AVL run case - lam, AR: 0.30434464835769004 9.99999999959832
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = wing, index = 1
Getting vortex lattice surface data
	VLM surface name - wing
	No "groupName" variable provided or no matches found, going to use tuple name
	Done getting vortex lattice surface data
Writing surface - wing (ID = 0)
	Section 1 of 3 (ID = 0)
	Section 2 of 3 (ID = 1)
	Section 3 of 3 (ID = 2)
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = wing, index = 1
Getting vortex lattice surface data
	VLM surface name - wing
	No "groupName" variable provided or no matches found, going to use tuple name
	Done getting vortex lattice surface data
Writing surface - wing (ID = 0)
	Section 1 of 3 (ID = 0)
	Section 2 of 3 (ID = 1)
	Section 3 of 3 (ID = 2)
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = wing, index = 1
Getting vortex lattice surface data
	VLM surface name - wing
	No "groupName" variable provided or no matches found, going to use tuple name
	Done getting vortex lattice surface data
Writing surface - wing (ID = 0)
	Section 1 of 3 (ID = 0)
	Section 2 of 3 (ID = 1)
	Section 3 of 3 (ID = 2)
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = wing, index = 1
Getting vortex lattice surface data
	VLM surface name - wing
	No "groupName" variable provided or no matches found, going to use tuple name
	Done getting vortex lattice surface data
Writing surface - wing (ID = 0)
	Section 1 of 3 (ID = 0)
	Section 2 of 3 (ID = 1)
	Section 3 of 3 (ID = 2)
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = wing, index = 1
Getting vortex lattice surface data
	VLM surface name - wing
	No "groupName" variable provided or no matches found, going to use tuple name
	Done getting vortex lattice surface data
Writing surface - wing (ID = 0)
	Section 1 of 3 (ID = 0)
	Section 2 of 3 (ID = 1)
	Section 3 of 3 (ID = 2)
y: 0.9893844569300133 dimensionless
dydx: [&lt;Quantity(0.061358790088644755, 'dimensionless')&gt;, &lt;Quantity(-0.001469791715157931, 'dimensionless')&gt;]
logspace stuff at 1.8736 seconds
Starting iteration 2 at 1.8905 seconds
AR : 9.99999999959832 dimensionless
CD : 0.07217242517886707 dimensionless
CL : 0.9999998041107226 dimensionless
S : 0.6639218068635588 meter ** 2
V : 3.6000690493939635 meter / second
W : 5.270412441791246 newton
Wwing : 0.20138432037500312 newton
e : 0.9893868959019062 dimensionless
lam : 0.30434464835769004 dimensionless
Calling cvxopt.solvers.cp at 1.8943 seconds
Got sol from cvxopt at 1.9010 seconds
status optimal
x [ 7.75e-13]
[-3.52e-04]
[ 4.29e-09]
[-2.11e-10]
[-1.42e-09]
[ 1.25e-09]
[-3.17e-10]
[ 7.91e-04]
[ 4.20e-02]
[ 7.26e-21]
[-7.89e-21]
[ 2.23e-16]
[ 5.45e-17]
[ 2.20e-16]
[ 1.24e-26]
[ 5.00e-16]
[ 6.65e-26]

y [ 1.45e-05]
[-1.58e-05]
[ 4.45e-01]

znl [ 1.00e+00]
[ 1.33e-10]

zl [ 1.09e-01]
[ 4.39e-01]
[ 2.49e-11]

snl [ 2.02e-11]
[ 2.03e-01]

sl [ 1.92e-07]
[ 3.94e-11]
[ 8.74e-01]

gap 2.097954193386208e-08
relative gap 7.980432613224019e-09
primal objective -2.628872763000068
dual objective -2.628872773631917
primal slack 2.0226195523752228e-11
dual slack 2.4870270238975127e-11
primal infeasibility 3.030673275151341e-09
dual infeasibility 3.0769326689078285e-09
AVL run case - lam, AR: 0.3174093513141515 9.999999999606068
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = wing, index = 1
Getting vortex lattice surface data
	VLM surface name - wing
	No "groupName" variable provided or no matches found, going to use tuple name
	Done getting vortex lattice surface data
Writing surface - wing (ID = 0)
	Section 1 of 3 (ID = 0)
	Section 2 of 3 (ID = 1)
	Section 3 of 3 (ID = 2)
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = wing, index = 1
Getting vortex lattice surface data
	VLM surface name - wing
	No "groupName" variable provided or no matches found, going to use tuple name
	Done getting vortex lattice surface data
Writing surface - wing (ID = 0)
	Section 1 of 3 (ID = 0)
	Section 2 of 3 (ID = 1)
	Section 3 of 3 (ID = 2)
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = wing, index = 1
Getting vortex lattice surface data
	VLM surface name - wing
	No "groupName" variable provided or no matches found, going to use tuple name
	Done getting vortex lattice surface data
Writing surface - wing (ID = 0)
	Section 1 of 3 (ID = 0)
	Section 2 of 3 (ID = 1)
	Section 3 of 3 (ID = 2)
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = wing, index = 1
Getting vortex lattice surface data
	VLM surface name - wing
	No "groupName" variable provided or no matches found, going to use tuple name
	Done getting vortex lattice surface data
Writing surface - wing (ID = 0)
	Section 1 of 3 (ID = 0)
	Section 2 of 3 (ID = 1)
	Section 3 of 3 (ID = 2)
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = wing, index = 1
Getting vortex lattice surface data
	VLM surface name - wing
	No "groupName" variable provided or no matches found, going to use tuple name
	Done getting vortex lattice surface data
Writing surface - wing (ID = 0)
	Section 1 of 3 (ID = 0)
	Section 2 of 3 (ID = 1)
	Section 3 of 3 (ID = 2)
y: 0.9901147289476044 dimensionless
dydx: [&lt;Quantity(0.05073085616785211, 'dimensionless')&gt;, &lt;Quantity(-0.001419190987608232, 'dimensionless')&gt;]
logspace stuff at 2.4699 seconds
Starting iteration 3 at 2.4869 seconds
AR : 9.999999999606068 dimensionless
CD : 0.07214699157334123 dimensionless
CL : 0.9999998084033913 dimensionless
S : 0.6639218067235316 meter ** 2
V : 3.6000690442960233 meter / second
W : 5.270412448377285 newton
Wwing : 0.20138432031121437 newton
e : 0.9901696737885595 dimensionless
lam : 0.3174093513141515 dimensionless
Calling cvxopt.solvers.cp at 2.4907 seconds
Got sol from cvxopt at 2.4975 seconds
status optimal
x [ 2.14e-12]
[-1.28e-03]
[ 1.17e-08]
[-5.10e-10]
[-3.51e-09]
[ 4.16e-09]
[-7.67e-10]
[ 2.88e-03]
[ 1.81e-01]
[-4.10e-21]
[ 4.49e-21]
[ 2.23e-16]
[ 5.51e-17]
[ 2.20e-16]
[ 1.18e-26]
[ 5.00e-16]
[ 6.61e-26]

y [-8.19e-06]
[ 8.98e-06]
[ 4.45e-01]

znl [ 1.00e+00]
[ 1.32e-10]

zl [ 1.10e-01]
[ 4.40e-01]
[ 2.37e-11]

snl [ 1.92e-11]
[ 2.03e-01]

sl [ 1.80e-07]
[ 3.73e-11]
[ 8.74e-01]

gap 1.9913348949433526e-08
relative gap 7.57253767423933e-09
primal objective -2.629679746219796
dual objective -2.629679756312171
primal slack 1.9233234440857094e-11
dual slack 2.3654666051747643e-11
primal infeasibility 2.8765759057609882e-09
dual infeasibility 2.9202707353765115e-09
AVL run case - lam, AR: 0.38029905717662316 9.999999999627487
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = wing, index = 1
Getting vortex lattice surface data
	VLM surface name - wing
	No "groupName" variable provided or no matches found, going to use tuple name
	Done getting vortex lattice surface data
Writing surface - wing (ID = 0)
	Section 1 of 3 (ID = 0)
	Section 2 of 3 (ID = 1)
	Section 3 of 3 (ID = 2)
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = wing, index = 1
Getting vortex lattice surface data
	VLM surface name - wing
	No "groupName" variable provided or no matches found, going to use tuple name
	Done getting vortex lattice surface data
Writing surface - wing (ID = 0)
	Section 1 of 3 (ID = 0)
	Section 2 of 3 (ID = 1)
	Section 3 of 3 (ID = 2)
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = wing, index = 1
Getting vortex lattice surface data
	VLM surface name - wing
	No "groupName" variable provided or no matches found, going to use tuple name
	Done getting vortex lattice surface data
Writing surface - wing (ID = 0)
	Section 1 of 3 (ID = 0)
	Section 2 of 3 (ID = 1)
	Section 3 of 3 (ID = 2)
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = wing, index = 1
Getting vortex lattice surface data
	VLM surface name - wing
	No "groupName" variable provided or no matches found, going to use tuple name
	Done getting vortex lattice surface data
Writing surface - wing (ID = 0)
	Section 1 of 3 (ID = 0)
	Section 2 of 3 (ID = 1)
	Section 3 of 3 (ID = 2)
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = wing, index = 1
Getting vortex lattice surface data
	VLM surface name - wing
	No "groupName" variable provided or no matches found, going to use tuple name
	Done getting vortex lattice surface data
Writing surface - wing (ID = 0)
	Section 1 of 3 (ID = 0)
	Section 2 of 3 (ID = 1)
	Section 3 of 3 (ID = 2)
y: 0.9919295458295864 dimensionless
dydx: [&lt;Quantity(0.009583432732646058, 'dimensionless')&gt;, &lt;Quantity(-0.0013533445524760435, 'dimensionless')&gt;]
logspace stuff at 3.0512 seconds
Starting iteration 4 at 3.0682 seconds
AR : 9.999999999627487 dimensionless
CD : 0.0720544031114864 dimensionless
CL : 0.9999998201037487 dimensionless
S : 0.6639218063847038 meter ** 2
V : 3.600069031643119 meter / second
W : 5.270412470306208 newton
Wwing : 0.20138432015683602 newton
e : 0.993029781490428 dimensionless
lam : 0.38029905717662316 dimensionless
Calling cvxopt.solvers.cp at 3.0719 seconds
Got sol from cvxopt at 3.0785 seconds
status optimal
x [-1.57e-12]
[ 4.08e-04]
[-8.59e-09]
[ 5.53e-10]
[ 3.53e-09]
[-9.72e-10]
[ 8.30e-10]
[-9.18e-04]
[ 5.19e-02]
[-2.12e-20]
[ 2.32e-20]
[ 2.24e-16]
[ 5.46e-17]
[ 2.20e-16]
[ 1.23e-26]
[ 5.00e-16]
[ 6.59e-26]

y [-4.25e-05]
[ 4.64e-05]
[ 4.47e-01]

znl [ 1.00e+00]
[ 1.32e-10]

zl [ 1.09e-01]
[ 4.39e-01]
[ 2.45e-11]

snl [ 1.99e-11]
[ 2.03e-01]

sl [ 1.88e-07]
[ 3.88e-11]
[ 8.74e-01]

gap 2.0688403479344937e-08
relative gap 7.866667127626345e-09
primal objective -2.629881644119772
dual objective -2.629881654604473
primal slack 1.9944303018503003e-11
dual slack 2.4539201182220112e-11
primal infeasibility 2.9853825022328838e-09
dual infeasibility 3.036428971722002e-09
AVL run case - lam, AR: 0.4005573159778744 9.999999999611775
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = wing, index = 1
Getting vortex lattice surface data
	VLM surface name - wing
	No "groupName" variable provided or no matches found, going to use tuple name
	Done getting vortex lattice surface data
Writing surface - wing (ID = 0)
	Section 1 of 3 (ID = 0)
	Section 2 of 3 (ID = 1)
	Section 3 of 3 (ID = 2)
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = wing, index = 1
Getting vortex lattice surface data
	VLM surface name - wing
	No "groupName" variable provided or no matches found, going to use tuple name
	Done getting vortex lattice surface data
Writing surface - wing (ID = 0)
	Section 1 of 3 (ID = 0)
	Section 2 of 3 (ID = 1)
	Section 3 of 3 (ID = 2)
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = wing, index = 1
Getting vortex lattice surface data
	VLM surface name - wing
	No "groupName" variable provided or no matches found, going to use tuple name
	Done getting vortex lattice surface data
Writing surface - wing (ID = 0)
	Section 1 of 3 (ID = 0)
	Section 2 of 3 (ID = 1)
	Section 3 of 3 (ID = 2)
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = wing, index = 1
Getting vortex lattice surface data
	VLM surface name - wing
	No "groupName" variable provided or no matches found, going to use tuple name
	Done getting vortex lattice surface data
Writing surface - wing (ID = 0)
	Section 1 of 3 (ID = 0)
	Section 2 of 3 (ID = 1)
	Section 3 of 3 (ID = 2)
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = wing, index = 1
Getting vortex lattice surface data
	VLM surface name - wing
	No "groupName" variable provided or no matches found, going to use tuple name
	Done getting vortex lattice surface data
Writing surface - wing (ID = 0)
	Section 1 of 3 (ID = 0)
	Section 2 of 3 (ID = 1)
	Section 3 of 3 (ID = 2)
y: 0.9920150584836487 dimensionless
dydx: [&lt;Quantity(-0.0008541793310445911, 'dimensionless')&gt;, &lt;Quantity(-0.0013850816280491784, 'dimensionless')&gt;]
logspace stuff at 3.6459 seconds
Starting iteration 5 at 3.6630 seconds
AR : 9.999999999611775 dimensionless
CD : 0.07208383829260301 dimensionless
CL : 0.9999998115160276 dimensionless
S : 0.6639218067517705 meter ** 2
V : 3.600069044356998 meter / second
W : 5.270412465184867 newton
Wwing : 0.20138432032400524 newton
e : 0.9921187131764504 dimensionless
lam : 0.4005573159778744 dimensionless
Calling cvxopt.solvers.cp at 3.6667 seconds
Got sol from cvxopt at 3.6734 seconds
status optimal
x [ 8.00e-13]
[ 4.58e-05]
[ 4.24e-09]
[-2.43e-10]
[-1.58e-09]
[ 8.36e-10]
[-3.65e-10]
[-1.03e-04]
[-4.33e-03]
[-2.09e-21]
[ 2.29e-21]
[ 2.23e-16]
[ 5.49e-17]
[ 2.19e-16]
[ 1.20e-26]
[ 5.00e-16]
[ 6.74e-26]

y [-4.18e-06]
[ 4.57e-06]
[ 4.45e-01]

znl [ 1.00e+00]
[ 1.35e-10]

zl [ 1.10e-01]
[ 4.39e-01]
[ 2.41e-11]

snl [ 1.96e-11]
[ 2.03e-01]

sl [ 1.84e-07]
[ 3.80e-11]
[ 8.74e-01]

gap 2.031955843004712e-08
relative gap 7.726423169498243e-09
primal objective -2.6298790506664265
dual objective -2.629879060964246
primal slack 1.961702717405949e-11
dual slack 2.4096853737212874e-11
primal infeasibility 2.93236429442893e-09
dual infeasibility 2.967263152169171e-09
AVL run case - lam, AR: 0.39882645454912435 9.999999999619773
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = wing, index = 1
Getting vortex lattice surface data
	VLM surface name - wing
	No "groupName" variable provided or no matches found, going to use tuple name
	Done getting vortex lattice surface data
Writing surface - wing (ID = 0)
	Section 1 of 3 (ID = 0)
	Section 2 of 3 (ID = 1)
	Section 3 of 3 (ID = 2)
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = wing, index = 1
Getting vortex lattice surface data
	VLM surface name - wing
	No "groupName" variable provided or no matches found, going to use tuple name
	Done getting vortex lattice surface data
Writing surface - wing (ID = 0)
	Section 1 of 3 (ID = 0)
	Section 2 of 3 (ID = 1)
	Section 3 of 3 (ID = 2)
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = wing, index = 1
Getting vortex lattice surface data
	VLM surface name - wing
	No "groupName" variable provided or no matches found, going to use tuple name
	Done getting vortex lattice surface data
Writing surface - wing (ID = 0)
	Section 1 of 3 (ID = 0)
	Section 2 of 3 (ID = 1)
	Section 3 of 3 (ID = 2)
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = wing, index = 1
Getting vortex lattice surface data
	VLM surface name - wing
	No "groupName" variable provided or no matches found, going to use tuple name
	Done getting vortex lattice surface data
Writing surface - wing (ID = 0)
	Section 1 of 3 (ID = 0)
	Section 2 of 3 (ID = 1)
	Section 3 of 3 (ID = 2)
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = wing, index = 1
Getting vortex lattice surface data
	VLM surface name - wing
	No "groupName" variable provided or no matches found, going to use tuple name
	Done getting vortex lattice surface data
Writing surface - wing (ID = 0)
	Section 1 of 3 (ID = 0)
	Section 2 of 3 (ID = 1)
	Section 3 of 3 (ID = 2)
y: 0.9920158805953975 dimensionless
dydx: [&lt;Quantity(-6.436454802472014e-06, 'dimensionless')&gt;, &lt;Quantity(-0.0013814190268079951, 'dimensionless')&gt;]
logspace stuff at 4.2619 seconds
Starting iteration 6 at 4.2789 seconds
AR : 9.999999999619773 dimensionless
CD : 0.07208714305299402 dimensionless
CL : 0.9999998157581855 dimensionless
S : 0.6639218065905538 meter ** 2
V : 3.6000690386621352 meter / second
W : 5.270412469588729 newton
Wwing : 0.20138432025057307 newton
e : 0.9920165401543579 dimensionless
lam : 0.39882645454912435 dimensionless
Calling cvxopt.solvers.cp at 4.2826 seconds
Got sol from cvxopt at 4.2894 seconds
status optimal
x [ 2.35e-13]
[ 2.97e-07]
[ 1.09e-09]
[-5.55e-11]
[-3.69e-10]
[ 2.96e-10]
[-8.34e-11]
[-6.65e-07]
[-3.26e-05]
[ 1.22e-24]
[-1.28e-24]
[ 2.23e-16]
[ 5.49e-17]
[ 2.19e-16]
[ 1.20e-26]
[ 5.00e-16]
[ 6.76e-26]

y [ 2.45e-09]
[-2.57e-09]
[ 4.45e-01]

znl [ 1.00e+00]
[ 1.35e-10]

zl [ 1.10e-01]
[ 4.39e-01]
[ 2.40e-11]

snl [ 1.95e-11]
[ 2.03e-01]

sl [ 1.83e-07]
[ 3.78e-11]
[ 8.74e-01]

gap 2.0211071384287106e-08
relative gap 7.685171306970461e-09
primal objective -2.6298790979396434
dual objective -2.629879108182298
primal slack 1.9527381359129242e-11
dual slack 2.395834706018389e-11
primal infeasibility 2.9156313147459703e-09
dual infeasibility 2.9337884446774703e-09
AVL run case - lam, AR: 0.39881343719465984 9.999999999622123
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = wing, index = 1
Getting vortex lattice surface data
	VLM surface name - wing
	No "groupName" variable provided or no matches found, going to use tuple name
	Done getting vortex lattice surface data
Writing surface - wing (ID = 0)
	Section 1 of 3 (ID = 0)
	Section 2 of 3 (ID = 1)
	Section 3 of 3 (ID = 2)
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = wing, index = 1
Getting vortex lattice surface data
	VLM surface name - wing
	No "groupName" variable provided or no matches found, going to use tuple name
	Done getting vortex lattice surface data
Writing surface - wing (ID = 0)
	Section 1 of 3 (ID = 0)
	Section 2 of 3 (ID = 1)
	Section 3 of 3 (ID = 2)
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = wing, index = 1
Getting vortex lattice surface data
	VLM surface name - wing
	No "groupName" variable provided or no matches found, going to use tuple name
	Done getting vortex lattice surface data
Writing surface - wing (ID = 0)
	Section 1 of 3 (ID = 0)
	Section 2 of 3 (ID = 1)
	Section 3 of 3 (ID = 2)
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = wing, index = 1
Getting vortex lattice surface data
	VLM surface name - wing
	No "groupName" variable provided or no matches found, going to use tuple name
	Done getting vortex lattice surface data
Writing surface - wing (ID = 0)
	Section 1 of 3 (ID = 0)
	Section 2 of 3 (ID = 1)
	Section 3 of 3 (ID = 2)
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = wing, index = 1
Getting vortex lattice surface data
	VLM surface name - wing
	No "groupName" variable provided or no matches found, going to use tuple name
	Done getting vortex lattice surface data
Writing surface - wing (ID = 0)
	Section 1 of 3 (ID = 0)
	Section 2 of 3 (ID = 1)
	Section 3 of 3 (ID = 2)
y: 0.9920158812322912 dimensionless
dydx: [&lt;Quantity(-5.709581030188815e-07, 'dimensionless')&gt;, &lt;Quantity(-0.0013813957758107565, 'dimensionless')&gt;]
logspace stuff at 4.8482 seconds

Objective
---------
   0.072 dimensionless

Variables
---------
   AR     :  10.000        [-]         Wing aspect ratio       
   CD     :   0.072        [-]         Drag Coefficient        
   CL     :   1.000        [-]         Lift Coefficient        
   S      :   0.664     meter ** 2     Wing area               
   V      :   3.600   meter / second   Airspeed                
   W      :   5.270       newton       Aircraft weight         
   Wwing  :   0.201       newton       Wing weight             
   e      :   0.992        [-]         Oswald efficiency factor
   lam    :   0.399        [-]         Wing taper ratio        

Sensitivities
-------------
   Sensitivities not available for optimizations of type Sequential Log Convex Program 

Solve Report
------------
   Solve Method           :  Sequential Log Convex Program 
   Classification         :  Iterative 
   Solver                 :  cvxopt 
   Number of Iterations   :  7 
   Termination Status     :  Converged, gradient of Lagrangian (1.043842e-07) within tolerance (1.000000e-06)  

Messages
--------
   1. Wolfe Condition 1 failed at iteration 3 (Step 3).  Watchdog counter is 1

13.872092548132818

real	0m5.669s
user	0m4.191s
sys	0m1.898s
+ status=0
+ set +x

=================================================
CAPS verification (using pyCAPS) case pyCAPS/optWingAvl.py passed (as expected)
=================================================


=================================================
+ echo 'pyCAPS/GPSize.py test;'
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESP126/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
pyCAPS/GPSize.py test;
+ python -u pyCAPS/GPSize.py -outLevel=0
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESP126/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt

Objective
---------
   6339.9402476213 newton

Variables
---------
   AR          :       18.0583068591        [-]         aspect ratio                                                            
   C_D_0       :        0.0127966186        [-]         Drag Coefficient, segment 0                                             
   C_D_1       :        0.0128135534        [-]         Drag Coefficient, segment 1                                             
   C_D_2       :        0.0077622395        [-]         Drag Coefficient, segment 2                                             
   C_Dfuse_0   :        0.0017626506        [-]         Fuselage Drag Coefficient, segment 0                                    
   C_Dfuse_1   :        0.0017626506        [-]         Fuselage Drag Coefficient, segment 1                                    
   C_Dfuse_2   :        0.0017626510        [-]         Fuselage Drag Coefficient, segment 2                                    
   C_Di_0      :        0.0056016002        [-]         Induced Drag Coefficient, segment 0                                     
   C_Di_1      :        0.0056028716        [-]         Induced Drag Coefficient, segment 1                                     
   C_Di_2      :        0.0002594009        [-]         Induced Drag Coefficient, segment 2                                     
   C_Dp_0      :        0.0054327043        [-]         Wing Profile Drag Coefficient, segment 0                                
   C_Dp_1      :        0.0054483614        [-]         Wing Profile Drag Coefficient, segment 1                                
   C_Dp_2      :        0.0057382717        [-]         Wing Profile Drag Coefficient, segment 2                                
   C_L_0       :        0.5494535783        [-]         Lift Coefficient, segment 0                                             
   C_L_1       :        0.5495159270        [-]         Lift Coefficient, segment 1                                             
   C_L_2       :        0.1182390122        [-]         Lift Coefficient, segment 2                                             
   I_cap_bar   :        0.0000193397        [-]         Area moment of inertia of cap on 2D cross section, normalized by chord^4
   M_r_bar     :    32106.9717613474       newton       Root Bending unit per unit chord                                        
   P_max       :  1211155.7559680410        watt        Maximum Engine Power                                                    
   R           :     4999.9816129528     kilometer      Single Segment range                                                    
   Re_0        :  4636790.3991634697        [-]         Reynolds Number, segment 0                                              
   Re_1        :  4427330.4209076529        [-]         Reynolds Number, segment 1                                              
   Re_2        :  9995446.9239517339        [-]         Reynolds Number, segment 2                                              
   S           :       28.3664420021     meter ** 2     total wing area                                                         
   T_0         :      799.0178645705       newton       Thrust, segment 0                                                       
   T_1         :      729.4239244544       newton       Thrust, segment 1                                                       
   T_2         :     2252.7493855701       newton       Thrust, segment 2                                                       
   V_0         :       69.5874592840   meter / second   Velocity, segment 0                                                     
   V_1         :       66.4439512429   meter / second   Velocity, segment 1                                                     
   V_2         :      150.0084591036   meter / second   Velocity, segment 2                                                     
   V_stall     :       37.9986643205   meter / second   stall speed                                                             
   W_0         :    34307.5807516552       newton       Weight, segment 0                                                       
   W_1         :    31281.5531631160       newton       Weight, segment 1                                                       
   W_2         :    34307.5610637156       newton       Weight, segment 2                                                       
   W_MTO       :    37630.4011124297       newton       Maximum Takeoff Weight                                                  
   W_cap       :     4278.1047592241       newton       Weight of Wing Spar Cap                                                 
   W_eng       :     2854.2361754189       newton       Engine Weight                                                           
   W_fuel_out  :     3314.0247993997       newton       Weight of fuel, outbound                                                
   W_fuel_ret  :     3025.9122892774       newton       Weight of fuel, return                                                  
   W_pay       :     4905.2326701420       newton       Payload Weight                                                          
   W_tilde     :    22457.8594632444       newton       Dry Weight, no wing                                                     
   W_web       :      133.6940460361       newton       Weight of Wing Spar Shear Web                                           
   W_wing      :     8823.3040844200       newton       wing weight                                                             
   W_zfw       :    31281.2018350684       newton       Zero Fuel Weight                                                        
   eta_0_0     :        0.2693167459        [-]         Overall Efficiency, segment 0                                           
   eta_0_1     :        0.2692858916        [-]         Overall Efficiency, segment 1                                           
   eta_0_2     :        0.2791280518        [-]         Overall Efficiency, segment 2                                           
   eta_i_0     :        0.9052651192        [-]         Inviscid Propeller Efficiency, segment 0                                
   eta_i_1     :        0.9051614203        [-]         Inviscid Propeller Efficiency, segment 1                                
   eta_i_2     :        0.9382448822        [-]         Inviscid Propeller Efficiency, segment 2                                
   eta_prop_0  :        0.7694756986        [-]         Propeller Efficiency, segment 0                                         
   eta_prop_1  :        0.7693875506        [-]         Propeller Efficiency, segment 1                                         
   eta_prop_2  :        0.7975082496        [-]         Propeller Efficiency, segment 2                                         
   nu          :        0.7860410805        [-]         Placeholder, (1+lam_w+lam_w**2)/(1+lam_w)**2                            
   p           :        1.9000448519        [-]         Dummy Variable (1+2*lam_w)                                              
   q           :        1.4500404597        [-]         Dummy Variable (1+lam_w)                                                
   t_cap_bar   :        0.0043345438        [-]         Spar cap thickness per unit chord                                       
   t_web_bar   :        0.0006000270        [-]         Spar web thickness per unit chord                                       
   tau         :        0.1499996279        [-]         airfoil thickness to chord ratio                                        
   z_bre_0     :        0.0922115805        [-]         Breguet Range Factor, segment 0                                         
   z_bre_1     :        0.0923337617        [-]         Breguet Range Factor, segment 1                                         

Constants
---------
   A_prop           :         0.7850000000           meter ** 2          Disk area of propeller                             
   CDA0             :         0.0500000000           meter ** 2          fuselage drag area                                 
   C_Lmax           :         1.5000000000              [-]              max CL with flaps down                             
   N_lift           :         6                         [-]              Ultimate Load Factor                               
   W_fixed          :     14700                        newton            fixed weight                                       
   e                :         0.9500000000              [-]              Oswald efficiency factor                           
   eta_eng          :         0.3500000000              [-]              Engine Efficiency                                  
   eta_v            :         0.8500000000              [-]              Propeller Viscous Efficiency                       
   f_wadd           :         2                         [-]              Added Weight Fraction                              
   g                :         9.8100000000      meter / second ** 2      Gravitational constant                             
   h_fuel           :  46000000                   joule / kilogram       Fuel Specific energy density                       
   k_ew             :         0.0372000000     newton / watt ** 0.803    Constant for engine weight                         
   mu               :         0.0000171000   kilogram / meter / second   viscosity of air                                   
   r_h              :         0.7500000000              [-]              Ratio of height at rear spar to maximum wing height
   rho              :         0.9091220000     kilogram / meter ** 3     density of air                                     
   rho_SL           :         1.2250000000     kilogram / meter ** 3     density of air, sea level                          
   rho_cap          :      2700                kilogram / meter ** 3     Density of wing cap material (aluminum)            
   rho_web          :      2700                kilogram / meter ** 3     Density of wing web material (aluminum)            
   sigma_max        :       250                      megapascal          Allowable tensile stress of aluminum               
   sigma_max_shear  :       167                      megapascal          Allowable shear stress of aluminum                 
   w_bar            :         0.5000000000              [-]              Ratio of spar box width to chord length            

Sensitivities
-------------
   Sensitivities not computed

Solve Report
------------
   Solve Method           :  Geometric Program 
   Classification         :  Convex 
   Solver                 :  cvxopt 

 EGADS Info: 0 Objects, 0 Reference in Use (of 0) at Close!

real	0m4.659s
user	0m5.110s
sys	0m0.116s
+ status=0
+ set +x

=================================================
CAPS verification (using pyCAPS) case pyCAPS/GPSize.py passed (as expected)
=================================================

mses: /Users/jenkins/workspace/ESP_bPreBuilt/ESP126/EngSketchPad/bin/mses

=================================================
+ echo 'pyCAPS/MSES.py test;'
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESP126/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
pyCAPS/MSES.py test;
+ python -u pyCAPS/MSES.py -outLevel=0
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESP126/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Objective
---------
   6436.9111747642 newton

Variables
---------
   AR                :        17.8847143703        [-]         aspect ratio                                                            
   Alpha_p20_MSES_0  :        22.6676624733       degree       Angle of Attack + 20deg from MSES, segment 0                            
   Alpha_p20_MSES_1  :        22.7725605594       degree       Angle of Attack + 20deg from MSES, segment 1                            
   Alpha_p20_MSES_2  :        18.8664426951       degree       Angle of Attack + 20deg from MSES, segment 2                            
   C_D_0             :         0.0127680026        [-]         Drag Coefficient, segment 0                                             
   C_D_1             :         0.0130143941        [-]         Drag Coefficient, segment 1                                             
   C_D_2             :         0.0074765087        [-]         Drag Coefficient, segment 2                                             
   C_Dfuse_0         :         0.0017731859        [-]         Fuselage Drag Coefficient, segment 0                                    
   C_Dfuse_1         :         0.0017731859        [-]         Fuselage Drag Coefficient, segment 1                                    
   C_Dfuse_2         :         0.0017731859        [-]         Fuselage Drag Coefficient, segment 2                                    
   C_Di_0            :         0.0053689965        [-]         Induced Drag Coefficient, segment 0                                     
   C_Di_1            :         0.0055861389        [-]         Induced Drag Coefficient, segment 1                                     
   C_Di_2            :         0.0002610120        [-]         Induced Drag Coefficient, segment 2                                     
   C_Dp_0            :         0.0056258204        [-]         Wing Profile Drag Coefficient, segment 0                                
   C_Dp_1            :         0.0056550700        [-]         Wing Profile Drag Coefficient, segment 1                                
   C_Dp_2            :         0.0054423095        [-]         Wing Profile Drag Coefficient, segment 2                                
   C_L_0             :         0.5353228067        [-]         Lift Coefficient, segment 0                                             
   C_L_1             :         0.5460488610        [-]         Lift Coefficient, segment 1                                             
   C_L_2             :         0.1180337615        [-]         Lift Coefficient, segment 2                                             
   C_L_MSES_0        :         0.5353228067        [-]         Lift Coefficient from MSES, segment 0                                   
   C_L_MSES_1        :         0.5460488610        [-]         Lift Coefficient from MSES, segment 1                                   
   C_L_MSES_2        :         0.1180337615        [-]         Lift Coefficient from MSES, segment 2                                   
   I_cap_bar         :         0.0000189923        [-]         Area moment of inertia of cap on 2D cross section, normalized by chord^4
   M_r_bar           :     31649.2629256045       newton       Root Bending unit per unit chord                                        
   P_max             :   1155819.0983774771        watt        Maximum Engine Power                                                    
   R                 :      5000.0000010210     kilometer      Single Segment range                                                    
   Re_0              :   4702125.2746726070        [-]         Reynolds Number, segment 0                                              
   Re_1              :   4440814.5793337049        [-]         Reynolds Number, segment 1                                              
   Re_2              :  10013489.5565969180        [-]         Reynolds Number, segment 2                                              
   S                 :        28.1978812745     meter ** 2     total wing area                                                         
   T_0               :       811.9144361127       newton       Thrust, segment 0                                                       
   T_1               :       738.1899382843       newton       Thrust, segment 1                                                       
   T_2               :      2156.2042613309       newton       Thrust, segment 2                                                       
   V_0               :        70.4366540784   meter / second   Velocity, segment 0                                                     
   V_1               :        66.5224856090   meter / second   Velocity, segment 1                                                     
   V_2               :       150.0000049409   meter / second   Velocity, segment 2                                                     
   V_stall           :        37.9999998304   meter / second   stall speed                                                             
   W_0               :     34040.6240956632       newton       Weight, segment 0                                                       
   W_1               :     30972.5122439076       newton       Weight, segment 1                                                       
   W_2               :     34040.6240956631       newton       Weight, segment 2                                                       
   W_MTO             :     37409.4238057056       newton       Maximum Takeoff Weight                                                  
   W_cap             :      4178.0707911956       newton       Weight of Wing Spar Cap                                                 
   W_eng             :      2748.1693321190       newton       Engine Weight                                                           
   W_fuel_out        :      3368.7993606073       newton       Weight of fuel, outbound                                                
   W_fuel_ret        :      3068.1118141569       newton       Weight of fuel, return                                                  
   W_pay             :      4905.0000238714       newton       Payload Weight                                                          
   W_tilde           :     22353.1693245709       newton       Dry Weight, no wing                                                     
   W_web             :       131.6008887574       newton       Weight of Wing Spar Shear Web                                           
   W_wing            :      8619.3429955669       newton       wing weight                                                             
   W_zfw             :     30972.5122296163       newton       Zero Fuel Weight                                                        
   eta_0_0           :         0.2695063546        [-]         Overall Efficiency, segment 0                                           
   eta_0_1           :         0.2690604520        [-]         Overall Efficiency, segment 1                                           
   eta_0_2           :         0.2798281448        [-]         Overall Efficiency, segment 2                                           
   eta_i_0           :         0.9059037131        [-]         Inviscid Propeller Efficiency, segment 0                                
   eta_i_1           :         0.9044048805        [-]         Inviscid Propeller Efficiency, segment 1                                
   eta_i_2           :         0.9405988059        [-]         Inviscid Propeller Efficiency, segment 2                                
   eta_prop_0        :         0.7700181561        [-]         Propeller Efficiency, segment 0                                         
   eta_prop_1        :         0.7687441484        [-]         Propeller Efficiency, segment 1                                         
   eta_prop_2        :         0.7995089850        [-]         Propeller Efficiency, segment 2                                         
   nu                :         0.7859963973        [-]         Placeholder, (1+lam_w+lam_w**2)/(1+lam_w)**2                            
   p                 :         1.9000000011        [-]         Dummy Variable (1+2*lam_w)                                              
   q                 :         1.4500000023        [-]         Dummy Variable (1+lam_w)                                                
   t_cap_bar         :         0.0042510724        [-]         Spar cap thickness per unit chord                                       
   t_web_bar         :         0.0005949804        [-]         Spar web thickness per unit chord                                       
   tau               :         0.1499998017        [-]         airfoil thickness to chord ratio                                        
   z_bre_0           :         0.0943682262        [-]         Breguet Range Factor, segment 0                                         
   z_bre_1           :         0.0944547882        [-]         Breguet Range Factor, segment 1                                         

Sensitivities
-------------
   Sensitivities not available for optimizations of type Sequential Log Convex Program 

Solve Report
------------
   Solve Method           :  Sequential Log Convex Program 
   Classification         :  Iterative 
   Solver                 :  cvxopt 
   Number of Iterations   :  31 
   Termination Status     :  Converged, relative change in the objective function (8.48e-06) is witin specified tolerance (1.00e-05) 

Messages
--------
    1. Attempted step of size 1.00e+00 at iteration 2 is too large and is causing a constraint to return as imaginary.  Decreasing according to the tau schedule.
    2. Attempted step of size 9.00e-01 at iteration 2 is too large and is causing a constraint to return as imaginary.  Decreasing according to the tau schedule.
    3. Wolfe Condition 1 failed at iteration 4 (Step 4).  Watchdog counter is 1
    4. Wolfe Condition 1 failed at iteration 7 (Step 7).  Watchdog counter is 1
    5. Wolfe Condition 1 failed at iteration 8 (Step 8).  Watchdog counter is 2
    6. Wolfe Condition 1 failed at iteration 11 (Step 11).  Watchdog counter is 1
    7. Wolfe Condition 1 failed at iteration 12 (Step 12).  Watchdog counter is 2
    8. Wolfe Condition 1 failed at iteration 13 (Step 13).  Watchdog counter is 3
    9. Attempted step of size 1.00e+00 at iteration 14 is too large and is causing a constraint to return as imaginary.  Decreasing according to the tau schedule.
   10. Wolfe Condition 1 failed at iteration 14 (Step 14).  Watchdog counter is 4
   11. Wolfe Condition 1 failed at iteration 16 (Step 16).  Watchdog counter is 1
   12. Wolfe Condition 1 failed at iteration 17 (Step 17).  Watchdog counter is 2


real	3m23.834s
user	3m20.135s
sys	0m3.605s
+ status=0
+ set +x

=================================================
CAPS verification (using pyCAPS) case pyCAPS/MSES.py passed (as expected)
=================================================


=================================================
+ echo 'pyCAPS/Camber.py test;'
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESP126/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
pyCAPS/Camber.py test;
+ python -u pyCAPS/Camber.py -outLevel=0
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESP126/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Objective
---------
   5491.4359225133 newton

Variables
---------
   AR                :        16.4147174429        [-]         aspect ratio                                                            
   Alpha_p20_MSES_0  :        18.0126155823       degree       Angle of Attack + 20deg from MSES, segment 0                            
   Alpha_p20_MSES_1  :        18.1754881520       degree       Angle of Attack + 20deg from MSES, segment 1                            
   Alpha_p20_MSES_2  :        14.5292099988       degree       Angle of Attack + 20deg from MSES, segment 2                            
   C_D_0             :         0.0102948117        [-]         Drag Coefficient, segment 0                                             
   C_D_1             :         0.0107150833        [-]         Drag Coefficient, segment 1                                             
   C_D_2             :         0.0069659104        [-]         Drag Coefficient, segment 2                                             
   C_Dfuse_0         :         0.0019058054        [-]         Fuselage Drag Coefficient, segment 0                                    
   C_Dfuse_1         :         0.0019058054        [-]         Fuselage Drag Coefficient, segment 1                                    
   C_Dfuse_2         :         0.0019058054        [-]         Fuselage Drag Coefficient, segment 2                                    
   C_Di_0            :         0.0044487314        [-]         Induced Drag Coefficient, segment 0                                     
   C_Di_1            :         0.0048480057        [-]         Induced Drag Coefficient, segment 1                                     
   C_Di_2            :         0.0002903621        [-]         Induced Drag Coefficient, segment 2                                     
   C_Dp_0            :         0.0039402749        [-]         Wing Profile Drag Coefficient, segment 0                                
   C_Dp_1            :         0.0039612726        [-]         Wing Profile Drag Coefficient, segment 1                                
   C_Dp_2            :         0.0047697411        [-]         Wing Profile Drag Coefficient, segment 2                                
   C_L_0             :         0.4642555300        [-]         Lift Coefficient, segment 0                                             
   C_L_1             :         0.4845048407        [-]         Lift Coefficient, segment 1                                             
   C_L_2             :         0.1187898747        [-]         Lift Coefficient, segment 2                                             
   C_L_MSES_0        :         0.4642555300        [-]         Lift Coefficient from MSES, segment 0                                   
   C_L_MSES_1        :         0.4845048407        [-]         Lift Coefficient from MSES, segment 1                                   
   C_L_MSES_2        :         0.1187898747        [-]         Lift Coefficient from MSES, segment 2                                   
   I_cap_bar         :         0.0000169655        [-]         Area moment of inertia of cap on 2D cross section, normalized by chord^4
   M_r_bar           :     28632.8148697486       newton       Root Bending unit per unit chord                                        
   P_max             :    995317.3030262130        watt        Maximum Engine Power                                                    
   R                 :      5000.0000150914     kilometer      Single Segment range                                                    
   Re_0              :   5146611.2342969924        [-]         Reynolds Number, segment 0                                              
   Re_1              :   4834919.6517840819        [-]         Reynolds Number, segment 1                                              
   Re_2              :  10114462.7451584097        [-]         Reynolds Number, segment 2                                              
   S                 :        26.2686333615     meter ** 2     total wing area                                                         
   T_0               :       708.1364694815       newton       Thrust, segment 0                                                       
   T_1               :       647.1687649939       newton       Thrust, segment 1                                                       
   T_2               :      1869.9310318896       newton       Thrust, segment 2                                                       
   V_0               :        76.2664901710   meter / second   Velocity, segment 0                                                     
   V_1               :        71.6311268476   meter / second   Velocity, segment 1                                                     
   V_2               :       150.0000569370   meter / second   Velocity, segment 2                                                     
   V_stall           :        37.9862969911   meter / second   stall speed                                                             
   W_0               :     31915.7596170390       newton       Weight, segment 0                                                       
   W_1               :     29289.9561426453       newton       Weight, segment 1                                                       
   W_2               :     31915.7596170390       newton       Weight, segment 2                                                       
   W_MTO             :     34825.3028076972       newton       Maximum Takeoff Weight                                                  
   W_cap             :      3504.9733685113       newton       Weight of Wing Spar Cap                                                 
   W_eng             :      2435.1503729458       newton       Engine Weight                                                           
   W_fuel_out        :      2865.6326794429       newton       Weight of fuel, outbound                                                
   W_fuel_ret        :      2625.8032430704       newton       Weight of fuel, return                                                  
   W_pay             :      4905.0001242919       newton       Payload Weight                                                          
   W_tilde           :     22040.1505203108       newton       Dry Weight, no wing                                                     
   W_web             :       119.9293311624       newton       Weight of Wing Spar Shear Web                                           
   W_wing            :      7249.8053469954       newton       wing weight                                                             
   W_zfw             :     29289.9559483835       newton       Zero Fuel Weight                                                        
   camberLocation    :         0.7087509688        [-]         location of maximum airfoil camber scaled by chord                      
   eta_0_0           :         0.2755554590        [-]         Overall Efficiency, segment 0                                           
   eta_0_1           :         0.2747888706        [-]         Overall Efficiency, segment 1                                           
   eta_0_2           :         0.2819554372        [-]         Overall Efficiency, segment 2                                           
   eta_i_0           :         0.9262368370        [-]         Inviscid Propeller Efficiency, segment 0                                
   eta_i_1           :         0.9236600693        [-]         Inviscid Propeller Efficiency, segment 1                                
   eta_i_2           :         0.9477493688        [-]         Inviscid Propeller Efficiency, segment 2                                
   eta_prop_0        :         0.7873013115        [-]         Propeller Efficiency, segment 0                                         
   eta_prop_1        :         0.7851110589        [-]         Propeller Efficiency, segment 1                                         
   eta_prop_2        :         0.8055869634        [-]         Propeller Efficiency, segment 2                                         
   maxCamber         :         0.0491463515        [-]         maximum airfoil camber scaled by chord                                  
   nu                :         0.7859964213        [-]         Placeholder, (1+lam_w+lam_w**2)/(1+lam_w)**2                            
   p                 :         1.9000000162        [-]         Dummy Variable (1+2*lam_w)                                              
   q                 :         1.4500000250        [-]         Dummy Variable (1+lam_w)                                                
   t_cap_bar         :         0.0037976551        [-]         Spar cap thickness per unit chord                                       
   t_web_bar         :         0.0005785209        [-]         Spar web thickness per unit chord                                       
   tau               :         0.1495748504        [-]         airfoil thickness to chord ratio                                        
   z_bre_0           :         0.0860294936        [-]         Breguet Range Factor, segment 0                                         
   z_bre_1           :         0.0859477878        [-]         Breguet Range Factor, segment 1                                         

Sensitivities
-------------
   Sensitivities not available for optimizations of type Sequential Log Convex Program 

Solve Report
------------
   Solve Method           :  Sequential Log Convex Program 
   Classification         :  Iterative 
   Solver                 :  cvxopt 
   Number of Iterations   :  99 
   Termination Status     :  Converged, relative change in the objective function (7.65e-06) is witin specified tolerance (1.00e-05) 

Messages
--------
    1. Attempted step of size 1.00e+00 at iteration 1 is too large and is causing a constraint to return as imaginary.  Decreasing according to the tau schedule.
    2. Attempted step of size 1.00e+00 at iteration 3 is too large and is causing a constraint to return as imaginary.  Decreasing according to the tau schedule.
    3. Attempted step of size 1.00e+00 at iteration 7 is too large and is causing a constraint to return as imaginary.  Decreasing according to the tau schedule.
    4. Wolfe Condition 1 failed at iteration 8 (Step 8).  Watchdog counter is 1
    5. Attempted step of size 1.00e+00 at iteration 10 is too large and is causing a constraint to return as imaginary.  Decreasing according to the tau schedule.
    6. Wolfe Condition 1 failed at iteration 11 (Step 11).  Watchdog counter is 1
    7. Attempted step of size 1.00e+00 at iteration 12 is too large and is causing a constraint to return as imaginary.  Decreasing according to the tau schedule.
    8. Wolfe Condition 1 failed at iteration 14 (Step 14).  Watchdog counter is 1
    9. Attempted step of size 1.00e+00 at iteration 15 is too large and is causing a constraint to return as imaginary.  Decreasing according to the tau schedule.
   10. Wolfe Condition 1 failed at iteration 18 (Step 18).  Watchdog counter is 1
   11. Wolfe Condition 1 failed at iteration 21 (Step 21).  Watchdog counter is 1
   12. Attempted step of size 2.15e-01 at iteration 27 is too large and is causing a constraint to return as imaginary.  Decreasing according to the tau schedule.
   13. Attempted step of size 1.77e-01 at iteration 32 is too large and is causing a constraint to return as imaginary.  Decreasing according to the tau schedule.
   14. Attempted step of size 1.57e-01 at iteration 36 is too large and is causing a constraint to return as imaginary.  Decreasing according to the tau schedule.
   15. Wolfe Condition 1 failed at iteration 37 (Step 37).  Watchdog counter is 1
   16. Attempted step of size 1.42e-01 at iteration 40 is too large and is causing a constraint to return as imaginary.  Decreasing according to the tau schedule.
   17. Wolfe Condition 1 failed at iteration 43 (Step 43).  Watchdog counter is 1
   18. Attempted step of size 1.30e-01 at iteration 44 is too large and is causing a constraint to return as imaginary.  Decreasing according to the tau schedule.
   19. Wolfe Condition 1 failed at iteration 49 (Step 49).  Watchdog counter is 1
   20. Wolfe Condition 1 failed at iteration 50 (Step 50).  Watchdog counter is 2
   21. Attempted step of size 1.13e-01 at iteration 52 is too large and is causing a constraint to return as imaginary.  Decreasing according to the tau schedule.
   22. Attempted step of size 1.09e-01 at iteration 54 is too large and is causing a constraint to return as imaginary.  Decreasing according to the tau schedule.
   23. Attempted step of size 3.28e-02 at iteration 54 is too large and is causing a constraint to return as imaginary.  Decreasing according to the tau schedule.
   24. Wolfe Condition 1 failed at iteration 59 (Step 59).  Watchdog counter is 1
   25. Wolfe Condition 1 failed at iteration 60 (Step 60).  Watchdog counter is 2
   26. Wolfe Condition 1 failed at iteration 62 (Step 62).  Watchdog counter is 1
   27. Wolfe Condition 1 failed at iteration 67 (Step 67).  Watchdog counter is 1
   28. Wolfe Condition 1 failed at iteration 68 (Step 68).  Watchdog counter is 2
   29. Attempted step of size 8.84e-02 at iteration 71 is too large and is causing a constraint to return as imaginary.  Decreasing according to the tau schedule.
   30. Wolfe Condition 1 failed at iteration 72 (Step 72).  Watchdog counter is 1
   31. Wolfe Condition 1 failed at iteration 73 (Step 73).  Watchdog counter is 2
   32. Wolfe Condition 1 failed at iteration 74 (Step 74).  Watchdog counter is 3
   33. Wolfe Condition 1 failed at iteration 75 (Step 75).  Watchdog counter is 4
   34. Wolfe Condition 1 failed at iteration 95 (Step 95).  Watchdog counter is 1


real	10m54.937s
user	10m41.975s
sys	0m11.323s
+ status=0
+ set +x

=================================================
CAPS verification (using pyCAPS) case pyCAPS/Camber.py passed (as expected)
=================================================


=================================================
+ echo 'pyCAPS/CMConstraint.py test;'
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESP126/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
pyCAPS/CMConstraint.py test;
+ python -u pyCAPS/CMConstraint.py -outLevel=0
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESP126/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Objective
---------
   6389.1599788872 newton

Variables
---------
   AR                :       18.1246600755        [-]         aspect ratio                                                            
   Alpha_p20_MSES_0  :       22.7354842586       degree       Angle of Attack + 20deg from MSES, segment 0                            
   Alpha_p20_MSES_1  :       22.7563511509       degree       Angle of Attack + 20deg from MSES, segment 1                            
   Alpha_p20_MSES_2  :       18.6841775414       degree       Angle of Attack + 20deg from MSES, segment 2                            
   C_D_0             :        0.0132149995        [-]         Drag Coefficient, segment 0                                             
   C_D_1             :        0.0132499519        [-]         Drag Coefficient, segment 1                                             
   C_D_2             :        0.0075834110        [-]         Drag Coefficient, segment 2                                             
   C_Dfuse_0         :        0.0017623324        [-]         Fuselage Drag Coefficient, segment 0                                    
   C_Dfuse_1         :        0.0017623324        [-]         Fuselage Drag Coefficient, segment 1                                    
   C_Dfuse_2         :        0.0017623324        [-]         Fuselage Drag Coefficient, segment 2                                    
   C_Di_0            :        0.0058797215        [-]         Induced Drag Coefficient, segment 0                                     
   C_Di_1            :        0.0059269314        [-]         Induced Drag Coefficient, segment 1                                     
   C_Di_2            :        0.0002582450        [-]         Induced Drag Coefficient, segment 2                                     
   C_Dp_0            :        0.0055729459        [-]         Wing Profile Drag Coefficient, segment 0                                
   C_Dp_1            :        0.0055606884        [-]         Wing Profile Drag Coefficient, segment 1                                
   C_Dp_2            :        0.0055628314        [-]         Wing Profile Drag Coefficient, segment 2                                
   C_L_0             :        0.5638905478        [-]         Lift Coefficient, segment 0                                             
   C_L_1             :        0.5661550132        [-]         Lift Coefficient, segment 1                                             
   C_L_2             :        0.1181879141        [-]         Lift Coefficient, segment 2                                             
   C_L_MSES_0        :        0.5638905478        [-]         Lift Coefficient from MSES, segment 0                                   
   C_L_MSES_1        :        0.5661550132        [-]         Lift Coefficient from MSES, segment 1                                   
   C_L_MSES_2        :        0.1181879141        [-]         Lift Coefficient from MSES, segment 2                                   
   I_cap_bar         :        0.0000194277        [-]         Area moment of inertia of cap on 2D cross section, normalized by chord^4
   M_r_bar           :    32142.4766677387       newton       Root Bending unit per unit chord                                        
   P_max             :  1180922.1189759877        watt        Maximum Engine Power                                                    
   R                 :     5000.0000115189     kilometer      Single Segment range                                                    
   Re_0              :  4569113.0350051858        [-]         Reynolds Number, segment 0                                              
   Re_1              :  4352777.0943119153        [-]         Reynolds Number, segment 1                                              
   Re_2              :  9977785.5636399947        [-]         Reynolds Number, segment 2                                              
   S                 :       28.3718598326     meter ** 2     total wing area                                                         
   T_0               :      803.8161139074       newton       Thrust, segment 0                                                       
   T_1               :      731.4741552257       newton       Thrust, segment 1                                                       
   T_2               :     2200.5003332610       newton       Thrust, segment 2                                                       
   V_0               :       68.6872633568   meter / second   Velocity, segment 0                                                     
   V_1               :       65.4352286761   meter / second   Velocity, segment 1                                                     
   V_2               :      150.0000174706   meter / second   Velocity, segment 2                                                     
   V_stall           :       37.9999992819   meter / second   stall speed                                                             
   W_0               :    34295.4186254629       newton       Weight, segment 0                                                       
   W_1               :    31251.0744708949       newton       Weight, segment 1                                                       
   W_2               :    34295.4186254629       newton       Weight, segment 2                                                       
   W_MTO             :    37640.2357223150       newton       Maximum Takeoff Weight                                                  
   W_cap             :     4291.8687051105       newton       Weight of Wing Spar Cap                                                 
   W_eng             :     2795.9949775438       newton       Engine Weight                                                           
   W_fuel_out        :     3344.8158627813       newton       Weight of fuel, outbound                                                
   W_fuel_ret        :     3044.3441161059       newton       Weight of fuel, return                                                  
   W_pay             :     4905.0002866763       newton       Payload Weight                                                          
   W_tilde           :    22400.9952205062       newton       Dry Weight, no wing                                                     
   W_web             :      133.1707762079       newton       Weight of Wing Spar Shear Web                                           
   W_wing            :     8850.0789606646       newton       wing weight                                                             
   W_zfw             :    31251.0742320470       newton       Zero Fuel Weight                                                        
   camberLocation    :        0.3743117570        [-]         location of maximum airfoil camber scaled by chord                      
   eta_0_0           :        0.2685537422        [-]         Overall Efficiency, segment 0                                           
   eta_0_1           :        0.2684906678        [-]         Overall Efficiency, segment 1                                           
   eta_0_2           :        0.2795064938        [-]         Overall Efficiency, segment 2                                           
   eta_i_0           :        0.9027016546        [-]         Inviscid Propeller Efficiency, segment 0                                
   eta_i_1           :        0.9024896397        [-]         Inviscid Propeller Efficiency, segment 1                                
   eta_i_2           :        0.9395176263        [-]         Inviscid Propeller Efficiency, segment 2                                
   eta_prop_0        :        0.7672964064        [-]         Propeller Efficiency, segment 0                                         
   eta_prop_1        :        0.7671161938        [-]         Propeller Efficiency, segment 1                                         
   eta_prop_2        :        0.7985899824        [-]         Propeller Efficiency, segment 2                                         
   maxCamber         :        0.0222539259        [-]         maximum airfoil camber scaled by chord                                  
   negCMp1_0         :        1.0554550403        [-]         Negative CM about 0.25c + 1, segment 0                                  
   negCMp1_1         :        1.0551745498        [-]         Negative CM about 0.25c + 1, segment 1                                  
   negCMp1_2         :        1.0580510080        [-]         Negative CM about 0.25c + 1, segment 2                                  
   nu                :        0.7859964727        [-]         Placeholder, (1+lam_w+lam_w**2)/(1+lam_w)**2                            
   p                 :        1.9000000085        [-]         Dummy Variable (1+2*lam_w)                                              
   q                 :        1.4500000156        [-]         Dummy Variable (1+lam_w)                                                
   t_cap_bar         :        0.0043555913        [-]         Spar cap thickness per unit chord                                       
   t_web_bar         :        0.0006005377        [-]         Spar web thickness per unit chord                                       
   tau               :        0.1499999234        [-]         airfoil thickness to chord ratio                                        
   z_bre_0           :        0.0930629119        [-]         Breguet Range Factor, segment 0                                         
   z_bre_1           :        0.0929596776        [-]         Breguet Range Factor, segment 1                                         

Sensitivities
-------------
   Sensitivities not available for optimizations of type Sequential Log Convex Program 

Solve Report
------------
   Solve Method           :  Sequential Log Convex Program 
   Classification         :  Iterative 
   Solver                 :  cvxopt 
   Number of Iterations   :  26 
   Termination Status     :  Converged, relative change in the objective function (3.87e-06) is witin specified tolerance (1.00e-05) 

Messages
--------
    1. Wolfe Condition 1 failed at iteration 3 (Step 3).  Watchdog counter is 1
    2. Attempted step of size 1.00e+00 at iteration 6 is too large and is causing a constraint to return as imaginary.  Decreasing according to the tau schedule.
    3. Wolfe Condition 1 failed at iteration 7 (Step 7).  Watchdog counter is 1
    4. Wolfe Condition 1 failed at iteration 9 (Step 9).  Watchdog counter is 1
    5. Wolfe Condition 1 failed at iteration 12 (Step 12).  Watchdog counter is 1
    6. Wolfe Condition 1 failed at iteration 13 (Step 13).  Watchdog counter is 2
    7. Attempted step of size 1.00e+00 at iteration 14 is too large and is causing a constraint to return as imaginary.  Decreasing according to the tau schedule.
    8. Attempted step of size 1.00e+00 at iteration 15 is too large and is causing a constraint to return as imaginary.  Decreasing according to the tau schedule.
    9. Wolfe Condition 1 failed at iteration 21 (Step 21).  Watchdog counter is 1
   10. Attempted step of size 2.87e-01 at iteration 22 is too large and is causing a constraint to return as imaginary.  Decreasing according to the tau schedule.
   11. Attempted step of size 2.37e-01 at iteration 25 is too large and is causing a constraint to return as imaginary.  Decreasing according to the tau schedule.
   12. Attempted step of size 7.12e-02 at iteration 25 is too large and is causing a constraint to return as imaginary.  Decreasing according to the tau schedule.
   13. Attempted step of size 2.14e-02 at iteration 25 is too large and is causing a constraint to return as imaginary.  Decreasing according to the tau schedule.
   14. Attempted step of size 6.41e-03 at iteration 25 is too large and is causing a constraint to return as imaginary.  Decreasing according to the tau schedule.


real	3m36.267s
user	3m32.772s
sys	0m3.454s
+ status=0
+ set +x

=================================================
CAPS verification (using pyCAPS) case pyCAPS/CMConstraint.py passed (as expected)
=================================================

Traceback (most recent call last):
  File "&lt;string&gt;", line 1, in &lt;module&gt;
ModuleNotFoundError: No module named 'torch'

*************************************************
*************************************************

=================================================
Did not run examples for:

awave
autoLink
Pointwise
Fun3D
abaqus
Nastran
Mystran
Plato
Mystran
=================================================

All tests pass!


=================================================
=================================================
+ cd /Users/jenkins/workspace/ESP_bPreBuilt/CAPS/training/2023
+ bash -e execute_Training.sh

=================================================
Using python : /Users/jenkins/workspace/ESP_bPreBuilt/ESP126/Python-3.11.9/bin/python
=================================================


=================================================
+ echo 'transport.csm test;'
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/CAPS/training/2023/training.log
transport.csm test;
+ /Users/jenkins/workspace/ESP_bPreBuilt/ESP126/EngSketchPad/bin/serveESP -batch -verify -outLevel 0 transport.csm
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/CAPS/training/2023/training.log
WARNING:: cannot open "./verify_7.8.1/transport.vfy", so verification is being skipped

MESSAGE:: Building wingOml


MESSAGE:: Building wingWaffle


MESSAGE:: Building wingHinges


MESSAGE:: Building nacelleOml


MESSAGE:: Building htailOml


MESSAGE:: Building htailWaffle


MESSAGE:: Building htailHinges


MESSAGE:: Building vtailOml


MESSAGE:: Building vtailWaffle


MESSAGE:: Building vtailHinges


MESSAGE:: Building fuseOml


MESSAGE:: Building fuseWaffle


MESSAGE:: Building fuseIml


MESSAGE:: Building payload

==&gt; serveESP completed successfully with 5 warnings and no verification data

real	0m8.759s
user	0m10.498s
sys	0m7.807s
+ status=0
+ set +x

=================================================
data/ESP/transport             passed (as expected)
=================================================

execute_Training.sh: line 157: /Users/jenkins/workspace/ESP_bPreBuilt/ESP126/EngSketchPad/test/template_avl: No such file or directory

=================================================
template_avl.py test;
+ python template_avl.py
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/CAPS/training/2023/training.log

==&gt; Loading geometry from file "../ESP/transport.csm"...

==&gt; Setting Build Variables and Geometry Values...

==&gt; Creating AVL aim...
{'wingHinge1': {'deflectionAngle': -10.0}, 'wingHinge2': {'deflectionAngle': 10.0}, 'wingHinge3': {'deflectionAngle': 15.0}, 'wingHinge4': {'deflectionAngle': 15.0}, 'wingHinge5': {'deflectionAngle': 10.0}, 'wingHinge6': {'deflectionAngle': 10.0}, 'htailHinge1': {'deflectionAngle': 5.0}, 'htailHinge2': {'deflectionAngle': 5.0}}

==&gt; Running AVL...

MESSAGE:: Building wingOml


MESSAGE:: Building wingHinges


MESSAGE:: Building htailOml


MESSAGE:: Building htailHinges


MESSAGE:: Building vtailOml


MESSAGE:: Building vtailHinges

Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 3
	Name = Wing, index = 1
	Name = Htail, index = 2
	Name = Vtail, index = 3
Getting vortex lattice control surface data
	VLM control surface name - htailHinge1
	VLM control surface name - htailHinge2
	VLM control surface name - wingHinge1
	VLM control surface name - wingHinge2
	VLM control surface name - wingHinge3
	VLM control surface name - wingHinge4
	VLM control surface name - wingHinge5
	VLM control surface name - wingHinge6
	Done getting vortex lattice control surface data
Getting vortex lattice surface data
	VLM surface name - Htail
	No "groupName" variable provided or no matches found, going to use tuple name
	VLM surface name - Wing
	No "groupName" variable provided or no matches found, going to use tuple name
	Done getting vortex lattice surface data
Warning: Control htailControl1 not found in controls tuple! Only defaults will be used.
Warning: Control htailControl1 not found in controls tuple! Only defaults will be used.
Warning: Control htailControl1 not found in controls tuple! Only defaults will be used.
Warning: Control htailControl1 not found in controls tuple! Only defaults will be used.
Warning: Control WingControl1 not found in controls tuple! Only defaults will be used.
Warning: Control WingControl1 not found in controls tuple! Only defaults will be used.
Warning: Control WingControl2 not found in controls tuple! Only defaults will be used.
Warning: Control WingControl2 not found in controls tuple! Only defaults will be used.
Warning: Control WingControl3 not found in controls tuple! Only defaults will be used.
Warning: Control WingControl3 not found in controls tuple! Only defaults will be used.
Warning: Control WingControl3 not found in controls tuple! Only defaults will be used.
Warning: Control WingControl3 not found in controls tuple! Only defaults will be used.
Warning: Control WingControl2 not found in controls tuple! Only defaults will be used.
Warning: Control WingControl2 not found in controls tuple! Only defaults will be used.
Warning: Control WingControl4 not found in controls tuple! Only defaults will be used.
Warning: Control WingControl4 not found in controls tuple! Only defaults will be used.
Writing surface - Htail (ID = 0)
	Section 1 of 7 (ID = 0)
	Section 2 of 7 (ID = 3)
	  Control surface 1 of 1 
	Section 3 of 7 (ID = 4)
	  Control surface 1 of 1 
	Section 4 of 7 (ID = 1)
	Section 5 of 7 (ID = 5)
	  Control surface 1 of 1 
	Section 6 of 7 (ID = 6)
	  Control surface 1 of 1 
	Section 7 of 7 (ID = 2)
Writing surface - Wing (ID = 1)
	Section 1 of 17 (ID = 0)
	Section 2 of 17 (ID = 5)
	  Control surface 1 of 1 
	Section 3 of 17 (ID = 6)
	  Control surface 1 of 1 
	Section 4 of 17 (ID = 7)
	  Control surface 1 of 1 
	Section 5 of 17 (ID = 8)
	  Control surface 1 of 1 
	Section 6 of 17 (ID = 4)
	Section 7 of 17 (ID = 9)
	  Control surface 1 of 1 
	Section 8 of 17 (ID = 10)
	  Control surface 1 of 1 
	Section 9 of 17 (ID = 1)
	Section 10 of 17 (ID = 11)
	  Control surface 1 of 1 
	Section 11 of 17 (ID = 12)
	  Control surface 1 of 1 
	Section 12 of 17 (ID = 3)
	Section 13 of 17 (ID = 13)
	  Control surface 1 of 1 
	Section 14 of 17 (ID = 14)
	  Control surface 1 of 1 
	Section 15 of 17 (ID = 15)
	  Control surface 1 of 1 
	Section 16 of 17 (ID = 16)
	  Control surface 1 of 1 
	Section 17 of 17 (ID = 2)

================ run_avl.py complete ==================


Force/moment coefficients:
CXtot  : 0.1440096030964816
CYtot  : -3.53511379732127e-11
CZtot  : -1.170781090342353
Cltot  : -3.063862377222321e-10
Cmtot  : -1.825893600985071
Cntot  : 2.402339104754559e-10
CLtot  : 1.178001299993477
CDtot  : 0.06148222914722529
e      : 0.7858931265075788

real	0m10.708s
user	0m10.695s
sys	0m18.425s
+ status=0
+ set +x

=================================================
data/session01/template_avl.py passed (as expected)
=================================================


=================================================
+ echo 'f118-A.csm test;'
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/CAPS/training/2023/training.log
f118-A.csm test;
+ /Users/jenkins/workspace/ESP_bPreBuilt/ESP126/EngSketchPad/bin/serveESP -batch -verify -outLevel 0 f118-A.csm
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/CAPS/training/2023/training.log
WARNING:: cannot open "./verify_7.8.1/f118-A.vfy", so verification is being skipped
==&gt; serveESP completed successfully with no verification data

real	0m0.102s
user	0m0.103s
sys	0m0.006s
+ status=0
+ set +x

=================================================
data/session02/f118-A          passed (as expected)
=================================================


=================================================
1_f118_Geom.py test;
+ python 1_f118_Geom.py
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/CAPS/training/2023/training.log

==&gt; Loading geometry from file "f118-A.csm"...

==&gt; Bulding and viewing geometry...

real	0m0.220s
user	0m0.272s
sys	0m0.056s
+ status=0
+ set +x

=================================================
data/session02/1_f118_Geom.py  passed (as expected)
=================================================


=================================================
2_f118_DESPMTR.py test;
+ python 2_f118_DESPMTR.py
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/CAPS/training/2023/training.log

==&gt; Loading geometry from file "f118-A.csm"...
--&gt; old htail:area =  1210.0
--&gt; new htail:area =  2420.0

==&gt; Bulding and viewing Wide Body geometry...

==&gt; Bulding and viewing Canard geometry...

==&gt; All design parameters
--&gt; wing:area    = 1210.0
--&gt; wing:aspect  = 9.0
--&gt; wing:thick   = 0.1
--&gt; wing:xroot   = 54.0
--&gt; wing:zroot   = -5.0
--&gt; htail:area   = 4240.0
--&gt; htail:aspect = 4.15
--&gt; htail:thick  = 0.08
--&gt; htail:xroot  = 145.0
--&gt; htail:zroot  = 5.0
--&gt; vtail        = [[1220.0, 1.8, 0.08, 150.0, -8.0, 9.0], [1220.0, 1.8, 0.08, 150.0, 8.0, 9.0]]
--&gt; fuse:length  = 180.0
--&gt; fuse:width   = 20.0
--&gt; fuse:height  = 20.0

real	0m0.255s
user	0m0.302s
sys	0m0.068s
+ status=0
+ set +x

=================================================
data/session02/2_f118_DESPMTR.py passed (as expected)
=================================================


=================================================
3_f118_Save.py test;
+ python 3_f118_Save.py
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/CAPS/training/2023/training.log

==&gt; Loading geometry from file "f118-A.csm"...
--&gt; old htail:area =  1210.0
--&gt; new htail:area =  2420.0

==&gt; Bulding and saving Wide Body geometry...

==&gt; Bulding and saving Canard geometry...

==&gt; All design parameters
--&gt; wing:area    = 1210.0
--&gt; wing:aspect  = 9.0
--&gt; wing:thick   = 0.1
--&gt; wing:xroot   = 54.0
--&gt; wing:zroot   = -5.0
--&gt; htail:area   = 4240.0
--&gt; htail:aspect = 4.15
--&gt; htail:thick  = 0.08
--&gt; htail:xroot  = 145.0
--&gt; htail:zroot  = 5.0
--&gt; vtail        = [[1220.0, 1.8, 0.08, 150.0, -8.0, 9.0], [1220.0, 1.8, 0.08, 150.0, 8.0, 9.0]]
--&gt; fuse:length  = 180.0
--&gt; fuse:width   = 20.0
--&gt; fuse:height  = 20.0

real	0m0.236s
user	0m0.292s
sys	0m0.066s
+ status=0
+ set +x

=================================================
data/session02/3_f118_Save.py  passed (as expected)
=================================================


=================================================
4_f118_Shortcut.py test;
+ python 4_f118_Shortcut.py
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/CAPS/training/2023/training.log

==&gt; Loading geometry from file "f118-A.csm"...
--&gt; old htail:area =  1210.0
--&gt; new htail:area =  2420.0

==&gt; Bulding and viewing Wide Body geometry...

==&gt; Bulding and viewing Canard geometry...

==&gt; Grouped parameters
--&gt; fuse
    fuse:length  = 180.0
    fuse:width   = 20.0
    fuse:height  = 20.0
--&gt; wing
    wing:area    = 1210.0
    wing:aspect  = 9.0
    wing:thick   = 0.1
    wing:xroot   = 54.0
    wing:zroot   = -5.0
--&gt; htail
    htail:area   = 4240.0
    htail:aspect = 4.15
    htail:thick  = 0.08
    htail:xroot  = 145.0
    htail:zroot  = 5.0

real	0m0.241s
user	0m0.299s
sys	0m0.068s
+ status=0
+ set +x

=================================================
data/session02/4_f118_Shortcut.py passed (as expected)
=================================================


=================================================
5_f118_writeParameters.py test;
+ python 5_f118_writeParameters.py
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/CAPS/training/2023/training.log

==&gt; Loading geometry from file "f118-A.csm"...

==&gt; Saving parameters to "f118_4.params"...

==&gt; Loading 2nd geometry from file "f118-A.csm"...

==&gt; Reading parameters from "f118_4.params"...
--&gt; Opening DESPMTR file "f118_4.params"
    updating CFGPMTR nrow                            [ 1, 1] =     1.000000
    updating DESPMTR wing:area                       [ 1, 1] =  4240.000000
    updating DESPMTR wing:aspect                     [ 1, 1] =     9.000000
    updating DESPMTR wing:thick                      [ 1, 1] =     0.100000
    updating DESPMTR wing:xroot                      [ 1, 1] =    54.000000
    updating DESPMTR wing:zroot                      [ 1, 1] =    -5.000000
    updating DESPMTR htail:area                      [ 1, 1] =  2420.000000
    updating DESPMTR htail:aspect                    [ 1, 1] =     4.150000
    updating DESPMTR htail:thick                     [ 1, 1] =     0.080000
    updating DESPMTR htail:xroot                     [ 1, 1] =   145.000000
    updating DESPMTR htail:zroot                     [ 1, 1] =     5.000000
    updating DESPMTR vtail                           [ 1, 1] =  1220.000000
    updating DESPMTR vtail                           [ 1, 2] =     1.800000
    updating DESPMTR vtail                           [ 1, 3] =     0.080000
    updating DESPMTR vtail                           [ 1, 4] =   150.000000
    updating DESPMTR vtail                           [ 1, 5] =     0.000000
    updating DESPMTR vtail                           [ 1, 6] =     9.000000
    updating DESPMTR fuse:length                     [ 1, 1] =   180.000000
    updating DESPMTR fuse:width                      [ 1, 1] =    60.000000
    updating DESPMTR fuse:height                     [ 1, 1] =    20.000000

==&gt; Building and viewing the geometry...
 EGADS Info: 0 Objects, 0 Reference in Use (of 0) at Close!

real	0m0.267s
user	0m0.322s
sys	0m0.097s
+ status=0
+ set +x

=================================================
data/session02/5_f118_writeParameters.py passed (as expected)
=================================================


=================================================
6_f118_bodies.py test;
+ python 6_f118_bodies.py
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/CAPS/training/2023/training.log

==&gt; Loading geometry from file "f118-A.csm"...

==&gt; pyEGADS egos...
Wing &lt;pyEGADS.egads_common.ego object at 0x10a572710&gt;
Htail &lt;pyEGADS.egads_common.ego object at 0x10a572350&gt;
Vtail1 &lt;pyEGADS.egads_common.ego object at 0x10a572ed0&gt;
Fuselage &lt;pyEGADS.egads_common.ego object at 0x10a572dd0&gt;

real	0m0.221s
user	0m0.271s
sys	0m0.057s
+ status=0
+ set +x

=================================================
data/session02/6_f118_bodies.py passed (as expected)
=================================================


=================================================
+ echo '7_f118_OUTPMTR.py test;'
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/CAPS/training/2023/training.log
7_f118_OUTPMTR.py test;
+ python 7_f118_OUTPMTR.py
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/CAPS/training/2023/training.log

==&gt; Loading geometry from file "f118-A.csm"...
--&gt; wing:wet      = 9422.222222222223
--&gt; wing:volume   = 9202.959910328365

--&gt; htail:prop[0] = 2660.2506024096383
--&gt; htail:prop[1] = 1652.8901595442062

--&gt; vtail:prop    = [1371.822222222222, None]

--&gt; fuse:wet      = None
--&gt; fuse:volume   = None

Traceback (most recent call last):
  File "/Users/jenkins/workspace/ESP_bPreBuilt/CAPS/training/2023/data/session02/7_f118_OUTPMTR.py", line 34, in &lt;module&gt;
    print ("--&gt; wing:span     =", f118.outpmtr.wing.span )
                                  ^^^^^^^^^^^^^^^^^^^^^^
  File "/Users/jenkins/workspace/ESP_bPreBuilt/ESP126/EngSketchPad/pyESP/pyCAPS/problem.py", line 1954, in __getattr__
    raise AttributeError("No Out Value: {!r}".format(name))
AttributeError: No Out Value: 'span'

real	0m0.222s
user	0m0.271s
sys	0m0.058s
+ status=1
+ set +x

=================================================
data/session02/7_f118_OUTPMTR.py failed (as expected)
=================================================


=================================================
8_f118_Phasing.py test;
+ python 8_f118_Phasing.py
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/CAPS/training/2023/training.log

==&gt; Loading geometry from file "f118-A.csm"...
--&gt; old htail:area =  1210.0
--&gt; new htail:area =  2420.0

==&gt; Bulding and viewing Wide Body geometry...

==&gt; Bulding and viewing geometry from WideBody phase...

==&gt; Bulding and viewing Canard geometry...

real	0m0.295s
user	0m0.361s
sys	0m0.111s
+ status=0
+ set +x

=================================================
data/session02/8_f118_Phasing.py passed (as expected)
=================================================


=================================================
f118_Custom.py test;
+ python f118_Custom.py
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/CAPS/training/2023/training.log

==&gt; Loading geometry from file "../../data/session02/f118-A.csm"...

==&gt; Bulding and viewing geometry...

real	0m0.224s
user	0m0.276s
sys	0m0.059s
+ status=0
+ set +x

=================================================
solutions/session02/f118_Custom.py passed (as expected)
=================================================


=================================================
+ echo 'f118-B.csm test;'
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/CAPS/training/2023/training.log
f118-B.csm test;
+ /Users/jenkins/workspace/ESP_bPreBuilt/ESP126/EngSketchPad/bin/serveESP -batch -verify -outLevel 0 f118-B.csm
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/CAPS/training/2023/training.log
WARNING:: cannot open "./verify_7.8.1/f118-B.vfy", so verification is being skipped
==&gt; serveESP completed successfully with no verification data

real	0m0.102s
user	0m0.103s
sys	0m0.006s
+ status=0
+ set +x

=================================================
data/session03/f118-B          passed (as expected)
=================================================


=================================================
+ echo 'f118-C.csm test;'
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/CAPS/training/2023/training.log
f118-C.csm test;
+ /Users/jenkins/workspace/ESP_bPreBuilt/ESP126/EngSketchPad/bin/serveESP -batch -verify -outLevel 0 f118-C.csm
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/CAPS/training/2023/training.log
WARNING:: cannot open "./verify_7.8.1/f118-C.vfy", so verification is being skipped
==&gt; serveESP completed successfully with no verification data

real	0m0.102s
user	0m0.103s
sys	0m0.006s
+ status=0
+ set +x

=================================================
data/session03/f118-C          passed (as expected)
=================================================


=================================================
+ echo 'naca.csm test;'
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/CAPS/training/2023/training.log
naca.csm test;
+ /Users/jenkins/workspace/ESP_bPreBuilt/ESP126/EngSketchPad/bin/serveESP -batch -verify -outLevel 0 naca.csm
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/CAPS/training/2023/training.log
WARNING:: cannot open "./verify_7.8.1/naca.vfy", so verification is being skipped
==&gt; serveESP completed successfully with no verification data

real	0m0.111s
user	0m0.106s
sys	0m0.006s
+ status=0
+ set +x

=================================================
data/session03/naca            passed (as expected)
=================================================


=================================================
01_xfoil_input.py test;
+ python 01_xfoil_input.py
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/CAPS/training/2023/training.log

==&gt; Loading geometry from file "naca.csm"...

==&gt; Creating xfoilAIM

==&gt; Modified Mach = 0.5

==&gt; Default Alpha = None

==&gt; Modified Alpha = 2.5

==&gt; Modified Alpha = [0.0, 3.0, 5.0, 7.0, 8.0]

==&gt; Unset Alpha = None

 EGADS Info: 0 Objects, 0 Reference in Use (of 0) at Close!

real	0m0.210s
user	0m0.262s
sys	0m0.046s
+ status=0
+ set +x

=================================================
data/session03/01_xfoil_input.py passed (as expected)
=================================================


=================================================
02_xfoil_Analysis.py test;
+ python 02_xfoil_Analysis.py
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/CAPS/training/2023/training.log

==&gt; Loading geometry from file "naca.csm"...

==&gt; Creating xfoilAIM

==&gt; Setting analysis values

==&gt; Running preAnalysis


==&gt; Running xFoil......

==&gt; Running postAnalysis

==&gt; Retrieve analysis results

--&gt; Alpha = [0.0, 3.0, 5.0, 7.0, 8.0]
--&gt; Cl    = [-3.53757125655385e-07, 0.377437462009099, 0.642259371967833, 0.955175653138806, 1.00909750957761]
--&gt; Cd    = [0.00617285380994127, 0.00729426778019113, 0.0100194565543501, 0.0148710807063523, 0.0185150448281103]


real	0m0.595s
user	0m0.839s
sys	0m0.062s
+ status=0
+ set +x

=================================================
data/session03/02_xfoil_Analysis.py passed (as expected)
=================================================


=================================================
03_xfoil_AutoExec.py test;
+ python 03_xfoil_AutoExec.py
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/CAPS/training/2023/training.log

==&gt; Loading geometry from file "naca.csm"...

==&gt; Creating xfoilAIM

==&gt; Setting analysis values

==&gt; Retrieve analysis results

--&gt; Alpha = [0.0, 3.0, 5.0, 7.0, 8.0]
--&gt; Cl    = [-3.53757125655385e-07, 0.377437462009099, 0.642259371967833, 0.955175653138806, 1.00909750957761]
--&gt; Cd    = [0.00617285380994127, 0.00729426778019113, 0.0100194565543501, 0.0148710807063523, 0.0185150448281103]


real	0m0.596s
user	0m0.839s
sys	0m0.064s
+ status=0
+ set +x

=================================================
data/session03/03_xfoil_AutoExec.py passed (as expected)
=================================================


=================================================
04_xfoil_MultiAnalysis.py test;
+ python 04_xfoil_MultiAnalysis.py
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/CAPS/training/2023/training.log

==&gt; Loading geometry from file "naca.csm"...

==&gt; Creating xfoilAIM

==&gt; Setting analysis values

==&gt; Retrieve analysis results

--&gt; Alpha = [0.0, 3.0, 5.0, 7.0, 8.0]
--&gt; Cl    = [-3.53757125655385e-07, 0.377437462009099, 0.642259371967833, 0.955175653138806, 1.00909750957761]
--&gt; Cd    = [0.00617285380994127, 0.00729426778019113, 0.0100194565543501, 0.0148710807063523, 0.0185150448281103]


==&gt; Retrieve analysis results

--&gt; Alpha = [2.87619228202795e-06, 0.789686474041505, 1.18477801663719, 2.37671255179738, 3.18364393502637]
--&gt; Cl    = [-1.68829566253184e-16, 0.1, 0.150000000000232, 0.300000000000164, 0.4]
--&gt; Cd    = [0.00617285381076772, 0.00623021348481478, 0.00630554753827162, 0.00680929883615774, 0.00747424244863518]


real	0m0.834s
user	0m1.062s
sys	0m0.076s
+ status=0
+ set +x

=================================================
data/session03/04_xfoil_MultiAnalysis.py passed (as expected)
=================================================


=================================================
05_xfoil_Camber_Plot.py test;
+ python 05_xfoil_Camber_Plot.py
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/CAPS/training/2023/training.log

==&gt; Loading geometry from file "naca.csm"...

==&gt; Creating xfoilAIM

==&gt; Setting analysis values

==&gt; Retrieve analysis results. camber =  0.0

==&gt; Retrieve analysis results. camber =  0.01

==&gt; Retrieve analysis results. camber =  0.04

==&gt; Retrieve analysis results. camber =  0.07

==&gt; Plotting analysis results (close plot window to finish Python script
/Users/jenkins/workspace/ESP_bPreBuilt/CAPS/training/2023/data/session03/05_xfoil_Camber_Plot.py:65: UserWarning: FigureCanvasAgg is non-interactive, and thus cannot be shown
  plt.show()

real	0m3.310s
user	0m3.488s
sys	0m0.117s
+ status=0
+ set +x

=================================================
data/session03/05_xfoil_Camber_Plot.py passed (as expected)
=================================================


=================================================
05_xfoil_Camber.py test;
+ python 05_xfoil_Camber.py
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/CAPS/training/2023/training.log

==&gt; Loading geometry from file "naca.csm"...

==&gt; Creating xfoilAIM

==&gt; Setting analysis values

==&gt; Retrieve analysis results. camber =  0.0

==&gt; Retrieve analysis results. camber =  0.01

==&gt; Retrieve analysis results. camber =  0.04

==&gt; Retrieve analysis results. camber =  0.07

--&gt; Cambers = [0.0, 0.01, 0.04, 0.07]
--&gt; Alpha   = [[0.0, 1.0, 3.0], [0.0, 1.0, 3.0], [0.0, 1.0, 3.0], [0.0, 1.0]]
--&gt; Cl      = [[-3.53757125655385e-07, 0.126697477361167, 0.377437462181223], [0.140339949737382, 0.266469023977517, 0.514670926888889], [0.554542727545724, 0.680708956698588, 0.940291957324874], [0.919771481559598, 1.03861131519228]]
--&gt; Cd      = [[0.00617285380994127, 0.00627268560115845, 0.00729426778762296], [0.00625861871528683, 0.00622635244563391, 0.00706717658622291], [0.00787687247022521, 0.00739456756394117, 0.00782133651724681], [0.00972065010479203, 0.0101041953398598]]


real	0m1.624s
user	0m1.821s
sys	0m0.102s
+ status=0
+ set +x

=================================================
data/session03/05_xfoil_Camber.py passed (as expected)
=================================================


=================================================
06_xfoil_CleanDirty.py test;
+ python 06_xfoil_CleanDirty.py
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/CAPS/training/2023/training.log

==&gt; Loading geometry from file "naca.csm"...

==&gt; Creating xfoilAIM

1. No Errors  --------------------------------------------------------------------------------

==&gt; Setting alpha sequence

==&gt; Running preAnalysis


==&gt; Running xFoil......

==&gt; Running postAnalysis

--&gt; Cl    = [-3.53757125655385e-07, 0.377437462009099, 0.642259371967833, 0.955175653138806, 1.00909750957761]

2. DIRTY AnalysisVal Error  --------------------------------------------------------------------------------

==&gt; Setting new alpha sequence

==&gt; Attempting to get Cl

==&gt; CAPSError = CAPS_DIRTY:
================================================================================
================================================================================


==&gt; Running preAnalysis


==&gt; Running xFoil......

==&gt; Running postAnalysis

==&gt; Attempting to get Cl

--&gt; Cl    = 0.252764696628542

3. DIRTY GeometryVal Error  --------------------------------------------------------------------------------

==&gt; Modifying camber

==&gt; Attempting to get Cl

==&gt; CAPSError = CAPS_DIRTY:
================================================================================
================================================================================


==&gt; Running preAnalysis


==&gt; Running xFoil......

==&gt; Running postAnalysis

==&gt; Attempting to get Cl

--&gt; Cl    = [1.03861130997329, 1.15325582947796]

4. DIRTY pre- but no postAnalysis Error  --------------------------------------------------------------------------------

==&gt; Modifying Mach

==&gt; Running preAnalysis but not running postAnalysis

==&gt; Attempting to get Cl

==&gt; CAPSError = CAPS_DIRTY:
================================================================================
================================================================================



==&gt; Running xFoil......

==&gt; Running postAnalysis

==&gt; Attempting to get Cl

--&gt; Cl    = [0.967203918355951, 1.07899610948977]

5. CLEAN Error  --------------------------------------------------------------------------------

==&gt; Running preAnalysis

==&gt; CAPSError = CAPS_CLEAN:
================================================================================
================================================================================


real	0m1.491s
user	0m1.680s
sys	0m0.101s
+ status=0
+ set +x

=================================================
data/session03/06_xfoil_CleanDirty.py passed (as expected)
=================================================


=================================================
07_masstran_f118_AIM.py test;
+ python 07_masstran_f118_AIM.py
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/CAPS/training/2023/training.log

==&gt; Loading geometry from file "f118-B.csm"...
==&gt; Geometry used by masstranAll instance with no capsIntent
==&gt; Geometry used by Wing instance with capsIntent='wing'
==&gt; Geometry used by Tail instance with capsIntent='tail'
==&gt; Geometry used by WingFuse instance with capsIntent=['wing','fuse']

real	0m0.466s
user	0m0.495s
sys	0m0.273s
+ status=0
+ set +x

=================================================
data/session03/07_masstran_f118_AIM.py passed (as expected)
=================================================


=================================================
08_masstran_f118_Wing.py test;
+ python 08_masstran_f118_Wing.py
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/CAPS/training/2023/training.log

==&gt; Loading geometry from file "f118-C.csm"...
Mapping Csys attributes ................
	Number of unique Csys attributes = 0

Getting FEA coordinate systems.......
	Number of coordinate systems - 0
	No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
	Number of unique capsConstraint attributes = 0
Mapping capsLoad attributes ................
	Number of unique capsLoad attributes = 0
Mapping capsBound attributes ................
	Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
	Number of unique capsConnect attributes = 0
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = wing:faces, index = 1
Setting FEA Data
	Mesh for body = 0
	Number of nodal coordinates = 900
	Number of elements = 1796
	Elemental Nodes = 0
	Elemental Rods  = 0
	Elemental Tria3 = 1796
	Elemental Quad4 = 0

Getting FEA materials.......
	Number of materials - 1
	Material name - Unobtainium
	No "materialType" specified for Material tuple Unobtainium, defaulting to "Isotropic"
	Done getting FEA materials

Getting FEA properties.......
	Number of properties - 1
	Property name - wing:faces
	Done getting FEA properties
Updating mesh element types based on properties input

--&gt; Mass = 14792888.88889
--&gt; CG   = [64.85254706407, 3.3674366504e-14, -3.914745293593]

real	0m0.297s
user	0m0.358s
sys	0m0.122s
+ status=0
+ set +x

=================================================
data/session03/08_masstran_f118_Wing.py passed (as expected)
=================================================


=================================================
09_masstran_f118.py test;
+ python 09_masstran_f118.py
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/CAPS/training/2023/training.log

==&gt; Loading geometry from file "f118-C.csm"...
Mapping Csys attributes ................
	Number of unique Csys attributes = 0

Getting FEA coordinate systems.......
	Number of coordinate systems - 0
	No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
	Number of unique capsConstraint attributes = 0
Mapping capsLoad attributes ................
	Number of unique capsLoad attributes = 0
Mapping capsBound attributes ................
	Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
	Number of unique capsConnect attributes = 0
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 6
	Name = wing:faces, index = 1
	Name = htail:faces, index = 2
	Name = vtail:faces, index = 3
	Name = fuse:nose, index = 4
	Name = fuse:tail, index = 5
	Name = fuse:side, index = 6
Setting FEA Data
	Mesh for body = 0
	Number of nodal coordinates = 900
	Number of elements = 1796
	Elemental Nodes = 0
	Elemental Rods  = 0
	Elemental Tria3 = 1796
	Elemental Quad4 = 0
Setting FEA Data
	Mesh for body = 1
	Number of nodal coordinates = 170
	Number of elements = 336
	Elemental Nodes = 0
	Elemental Rods  = 0
	Elemental Tria3 = 336
	Elemental Quad4 = 0
Setting FEA Data
	Mesh for body = 2
	Number of nodal coordinates = 90
	Number of elements = 176
	Elemental Nodes = 0
	Elemental Rods  = 0
	Elemental Tria3 = 176
	Elemental Quad4 = 0
Setting FEA Data
	Mesh for body = 3
	Number of nodal coordinates = 1698
	Number of elements = 3392
	Elemental Nodes = 0
	Elemental Rods  = 0
	Elemental Tria3 = 3392
	Elemental Quad4 = 0
Combining multiple FEA meshes!
	Combined Number of nodal coordinates = 2858
	Combined Number of elements = 5700
	Combined Elemental Nodes = 0
	Combined Elemental Rods  = 0
	Combined Elemental Tria3 = 5700
	Combined Elemental Quad4 = 0

Getting FEA materials.......
	Number of materials - 2
	Material name - Madeupium
	No "materialType" specified for Material tuple Madeupium, defaulting to "Isotropic"
	Material name - Unobtainium
	No "materialType" specified for Material tuple Unobtainium, defaulting to "Isotropic"
	Done getting FEA materials

Getting FEA properties.......
	Number of properties - 6
	Property name - fuse:nose
	Property name - fuse:side
	Property name - fuse:tail
	Property name - htail:faces
	Property name - vtail:faces
	Property name - wing:faces
	Done getting FEA properties
Updating mesh element types based on properties input

--&gt;Mass = 52825838.86801
--&gt;CG   = [91.69615213878, 5.294802100603e-15, 0.7254947287442]

real	0m0.303s
user	0m0.368s
sys	0m0.123s
+ status=0
+ set +x

=================================================
data/session03/09_masstran_f118.py passed (as expected)
=================================================


=================================================
10_masstran_f118_journal.py test;
+ python 10_masstran_f118_journal.py
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/CAPS/training/2023/training.log

################################################################################
==&gt; First execution

==&gt; Loading geometry from file "f118-C.csm"...
================================================================================
==&gt; Computing mass 1
Mapping Csys attributes ................
	Number of unique Csys attributes = 0

Getting FEA coordinate systems.......
	Number of coordinate systems - 0
	No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
	Number of unique capsConstraint attributes = 0
Mapping capsLoad attributes ................
	Number of unique capsLoad attributes = 0
Mapping capsBound attributes ................
	Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
	Number of unique capsConnect attributes = 0
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = wing:faces, index = 1
Setting FEA Data
	Mesh for body = 0
	Number of nodal coordinates = 488
	Number of elements = 972
	Elemental Nodes = 0
	Elemental Rods  = 0
	Elemental Tria3 = 972
	Elemental Quad4 = 0

Getting FEA materials.......
	Number of materials - 1
	Material name - Unobtainium
	No "materialType" specified for Material tuple Unobtainium, defaulting to "Isotropic"
	Done getting FEA materials

Getting FEA properties.......
	Number of properties - 1
	Property name - wing:faces
	Done getting FEA properties
Updating mesh element types based on properties input
--&gt; 14792888.88889
Something went wrong!

################################################################################
==&gt; Second execution

==&gt; Loading geometry from file "f118-C.csm"...
================================================================================
==&gt; Computing mass 1
--&gt; 14792888.88889
 CAPS Info: Hit last success -- going live!
================================================================================
==&gt; Computing mass 2
Mapping Csys attributes ................
	Number of unique Csys attributes = 0

Getting FEA coordinate systems.......
	Number of coordinate systems - 0
	No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
	Number of unique capsConstraint attributes = 0
Mapping capsLoad attributes ................
	Number of unique capsLoad attributes = 0
Mapping capsBound attributes ................
	Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
	Number of unique capsConnect attributes = 0
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = wing:faces, index = 1
Setting FEA Data
	Mesh for body = 0
	Number of nodal coordinates = 488
	Number of elements = 972
	Elemental Nodes = 0
	Elemental Rods  = 0
	Elemental Tria3 = 972
	Elemental Quad4 = 0

Getting FEA materials.......
	Number of materials - 1
	Material name - Unobtainium
	No "materialType" specified for Material tuple Unobtainium, defaulting to "Isotropic"
	Done getting FEA materials

Getting FEA properties.......
	Number of properties - 1
	Property name - wing:faces
	Done getting FEA properties
Updating mesh element types based on properties input
--&gt; 1479288.888889
Something went wrong!

################################################################################
==&gt; Third execution

==&gt; Loading geometry from file "f118-C.csm"...
================================================================================
==&gt; Computing mass 1
--&gt; 14792888.88889
================================================================================
==&gt; Computing mass 2
--&gt; 1479288.888889
 CAPS Info: Hit last success -- going live!
================================================================================
==&gt; Computing mass 3
Mapping Csys attributes ................
	Number of unique Csys attributes = 0

Getting FEA coordinate systems.......
	Number of coordinate systems - 0
	No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
	Number of unique capsConstraint attributes = 0
Mapping capsLoad attributes ................
	Number of unique capsLoad attributes = 0
Mapping capsBound attributes ................
	Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
	Number of unique capsConnect attributes = 0
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = wing:faces, index = 1
Setting FEA Data
	Mesh for body = 0
	Number of nodal coordinates = 488
	Number of elements = 972
	Elemental Nodes = 0
	Elemental Rods  = 0
	Elemental Tria3 = 972
	Elemental Quad4 = 0

Getting FEA materials.......
	Number of materials - 1
	Material name - Unobtainium
	No "materialType" specified for Material tuple Unobtainium, defaulting to "Isotropic"
	Done getting FEA materials

Getting FEA properties.......
	Number of properties - 1
	Property name - wing:faces
	Done getting FEA properties
Updating mesh element types based on properties input
--&gt; 147928.8888889

################################################################################
==&gt; Fourth execution

==&gt; Loading geometry from file "f118-C.csm"...
================================================================================
==&gt; Computing mass 1
--&gt; 14792888.88889
================================================================================
==&gt; Computing mass 2
--&gt; 1479288.888889
================================================================================
==&gt; Computing mass 3
--&gt; 147928.8888889

real	0m0.344s
user	0m0.426s
sys	0m0.147s
+ status=0
+ set +x

=================================================
data/session03/10_masstran_f118_journal.py passed (as expected)
=================================================


=================================================
+ echo 'f118-C.csm test;'
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/CAPS/training/2023/training.log
f118-C.csm test;
+ /Users/jenkins/workspace/ESP_bPreBuilt/ESP126/EngSketchPad/bin/serveESP -batch -verify -outLevel 0 f118-C.csm
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/CAPS/training/2023/training.log
WARNING:: cannot open "./verify_7.8.1/f118-C.vfy", so verification is being skipped
==&gt; serveESP completed successfully with no verification data

real	0m0.102s
user	0m0.103s
sys	0m0.006s
+ status=0
+ set +x

=================================================
solutions/session03/f118-C     passed (as expected)
=================================================


=================================================
xfoil_thickness.py test;
+ python xfoil_thickness.py
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/CAPS/training/2023/training.log

==&gt; Loading geometry from file "../../data/session03/naca.csm"...

==&gt; Create xfoilAIM

==&gt; Setting analysis values

==&gt; Retrieve analysis results

==&gt; Retrieve analysis results

==&gt; Retrieve analysis results

==&gt; Retrieve analysis results

--&gt; Thickness = [0.08, 0.1, 0.12, 0.16]
--&gt; Alpha     = [[0.0, 1.0, 3.0], [0.0, 1.0, 3.0], [0.0, 1.0, 3.0], [0.0, 1.0, 3.0]]
--&gt; Cl        = [[4.33419461234289e-07, 0.118003705247125, 0.4078230913009], [3.88197275319707e-07, 0.12399312361356, 0.371340021267165], [-3.53757125655385e-07, 0.126697477361167, 0.377437462181223], [2.73507879809025e-07, 0.127624319978928, 0.380868543480744]]
--&gt; Cd        = [[0.00449613835213978, 0.00482192214520964, 0.00769709940290085], [0.00540044826496585, 0.0055477373653873, 0.00718424709040834], [0.00617285380994127, 0.00627268560115845, 0.00729426778762296], [0.00752780925536514, 0.0075937493874947, 0.00822813502005816]]


real	0m0.934s
user	0m1.136s
sys	0m0.098s
+ status=0
+ set +x

=================================================
solutions/session03/xfoil_thickness.py passed (as expected)
=================================================


=================================================
f118_masstran.py test;
+ python f118_masstran.py
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/CAPS/training/2023/training.log

==&gt; Loading geometry from file "../../data/session03/f118-B.csm"...
==&gt; Geometry with capsIntent=['wing','fuse', 'htail']

real	0m0.281s
user	0m0.337s
sys	0m0.110s
+ status=0
+ set +x

=================================================
solutions/session03/f118_masstran.py passed (as expected)
=================================================


=================================================
masstran_topbot.py test;
+ python masstran_topbot.py
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/CAPS/training/2023/training.log

==&gt; Loading geometry from file "f118-C.csm"...
Mapping Csys attributes ................
	Number of unique Csys attributes = 0

Getting FEA coordinate systems.......
	Number of coordinate systems - 0
	No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
	Number of unique capsConstraint attributes = 0
Mapping capsLoad attributes ................
	Number of unique capsLoad attributes = 0
Mapping capsBound attributes ................
	Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
	Number of unique capsConnect attributes = 0
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 8
	Name = wing:faces, index = 1
	Name = htail:faces, index = 2
	Name = vtail:faces, index = 3
	Name = fuse:nose, index = 4
	Name = fuse:tail, index = 5
	Name = fuse:side, index = 6
	Name = fuse:bottom, index = 7
	Name = fuse:top, index = 8
Setting FEA Data
	Mesh for body = 0
	Number of nodal coordinates = 900
	Number of elements = 1796
	Elemental Nodes = 0
	Elemental Rods  = 0
	Elemental Tria3 = 1796
	Elemental Quad4 = 0
Setting FEA Data
	Mesh for body = 1
	Number of nodal coordinates = 170
	Number of elements = 336
	Elemental Nodes = 0
	Elemental Rods  = 0
	Elemental Tria3 = 336
	Elemental Quad4 = 0
Setting FEA Data
	Mesh for body = 2
	Number of nodal coordinates = 90
	Number of elements = 176
	Elemental Nodes = 0
	Elemental Rods  = 0
	Elemental Tria3 = 176
	Elemental Quad4 = 0
Setting FEA Data
	Mesh for body = 3
	Number of nodal coordinates = 1698
	Number of elements = 3392
	Elemental Nodes = 0
	Elemental Rods  = 0
	Elemental Tria3 = 3392
	Elemental Quad4 = 0
Combining multiple FEA meshes!
	Combined Number of nodal coordinates = 2858
	Combined Number of elements = 5700
	Combined Elemental Nodes = 0
	Combined Elemental Rods  = 0
	Combined Elemental Tria3 = 5700
	Combined Elemental Quad4 = 0

Getting FEA materials.......
	Number of materials - 2
	Material name - Madeupium
	No "materialType" specified for Material tuple Madeupium, defaulting to "Isotropic"
	Material name - Unobtainium
	No "materialType" specified for Material tuple Unobtainium, defaulting to "Isotropic"
	Done getting FEA materials

Getting FEA properties.......
	Number of properties - 8
	Property name - fuse:bottom
	Property name - fuse:nose
	Property name - fuse:side
	Property name - fuse:tail
	Property name - fuse:top
	Property name - htail:faces
	Property name - vtail:faces
	Property name - wing:faces
	Done getting FEA properties
Updating mesh element types based on properties input

--&gt;Mass = 52073438.86801
--&gt;CG   = [91.72065954403, 0.04009689171826, 0.1932821772294]

real	0m0.317s
user	0m0.384s
sys	0m0.138s
+ status=0
+ set +x

=================================================
solutions/session03/masstran_topbot.py passed (as expected)
=================================================


=================================================
masstran_CG.py test;
+ python masstran_CG.py
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/CAPS/training/2023/training.log

==&gt; Loading geometry from file "f118-C.csm"...
Mapping Csys attributes ................
	Number of unique Csys attributes = 0

Getting FEA coordinate systems.......
	Number of coordinate systems - 0
	No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
	Number of unique capsConstraint attributes = 0
Mapping capsLoad attributes ................
	Number of unique capsLoad attributes = 0
Mapping capsBound attributes ................
	Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
	Number of unique capsConnect attributes = 0
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 8
	Name = wing:faces, index = 1
	Name = htail:faces, index = 2
	Name = vtail:faces, index = 3
	Name = fuse:nose, index = 4
	Name = fuse:tail, index = 5
	Name = fuse:side, index = 6
	Name = fuse:bottom, index = 7
	Name = fuse:top, index = 8
Setting FEA Data
	Mesh for body = 0
	Number of nodal coordinates = 900
	Number of elements = 1796
	Elemental Nodes = 0
	Elemental Rods  = 0
	Elemental Tria3 = 1796
	Elemental Quad4 = 0
Setting FEA Data
	Mesh for body = 1
	Number of nodal coordinates = 170
	Number of elements = 336
	Elemental Nodes = 0
	Elemental Rods  = 0
	Elemental Tria3 = 336
	Elemental Quad4 = 0
Setting FEA Data
	Mesh for body = 2
	Number of nodal coordinates = 90
	Number of elements = 176
	Elemental Nodes = 0
	Elemental Rods  = 0
	Elemental Tria3 = 176
	Elemental Quad4 = 0
Setting FEA Data
	Mesh for body = 3
	Number of nodal coordinates = 1698
	Number of elements = 3392
	Elemental Nodes = 0
	Elemental Rods  = 0
	Elemental Tria3 = 3392
	Elemental Quad4 = 0
Combining multiple FEA meshes!
	Combined Number of nodal coordinates = 2858
	Combined Number of elements = 5700
	Combined Elemental Nodes = 0
	Combined Elemental Rods  = 0
	Combined Elemental Tria3 = 5700
	Combined Elemental Quad4 = 0

Getting FEA materials.......
	Number of materials - 2
	Material name - Madeupium
	No "materialType" specified for Material tuple Madeupium, defaulting to "Isotropic"
	Material name - Unobtainium
	No "materialType" specified for Material tuple Unobtainium, defaulting to "Isotropic"
	Done getting FEA materials

Getting FEA properties.......
	Number of properties - 8
	Property name - fuse:bottom
	Property name - fuse:nose
	Property name - fuse:side
	Property name - fuse:tail
	Property name - fuse:top
	Property name - htail:faces
	Property name - vtail:faces
	Property name - wing:faces
	Done getting FEA properties
Updating mesh element types based on properties input
Mapping Csys attributes ................
	Number of unique Csys attributes = 0

Getting FEA coordinate systems.......
	Number of coordinate systems - 0
	No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
	Number of unique capsConstraint attributes = 0
Mapping capsLoad attributes ................
	Number of unique capsLoad attributes = 0
Mapping capsBound attributes ................
	Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
	Number of unique capsConnect attributes = 0
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 8
	Name = wing:faces, index = 1
	Name = htail:faces, index = 2
	Name = vtail:faces, index = 3
	Name = fuse:nose, index = 4
	Name = fuse:tail, index = 5
	Name = fuse:side, index = 6
	Name = fuse:bottom, index = 7
	Name = fuse:top, index = 8
Setting FEA Data
	Mesh for body = 0
	Number of nodal coordinates = 900
	Number of elements = 1796
	Elemental Nodes = 0
	Elemental Rods  = 0
	Elemental Tria3 = 1796
	Elemental Quad4 = 0
Setting FEA Data
	Mesh for body = 1
	Number of nodal coordinates = 170
	Number of elements = 336
	Elemental Nodes = 0
	Elemental Rods  = 0
	Elemental Tria3 = 336
	Elemental Quad4 = 0
Setting FEA Data
	Mesh for body = 2
	Number of nodal coordinates = 90
	Number of elements = 176
	Elemental Nodes = 0
	Elemental Rods  = 0
	Elemental Tria3 = 176
	Elemental Quad4 = 0
Setting FEA Data
	Mesh for body = 3
	Number of nodal coordinates = 1698
	Number of elements = 3392
	Elemental Nodes = 0
	Elemental Rods  = 0
	Elemental Tria3 = 3392
	Elemental Quad4 = 0
Combining multiple FEA meshes!
	Combined Number of nodal coordinates = 2858
	Combined Number of elements = 5700
	Combined Elemental Nodes = 0
	Combined Elemental Rods  = 0
	Combined Elemental Tria3 = 5700
	Combined Elemental Quad4 = 0
Updating mesh element types based on properties input
Mapping Csys attributes ................
	Number of unique Csys attributes = 0

Getting FEA coordinate systems.......
	Number of coordinate systems - 0
	No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
	Number of unique capsConstraint attributes = 0
Mapping capsLoad attributes ................
	Number of unique capsLoad attributes = 0
Mapping capsBound attributes ................
	Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
	Number of unique capsConnect attributes = 0
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 8
	Name = wing:faces, index = 1
	Name = htail:faces, index = 2
	Name = vtail:faces, index = 3
	Name = fuse:nose, index = 4
	Name = fuse:tail, index = 5
	Name = fuse:side, index = 6
	Name = fuse:bottom, index = 7
	Name = fuse:top, index = 8
Setting FEA Data
	Mesh for body = 0
	Number of nodal coordinates = 900
	Number of elements = 1796
	Elemental Nodes = 0
	Elemental Rods  = 0
	Elemental Tria3 = 1796
	Elemental Quad4 = 0
Setting FEA Data
	Mesh for body = 1
	Number of nodal coordinates = 170
	Number of elements = 336
	Elemental Nodes = 0
	Elemental Rods  = 0
	Elemental Tria3 = 336
	Elemental Quad4 = 0
Setting FEA Data
	Mesh for body = 2
	Number of nodal coordinates = 90
	Number of elements = 176
	Elemental Nodes = 0
	Elemental Rods  = 0
	Elemental Tria3 = 176
	Elemental Quad4 = 0
Setting FEA Data
	Mesh for body = 3
	Number of nodal coordinates = 1698
	Number of elements = 3392
	Elemental Nodes = 0
	Elemental Rods  = 0
	Elemental Tria3 = 3392
	Elemental Quad4 = 0
Combining multiple FEA meshes!
	Combined Number of nodal coordinates = 2858
	Combined Number of elements = 5700
	Combined Elemental Nodes = 0
	Combined Elemental Rods  = 0
	Combined Elemental Tria3 = 5700
	Combined Elemental Quad4 = 0
Updating mesh element types based on properties input
Mapping Csys attributes ................
	Number of unique Csys attributes = 0

Getting FEA coordinate systems.......
	Number of coordinate systems - 0
	No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
	Number of unique capsConstraint attributes = 0
Mapping capsLoad attributes ................
	Number of unique capsLoad attributes = 0
Mapping capsBound attributes ................
	Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
	Number of unique capsConnect attributes = 0
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 8
	Name = wing:faces, index = 1
	Name = htail:faces, index = 2
	Name = vtail:faces, index = 3
	Name = fuse:nose, index = 4
	Name = fuse:tail, index = 5
	Name = fuse:side, index = 6
	Name = fuse:bottom, index = 7
	Name = fuse:top, index = 8
Setting FEA Data
	Mesh for body = 0
	Number of nodal coordinates = 900
	Number of elements = 1796
	Elemental Nodes = 0
	Elemental Rods  = 0
	Elemental Tria3 = 1796
	Elemental Quad4 = 0
Setting FEA Data
	Mesh for body = 1
	Number of nodal coordinates = 170
	Number of elements = 336
	Elemental Nodes = 0
	Elemental Rods  = 0
	Elemental Tria3 = 336
	Elemental Quad4 = 0
Setting FEA Data
	Mesh for body = 2
	Number of nodal coordinates = 90
	Number of elements = 176
	Elemental Nodes = 0
	Elemental Rods  = 0
	Elemental Tria3 = 176
	Elemental Quad4 = 0
Setting FEA Data
	Mesh for body = 3
	Number of nodal coordinates = 1698
	Number of elements = 3392
	Elemental Nodes = 0
	Elemental Rods  = 0
	Elemental Tria3 = 3392
	Elemental Quad4 = 0
Combining multiple FEA meshes!
	Combined Number of nodal coordinates = 2858
	Combined Number of elements = 5700
	Combined Elemental Nodes = 0
	Combined Elemental Rods  = 0
	Combined Elemental Tria3 = 5700
	Combined Elemental Quad4 = 0
Updating mesh element types based on properties input
Mapping Csys attributes ................
	Number of unique Csys attributes = 0

Getting FEA coordinate systems.......
	Number of coordinate systems - 0
	No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
	Number of unique capsConstraint attributes = 0
Mapping capsLoad attributes ................
	Number of unique capsLoad attributes = 0
Mapping capsBound attributes ................
	Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
	Number of unique capsConnect attributes = 0
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 8
	Name = wing:faces, index = 1
	Name = htail:faces, index = 2
	Name = vtail:faces, index = 3
	Name = fuse:nose, index = 4
	Name = fuse:tail, index = 5
	Name = fuse:side, index = 6
	Name = fuse:bottom, index = 7
	Name = fuse:top, index = 8
Setting FEA Data
	Mesh for body = 0
	Number of nodal coordinates = 900
	Number of elements = 1796
	Elemental Nodes = 0
	Elemental Rods  = 0
	Elemental Tria3 = 1796
	Elemental Quad4 = 0
Setting FEA Data
	Mesh for body = 1
	Number of nodal coordinates = 170
	Number of elements = 336
	Elemental Nodes = 0
	Elemental Rods  = 0
	Elemental Tria3 = 336
	Elemental Quad4 = 0
Setting FEA Data
	Mesh for body = 2
	Number of nodal coordinates = 90
	Number of elements = 176
	Elemental Nodes = 0
	Elemental Rods  = 0
	Elemental Tria3 = 176
	Elemental Quad4 = 0
Setting FEA Data
	Mesh for body = 3
	Number of nodal coordinates = 1698
	Number of elements = 3392
	Elemental Nodes = 0
	Elemental Rods  = 0
	Elemental Tria3 = 3392
	Elemental Quad4 = 0
Combining multiple FEA meshes!
	Combined Number of nodal coordinates = 2858
	Combined Number of elements = 5700
	Combined Elemental Nodes = 0
	Combined Elemental Rods  = 0
	Combined Elemental Tria3 = 5700
	Combined Elemental Quad4 = 0
Updating mesh element types based on properties input
Mapping Csys attributes ................
	Number of unique Csys attributes = 0

Getting FEA coordinate systems.......
	Number of coordinate systems - 0
	No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
	Number of unique capsConstraint attributes = 0
Mapping capsLoad attributes ................
	Number of unique capsLoad attributes = 0
Mapping capsBound attributes ................
	Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
	Number of unique capsConnect attributes = 0
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 8
	Name = wing:faces, index = 1
	Name = htail:faces, index = 2
	Name = vtail:faces, index = 3
	Name = fuse:nose, index = 4
	Name = fuse:tail, index = 5
	Name = fuse:side, index = 6
	Name = fuse:bottom, index = 7
	Name = fuse:top, index = 8
Setting FEA Data
	Mesh for body = 0
	Number of nodal coordinates = 900
	Number of elements = 1796
	Elemental Nodes = 0
	Elemental Rods  = 0
	Elemental Tria3 = 1796
	Elemental Quad4 = 0
Setting FEA Data
	Mesh for body = 1
	Number of nodal coordinates = 170
	Number of elements = 336
	Elemental Nodes = 0
	Elemental Rods  = 0
	Elemental Tria3 = 336
	Elemental Quad4 = 0
Setting FEA Data
	Mesh for body = 2
	Number of nodal coordinates = 90
	Number of elements = 176
	Elemental Nodes = 0
	Elemental Rods  = 0
	Elemental Tria3 = 176
	Elemental Quad4 = 0
Setting FEA Data
	Mesh for body = 3
	Number of nodal coordinates = 1698
	Number of elements = 3392
	Elemental Nodes = 0
	Elemental Rods  = 0
	Elemental Tria3 = 3392
	Elemental Quad4 = 0
Combining multiple FEA meshes!
	Combined Number of nodal coordinates = 2858
	Combined Number of elements = 5700
	Combined Elemental Nodes = 0
	Combined Elemental Rods  = 0
	Combined Elemental Tria3 = 5700
	Combined Elemental Quad4 = 0
Updating mesh element types based on properties input
Mapping Csys attributes ................
	Number of unique Csys attributes = 0

Getting FEA coordinate systems.......
	Number of coordinate systems - 0
	No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
	Number of unique capsConstraint attributes = 0
Mapping capsLoad attributes ................
	Number of unique capsLoad attributes = 0
Mapping capsBound attributes ................
	Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
	Number of unique capsConnect attributes = 0
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 8
	Name = wing:faces, index = 1
	Name = htail:faces, index = 2
	Name = vtail:faces, index = 3
	Name = fuse:nose, index = 4
	Name = fuse:tail, index = 5
	Name = fuse:side, index = 6
	Name = fuse:bottom, index = 7
	Name = fuse:top, index = 8
Setting FEA Data
	Mesh for body = 0
	Number of nodal coordinates = 900
	Number of elements = 1796
	Elemental Nodes = 0
	Elemental Rods  = 0
	Elemental Tria3 = 1796
	Elemental Quad4 = 0
Setting FEA Data
	Mesh for body = 1
	Number of nodal coordinates = 170
	Number of elements = 336
	Elemental Nodes = 0
	Elemental Rods  = 0
	Elemental Tria3 = 336
	Elemental Quad4 = 0
Setting FEA Data
	Mesh for body = 2
	Number of nodal coordinates = 90
	Number of elements = 176
	Elemental Nodes = 0
	Elemental Rods  = 0
	Elemental Tria3 = 176
	Elemental Quad4 = 0
Setting FEA Data
	Mesh for body = 3
	Number of nodal coordinates = 1698
	Number of elements = 3392
	Elemental Nodes = 0
	Elemental Rods  = 0
	Elemental Tria3 = 3392
	Elemental Quad4 = 0
Combining multiple FEA meshes!
	Combined Number of nodal coordinates = 2858
	Combined Number of elements = 5700
	Combined Elemental Nodes = 0
	Combined Elemental Rods  = 0
	Combined Elemental Tria3 = 5700
	Combined Elemental Quad4 = 0
Updating mesh element types based on properties input
Mapping Csys attributes ................
	Number of unique Csys attributes = 0

Getting FEA coordinate systems.......
	Number of coordinate systems - 0
	No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
	Number of unique capsConstraint attributes = 0
Mapping capsLoad attributes ................
	Number of unique capsLoad attributes = 0
Mapping capsBound attributes ................
	Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
	Number of unique capsConnect attributes = 0
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 8
	Name = wing:faces, index = 1
	Name = htail:faces, index = 2
	Name = vtail:faces, index = 3
	Name = fuse:nose, index = 4
	Name = fuse:tail, index = 5
	Name = fuse:side, index = 6
	Name = fuse:bottom, index = 7
	Name = fuse:top, index = 8
Setting FEA Data
	Mesh for body = 0
	Number of nodal coordinates = 900
	Number of elements = 1796
	Elemental Nodes = 0
	Elemental Rods  = 0
	Elemental Tria3 = 1796
	Elemental Quad4 = 0
Setting FEA Data
	Mesh for body = 1
	Number of nodal coordinates = 170
	Number of elements = 336
	Elemental Nodes = 0
	Elemental Rods  = 0
	Elemental Tria3 = 336
	Elemental Quad4 = 0
Setting FEA Data
	Mesh for body = 2
	Number of nodal coordinates = 90
	Number of elements = 176
	Elemental Nodes = 0
	Elemental Rods  = 0
	Elemental Tria3 = 176
	Elemental Quad4 = 0
Setting FEA Data
	Mesh for body = 3
	Number of nodal coordinates = 1698
	Number of elements = 3392
	Elemental Nodes = 0
	Elemental Rods  = 0
	Elemental Tria3 = 3392
	Elemental Quad4 = 0
Combining multiple FEA meshes!
	Combined Number of nodal coordinates = 2858
	Combined Number of elements = 5700
	Combined Elemental Nodes = 0
	Combined Elemental Rods  = 0
	Combined Elemental Tria3 = 5700
	Combined Elemental Quad4 = 0
Updating mesh element types based on properties input
Mapping Csys attributes ................
	Number of unique Csys attributes = 0

Getting FEA coordinate systems.......
	Number of coordinate systems - 0
	No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
	Number of unique capsConstraint attributes = 0
Mapping capsLoad attributes ................
	Number of unique capsLoad attributes = 0
Mapping capsBound attributes ................
	Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
	Number of unique capsConnect attributes = 0
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 8
	Name = wing:faces, index = 1
	Name = htail:faces, index = 2
	Name = vtail:faces, index = 3
	Name = fuse:nose, index = 4
	Name = fuse:tail, index = 5
	Name = fuse:side, index = 6
	Name = fuse:bottom, index = 7
	Name = fuse:top, index = 8
Setting FEA Data
	Mesh for body = 0
	Number of nodal coordinates = 900
	Number of elements = 1796
	Elemental Nodes = 0
	Elemental Rods  = 0
	Elemental Tria3 = 1796
	Elemental Quad4 = 0
Setting FEA Data
	Mesh for body = 1
	Number of nodal coordinates = 170
	Number of elements = 336
	Elemental Nodes = 0
	Elemental Rods  = 0
	Elemental Tria3 = 336
	Elemental Quad4 = 0
Setting FEA Data
	Mesh for body = 2
	Number of nodal coordinates = 90
	Number of elements = 176
	Elemental Nodes = 0
	Elemental Rods  = 0
	Elemental Tria3 = 176
	Elemental Quad4 = 0
Setting FEA Data
	Mesh for body = 3
	Number of nodal coordinates = 1698
	Number of elements = 3392
	Elemental Nodes = 0
	Elemental Rods  = 0
	Elemental Tria3 = 3392
	Elemental Quad4 = 0
Combining multiple FEA meshes!
	Combined Number of nodal coordinates = 2858
	Combined Number of elements = 5700
	Combined Elemental Nodes = 0
	Combined Elemental Rods  = 0
	Combined Elemental Tria3 = 5700
	Combined Elemental Quad4 = 0
Updating mesh element types based on properties input
Mapping Csys attributes ................
	Number of unique Csys attributes = 0

Getting FEA coordinate systems.......
	Number of coordinate systems - 0
	No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
	Number of unique capsConstraint attributes = 0
Mapping capsLoad attributes ................
	Number of unique capsLoad attributes = 0
Mapping capsBound attributes ................
	Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
	Number of unique capsConnect attributes = 0
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 8
	Name = wing:faces, index = 1
	Name = htail:faces, index = 2
	Name = vtail:faces, index = 3
	Name = fuse:nose, index = 4
	Name = fuse:tail, index = 5
	Name = fuse:side, index = 6
	Name = fuse:bottom, index = 7
	Name = fuse:top, index = 8
Setting FEA Data
	Mesh for body = 0
	Number of nodal coordinates = 900
	Number of elements = 1796
	Elemental Nodes = 0
	Elemental Rods  = 0
	Elemental Tria3 = 1796
	Elemental Quad4 = 0
Setting FEA Data
	Mesh for body = 1
	Number of nodal coordinates = 170
	Number of elements = 336
	Elemental Nodes = 0
	Elemental Rods  = 0
	Elemental Tria3 = 336
	Elemental Quad4 = 0
Setting FEA Data
	Mesh for body = 2
	Number of nodal coordinates = 90
	Number of elements = 176
	Elemental Nodes = 0
	Elemental Rods  = 0
	Elemental Tria3 = 176
	Elemental Quad4 = 0
Setting FEA Data
	Mesh for body = 3
	Number of nodal coordinates = 1698
	Number of elements = 3392
	Elemental Nodes = 0
	Elemental Rods  = 0
	Elemental Tria3 = 3392
	Elemental Quad4 = 0
Combining multiple FEA meshes!
	Combined Number of nodal coordinates = 2858
	Combined Number of elements = 5700
	Combined Elemental Nodes = 0
	Combined Elemental Rods  = 0
	Combined Elemental Tria3 = 5700
	Combined Elemental Quad4 = 0
Updating mesh element types based on properties input
Mapping Csys attributes ................
	Number of unique Csys attributes = 0

Getting FEA coordinate systems.......
	Number of coordinate systems - 0
	No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
	Number of unique capsConstraint attributes = 0
Mapping capsLoad attributes ................
	Number of unique capsLoad attributes = 0
Mapping capsBound attributes ................
	Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
	Number of unique capsConnect attributes = 0
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 8
	Name = wing:faces, index = 1
	Name = htail:faces, index = 2
	Name = vtail:faces, index = 3
	Name = fuse:nose, index = 4
	Name = fuse:tail, index = 5
	Name = fuse:side, index = 6
	Name = fuse:bottom, index = 7
	Name = fuse:top, index = 8
Setting FEA Data
	Mesh for body = 0
	Number of nodal coordinates = 900
	Number of elements = 1796
	Elemental Nodes = 0
	Elemental Rods  = 0
	Elemental Tria3 = 1796
	Elemental Quad4 = 0
Setting FEA Data
	Mesh for body = 1
	Number of nodal coordinates = 170
	Number of elements = 336
	Elemental Nodes = 0
	Elemental Rods  = 0
	Elemental Tria3 = 336
	Elemental Quad4 = 0
Setting FEA Data
	Mesh for body = 2
	Number of nodal coordinates = 90
	Number of elements = 176
	Elemental Nodes = 0
	Elemental Rods  = 0
	Elemental Tria3 = 176
	Elemental Quad4 = 0
Setting FEA Data
	Mesh for body = 3
	Number of nodal coordinates = 1698
	Number of elements = 3392
	Elemental Nodes = 0
	Elemental Rods  = 0
	Elemental Tria3 = 3392
	Elemental Quad4 = 0
Combining multiple FEA meshes!
	Combined Number of nodal coordinates = 2858
	Combined Number of elements = 5700
	Combined Elemental Nodes = 0
	Combined Elemental Rods  = 0
	Combined Elemental Tria3 = 5700
	Combined Elemental Quad4 = 0
Updating mesh element types based on properties input
Mapping Csys attributes ................
	Number of unique Csys attributes = 0

Getting FEA coordinate systems.......
	Number of coordinate systems - 0
	No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
	Number of unique capsConstraint attributes = 0
Mapping capsLoad attributes ................
	Number of unique capsLoad attributes = 0
Mapping capsBound attributes ................
	Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
	Number of unique capsConnect attributes = 0
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 8
	Name = wing:faces, index = 1
	Name = htail:faces, index = 2
	Name = vtail:faces, index = 3
	Name = fuse:nose, index = 4
	Name = fuse:tail, index = 5
	Name = fuse:side, index = 6
	Name = fuse:bottom, index = 7
	Name = fuse:top, index = 8
Setting FEA Data
	Mesh for body = 0
	Number of nodal coordinates = 900
	Number of elements = 1796
	Elemental Nodes = 0
	Elemental Rods  = 0
	Elemental Tria3 = 1796
	Elemental Quad4 = 0
Setting FEA Data
	Mesh for body = 1
	Number of nodal coordinates = 170
	Number of elements = 336
	Elemental Nodes = 0
	Elemental Rods  = 0
	Elemental Tria3 = 336
	Elemental Quad4 = 0
Setting FEA Data
	Mesh for body = 2
	Number of nodal coordinates = 90
	Number of elements = 176
	Elemental Nodes = 0
	Elemental Rods  = 0
	Elemental Tria3 = 176
	Elemental Quad4 = 0
Setting FEA Data
	Mesh for body = 3
	Number of nodal coordinates = 1698
	Number of elements = 3392
	Elemental Nodes = 0
	Elemental Rods  = 0
	Elemental Tria3 = 3392
	Elemental Quad4 = 0
Combining multiple FEA meshes!
	Combined Number of nodal coordinates = 2858
	Combined Number of elements = 5700
	Combined Elemental Nodes = 0
	Combined Elemental Rods  = 0
	Combined Elemental Tria3 = 5700
	Combined Elemental Quad4 = 0
Updating mesh element types based on properties input

--&gt;Oringal CG = 91.72065954403
--&gt;CG sweep   = [84.05056882825, 85.58458697141, 87.11860511456, 88.65262325772, 90.18664140087, 91.72065954403, 93.25467768718, 94.78869583034, 96.32271397349, 97.85673211665, 99.3907502598]

real	0m0.558s
user	0m0.610s
sys	0m0.274s
+ status=0
+ set +x

=================================================
solutions/session03/masstran_CG.py passed (as expected)
=================================================


=================================================
+ echo 'f118-D.csm test;'
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/CAPS/training/2023/training.log
f118-D.csm test;
+ /Users/jenkins/workspace/ESP_bPreBuilt/ESP126/EngSketchPad/bin/serveESP -batch -verify -outLevel 0 f118-D.csm
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/CAPS/training/2023/training.log
WARNING:: cannot open "./verify_7.8.1/f118-D.vfy", so verification is being skipped
==&gt; serveESP completed successfully with no verification data

real	0m0.102s
user	0m0.102s
sys	0m0.006s
+ status=0
+ set +x

=================================================
data/session04/f118-D          passed (as expected)
=================================================


=================================================
+ echo 'naca.csm test;'
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/CAPS/training/2023/training.log
naca.csm test;
+ /Users/jenkins/workspace/ESP_bPreBuilt/ESP126/EngSketchPad/bin/serveESP -batch -verify -outLevel 0 naca.csm
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/CAPS/training/2023/training.log
WARNING:: cannot open "./verify_7.8.1/naca.vfy", so verification is being skipped
==&gt; serveESP completed successfully with no verification data

real	0m0.110s
user	0m0.107s
sys	0m0.006s
+ status=0
+ set +x

=================================================
data/session04/naca            passed (as expected)
=================================================


=================================================
1_mses_Deriv.py test;
+ python 1_mses_Deriv.py
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/CAPS/training/2023/training.log

==&gt; Loading geometry from file "naca.csm"...

==&gt; Area and Area derivatives...
--&gt; Area          0.082218968985062
--&gt; dArea/dthick  0.6847211877073472

==&gt; Drag and Drag derivatives...

Getting CFD design variables.......
	Number of design variables - 2
	Design Variable name - camber
	Design Variable name - thick
	Done getting CFD design variables
--&gt; CD          = 0.005288407930235986
--&gt; dCD/dAlpha  = -2.872255740855454e-07
--&gt; dCD/dMach   = 0.0012453366375636868
--&gt; dCD/dcamber = -3.202096592002027e-05
--&gt; dCD/dthick  = 0.01572066789258299

==&gt; All Drag derivatives...
--&gt; CD derivs   = {'Alpha': -2.872255740855454e-07, 'Mach': 0.0012453366375636868, 'Re': -3.6387727030798095e-11, 'camber': -3.202096592002027e-05, 'thick': 0.01572066789258299}

real	0m1.748s
user	0m1.972s
sys	0m0.082s
+ status=0
+ set +x

=================================================
data/session04/1_mses_Deriv.py passed (as expected)
=================================================


=================================================
2_mses_DerivPlot_CD_Alpha.py test;
+ python 2_mses_DerivPlot_CD_Alpha.py
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/CAPS/training/2023/training.log

==&gt; Loading geometry from file "naca.csm"...
--&gt; Alpha -3.0
--&gt; Alpha -2.5714285714285716
--&gt; Alpha -2.142857142857143
--&gt; Alpha -1.7142857142857144
--&gt; Alpha -1.2857142857142858
--&gt; Alpha -0.8571428571428572
--&gt; Alpha -0.4285714285714288
--&gt; Alpha 0.0
--&gt; Alpha 0.4285714285714284
--&gt; Alpha 0.8571428571428568
--&gt; Alpha 1.2857142857142856
--&gt; Alpha 1.7142857142857144
--&gt; Alpha 2.1428571428571423
--&gt; Alpha 2.571428571428571
--&gt; Alpha 3.0
/Users/jenkins/workspace/ESP_bPreBuilt/CAPS/training/2023/data/session04/2_mses_DerivPlot_CD_Alpha.py:77: UserWarning: FigureCanvasAgg is non-interactive, and thus cannot be shown
  plt.show()

real	0m23.085s
user	0m23.023s
sys	0m0.375s
+ status=0
+ set +x

=================================================
data/session04/2_mses_DerivPlot_CD_Alpha.py passed (as expected)
=================================================


=================================================
3_mses_OpenMDAO_CD_Alpha.py test;
+ python 3_mses_OpenMDAO_CD_Alpha.py
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/CAPS/training/2023/training.log
[VIGGEN.MIT.EDU:52731] shmem: mmap: an error occurred while determining whether or not /var/folders/l7/7s0m18td3fxg_w_dxpkj1d600000gp/T//ompi.VIGGEN.502/jf.0/3985702912/sm_segment.VIGGEN.502.ed910000.0 could be created.

==&gt; Starting Optimization...
--&gt; Alpha [3.]
--&gt; CD [0.00803595]
--&gt; Alpha [3.]
--&gt; CD [0.00803595]
--&gt; Alpha [3.]
--&gt; CD_alpha [[0.00014124]]
RUNNING THE L-BFGS-B CODE

           * * *

Machine precision = 2.220D-16
 N =            1     M =           10

At X0         0 variables are exactly at the bounds

At iterate    0    f=  8.03595D-03    |proj g|=  1.41235D-04
--&gt; Alpha [2.99985876]
--&gt; CD [0.00803593]
--&gt; Alpha [2.99985876]
--&gt; CD_alpha [[0.00014123]]

At iterate    1    f=  8.03593D-03    |proj g|=  1.41231D-04
--&gt; Alpha [-1.95855368]
--&gt; CD [0.0079199]
--&gt; Alpha [-1.95855368]
--&gt; CD_alpha [[-8.82237932e-05]]

At iterate    2    f=  7.91990D-03    |proj g|=  8.82238D-05
--&gt; Alpha [-0.05208071]
--&gt; CD [0.00783467]
--&gt; Alpha [-0.05208071]
--&gt; CD_alpha [[-2.58066379e-06]]

At iterate    3    f=  7.83467D-03    |proj g|=  2.58066D-06
--&gt; Alpha [0.00536658]
--&gt; CD [0.0078346]
--&gt; Alpha [0.00536658]
--&gt; CD_alpha [[1.71380689e-08]]

At iterate    4    f=  7.83460D-03    |proj g|=  1.71381D-08
--&gt; Alpha [0.00498759]
--&gt; CD [0.0078346]
--&gt; Alpha [0.00498759]
--&gt; CD_alpha [[-2.03931178e-09]]

At iterate    5    f=  7.83460D-03    |proj g|=  2.03931D-09

           * * *

Tit   = total number of iterations
Tnf   = total number of function evaluations
Tnint = total number of segments explored during Cauchy searches
Skip  = number of BFGS updates skipped
Nact  = number of active bounds at final generalized Cauchy point
Projg = norm of the final projected gradient
F     = final function value

           * * *

   N    Tit     Tnf  Tnint  Skip  Nact     Projg        F
    1      5      6      5     0     0   2.039D-09   7.835D-03
  F =   7.8346014199255319E-003

CONVERGENCE: REL_REDUCTION_OF_F_&lt;=_FACTR*EPSMCH             
Optimization Complete
-----------------------------------
--&gt; Optimized value: [0.00498759]

real	0m10.162s
user	0m10.535s
sys	0m0.263s
+ status=0
+ set +x

=================================================
data/session04/3_mses_OpenMDAO_CD_Alpha.py passed (as expected)
=================================================


=================================================
4_mses_DerivPlot_CD_camber.py test;
+ python 4_mses_DerivPlot_CD_camber.py
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/CAPS/training/2023/training.log

==&gt; Loading geometry from file "naca.csm"...
--&gt; camber -0.1

Getting CFD design variables.......
	Number of design variables - 1
	Design Variable name - camber
	Done getting CFD design variables
--&gt; camber -0.08571428571428572
--&gt; camber -0.07142857142857142
--&gt; camber -0.05714285714285715
--&gt; camber -0.04285714285714286
--&gt; camber -0.028571428571428567
--&gt; camber -0.01428571428571429
--&gt; camber 0.0
--&gt; camber 0.01428571428571429
--&gt; camber 0.02857142857142858
--&gt; camber 0.04285714285714287
--&gt; camber 0.05714285714285716
--&gt; camber 0.07142857142857142
--&gt; camber 0.08571428571428572
--&gt; camber 0.1
/Users/jenkins/workspace/ESP_bPreBuilt/CAPS/training/2023/data/session04/4_mses_DerivPlot_CD_camber.py:80: UserWarning: FigureCanvasAgg is non-interactive, and thus cannot be shown
  plt.show()

real	0m24.470s
user	0m24.350s
sys	0m0.421s
+ status=0
+ set +x

=================================================
data/session04/4_mses_DerivPlot_CD_camber.py passed (as expected)
=================================================


=================================================
5_mses_OpenMDAO_CD_camber.py test;
+ python 5_mses_OpenMDAO_CD_camber.py
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/CAPS/training/2023/training.log
[VIGGEN.MIT.EDU:52894] shmem: mmap: an error occurred while determining whether or not /var/folders/l7/7s0m18td3fxg_w_dxpkj1d600000gp/T//ompi.VIGGEN.502/jf.0/1892155392/sm_segment.VIGGEN.502.70c80000.0 could be created.

==&gt; Starting Optimization...
--&gt; camber [0.1]

Getting CFD design variables.......
	Number of design variables - 1
	Design Variable name - camber
	Done getting CFD design variables
--&gt; CD     [0.01370215]
--&gt; camber [0.1]
--&gt; CD     [0.01370215]
--&gt; camber     [0.1]
--&gt; CD_camber [[0.17593485]]
RUNNING THE L-BFGS-B CODE

           * * *

Machine precision = 2.220D-16
 N =            1     M =           10

At X0         1 variables are exactly at the bounds

At iterate    0    f=  1.37022D-02    |proj g|=  1.75935D-01
--&gt; camber [-0.07593485]
--&gt; CD     [0.01053684]
--&gt; camber     [-0.07593485]
--&gt; CD_camber [[-0.07712924]]

At iterate    1    f=  1.05368D-02    |proj g|=  7.71292D-02
--&gt; camber [-0.02231317]
--&gt; CD     [0.00803517]
--&gt; camber     [-0.02231317]
--&gt; CD_camber [[-0.0171107]]

At iterate    2    f=  8.03517D-03    |proj g|=  1.71107D-02
--&gt; camber [-0.00702616]
--&gt; CD     [0.0078537]
--&gt; camber     [-0.00702616]
--&gt; CD_camber [[-0.00523687]]

At iterate    3    f=  7.85370D-03    |proj g|=  5.23687D-03
--&gt; camber [-0.00028392]
--&gt; CD     [0.00783468]
--&gt; camber     [-0.00028392]
--&gt; CD_camber [[-0.00015053]]

At iterate    4    f=  7.83468D-03    |proj g|=  1.50527D-04
--&gt; camber [-8.43924833e-05]
--&gt; CD     [0.00783469]
--&gt; camber     [-8.43924833e-05]
--&gt; CD_camber [[-4.75268316e-07]]
--&gt; camber [-0.00023422]
--&gt; CD     [0.00783469]
--&gt; camber     [-0.00023422]
--&gt; CD_camber [[-0.00011282]]
--&gt; camber [-0.00027527]
--&gt; CD     [0.00783469]
--&gt; camber     [-0.00027527]
--&gt; CD_camber [[-0.00014369]]
--&gt; camber [-0.00028357]
--&gt; CD     [0.00783468]
--&gt; camber     [-0.00028357]
--&gt; CD_camber [[-0.00015009]]
--&gt; camber [-0.00028392]
--&gt; CD     [0.00783469]
--&gt; camber     [-0.00028392]
--&gt; CD_camber [[-0.00015045]]
--&gt; camber [-0.00028392]
--&gt; CD     [0.00783468]
--&gt; camber     [-0.00028392]
--&gt; CD_camber [[-0.00015053]]
--&gt; camber [-0.00028392]
--&gt; CD     [0.00783468]
--&gt; camber     [-0.00028392]
--&gt; CD_camber [[-0.00015048]]
--&gt; camber [-0.00028392]
--&gt; CD     [0.00783468]
--&gt; camber     [-0.00028392]
--&gt; CD_camber [[-0.00015048]]
--&gt; camber [-0.00028392]
--&gt; CD     [0.00783468]
--&gt; camber     [-0.00028392]
--&gt; CD_camber [[-0.00015048]]

At iterate    5    f=  7.83468D-03    |proj g|=  1.50476D-04

           * * *

Tit   = total number of iterations
Tnf   = total number of function evaluations
Tnint = total number of segments explored during Cauchy searches
Skip  = number of BFGS updates skipped
Nact  = number of active bounds at final generalized Cauchy point
Projg = norm of the final projected gradient
F     = final function value

           * * *

   N    Tit     Tnf  Tnint  Skip  Nact     Projg        F
    1      5     14      5     0     0   1.505D-04   7.835D-03
  F =   7.8346831540125825E-003

CONVERGENCE: REL_REDUCTION_OF_F_&lt;=_FACTR*EPSMCH             
Optimization Complete
-----------------------------------
--&gt; Optimized value: [-0.00028392]

real	0m22.730s
user	0m22.918s
sys	0m0.456s
+ status=0
+ set +x

=================================================
data/session04/5_mses_OpenMDAO_CD_camber.py passed (as expected)
=================================================


=================================================
6_mses_DerivPlot_CL2_camber.py test;
+ python 6_mses_DerivPlot_CL2_camber.py
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/CAPS/training/2023/training.log

==&gt; Loading geometry from file "naca.csm"...
--&gt; camber -0.1

Getting CFD design variables.......
	Number of design variables - 1
	Design Variable name - camber
	Done getting CFD design variables
--&gt; camber -0.08571428571428572
--&gt; camber -0.07142857142857142
--&gt; camber -0.05714285714285715
--&gt; camber -0.04285714285714286
--&gt; camber -0.028571428571428567
--&gt; camber -0.01428571428571429
--&gt; camber 0.0
--&gt; camber 0.01428571428571429
--&gt; camber 0.02857142857142858
--&gt; camber 0.04285714285714287
--&gt; camber 0.05714285714285716
--&gt; camber 0.07142857142857142
--&gt; camber 0.08571428571428572
--&gt; camber 0.1
/Users/jenkins/workspace/ESP_bPreBuilt/CAPS/training/2023/data/session04/6_mses_DerivPlot_CL2_camber.py:82: UserWarning: FigureCanvasAgg is non-interactive, and thus cannot be shown
  plt.show()

real	0m24.447s
user	0m24.350s
sys	0m0.417s
+ status=0
+ set +x

=================================================
data/session04/6_mses_DerivPlot_CL2_camber.py passed (as expected)
=================================================


=================================================
7_mses_OpenMDAO_CL2_camber.py test;
+ python 7_mses_OpenMDAO_CL2_camber.py
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/CAPS/training/2023/training.log
[VIGGEN.MIT.EDU:53119] shmem: mmap: an error occurred while determining whether or not /var/folders/l7/7s0m18td3fxg_w_dxpkj1d600000gp/T//ompi.VIGGEN.502/jf.0/1119617024/sm_segment.VIGGEN.502.42bc0000.0 could be created.

==&gt; Starting Optimization...
--&gt; camber [0.1]

Getting CFD design variables.......
	Number of design variables - 1
	Design Variable name - camber
	Done getting CFD design variables
--&gt; CL2    [1.23492174]
--&gt; camber [0.1]
--&gt; CL2    [1.23492174]
--&gt; camber     [0.1]
--&gt; CL2_camber [[14.37217996]]
RUNNING THE L-BFGS-B CODE

           * * *

Machine precision = 2.220D-16
 N =            1     M =           10

At X0         1 variables are exactly at the bounds

At iterate    0    f=  1.23492D+00    |proj g|=  2.00000D-01
--&gt; camber [-0.1]
--&gt; CL2    [1.23490353]
--&gt; camber     [-0.1]
--&gt; CL2_camber [[-14.37225246]]
--&gt; camber [9.91451295e-05]
--&gt; CL2    [1.68377899e-06]
--&gt; camber     [9.91451295e-05]
--&gt; CL2_camber [[0.03419212]]

At iterate    1    f=  1.68378D-06    |proj g|=  3.41921D-02
--&gt; camber [-0.00013909]
--&gt; CL2    [3.35149206e-06]
--&gt; camber     [-0.00013909]
--&gt; CL2_camber [[-0.04823952]]
--&gt; camber [2.48992281e-07]
--&gt; CL2    [1.02478314e-12]
--&gt; camber     [2.48992281e-07]
--&gt; CL2_camber [[-2.66746531e-05]]

At iterate    2    f=  1.02478D-12    |proj g|=  2.66747D-05
--&gt; camber [3.26085013e-07]
--&gt; CL2    [1.67189956e-13]
--&gt; camber     [3.26085013e-07]
--&gt; CL2_camber [[1.07742885e-05]]

At iterate    3    f=  1.67190D-13    |proj g|=  1.07743D-05

           * * *

Tit   = total number of iterations
Tnf   = total number of function evaluations
Tnint = total number of segments explored during Cauchy searches
Skip  = number of BFGS updates skipped
Nact  = number of active bounds at final generalized Cauchy point
Projg = norm of the final projected gradient
F     = final function value

           * * *

   N    Tit     Tnf  Tnint  Skip  Nact     Projg        F
    1      3      6      3     0     0   1.077D-05   1.672D-13
  F =   1.6718995645907989E-013

CONVERGENCE: REL_REDUCTION_OF_F_&lt;=_FACTR*EPSMCH             
Optimization Complete
-----------------------------------
--&gt; Optimized value: [3.26085013e-07]

real	0m10.598s
user	0m11.006s
sys	0m0.273s
+ status=0
+ set +x

=================================================
data/session04/7_mses_OpenMDAO_CL2_camber.py passed (as expected)
=================================================


=================================================
8_mses_OpenMDAO_CDCL.py test;
+ python 8_mses_OpenMDAO_CDCL.py
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/CAPS/training/2023/training.log
[VIGGEN.MIT.EDU:53177] shmem: mmap: an error occurred while determining whether or not /var/folders/l7/7s0m18td3fxg_w_dxpkj1d600000gp/T//ompi.VIGGEN.502/jf.0/394592256/sm_segment.VIGGEN.502.17850000.0 could be created.

==&gt; Starting Optimization...
--&gt; Alpha [0.]
--&gt; camber [0.1]

Getting CFD design variables.......
	Number of design variables - 1
	Design Variable name - camber
	Done getting CFD design variables
--&gt; CD     [0.01370215]
--&gt; CL     [1.11127033]
--&gt; Alpha [0.]
--&gt; camber [0.1]
--&gt; CD     [0.01370215]
--&gt; CL     [1.11127033]
--&gt; Alpha [0.]
--&gt; camber     [0.1]
--&gt; CD_Alpha [[0.00105841]]
--&gt; CL_Alpha [[0.09897622]]
--&gt; CD_camber [[0.17593485]]
--&gt; CL_camber [[6.46655435]]
--&gt; Alpha [0.00077914]
--&gt; camber [0.04412056]
--&gt; CD     [0.00864294]
--&gt; CL     [0.57036568]
--&gt; Alpha [0.00077914]
--&gt; camber     [0.04412056]
--&gt; CD_Alpha [[0.00023873]]
--&gt; CL_Alpha [[0.12984106]]
--&gt; CD_camber [[0.03642485]]
--&gt; CL_camber [[12.533991]]
--&gt; Alpha [0.00103084]
--&gt; camber [0.05844972]
--&gt; CD     [0.0093022]
--&gt; CL     [0.7443929]
--&gt; Alpha [0.00103084]
--&gt; camber     [0.05844972]
--&gt; CD_Alpha [[0.00033987]]
--&gt; CL_Alpha [[0.12673046]]
--&gt; CD_camber [[0.05177195]]
--&gt; CL_camber [[11.83406756]]
--&gt; Alpha [0.00125705]
--&gt; camber [0.05892111]
--&gt; CD     [0.00932813]
--&gt; CL     [0.74994779]
Optimization terminated successfully    (Exit mode 0)
            Current function value: 0.009328127623067835
            Iterations: 3
            Function evaluations: 4
            Gradient evaluations: 3
Optimization Complete
-----------------------------------
--&gt; Optimized value: [0.05892111]

real	0m7.599s
user	0m8.089s
sys	0m0.231s
+ status=0
+ set +x

=================================================
data/session04/8_mses_OpenMDAO_CDCL.py passed (as expected)
=================================================


=================================================
9_masstran_OpenMDAO_thick.py test;
+ python 9_masstran_OpenMDAO_thick.py
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/CAPS/training/2023/training.log
[VIGGEN.MIT.EDU:53223] shmem: mmap: an error occurred while determining whether or not /var/folders/l7/7s0m18td3fxg_w_dxpkj1d600000gp/T//ompi.VIGGEN.502/jf.0/1749483520/sm_segment.VIGGEN.502.68470000.0 could be created.

==&gt; Starting Optimization...
/Users/jenkins/workspace/ESP_bPreBuilt/ESP126/Python-3.11.9/lib/python3.11/site-packages/openmdao/core/driver.py:619: DriverWarning:The following design variable initial conditions are out of their specified bounds:
  masstranSystem.x2
    val: [0.]
    lower: 0.01
    upper: 10.0
Set the initial value of the design variable to a valid value or set the driver option['invalid_desvar_behavior'] to 'ignore'.
--&gt; x1 [0.1]
--&gt; x2 [0.]
Mapping Csys attributes ................
	Number of unique Csys attributes = 0

Getting FEA coordinate systems.......
	Number of coordinate systems - 0
	No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
	Number of unique capsConstraint attributes = 0
Mapping capsLoad attributes ................
	Number of unique capsLoad attributes = 0
Mapping capsBound attributes ................
	Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
	Number of unique capsConnect attributes = 0
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 4
	Name = wing, index = 1
	Name = htail, index = 2
	Name = vtail, index = 3
	Name = fuse, index = 4
Setting FEA Data
	Mesh for body = 0
	Number of nodal coordinates = 2168
	Number of elements = 2166
	Elemental Nodes = 0
	Elemental Rods  = 0
	Elemental Tria3 = 0
	Elemental Quad4 = 2166
Setting FEA Data
	Mesh for body = 1
	Number of nodal coordinates = 2168
	Number of elements = 2166
	Elemental Nodes = 0
	Elemental Rods  = 0
	Elemental Tria3 = 0
	Elemental Quad4 = 2166
Setting FEA Data
	Mesh for body = 2
	Number of nodal coordinates = 2168
	Number of elements = 2166
	Elemental Nodes = 0
	Elemental Rods  = 0
	Elemental Tria3 = 0
	Elemental Quad4 = 2166
Setting FEA Data
	Mesh for body = 3
	Number of nodal coordinates = 2168
	Number of elements = 2166
	Elemental Nodes = 0
	Elemental Rods  = 0
	Elemental Tria3 = 0
	Elemental Quad4 = 2166
Combining multiple FEA meshes!
	Combined Number of nodal coordinates = 8672
	Combined Number of elements = 8664
	Combined Elemental Nodes = 0
	Combined Elemental Rods  = 0
	Combined Elemental Tria3 = 0
	Combined Elemental Quad4 = 8664

Getting FEA materials.......
	Number of materials - 2
	Material name - madeupium
	Material name - unobtainium
	Done getting FEA materials

Getting FEA properties.......
	Number of properties - 4
	Property name - fuse
	Property name - htail
	Property name - vtail
	Property name - wing
	Done getting FEA properties
Updating mesh element types based on properties input

Getting FEA design variables.......
	Number of design variables          - 2
	Design_Variable name - x1
	Design_Variable name - x2
	Design_Variable_Relation name - fuseRel
	Design_Variable_Relation name - wingRel
	Number of design variable relations - 2
	Done getting FEA design variables
--&gt; dCGx [2.75695334]
--&gt; x1 [0.1]
--&gt; x2 [0.01]
/Users/jenkins/workspace/ESP_bPreBuilt/CAPS/training/2023/data/session04/9_masstran_OpenMDAO_thick.py:52: DeprecationWarning: Conversion of an array with ndim &gt; 0 to a scalar is deprecated, and will error in future. Ensure you extract a single element from your array before performing this operation. (Deprecated NumPy 1.25.)
  "x1": {"initialValue":float(inputs['x1'])},
/Users/jenkins/workspace/ESP_bPreBuilt/CAPS/training/2023/data/session04/9_masstran_OpenMDAO_thick.py:53: DeprecationWarning: Conversion of an array with ndim &gt; 0 to a scalar is deprecated, and will error in future. Ensure you extract a single element from your array before performing this operation. (Deprecated NumPy 1.25.)
  "x2": {"initialValue":float(inputs['x2'])},
Updating mesh element types based on properties input

Getting FEA design variables.......
	Number of design variables          - 2
	Design_Variable name - x1
	Design_Variable name - x2
	Design_Variable_Relation name - fuseRel
	Design_Variable_Relation name - wingRel
	Number of design variable relations - 2
	Done getting FEA design variables
--&gt; dCGx [2.70119648]
--&gt; x1 [0.1]
--&gt; x2 [0.01]
--&gt; dCGx_x1 [[-68.82272937]]
--&gt; dCGx_x2 [[-5.53091882]]
RUNNING THE L-BFGS-B CODE

           * * *

Machine precision = 2.220D-16
 N =            2     M =           10

At X0         1 variables are exactly at the bounds

At iterate    0    f=  2.70120D+00    |proj g|=  9.90000D+00
--&gt; x1 [10.]
--&gt; x2 [5.54091882]
Updating mesh element types based on properties input

Getting FEA design variables.......
	Number of design variables          - 2
	Design_Variable name - x1
	Design_Variable name - x2
	Design_Variable_Relation name - fuseRel
	Design_Variable_Relation name - wingRel
	Number of design variable relations - 2
	Done getting FEA design variables
--&gt; dCGx [10.16370853]
--&gt; x1 [10.]
--&gt; x2 [5.54091882]
--&gt; dCGx_x1 [[0.04843981]]
--&gt; dCGx_x2 [[0.03754845]]
--&gt; x1 [3.33378327]
--&gt; x2 [1.81664573]
Updating mesh element types based on properties input

Getting FEA design variables.......
	Number of design variables          - 2
	Design_Variable name - x1
	Design_Variable name - x2
	Design_Variable_Relation name - fuseRel
	Design_Variable_Relation name - wingRel
	Number of design variable relations - 2
	Done getting FEA design variables
--&gt; dCGx [8.85443326]
--&gt; x1 [3.33378327]
--&gt; x2 [1.81664573]
--&gt; dCGx_x1 [[0.48418692]]
--&gt; dCGx_x2 [[0.1268106]]
--&gt; x1 [1.12760341]
--&gt; x2 [0.5841001]
Updating mesh element types based on properties input

Getting FEA design variables.......
	Number of design variables          - 2
	Design_Variable name - x1
	Design_Variable name - x2
	Design_Variable_Relation name - fuseRel
	Design_Variable_Relation name - wingRel
	Number of design variable relations - 2
	Done getting FEA design variables
--&gt; dCGx [5.7972651]
--&gt; x1 [1.12760341]
--&gt; x2 [0.5841001]
--&gt; dCGx_x1 [[3.182136]]
--&gt; dCGx_x2 [[0.42790152]]
--&gt; x1 [0.42334159]
--&gt; x2 [0.19064405]
Updating mesh element types based on properties input

Getting FEA design variables.......
	Number of design variables          - 2
	Design_Variable name - x1
	Design_Variable name - x2
	Design_Variable_Relation name - fuseRel
	Design_Variable_Relation name - wingRel
	Number of design variable relations - 2
	Done getting FEA design variables
--&gt; dCGx [1.60230885]
--&gt; x1 [0.42334159]
--&gt; x2 [0.19064405]
--&gt; dCGx_x1 [[8.88674345]]
--&gt; dCGx_x2 [[0.86253194]]

At iterate    1    f=  1.60231D+00    |proj g|=  4.13342D-01
--&gt; x1 [0.38612876]
--&gt; x2 [0.16914154]
Updating mesh element types based on properties input

Getting FEA design variables.......
	Number of design variables          - 2
	Design_Variable name - x1
	Design_Variable name - x2
	Design_Variable_Relation name - fuseRel
	Design_Variable_Relation name - wingRel
	Number of design variable relations - 2
	Done getting FEA design variables
--&gt; dCGx [1.24954556]
--&gt; x1 [0.38612876]
--&gt; x2 [0.16914154]
--&gt; dCGx_x1 [[9.04121089]]
--&gt; dCGx_x2 [[0.8599867]]
--&gt; x1 [0.23727742]
--&gt; x2 [0.08313149]
Updating mesh element types based on properties input

Getting FEA design variables.......
	Number of design variables          - 2
	Design_Variable name - x1
	Design_Variable name - x2
	Design_Variable_Relation name - fuseRel
	Design_Variable_Relation name - wingRel
	Number of design variable relations - 2
	Done getting FEA design variables
--&gt; dCGx [0.04927766]
--&gt; x1 [0.23727742]
--&gt; x2 [0.08313149]
--&gt; dCGx_x1 [[3.58807069]]
--&gt; dCGx_x2 [[0.31359947]]

At iterate    2    f=  4.92777D-02    |proj g|=  2.27277D-01
--&gt; x1 [0.11213433]
--&gt; x2 [0.01347811]
Updating mesh element types based on properties input

Getting FEA design variables.......
	Number of design variables          - 2
	Design_Variable name - x1
	Design_Variable name - x2
	Design_Variable_Relation name - fuseRel
	Design_Variable_Relation name - wingRel
	Number of design variable relations - 2
	Done getting FEA design variables
--&gt; dCGx [1.95060563]
--&gt; x1 [0.11213433]
--&gt; x2 [0.01347811]
--&gt; dCGx_x1 [[-52.76118222]]
--&gt; dCGx_x2 [[-4.27221829]]
--&gt; x1 [0.21361795]
--&gt; x2 [0.06996287]
Updating mesh element types based on properties input

Getting FEA design variables.......
	Number of design variables          - 2
	Design_Variable name - x1
	Design_Variable name - x2
	Design_Variable_Relation name - fuseRel
	Design_Variable_Relation name - wingRel
	Number of design variable relations - 2
	Done getting FEA design variables
--&gt; dCGx [5.61440048e-05]
--&gt; x1 [0.21361795]
--&gt; x2 [0.06996287]
--&gt; dCGx_x1 [[0.13868009]]
--&gt; dCGx_x2 [[0.01195172]]

At iterate    3    f=  5.61440D-05    |proj g|=  1.38680D-01
--&gt; x1 [0.21266725]
--&gt; x2 [0.06943529]
Updating mesh element types based on properties input

Getting FEA design variables.......
	Number of design variables          - 2
	Design_Variable name - x1
	Design_Variable name - x2
	Design_Variable_Relation name - fuseRel
	Design_Variable_Relation name - wingRel
	Number of design variable relations - 2
	Done getting FEA design variables
--&gt; dCGx [3.06804662e-06]
--&gt; x1 [0.21266725]
--&gt; x2 [0.06943529]
--&gt; dCGx_x1 [[-0.03260179]]
--&gt; dCGx_x2 [[-0.00280809]]

At iterate    4    f=  3.06805D-06    |proj g|=  3.26018D-02
--&gt; x1 [0.2128482]
--&gt; x2 [0.0695357]
Updating mesh element types based on properties input

Getting FEA design variables.......
	Number of design variables          - 2
	Design_Variable name - x1
	Design_Variable name - x2
	Design_Variable_Relation name - fuseRel
	Design_Variable_Relation name - wingRel
	Number of design variable relations - 2
	Done getting FEA design variables
--&gt; dCGx [1.43517357e-10]
--&gt; x1 [0.2128482]
--&gt; x2 [0.0695357]
--&gt; dCGx_x1 [[0.00022274]]
--&gt; dCGx_x2 [[1.91872578e-05]]

At iterate    5    f=  1.43517D-10    |proj g|=  2.22739D-04
--&gt; x1 [0.21284697]
--&gt; x2 [0.06953502]
Updating mesh element types based on properties input

Getting FEA design variables.......
	Number of design variables          - 2
	Design_Variable name - x1
	Design_Variable name - x2
	Design_Variable_Relation name - fuseRel
	Design_Variable_Relation name - wingRel
	Number of design variable relations - 2
	Done getting FEA design variables
--&gt; dCGx [3.63550505e-16]
--&gt; x1 [0.21284697]
--&gt; x2 [0.06953502]
--&gt; dCGx_x1 [[3.54510824e-07]]
--&gt; dCGx_x2 [[3.05383747e-08]]

At iterate    6    f=  3.63551D-16    |proj g|=  3.54511D-07

           * * *

Tit   = total number of iterations
Tnf   = total number of function evaluations
Tnint = total number of segments explored during Cauchy searches
Skip  = number of BFGS updates skipped
Nact  = number of active bounds at final generalized Cauchy point
Projg = norm of the final projected gradient
F     = final function value

           * * *

   N    Tit     Tnf  Tnint  Skip  Nact     Projg        F
    2      6     12      7     0     0   3.545D-07   3.636D-16
  F =   3.6355050512987024E-016

CONVERGENCE: REL_REDUCTION_OF_F_&lt;=_FACTR*EPSMCH             
Optimization Complete
-----------------------------------
==&gt; Optimized value:
--&gt; x1 [0.21284697]
--&gt; x2 [0.06953502]

real	0m1.340s
user	0m1.699s
sys	0m0.346s
+ status=0
+ set +x

=================================================
data/session04/9_masstran_OpenMDAO_thick.py passed (as expected)
=================================================


=================================================
masstran_OpenMDAO_geom.py test;
+ python masstran_OpenMDAO_geom.py
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/CAPS/training/2023/training.log
[VIGGEN.MIT.EDU:53268] shmem: mmap: an error occurred while determining whether or not /var/folders/l7/7s0m18td3fxg_w_dxpkj1d600000gp/T//ompi.VIGGEN.502/jf.0/2702311424/sm_segment.VIGGEN.502.a1120000.0 could be created.
==&gt; Initial values:
htail:lh   5.0
wing:xroot 4.0

==&gt; Starting Optimization...
--&gt; htail:lh   [5.]
--&gt; wing:xroot [4.]
Mapping Csys attributes ................
	Number of unique Csys attributes = 0

Getting FEA coordinate systems.......
	Number of coordinate systems - 0
	No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
	Number of unique capsConstraint attributes = 0
Mapping capsLoad attributes ................
	Number of unique capsLoad attributes = 0
Mapping capsBound attributes ................
	Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
	Number of unique capsConnect attributes = 0
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 4
	Name = wing, index = 1
	Name = htail, index = 2
	Name = vtail, index = 3
	Name = fuse, index = 4
Setting FEA Data
	Mesh for body = 0
	Number of nodal coordinates = 2168
	Number of elements = 2166
	Elemental Nodes = 0
	Elemental Rods  = 0
	Elemental Tria3 = 0
	Elemental Quad4 = 2166
Setting FEA Data
	Mesh for body = 1
	Number of nodal coordinates = 2168
	Number of elements = 2166
	Elemental Nodes = 0
	Elemental Rods  = 0
	Elemental Tria3 = 0
	Elemental Quad4 = 2166
Setting FEA Data
	Mesh for body = 2
	Number of nodal coordinates = 2168
	Number of elements = 2166
	Elemental Nodes = 0
	Elemental Rods  = 0
	Elemental Tria3 = 0
	Elemental Quad4 = 2166
Setting FEA Data
	Mesh for body = 3
	Number of nodal coordinates = 2168
	Number of elements = 2166
	Elemental Nodes = 0
	Elemental Rods  = 0
	Elemental Tria3 = 0
	Elemental Quad4 = 2166
Combining multiple FEA meshes!
	Combined Number of nodal coordinates = 8672
	Combined Number of elements = 8664
	Combined Elemental Nodes = 0
	Combined Elemental Rods  = 0
	Combined Elemental Tria3 = 0
	Combined Elemental Quad4 = 8664

Getting FEA materials.......
	Number of materials - 2
	Material name - madeupium
	Material name - unobtainium
	Done getting FEA materials

Getting FEA properties.......
	Number of properties - 4
	Property name - fuse
	Property name - htail
	Property name - vtail
	Property name - wing
	Done getting FEA properties
Updating mesh element types based on properties input

Getting FEA design variables.......
	Number of design variables          - 2
	Design_Variable name - htail:lh
	Design_Variable name - wing:xroot
	Number of design variable relations - 0
	Done getting FEA design variables
--&gt; dCGx [2.10539929]
--&gt; htail:lh   [5.]
--&gt; wing:xroot [4.]
--&gt; dCGx [2.10539929]
--&gt; htail:lh   [5.]
--&gt; wing:xroot [4.]
--&gt; dCGx_htail:lh [[-0.40374365]]
--&gt; dCGx_wing:xroot [[-1.15229479]]
RUNNING THE L-BFGS-B CODE

           * * *

Machine precision = 2.220D-16
 N =            2     M =           10

At X0         0 variables are exactly at the bounds

At iterate    0    f=  2.10540D+00    |proj g|=  1.15229D+00
--&gt; htail:lh   [5.40374365]
--&gt; wing:xroot [5.15229479]
Mapping Csys attributes ................
	Number of unique Csys attributes = 0

Getting FEA coordinate systems.......
	Number of coordinate systems - 0
	No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
	Number of unique capsConstraint attributes = 0
Mapping capsLoad attributes ................
	Number of unique capsLoad attributes = 0
Mapping capsBound attributes ................
	Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
	Number of unique capsConnect attributes = 0
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 4
	Name = wing, index = 1
	Name = htail, index = 2
	Name = vtail, index = 3
	Name = fuse, index = 4
Setting FEA Data
	Mesh for body = 0
	Number of nodal coordinates = 2168
	Number of elements = 2166
	Elemental Nodes = 0
	Elemental Rods  = 0
	Elemental Tria3 = 0
	Elemental Quad4 = 2166
Setting FEA Data
	Mesh for body = 1
	Number of nodal coordinates = 2168
	Number of elements = 2166
	Elemental Nodes = 0
	Elemental Rods  = 0
	Elemental Tria3 = 0
	Elemental Quad4 = 2166
Setting FEA Data
	Mesh for body = 2
	Number of nodal coordinates = 2168
	Number of elements = 2166
	Elemental Nodes = 0
	Elemental Rods  = 0
	Elemental Tria3 = 0
	Elemental Quad4 = 2166
Setting FEA Data
	Mesh for body = 3
	Number of nodal coordinates = 2168
	Number of elements = 2166
	Elemental Nodes = 0
	Elemental Rods  = 0
	Elemental Tria3 = 0
	Elemental Quad4 = 2166
Combining multiple FEA meshes!
	Combined Number of nodal coordinates = 8672
	Combined Number of elements = 8664
	Combined Elemental Nodes = 0
	Combined Elemental Rods  = 0
	Combined Elemental Tria3 = 0
	Combined Elemental Quad4 = 8664
Updating mesh element types based on properties input

Getting FEA design variables.......
	Number of design variables          - 2
	Design_Variable name - htail:lh
	Design_Variable name - wing:xroot
	Number of design variable relations - 0
	Done getting FEA design variables
--&gt; dCGx [0.86918465]
--&gt; htail:lh   [5.40374365]
--&gt; wing:xroot [5.15229479]
--&gt; dCGx_htail:lh [[-0.30002756]]
--&gt; dCGx_wing:xroot [[-0.74124931]]

At iterate    1    f=  8.69185D-01    |proj g|=  7.41249D-01
--&gt; htail:lh   [6.474753]
--&gt; wing:xroot [7.25471671]
Mapping Csys attributes ................
	Number of unique Csys attributes = 0

Getting FEA coordinate systems.......
	Number of coordinate systems - 0
	No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
	Number of unique capsConstraint attributes = 0
Mapping capsLoad attributes ................
	Number of unique capsLoad attributes = 0
Mapping capsBound attributes ................
	Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
	Number of unique capsConnect attributes = 0
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 4
	Name = wing, index = 1
	Name = htail, index = 2
	Name = vtail, index = 3
	Name = fuse, index = 4
Setting FEA Data
	Mesh for body = 0
	Number of nodal coordinates = 2168
	Number of elements = 2166
	Elemental Nodes = 0
	Elemental Rods  = 0
	Elemental Tria3 = 0
	Elemental Quad4 = 2166
Setting FEA Data
	Mesh for body = 1
	Number of nodal coordinates = 2168
	Number of elements = 2166
	Elemental Nodes = 0
	Elemental Rods  = 0
	Elemental Tria3 = 0
	Elemental Quad4 = 2166
Setting FEA Data
	Mesh for body = 2
	Number of nodal coordinates = 2168
	Number of elements = 2166
	Elemental Nodes = 0
	Elemental Rods  = 0
	Elemental Tria3 = 0
	Elemental Quad4 = 2166
Setting FEA Data
	Mesh for body = 3
	Number of nodal coordinates = 2168
	Number of elements = 2166
	Elemental Nodes = 0
	Elemental Rods  = 0
	Elemental Tria3 = 0
	Elemental Quad4 = 2166
Combining multiple FEA meshes!
	Combined Number of nodal coordinates = 8672
	Combined Number of elements = 8664
	Combined Elemental Nodes = 0
	Combined Elemental Rods  = 0
	Combined Elemental Tria3 = 0
	Combined Elemental Quad4 = 8664
Updating mesh element types based on properties input

Getting FEA design variables.......
	Number of design variables          - 2
	Design_Variable name - htail:lh
	Design_Variable name - wing:xroot
	Number of design variable relations - 0
	Done getting FEA design variables
--&gt; dCGx [0.00905292]
--&gt; htail:lh   [6.474753]
--&gt; wing:xroot [7.25471671]
--&gt; dCGx_htail:lh [[0.03711399]]
--&gt; dCGx_wing:xroot [[0.07531706]]

At iterate    2    f=  9.05292D-03    |proj g|=  7.53171D-02
--&gt; htail:lh   [6.35917671]
--&gt; wing:xroot [7.05983716]
Mapping Csys attributes ................
	Number of unique Csys attributes = 0

Getting FEA coordinate systems.......
	Number of coordinate systems - 0
	No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
	Number of unique capsConstraint attributes = 0
Mapping capsLoad attributes ................
	Number of unique capsLoad attributes = 0
Mapping capsBound attributes ................
	Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
	Number of unique capsConnect attributes = 0
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 4
	Name = wing, index = 1
	Name = htail, index = 2
	Name = vtail, index = 3
	Name = fuse, index = 4
Setting FEA Data
	Mesh for body = 0
	Number of nodal coordinates = 2168
	Number of elements = 2166
	Elemental Nodes = 0
	Elemental Rods  = 0
	Elemental Tria3 = 0
	Elemental Quad4 = 2166
Setting FEA Data
	Mesh for body = 1
	Number of nodal coordinates = 2168
	Number of elements = 2166
	Elemental Nodes = 0
	Elemental Rods  = 0
	Elemental Tria3 = 0
	Elemental Quad4 = 2166
Setting FEA Data
	Mesh for body = 2
	Number of nodal coordinates = 2168
	Number of elements = 2166
	Elemental Nodes = 0
	Elemental Rods  = 0
	Elemental Tria3 = 0
	Elemental Quad4 = 2166
Setting FEA Data
	Mesh for body = 3
	Number of nodal coordinates = 2168
	Number of elements = 2166
	Elemental Nodes = 0
	Elemental Rods  = 0
	Elemental Tria3 = 0
	Elemental Quad4 = 2166
Combining multiple FEA meshes!
	Combined Number of nodal coordinates = 8672
	Combined Number of elements = 8664
	Combined Elemental Nodes = 0
	Combined Elemental Rods  = 0
	Combined Elemental Tria3 = 0
	Combined Elemental Quad4 = 8664
Updating mesh element types based on properties input

Getting FEA design variables.......
	Number of design variables          - 2
	Design_Variable name - htail:lh
	Design_Variable name - wing:xroot
	Number of design variable relations - 0
	Done getting FEA design variables
--&gt; dCGx [1.94377289e-05]
--&gt; htail:lh   [6.35917671]
--&gt; wing:xroot [7.05983716]
--&gt; dCGx_htail:lh [[-0.00169617]]
--&gt; dCGx_wing:xroot [[-0.00349307]]

At iterate    3    f=  1.94377D-05    |proj g|=  3.49307D-03
--&gt; htail:lh   [6.3642348]
--&gt; wing:xroot [7.06847132]
Mapping Csys attributes ................
	Number of unique Csys attributes = 0

Getting FEA coordinate systems.......
	Number of coordinate systems - 0
	No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
	Number of unique capsConstraint attributes = 0
Mapping capsLoad attributes ................
	Number of unique capsLoad attributes = 0
Mapping capsBound attributes ................
	Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
	Number of unique capsConnect attributes = 0
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 4
	Name = wing, index = 1
	Name = htail, index = 2
	Name = vtail, index = 3
	Name = fuse, index = 4
Setting FEA Data
	Mesh for body = 0
	Number of nodal coordinates = 2168
	Number of elements = 2166
	Elemental Nodes = 0
	Elemental Rods  = 0
	Elemental Tria3 = 0
	Elemental Quad4 = 2166
Setting FEA Data
	Mesh for body = 1
	Number of nodal coordinates = 2168
	Number of elements = 2166
	Elemental Nodes = 0
	Elemental Rods  = 0
	Elemental Tria3 = 0
	Elemental Quad4 = 2166
Setting FEA Data
	Mesh for body = 2
	Number of nodal coordinates = 2168
	Number of elements = 2166
	Elemental Nodes = 0
	Elemental Rods  = 0
	Elemental Tria3 = 0
	Elemental Quad4 = 2166
Setting FEA Data
	Mesh for body = 3
	Number of nodal coordinates = 2168
	Number of elements = 2166
	Elemental Nodes = 0
	Elemental Rods  = 0
	Elemental Tria3 = 0
	Elemental Quad4 = 2166
Combining multiple FEA meshes!
	Combined Number of nodal coordinates = 8672
	Combined Number of elements = 8664
	Combined Elemental Nodes = 0
	Combined Elemental Rods  = 0
	Combined Elemental Tria3 = 0
	Combined Elemental Quad4 = 8664
Updating mesh element types based on properties input

Getting FEA design variables.......
	Number of design variables          - 2
	Design_Variable name - htail:lh
	Design_Variable name - wing:xroot
	Number of design variable relations - 0
	Done getting FEA design variables
--&gt; dCGx [2.31615861e-10]
--&gt; htail:lh   [6.3642348]
--&gt; wing:xroot [7.06847132]
--&gt; dCGx_htail:lh [[-5.85873617e-06]]
--&gt; dCGx_wing:xroot [[-1.20573655e-05]]

At iterate    4    f=  2.31616D-10    |proj g|=  1.20574D-05
--&gt; htail:lh   [6.36425233]
--&gt; wing:xroot [7.06850123]
Mapping Csys attributes ................
	Number of unique Csys attributes = 0

Getting FEA coordinate systems.......
	Number of coordinate systems - 0
	No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
	Number of unique capsConstraint attributes = 0
Mapping capsLoad attributes ................
	Number of unique capsLoad attributes = 0
Mapping capsBound attributes ................
	Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
	Number of unique capsConnect attributes = 0
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 4
	Name = wing, index = 1
	Name = htail, index = 2
	Name = vtail, index = 3
	Name = fuse, index = 4
Setting FEA Data
	Mesh for body = 0
	Number of nodal coordinates = 2168
	Number of elements = 2166
	Elemental Nodes = 0
	Elemental Rods  = 0
	Elemental Tria3 = 0
	Elemental Quad4 = 2166
Setting FEA Data
	Mesh for body = 1
	Number of nodal coordinates = 2168
	Number of elements = 2166
	Elemental Nodes = 0
	Elemental Rods  = 0
	Elemental Tria3 = 0
	Elemental Quad4 = 2166
Setting FEA Data
	Mesh for body = 2
	Number of nodal coordinates = 2168
	Number of elements = 2166
	Elemental Nodes = 0
	Elemental Rods  = 0
	Elemental Tria3 = 0
	Elemental Quad4 = 2166
Setting FEA Data
	Mesh for body = 3
	Number of nodal coordinates = 2168
	Number of elements = 2166
	Elemental Nodes = 0
	Elemental Rods  = 0
	Elemental Tria3 = 0
	Elemental Quad4 = 2166
Combining multiple FEA meshes!
	Combined Number of nodal coordinates = 8672
	Combined Number of elements = 8664
	Combined Elemental Nodes = 0
	Combined Elemental Rods  = 0
	Combined Elemental Tria3 = 0
	Combined Elemental Quad4 = 8664
Updating mesh element types based on properties input

Getting FEA design variables.......
	Number of design variables          - 2
	Design_Variable name - htail:lh
	Design_Variable name - wing:xroot
	Number of design variable relations - 0
	Done getting FEA design variables
--&gt; dCGx [6.3756283e-18]
--&gt; htail:lh   [6.36425233]
--&gt; wing:xroot [7.06850123]
--&gt; dCGx_htail:lh [[9.72035735e-10]]
--&gt; dCGx_wing:xroot [[2.00045928e-09]]

At iterate    5    f=  6.37563D-18    |proj g|=  2.00046D-09

           * * *

Tit   = total number of iterations
Tnf   = total number of function evaluations
Tnint = total number of segments explored during Cauchy searches
Skip  = number of BFGS updates skipped
Nact  = number of active bounds at final generalized Cauchy point
Projg = norm of the final projected gradient
F     = final function value

           * * *

   N    Tit     Tnf  Tnint  Skip  Nact     Projg        F
    2      5      6      5     0     0   2.000D-09   6.376D-18
  F =   6.3756282976940919E-018

CONVERGENCE: REL_REDUCTION_OF_F_&lt;=_FACTR*EPSMCH             
Optimization Complete
-----------------------------------
==&gt; Optimized values:
--&gt; htail:lh   6.3642523342704855
--&gt; wing:xroot 7.068501228645885

real	0m1.292s
user	0m1.782s
sys	0m0.277s
+ status=0
+ set +x

=================================================
solutions/session04/masstran_OpenMDAO_geom.py passed (as expected)
=================================================


=================================================
+ echo 'avlPlaneVanilla.csm test;'
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/CAPS/training/2023/training.log
avlPlaneVanilla.csm test;
+ /Users/jenkins/workspace/ESP_bPreBuilt/ESP126/EngSketchPad/bin/serveESP -batch -verify -outLevel 0 avlPlaneVanilla.csm
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/CAPS/training/2023/training.log
WARNING:: cannot open "./verify_7.8.1/avlPlaneVanilla.vfy", so verification is being skipped
==&gt; serveESP completed successfully with no verification data

real	0m0.218s
user	0m0.225s
sys	0m0.007s
+ status=0
+ set +x

=================================================
data/session06/avlPlaneVanilla passed (as expected)
=================================================


=================================================
1_avl_PlaneVanilla.py test;
+ python 1_avl_PlaneVanilla.py
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/CAPS/training/2023/training.log

==&gt; Loading geometry from file "avlPlaneVanilla.csm"...

==&gt; Viewing Plane Vanilla bodies...

==&gt; Create avlAIM

==&gt; Viewing AVL Plane Vanilla bodies...

==&gt; Setting analysis values
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 3
	Name = Wing, index = 1
	Name = Htail, index = 2
	Name = Vtail, index = 3
Getting vortex lattice surface data
	VLM surface name - Htail
	No "groupName" variable provided or no matches found, going to use tuple name
	VLM surface name - Vtail
	No "groupName" variable provided or no matches found, going to use tuple name
	VLM surface name - Wing
	No "groupName" variable provided or no matches found, going to use tuple name
	Done getting vortex lattice surface data
Warning: Control Elevator not found in controls tuple! Only defaults will be used.
Warning: Control Elevator not found in controls tuple! Only defaults will be used.
Warning: Control Elevator not found in controls tuple! Only defaults will be used.
Warning: Control Rudder not found in controls tuple! Only defaults will be used.
Warning: Control Rudder not found in controls tuple! Only defaults will be used.
Warning: Control AileronRight not found in controls tuple! Only defaults will be used.
Warning: Control AileronLeft not found in controls tuple! Only defaults will be used.
Warning: Control AileronRight not found in controls tuple! Only defaults will be used.
Warning: Control AileronLeft not found in controls tuple! Only defaults will be used.
Writing surface - Htail (ID = 0)
	Section 1 of 3 (ID = 1)
	  Control surface 1 of 1 
	Section 2 of 3 (ID = 0)
	  Control surface 1 of 1 
	Section 3 of 3 (ID = 2)
	  Control surface 1 of 1 
Writing surface - Vtail (ID = 1)
	Section 1 of 2 (ID = 1)
	  Control surface 1 of 1 
	Section 2 of 2 (ID = 0)
	  Control surface 1 of 1 
Writing surface - Wing (ID = 2)
	Section 1 of 3 (ID = 1)
	  Control surface 1 of 1 
	Section 2 of 3 (ID = 0)
	  Control surface 1 of 2 
	  Control surface 2 of 2 
	Section 3 of 3 (ID = 2)
	  Control surface 1 of 1 
--&gt; CLtot = 0.5813612009189711
--&gt; CDtot = 0.006414738598441995
--&gt; CDind = 0.006414738598441995
--&gt; e     = 0.9155417145048229

real	0m0.584s
user	0m0.628s
sys	0m0.258s
+ status=0
+ set +x

=================================================
data/session06/1_avl_PlaneVanilla.py passed (as expected)
=================================================


=================================================
2_avl_PlaneVanillaControl.py test;
+ python 2_avl_PlaneVanillaControl.py
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/CAPS/training/2023/training.log

==&gt; Loading geometry from file "avlPlaneVanilla.csm"...

==&gt; Creating avlAIM

==&gt; Setting analysis values

==&gt; Some stability derivatives (old)
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 3
	Name = Wing, index = 1
	Name = Htail, index = 2
	Name = Vtail, index = 3
Getting vortex lattice control surface data
	VLM control surface name - AileronLeft
	VLM control surface name - AileronRight
	VLM control surface name - Elevator
	VLM control surface name - Rudder
	Done getting vortex lattice control surface data
Getting vortex lattice surface data
	VLM surface name - Htail
	No "groupName" variable provided or no matches found, going to use tuple name
	VLM surface name - Vtail
	No "groupName" variable provided or no matches found, going to use tuple name
	VLM surface name - Wing
	No "groupName" variable provided or no matches found, going to use tuple name
	Done getting vortex lattice surface data
Writing surface - Htail (ID = 0)
	Section 1 of 3 (ID = 1)
	  Control surface 1 of 1 
	Section 2 of 3 (ID = 0)
	  Control surface 1 of 1 
	Section 3 of 3 (ID = 2)
	  Control surface 1 of 1 
Writing surface - Vtail (ID = 1)
	Section 1 of 2 (ID = 1)
	  Control surface 1 of 1 
	Section 2 of 2 (ID = 0)
	  Control surface 1 of 1 
Writing surface - Wing (ID = 2)
	Section 1 of 3 (ID = 1)
	  Control surface 1 of 1 
	Section 2 of 3 (ID = 0)
	  Control surface 1 of 2 
	  Control surface 2 of 2 
	Section 3 of 3 (ID = 2)
	  Control surface 1 of 1 
--&gt; CLa  = 6.186807004014293
--&gt; CLb  = 0.06076552926076213
--&gt; CLp' = 0.07726884270666666
--&gt; CLq' = 11.77186898086249
--&gt; CLr' = 0.9883703770429457
--&gt; dCL/dAileronRight = 0.02247452142379
--&gt; dCL/dAileronLeft  = 0.02252467496153
--&gt; dCL/dElevator     = 0.005432144424891
--&gt; dCL/dRudder       = -2.654018025316e-06

==&gt; Some stability derivatives (new)
--&gt; dCL/dAlpha  = 6.186807004014293
--&gt; dCL/dBeta   = 0.06076552926076213
--&gt; dCL/dp'     = 0.07726884270666666
--&gt; dCL/dq'     = 11.77186898086249
--&gt; dCL/dr'     = 0.9883703770429457
--&gt; dCL/dAileronRight = 0.02247452142379324
--&gt; dCL/dAileronLeft  = 0.02252467496152878
--&gt; dCL/dElevator     = 0.005432144424890901
--&gt; dCL/dRudder       = -2.654018025315729e-06

real	0m0.569s
user	0m0.619s
sys	0m0.256s
+ status=0
+ set +x

=================================================
data/session06/2_avl_PlaneVanillaControl.py passed (as expected)
=================================================


=================================================
3_avl_TransportGeom.py test;
+ python 3_avl_TransportGeom.py
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/CAPS/training/2023/training.log

==&gt; Loading geometry from file "../ESP/transport.csm"...

==&gt; Viewing transport bodies...

MESSAGE:: Building wingOml


MESSAGE:: Building wingHinges


MESSAGE:: Building htailOml


MESSAGE:: Building htailHinges


MESSAGE:: Building vtailOml


MESSAGE:: Building vtailHinges


==&gt; Create AVL aim...

==&gt; Viewing avl bodies...

real	0m9.543s
user	0m9.600s
sys	0m18.086s
+ status=0
+ set +x

=================================================
data/session06/3_avl_TransportGeom.py passed (as expected)
=================================================


=================================================
4_avl_TransportControl.py test;
+ python 4_avl_TransportControl.py
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/CAPS/training/2023/training.log

==&gt; Loading geometry from file "../ESP/transport.csm"...

==&gt; Setting Build Variables and Geometry Values...

==&gt; Creating AVL aim...

MESSAGE:: Building wingOml


MESSAGE:: Building wingHinges


MESSAGE:: Building htailOml


MESSAGE:: Building htailHinges


MESSAGE:: Building vtailOml


MESSAGE:: Building vtailHinges

Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 3
	Name = Wing, index = 1
	Name = Htail, index = 2
	Name = Vtail, index = 3
Getting vortex lattice control surface data
	VLM control surface name - HtailControl_1
	VLM control surface name - VtailControl_1
	VLM control surface name - WingControl_1
	VLM control surface name - WingControl_2
	VLM control surface name - WingControl_3
	VLM control surface name - WingControl_4
	Done getting vortex lattice control surface data
Getting vortex lattice surface data
	VLM surface name - Htail
	No "groupName" variable provided or no matches found, going to use tuple name
	VLM surface name - Vtail
	No "groupName" variable provided or no matches found, going to use tuple name
	VLM surface name - Wing
	No "groupName" variable provided or no matches found, going to use tuple name
	Done getting vortex lattice surface data
Warning: Control htailControl1 not found in controls tuple! Only defaults will be used.
Warning: Control htailControl1 not found in controls tuple! Only defaults will be used.
Warning: Control htailControl1 not found in controls tuple! Only defaults will be used.
Warning: Control htailControl1 not found in controls tuple! Only defaults will be used.
Warning: Control VtailControl1 not found in controls tuple! Only defaults will be used.
Warning: Control VtailControl1 not found in controls tuple! Only defaults will be used.
Warning: Control WingControl1 not found in controls tuple! Only defaults will be used.
Warning: Control WingControl1 not found in controls tuple! Only defaults will be used.
Warning: Control WingControl2 not found in controls tuple! Only defaults will be used.
Warning: Control WingControl2 not found in controls tuple! Only defaults will be used.
Warning: Control WingControl3 not found in controls tuple! Only defaults will be used.
Warning: Control WingControl3 not found in controls tuple! Only defaults will be used.
Warning: Control WingControl3 not found in controls tuple! Only defaults will be used.
Warning: Control WingControl3 not found in controls tuple! Only defaults will be used.
Warning: Control WingControl2 not found in controls tuple! Only defaults will be used.
Warning: Control WingControl2 not found in controls tuple! Only defaults will be used.
Warning: Control WingControl4 not found in controls tuple! Only defaults will be used.
Warning: Control WingControl4 not found in controls tuple! Only defaults will be used.
Writing surface - Htail (ID = 0)
	Section 1 of 7 (ID = 0)
	Section 2 of 7 (ID = 3)
	  Control surface 1 of 1 
	Section 3 of 7 (ID = 4)
	  Control surface 1 of 1 
	Section 4 of 7 (ID = 1)
	Section 5 of 7 (ID = 5)
	  Control surface 1 of 1 
	Section 6 of 7 (ID = 6)
	  Control surface 1 of 1 
	Section 7 of 7 (ID = 2)
Writing surface - Vtail (ID = 1)
	Section 1 of 4 (ID = 1)
	Section 2 of 4 (ID = 3)
	  Control surface 1 of 1 
	Section 3 of 4 (ID = 2)
	  Control surface 1 of 1 
	Section 4 of 4 (ID = 0)
Writing surface - Wing (ID = 2)
	Section 1 of 17 (ID = 0)
	Section 2 of 17 (ID = 5)
	  Control surface 1 of 1 
	Section 3 of 17 (ID = 6)
	  Control surface 1 of 1 
	Section 4 of 17 (ID = 7)
	  Control surface 1 of 1 
	Section 5 of 17 (ID = 8)
	  Control surface 1 of 1 
	Section 6 of 17 (ID = 4)
	Section 7 of 17 (ID = 9)
	  Control surface 1 of 1 
	Section 8 of 17 (ID = 10)
	  Control surface 1 of 1 
	Section 9 of 17 (ID = 1)
	Section 10 of 17 (ID = 11)
	  Control surface 1 of 1 
	Section 11 of 17 (ID = 12)
	  Control surface 1 of 1 
	Section 12 of 17 (ID = 3)
	Section 13 of 17 (ID = 13)
	  Control surface 1 of 1 
	Section 14 of 17 (ID = 14)
	  Control surface 1 of 1 
	Section 15 of 17 (ID = 15)
	  Control surface 1 of 1 
	Section 16 of 17 (ID = 16)
	  Control surface 1 of 1 
	Section 17 of 17 (ID = 2)

==&gt; Some stability derivatives
--&gt; CLa  = 5.329630947526096
--&gt; CLb  = 4.550909963080161e-09
--&gt; CLp' = -1.341952384696066e-09
--&gt; CLq' = 28.72846815689969
--&gt; CLr' = -3.260899281924948e-09
--&gt; Xcg =  55.4263
--&gt; Xnp =  91.29113395768172
--&gt; StaticMargin =  1.6523694274698266
--&gt; htailControl1 {'CLtot': 0.008154370130359, 'CYtot': -9.150042215949e-11, "Cl'tot": -4.341969980189e-12, 'Cmtot': -0.03748884158765, "Cn'tot": 5.676266392608e-11, 'CDff': 0.001133243748512, 'e': -0.003225846838851}
--&gt; VtailControl1 {'CLtot': -3.394363229977e-11, 'CYtot': 0.001746902759648, "Cl'tot": 0.00015788879711, 'Cmtot': 1.638782106979e-10, "Cn'tot": -0.0009155267227964, 'CDff': 7.439468599435e-12, 'e': -9.055415862979e-11}
--&gt; WingControl1 {'CLtot': 0.00245427242356, 'CYtot': 0.0001047561004524, "Cl'tot": 0.0008699288737981, 'Cmtot': -0.006084028421025, "Cn'tot": 0.0001105827384316, 'CDff': 4.762247994044e-05, 'e': 0.002671724673481}
--&gt; WingControl2 {'CLtot': 0.00887521630351, 'CYtot': -6.354525089904e-12, "Cl'tot": -1.792994381086e-13, 'Cmtot': -0.01681583906716, "Cn'tot": 3.382459389563e-12, 'CDff': 0.0003695424562226, 'e': 0.007231117327731}
--&gt; WingControl3 {'CLtot': 0.005956182076864, 'CYtot': 1.810237567303e-11, "Cl'tot": 7.034779654232e-13, 'Cmtot': -0.005500424410978, "Cn'tot": -1.104493635082e-11, 'CDff': 0.0007054645324542, 'e': -0.0007874262410477}
--&gt; WingControl4 {'CLtot': 0.002454272422219, 'CYtot': -0.0001047561036864, "Cl'tot": -0.000869928873921, 'Cmtot': -0.006084028416179, "Cn'tot": -0.0001105827366425, 'CDff': 4.762247984573e-05, 'e': 0.002671724673447}

real	0m9.959s
user	0m9.978s
sys	0m18.245s
+ status=0
+ set +x

=================================================
data/session06/4_avl_TransportControl.py passed (as expected)
=================================================


=================================================
5_avl_TransportEigen.py test;
+ python 5_avl_TransportEigen.py
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/CAPS/training/2023/training.log

==&gt; Loading geometry from file "../ESP/transport.csm"...

==&gt; Setting Build Variables and Geometry Values...

==&gt; Create AVL aim...

==&gt; Running Analysis

MESSAGE:: Building wingOml


MESSAGE:: Building htailOml


MESSAGE:: Building vtailOml

Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 3
	Name = Wing, index = 1
	Name = Htail, index = 2
	Name = Vtail, index = 3
Getting vortex lattice surface data
	VLM surface name - Htail
	No "groupName" variable provided or no matches found, going to use tuple name
	VLM surface name - Vtail
	No "groupName" variable provided or no matches found, going to use tuple name
	VLM surface name - Wing
	No "groupName" variable provided or no matches found, going to use tuple name
	Done getting vortex lattice surface data
Writing surface - Htail (ID = 0)
	Section 1 of 3 (ID = 0)
	Section 2 of 3 (ID = 1)
	Section 3 of 3 (ID = 2)
Writing surface - Vtail (ID = 1)
	Section 1 of 2 (ID = 1)
	Section 2 of 2 (ID = 0)
Writing surface - Wing (ID = 2)
	Section 1 of 5 (ID = 0)
	Section 2 of 5 (ID = 4)
	Section 3 of 5 (ID = 1)
	Section 4 of 5 (ID = 3)
	Section 5 of 5 (ID = 2)
Writing mass properties file: caps.mass
Parsing MassProp
Note: The following floating-point exceptions are signalling: IEEE_DIVIDE_BY_ZERO

==&gt; Outputs
--&gt; Xcg =  89.3122 meter
--&gt; Xnp =  92.43912771102477 meter
--&gt; StaticMargin =  0.472651679029349
--&gt; EigenValues  {'case 1': [[-3.1240286, 0.0], [0.019757061, 0.97330897], [0.019757061, -0.97330897], [-0.01302709, 0.0], [-0.32616585, 0.92439209], [-0.32616585, -0.92439209], [-0.013243777, 0.13183874], [-0.013243777, -0.13183874]]}

--&gt; Real Eigen Values = [-3.1240286, 0.019757061, 0.019757061, -0.01302709, -0.32616585, -0.32616585, -0.013243777, -0.013243777]

real	0m2.962s
user	0m2.697s
sys	0m4.051s
+ status=0
+ set +x

=================================================
data/session06/5_avl_TransportEigen.py passed (as expected)
=================================================


=================================================
6_avl_masstran_Geom.py test;
+ python 6_avl_masstran_Geom.py
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/CAPS/training/2023/training.log

==&gt; Loading geometry from file "../ESP/transport.csm"...

==&gt; Vewing AVL geometry

MESSAGE:: Building wingOml


MESSAGE:: Building htailOml


MESSAGE:: Building vtailOml


MESSAGE:: Building fuseOml


==&gt; Vewing Masstran geometry

real	0m2.857s
user	0m2.458s
sys	0m4.201s
+ status=0
+ set +x

=================================================
data/session06/6_avl_masstran_Geom.py passed (as expected)
=================================================


=================================================
7_avl_masstran_Eigen.py test;
+ python 7_avl_masstran_Eigen.py
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/CAPS/training/2023/training.log

==&gt; Loading geometry from file "../ESP/transport.csm"...

==&gt; Setting Build Variables and Geometry Values...

==&gt; Creating masstran aim...

==&gt; Creating AVL aim...

==&gt; Running Analysis

MESSAGE:: Building wingOml


MESSAGE:: Building htailOml


MESSAGE:: Building vtailOml


MESSAGE:: Building fuseOml

Mapping Csys attributes ................
	Number of unique Csys attributes = 0

Getting FEA coordinate systems.......
	Number of coordinate systems - 0
	No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
	Number of unique capsConstraint attributes = 0
Mapping capsLoad attributes ................
	Number of unique capsLoad attributes = 0
Mapping capsBound attributes ................
	Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
	Number of unique capsConnect attributes = 0
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 4
	Name = wingSkin, index = 1
	Name = fuseSkin, index = 2
	Name = htailSkin, index = 3
	Name = vtailSkin, index = 4
Setting FEA Data
	Mesh for body = 0
	Number of nodal coordinates = 5622
	Number of elements = 11240
	Elemental Nodes = 0
	Elemental Rods  = 0
	Elemental Tria3 = 11240
	Elemental Quad4 = 0
Setting FEA Data
	Mesh for body = 1
	Number of nodal coordinates = 5460
	Number of elements = 10916
	Elemental Nodes = 0
	Elemental Rods  = 0
	Elemental Tria3 = 10916
	Elemental Quad4 = 0
Setting FEA Data
	Mesh for body = 2
	Number of nodal coordinates = 5144
	Number of elements = 10284
	Elemental Nodes = 0
	Elemental Rods  = 0
	Elemental Tria3 = 10284
	Elemental Quad4 = 0
Setting FEA Data
	Mesh for body = 3
	Number of nodal coordinates = 2722
	Number of elements = 5440
	Elemental Nodes = 0
	Elemental Rods  = 0
	Elemental Tria3 = 5440
	Elemental Quad4 = 0
Combining multiple FEA meshes!
	Combined Number of nodal coordinates = 18948
	Combined Number of elements = 37880
	Combined Elemental Nodes = 0
	Combined Elemental Rods  = 0
	Combined Elemental Tria3 = 37880
	Combined Elemental Quad4 = 0

Getting FEA materials.......
	Number of materials - 1
	Material name - Unobtainium
	No "materialType" specified for Material tuple Unobtainium, defaulting to "Isotropic"
	Done getting FEA materials

Getting FEA properties.......
	Number of properties - 4
	Property name - fuseSkin
	Property name - htailSkin
	Property name - vtailSkin
	Property name - wingSkin
	Done getting FEA properties
Updating mesh element types based on properties input
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 3
	Name = Wing, index = 1
	Name = Htail, index = 2
	Name = Vtail, index = 3
Getting vortex lattice surface data
	VLM surface name - Htail
	No "groupName" variable provided or no matches found, going to use tuple name
	VLM surface name - Vtail
	No "groupName" variable provided or no matches found, going to use tuple name
	VLM surface name - Wing
	No "groupName" variable provided or no matches found, going to use tuple name
	Done getting vortex lattice surface data
Writing surface - Htail (ID = 0)
	Section 1 of 3 (ID = 0)
	Section 2 of 3 (ID = 1)
	Section 3 of 3 (ID = 2)
Writing surface - Vtail (ID = 1)
	Section 1 of 2 (ID = 1)
	Section 2 of 2 (ID = 0)
Writing surface - Wing (ID = 2)
	Section 1 of 5 (ID = 0)
	Section 2 of 5 (ID = 4)
	Section 3 of 5 (ID = 1)
	Section 4 of 5 (ID = 3)
	Section 5 of 5 (ID = 2)
Writing mass properties file: caps.mass
Parsing MassProp
Note: The following floating-point exceptions are signalling: IEEE_DIVIDE_BY_ZERO

==&gt; Outputs
--&gt; Xcg =  89.6972 meter
--&gt; Xnp =  92.42424816606338 meter
--&gt; StaticMargin =  0.41220776864756814
--&gt; EigenValues  {'case 1': [[-0.70464716, 0.0], [0.13847231, 0.55144718], [0.13847231, -0.55144718], [-0.16139632, 0.51326027], [-0.16139632, -0.51326027], [-0.0068175359, 0.0], [-0.0164897, 0.12092115], [-0.0164897, -0.12092115]]}

--&gt; Real Eigen Values = [-0.70464716, 0.13847231, 0.13847231, -0.16139632, -0.16139632, -0.0068175359, -0.0164897, -0.0164897]

real	0m4.491s
user	0m4.539s
sys	0m4.238s
+ status=0
+ set +x

=================================================
data/session06/7_avl_masstran_Eigen.py passed (as expected)
=================================================


=================================================
8_avl_friction_Link.py test;
+ python 8_avl_friction_Link.py
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/CAPS/training/2023/training.log

==&gt; Loading geometry from file "../ESP/transport.csm"...

MESSAGE:: Building wingOml


MESSAGE:: Building htailOml


MESSAGE:: Building vtailOml

Lifting Surface: Body = 1, units ft
	XLE:   118.390617 -97.671924 3.992604
	XTE:   123.551941 -97.671924 4.717949
	Chord: 5.212043
	Arc:   10.531921
	T/C:   0.153243
	Type: Wing
Lifting Surface: Body = 2, units ft
	XLE:   50.000000 0.000000 -8.000000
	XTE:   97.200785 -0.000000 -7.176107
	Chord: 47.207975
	Arc:   97.395848
	T/C:   0.145499
	Type: Wing
Lifting Surface: Body = 3, units ft
	XLE:   118.390617 97.671924 3.992604
	XTE:   123.551941 97.671924 4.717949
	Chord: 5.212043
	Arc:   10.531921
	T/C:   0.153243
	Type: Wing
Lifting Surface: Body = 4, units ft
	XLE:   75.304787 36.138982 -3.562691
	XTE:   97.933561 36.138982 -2.376767
	Chord: 22.659828
	Arc:   46.801094
	T/C:   0.167991
	Type: Wing
Lifting Surface: Body = 5, units ft
	XLE:   75.304787 -36.138982 -3.562691
	XTE:   97.933561 -36.138982 -2.376767
	Chord: 22.659828
	Arc:   46.801094
	T/C:   0.167991
	Type: Wing
Lifting Surface: Body = 6, units ft
	XLE:   165.023151 -35.780198 13.605316
	XTE:   173.282263 -35.780198 13.605316
	Chord: 8.259112
	Arc:   16.684575
	T/C:   0.080010
	Type: Horizontal_Tail
Lifting Surface: Body = 7, units ft
	XLE:   135.000000 0.000000 6.000000
	XTE:   160.026192 -0.000000 6.000000
	Chord: 25.026192
	Arc:   50.556450
	T/C:   0.080010
	Type: Horizontal_Tail
Lifting Surface: Body = 8, units ft
	XLE:   165.023151 35.780198 13.605316
	XTE:   173.282263 35.780198 13.605316
	Chord: 8.259112
	Arc:   16.684575
	T/C:   0.080010
	Type: Horizontal_Tail
Lifting Surface: Body = 9, units ft
	XLE:   136.456162 0.000000 9.001500
	XTE:   159.447890 -0.000000 9.001500
	Chord: 22.991728
	Arc:   46.446544
	T/C:   0.080010
	Type: Vertical_Tail
Lifting Surface: Body = 10, units ft
	XLE:   162.940713 0.000000 35.486051
	XTE:   169.379597 -0.000000 35.486051
	Chord: 6.438884
	Arc:   13.007456
	T/C:   0.080010
	Type: Vertical_Tail
Number of sections 7, number of revolution sections 0
Number of Mach-Altitude cases = 1
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 3
	Name = Wing, index = 1
	Name = Htail, index = 2
	Name = Vtail, index = 3
Getting vortex lattice surface data
	VLM surface name - Htail
	No "groupName" variable provided or no matches found, going to use tuple name
	VLM surface name - Vtail
	No "groupName" variable provided or no matches found, going to use tuple name
	VLM surface name - Wing
	No "groupName" variable provided or no matches found, going to use tuple name
	Done getting vortex lattice surface data
Writing surface - Htail (ID = 0)
	Section 1 of 3 (ID = 0)
	Section 2 of 3 (ID = 1)
	Section 3 of 3 (ID = 2)
Writing surface - Vtail (ID = 1)
	Section 1 of 2 (ID = 1)
	Section 2 of 2 (ID = 0)
Writing surface - Wing (ID = 2)
	Section 1 of 5 (ID = 0)
	Section 2 of 5 (ID = 4)
	Section 3 of 5 (ID = 1)
	Section 4 of 5 (ID = 3)
	Section 5 of 5 (ID = 2)
Lifting Surface: Body = 1, units ft
	XLE:   118.390617 -97.671924 3.992604
	XTE:   123.551941 -97.671924 4.717949
	Chord: 5.212043
	Arc:   10.531921
	T/C:   0.153243
	Type: Wing
Lifting Surface: Body = 2, units ft
	XLE:   50.000000 0.000000 -8.000000
	XTE:   97.200785 -0.000000 -7.176107
	Chord: 47.207975
	Arc:   97.395848
	T/C:   0.145499
	Type: Wing
Lifting Surface: Body = 3, units ft
	XLE:   118.390617 97.671924 3.992604
	XTE:   123.551941 97.671924 4.717949
	Chord: 5.212043
	Arc:   10.531921
	T/C:   0.153243
	Type: Wing
Lifting Surface: Body = 4, units ft
	XLE:   75.304787 36.138982 -3.562691
	XTE:   97.933561 36.138982 -2.376767
	Chord: 22.659828
	Arc:   46.801094
	T/C:   0.167991
	Type: Wing
Lifting Surface: Body = 5, units ft
	XLE:   75.304787 -36.138982 -3.562691
	XTE:   97.933561 -36.138982 -2.376767
	Chord: 22.659828
	Arc:   46.801094
	T/C:   0.167991
	Type: Wing
Lifting Surface: Body = 6, units ft
	XLE:   165.023151 -35.780198 13.605316
	XTE:   173.282263 -35.780198 13.605316
	Chord: 8.259112
	Arc:   16.684575
	T/C:   0.080010
	Type: Horizontal_Tail
Lifting Surface: Body = 7, units ft
	XLE:   135.000000 0.000000 6.000000
	XTE:   160.026192 -0.000000 6.000000
	Chord: 25.026192
	Arc:   50.556450
	T/C:   0.080010
	Type: Horizontal_Tail
Lifting Surface: Body = 8, units ft
	XLE:   165.023151 35.780198 13.605316
	XTE:   173.282263 35.780198 13.605316
	Chord: 8.259112
	Arc:   16.684575
	T/C:   0.080010
	Type: Horizontal_Tail
Lifting Surface: Body = 9, units ft
	XLE:   136.456162 0.000000 9.001500
	XTE:   159.447890 -0.000000 9.001500
	Chord: 22.991728
	Arc:   46.446544
	T/C:   0.080010
	Type: Vertical_Tail
Lifting Surface: Body = 10, units ft
	XLE:   162.940713 0.000000 35.486051
	XTE:   169.379597 -0.000000 35.486051
	Chord: 6.438884
	Arc:   13.007456
	T/C:   0.080010
	Type: Vertical_Tail
Number of sections 7, number of revolution sections 0
Number of Mach-Altitude cases = 1
Writing surface - Htail (ID = 0)
	Section 1 of 3 (ID = 0)
	Section 2 of 3 (ID = 1)
	Section 3 of 3 (ID = 2)
Writing surface - Vtail (ID = 1)
	Section 1 of 2 (ID = 1)
	Section 2 of 2 (ID = 0)
Writing surface - Wing (ID = 2)
	Section 1 of 5 (ID = 0)
	Section 2 of 5 (ID = 4)
	Section 3 of 5 (ID = 1)
	Section 4 of 5 (ID = 3)
	Section 5 of 5 (ID = 2)
Lifting Surface: Body = 1, units ft
	XLE:   118.390617 -97.671924 3.992604
	XTE:   123.551941 -97.671924 4.717949
	Chord: 5.212043
	Arc:   10.531921
	T/C:   0.153243
	Type: Wing
Lifting Surface: Body = 2, units ft
	XLE:   50.000000 0.000000 -8.000000
	XTE:   97.200785 -0.000000 -7.176107
	Chord: 47.207975
	Arc:   97.395848
	T/C:   0.145499
	Type: Wing
Lifting Surface: Body = 3, units ft
	XLE:   118.390617 97.671924 3.992604
	XTE:   123.551941 97.671924 4.717949
	Chord: 5.212043
	Arc:   10.531921
	T/C:   0.153243
	Type: Wing
Lifting Surface: Body = 4, units ft
	XLE:   75.304787 36.138982 -3.562691
	XTE:   97.933561 36.138982 -2.376767
	Chord: 22.659828
	Arc:   46.801094
	T/C:   0.167991
	Type: Wing
Lifting Surface: Body = 5, units ft
	XLE:   75.304787 -36.138982 -3.562691
	XTE:   97.933561 -36.138982 -2.376767
	Chord: 22.659828
	Arc:   46.801094
	T/C:   0.167991
	Type: Wing
Lifting Surface: Body = 6, units ft
	XLE:   165.023151 -35.780198 13.605316
	XTE:   173.282263 -35.780198 13.605316
	Chord: 8.259112
	Arc:   16.684575
	T/C:   0.080010
	Type: Horizontal_Tail
Lifting Surface: Body = 7, units ft
	XLE:   135.000000 0.000000 6.000000
	XTE:   160.026192 -0.000000 6.000000
	Chord: 25.026192
	Arc:   50.556450
	T/C:   0.080010
	Type: Horizontal_Tail
Lifting Surface: Body = 8, units ft
	XLE:   165.023151 35.780198 13.605316
	XTE:   173.282263 35.780198 13.605316
	Chord: 8.259112
	Arc:   16.684575
	T/C:   0.080010
	Type: Horizontal_Tail
Lifting Surface: Body = 9, units ft
	XLE:   136.456162 0.000000 9.001500
	XTE:   159.447890 -0.000000 9.001500
	Chord: 22.991728
	Arc:   46.446544
	T/C:   0.080010
	Type: Vertical_Tail
Lifting Surface: Body = 10, units ft
	XLE:   162.940713 0.000000 35.486051
	XTE:   169.379597 -0.000000 35.486051
	Chord: 6.438884
	Arc:   13.007456
	T/C:   0.080010
	Type: Vertical_Tail
Number of sections 7, number of revolution sections 0
Number of Mach-Altitude cases = 1
Writing surface - Htail (ID = 0)
	Section 1 of 3 (ID = 0)
	Section 2 of 3 (ID = 1)
	Section 3 of 3 (ID = 2)
Writing surface - Vtail (ID = 1)
	Section 1 of 2 (ID = 1)
	Section 2 of 2 (ID = 0)
Writing surface - Wing (ID = 2)
	Section 1 of 5 (ID = 0)
	Section 2 of 5 (ID = 4)
	Section 3 of 5 (ID = 1)
	Section 4 of 5 (ID = 3)
	Section 5 of 5 (ID = 2)
Lifting Surface: Body = 1, units ft
	XLE:   118.390617 -97.671924 3.992604
	XTE:   123.551941 -97.671924 4.717949
	Chord: 5.212043
	Arc:   10.531921
	T/C:   0.153243
	Type: Wing
Lifting Surface: Body = 2, units ft
	XLE:   50.000000 0.000000 -8.000000
	XTE:   97.200785 -0.000000 -7.176107
	Chord: 47.207975
	Arc:   97.395848
	T/C:   0.145499
	Type: Wing
Lifting Surface: Body = 3, units ft
	XLE:   118.390617 97.671924 3.992604
	XTE:   123.551941 97.671924 4.717949
	Chord: 5.212043
	Arc:   10.531921
	T/C:   0.153243
	Type: Wing
Lifting Surface: Body = 4, units ft
	XLE:   75.304787 36.138982 -3.562691
	XTE:   97.933561 36.138982 -2.376767
	Chord: 22.659828
	Arc:   46.801094
	T/C:   0.167991
	Type: Wing
Lifting Surface: Body = 5, units ft
	XLE:   75.304787 -36.138982 -3.562691
	XTE:   97.933561 -36.138982 -2.376767
	Chord: 22.659828
	Arc:   46.801094
	T/C:   0.167991
	Type: Wing
Lifting Surface: Body = 6, units ft
	XLE:   165.023151 -35.780198 13.605316
	XTE:   173.282263 -35.780198 13.605316
	Chord: 8.259112
	Arc:   16.684575
	T/C:   0.080010
	Type: Horizontal_Tail
Lifting Surface: Body = 7, units ft
	XLE:   135.000000 0.000000 6.000000
	XTE:   160.026192 -0.000000 6.000000
	Chord: 25.026192
	Arc:   50.556450
	T/C:   0.080010
	Type: Horizontal_Tail
Lifting Surface: Body = 8, units ft
	XLE:   165.023151 35.780198 13.605316
	XTE:   173.282263 35.780198 13.605316
	Chord: 8.259112
	Arc:   16.684575
	T/C:   0.080010
	Type: Horizontal_Tail
Lifting Surface: Body = 9, units ft
	XLE:   136.456162 0.000000 9.001500
	XTE:   159.447890 -0.000000 9.001500
	Chord: 22.991728
	Arc:   46.446544
	T/C:   0.080010
	Type: Vertical_Tail
Lifting Surface: Body = 10, units ft
	XLE:   162.940713 0.000000 35.486051
	XTE:   169.379597 -0.000000 35.486051
	Chord: 6.438884
	Arc:   13.007456
	T/C:   0.080010
	Type: Vertical_Tail
Number of sections 7, number of revolution sections 0
Number of Mach-Altitude cases = 1
Writing surface - Htail (ID = 0)
	Section 1 of 3 (ID = 0)
	Section 2 of 3 (ID = 1)
	Section 3 of 3 (ID = 2)
Writing surface - Vtail (ID = 1)
	Section 1 of 2 (ID = 1)
	Section 2 of 2 (ID = 0)
Writing surface - Wing (ID = 2)
	Section 1 of 5 (ID = 0)
	Section 2 of 5 (ID = 4)
	Section 3 of 5 (ID = 1)
	Section 4 of 5 (ID = 3)
	Section 5 of 5 (ID = 2)
Lifting Surface: Body = 1, units ft
	XLE:   118.390617 -97.671924 3.992604
	XTE:   123.551941 -97.671924 4.717949
	Chord: 5.212043
	Arc:   10.531921
	T/C:   0.153243
	Type: Wing
Lifting Surface: Body = 2, units ft
	XLE:   50.000000 0.000000 -8.000000
	XTE:   97.200785 -0.000000 -7.176107
	Chord: 47.207975
	Arc:   97.395848
	T/C:   0.145499
	Type: Wing
Lifting Surface: Body = 3, units ft
	XLE:   118.390617 97.671924 3.992604
	XTE:   123.551941 97.671924 4.717949
	Chord: 5.212043
	Arc:   10.531921
	T/C:   0.153243
	Type: Wing
Lifting Surface: Body = 4, units ft
	XLE:   75.304787 36.138982 -3.562691
	XTE:   97.933561 36.138982 -2.376767
	Chord: 22.659828
	Arc:   46.801094
	T/C:   0.167991
	Type: Wing
Lifting Surface: Body = 5, units ft
	XLE:   75.304787 -36.138982 -3.562691
	XTE:   97.933561 -36.138982 -2.376767
	Chord: 22.659828
	Arc:   46.801094
	T/C:   0.167991
	Type: Wing
Lifting Surface: Body = 6, units ft
	XLE:   165.023151 -35.780198 13.605316
	XTE:   173.282263 -35.780198 13.605316
	Chord: 8.259112
	Arc:   16.684575
	T/C:   0.080010
	Type: Horizontal_Tail
Lifting Surface: Body = 7, units ft
	XLE:   135.000000 0.000000 6.000000
	XTE:   160.026192 -0.000000 6.000000
	Chord: 25.026192
	Arc:   50.556450
	T/C:   0.080010
	Type: Horizontal_Tail
Lifting Surface: Body = 8, units ft
	XLE:   165.023151 35.780198 13.605316
	XTE:   173.282263 35.780198 13.605316
	Chord: 8.259112
	Arc:   16.684575
	T/C:   0.080010
	Type: Horizontal_Tail
Lifting Surface: Body = 9, units ft
	XLE:   136.456162 0.000000 9.001500
	XTE:   159.447890 -0.000000 9.001500
	Chord: 22.991728
	Arc:   46.446544
	T/C:   0.080010
	Type: Vertical_Tail
Lifting Surface: Body = 10, units ft
	XLE:   162.940713 0.000000 35.486051
	XTE:   169.379597 -0.000000 35.486051
	Chord: 6.438884
	Arc:   13.007456
	T/C:   0.080010
	Type: Vertical_Tail
Number of sections 7, number of revolution sections 0
Number of Mach-Altitude cases = 1
Writing surface - Htail (ID = 0)
	Section 1 of 3 (ID = 0)
	Section 2 of 3 (ID = 1)
	Section 3 of 3 (ID = 2)
Writing surface - Vtail (ID = 1)
	Section 1 of 2 (ID = 1)
	Section 2 of 2 (ID = 0)
Writing surface - Wing (ID = 2)
	Section 1 of 5 (ID = 0)
	Section 2 of 5 (ID = 4)
	Section 3 of 5 (ID = 1)
	Section 4 of 5 (ID = 3)
	Section 5 of 5 (ID = 2)
Lifting Surface: Body = 1, units ft
	XLE:   118.390617 -97.671924 3.992604
	XTE:   123.551941 -97.671924 4.717949
	Chord: 5.212043
	Arc:   10.531921
	T/C:   0.153243
	Type: Wing
Lifting Surface: Body = 2, units ft
	XLE:   50.000000 0.000000 -8.000000
	XTE:   97.200785 -0.000000 -7.176107
	Chord: 47.207975
	Arc:   97.395848
	T/C:   0.145499
	Type: Wing
Lifting Surface: Body = 3, units ft
	XLE:   118.390617 97.671924 3.992604
	XTE:   123.551941 97.671924 4.717949
	Chord: 5.212043
	Arc:   10.531921
	T/C:   0.153243
	Type: Wing
Lifting Surface: Body = 4, units ft
	XLE:   75.304787 36.138982 -3.562691
	XTE:   97.933561 36.138982 -2.376767
	Chord: 22.659828
	Arc:   46.801094
	T/C:   0.167991
	Type: Wing
Lifting Surface: Body = 5, units ft
	XLE:   75.304787 -36.138982 -3.562691
	XTE:   97.933561 -36.138982 -2.376767
	Chord: 22.659828
	Arc:   46.801094
	T/C:   0.167991
	Type: Wing
Lifting Surface: Body = 6, units ft
	XLE:   165.023151 -35.780198 13.605316
	XTE:   173.282263 -35.780198 13.605316
	Chord: 8.259112
	Arc:   16.684575
	T/C:   0.080010
	Type: Horizontal_Tail
Lifting Surface: Body = 7, units ft
	XLE:   135.000000 0.000000 6.000000
	XTE:   160.026192 -0.000000 6.000000
	Chord: 25.026192
	Arc:   50.556450
	T/C:   0.080010
	Type: Horizontal_Tail
Lifting Surface: Body = 8, units ft
	XLE:   165.023151 35.780198 13.605316
	XTE:   173.282263 35.780198 13.605316
	Chord: 8.259112
	Arc:   16.684575
	T/C:   0.080010
	Type: Horizontal_Tail
Lifting Surface: Body = 9, units ft
	XLE:   136.456162 0.000000 9.001500
	XTE:   159.447890 -0.000000 9.001500
	Chord: 22.991728
	Arc:   46.446544
	T/C:   0.080010
	Type: Vertical_Tail
Lifting Surface: Body = 10, units ft
	XLE:   162.940713 0.000000 35.486051
	XTE:   169.379597 -0.000000 35.486051
	Chord: 6.438884
	Arc:   13.007456
	T/C:   0.080010
	Type: Vertical_Tail
Number of sections 7, number of revolution sections 0
Number of Mach-Altitude cases = 1
Writing surface - Htail (ID = 0)
	Section 1 of 3 (ID = 0)
	Section 2 of 3 (ID = 1)
	Section 3 of 3 (ID = 2)
Writing surface - Vtail (ID = 1)
	Section 1 of 2 (ID = 1)
	Section 2 of 2 (ID = 0)
Writing surface - Wing (ID = 2)
	Section 1 of 5 (ID = 0)
	Section 2 of 5 (ID = 4)
	Section 3 of 5 (ID = 1)
	Section 4 of 5 (ID = 3)
	Section 5 of 5 (ID = 2)
Lifting Surface: Body = 1, units ft
	XLE:   118.390617 -97.671924 3.992604
	XTE:   123.551941 -97.671924 4.717949
	Chord: 5.212043
	Arc:   10.531921
	T/C:   0.153243
	Type: Wing
Lifting Surface: Body = 2, units ft
	XLE:   50.000000 0.000000 -8.000000
	XTE:   97.200785 -0.000000 -7.176107
	Chord: 47.207975
	Arc:   97.395848
	T/C:   0.145499
	Type: Wing
Lifting Surface: Body = 3, units ft
	XLE:   118.390617 97.671924 3.992604
	XTE:   123.551941 97.671924 4.717949
	Chord: 5.212043
	Arc:   10.531921
	T/C:   0.153243
	Type: Wing
Lifting Surface: Body = 4, units ft
	XLE:   75.304787 36.138982 -3.562691
	XTE:   97.933561 36.138982 -2.376767
	Chord: 22.659828
	Arc:   46.801094
	T/C:   0.167991
	Type: Wing
Lifting Surface: Body = 5, units ft
	XLE:   75.304787 -36.138982 -3.562691
	XTE:   97.933561 -36.138982 -2.376767
	Chord: 22.659828
	Arc:   46.801094
	T/C:   0.167991
	Type: Wing
Lifting Surface: Body = 6, units ft
	XLE:   165.023151 -35.780198 13.605316
	XTE:   173.282263 -35.780198 13.605316
	Chord: 8.259112
	Arc:   16.684575
	T/C:   0.080010
	Type: Horizontal_Tail
Lifting Surface: Body = 7, units ft
	XLE:   135.000000 0.000000 6.000000
	XTE:   160.026192 -0.000000 6.000000
	Chord: 25.026192
	Arc:   50.556450
	T/C:   0.080010
	Type: Horizontal_Tail
Lifting Surface: Body = 8, units ft
	XLE:   165.023151 35.780198 13.605316
	XTE:   173.282263 35.780198 13.605316
	Chord: 8.259112
	Arc:   16.684575
	T/C:   0.080010
	Type: Horizontal_Tail
Lifting Surface: Body = 9, units ft
	XLE:   136.456162 0.000000 9.001500
	XTE:   159.447890 -0.000000 9.001500
	Chord: 22.991728
	Arc:   46.446544
	T/C:   0.080010
	Type: Vertical_Tail
Lifting Surface: Body = 10, units ft
	XLE:   162.940713 0.000000 35.486051
	XTE:   169.379597 -0.000000 35.486051
	Chord: 6.438884
	Arc:   13.007456
	T/C:   0.080010
	Type: Vertical_Tail
Number of sections 7, number of revolution sections 0
Number of Mach-Altitude cases = 1
Writing surface - Htail (ID = 0)
	Section 1 of 3 (ID = 0)
	Section 2 of 3 (ID = 1)
	Section 3 of 3 (ID = 2)
Writing surface - Vtail (ID = 1)
	Section 1 of 2 (ID = 1)
	Section 2 of 2 (ID = 0)
Writing surface - Wing (ID = 2)
	Section 1 of 5 (ID = 0)
	Section 2 of 5 (ID = 4)
	Section 3 of 5 (ID = 1)
	Section 4 of 5 (ID = 3)
	Section 5 of 5 (ID = 2)

--&gt; Mach = [0.1, 0.2, 0.30000000000000004, 0.4, 0.5, 0.6, 0.7000000000000001]
--&gt; CDp  = [0.01592, 0.01416, 0.01323, 0.01259, 0.01209, 0.01167, 0.0113]
--&gt; CD   = [0.02455060220988743, 0.02466896350126657, 0.02487666257532763, 0.02519203549494272, 0.02564765931512183, 0.02630248998864366, 0.02727263653466326]


real	0m5.296s
user	0m4.508s
sys	0m4.509s
+ status=0
+ set +x

=================================================
data/session06/8_avl_friction_Link.py passed (as expected)
=================================================


=================================================
avl_masstran_MainGear.py test;
+ python avl_masstran_MainGear.py
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/CAPS/training/2023/training.log

==&gt; Loading geometry from file "../../data/ESP/transport.csm"...

==&gt; Setting Build Variables and Geometry Values...

==&gt; Create masstran aim...

==&gt; Computing mass properties...

MESSAGE:: Building wingOml


MESSAGE:: Building htailOml


MESSAGE:: Building vtailOml


MESSAGE:: Building fuseOml

Mapping Csys attributes ................
	Number of unique Csys attributes = 0

Getting FEA coordinate systems.......
	Number of coordinate systems - 0
	No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
	Number of unique capsConstraint attributes = 0
Mapping capsLoad attributes ................
	Number of unique capsLoad attributes = 0
Mapping capsBound attributes ................
	Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
	Number of unique capsConnect attributes = 0
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 4
	Name = wingSkin, index = 1
	Name = fuseSkin, index = 2
	Name = htailSkin, index = 3
	Name = vtailSkin, index = 4
Setting FEA Data
	Mesh for body = 0
	Number of nodal coordinates = 5622
	Number of elements = 11240
	Elemental Nodes = 0
	Elemental Rods  = 0
	Elemental Tria3 = 11240
	Elemental Quad4 = 0
Setting FEA Data
	Mesh for body = 1
	Number of nodal coordinates = 5460
	Number of elements = 10916
	Elemental Nodes = 0
	Elemental Rods  = 0
	Elemental Tria3 = 10916
	Elemental Quad4 = 0
Setting FEA Data
	Mesh for body = 2
	Number of nodal coordinates = 5144
	Number of elements = 10284
	Elemental Nodes = 0
	Elemental Rods  = 0
	Elemental Tria3 = 10284
	Elemental Quad4 = 0
Setting FEA Data
	Mesh for body = 3
	Number of nodal coordinates = 2722
	Number of elements = 5440
	Elemental Nodes = 0
	Elemental Rods  = 0
	Elemental Tria3 = 5440
	Elemental Quad4 = 0
Combining multiple FEA meshes!
	Combined Number of nodal coordinates = 18948
	Combined Number of elements = 37880
	Combined Elemental Nodes = 0
	Combined Elemental Rods  = 0
	Combined Elemental Tria3 = 37880
	Combined Elemental Quad4 = 0

Getting FEA materials.......
	Number of materials - 1
	Material name - Unobtainium
	No "materialType" specified for Material tuple Unobtainium, defaulting to "Isotropic"
	Done getting FEA materials

Getting FEA properties.......
	Number of properties - 4
	Property name - fuseSkin
	Property name - htailSkin
	Property name - vtailSkin
	Property name - wingSkin
	Done getting FEA properties
Updating mesh element types based on properties input

==&gt; Computed mass properties...
--&gt; aircraft_skin =  {'mass': &lt;Quantity 37680.23920685 kg&gt;, 'CG': &lt;Quantity [28.71144056095, 0.0001760540729288, 0.3509995725871] meter&gt;, 'massInertia': &lt;Quantity [3048975.243572, 5627298.16578, 8320479.914785, 110.5249426469, 521135.0644149, 27.78569267508] m2.kg&gt;}

==&gt; Creating AVL aim...

==&gt; Outputs
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 3
	Name = Wing, index = 1
	Name = Htail, index = 2
	Name = Vtail, index = 3
Getting vortex lattice surface data
	VLM surface name - Htail
	No "groupName" variable provided or no matches found, going to use tuple name
	VLM surface name - Vtail
	No "groupName" variable provided or no matches found, going to use tuple name
	VLM surface name - Wing
	No "groupName" variable provided or no matches found, going to use tuple name
	Done getting vortex lattice surface data
Writing surface - Htail (ID = 0)
	Section 1 of 3 (ID = 0)
	Section 2 of 3 (ID = 1)
	Section 3 of 3 (ID = 2)
Writing surface - Vtail (ID = 1)
	Section 1 of 2 (ID = 1)
	Section 2 of 2 (ID = 0)
Writing surface - Wing (ID = 2)
	Section 1 of 5 (ID = 0)
	Section 2 of 5 (ID = 4)
	Section 3 of 5 (ID = 1)
	Section 4 of 5 (ID = 3)
	Section 5 of 5 (ID = 2)
Writing mass properties file: caps.mass
Parsing MassProp
Note: The following floating-point exceptions are signalling: IEEE_DIVIDE_BY_ZERO
--&gt; Xcg =  89.1676 meter
--&gt; Xnp =  92.42449260375724 meter
--&gt; StaticMargin =  0.4922965606645398
--&gt; EigenValues  {'case 1': [[-0.70484997, 0.0], [0.13849195, 0.55140288], [0.13849195, -0.55140288], [-0.1642923, 0.56419037], [-0.1642923, -0.56419037], [-0.006812761, 0.0], [-0.013696194, 0.11026784], [-0.013696194, -0.11026784]]}

--&gt; Real Eigen Values = [-0.70484997, 0.13849195, 0.13849195, -0.1642923, -0.1642923, -0.006812761, -0.013696194, -0.013696194]

real	0m4.517s
user	0m4.562s
sys	0m4.257s
+ status=0
+ set +x

=================================================
solutions/session06/avl_masstran_MainGear.py passed (as expected)
=================================================


=================================================
avl_masstran_MultiMat.py test;
+ python avl_masstran_MultiMat.py
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/CAPS/training/2023/training.log

==&gt; Loading geometry from file "../../data/ESP/transport.csm"...

==&gt; Setting Build Variables and Geometry Values...

==&gt; Create masstran aim...

==&gt; Computing mass properties...

MESSAGE:: Building wingOml


MESSAGE:: Building htailOml


MESSAGE:: Building vtailOml


MESSAGE:: Building fuseOml

Mapping Csys attributes ................
	Number of unique Csys attributes = 0

Getting FEA coordinate systems.......
	Number of coordinate systems - 0
	No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
	Number of unique capsConstraint attributes = 0
Mapping capsLoad attributes ................
	Number of unique capsLoad attributes = 0
Mapping capsBound attributes ................
	Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
	Number of unique capsConnect attributes = 0
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 4
	Name = wingSkin, index = 1
	Name = fuseSkin, index = 2
	Name = htailSkin, index = 3
	Name = vtailSkin, index = 4
Setting FEA Data
	Mesh for body = 0
	Number of nodal coordinates = 5622
	Number of elements = 11240
	Elemental Nodes = 0
	Elemental Rods  = 0
	Elemental Tria3 = 11240
	Elemental Quad4 = 0
Setting FEA Data
	Mesh for body = 1
	Number of nodal coordinates = 5460
	Number of elements = 10916
	Elemental Nodes = 0
	Elemental Rods  = 0
	Elemental Tria3 = 10916
	Elemental Quad4 = 0
Setting FEA Data
	Mesh for body = 2
	Number of nodal coordinates = 5144
	Number of elements = 10284
	Elemental Nodes = 0
	Elemental Rods  = 0
	Elemental Tria3 = 10284
	Elemental Quad4 = 0
Setting FEA Data
	Mesh for body = 3
	Number of nodal coordinates = 2722
	Number of elements = 5440
	Elemental Nodes = 0
	Elemental Rods  = 0
	Elemental Tria3 = 5440
	Elemental Quad4 = 0
Combining multiple FEA meshes!
	Combined Number of nodal coordinates = 18948
	Combined Number of elements = 37880
	Combined Elemental Nodes = 0
	Combined Elemental Rods  = 0
	Combined Elemental Tria3 = 37880
	Combined Elemental Quad4 = 0

Getting FEA materials.......
	Number of materials - 3
	Material name - fuseium
	No "materialType" specified for Material tuple fuseium, defaulting to "Isotropic"
	Material name - tailium
	No "materialType" specified for Material tuple tailium, defaulting to "Isotropic"
	Material name - wingium
	No "materialType" specified for Material tuple wingium, defaulting to "Isotropic"
	Done getting FEA materials

Getting FEA properties.......
	Number of properties - 4
	Property name - fuseSkin
	Property name - htailSkin
	Property name - vtailSkin
	Property name - wingSkin
	Done getting FEA properties
Updating mesh element types based on properties input

==&gt; Computed mass properties...
--&gt; aircraft_skin =  {'mass': &lt;Quantity 52814.66618698 kg&gt;, 'CG': &lt;Quantity [25.21445079983, 3.934787049156e-05, 0.007162108227903] meter&gt;, 'massInertia': &lt;Quantity [3041343.02095, 6969268.211845, 9624962.495276, 24.33339932984, 262918.1236746, 18.91803491383] m2.kg&gt;}

==&gt; Creating AVL aim...

==&gt; Outputs
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 3
	Name = Wing, index = 1
	Name = Htail, index = 2
	Name = Vtail, index = 3
Getting vortex lattice surface data
	VLM surface name - Htail
	No "groupName" variable provided or no matches found, going to use tuple name
	VLM surface name - Vtail
	No "groupName" variable provided or no matches found, going to use tuple name
	VLM surface name - Wing
	No "groupName" variable provided or no matches found, going to use tuple name
	Done getting vortex lattice surface data
Writing surface - Htail (ID = 0)
	Section 1 of 3 (ID = 0)
	Section 2 of 3 (ID = 1)
	Section 3 of 3 (ID = 2)
Writing surface - Vtail (ID = 1)
	Section 1 of 2 (ID = 1)
	Section 2 of 2 (ID = 0)
Writing surface - Wing (ID = 2)
	Section 1 of 5 (ID = 0)
	Section 2 of 5 (ID = 4)
	Section 3 of 5 (ID = 1)
	Section 4 of 5 (ID = 3)
	Section 5 of 5 (ID = 2)
Writing mass properties file: caps.mass
Parsing MassProp
Note: The following floating-point exceptions are signalling: IEEE_DIVIDE_BY_ZERO
--&gt; Xcg =  80.2256 meter
--&gt; Xnp =  92.49086428236849 meter
--&gt; StaticMargin =  1.853959634679339
--&gt; EigenValues  {'case 1': [[-0.67265764, 0.0], [0.12206744, 0.57566409], [0.12206744, -0.57566409], [-0.15647634, 1.0546663], [-0.15647634, -1.0546663], [-0.0068085373, 0.0], [-0.00033021093, 0.049308946], [-0.00033021093, -0.049308946]]}

--&gt; Real Eigen Values = [-0.67265764, 0.12206744, 0.12206744, -0.15647634, -0.15647634, -0.0068085373, -0.00033021093, -0.00033021093]

real	0m4.502s
user	0m4.549s
sys	0m4.228s
+ status=0
+ set +x

=================================================
solutions/session06/avl_masstran_MultiMat.py passed (as expected)
=================================================


=================================================
masstran_MultiAIM.py test;
+ python masstran_MultiAIM.py
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/CAPS/training/2023/training.log

==&gt; Loading geometry from file "../../data/ESP/transport.csm"...

==&gt; Setting Build Variables and Geometry Values...

==&gt; Loading masstran aims...

==&gt; Computing mass properties...

MESSAGE:: Building wingOml


MESSAGE:: Building htailOml


MESSAGE:: Building vtailOml


MESSAGE:: Building fuseOml

Mapping Csys attributes ................
	Number of unique Csys attributes = 0

Getting FEA coordinate systems.......
	Number of coordinate systems - 0
	No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
	Number of unique capsConstraint attributes = 0
Mapping capsLoad attributes ................
	Number of unique capsLoad attributes = 0
Mapping capsBound attributes ................
	Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
	Number of unique capsConnect attributes = 0
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = fuseSkin, index = 1
Setting FEA Data
	Mesh for body = 0
	Number of nodal coordinates = 7445
	Number of elements = 14886
	Elemental Nodes = 0
	Elemental Rods  = 0
	Elemental Tria3 = 14886
	Elemental Quad4 = 0

Getting FEA materials.......
	Number of materials - 1
	Material name - fuseium
	No "materialType" specified for Material tuple fuseium, defaulting to "Isotropic"
	Done getting FEA materials

Getting FEA properties.......
	Number of properties - 1
	Property name - fuseSkin
	Done getting FEA properties
Updating mesh element types based on properties input
Mapping Csys attributes ................
	Number of unique Csys attributes = 0

Getting FEA coordinate systems.......
	Number of coordinate systems - 0
	No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
	Number of unique capsConstraint attributes = 0
Mapping capsLoad attributes ................
	Number of unique capsLoad attributes = 0
Mapping capsBound attributes ................
	Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
	Number of unique capsConnect attributes = 0
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = wingSkin, index = 1
Setting FEA Data
	Mesh for body = 0
	Number of nodal coordinates = 5622
	Number of elements = 11240
	Elemental Nodes = 0
	Elemental Rods  = 0
	Elemental Tria3 = 11240
	Elemental Quad4 = 0

Getting FEA materials.......
	Number of materials - 1
	Material name - wingium
	No "materialType" specified for Material tuple wingium, defaulting to "Isotropic"
	Done getting FEA materials

Getting FEA properties.......
	Number of properties - 1
	Property name - wingSkin
	Done getting FEA properties
Updating mesh element types based on properties input
Mapping Csys attributes ................
	Number of unique Csys attributes = 0

Getting FEA coordinate systems.......
	Number of coordinate systems - 0
	No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
	Number of unique capsConstraint attributes = 0
Mapping capsLoad attributes ................
	Number of unique capsLoad attributes = 0
Mapping capsBound attributes ................
	Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
	Number of unique capsConnect attributes = 0
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 2
	Name = htailSkin, index = 1
	Name = vtailSkin, index = 2
Setting FEA Data
	Mesh for body = 0
	Number of nodal coordinates = 3488
	Number of elements = 6972
	Elemental Nodes = 0
	Elemental Rods  = 0
	Elemental Tria3 = 6972
	Elemental Quad4 = 0
Setting FEA Data
	Mesh for body = 1
	Number of nodal coordinates = 3480
	Number of elements = 6956
	Elemental Nodes = 0
	Elemental Rods  = 0
	Elemental Tria3 = 6956
	Elemental Quad4 = 0
Combining multiple FEA meshes!
	Combined Number of nodal coordinates = 6968
	Combined Number of elements = 13928
	Combined Elemental Nodes = 0
	Combined Elemental Rods  = 0
	Combined Elemental Tria3 = 13928
	Combined Elemental Quad4 = 0

Getting FEA materials.......
	Number of materials - 1
	Material name - tailium
	No "materialType" specified for Material tuple tailium, defaulting to "Isotropic"
	Done getting FEA materials

Getting FEA properties.......
	Number of properties - 2
	Property name - htailSkin
	Property name - vtailSkin
	Done getting FEA properties
Updating mesh element types based on properties input

==&gt; Computed mass properties...
--&gt; fuse_skin =  {'mass': &lt;Quantity 7849.475274166 kg&gt;, 'CG': &lt;Quantity [23.60861887848, -5.59439230963e-05, 0.1631067332576] meter&gt;, 'massInertia': &lt;Quantity [64256.8299145, 1266909.722239, 1265121.586758, -7.997972199888, 26539.85606389, -0.8824247963638] m2.kg&gt;}
--&gt; wing_skin =  {'mass': &lt;Quantity 23992.67003648 kg&gt;, 'CG': &lt;Quantity [26.65600801849, 3.498760694801e-05, -0.6718794767923] meter&gt;, 'massInertia': &lt;Quantity [4029452.651317, 529853.8379244, 4523798.230161, -19.40420203165, 69301.12468094, 23.37530324144] m2.kg&gt;}
--&gt; tail_skin =  {'mass': &lt;Quantity 748.6464447905 kg&gt;, 'CG': &lt;Quantity [47.57149390357, -1.45642951031e-06, 3.576129105462] meter&gt;, 'massInertia': &lt;Quantity [19383.57137666, 6924.661310066, 21171.65394983, 0.00913598087453, 1134.160412188, 0.004686577596883] m2.kg&gt;}

real	0m2.542s
user	0m2.440s
sys	0m0.842s
+ status=0
+ set +x

=================================================
solutions/session06/masstran_MultiAIM.py passed (as expected)
=================================================


=================================================
masstran_MultiMat.py test;
+ python masstran_MultiMat.py
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/CAPS/training/2023/training.log

==&gt; Loading geometry from file "../../data/ESP/transport.csm"...

==&gt; Setting Build Variables and Geometry Values...

==&gt; Loading masstran aim...

==&gt; Computing mass properties...

MESSAGE:: Building wingOml


MESSAGE:: Building htailOml


MESSAGE:: Building vtailOml


MESSAGE:: Building fuseOml

Mapping Csys attributes ................
	Number of unique Csys attributes = 0

Getting FEA coordinate systems.......
	Number of coordinate systems - 0
	No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
	Number of unique capsConstraint attributes = 0
Mapping capsLoad attributes ................
	Number of unique capsLoad attributes = 0
Mapping capsBound attributes ................
	Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
	Number of unique capsConnect attributes = 0
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 4
	Name = wingSkin, index = 1
	Name = fuseSkin, index = 2
	Name = htailSkin, index = 3
	Name = vtailSkin, index = 4
Setting FEA Data
	Mesh for body = 0
	Number of nodal coordinates = 5622
	Number of elements = 11240
	Elemental Nodes = 0
	Elemental Rods  = 0
	Elemental Tria3 = 11240
	Elemental Quad4 = 0
Setting FEA Data
	Mesh for body = 1
	Number of nodal coordinates = 5460
	Number of elements = 10916
	Elemental Nodes = 0
	Elemental Rods  = 0
	Elemental Tria3 = 10916
	Elemental Quad4 = 0
Setting FEA Data
	Mesh for body = 2
	Number of nodal coordinates = 5144
	Number of elements = 10284
	Elemental Nodes = 0
	Elemental Rods  = 0
	Elemental Tria3 = 10284
	Elemental Quad4 = 0
Setting FEA Data
	Mesh for body = 3
	Number of nodal coordinates = 2722
	Number of elements = 5440
	Elemental Nodes = 0
	Elemental Rods  = 0
	Elemental Tria3 = 5440
	Elemental Quad4 = 0
Combining multiple FEA meshes!
	Combined Number of nodal coordinates = 18948
	Combined Number of elements = 37880
	Combined Elemental Nodes = 0
	Combined Elemental Rods  = 0
	Combined Elemental Tria3 = 37880
	Combined Elemental Quad4 = 0

Getting FEA materials.......
	Number of materials - 3
	Material name - fuseium
	No "materialType" specified for Material tuple fuseium, defaulting to "Isotropic"
	Material name - tailium
	No "materialType" specified for Material tuple tailium, defaulting to "Isotropic"
	Material name - wingium
	No "materialType" specified for Material tuple wingium, defaulting to "Isotropic"
	Done getting FEA materials

Getting FEA properties.......
	Number of properties - 4
	Property name - fuseSkin
	Property name - htailSkin
	Property name - vtailSkin
	Property name - wingSkin
	Done getting FEA properties
Updating mesh element types based on properties input

==&gt; Computed mass properties...
--&gt; aircraft_skin =  {'mass': &lt;Quantity 71849.72412333566 lb&gt;, 'CG': &lt;Quantity [86.62612896295931, 0.0001609398352649606, -1.2242696390590548] ft&gt;, 'massInertia': &lt;Quantity [97984905.06860435, 52635694.4981757, 147326784.86648563, -44.22778238683339, 3464450.8348036557, 599.6888840550322] lb*ft^2&gt;}

real	0m2.127s
user	0m2.544s
sys	0m0.420s
+ status=0
+ set +x

=================================================
solutions/session06/masstran_MultiMat.py passed (as expected)
=================================================


=================================================
01_aflr4_InviscidWing.py test;
+ python 01_aflr4_InviscidWing.py
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/CAPS/training/2023/training.log

MESSAGE:: Building wingOml

Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 2
	Name = Wing, index = 1
	Name = Farfield, index = 2
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 3
	Name = leftWing, index = 1
	Name = riteWing, index = 2
	Name = Farfield, index = 3

Getting mesh sizing parameters
	Mesh sizing name - Farfield
	Done getting mesh sizing parameters
 
AFLR2    : ---------------------------------------
AFLR2    : AFLR2 LIBRARY
AFLR2    : ADVANCING-FRONT/LOCAL-RECONNECTION
AFLR2    : TRIA/QUAD GRID GENERATOR
AFLR2    : Version Number 9.18.1
AFLR2    : Version Date   06/11/24 @ 05:52PM
AFLR2    : Compile OS     Darwin 23.5.0 arm64
AFLR2    : Compile Date   06/11/24 @ 05:52PM
AFLR2    : Copyright 1994-2021, D.L. Marcum
AFLR2    : ---------------------------------------
 
AFLR4    : ---------------------------------------
AFLR4    : AFLR4 LIBRARY
AFLR4    : ADVANCING-FRONT/LOCAL-RECONNECTION
AFLR4    : TRIA/QUAD SURFACE GRID GENERATOR
AFLR4    : Version Number 11.5.15
AFLR4    : Version Date   07/19/24 @ 07:04PM
AFLR4    : Compile OS     Darwin 23.5.0 arm64
AFLR4    : Compile Date   07/19/24 @ 07:06PM
AFLR4    : Copyright 1994-2021, D.L. Marcum
AFLR4    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.8.1
EGADS    : ---------------------------------------

EGADS    : EGADS CAD Geometry Setup

EGADS    : Model has 2 Active Bodies

EGADS    : Body 0 is a SolidBody
EGADS    : Body 0 has 1 Shells
EGADS    : Body 0 has 10 Faces
EGADS    : Body 0 has 18 Edges
EGADS    : Body 0 has 10 Loops
EGADS    : Body 0 has 10 Nodes
EGADS    : Body 1 is a SolidBody
EGADS    : Body 1 has 1 Shells
EGADS    : Body 1 has 6 Faces
EGADS    : Body 1 has 12 Edges
EGADS    : Body 1 has 6 Loops
EGADS    : Body 1 has 8 Nodes

EGADS    : Check Grid BCs

EGADS    : Grid BCs are OK

EGADS    : Face Neighbor-Faces Information

EGADS    : QC  = Face Quad Combination Flag
EGADS    : IER = Face Isolated Edge Refinement Flag
EGADS    : ER  = Face Edge Refinement Factor
EGADS    :       Not applicable for Faces with a FarField Grid BC.
EGADS    : SF  = Face Scale Factor
EGADS    :       Not applicable for Faces with a FarField Grid BC.

EGADS    :   Face          Body    QC   IER       ER    Scale   Neighbor
EGADS    :     ID  Active    ID  Flag  Flag   Weight   Factor   Faces
EGADS    :      1     Yes     0     0     1        0        1   2 3 6
EGADS    :      2     Yes     0     0     1        0        1   1 4 5
EGADS    :      3     Yes     0     0     1        0        1   1 4 8
EGADS    :      4     Yes     0     0     1        0        1   2 3 5
EGADS    :      5     Yes     0     0     1        0        1   2 4
EGADS    :      6     Yes     0     0     1        0        1   1 7 8
EGADS    :      7     Yes     0     0     1        0        1   6 9 10
EGADS    :      8     Yes     0     0     1        0        1   3 6 9
EGADS    :      9     Yes     0     0     1        0        1   7 8 10
EGADS    :     10     Yes     0     0     1        0        1   7 9
EGADS    :     11     Yes     1     0     1       NA       NA   13 14 15 16
EGADS    :     12     Yes     1     0     1       NA       NA   13 14 15 16
EGADS    :     13     Yes     1     0     1       NA       NA   11 12 15 16
EGADS    :     14     Yes     1     0     1       NA       NA   11 12 15 16
EGADS    :     15     Yes     1     0     1       NA       NA   11 12 13 14
EGADS    :     16     Yes     1     0     1       NA       NA   11 12 13 14

EGADS    : Face Edges Information

EGADS    :   Face   Edges
EGADS    :      1   -1 2 3 -4
EGADS    :      2   -5 4 6 -7
EGADS    :      3   -3 8 1 -9
EGADS    :      4   -6 9 5 -10
EGADS    :      5   7 10
EGADS    :      6   11 13 -12 -2
EGADS    :      7   14 16 -15 -13
EGADS    :      8   12 17 -11 -8
EGADS    :      9   15 18 -14 -17
EGADS    :     10   -16 -18
EGADS    :     11   19 20 -21 -22
EGADS    :     12   -23 26 25 -24
EGADS    :     13   27 23 -28 -19
EGADS    :     14   -29 21 30 -25
EGADS    :     15   22 29 -26 -27
EGADS    :     16   -20 28 24 -30

EGADS    : Face Loops Information

EGADS    :   Face   Loops
EGADS    :      1   1
EGADS    :      2   2
EGADS    :      3   3
EGADS    :      4   4
EGADS    :      5   5
EGADS    :      6   6
EGADS    :      7   7
EGADS    :      8   8
EGADS    :      9   9
EGADS    :     10   10
EGADS    :     11   11
EGADS    :     12   12
EGADS    :     13   13
EGADS    :     14   14
EGADS    :     15   15
EGADS    :     16   16

EGADS    : Loop Edges Information

EGADS    :   Loop  Active   Edges
EGADS    :      1     Yes   -1 2 3 -4
EGADS    :      2     Yes   -5 4 6 -7
EGADS    :      3     Yes   -3 8 1 -9
EGADS    :      4     Yes   -6 9 5 -10
EGADS    :      5     Yes   7 10
EGADS    :      6     Yes   11 13 -12 -2
EGADS    :      7     Yes   14 16 -15 -13
EGADS    :      8     Yes   12 17 -11 -8
EGADS    :      9     Yes   15 18 -14 -17
EGADS    :     10     Yes   -16 -18
EGADS    :     11     Yes   19 20 -21 -22
EGADS    :     12     Yes   -23 26 25 -24
EGADS    :     13     Yes   27 23 -28 -19
EGADS    :     14     Yes   -29 21 30 -25
EGADS    :     15     Yes   22 29 -26 -27
EGADS    :     16     Yes   -20 28 24 -30

EGADS    : Edge Node, Scale Factor, and Neighbor-Faces Information

EGADS    : ESF = Edge Scale Factor
EGADS    :       Not applicable for DEGENERATE Edges or Edges with a FarField
EGADS    :       Grid BC Neighbor Face.

EGADS    :                                             Neighbor
EGADS    :   Edge  Body  Active Node1 Node2      ESF   Faces
EGADS    :      1     0     Yes     1     2        1   1 3
EGADS    :      2     0     Yes     1     3        1   1 6
EGADS    :      3     0     Yes     3     4        1   1 3
EGADS    :      4     0     Yes     2     4        1   1 2
EGADS    :      5     0     Yes     2     5        1   2 4
EGADS    :      6     0     Yes     4     6        1   2 4
EGADS    :      7     0     Yes     5     6        1   2 5
EGADS    :      8     0     Yes     3     1        1   3 8
EGADS    :      9     0     Yes     4     2        1   3 4
EGADS    :     10     0     Yes     6     5        1   4 5
EGADS    :     11     0     Yes     1     7        1   6 8
EGADS    :     12     0     Yes     3     8        1   6 8
EGADS    :     13     0     Yes     7     8        1   6 7
EGADS    :     14     0     Yes     7     9        1   7 9
EGADS    :     15     0     Yes     8    10        1   7 9
EGADS    :     16     0     Yes     9    10        1   7 10
EGADS    :     17     0     Yes     8     7        1   8 9
EGADS    :     18     0     Yes    10     9        1   9 10
EGADS    :     19     1     Yes    12    11       NA   11 13
EGADS    :     20     1     Yes    11    13       NA   11 16
EGADS    :     21     1     Yes    14    13       NA   11 14
EGADS    :     22     1     Yes    12    14       NA   11 15
EGADS    :     23     1     Yes    16    15       NA   12 13
EGADS    :     24     1     Yes    15    17       NA   12 16
EGADS    :     25     1     Yes    18    17       NA   12 14
EGADS    :     26     1     Yes    16    18       NA   12 15
EGADS    :     27     1     Yes    12    16       NA   13 15
EGADS    :     28     1     Yes    11    15       NA   13 16
EGADS    :     29     1     Yes    14    18       NA   14 15
EGADS    :     30     1     Yes    13    17       NA   14 16

EGADS    : Node Information

EGADS    :   Node  Active      Coordinates
EGADS    :      1     Yes       97.2007855                0                0
EGADS    :      2     Yes       97.9335611                0                0
EGADS    :      3     Yes               50                0                0
EGADS    :      4     Yes       75.3047874                0                0
EGADS    :      5     Yes       123.552357                0        4.7180639
EGADS    :      6     Yes       118.391317                0       3.99272703
EGADS    :      7     Yes       97.9335611       36.1389817                0
EGADS    :      8     Yes       75.3047874       36.1389817                0
EGADS    :      9     Yes       123.552357       97.6729236        4.7180639
EGADS    :     10     Yes       118.391317       97.6729236       3.99272703
EGADS    :     11     Yes                0                0       1951.57774
EGADS    :     12     Yes                0                0                0
EGADS    :     13     Yes                0       1953.45847       1951.57774
EGADS    :     14     Yes                0       1953.45847                0
EGADS    :     15     Yes       2040.21562                0       1951.57774
EGADS    :     16     Yes       2040.21562                0                0
EGADS    :     17     Yes       2040.21562       1953.45847       1951.57774
EGADS    :     18     Yes       2040.21562       1953.45847                0

EGADS    : Face and Edge Match Information

EGADS    : No Face Matches Found

AFLR4    : Surface Mesh Spacing Setup

AFLR4    : Max Bounding Box Length     = 3906.92
AFLR4    : Min Bounding Box Length     = 3906.92
AFLR4    : Max Ref Bounding Box Length = 195.346
AFLR4    : Min Ref Bounding Box Length = 13.1976
AFLR4    : Reference Length            = 21.7051
AFLR4    : BL Thickness                = 0
AFLR4    : FarField Spacing            = 428.342
AFLR4    : Abs Min Surf Spacing        = 0.0542627
AFLR4    : Min Surf Spacing            = 0.108525
AFLR4    : Max Surf Spacing            = 2.17051
AFLR4    : Global Scale Factor         = 1

AFLR4    : Geometry Definition Information

AFLR4    : Definition              Definition   Composite             Grid BC
AFLR4    :         ID                    Type          ID                Type
AFLR4    :          0     glue-only composite           -                   -
AFLR4    :          1            CAD geometry           0            STD w/BL
AFLR4    :          2            CAD geometry           0            STD w/BL
AFLR4    :          3            CAD geometry           0            STD w/BL
AFLR4    :          4            CAD geometry           0            STD w/BL
AFLR4    :          5            CAD geometry           0            STD w/BL
AFLR4    :          6            CAD geometry           0            STD w/BL
AFLR4    :          7            CAD geometry           0            STD w/BL
AFLR4    :          8            CAD geometry           0            STD w/BL
AFLR4    :          9            CAD geometry           0            STD w/BL
AFLR4    :         10            CAD geometry           0            STD w/BL
AFLR4    :         11            CAD geometry           0            FARFIELD
AFLR4    :         12            CAD geometry           0            FARFIELD
AFLR4    :         13            CAD geometry           0            FARFIELD
AFLR4    :         14            CAD geometry           0            FARFIELD
AFLR4    :         15            CAD geometry           0            FARFIELD
AFLR4    :         16            CAD geometry           0            FARFIELD

AFLR4    : Define CAD surface definition 1
AFLR4    : Define CAD surface definition 2
AFLR4    : Define CAD surface definition 3
AFLR4    : Define CAD surface definition 4
AFLR4    : Define CAD surface definition 5
AFLR4    : Define CAD surface definition 6
AFLR4    : Define CAD surface definition 7
AFLR4    : Define CAD surface definition 8
AFLR4    : Define CAD surface definition 9
AFLR4    : Define CAD surface definition 10
AFLR4    : Define CAD surface definition 11
AFLR4    : Define CAD surface definition 12
AFLR4    : Define CAD surface definition 13
AFLR4    : Define CAD surface definition 14
AFLR4    : Define CAD surface definition 15
AFLR4    : Define CAD surface definition 16

AFLR4    : Surface Grid Generation

AFLR4    : Generate optimal mesh on surface definition 1
AFLR2    : Nodes, Trias,Quads=      8732     16959         0
AFLR4    : Nodes, Trias,Quads=      5233      9961         0

AFLR4    : Generate optimal mesh on surface definition 2
AFLR2    : Nodes, Trias,Quads=     18087     35388         0
AFLR4    : Nodes, Trias,Quads=      5569     10352         0

AFLR4    : Generate optimal mesh on surface definition 3
AFLR2    : Nodes, Trias,Quads=     10182     19859         0
AFLR4    : Nodes, Trias,Quads=      4951      9397         0

AFLR4    : Generate optimal mesh on surface definition 4
AFLR2    : Nodes, Trias,Quads=     16336     31887         0
AFLR4    : Nodes, Trias,Quads=      5435     10085         0

AFLR4    : Generate optimal mesh on surface definition 5
AFLR2    : Nodes, Trias,Quads=        55        71         0
AFLR4    : Nodes, Trias,Quads=        45        51         0

AFLR4    : Generate optimal mesh on surface definition 6
AFLR2    : Nodes, Trias,Quads=      8705     16905         0
AFLR4    : Nodes, Trias,Quads=      5312     10119         0

AFLR4    : Generate optimal mesh on surface definition 7
AFLR2    : Nodes, Trias,Quads=     17908     35030         0
AFLR4    : Nodes, Trias,Quads=      5567     10348         0

AFLR4    : Generate optimal mesh on surface definition 8
AFLR2    : Nodes, Trias,Quads=      8823     17141         0
AFLR4    : Nodes, Trias,Quads=      4980      9455         0

AFLR4    : Generate optimal mesh on surface definition 9
AFLR2    : Nodes, Trias,Quads=     16876     32967         0
AFLR4    : Nodes, Trias,Quads=      5357      9929         0

AFLR4    : Generate optimal mesh on surface definition 10
AFLR2    : Nodes, Trias,Quads=        55        71         0
AFLR4    : Nodes, Trias,Quads=        46        53         0

AFLR4    : Generate optimal mesh on surface definition 11
AFLR2    : Nodes, Trias,Quads=       113       188         0
AFLR4    : Nodes, Trias,Quads=       109       180         0

AFLR4    : Generate optimal mesh on surface definition 12
AFLR2    : Nodes, Trias,Quads=       112       186         0
AFLR4    : Nodes, Trias,Quads=       108       178         0

AFLR4    : Generate optimal mesh on surface definition 13
AFLR2    : Nodes, Trias,Quads=       112       186         0
AFLR4    : Nodes, Trias,Quads=       108       178         0

AFLR4    : Generate optimal mesh on surface definition 14
AFLR2    : Nodes, Trias,Quads=       113       188         0
AFLR4    : Nodes, Trias,Quads=       109       180         0

AFLR4    : Generate optimal mesh on surface definition 15
AFLR2    : Nodes, Trias,Quads=       112       186         0
AFLR4    : Nodes, Trias,Quads=       108       178         0

AFLR4    : Generate optimal mesh on surface definition 16
AFLR2    : Nodes, Trias,Quads=       113       188         0
AFLR4    : Nodes, Trias,Quads=       109       180         0

DGEOM    : Add surface definitions to composite definition 0
DGEOM    : Glue composite surface definition 0
DGEOM    : Nodes,Faces,BEdges=     40416     80824      5436

AFLR4    : Curvature BG Surface Grid Generation

AFLR4    : Nodes, Faces      =     40416     80824

AFLR4    : Surface Grid Generation

AFLR4    : Generate optimal mesh on surface definition 1
AFLR2    : Nodes, Trias,Quads=      8498     16494         0
AFLR4    : Nodes, Trias,Quads=      6521     12540         0

AFLR4    : Generate optimal mesh on surface definition 2
AFLR2    : Nodes, Trias,Quads=     14215     27654         0
AFLR4    : Nodes, Trias,Quads=     10037     19298         0

AFLR4    : Generate optimal mesh on surface definition 3
AFLR2    : Nodes, Trias,Quads=      8900     17298         0
AFLR4    : Nodes, Trias,Quads=      6655     12808         0

AFLR4    : Generate optimal mesh on surface definition 4
AFLR2    : Nodes, Trias,Quads=     13476     26178         0
AFLR4    : Nodes, Trias,Quads=      9810     18846         0

AFLR4    : Generate optimal mesh on surface definition 5
AFLR2    : Nodes, Trias,Quads=        59        77         0
AFLR4    : Nodes, Trias,Quads=        49        57         0

AFLR4    : Generate optimal mesh on surface definition 6
AFLR2    : Nodes, Trias,Quads=      8503     16504         0
AFLR4    : Nodes, Trias,Quads=      6543     12584         0

AFLR4    : Generate optimal mesh on surface definition 7
AFLR2    : Nodes, Trias,Quads=     13624     26478         0
AFLR4    : Nodes, Trias,Quads=      9963     19156         0

AFLR4    : Generate optimal mesh on surface definition 8
AFLR2    : Nodes, Trias,Quads=      8761     17020         0
AFLR4    : Nodes, Trias,Quads=      6664     12826         0

AFLR4    : Generate optimal mesh on surface definition 9
AFLR2    : Nodes, Trias,Quads=     13534     26300         0
AFLR4    : Nodes, Trias,Quads=      9965     19162         0

AFLR4    : Generate optimal mesh on surface definition 10
AFLR2    : Nodes, Trias,Quads=        60        79         0
AFLR4    : Nodes, Trias,Quads=        49        57         0

AFLR4    : Generate optimal mesh on surface definition 11
AFLR2    : Nodes, Trias,Quads=       113       188         0
AFLR4    : Nodes, Trias,Quads=       109       180         0

AFLR4    : Generate optimal mesh on surface definition 12
AFLR2    : Nodes, Trias,Quads=       112       186         0
AFLR4    : Nodes, Trias,Quads=       107       176         0

AFLR4    : Generate optimal mesh on surface definition 13
AFLR2    : Nodes, Trias,Quads=       113       188         0
AFLR4    : Nodes, Trias,Quads=       108       178         0

AFLR4    : Generate optimal mesh on surface definition 14
AFLR2    : Nodes, Trias,Quads=       112       186         0
AFLR4    : Nodes, Trias,Quads=       109       180         0

AFLR4    : Generate optimal mesh on surface definition 15
AFLR2    : Nodes, Trias,Quads=       111       184         0
AFLR4    : Nodes, Trias,Quads=       107       176         0

AFLR4    : Generate optimal mesh on surface definition 16
AFLR2    : Nodes, Trias,Quads=       113       188         0
AFLR4    : Nodes, Trias,Quads=       109       180         0

DGEOM    : Add surface definitions to composite definition 0
DGEOM    : Glue composite surface definition 0
DGEOM    : Nodes,Faces,BEdges=     64206    128404      5374

OVERALL  : CPU Time          =     1.148   seconds
Body 1 (of 2)
Number of nodes    = 63669
Number of elements = 127334
Number of triangle elements      = 127334
Number of quadrilateral elements = 0
Body 2 (of 2)
Number of nodes    = 537
Number of elements = 1070
Number of triangle elements      = 1070
Number of quadrilateral elements = 0
----------------------------
Total number of nodes    = 64206
Total number of elements = 128404
Total number of triangle elements      = 128404
Total number of quadrilateral elements = 0

real	0m2.559s
user	0m2.406s
sys	0m0.448s
+ status=0
+ set +x

=================================================
data/session07/01_aflr4_InviscidWing.py passed (as expected)
=================================================


=================================================
02_aflr4_Farfield.py test;
+ python 02_aflr4_Farfield.py
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/CAPS/training/2023/training.log

MESSAGE:: Building wingOml

Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 2
	Name = Wing, index = 1
	Name = Farfield, index = 2
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 3
	Name = leftWing, index = 1
	Name = riteWing, index = 2
	Name = Farfield, index = 3

Getting mesh sizing parameters
	Mesh sizing name - Farfield
	Done getting mesh sizing parameters
 
AFLR2    : ---------------------------------------
AFLR2    : AFLR2 LIBRARY
AFLR2    : ADVANCING-FRONT/LOCAL-RECONNECTION
AFLR2    : TRIA/QUAD GRID GENERATOR
AFLR2    : Version Number 9.18.1
AFLR2    : Version Date   06/11/24 @ 05:52PM
AFLR2    : Compile OS     Darwin 23.5.0 arm64
AFLR2    : Compile Date   06/11/24 @ 05:52PM
AFLR2    : Copyright 1994-2021, D.L. Marcum
AFLR2    : ---------------------------------------
 
AFLR4    : ---------------------------------------
AFLR4    : AFLR4 LIBRARY
AFLR4    : ADVANCING-FRONT/LOCAL-RECONNECTION
AFLR4    : TRIA/QUAD SURFACE GRID GENERATOR
AFLR4    : Version Number 11.5.15
AFLR4    : Version Date   07/19/24 @ 07:04PM
AFLR4    : Compile OS     Darwin 23.5.0 arm64
AFLR4    : Compile Date   07/19/24 @ 07:06PM
AFLR4    : Copyright 1994-2021, D.L. Marcum
AFLR4    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.8.1
EGADS    : ---------------------------------------

EGADS    : EGADS CAD Geometry Setup

EGADS    : Model has 2 Active Bodies

EGADS    : Body 0 is a SolidBody
EGADS    : Body 0 has 1 Shells
EGADS    : Body 0 has 10 Faces
EGADS    : Body 0 has 18 Edges
EGADS    : Body 0 has 10 Loops
EGADS    : Body 0 has 10 Nodes
EGADS    : Body 1 is a SolidBody
EGADS    : Body 1 has 1 Shells
EGADS    : Body 1 has 6 Faces
EGADS    : Body 1 has 12 Edges
EGADS    : Body 1 has 6 Loops
EGADS    : Body 1 has 8 Nodes

EGADS    : Check Grid BCs

EGADS    : Grid BCs are OK

EGADS    : Face Neighbor-Faces Information

EGADS    : QC  = Face Quad Combination Flag
EGADS    : IER = Face Isolated Edge Refinement Flag
EGADS    : ER  = Face Edge Refinement Factor
EGADS    :       Not applicable for Faces with a FarField Grid BC.
EGADS    : SF  = Face Scale Factor
EGADS    :       Not applicable for Faces with a FarField Grid BC.

EGADS    :   Face          Body    QC   IER       ER    Scale   Neighbor
EGADS    :     ID  Active    ID  Flag  Flag   Weight   Factor   Faces
EGADS    :      1     Yes     0     0     1        0        1   2 3 6
EGADS    :      2     Yes     0     0     1        0        1   1 4 5
EGADS    :      3     Yes     0     0     1        0        1   1 4 8
EGADS    :      4     Yes     0     0     1        0        1   2 3 5
EGADS    :      5     Yes     0     0     1        0        1   2 4
EGADS    :      6     Yes     0     0     1        0        1   1 7 8
EGADS    :      7     Yes     0     0     1        0        1   6 9 10
EGADS    :      8     Yes     0     0     1        0        1   3 6 9
EGADS    :      9     Yes     0     0     1        0        1   7 8 10
EGADS    :     10     Yes     0     0     1        0        1   7 9
EGADS    :     11     Yes     1     0     1       NA       NA   13 14 15 16
EGADS    :     12     Yes     1     0     1       NA       NA   13 14 15 16
EGADS    :     13     Yes     1     0     1       NA       NA   11 12 15 16
EGADS    :     14     Yes     1     0     1       NA       NA   11 12 15 16
EGADS    :     15     Yes     1     0     1       NA       NA   11 12 13 14
EGADS    :     16     Yes     1     0     1       NA       NA   11 12 13 14

EGADS    : Face Edges Information

EGADS    :   Face   Edges
EGADS    :      1   -1 2 3 -4
EGADS    :      2   -5 4 6 -7
EGADS    :      3   -3 8 1 -9
EGADS    :      4   -6 9 5 -10
EGADS    :      5   7 10
EGADS    :      6   11 13 -12 -2
EGADS    :      7   14 16 -15 -13
EGADS    :      8   12 17 -11 -8
EGADS    :      9   15 18 -14 -17
EGADS    :     10   -16 -18
EGADS    :     11   19 20 -21 -22
EGADS    :     12   -23 26 25 -24
EGADS    :     13   27 23 -28 -19
EGADS    :     14   -29 21 30 -25
EGADS    :     15   22 29 -26 -27
EGADS    :     16   -20 28 24 -30

EGADS    : Face Loops Information

EGADS    :   Face   Loops
EGADS    :      1   1
EGADS    :      2   2
EGADS    :      3   3
EGADS    :      4   4
EGADS    :      5   5
EGADS    :      6   6
EGADS    :      7   7
EGADS    :      8   8
EGADS    :      9   9
EGADS    :     10   10
EGADS    :     11   11
EGADS    :     12   12
EGADS    :     13   13
EGADS    :     14   14
EGADS    :     15   15
EGADS    :     16   16

EGADS    : Loop Edges Information

EGADS    :   Loop  Active   Edges
EGADS    :      1     Yes   -1 2 3 -4
EGADS    :      2     Yes   -5 4 6 -7
EGADS    :      3     Yes   -3 8 1 -9
EGADS    :      4     Yes   -6 9 5 -10
EGADS    :      5     Yes   7 10
EGADS    :      6     Yes   11 13 -12 -2
EGADS    :      7     Yes   14 16 -15 -13
EGADS    :      8     Yes   12 17 -11 -8
EGADS    :      9     Yes   15 18 -14 -17
EGADS    :     10     Yes   -16 -18
EGADS    :     11     Yes   19 20 -21 -22
EGADS    :     12     Yes   -23 26 25 -24
EGADS    :     13     Yes   27 23 -28 -19
EGADS    :     14     Yes   -29 21 30 -25
EGADS    :     15     Yes   22 29 -26 -27
EGADS    :     16     Yes   -20 28 24 -30

EGADS    : Edge Node, Scale Factor, and Neighbor-Faces Information

EGADS    : ESF = Edge Scale Factor
EGADS    :       Not applicable for DEGENERATE Edges or Edges with a FarField
EGADS    :       Grid BC Neighbor Face.

EGADS    :                                             Neighbor
EGADS    :   Edge  Body  Active Node1 Node2      ESF   Faces
EGADS    :      1     0     Yes     1     2        1   1 3
EGADS    :      2     0     Yes     1     3        1   1 6
EGADS    :      3     0     Yes     3     4        1   1 3
EGADS    :      4     0     Yes     2     4        1   1 2
EGADS    :      5     0     Yes     2     5        1   2 4
EGADS    :      6     0     Yes     4     6        1   2 4
EGADS    :      7     0     Yes     5     6        1   2 5
EGADS    :      8     0     Yes     3     1        1   3 8
EGADS    :      9     0     Yes     4     2        1   3 4
EGADS    :     10     0     Yes     6     5        1   4 5
EGADS    :     11     0     Yes     1     7        1   6 8
EGADS    :     12     0     Yes     3     8        1   6 8
EGADS    :     13     0     Yes     7     8        1   6 7
EGADS    :     14     0     Yes     7     9        1   7 9
EGADS    :     15     0     Yes     8    10        1   7 9
EGADS    :     16     0     Yes     9    10        1   7 10
EGADS    :     17     0     Yes     8     7        1   8 9
EGADS    :     18     0     Yes    10     9        1   9 10
EGADS    :     19     1     Yes    12    11       NA   11 13
EGADS    :     20     1     Yes    11    13       NA   11 16
EGADS    :     21     1     Yes    14    13       NA   11 14
EGADS    :     22     1     Yes    12    14       NA   11 15
EGADS    :     23     1     Yes    16    15       NA   12 13
EGADS    :     24     1     Yes    15    17       NA   12 16
EGADS    :     25     1     Yes    18    17       NA   12 14
EGADS    :     26     1     Yes    16    18       NA   12 15
EGADS    :     27     1     Yes    12    16       NA   13 15
EGADS    :     28     1     Yes    11    15       NA   13 16
EGADS    :     29     1     Yes    14    18       NA   14 15
EGADS    :     30     1     Yes    13    17       NA   14 16

EGADS    : Node Information

EGADS    :   Node  Active      Coordinates
EGADS    :      1     Yes       97.2007855                0                0
EGADS    :      2     Yes       97.9335611                0                0
EGADS    :      3     Yes               50                0                0
EGADS    :      4     Yes       75.3047874                0                0
EGADS    :      5     Yes       123.552357                0        4.7180639
EGADS    :      6     Yes       118.391317                0       3.99272703
EGADS    :      7     Yes       97.9335611       36.1389817                0
EGADS    :      8     Yes       75.3047874       36.1389817                0
EGADS    :      9     Yes       123.552357       97.6729236        4.7180639
EGADS    :     10     Yes       118.391317       97.6729236       3.99272703
EGADS    :     11     Yes                0                0       1951.57774
EGADS    :     12     Yes                0                0                0
EGADS    :     13     Yes                0       1953.45847       1951.57774
EGADS    :     14     Yes                0       1953.45847                0
EGADS    :     15     Yes       2040.21562                0       1951.57774
EGADS    :     16     Yes       2040.21562                0                0
EGADS    :     17     Yes       2040.21562       1953.45847       1951.57774
EGADS    :     18     Yes       2040.21562       1953.45847                0

EGADS    : Face and Edge Match Information

EGADS    : No Face Matches Found

AFLR4    : Surface Mesh Spacing Setup

AFLR4    : Max Bounding Box Length     = 3906.92
AFLR4    : Min Bounding Box Length     = 3906.92
AFLR4    : Max Ref Bounding Box Length = 195.346
AFLR4    : Min Ref Bounding Box Length = 13.1976
AFLR4    : Reference Length            = 21.7051
AFLR4    : BL Thickness                = 0
AFLR4    : FarField Spacing            = 530.302
AFLR4    : Abs Min Surf Spacing        = 0.0542627
AFLR4    : Min Surf Spacing            = 0.108525
AFLR4    : Max Surf Spacing            = 2.17051
AFLR4    : Global Scale Factor         = 1

AFLR4    : Geometry Definition Information

AFLR4    : Definition              Definition   Composite             Grid BC
AFLR4    :         ID                    Type          ID                Type
AFLR4    :          0     glue-only composite           -                   -
AFLR4    :          1            CAD geometry           0            STD w/BL
AFLR4    :          2            CAD geometry           0            STD w/BL
AFLR4    :          3            CAD geometry           0            STD w/BL
AFLR4    :          4            CAD geometry           0            STD w/BL
AFLR4    :          5            CAD geometry           0            STD w/BL
AFLR4    :          6            CAD geometry           0            STD w/BL
AFLR4    :          7            CAD geometry           0            STD w/BL
AFLR4    :          8            CAD geometry           0            STD w/BL
AFLR4    :          9            CAD geometry           0            STD w/BL
AFLR4    :         10            CAD geometry           0            STD w/BL
AFLR4    :         11            CAD geometry           0            FARFIELD
AFLR4    :         12            CAD geometry           0            FARFIELD
AFLR4    :         13            CAD geometry           0            FARFIELD
AFLR4    :         14            CAD geometry           0            FARFIELD
AFLR4    :         15            CAD geometry           0            FARFIELD
AFLR4    :         16            CAD geometry           0            FARFIELD

AFLR4    : Define CAD surface definition 1
AFLR4    : Define CAD surface definition 2
AFLR4    : Define CAD surface definition 3
AFLR4    : Define CAD surface definition 4
AFLR4    : Define CAD surface definition 5
AFLR4    : Define CAD surface definition 6
AFLR4    : Define CAD surface definition 7
AFLR4    : Define CAD surface definition 8
AFLR4    : Define CAD surface definition 9
AFLR4    : Define CAD surface definition 10
AFLR4    : Define CAD surface definition 11
AFLR4    : Define CAD surface definition 12
AFLR4    : Define CAD surface definition 13
AFLR4    : Define CAD surface definition 14
AFLR4    : Define CAD surface definition 15
AFLR4    : Define CAD surface definition 16

AFLR4    : Surface Grid Generation

AFLR4    : Generate optimal mesh on surface definition 1
AFLR2    : Nodes, Trias,Quads=      8732     16959         0
AFLR4    : Nodes, Trias,Quads=      5233      9961         0

AFLR4    : Generate optimal mesh on surface definition 2
AFLR2    : Nodes, Trias,Quads=     18087     35388         0
AFLR4    : Nodes, Trias,Quads=      5569     10352         0

AFLR4    : Generate optimal mesh on surface definition 3
AFLR2    : Nodes, Trias,Quads=     10182     19859         0
AFLR4    : Nodes, Trias,Quads=      4951      9397         0

AFLR4    : Generate optimal mesh on surface definition 4
AFLR2    : Nodes, Trias,Quads=     16336     31887         0
AFLR4    : Nodes, Trias,Quads=      5435     10085         0

AFLR4    : Generate optimal mesh on surface definition 5
AFLR2    : Nodes, Trias,Quads=        55        71         0
AFLR4    : Nodes, Trias,Quads=        45        51         0

AFLR4    : Generate optimal mesh on surface definition 6
AFLR2    : Nodes, Trias,Quads=      8705     16905         0
AFLR4    : Nodes, Trias,Quads=      5312     10119         0

AFLR4    : Generate optimal mesh on surface definition 7
AFLR2    : Nodes, Trias,Quads=     17908     35030         0
AFLR4    : Nodes, Trias,Quads=      5567     10348         0

AFLR4    : Generate optimal mesh on surface definition 8
AFLR2    : Nodes, Trias,Quads=      8823     17141         0
AFLR4    : Nodes, Trias,Quads=      4980      9455         0

AFLR4    : Generate optimal mesh on surface definition 9
AFLR2    : Nodes, Trias,Quads=     16876     32967         0
AFLR4    : Nodes, Trias,Quads=      5357      9929         0

AFLR4    : Generate optimal mesh on surface definition 10
AFLR2    : Nodes, Trias,Quads=        55        71         0
AFLR4    : Nodes, Trias,Quads=        46        53         0

AFLR4    : Generate optimal mesh on surface definition 11
AFLR2    : Nodes, Trias,Quads=        73       116         0
AFLR4    : Nodes, Trias,Quads=        68       106         0

AFLR4    : Generate optimal mesh on surface definition 12
AFLR2    : Nodes, Trias,Quads=        73       116         0
AFLR4    : Nodes, Trias,Quads=        68       106         0

AFLR4    : Generate optimal mesh on surface definition 13
AFLR2    : Nodes, Trias,Quads=        73       116         0
AFLR4    : Nodes, Trias,Quads=        68       106         0

AFLR4    : Generate optimal mesh on surface definition 14
AFLR2    : Nodes, Trias,Quads=        73       116         0
AFLR4    : Nodes, Trias,Quads=        68       106         0

AFLR4    : Generate optimal mesh on surface definition 15
AFLR2    : Nodes, Trias,Quads=        73       116         0
AFLR4    : Nodes, Trias,Quads=        68       106         0

AFLR4    : Generate optimal mesh on surface definition 16
AFLR2    : Nodes, Trias,Quads=        73       116         0
AFLR4    : Nodes, Trias,Quads=        68       106         0

DGEOM    : Add surface definitions to composite definition 0
DGEOM    : Glue composite surface definition 0
DGEOM    : Nodes,Faces,BEdges=     40197     80386      5388

AFLR4    : Curvature BG Surface Grid Generation

AFLR4    : Nodes, Faces      =     40197     80386

AFLR4    : Surface Grid Generation

AFLR4    : Generate optimal mesh on surface definition 1
AFLR2    : Nodes, Trias,Quads=      8498     16494         0
AFLR4    : Nodes, Trias,Quads=      6521     12540         0

AFLR4    : Generate optimal mesh on surface definition 2
AFLR2    : Nodes, Trias,Quads=     14215     27654         0
AFLR4    : Nodes, Trias,Quads=     10037     19298         0

AFLR4    : Generate optimal mesh on surface definition 3
AFLR2    : Nodes, Trias,Quads=      8900     17298         0
AFLR4    : Nodes, Trias,Quads=      6655     12808         0

AFLR4    : Generate optimal mesh on surface definition 4
AFLR2    : Nodes, Trias,Quads=     13476     26178         0
AFLR4    : Nodes, Trias,Quads=      9810     18846         0

AFLR4    : Generate optimal mesh on surface definition 5
AFLR2    : Nodes, Trias,Quads=        59        77         0
AFLR4    : Nodes, Trias,Quads=        49        57         0

AFLR4    : Generate optimal mesh on surface definition 6
AFLR2    : Nodes, Trias,Quads=      8503     16504         0
AFLR4    : Nodes, Trias,Quads=      6543     12584         0

AFLR4    : Generate optimal mesh on surface definition 7
AFLR2    : Nodes, Trias,Quads=     13624     26478         0
AFLR4    : Nodes, Trias,Quads=      9963     19156         0

AFLR4    : Generate optimal mesh on surface definition 8
AFLR2    : Nodes, Trias,Quads=      8761     17020         0
AFLR4    : Nodes, Trias,Quads=      6664     12826         0

AFLR4    : Generate optimal mesh on surface definition 9
AFLR2    : Nodes, Trias,Quads=     13534     26300         0
AFLR4    : Nodes, Trias,Quads=      9965     19162         0

AFLR4    : Generate optimal mesh on surface definition 10
AFLR2    : Nodes, Trias,Quads=        60        79         0
AFLR4    : Nodes, Trias,Quads=        49        57         0

AFLR4    : Generate optimal mesh on surface definition 11
AFLR2    : Nodes, Trias,Quads=        73       116         0
AFLR4    : Nodes, Trias,Quads=        68       106         0

AFLR4    : Generate optimal mesh on surface definition 12
AFLR2    : Nodes, Trias,Quads=        73       116         0
AFLR4    : Nodes, Trias,Quads=        68       106         0

AFLR4    : Generate optimal mesh on surface definition 13
AFLR2    : Nodes, Trias,Quads=        73       116         0
AFLR4    : Nodes, Trias,Quads=        68       106         0

AFLR4    : Generate optimal mesh on surface definition 14
AFLR2    : Nodes, Trias,Quads=        73       116         0
AFLR4    : Nodes, Trias,Quads=        68       106         0

AFLR4    : Generate optimal mesh on surface definition 15
AFLR2    : Nodes, Trias,Quads=        73       116         0
AFLR4    : Nodes, Trias,Quads=        68       106         0

AFLR4    : Generate optimal mesh on surface definition 16
AFLR2    : Nodes, Trias,Quads=        73       116         0
AFLR4    : Nodes, Trias,Quads=        68       106         0

DGEOM    : Add surface definitions to composite definition 0
DGEOM    : Glue composite surface definition 0
DGEOM    : Nodes,Faces,BEdges=     63989    127970      5326

OVERALL  : CPU Time          =     1.147   seconds
Body 1 (of 2)
Number of nodes    = 63669
Number of elements = 127334
Number of triangle elements      = 127334
Number of quadrilateral elements = 0
Body 2 (of 2)
Number of nodes    = 320
Number of elements = 636
Number of triangle elements      = 636
Number of quadrilateral elements = 0
----------------------------
Total number of nodes    = 63989
Total number of elements = 127970
Total number of triangle elements      = 127970
Total number of quadrilateral elements = 0

Getting mesh sizing parameters
	Mesh sizing name - Farfield
	Done getting mesh sizing parameters

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.8.1
EGADS    : ---------------------------------------

EGADS    : EGADS CAD Geometry Setup

EGADS    : Model has 2 Active Bodies

EGADS    : Body 0 is a SolidBody
EGADS    : Body 0 has 1 Shells
EGADS    : Body 0 has 10 Faces
EGADS    : Body 0 has 18 Edges
EGADS    : Body 0 has 10 Loops
EGADS    : Body 0 has 10 Nodes
EGADS    : Body 1 is a SolidBody
EGADS    : Body 1 has 1 Shells
EGADS    : Body 1 has 6 Faces
EGADS    : Body 1 has 12 Edges
EGADS    : Body 1 has 6 Loops
EGADS    : Body 1 has 8 Nodes

EGADS    : Check Grid BCs

EGADS    : Grid BCs are OK

EGADS    : Face Neighbor-Faces Information

EGADS    : QC  = Face Quad Combination Flag
EGADS    : IER = Face Isolated Edge Refinement Flag
EGADS    : ER  = Face Edge Refinement Factor
EGADS    :       Not applicable for Faces with a FarField Grid BC.
EGADS    : SF  = Face Scale Factor
EGADS    :       Not applicable for Faces with a FarField Grid BC.

EGADS    :   Face          Body    QC   IER       ER    Scale   Neighbor
EGADS    :     ID  Active    ID  Flag  Flag   Weight   Factor   Faces
EGADS    :      1     Yes     0     0     1        0        1   2 3 6
EGADS    :      2     Yes     0     0     1        0        1   1 4 5
EGADS    :      3     Yes     0     0     1        0        1   1 4 8
EGADS    :      4     Yes     0     0     1        0        1   2 3 5
EGADS    :      5     Yes     0     0     1        0        1   2 4
EGADS    :      6     Yes     0     0     1        0        1   1 7 8
EGADS    :      7     Yes     0     0     1        0        1   6 9 10
EGADS    :      8     Yes     0     0     1        0        1   3 6 9
EGADS    :      9     Yes     0     0     1        0        1   7 8 10
EGADS    :     10     Yes     0     0     1        0        1   7 9
EGADS    :     11     Yes     1     0     1       NA       NA   13 14 15 16
EGADS    :     12     Yes     1     0     1       NA       NA   13 14 15 16
EGADS    :     13     Yes     1     0     1       NA       NA   11 12 15 16
EGADS    :     14     Yes     1     0     1       NA       NA   11 12 15 16
EGADS    :     15     Yes     1     0     1       NA       NA   11 12 13 14
EGADS    :     16     Yes     1     0     1       NA       NA   11 12 13 14

EGADS    : Face Edges Information

EGADS    :   Face   Edges
EGADS    :      1   -1 2 3 -4
EGADS    :      2   -5 4 6 -7
EGADS    :      3   -3 8 1 -9
EGADS    :      4   -6 9 5 -10
EGADS    :      5   7 10
EGADS    :      6   11 13 -12 -2
EGADS    :      7   14 16 -15 -13
EGADS    :      8   12 17 -11 -8
EGADS    :      9   15 18 -14 -17
EGADS    :     10   -16 -18
EGADS    :     11   19 20 -21 -22
EGADS    :     12   -23 26 25 -24
EGADS    :     13   27 23 -28 -19
EGADS    :     14   -29 21 30 -25
EGADS    :     15   22 29 -26 -27
EGADS    :     16   -20 28 24 -30

EGADS    : Face Loops Information

EGADS    :   Face   Loops
EGADS    :      1   1
EGADS    :      2   2
EGADS    :      3   3
EGADS    :      4   4
EGADS    :      5   5
EGADS    :      6   6
EGADS    :      7   7
EGADS    :      8   8
EGADS    :      9   9
EGADS    :     10   10
EGADS    :     11   11
EGADS    :     12   12
EGADS    :     13   13
EGADS    :     14   14
EGADS    :     15   15
EGADS    :     16   16

EGADS    : Loop Edges Information

EGADS    :   Loop  Active   Edges
EGADS    :      1     Yes   -1 2 3 -4
EGADS    :      2     Yes   -5 4 6 -7
EGADS    :      3     Yes   -3 8 1 -9
EGADS    :      4     Yes   -6 9 5 -10
EGADS    :      5     Yes   7 10
EGADS    :      6     Yes   11 13 -12 -2
EGADS    :      7     Yes   14 16 -15 -13
EGADS    :      8     Yes   12 17 -11 -8
EGADS    :      9     Yes   15 18 -14 -17
EGADS    :     10     Yes   -16 -18
EGADS    :     11     Yes   19 20 -21 -22
EGADS    :     12     Yes   -23 26 25 -24
EGADS    :     13     Yes   27 23 -28 -19
EGADS    :     14     Yes   -29 21 30 -25
EGADS    :     15     Yes   22 29 -26 -27
EGADS    :     16     Yes   -20 28 24 -30

EGADS    : Edge Node, Scale Factor, and Neighbor-Faces Information

EGADS    : ESF = Edge Scale Factor
EGADS    :       Not applicable for DEGENERATE Edges or Edges with a FarField
EGADS    :       Grid BC Neighbor Face.

EGADS    :                                             Neighbor
EGADS    :   Edge  Body  Active Node1 Node2      ESF   Faces
EGADS    :      1     0     Yes     1     2        1   1 3
EGADS    :      2     0     Yes     1     3        1   1 6
EGADS    :      3     0     Yes     3     4        1   1 3
EGADS    :      4     0     Yes     2     4        1   1 2
EGADS    :      5     0     Yes     2     5        1   2 4
EGADS    :      6     0     Yes     4     6        1   2 4
EGADS    :      7     0     Yes     5     6        1   2 5
EGADS    :      8     0     Yes     3     1        1   3 8
EGADS    :      9     0     Yes     4     2        1   3 4
EGADS    :     10     0     Yes     6     5        1   4 5
EGADS    :     11     0     Yes     1     7        1   6 8
EGADS    :     12     0     Yes     3     8        1   6 8
EGADS    :     13     0     Yes     7     8        1   6 7
EGADS    :     14     0     Yes     7     9        1   7 9
EGADS    :     15     0     Yes     8    10        1   7 9
EGADS    :     16     0     Yes     9    10        1   7 10
EGADS    :     17     0     Yes     8     7        1   8 9
EGADS    :     18     0     Yes    10     9        1   9 10
EGADS    :     19     1     Yes    12    11       NA   11 13
EGADS    :     20     1     Yes    11    13       NA   11 16
EGADS    :     21     1     Yes    14    13       NA   11 14
EGADS    :     22     1     Yes    12    14       NA   11 15
EGADS    :     23     1     Yes    16    15       NA   12 13
EGADS    :     24     1     Yes    15    17       NA   12 16
EGADS    :     25     1     Yes    18    17       NA   12 14
EGADS    :     26     1     Yes    16    18       NA   12 15
EGADS    :     27     1     Yes    12    16       NA   13 15
EGADS    :     28     1     Yes    11    15       NA   13 16
EGADS    :     29     1     Yes    14    18       NA   14 15
EGADS    :     30     1     Yes    13    17       NA   14 16

EGADS    : Node Information

EGADS    :   Node  Active      Coordinates
EGADS    :      1     Yes       97.2007855                0                0
EGADS    :      2     Yes       97.9335611                0                0
EGADS    :      3     Yes               50                0                0
EGADS    :      4     Yes       75.3047874                0                0
EGADS    :      5     Yes       123.552357                0        4.7180639
EGADS    :      6     Yes       118.391317                0       3.99272703
EGADS    :      7     Yes       97.9335611       36.1389817                0
EGADS    :      8     Yes       75.3047874       36.1389817                0
EGADS    :      9     Yes       123.552357       97.6729236        4.7180639
EGADS    :     10     Yes       118.391317       97.6729236       3.99272703
EGADS    :     11     Yes                0                0       1951.57774
EGADS    :     12     Yes                0                0                0
EGADS    :     13     Yes                0       1953.45847       1951.57774
EGADS    :     14     Yes                0       1953.45847                0
EGADS    :     15     Yes       2040.21562                0       1951.57774
EGADS    :     16     Yes       2040.21562                0                0
EGADS    :     17     Yes       2040.21562       1953.45847       1951.57774
EGADS    :     18     Yes       2040.21562       1953.45847                0

EGADS    : Face and Edge Match Information

EGADS    : No Face Matches Found

AFLR4    : Surface Mesh Spacing Setup

AFLR4    : Max Bounding Box Length     = 3906.92
AFLR4    : Min Bounding Box Length     = 3906.92
AFLR4    : Max Ref Bounding Box Length = 195.346
AFLR4    : Min Ref Bounding Box Length = 13.1976
AFLR4    : Reference Length            = 21.7051
AFLR4    : BL Thickness                = 0
AFLR4    : FarField Spacing            = 168.806
AFLR4    : Abs Min Surf Spacing        = 0.0542627
AFLR4    : Min Surf Spacing            = 0.108525
AFLR4    : Max Surf Spacing            = 2.17051
AFLR4    : Global Scale Factor         = 1

AFLR4    : Geometry Definition Information

AFLR4    : Definition              Definition   Composite             Grid BC
AFLR4    :         ID                    Type          ID                Type
AFLR4    :          0     glue-only composite           -                   -
AFLR4    :          1            CAD geometry           0            STD w/BL
AFLR4    :          2            CAD geometry           0            STD w/BL
AFLR4    :          3            CAD geometry           0            STD w/BL
AFLR4    :          4            CAD geometry           0            STD w/BL
AFLR4    :          5            CAD geometry           0            STD w/BL
AFLR4    :          6            CAD geometry           0            STD w/BL
AFLR4    :          7            CAD geometry           0            STD w/BL
AFLR4    :          8            CAD geometry           0            STD w/BL
AFLR4    :          9            CAD geometry           0            STD w/BL
AFLR4    :         10            CAD geometry           0            STD w/BL
AFLR4    :         11            CAD geometry           0            FARFIELD
AFLR4    :         12            CAD geometry           0            FARFIELD
AFLR4    :         13            CAD geometry           0            FARFIELD
AFLR4    :         14            CAD geometry           0            FARFIELD
AFLR4    :         15            CAD geometry           0            FARFIELD
AFLR4    :         16            CAD geometry           0            FARFIELD

AFLR4    : Define CAD surface definition 1
AFLR4    : Define CAD surface definition 2
AFLR4    : Define CAD surface definition 3
AFLR4    : Define CAD surface definition 4
AFLR4    : Define CAD surface definition 5
AFLR4    : Define CAD surface definition 6
AFLR4    : Define CAD surface definition 7
AFLR4    : Define CAD surface definition 8
AFLR4    : Define CAD surface definition 9
AFLR4    : Define CAD surface definition 10
AFLR4    : Define CAD surface definition 11
AFLR4    : Define CAD surface definition 12
AFLR4    : Define CAD surface definition 13
AFLR4    : Define CAD surface definition 14
AFLR4    : Define CAD surface definition 15
AFLR4    : Define CAD surface definition 16

AFLR4    : Surface Grid Generation

AFLR4    : Generate optimal mesh on surface definition 1
AFLR2    : Nodes, Trias,Quads=      8732     16959         0
AFLR4    : Nodes, Trias,Quads=      5233      9961         0

AFLR4    : Generate optimal mesh on surface definition 2
AFLR2    : Nodes, Trias,Quads=     18087     35388         0
AFLR4    : Nodes, Trias,Quads=      5569     10352         0

AFLR4    : Generate optimal mesh on surface definition 3
AFLR2    : Nodes, Trias,Quads=     10182     19859         0
AFLR4    : Nodes, Trias,Quads=      4951      9397         0

AFLR4    : Generate optimal mesh on surface definition 4
AFLR2    : Nodes, Trias,Quads=     16336     31887         0
AFLR4    : Nodes, Trias,Quads=      5435     10085         0

AFLR4    : Generate optimal mesh on surface definition 5
AFLR2    : Nodes, Trias,Quads=        55        71         0
AFLR4    : Nodes, Trias,Quads=        45        51         0

AFLR4    : Generate optimal mesh on surface definition 6
AFLR2    : Nodes, Trias,Quads=      8705     16905         0
AFLR4    : Nodes, Trias,Quads=      5312     10119         0

AFLR4    : Generate optimal mesh on surface definition 7
AFLR2    : Nodes, Trias,Quads=     17908     35030         0
AFLR4    : Nodes, Trias,Quads=      5567     10348         0

AFLR4    : Generate optimal mesh on surface definition 8
AFLR2    : Nodes, Trias,Quads=      8823     17141         0
AFLR4    : Nodes, Trias,Quads=      4980      9455         0

AFLR4    : Generate optimal mesh on surface definition 9
AFLR2    : Nodes, Trias,Quads=     16876     32967         0
AFLR4    : Nodes, Trias,Quads=      5357      9929         0

AFLR4    : Generate optimal mesh on surface definition 10
AFLR2    : Nodes, Trias,Quads=        55        71         0
AFLR4    : Nodes, Trias,Quads=        46        53         0

AFLR4    : Generate optimal mesh on surface definition 11
AFLR2    : Nodes, Trias,Quads=       655      1216         0
AFLR4    : Nodes, Trias,Quads=       645      1196         0

AFLR4    : Generate optimal mesh on surface definition 12
AFLR2    : Nodes, Trias,Quads=       657      1220         0
AFLR4    : Nodes, Trias,Quads=       644      1194         0

AFLR4    : Generate optimal mesh on surface definition 13
AFLR2    : Nodes, Trias,Quads=       653      1212         0
AFLR4    : Nodes, Trias,Quads=       643      1192         0

AFLR4    : Generate optimal mesh on surface definition 14
AFLR2    : Nodes, Trias,Quads=       655      1216         0
AFLR4    : Nodes, Trias,Quads=       644      1194         0

AFLR4    : Generate optimal mesh on surface definition 15
AFLR2    : Nodes, Trias,Quads=       655      1216         0
AFLR4    : Nodes, Trias,Quads=       642      1190         0

AFLR4    : Generate optimal mesh on surface definition 16
AFLR2    : Nodes, Trias,Quads=       653      1212         0
AFLR4    : Nodes, Trias,Quads=       646      1198         0

DGEOM    : Add surface definitions to composite definition 0
DGEOM    : Glue composite surface definition 0
DGEOM    : Nodes,Faces,BEdges=     43461     86914      5772

AFLR4    : Curvature BG Surface Grid Generation

AFLR4    : Nodes, Faces      =     43461     86914

AFLR4    : Surface Grid Generation

AFLR4    : Generate optimal mesh on surface definition 1
AFLR2    : Nodes, Trias,Quads=      8498     16494         0
AFLR4    : Nodes, Trias,Quads=      6521     12540         0

AFLR4    : Generate optimal mesh on surface definition 2
AFLR2    : Nodes, Trias,Quads=     14215     27654         0
AFLR4    : Nodes, Trias,Quads=     10037     19298         0

AFLR4    : Generate optimal mesh on surface definition 3
AFLR2    : Nodes, Trias,Quads=      8900     17298         0
AFLR4    : Nodes, Trias,Quads=      6655     12808         0

AFLR4    : Generate optimal mesh on surface definition 4
AFLR2    : Nodes, Trias,Quads=     13476     26178         0
AFLR4    : Nodes, Trias,Quads=      9810     18846         0

AFLR4    : Generate optimal mesh on surface definition 5
AFLR2    : Nodes, Trias,Quads=        59        77         0
AFLR4    : Nodes, Trias,Quads=        49        57         0

AFLR4    : Generate optimal mesh on surface definition 6
AFLR2    : Nodes, Trias,Quads=      8503     16504         0
AFLR4    : Nodes, Trias,Quads=      6543     12584         0

AFLR4    : Generate optimal mesh on surface definition 7
AFLR2    : Nodes, Trias,Quads=     13624     26478         0
AFLR4    : Nodes, Trias,Quads=      9963     19156         0

AFLR4    : Generate optimal mesh on surface definition 8
AFLR2    : Nodes, Trias,Quads=      8761     17020         0
AFLR4    : Nodes, Trias,Quads=      6664     12826         0

AFLR4    : Generate optimal mesh on surface definition 9
AFLR2    : Nodes, Trias,Quads=     13534     26300         0
AFLR4    : Nodes, Trias,Quads=      9965     19162         0

AFLR4    : Generate optimal mesh on surface definition 10
AFLR2    : Nodes, Trias,Quads=        60        79         0
AFLR4    : Nodes, Trias,Quads=        49        57         0

AFLR4    : Generate optimal mesh on surface definition 11
AFLR2    : Nodes, Trias,Quads=       671      1248         0
AFLR4    : Nodes, Trias,Quads=       647      1200         0

AFLR4    : Generate optimal mesh on surface definition 12
AFLR2    : Nodes, Trias,Quads=       671      1248         0
AFLR4    : Nodes, Trias,Quads=       646      1198         0

AFLR4    : Generate optimal mesh on surface definition 13
AFLR2    : Nodes, Trias,Quads=       672      1250         0
AFLR4    : Nodes, Trias,Quads=       642      1190         0

AFLR4    : Generate optimal mesh on surface definition 14
AFLR2    : Nodes, Trias,Quads=       670      1246         0
AFLR4    : Nodes, Trias,Quads=       645      1196         0

AFLR4    : Generate optimal mesh on surface definition 15
AFLR2    : Nodes, Trias,Quads=       672      1250         0
AFLR4    : Nodes, Trias,Quads=       644      1194         0

AFLR4    : Generate optimal mesh on surface definition 16
AFLR2    : Nodes, Trias,Quads=       670      1246         0
AFLR4    : Nodes, Trias,Quads=       646      1198         0

DGEOM    : Add surface definitions to composite definition 0
DGEOM    : Glue composite surface definition 0
DGEOM    : Nodes,Faces,BEdges=     67259    134510      5710

OVERALL  : CPU Time          =     1.206   seconds
Body 1 (of 2)
Number of nodes    = 63669
Number of elements = 127334
Number of triangle elements      = 127334
Number of quadrilateral elements = 0
Body 2 (of 2)
Number of nodes    = 3590
Number of elements = 7176
Number of triangle elements      = 7176
Number of quadrilateral elements = 0
----------------------------
Total number of nodes    = 67259
Total number of elements = 134510
Total number of triangle elements      = 134510
Total number of quadrilateral elements = 0

real	0m4.415s
user	0m4.188s
sys	0m0.504s
+ status=0
+ set +x

=================================================
data/session07/02_aflr4_Farfield.py passed (as expected)
=================================================


=================================================
03_aflr4_MeshLength.py test;
+ python 03_aflr4_MeshLength.py
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/CAPS/training/2023/training.log

MESSAGE:: Building wingOml

Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 2
	Name = Wing, index = 1
	Name = Farfield, index = 2
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 3
	Name = leftWing, index = 1
	Name = riteWing, index = 2
	Name = Farfield, index = 3

Getting mesh sizing parameters
	Mesh sizing name - Farfield
	Done getting mesh sizing parameters
 
AFLR2    : ---------------------------------------
AFLR2    : AFLR2 LIBRARY
AFLR2    : ADVANCING-FRONT/LOCAL-RECONNECTION
AFLR2    : TRIA/QUAD GRID GENERATOR
AFLR2    : Version Number 9.18.1
AFLR2    : Version Date   06/11/24 @ 05:52PM
AFLR2    : Compile OS     Darwin 23.5.0 arm64
AFLR2    : Compile Date   06/11/24 @ 05:52PM
AFLR2    : Copyright 1994-2021, D.L. Marcum
AFLR2    : ---------------------------------------
 
AFLR4    : ---------------------------------------
AFLR4    : AFLR4 LIBRARY
AFLR4    : ADVANCING-FRONT/LOCAL-RECONNECTION
AFLR4    : TRIA/QUAD SURFACE GRID GENERATOR
AFLR4    : Version Number 11.5.15
AFLR4    : Version Date   07/19/24 @ 07:04PM
AFLR4    : Compile OS     Darwin 23.5.0 arm64
AFLR4    : Compile Date   07/19/24 @ 07:06PM
AFLR4    : Copyright 1994-2021, D.L. Marcum
AFLR4    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.8.1
EGADS    : ---------------------------------------

EGADS    : EGADS CAD Geometry Setup

EGADS    : Model has 2 Active Bodies

EGADS    : Body 0 is a SolidBody
EGADS    : Body 0 has 1 Shells
EGADS    : Body 0 has 10 Faces
EGADS    : Body 0 has 18 Edges
EGADS    : Body 0 has 10 Loops
EGADS    : Body 0 has 10 Nodes
EGADS    : Body 1 is a SolidBody
EGADS    : Body 1 has 1 Shells
EGADS    : Body 1 has 6 Faces
EGADS    : Body 1 has 12 Edges
EGADS    : Body 1 has 6 Loops
EGADS    : Body 1 has 8 Nodes

EGADS    : Check Grid BCs

EGADS    : Grid BCs are OK

EGADS    : Face Neighbor-Faces Information

EGADS    : QC  = Face Quad Combination Flag
EGADS    : IER = Face Isolated Edge Refinement Flag
EGADS    : ER  = Face Edge Refinement Factor
EGADS    :       Not applicable for Faces with a FarField Grid BC.
EGADS    : SF  = Face Scale Factor
EGADS    :       Not applicable for Faces with a FarField Grid BC.

EGADS    :   Face          Body    QC   IER       ER    Scale   Neighbor
EGADS    :     ID  Active    ID  Flag  Flag   Weight   Factor   Faces
EGADS    :      1     Yes     0     0     1        0        1   2 3 6
EGADS    :      2     Yes     0     0     1        0        1   1 4 5
EGADS    :      3     Yes     0     0     1        0        1   1 4 8
EGADS    :      4     Yes     0     0     1        0        1   2 3 5
EGADS    :      5     Yes     0     0     1        0        1   2 4
EGADS    :      6     Yes     0     0     1        0        1   1 7 8
EGADS    :      7     Yes     0     0     1        0        1   6 9 10
EGADS    :      8     Yes     0     0     1        0        1   3 6 9
EGADS    :      9     Yes     0     0     1        0        1   7 8 10
EGADS    :     10     Yes     0     0     1        0        1   7 9
EGADS    :     11     Yes     1     0     1       NA       NA   13 14 15 16
EGADS    :     12     Yes     1     0     1       NA       NA   13 14 15 16
EGADS    :     13     Yes     1     0     1       NA       NA   11 12 15 16
EGADS    :     14     Yes     1     0     1       NA       NA   11 12 15 16
EGADS    :     15     Yes     1     0     1       NA       NA   11 12 13 14
EGADS    :     16     Yes     1     0     1       NA       NA   11 12 13 14

EGADS    : Face Edges Information

EGADS    :   Face   Edges
EGADS    :      1   -1 2 3 -4
EGADS    :      2   -5 4 6 -7
EGADS    :      3   -3 8 1 -9
EGADS    :      4   -6 9 5 -10
EGADS    :      5   7 10
EGADS    :      6   11 13 -12 -2
EGADS    :      7   14 16 -15 -13
EGADS    :      8   12 17 -11 -8
EGADS    :      9   15 18 -14 -17
EGADS    :     10   -16 -18
EGADS    :     11   19 20 -21 -22
EGADS    :     12   -23 26 25 -24
EGADS    :     13   27 23 -28 -19
EGADS    :     14   -29 21 30 -25
EGADS    :     15   22 29 -26 -27
EGADS    :     16   -20 28 24 -30

EGADS    : Face Loops Information

EGADS    :   Face   Loops
EGADS    :      1   1
EGADS    :      2   2
EGADS    :      3   3
EGADS    :      4   4
EGADS    :      5   5
EGADS    :      6   6
EGADS    :      7   7
EGADS    :      8   8
EGADS    :      9   9
EGADS    :     10   10
EGADS    :     11   11
EGADS    :     12   12
EGADS    :     13   13
EGADS    :     14   14
EGADS    :     15   15
EGADS    :     16   16

EGADS    : Loop Edges Information

EGADS    :   Loop  Active   Edges
EGADS    :      1     Yes   -1 2 3 -4
EGADS    :      2     Yes   -5 4 6 -7
EGADS    :      3     Yes   -3 8 1 -9
EGADS    :      4     Yes   -6 9 5 -10
EGADS    :      5     Yes   7 10
EGADS    :      6     Yes   11 13 -12 -2
EGADS    :      7     Yes   14 16 -15 -13
EGADS    :      8     Yes   12 17 -11 -8
EGADS    :      9     Yes   15 18 -14 -17
EGADS    :     10     Yes   -16 -18
EGADS    :     11     Yes   19 20 -21 -22
EGADS    :     12     Yes   -23 26 25 -24
EGADS    :     13     Yes   27 23 -28 -19
EGADS    :     14     Yes   -29 21 30 -25
EGADS    :     15     Yes   22 29 -26 -27
EGADS    :     16     Yes   -20 28 24 -30

EGADS    : Edge Node, Scale Factor, and Neighbor-Faces Information

EGADS    : ESF = Edge Scale Factor
EGADS    :       Not applicable for DEGENERATE Edges or Edges with a FarField
EGADS    :       Grid BC Neighbor Face.

EGADS    :                                             Neighbor
EGADS    :   Edge  Body  Active Node1 Node2      ESF   Faces
EGADS    :      1     0     Yes     1     2        1   1 3
EGADS    :      2     0     Yes     1     3        1   1 6
EGADS    :      3     0     Yes     3     4        1   1 3
EGADS    :      4     0     Yes     2     4        1   1 2
EGADS    :      5     0     Yes     2     5        1   2 4
EGADS    :      6     0     Yes     4     6        1   2 4
EGADS    :      7     0     Yes     5     6        1   2 5
EGADS    :      8     0     Yes     3     1        1   3 8
EGADS    :      9     0     Yes     4     2        1   3 4
EGADS    :     10     0     Yes     6     5        1   4 5
EGADS    :     11     0     Yes     1     7        1   6 8
EGADS    :     12     0     Yes     3     8        1   6 8
EGADS    :     13     0     Yes     7     8        1   6 7
EGADS    :     14     0     Yes     7     9        1   7 9
EGADS    :     15     0     Yes     8    10        1   7 9
EGADS    :     16     0     Yes     9    10        1   7 10
EGADS    :     17     0     Yes     8     7        1   8 9
EGADS    :     18     0     Yes    10     9        1   9 10
EGADS    :     19     1     Yes    12    11       NA   11 13
EGADS    :     20     1     Yes    11    13       NA   11 16
EGADS    :     21     1     Yes    14    13       NA   11 14
EGADS    :     22     1     Yes    12    14       NA   11 15
EGADS    :     23     1     Yes    16    15       NA   12 13
EGADS    :     24     1     Yes    15    17       NA   12 16
EGADS    :     25     1     Yes    18    17       NA   12 14
EGADS    :     26     1     Yes    16    18       NA   12 15
EGADS    :     27     1     Yes    12    16       NA   13 15
EGADS    :     28     1     Yes    11    15       NA   13 16
EGADS    :     29     1     Yes    14    18       NA   14 15
EGADS    :     30     1     Yes    13    17       NA   14 16

EGADS    : Node Information

EGADS    :   Node  Active      Coordinates
EGADS    :      1     Yes       97.2007855                0                0
EGADS    :      2     Yes       97.9335611                0                0
EGADS    :      3     Yes               50                0                0
EGADS    :      4     Yes       75.3047874                0                0
EGADS    :      5     Yes       123.552357                0        4.7180639
EGADS    :      6     Yes       118.391317                0       3.99272703
EGADS    :      7     Yes       97.9335611       36.1389817                0
EGADS    :      8     Yes       75.3047874       36.1389817                0
EGADS    :      9     Yes       123.552357       97.6729236        4.7180639
EGADS    :     10     Yes       118.391317       97.6729236       3.99272703
EGADS    :     11     Yes                0                0       1951.57774
EGADS    :     12     Yes                0                0                0
EGADS    :     13     Yes                0       1953.45847       1951.57774
EGADS    :     14     Yes                0       1953.45847                0
EGADS    :     15     Yes       2040.21562                0       1951.57774
EGADS    :     16     Yes       2040.21562                0                0
EGADS    :     17     Yes       2040.21562       1953.45847       1951.57774
EGADS    :     18     Yes       2040.21562       1953.45847                0

EGADS    : Face and Edge Match Information

EGADS    : No Face Matches Found

AFLR4    : Surface Mesh Spacing Setup

AFLR4    : Max Bounding Box Length     = 3906.92
AFLR4    : Min Bounding Box Length     = 3906.92
AFLR4    : Max Ref Bounding Box Length = 195.346
AFLR4    : Min Ref Bounding Box Length = 13.1976
AFLR4    : Reference Length            = 21.7051
AFLR4    : BL Thickness                = 0
AFLR4    : FarField Spacing            = 530.379
AFLR4    : Abs Min Surf Spacing        = 0.0217051
AFLR4    : Min Surf Spacing            = 0.217051
AFLR4    : Max Surf Spacing            = 2.17051
AFLR4    : Global Scale Factor         = 1

AFLR4    : Geometry Definition Information

AFLR4    : Definition              Definition   Composite             Grid BC
AFLR4    :         ID                    Type          ID                Type
AFLR4    :          0     glue-only composite           -                   -
AFLR4    :          1            CAD geometry           0            STD w/BL
AFLR4    :          2            CAD geometry           0            STD w/BL
AFLR4    :          3            CAD geometry           0            STD w/BL
AFLR4    :          4            CAD geometry           0            STD w/BL
AFLR4    :          5            CAD geometry           0            STD w/BL
AFLR4    :          6            CAD geometry           0            STD w/BL
AFLR4    :          7            CAD geometry           0            STD w/BL
AFLR4    :          8            CAD geometry           0            STD w/BL
AFLR4    :          9            CAD geometry           0            STD w/BL
AFLR4    :         10            CAD geometry           0            STD w/BL
AFLR4    :         11            CAD geometry           0            FARFIELD
AFLR4    :         12            CAD geometry           0            FARFIELD
AFLR4    :         13            CAD geometry           0            FARFIELD
AFLR4    :         14            CAD geometry           0            FARFIELD
AFLR4    :         15            CAD geometry           0            FARFIELD
AFLR4    :         16            CAD geometry           0            FARFIELD

AFLR4    : Define CAD surface definition 1
AFLR4    : Define CAD surface definition 2
AFLR4    : Define CAD surface definition 3
AFLR4    : Define CAD surface definition 4
AFLR4    : Define CAD surface definition 5
AFLR4    : Define CAD surface definition 6
AFLR4    : Define CAD surface definition 7
AFLR4    : Define CAD surface definition 8
AFLR4    : Define CAD surface definition 9
AFLR4    : Define CAD surface definition 10
AFLR4    : Define CAD surface definition 11
AFLR4    : Define CAD surface definition 12
AFLR4    : Define CAD surface definition 13
AFLR4    : Define CAD surface definition 14
AFLR4    : Define CAD surface definition 15
AFLR4    : Define CAD surface definition 16

AFLR4    : Surface Grid Generation

AFLR4    : Generate optimal mesh on surface definition 1
AFLR2    : Nodes, Trias,Quads=      3815      7343         0
AFLR4    : Nodes, Trias,Quads=      2646      5005         0

AFLR4    : Generate optimal mesh on surface definition 2
AFLR2    : Nodes, Trias,Quads=      7199     13974         0
AFLR4    : Nodes, Trias,Quads=      2681      4938         0

AFLR4    : Generate optimal mesh on surface definition 3
AFLR2    : Nodes, Trias,Quads=      3862      7438         0
AFLR4    : Nodes, Trias,Quads=      2506      4726         0

AFLR4    : Generate optimal mesh on surface definition 4
AFLR2    : Nodes, Trias,Quads=      6786     13148         0
AFLR4    : Nodes, Trias,Quads=      2612      4800         0

AFLR4    : Generate optimal mesh on surface definition 5
AFLR2    : Nodes, Trias,Quads=        39        50         0
AFLR4    : Nodes, Trias,Quads=        26        24         0

AFLR4    : Generate optimal mesh on surface definition 6
AFLR2    : Nodes, Trias,Quads=      3812      7337         0
AFLR4    : Nodes, Trias,Quads=      2636      4985         0

AFLR4    : Generate optimal mesh on surface definition 7
AFLR2    : Nodes, Trias,Quads=      7156     13888         0
AFLR4    : Nodes, Trias,Quads=      2677      4930         0

AFLR4    : Generate optimal mesh on surface definition 8
AFLR2    : Nodes, Trias,Quads=      3757      7228         0
AFLR4    : Nodes, Trias,Quads=      2510      4734         0

AFLR4    : Generate optimal mesh on surface definition 9
AFLR2    : Nodes, Trias,Quads=      6920     13416         0
AFLR4    : Nodes, Trias,Quads=      2582      4740         0

AFLR4    : Generate optimal mesh on surface definition 10
AFLR2    : Nodes, Trias,Quads=        39        50         0
AFLR4    : Nodes, Trias,Quads=        26        24         0

AFLR4    : Generate optimal mesh on surface definition 11
AFLR2    : Nodes, Trias,Quads=        73       116         0
AFLR4    : Nodes, Trias,Quads=        68       106         0

AFLR4    : Generate optimal mesh on surface definition 12
AFLR2    : Nodes, Trias,Quads=        73       116         0
AFLR4    : Nodes, Trias,Quads=        68       106         0

AFLR4    : Generate optimal mesh on surface definition 13
AFLR2    : Nodes, Trias,Quads=        73       116         0
AFLR4    : Nodes, Trias,Quads=        68       106         0

AFLR4    : Generate optimal mesh on surface definition 14
AFLR2    : Nodes, Trias,Quads=        73       116         0
AFLR4    : Nodes, Trias,Quads=        68       106         0

AFLR4    : Generate optimal mesh on surface definition 15
AFLR2    : Nodes, Trias,Quads=        73       116         0
AFLR4    : Nodes, Trias,Quads=        68       106         0

AFLR4    : Generate optimal mesh on surface definition 16
AFLR2    : Nodes, Trias,Quads=        73       116         0
AFLR4    : Nodes, Trias,Quads=        68       106         0

DGEOM    : Add surface definitions to composite definition 0
DGEOM    : Glue composite surface definition 0
DGEOM    : Nodes,Faces,BEdges=     19775     39542      3046

AFLR4    : Curvature BG Surface Grid Generation

AFLR4    : Nodes, Faces      =     19775     39542

AFLR4    : Surface Grid Generation

AFLR4    : Generate optimal mesh on surface definition 1
AFLR2    : Nodes, Trias,Quads=      3762      7238         0
AFLR4    : Nodes, Trias,Quads=      3236      6186         0

AFLR4    : Generate optimal mesh on surface definition 2
AFLR2    : Nodes, Trias,Quads=      6248     12075         0
AFLR4    : Nodes, Trias,Quads=      4502      8583         0

AFLR4    : Generate optimal mesh on surface definition 3
AFLR2    : Nodes, Trias,Quads=      3744      7203         0
AFLR4    : Nodes, Trias,Quads=      3175      6065         0

AFLR4    : Generate optimal mesh on surface definition 4
AFLR2    : Nodes, Trias,Quads=      6002     11583         0
AFLR4    : Nodes, Trias,Quads=      4327      8233         0

AFLR4    : Generate optimal mesh on surface definition 5
AFLR2    : Nodes, Trias,Quads=        43        56         0
AFLR4    : Nodes, Trias,Quads=        29        28         0

AFLR4    : Generate optimal mesh on surface definition 6
AFLR2    : Nodes, Trias,Quads=      3772      7258         0
AFLR4    : Nodes, Trias,Quads=      3224      6162         0

AFLR4    : Generate optimal mesh on surface definition 7
AFLR2    : Nodes, Trias,Quads=      6181     11942         0
AFLR4    : Nodes, Trias,Quads=      4495      8570         0

AFLR4    : Generate optimal mesh on surface definition 8
AFLR2    : Nodes, Trias,Quads=      3662      7039         0
AFLR4    : Nodes, Trias,Quads=      3196      6107         0

AFLR4    : Generate optimal mesh on surface definition 9
AFLR2    : Nodes, Trias,Quads=      6208     11996         0
AFLR4    : Nodes, Trias,Quads=      4366      8312         0

AFLR4    : Generate optimal mesh on surface definition 10
AFLR2    : Nodes, Trias,Quads=        43        56         0
AFLR4    : Nodes, Trias,Quads=        29        28         0

AFLR4    : Generate optimal mesh on surface definition 11
AFLR2    : Nodes, Trias,Quads=        73       116         0
AFLR4    : Nodes, Trias,Quads=        68       106         0

AFLR4    : Generate optimal mesh on surface definition 12
AFLR2    : Nodes, Trias,Quads=        73       116         0
AFLR4    : Nodes, Trias,Quads=        68       106         0

AFLR4    : Generate optimal mesh on surface definition 13
AFLR2    : Nodes, Trias,Quads=        73       116         0
AFLR4    : Nodes, Trias,Quads=        68       106         0

AFLR4    : Generate optimal mesh on surface definition 14
AFLR2    : Nodes, Trias,Quads=        73       116         0
AFLR4    : Nodes, Trias,Quads=        68       106         0

AFLR4    : Generate optimal mesh on surface definition 15
AFLR2    : Nodes, Trias,Quads=        73       116         0
AFLR4    : Nodes, Trias,Quads=        68       106         0

AFLR4    : Generate optimal mesh on surface definition 16
AFLR2    : Nodes, Trias,Quads=        73       116         0
AFLR4    : Nodes, Trias,Quads=        68       106         0

DGEOM    : Add surface definitions to composite definition 0
DGEOM    : Glue composite surface definition 0
DGEOM    : Nodes,Faces,BEdges=     29459     58910      3032

OVERALL  : CPU Time          =     0.478   seconds
Body 1 (of 2)
Number of nodes    = 29139
Number of elements = 58274
Number of triangle elements      = 58274
Number of quadrilateral elements = 0
Body 2 (of 2)
Number of nodes    = 320
Number of elements = 636
Number of triangle elements      = 636
Number of quadrilateral elements = 0
----------------------------
Total number of nodes    = 29459
Total number of elements = 58910
Total number of triangle elements      = 58910
Total number of quadrilateral elements = 0

Getting mesh sizing parameters
	Mesh sizing name - Farfield
	Done getting mesh sizing parameters

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.8.1
EGADS    : ---------------------------------------

EGADS    : EGADS CAD Geometry Setup

EGADS    : Model has 2 Active Bodies

EGADS    : Body 0 is a SolidBody
EGADS    : Body 0 has 1 Shells
EGADS    : Body 0 has 10 Faces
EGADS    : Body 0 has 18 Edges
EGADS    : Body 0 has 10 Loops
EGADS    : Body 0 has 10 Nodes
EGADS    : Body 1 is a SolidBody
EGADS    : Body 1 has 1 Shells
EGADS    : Body 1 has 6 Faces
EGADS    : Body 1 has 12 Edges
EGADS    : Body 1 has 6 Loops
EGADS    : Body 1 has 8 Nodes

EGADS    : Check Grid BCs

EGADS    : Grid BCs are OK

EGADS    : Face Neighbor-Faces Information

EGADS    : QC  = Face Quad Combination Flag
EGADS    : IER = Face Isolated Edge Refinement Flag
EGADS    : ER  = Face Edge Refinement Factor
EGADS    :       Not applicable for Faces with a FarField Grid BC.
EGADS    : SF  = Face Scale Factor
EGADS    :       Not applicable for Faces with a FarField Grid BC.

EGADS    :   Face          Body    QC   IER       ER    Scale   Neighbor
EGADS    :     ID  Active    ID  Flag  Flag   Weight   Factor   Faces
EGADS    :      1     Yes     0     0     1        0        1   2 3 6
EGADS    :      2     Yes     0     0     1        0        1   1 4 5
EGADS    :      3     Yes     0     0     1        0        1   1 4 8
EGADS    :      4     Yes     0     0     1        0        1   2 3 5
EGADS    :      5     Yes     0     0     1        0        1   2 4
EGADS    :      6     Yes     0     0     1        0        1   1 7 8
EGADS    :      7     Yes     0     0     1        0        1   6 9 10
EGADS    :      8     Yes     0     0     1        0        1   3 6 9
EGADS    :      9     Yes     0     0     1        0        1   7 8 10
EGADS    :     10     Yes     0     0     1        0        1   7 9
EGADS    :     11     Yes     1     0     1       NA       NA   13 14 15 16
EGADS    :     12     Yes     1     0     1       NA       NA   13 14 15 16
EGADS    :     13     Yes     1     0     1       NA       NA   11 12 15 16
EGADS    :     14     Yes     1     0     1       NA       NA   11 12 15 16
EGADS    :     15     Yes     1     0     1       NA       NA   11 12 13 14
EGADS    :     16     Yes     1     0     1       NA       NA   11 12 13 14

EGADS    : Face Edges Information

EGADS    :   Face   Edges
EGADS    :      1   -1 2 3 -4
EGADS    :      2   -5 4 6 -7
EGADS    :      3   -3 8 1 -9
EGADS    :      4   -6 9 5 -10
EGADS    :      5   7 10
EGADS    :      6   11 13 -12 -2
EGADS    :      7   14 16 -15 -13
EGADS    :      8   12 17 -11 -8
EGADS    :      9   15 18 -14 -17
EGADS    :     10   -16 -18
EGADS    :     11   19 20 -21 -22
EGADS    :     12   -23 26 25 -24
EGADS    :     13   27 23 -28 -19
EGADS    :     14   -29 21 30 -25
EGADS    :     15   22 29 -26 -27
EGADS    :     16   -20 28 24 -30

EGADS    : Face Loops Information

EGADS    :   Face   Loops
EGADS    :      1   1
EGADS    :      2   2
EGADS    :      3   3
EGADS    :      4   4
EGADS    :      5   5
EGADS    :      6   6
EGADS    :      7   7
EGADS    :      8   8
EGADS    :      9   9
EGADS    :     10   10
EGADS    :     11   11
EGADS    :     12   12
EGADS    :     13   13
EGADS    :     14   14
EGADS    :     15   15
EGADS    :     16   16

EGADS    : Loop Edges Information

EGADS    :   Loop  Active   Edges
EGADS    :      1     Yes   -1 2 3 -4
EGADS    :      2     Yes   -5 4 6 -7
EGADS    :      3     Yes   -3 8 1 -9
EGADS    :      4     Yes   -6 9 5 -10
EGADS    :      5     Yes   7 10
EGADS    :      6     Yes   11 13 -12 -2
EGADS    :      7     Yes   14 16 -15 -13
EGADS    :      8     Yes   12 17 -11 -8
EGADS    :      9     Yes   15 18 -14 -17
EGADS    :     10     Yes   -16 -18
EGADS    :     11     Yes   19 20 -21 -22
EGADS    :     12     Yes   -23 26 25 -24
EGADS    :     13     Yes   27 23 -28 -19
EGADS    :     14     Yes   -29 21 30 -25
EGADS    :     15     Yes   22 29 -26 -27
EGADS    :     16     Yes   -20 28 24 -30

EGADS    : Edge Node, Scale Factor, and Neighbor-Faces Information

EGADS    : ESF = Edge Scale Factor
EGADS    :       Not applicable for DEGENERATE Edges or Edges with a FarField
EGADS    :       Grid BC Neighbor Face.

EGADS    :                                             Neighbor
EGADS    :   Edge  Body  Active Node1 Node2      ESF   Faces
EGADS    :      1     0     Yes     1     2        1   1 3
EGADS    :      2     0     Yes     1     3        1   1 6
EGADS    :      3     0     Yes     3     4        1   1 3
EGADS    :      4     0     Yes     2     4        1   1 2
EGADS    :      5     0     Yes     2     5        1   2 4
EGADS    :      6     0     Yes     4     6        1   2 4
EGADS    :      7     0     Yes     5     6        1   2 5
EGADS    :      8     0     Yes     3     1        1   3 8
EGADS    :      9     0     Yes     4     2        1   3 4
EGADS    :     10     0     Yes     6     5        1   4 5
EGADS    :     11     0     Yes     1     7        1   6 8
EGADS    :     12     0     Yes     3     8        1   6 8
EGADS    :     13     0     Yes     7     8        1   6 7
EGADS    :     14     0     Yes     7     9        1   7 9
EGADS    :     15     0     Yes     8    10        1   7 9
EGADS    :     16     0     Yes     9    10        1   7 10
EGADS    :     17     0     Yes     8     7        1   8 9
EGADS    :     18     0     Yes    10     9        1   9 10
EGADS    :     19     1     Yes    12    11       NA   11 13
EGADS    :     20     1     Yes    11    13       NA   11 16
EGADS    :     21     1     Yes    14    13       NA   11 14
EGADS    :     22     1     Yes    12    14       NA   11 15
EGADS    :     23     1     Yes    16    15       NA   12 13
EGADS    :     24     1     Yes    15    17       NA   12 16
EGADS    :     25     1     Yes    18    17       NA   12 14
EGADS    :     26     1     Yes    16    18       NA   12 15
EGADS    :     27     1     Yes    12    16       NA   13 15
EGADS    :     28     1     Yes    11    15       NA   13 16
EGADS    :     29     1     Yes    14    18       NA   14 15
EGADS    :     30     1     Yes    13    17       NA   14 16

EGADS    : Node Information

EGADS    :   Node  Active      Coordinates
EGADS    :      1     Yes       97.2007855                0                0
EGADS    :      2     Yes       97.9335611                0                0
EGADS    :      3     Yes               50                0                0
EGADS    :      4     Yes       75.3047874                0                0
EGADS    :      5     Yes       123.552357                0        4.7180639
EGADS    :      6     Yes       118.391317                0       3.99272703
EGADS    :      7     Yes       97.9335611       36.1389817                0
EGADS    :      8     Yes       75.3047874       36.1389817                0
EGADS    :      9     Yes       123.552357       97.6729236        4.7180639
EGADS    :     10     Yes       118.391317       97.6729236       3.99272703
EGADS    :     11     Yes                0                0       1951.57774
EGADS    :     12     Yes                0                0                0
EGADS    :     13     Yes                0       1953.45847       1951.57774
EGADS    :     14     Yes                0       1953.45847                0
EGADS    :     15     Yes       2040.21562                0       1951.57774
EGADS    :     16     Yes       2040.21562                0                0
EGADS    :     17     Yes       2040.21562       1953.45847       1951.57774
EGADS    :     18     Yes       2040.21562       1953.45847                0

EGADS    : Face and Edge Match Information

EGADS    : No Face Matches Found

AFLR4    : Surface Mesh Spacing Setup

AFLR4    : Max Bounding Box Length     = 3906.92
AFLR4    : Min Bounding Box Length     = 3906.92
AFLR4    : Max Ref Bounding Box Length = 195.346
AFLR4    : Min Ref Bounding Box Length = 13.1976
AFLR4    : Reference Length            = 21.7051
AFLR4    : BL Thickness                = 0
AFLR4    : FarField Spacing            = 1591.14
AFLR4    : Abs Min Surf Spacing        = 0.0217051
AFLR4    : Min Surf Spacing            = 0.217051
AFLR4    : Max Surf Spacing            = 2.17051
AFLR4    : Global Scale Factor         = 3

AFLR4    : Geometry Definition Information

AFLR4    : Definition              Definition   Composite             Grid BC
AFLR4    :         ID                    Type          ID                Type
AFLR4    :          0     glue-only composite           -                   -
AFLR4    :          1            CAD geometry           0            STD w/BL
AFLR4    :          2            CAD geometry           0            STD w/BL
AFLR4    :          3            CAD geometry           0            STD w/BL
AFLR4    :          4            CAD geometry           0            STD w/BL
AFLR4    :          5            CAD geometry           0            STD w/BL
AFLR4    :          6            CAD geometry           0            STD w/BL
AFLR4    :          7            CAD geometry           0            STD w/BL
AFLR4    :          8            CAD geometry           0            STD w/BL
AFLR4    :          9            CAD geometry           0            STD w/BL
AFLR4    :         10            CAD geometry           0            STD w/BL
AFLR4    :         11            CAD geometry           0            FARFIELD
AFLR4    :         12            CAD geometry           0            FARFIELD
AFLR4    :         13            CAD geometry           0            FARFIELD
AFLR4    :         14            CAD geometry           0            FARFIELD
AFLR4    :         15            CAD geometry           0            FARFIELD
AFLR4    :         16            CAD geometry           0            FARFIELD

AFLR4    : Define CAD surface definition 1
AFLR4    : Define CAD surface definition 2
AFLR4    : Define CAD surface definition 3
AFLR4    : Define CAD surface definition 4
AFLR4    : Define CAD surface definition 5
AFLR4    : Define CAD surface definition 6
AFLR4    : Define CAD surface definition 7
AFLR4    : Define CAD surface definition 8
AFLR4    : Define CAD surface definition 9
AFLR4    : Define CAD surface definition 10
AFLR4    : Define CAD surface definition 11
AFLR4    : Define CAD surface definition 12
AFLR4    : Define CAD surface definition 13
AFLR4    : Define CAD surface definition 14
AFLR4    : Define CAD surface definition 15
AFLR4    : Define CAD surface definition 16

AFLR4    : Surface Grid Generation

AFLR4    : Generate optimal mesh on surface definition 1
AFLR2    : Nodes, Trias,Quads=       890      1664         0
AFLR4    : Nodes, Trias,Quads=       575      1034         0

AFLR4    : Generate optimal mesh on surface definition 2
AFLR2    : Nodes, Trias,Quads=      1164      2167         0
AFLR4    : Nodes, Trias,Quads=       586      1011         0

AFLR4    : Generate optimal mesh on surface definition 3
AFLR2    : Nodes, Trias,Quads=       884      1654         0
AFLR4    : Nodes, Trias,Quads=       539       964         0

AFLR4    : Generate optimal mesh on surface definition 4
AFLR2    : Nodes, Trias,Quads=      1120      2080         0
AFLR4    : Nodes, Trias,Quads=       569       978         0

AFLR4    : Generate optimal mesh on surface definition 5
AFLR2    : Nodes, Trias,Quads=        17        20         0
AFLR4    : Nodes, Trias,Quads=        12        10         0

AFLR4    : Generate optimal mesh on surface definition 6
AFLR2    : Nodes, Trias,Quads=       887      1658         0
AFLR4    : Nodes, Trias,Quads=       575      1034         0

AFLR4    : Generate optimal mesh on surface definition 7
AFLR2    : Nodes, Trias,Quads=      1168      2175         0
AFLR4    : Nodes, Trias,Quads=       589      1017         0

AFLR4    : Generate optimal mesh on surface definition 8
AFLR2    : Nodes, Trias,Quads=       880      1646         0
AFLR4    : Nodes, Trias,Quads=       535       956         0

AFLR4    : Generate optimal mesh on surface definition 9
AFLR2    : Nodes, Trias,Quads=      1113      2066         0
AFLR4    : Nodes, Trias,Quads=       566       972         0

AFLR4    : Generate optimal mesh on surface definition 10
AFLR2    : Nodes, Trias,Quads=        17        20         0
AFLR4    : Nodes, Trias,Quads=        12        10         0

AFLR4    : Generate optimal mesh on surface definition 11
AFLR2    : Nodes, Trias,Quads=        12        14         0
AFLR4    : Nodes, Trias,Quads=         8         6         0

AFLR4    : Generate optimal mesh on surface definition 12
AFLR2    : Nodes, Trias,Quads=        12        14         0
AFLR4    : Nodes, Trias,Quads=         8         6         0

AFLR4    : Generate optimal mesh on surface definition 13
AFLR2    : Nodes, Trias,Quads=        12        14         0
AFLR4    : Nodes, Trias,Quads=         8         6         0

AFLR4    : Generate optimal mesh on surface definition 14
AFLR2    : Nodes, Trias,Quads=        12        14         0
AFLR4    : Nodes, Trias,Quads=         8         6         0

AFLR4    : Generate optimal mesh on surface definition 15
AFLR2    : Nodes, Trias,Quads=        12        14         0
AFLR4    : Nodes, Trias,Quads=         8         6         0

AFLR4    : Generate optimal mesh on surface definition 16
AFLR2    : Nodes, Trias,Quads=        12        14         0
AFLR4    : Nodes, Trias,Quads=         8         6         0

DGEOM    : Add surface definitions to composite definition 0
DGEOM    : Glue composite surface definition 0
DGEOM    : Nodes,Faces,BEdges=      4015      8022      1158

AFLR4    : Curvature BG Surface Grid Generation

AFLR4    : Nodes, Faces      =      4015      8022

AFLR4    : Surface Grid Generation

AFLR4    : Generate optimal mesh on surface definition 1
AFLR2    : Nodes, Trias,Quads=       936      1754         0
AFLR4    : Nodes, Trias,Quads=       785      1452         0

AFLR4    : Generate optimal mesh on surface definition 2
AFLR2    : Nodes, Trias,Quads=      1193      2225         0
AFLR4    : Nodes, Trias,Quads=       985      1809         0

AFLR4    : Generate optimal mesh on surface definition 3
AFLR2    : Nodes, Trias,Quads=       937      1757         0
AFLR4    : Nodes, Trias,Quads=       756      1395         0

AFLR4    : Generate optimal mesh on surface definition 4
AFLR2    : Nodes, Trias,Quads=      1171      2182         0
AFLR4    : Nodes, Trias,Quads=       949      1738         0

AFLR4    : Generate optimal mesh on surface definition 5
AFLR2    : Nodes, Trias,Quads=        23        30         0
AFLR4    : Nodes, Trias,Quads=        14        12         0

AFLR4    : Generate optimal mesh on surface definition 6
AFLR2    : Nodes, Trias,Quads=       884      1650         0
AFLR4    : Nodes, Trias,Quads=       775      1432         0

AFLR4    : Generate optimal mesh on surface definition 7
AFLR2    : Nodes, Trias,Quads=      1186      2212         0
AFLR4    : Nodes, Trias,Quads=       970      1780         0

AFLR4    : Generate optimal mesh on surface definition 8
AFLR2    : Nodes, Trias,Quads=       884      1651         0
AFLR4    : Nodes, Trias,Quads=       765      1413         0

AFLR4    : Generate optimal mesh on surface definition 9
AFLR2    : Nodes, Trias,Quads=      1164      2169         0
AFLR4    : Nodes, Trias,Quads=       949      1739         0

AFLR4    : Generate optimal mesh on surface definition 10
AFLR2    : Nodes, Trias,Quads=        24        32         0
AFLR4    : Nodes, Trias,Quads=        14        12         0

AFLR4    : Generate optimal mesh on surface definition 11
AFLR2    : Nodes, Trias,Quads=        12        14         0
AFLR4    : Nodes, Trias,Quads=         8         6         0

AFLR4    : Generate optimal mesh on surface definition 12
AFLR2    : Nodes, Trias,Quads=        12        14         0
AFLR4    : Nodes, Trias,Quads=         8         6         0

AFLR4    : Generate optimal mesh on surface definition 13
AFLR2    : Nodes, Trias,Quads=        12        14         0
AFLR4    : Nodes, Trias,Quads=         8         6         0

AFLR4    : Generate optimal mesh on surface definition 14
AFLR2    : Nodes, Trias,Quads=        12        14         0
AFLR4    : Nodes, Trias,Quads=         8         6         0

AFLR4    : Generate optimal mesh on surface definition 15
AFLR2    : Nodes, Trias,Quads=        12        14         0
AFLR4    : Nodes, Trias,Quads=         8         6         0

AFLR4    : Generate optimal mesh on surface definition 16
AFLR2    : Nodes, Trias,Quads=        12        14         0
AFLR4    : Nodes, Trias,Quads=         8         6         0

DGEOM    : Add surface definitions to composite definition 0
DGEOM    : Glue composite surface definition 0
DGEOM    : Nodes,Faces,BEdges=      6413     12818      1170

OVERALL  : CPU Time          =     0.129   seconds
Body 1 (of 2)
Number of nodes    = 6393
Number of elements = 12782
Number of triangle elements      = 12782
Number of quadrilateral elements = 0
Body 2 (of 2)
Number of nodes    = 20
Number of elements = 36
Number of triangle elements      = 36
Number of quadrilateral elements = 0
----------------------------
Total number of nodes    = 6413
Total number of elements = 12818
Total number of triangle elements      = 12818
Total number of quadrilateral elements = 0

Getting mesh sizing parameters
	Mesh sizing name - Farfield
	Done getting mesh sizing parameters

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.8.1
EGADS    : ---------------------------------------

EGADS    : EGADS CAD Geometry Setup

EGADS    : Model has 2 Active Bodies

EGADS    : Body 0 is a SolidBody
EGADS    : Body 0 has 1 Shells
EGADS    : Body 0 has 10 Faces
EGADS    : Body 0 has 18 Edges
EGADS    : Body 0 has 10 Loops
EGADS    : Body 0 has 10 Nodes
EGADS    : Body 1 is a SolidBody
EGADS    : Body 1 has 1 Shells
EGADS    : Body 1 has 6 Faces
EGADS    : Body 1 has 12 Edges
EGADS    : Body 1 has 6 Loops
EGADS    : Body 1 has 8 Nodes

EGADS    : Check Grid BCs

EGADS    : Grid BCs are OK

EGADS    : Face Neighbor-Faces Information

EGADS    : QC  = Face Quad Combination Flag
EGADS    : IER = Face Isolated Edge Refinement Flag
EGADS    : ER  = Face Edge Refinement Factor
EGADS    :       Not applicable for Faces with a FarField Grid BC.
EGADS    : SF  = Face Scale Factor
EGADS    :       Not applicable for Faces with a FarField Grid BC.

EGADS    :   Face          Body    QC   IER       ER    Scale   Neighbor
EGADS    :     ID  Active    ID  Flag  Flag   Weight   Factor   Faces
EGADS    :      1     Yes     0     0     1        0        1   2 3 6
EGADS    :      2     Yes     0     0     1        0        1   1 4 5
EGADS    :      3     Yes     0     0     1        0        1   1 4 8
EGADS    :      4     Yes     0     0     1        0        1   2 3 5
EGADS    :      5     Yes     0     0     1        0        1   2 4
EGADS    :      6     Yes     0     0     1        0        1   1 7 8
EGADS    :      7     Yes     0     0     1        0        1   6 9 10
EGADS    :      8     Yes     0     0     1        0        1   3 6 9
EGADS    :      9     Yes     0     0     1        0        1   7 8 10
EGADS    :     10     Yes     0     0     1        0        1   7 9
EGADS    :     11     Yes     1     0     1       NA       NA   13 14 15 16
EGADS    :     12     Yes     1     0     1       NA       NA   13 14 15 16
EGADS    :     13     Yes     1     0     1       NA       NA   11 12 15 16
EGADS    :     14     Yes     1     0     1       NA       NA   11 12 15 16
EGADS    :     15     Yes     1     0     1       NA       NA   11 12 13 14
EGADS    :     16     Yes     1     0     1       NA       NA   11 12 13 14

EGADS    : Face Edges Information

EGADS    :   Face   Edges
EGADS    :      1   -1 2 3 -4
EGADS    :      2   -5 4 6 -7
EGADS    :      3   -3 8 1 -9
EGADS    :      4   -6 9 5 -10
EGADS    :      5   7 10
EGADS    :      6   11 13 -12 -2
EGADS    :      7   14 16 -15 -13
EGADS    :      8   12 17 -11 -8
EGADS    :      9   15 18 -14 -17
EGADS    :     10   -16 -18
EGADS    :     11   19 20 -21 -22
EGADS    :     12   -23 26 25 -24
EGADS    :     13   27 23 -28 -19
EGADS    :     14   -29 21 30 -25
EGADS    :     15   22 29 -26 -27
EGADS    :     16   -20 28 24 -30

EGADS    : Face Loops Information

EGADS    :   Face   Loops
EGADS    :      1   1
EGADS    :      2   2
EGADS    :      3   3
EGADS    :      4   4
EGADS    :      5   5
EGADS    :      6   6
EGADS    :      7   7
EGADS    :      8   8
EGADS    :      9   9
EGADS    :     10   10
EGADS    :     11   11
EGADS    :     12   12
EGADS    :     13   13
EGADS    :     14   14
EGADS    :     15   15
EGADS    :     16   16

EGADS    : Loop Edges Information

EGADS    :   Loop  Active   Edges
EGADS    :      1     Yes   -1 2 3 -4
EGADS    :      2     Yes   -5 4 6 -7
EGADS    :      3     Yes   -3 8 1 -9
EGADS    :      4     Yes   -6 9 5 -10
EGADS    :      5     Yes   7 10
EGADS    :      6     Yes   11 13 -12 -2
EGADS    :      7     Yes   14 16 -15 -13
EGADS    :      8     Yes   12 17 -11 -8
EGADS    :      9     Yes   15 18 -14 -17
EGADS    :     10     Yes   -16 -18
EGADS    :     11     Yes   19 20 -21 -22
EGADS    :     12     Yes   -23 26 25 -24
EGADS    :     13     Yes   27 23 -28 -19
EGADS    :     14     Yes   -29 21 30 -25
EGADS    :     15     Yes   22 29 -26 -27
EGADS    :     16     Yes   -20 28 24 -30

EGADS    : Edge Node, Scale Factor, and Neighbor-Faces Information

EGADS    : ESF = Edge Scale Factor
EGADS    :       Not applicable for DEGENERATE Edges or Edges with a FarField
EGADS    :       Grid BC Neighbor Face.

EGADS    :                                             Neighbor
EGADS    :   Edge  Body  Active Node1 Node2      ESF   Faces
EGADS    :      1     0     Yes     1     2        1   1 3
EGADS    :      2     0     Yes     1     3        1   1 6
EGADS    :      3     0     Yes     3     4        1   1 3
EGADS    :      4     0     Yes     2     4        1   1 2
EGADS    :      5     0     Yes     2     5        1   2 4
EGADS    :      6     0     Yes     4     6        1   2 4
EGADS    :      7     0     Yes     5     6        1   2 5
EGADS    :      8     0     Yes     3     1        1   3 8
EGADS    :      9     0     Yes     4     2        1   3 4
EGADS    :     10     0     Yes     6     5        1   4 5
EGADS    :     11     0     Yes     1     7        1   6 8
EGADS    :     12     0     Yes     3     8        1   6 8
EGADS    :     13     0     Yes     7     8        1   6 7
EGADS    :     14     0     Yes     7     9        1   7 9
EGADS    :     15     0     Yes     8    10        1   7 9
EGADS    :     16     0     Yes     9    10        1   7 10
EGADS    :     17     0     Yes     8     7        1   8 9
EGADS    :     18     0     Yes    10     9        1   9 10
EGADS    :     19     1     Yes    12    11       NA   11 13
EGADS    :     20     1     Yes    11    13       NA   11 16
EGADS    :     21     1     Yes    14    13       NA   11 14
EGADS    :     22     1     Yes    12    14       NA   11 15
EGADS    :     23     1     Yes    16    15       NA   12 13
EGADS    :     24     1     Yes    15    17       NA   12 16
EGADS    :     25     1     Yes    18    17       NA   12 14
EGADS    :     26     1     Yes    16    18       NA   12 15
EGADS    :     27     1     Yes    12    16       NA   13 15
EGADS    :     28     1     Yes    11    15       NA   13 16
EGADS    :     29     1     Yes    14    18       NA   14 15
EGADS    :     30     1     Yes    13    17       NA   14 16

EGADS    : Node Information

EGADS    :   Node  Active      Coordinates
EGADS    :      1     Yes       97.2007855                0                0
EGADS    :      2     Yes       97.9335611                0                0
EGADS    :      3     Yes               50                0                0
EGADS    :      4     Yes       75.3047874                0                0
EGADS    :      5     Yes       123.552357                0        4.7180639
EGADS    :      6     Yes       118.391317                0       3.99272703
EGADS    :      7     Yes       97.9335611       36.1389817                0
EGADS    :      8     Yes       75.3047874       36.1389817                0
EGADS    :      9     Yes       123.552357       97.6729236        4.7180639
EGADS    :     10     Yes       118.391317       97.6729236       3.99272703
EGADS    :     11     Yes                0                0       1951.57774
EGADS    :     12     Yes                0                0                0
EGADS    :     13     Yes                0       1953.45847       1951.57774
EGADS    :     14     Yes                0       1953.45847                0
EGADS    :     15     Yes       2040.21562                0       1951.57774
EGADS    :     16     Yes       2040.21562                0                0
EGADS    :     17     Yes       2040.21562       1953.45847       1951.57774
EGADS    :     18     Yes       2040.21562       1953.45847                0

EGADS    : Face and Edge Match Information

EGADS    : No Face Matches Found

AFLR4    : Surface Mesh Spacing Setup

AFLR4    : Max Bounding Box Length     = 3906.92
AFLR4    : Min Bounding Box Length     = 3906.92
AFLR4    : Max Ref Bounding Box Length = 195.346
AFLR4    : Min Ref Bounding Box Length = 13.1976
AFLR4    : Reference Length            = 21.7051
AFLR4    : BL Thickness                = 0
AFLR4    : FarField Spacing            = 4773.42
AFLR4    : Abs Min Surf Spacing        = 0.0217051
AFLR4    : Min Surf Spacing            = 0.217051
AFLR4    : Max Surf Spacing            = 2.17051
AFLR4    : Global Scale Factor         = 9

AFLR4    : Geometry Definition Information

AFLR4    : Definition              Definition   Composite             Grid BC
AFLR4    :         ID                    Type          ID                Type
AFLR4    :          0     glue-only composite           -                   -
AFLR4    :          1            CAD geometry           0            STD w/BL
AFLR4    :          2            CAD geometry           0            STD w/BL
AFLR4    :          3            CAD geometry           0            STD w/BL
AFLR4    :          4            CAD geometry           0            STD w/BL
AFLR4    :          5            CAD geometry           0            STD w/BL
AFLR4    :          6            CAD geometry           0            STD w/BL
AFLR4    :          7            CAD geometry           0            STD w/BL
AFLR4    :          8            CAD geometry           0            STD w/BL
AFLR4    :          9            CAD geometry           0            STD w/BL
AFLR4    :         10            CAD geometry           0            STD w/BL
AFLR4    :         11            CAD geometry           0            FARFIELD
AFLR4    :         12            CAD geometry           0            FARFIELD
AFLR4    :         13            CAD geometry           0            FARFIELD
AFLR4    :         14            CAD geometry           0            FARFIELD
AFLR4    :         15            CAD geometry           0            FARFIELD
AFLR4    :         16            CAD geometry           0            FARFIELD

AFLR4    : Define CAD surface definition 1
AFLR4    : Define CAD surface definition 2
AFLR4    : Define CAD surface definition 3
AFLR4    : Define CAD surface definition 4
AFLR4    : Define CAD surface definition 5
AFLR4    : Define CAD surface definition 6
AFLR4    : Define CAD surface definition 7
AFLR4    : Define CAD surface definition 8
AFLR4    : Define CAD surface definition 9
AFLR4    : Define CAD surface definition 10
AFLR4    : Define CAD surface definition 11
AFLR4    : Define CAD surface definition 12
AFLR4    : Define CAD surface definition 13
AFLR4    : Define CAD surface definition 14
AFLR4    : Define CAD surface definition 15
AFLR4    : Define CAD surface definition 16

AFLR4    : Surface Grid Generation

AFLR4    : Generate optimal mesh on surface definition 1
AFLR2    : Nodes, Trias,Quads=       193       334         0
AFLR4    : Nodes, Trias,Quads=       166       280         0

AFLR4    : Generate optimal mesh on surface definition 2
AFLR2    : Nodes, Trias,Quads=       259       452         0
AFLR4    : Nodes, Trias,Quads=       152       238         0

AFLR4    : Generate optimal mesh on surface definition 3
AFLR2    : Nodes, Trias,Quads=       188       325         0
AFLR4    : Nodes, Trias,Quads=       150       249         0

AFLR4    : Generate optimal mesh on surface definition 4
AFLR2    : Nodes, Trias,Quads=       245       424         0
AFLR4    : Nodes, Trias,Quads=       151       236         0

AFLR4    : Generate optimal mesh on surface definition 5
AFLR2    : Nodes, Trias,Quads=         5         4         0
AFLR4    : Nodes, Trias,Quads=         4         2         0

AFLR4    : Generate optimal mesh on surface definition 6
AFLR2    : Nodes, Trias,Quads=       195       338         0
AFLR4    : Nodes, Trias,Quads=       166       280         0

AFLR4    : Generate optimal mesh on surface definition 7
AFLR2    : Nodes, Trias,Quads=       258       450         0
AFLR4    : Nodes, Trias,Quads=       150       234         0

AFLR4    : Generate optimal mesh on surface definition 8
AFLR2    : Nodes, Trias,Quads=       188       325         0
AFLR4    : Nodes, Trias,Quads=       151       251         0

AFLR4    : Generate optimal mesh on surface definition 9
AFLR2    : Nodes, Trias,Quads=       244       422         0
AFLR4    : Nodes, Trias,Quads=       150       234         0

AFLR4    : Generate optimal mesh on surface definition 10
AFLR2    : Nodes, Trias,Quads=         5         4         0
AFLR4    : Nodes, Trias,Quads=         4         2         0

AFLR4    : Generate optimal mesh on surface definition 11
AFLR2    : Nodes, Trias,Quads=         5         4         0
AFLR4    : Nodes, Trias,Quads=         4         2         0

AFLR4    : Generate optimal mesh on surface definition 12
AFLR2    : Nodes, Trias,Quads=         5         4         0
AFLR4    : Nodes, Trias,Quads=         4         2         0

AFLR4    : Generate optimal mesh on surface definition 13
AFLR2    : Nodes, Trias,Quads=         5         4         0
AFLR4    : Nodes, Trias,Quads=         4         2         0

AFLR4    : Generate optimal mesh on surface definition 14
AFLR2    : Nodes, Trias,Quads=         5         4         0
AFLR4    : Nodes, Trias,Quads=         4         2         0

AFLR4    : Generate optimal mesh on surface definition 15
AFLR2    : Nodes, Trias,Quads=         5         4         0
AFLR4    : Nodes, Trias,Quads=         4         2         0

AFLR4    : Generate optimal mesh on surface definition 16
AFLR2    : Nodes, Trias,Quads=         5         4         0
AFLR4    : Nodes, Trias,Quads=         4         2         0

DGEOM    : Add surface definitions to composite definition 0
DGEOM    : Glue composite surface definition 0
DGEOM    : Nodes,Faces,BEdges=      1013      2018       486

AFLR4    : Curvature BG Surface Grid Generation

AFLR4    : Nodes, Faces      =      1013      2018

AFLR4    : Surface Grid Generation

AFLR4    : Generate optimal mesh on surface definition 1
AFLR2    : Nodes, Trias,Quads=       208       362         0
AFLR4    : Nodes, Trias,Quads=       203       352         0

AFLR4    : Generate optimal mesh on surface definition 2
AFLR2    : Nodes, Trias,Quads=       242       420         0
AFLR4    : Nodes, Trias,Quads=       185       306         0

AFLR4    : Generate optimal mesh on surface definition 3
AFLR2    : Nodes, Trias,Quads=       203       353         0
AFLR4    : Nodes, Trias,Quads=       190       327         0

AFLR4    : Generate optimal mesh on surface definition 4
AFLR2    : Nodes, Trias,Quads=       243       422         0
AFLR4    : Nodes, Trias,Quads=       182       300         0

AFLR4    : Generate optimal mesh on surface definition 5
AFLR2    : Nodes, Trias,Quads=         5         4         0
AFLR4    : Nodes, Trias,Quads=         4         2         0

AFLR4    : Generate optimal mesh on surface definition 6
AFLR2    : Nodes, Trias,Quads=       209       364         0
AFLR4    : Nodes, Trias,Quads=       200       346         0

AFLR4    : Generate optimal mesh on surface definition 7
AFLR2    : Nodes, Trias,Quads=       246       427         0
AFLR4    : Nodes, Trias,Quads=       185       305         0

AFLR4    : Generate optimal mesh on surface definition 8
AFLR2    : Nodes, Trias,Quads=       207       361         0
AFLR4    : Nodes, Trias,Quads=       195       337         0

AFLR4    : Generate optimal mesh on surface definition 9
AFLR2    : Nodes, Trias,Quads=       248       431         0
AFLR4    : Nodes, Trias,Quads=       188       311         0

AFLR4    : Generate optimal mesh on surface definition 10
AFLR2    : Nodes, Trias,Quads=         5         4         0
AFLR4    : Nodes, Trias,Quads=         4         2         0

AFLR4    : Generate optimal mesh on surface definition 11
AFLR2    : Nodes, Trias,Quads=        12        14         0
AFLR4    : Nodes, Trias,Quads=         8         6         0

AFLR4    : Generate optimal mesh on surface definition 12
AFLR2    : Nodes, Trias,Quads=        12        14         0
AFLR4    : Nodes, Trias,Quads=         8         6         0

AFLR4    : Generate optimal mesh on surface definition 13
AFLR2    : Nodes, Trias,Quads=        12        14         0
AFLR4    : Nodes, Trias,Quads=         8         6         0

AFLR4    : Generate optimal mesh on surface definition 14
AFLR2    : Nodes, Trias,Quads=        12        14         0
AFLR4    : Nodes, Trias,Quads=         8         6         0

AFLR4    : Generate optimal mesh on surface definition 15
AFLR2    : Nodes, Trias,Quads=        12        14         0
AFLR4    : Nodes, Trias,Quads=         8         6         0

AFLR4    : Generate optimal mesh on surface definition 16
AFLR2    : Nodes, Trias,Quads=        12        14         0
AFLR4    : Nodes, Trias,Quads=         8         6         0

DGEOM    : Add surface definitions to composite definition 0
DGEOM    : Glue composite surface definition 0
DGEOM    : Nodes,Faces,BEdges=      1316      2624       512

OVERALL  : CPU Time          =     0.067   seconds
Body 1 (of 2)
Number of nodes    = 1296
Number of elements = 2588
Number of triangle elements      = 2588
Number of quadrilateral elements = 0
Body 2 (of 2)
Number of nodes    = 20
Number of elements = 36
Number of triangle elements      = 36
Number of quadrilateral elements = 0
----------------------------
Total number of nodes    = 1316
Total number of elements = 2624
Total number of triangle elements      = 2624
Total number of quadrilateral elements = 0

real	0m1.833s
user	0m1.635s
sys	0m0.469s
+ status=0
+ set +x

=================================================
data/session07/03_aflr4_MeshLength.py passed (as expected)
=================================================


=================================================
04_aflr4_EdgeWeight.py test;
+ python 04_aflr4_EdgeWeight.py
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/CAPS/training/2023/training.log

MESSAGE:: Building wingOml

Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 2
	Name = Wing, index = 1
	Name = Farfield, index = 2
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 3
	Name = leftWing, index = 1
	Name = riteWing, index = 2
	Name = Farfield, index = 3

Getting mesh sizing parameters
	Mesh sizing name - Farfield
	Mesh sizing name - leftWing
	Done getting mesh sizing parameters
 
AFLR2    : ---------------------------------------
AFLR2    : AFLR2 LIBRARY
AFLR2    : ADVANCING-FRONT/LOCAL-RECONNECTION
AFLR2    : TRIA/QUAD GRID GENERATOR
AFLR2    : Version Number 9.18.1
AFLR2    : Version Date   06/11/24 @ 05:52PM
AFLR2    : Compile OS     Darwin 23.5.0 arm64
AFLR2    : Compile Date   06/11/24 @ 05:52PM
AFLR2    : Copyright 1994-2021, D.L. Marcum
AFLR2    : ---------------------------------------
 
AFLR4    : ---------------------------------------
AFLR4    : AFLR4 LIBRARY
AFLR4    : ADVANCING-FRONT/LOCAL-RECONNECTION
AFLR4    : TRIA/QUAD SURFACE GRID GENERATOR
AFLR4    : Version Number 11.5.15
AFLR4    : Version Date   07/19/24 @ 07:04PM
AFLR4    : Compile OS     Darwin 23.5.0 arm64
AFLR4    : Compile Date   07/19/24 @ 07:06PM
AFLR4    : Copyright 1994-2021, D.L. Marcum
AFLR4    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.8.1
EGADS    : ---------------------------------------

EGADS    : EGADS CAD Geometry Setup

EGADS    : Model has 2 Active Bodies

EGADS    : Body 0 is a SolidBody
EGADS    : Body 0 has 1 Shells
EGADS    : Body 0 has 10 Faces
EGADS    : Body 0 has 18 Edges
EGADS    : Body 0 has 10 Loops
EGADS    : Body 0 has 10 Nodes
EGADS    : Body 1 is a SolidBody
EGADS    : Body 1 has 1 Shells
EGADS    : Body 1 has 6 Faces
EGADS    : Body 1 has 12 Edges
EGADS    : Body 1 has 6 Loops
EGADS    : Body 1 has 8 Nodes

EGADS    : Check Grid BCs

EGADS    : Grid BCs are OK

EGADS    : Face Neighbor-Faces Information

EGADS    : QC  = Face Quad Combination Flag
EGADS    : IER = Face Isolated Edge Refinement Flag
EGADS    : ER  = Face Edge Refinement Factor
EGADS    :       Not applicable for Faces with a FarField Grid BC.
EGADS    : SF  = Face Scale Factor
EGADS    :       Not applicable for Faces with a FarField Grid BC.

EGADS    :   Face          Body    QC   IER       ER    Scale   Neighbor
EGADS    :     ID  Active    ID  Flag  Flag   Weight   Factor   Faces
EGADS    :      1     Yes     0     0     1        1        1   2 3 6
EGADS    :      2     Yes     0     0     1        1        1   1 4 5
EGADS    :      3     Yes     0     0     1        1        1   1 4 8
EGADS    :      4     Yes     0     0     1        1        1   2 3 5
EGADS    :      5     Yes     0     0     1        1        1   2 4
EGADS    :      6     Yes     0     0     1        0        1   1 7 8
EGADS    :      7     Yes     0     0     1        0        1   6 9 10
EGADS    :      8     Yes     0     0     1        0        1   3 6 9
EGADS    :      9     Yes     0     0     1        0        1   7 8 10
EGADS    :     10     Yes     0     0     1        0        1   7 9
EGADS    :     11     Yes     1     0     1       NA       NA   13 14 15 16
EGADS    :     12     Yes     1     0     1       NA       NA   13 14 15 16
EGADS    :     13     Yes     1     0     1       NA       NA   11 12 15 16
EGADS    :     14     Yes     1     0     1       NA       NA   11 12 15 16
EGADS    :     15     Yes     1     0     1       NA       NA   11 12 13 14
EGADS    :     16     Yes     1     0     1       NA       NA   11 12 13 14

EGADS    : Face Edges Information

EGADS    :   Face   Edges
EGADS    :      1   -1 2 3 -4
EGADS    :      2   -5 4 6 -7
EGADS    :      3   -3 8 1 -9
EGADS    :      4   -6 9 5 -10
EGADS    :      5   7 10
EGADS    :      6   11 13 -12 -2
EGADS    :      7   14 16 -15 -13
EGADS    :      8   12 17 -11 -8
EGADS    :      9   15 18 -14 -17
EGADS    :     10   -16 -18
EGADS    :     11   19 20 -21 -22
EGADS    :     12   -23 26 25 -24
EGADS    :     13   27 23 -28 -19
EGADS    :     14   -29 21 30 -25
EGADS    :     15   22 29 -26 -27
EGADS    :     16   -20 28 24 -30

EGADS    : Face Loops Information

EGADS    :   Face   Loops
EGADS    :      1   1
EGADS    :      2   2
EGADS    :      3   3
EGADS    :      4   4
EGADS    :      5   5
EGADS    :      6   6
EGADS    :      7   7
EGADS    :      8   8
EGADS    :      9   9
EGADS    :     10   10
EGADS    :     11   11
EGADS    :     12   12
EGADS    :     13   13
EGADS    :     14   14
EGADS    :     15   15
EGADS    :     16   16

EGADS    : Loop Edges Information

EGADS    :   Loop  Active   Edges
EGADS    :      1     Yes   -1 2 3 -4
EGADS    :      2     Yes   -5 4 6 -7
EGADS    :      3     Yes   -3 8 1 -9
EGADS    :      4     Yes   -6 9 5 -10
EGADS    :      5     Yes   7 10
EGADS    :      6     Yes   11 13 -12 -2
EGADS    :      7     Yes   14 16 -15 -13
EGADS    :      8     Yes   12 17 -11 -8
EGADS    :      9     Yes   15 18 -14 -17
EGADS    :     10     Yes   -16 -18
EGADS    :     11     Yes   19 20 -21 -22
EGADS    :     12     Yes   -23 26 25 -24
EGADS    :     13     Yes   27 23 -28 -19
EGADS    :     14     Yes   -29 21 30 -25
EGADS    :     15     Yes   22 29 -26 -27
EGADS    :     16     Yes   -20 28 24 -30

EGADS    : Edge Node, Scale Factor, and Neighbor-Faces Information

EGADS    : ESF = Edge Scale Factor
EGADS    :       Not applicable for DEGENERATE Edges or Edges with a FarField
EGADS    :       Grid BC Neighbor Face.

EGADS    :                                             Neighbor
EGADS    :   Edge  Body  Active Node1 Node2      ESF   Faces
EGADS    :      1     0     Yes     1     2        1   1 3
EGADS    :      2     0     Yes     1     3        1   1 6
EGADS    :      3     0     Yes     3     4        1   1 3
EGADS    :      4     0     Yes     2     4        1   1 2
EGADS    :      5     0     Yes     2     5        1   2 4
EGADS    :      6     0     Yes     4     6        1   2 4
EGADS    :      7     0     Yes     5     6        1   2 5
EGADS    :      8     0     Yes     3     1        1   3 8
EGADS    :      9     0     Yes     4     2        1   3 4
EGADS    :     10     0     Yes     6     5        1   4 5
EGADS    :     11     0     Yes     1     7        1   6 8
EGADS    :     12     0     Yes     3     8        1   6 8
EGADS    :     13     0     Yes     7     8        1   6 7
EGADS    :     14     0     Yes     7     9        1   7 9
EGADS    :     15     0     Yes     8    10        1   7 9
EGADS    :     16     0     Yes     9    10        1   7 10
EGADS    :     17     0     Yes     8     7        1   8 9
EGADS    :     18     0     Yes    10     9        1   9 10
EGADS    :     19     1     Yes    12    11       NA   11 13
EGADS    :     20     1     Yes    11    13       NA   11 16
EGADS    :     21     1     Yes    14    13       NA   11 14
EGADS    :     22     1     Yes    12    14       NA   11 15
EGADS    :     23     1     Yes    16    15       NA   12 13
EGADS    :     24     1     Yes    15    17       NA   12 16
EGADS    :     25     1     Yes    18    17       NA   12 14
EGADS    :     26     1     Yes    16    18       NA   12 15
EGADS    :     27     1     Yes    12    16       NA   13 15
EGADS    :     28     1     Yes    11    15       NA   13 16
EGADS    :     29     1     Yes    14    18       NA   14 15
EGADS    :     30     1     Yes    13    17       NA   14 16

EGADS    : Node Information

EGADS    :   Node  Active      Coordinates
EGADS    :      1     Yes       97.2007855                0                0
EGADS    :      2     Yes       97.9335611                0                0
EGADS    :      3     Yes               50                0                0
EGADS    :      4     Yes       75.3047874                0                0
EGADS    :      5     Yes       123.552357                0        4.7180639
EGADS    :      6     Yes       118.391317                0       3.99272703
EGADS    :      7     Yes       97.9335611       36.1389817                0
EGADS    :      8     Yes       75.3047874       36.1389817                0
EGADS    :      9     Yes       123.552357       97.6729236        4.7180639
EGADS    :     10     Yes       118.391317       97.6729236       3.99272703
EGADS    :     11     Yes                0                0       1951.57774
EGADS    :     12     Yes                0                0                0
EGADS    :     13     Yes                0       1953.45847       1951.57774
EGADS    :     14     Yes                0       1953.45847                0
EGADS    :     15     Yes       2040.21562                0       1951.57774
EGADS    :     16     Yes       2040.21562                0                0
EGADS    :     17     Yes       2040.21562       1953.45847       1951.57774
EGADS    :     18     Yes       2040.21562       1953.45847                0

EGADS    : Face and Edge Match Information

EGADS    : No Face Matches Found

AFLR4    : Surface Mesh Spacing Setup

AFLR4    : Max Bounding Box Length     = 3906.92
AFLR4    : Min Bounding Box Length     = 3906.92
AFLR4    : Max Ref Bounding Box Length = 195.346
AFLR4    : Min Ref Bounding Box Length = 13.1976
AFLR4    : Reference Length            = 21.7051
AFLR4    : BL Thickness                = 0
AFLR4    : FarField Spacing            = 2651.51
AFLR4    : Abs Min Surf Spacing        = 0.0542627
AFLR4    : Min Surf Spacing            = 0.108525
AFLR4    : Max Surf Spacing            = 2.17051
AFLR4    : Global Scale Factor         = 5

AFLR4    : Geometry Definition Information

AFLR4    : Definition              Definition   Composite             Grid BC
AFLR4    :         ID                    Type          ID                Type
AFLR4    :          0     glue-only composite           -                   -
AFLR4    :          1            CAD geometry           0            STD w/BL
AFLR4    :          2            CAD geometry           0            STD w/BL
AFLR4    :          3            CAD geometry           0            STD w/BL
AFLR4    :          4            CAD geometry           0            STD w/BL
AFLR4    :          5            CAD geometry           0            STD w/BL
AFLR4    :          6            CAD geometry           0            STD w/BL
AFLR4    :          7            CAD geometry           0            STD w/BL
AFLR4    :          8            CAD geometry           0            STD w/BL
AFLR4    :          9            CAD geometry           0            STD w/BL
AFLR4    :         10            CAD geometry           0            STD w/BL
AFLR4    :         11            CAD geometry           0            FARFIELD
AFLR4    :         12            CAD geometry           0            FARFIELD
AFLR4    :         13            CAD geometry           0            FARFIELD
AFLR4    :         14            CAD geometry           0            FARFIELD
AFLR4    :         15            CAD geometry           0            FARFIELD
AFLR4    :         16            CAD geometry           0            FARFIELD

AFLR4    : Define CAD surface definition 1
AFLR4    : Define CAD surface definition 2
AFLR4    : Define CAD surface definition 3
AFLR4    : Define CAD surface definition 4
AFLR4    : Define CAD surface definition 5
AFLR4    : Define CAD surface definition 6
AFLR4    : Define CAD surface definition 7
AFLR4    : Define CAD surface definition 8
AFLR4    : Define CAD surface definition 9
AFLR4    : Define CAD surface definition 10
AFLR4    : Define CAD surface definition 11
AFLR4    : Define CAD surface definition 12
AFLR4    : Define CAD surface definition 13
AFLR4    : Define CAD surface definition 14
AFLR4    : Define CAD surface definition 15
AFLR4    : Define CAD surface definition 16

AFLR4    : Surface Grid Generation

AFLR4    : Generate optimal mesh on surface definition 1
AFLR2    : Nodes, Trias,Quads=      1107      2082         0
AFLR4    : Nodes, Trias,Quads=       685      1238         0

AFLR4    : Generate optimal mesh on surface definition 2
AFLR2    : Nodes, Trias,Quads=      1473      2759         0
AFLR4    : Nodes, Trias,Quads=       721      1255         0

AFLR4    : Generate optimal mesh on surface definition 3
AFLR2    : Nodes, Trias,Quads=      1116      2100         0
AFLR4    : Nodes, Trias,Quads=       671      1210         0

AFLR4    : Generate optimal mesh on surface definition 4
AFLR2    : Nodes, Trias,Quads=      1458      2729         0
AFLR4    : Nodes, Trias,Quads=       714      1241         0

AFLR4    : Generate optimal mesh on surface definition 5
AFLR2    : Nodes, Trias,Quads=        20        24         0
AFLR4    : Nodes, Trias,Quads=        14        12         0

AFLR4    : Generate optimal mesh on surface definition 6
AFLR2    : Nodes, Trias,Quads=      1108      2084         0
AFLR4    : Nodes, Trias,Quads=       683      1234         0

AFLR4    : Generate optimal mesh on surface definition 7
AFLR2    : Nodes, Trias,Quads=      1488      2789         0
AFLR4    : Nodes, Trias,Quads=       714      1241         0

AFLR4    : Generate optimal mesh on surface definition 8
AFLR2    : Nodes, Trias,Quads=      1112      2092         0
AFLR4    : Nodes, Trias,Quads=       653      1174         0

AFLR4    : Generate optimal mesh on surface definition 9
AFLR2    : Nodes, Trias,Quads=      1456      2725         0
AFLR4    : Nodes, Trias,Quads=       708      1229         0

AFLR4    : Generate optimal mesh on surface definition 10
AFLR2    : Nodes, Trias,Quads=        20        24         0
AFLR4    : Nodes, Trias,Quads=        14        12         0

AFLR4    : Generate optimal mesh on surface definition 11
AFLR2    : Nodes, Trias,Quads=         5         4         0
AFLR4    : Nodes, Trias,Quads=         4         2         0

AFLR4    : Generate optimal mesh on surface definition 12
AFLR2    : Nodes, Trias,Quads=         5         4         0
AFLR4    : Nodes, Trias,Quads=         4         2         0

AFLR4    : Generate optimal mesh on surface definition 13
AFLR2    : Nodes, Trias,Quads=         5         4         0
AFLR4    : Nodes, Trias,Quads=         4         2         0

AFLR4    : Generate optimal mesh on surface definition 14
AFLR2    : Nodes, Trias,Quads=         5         4         0
AFLR4    : Nodes, Trias,Quads=         4         2         0

AFLR4    : Generate optimal mesh on surface definition 15
AFLR2    : Nodes, Trias,Quads=         5         4         0
AFLR4    : Nodes, Trias,Quads=         4         2         0

AFLR4    : Generate optimal mesh on surface definition 16
AFLR2    : Nodes, Trias,Quads=         5         4         0
AFLR4    : Nodes, Trias,Quads=         4         2         0

DGEOM    : Add surface definitions to composite definition 0
DGEOM    : Glue composite surface definition 0
DGEOM    : Nodes,Faces,BEdges=      4933      9858      1312

AFLR4    : Curvature BG Surface Grid Generation

AFLR4    : Nodes, Faces      =      4933      9858

AFLR4    : Surface Grid Generation

AFLR4    : Generate optimal mesh on surface definition 1
AFLR2    : Nodes, Trias,Quads=     12796     24695         0
AFLR4    : Nodes, Trias,Quads=      7764     14631         0

AFLR4    : Generate optimal mesh on surface definition 2
AFLR2    : Nodes, Trias,Quads=     29251     57087         0
AFLR4    : Nodes, Trias,Quads=     12448     23481         0

AFLR4    : Generate optimal mesh on surface definition 3
AFLR2    : Nodes, Trias,Quads=     12136     23411         0
AFLR4    : Nodes, Trias,Quads=      7447     14033         0

AFLR4    : Generate optimal mesh on surface definition 4
AFLR2    : Nodes, Trias,Quads=     29424     57435         0
AFLR4    : Nodes, Trias,Quads=     12399     23385         0

AFLR4    : Generate optimal mesh on surface definition 5
AFLR2    : Nodes, Trias,Quads=       196       293         0
AFLR4    : Nodes, Trias,Quads=       188       277         0

AFLR4    : Generate optimal mesh on surface definition 6
AFLR2    : Nodes, Trias,Quads=      2367      4490         0
AFLR4    : Nodes, Trias,Quads=      1726      3208         0

AFLR4    : Generate optimal mesh on surface definition 7
AFLR2    : Nodes, Trias,Quads=      1453      2723         0
AFLR4    : Nodes, Trias,Quads=      1179      2175         0

AFLR4    : Generate optimal mesh on surface definition 8
AFLR2    : Nodes, Trias,Quads=      1738      3267         0
AFLR4    : Nodes, Trias,Quads=      1397      2585         0

AFLR4    : Generate optimal mesh on surface definition 9
AFLR2    : Nodes, Trias,Quads=      1477      2770         0
AFLR4    : Nodes, Trias,Quads=      1147      2110         0

AFLR4    : Generate optimal mesh on surface definition 10
AFLR2    : Nodes, Trias,Quads=        26        35         0
AFLR4    : Nodes, Trias,Quads=        15        13         0

AFLR4    : Generate optimal mesh on surface definition 11
AFLR2    : Nodes, Trias,Quads=        12        14         0
AFLR4    : Nodes, Trias,Quads=         8         6         0

AFLR4    : Generate optimal mesh on surface definition 12
AFLR2    : Nodes, Trias,Quads=        12        14         0
AFLR4    : Nodes, Trias,Quads=         8         6         0

AFLR4    : Generate optimal mesh on surface definition 13
AFLR2    : Nodes, Trias,Quads=        12        14         0
AFLR4    : Nodes, Trias,Quads=         8         6         0

AFLR4    : Generate optimal mesh on surface definition 14
AFLR2    : Nodes, Trias,Quads=        12        14         0
AFLR4    : Nodes, Trias,Quads=         8         6         0

AFLR4    : Generate optimal mesh on surface definition 15
AFLR2    : Nodes, Trias,Quads=        12        14         0
AFLR4    : Nodes, Trias,Quads=         8         6         0

AFLR4    : Generate optimal mesh on surface definition 16
AFLR2    : Nodes, Trias,Quads=        12        14         0
AFLR4    : Nodes, Trias,Quads=         8         6         0

DGEOM    : Add surface definitions to composite definition 0
DGEOM    : Glue composite surface definition 0
DGEOM    : Nodes,Faces,BEdges=     42971     85934      5550

OVERALL  : CPU Time          =     0.566   seconds
Body 1 (of 2)
Number of nodes    = 42951
Number of elements = 85898
Number of triangle elements      = 85898
Number of quadrilateral elements = 0
Body 2 (of 2)
Number of nodes    = 20
Number of elements = 36
Number of triangle elements      = 36
Number of quadrilateral elements = 0
----------------------------
Total number of nodes    = 42971
Total number of elements = 85934
Total number of triangle elements      = 85934
Total number of quadrilateral elements = 0

real	0m4.060s
user	0m3.884s
sys	0m0.447s
+ status=0
+ set +x

=================================================
data/session07/04_aflr4_EdgeWeight.py passed (as expected)
=================================================


=================================================
05_aflr4_ScaleFactor.py test;
+ python 05_aflr4_ScaleFactor.py
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/CAPS/training/2023/training.log

MESSAGE:: Building wingOml

Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 2
	Name = Wing, index = 1
	Name = Farfield, index = 2
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 3
	Name = leftWing, index = 1
	Name = riteWing, index = 2
	Name = Farfield, index = 3

Getting mesh sizing parameters
	Mesh sizing name - Farfield
	Mesh sizing name - leftWing
	Mesh sizing name - riteWing
	Done getting mesh sizing parameters
 
AFLR2    : ---------------------------------------
AFLR2    : AFLR2 LIBRARY
AFLR2    : ADVANCING-FRONT/LOCAL-RECONNECTION
AFLR2    : TRIA/QUAD GRID GENERATOR
AFLR2    : Version Number 9.18.1
AFLR2    : Version Date   06/11/24 @ 05:52PM
AFLR2    : Compile OS     Darwin 23.5.0 arm64
AFLR2    : Compile Date   06/11/24 @ 05:52PM
AFLR2    : Copyright 1994-2021, D.L. Marcum
AFLR2    : ---------------------------------------
 
AFLR4    : ---------------------------------------
AFLR4    : AFLR4 LIBRARY
AFLR4    : ADVANCING-FRONT/LOCAL-RECONNECTION
AFLR4    : TRIA/QUAD SURFACE GRID GENERATOR
AFLR4    : Version Number 11.5.15
AFLR4    : Version Date   07/19/24 @ 07:04PM
AFLR4    : Compile OS     Darwin 23.5.0 arm64
AFLR4    : Compile Date   07/19/24 @ 07:06PM
AFLR4    : Copyright 1994-2021, D.L. Marcum
AFLR4    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.8.1
EGADS    : ---------------------------------------

EGADS    : EGADS CAD Geometry Setup

EGADS    : Model has 2 Active Bodies

EGADS    : Body 0 is a SolidBody
EGADS    : Body 0 has 1 Shells
EGADS    : Body 0 has 10 Faces
EGADS    : Body 0 has 18 Edges
EGADS    : Body 0 has 10 Loops
EGADS    : Body 0 has 10 Nodes
EGADS    : Body 1 is a SolidBody
EGADS    : Body 1 has 1 Shells
EGADS    : Body 1 has 6 Faces
EGADS    : Body 1 has 12 Edges
EGADS    : Body 1 has 6 Loops
EGADS    : Body 1 has 8 Nodes

EGADS    : Check Grid BCs

EGADS    : Grid BCs are OK

EGADS    : Face Neighbor-Faces Information

EGADS    : QC  = Face Quad Combination Flag
EGADS    : IER = Face Isolated Edge Refinement Flag
EGADS    : ER  = Face Edge Refinement Factor
EGADS    :       Not applicable for Faces with a FarField Grid BC.
EGADS    : SF  = Face Scale Factor
EGADS    :       Not applicable for Faces with a FarField Grid BC.

EGADS    :   Face          Body    QC   IER       ER    Scale   Neighbor
EGADS    :     ID  Active    ID  Flag  Flag   Weight   Factor   Faces
EGADS    :      1     Yes     0     0     1        0      0.5   2 3 6
EGADS    :      2     Yes     0     0     1        0      0.5   1 4 5
EGADS    :      3     Yes     0     0     1        0      0.5   1 4 8
EGADS    :      4     Yes     0     0     1        0      0.5   2 3 5
EGADS    :      5     Yes     0     0     1        0      0.5   2 4
EGADS    :      6     Yes     0     0     1        0        2   1 7 8
EGADS    :      7     Yes     0     0     1        0        2   6 9 10
EGADS    :      8     Yes     0     0     1        0        2   3 6 9
EGADS    :      9     Yes     0     0     1        0        2   7 8 10
EGADS    :     10     Yes     0     0     1        0        2   7 9
EGADS    :     11     Yes     1     0     1       NA       NA   13 14 15 16
EGADS    :     12     Yes     1     0     1       NA       NA   13 14 15 16
EGADS    :     13     Yes     1     0     1       NA       NA   11 12 15 16
EGADS    :     14     Yes     1     0     1       NA       NA   11 12 15 16
EGADS    :     15     Yes     1     0     1       NA       NA   11 12 13 14
EGADS    :     16     Yes     1     0     1       NA       NA   11 12 13 14

EGADS    : Face Edges Information

EGADS    :   Face   Edges
EGADS    :      1   -1 2 3 -4
EGADS    :      2   -5 4 6 -7
EGADS    :      3   -3 8 1 -9
EGADS    :      4   -6 9 5 -10
EGADS    :      5   7 10
EGADS    :      6   11 13 -12 -2
EGADS    :      7   14 16 -15 -13
EGADS    :      8   12 17 -11 -8
EGADS    :      9   15 18 -14 -17
EGADS    :     10   -16 -18
EGADS    :     11   19 20 -21 -22
EGADS    :     12   -23 26 25 -24
EGADS    :     13   27 23 -28 -19
EGADS    :     14   -29 21 30 -25
EGADS    :     15   22 29 -26 -27
EGADS    :     16   -20 28 24 -30

EGADS    : Face Loops Information

EGADS    :   Face   Loops
EGADS    :      1   1
EGADS    :      2   2
EGADS    :      3   3
EGADS    :      4   4
EGADS    :      5   5
EGADS    :      6   6
EGADS    :      7   7
EGADS    :      8   8
EGADS    :      9   9
EGADS    :     10   10
EGADS    :     11   11
EGADS    :     12   12
EGADS    :     13   13
EGADS    :     14   14
EGADS    :     15   15
EGADS    :     16   16

EGADS    : Loop Edges Information

EGADS    :   Loop  Active   Edges
EGADS    :      1     Yes   -1 2 3 -4
EGADS    :      2     Yes   -5 4 6 -7
EGADS    :      3     Yes   -3 8 1 -9
EGADS    :      4     Yes   -6 9 5 -10
EGADS    :      5     Yes   7 10
EGADS    :      6     Yes   11 13 -12 -2
EGADS    :      7     Yes   14 16 -15 -13
EGADS    :      8     Yes   12 17 -11 -8
EGADS    :      9     Yes   15 18 -14 -17
EGADS    :     10     Yes   -16 -18
EGADS    :     11     Yes   19 20 -21 -22
EGADS    :     12     Yes   -23 26 25 -24
EGADS    :     13     Yes   27 23 -28 -19
EGADS    :     14     Yes   -29 21 30 -25
EGADS    :     15     Yes   22 29 -26 -27
EGADS    :     16     Yes   -20 28 24 -30

EGADS    : Edge Node, Scale Factor, and Neighbor-Faces Information

EGADS    : ESF = Edge Scale Factor
EGADS    :       Not applicable for DEGENERATE Edges or Edges with a FarField
EGADS    :       Grid BC Neighbor Face.

EGADS    :                                             Neighbor
EGADS    :   Edge  Body  Active Node1 Node2      ESF   Faces
EGADS    :      1     0     Yes     1     2        1   1 3
EGADS    :      2     0     Yes     1     3        1   1 6
EGADS    :      3     0     Yes     3     4        1   1 3
EGADS    :      4     0     Yes     2     4        1   1 2
EGADS    :      5     0     Yes     2     5        1   2 4
EGADS    :      6     0     Yes     4     6        1   2 4
EGADS    :      7     0     Yes     5     6        1   2 5
EGADS    :      8     0     Yes     3     1        1   3 8
EGADS    :      9     0     Yes     4     2        1   3 4
EGADS    :     10     0     Yes     6     5        1   4 5
EGADS    :     11     0     Yes     1     7        1   6 8
EGADS    :     12     0     Yes     3     8        1   6 8
EGADS    :     13     0     Yes     7     8        1   6 7
EGADS    :     14     0     Yes     7     9        1   7 9
EGADS    :     15     0     Yes     8    10        1   7 9
EGADS    :     16     0     Yes     9    10        1   7 10
EGADS    :     17     0     Yes     8     7        1   8 9
EGADS    :     18     0     Yes    10     9        1   9 10
EGADS    :     19     1     Yes    12    11       NA   11 13
EGADS    :     20     1     Yes    11    13       NA   11 16
EGADS    :     21     1     Yes    14    13       NA   11 14
EGADS    :     22     1     Yes    12    14       NA   11 15
EGADS    :     23     1     Yes    16    15       NA   12 13
EGADS    :     24     1     Yes    15    17       NA   12 16
EGADS    :     25     1     Yes    18    17       NA   12 14
EGADS    :     26     1     Yes    16    18       NA   12 15
EGADS    :     27     1     Yes    12    16       NA   13 15
EGADS    :     28     1     Yes    11    15       NA   13 16
EGADS    :     29     1     Yes    14    18       NA   14 15
EGADS    :     30     1     Yes    13    17       NA   14 16

EGADS    : Node Information

EGADS    :   Node  Active      Coordinates
EGADS    :      1     Yes       97.2007855                0                0
EGADS    :      2     Yes       97.9335611                0                0
EGADS    :      3     Yes               50                0                0
EGADS    :      4     Yes       75.3047874                0                0
EGADS    :      5     Yes       123.552357                0        4.7180639
EGADS    :      6     Yes       118.391317                0       3.99272703
EGADS    :      7     Yes       97.9335611       36.1389817                0
EGADS    :      8     Yes       75.3047874       36.1389817                0
EGADS    :      9     Yes       123.552357       97.6729236        4.7180639
EGADS    :     10     Yes       118.391317       97.6729236       3.99272703
EGADS    :     11     Yes                0                0       1951.57774
EGADS    :     12     Yes                0                0                0
EGADS    :     13     Yes                0       1953.45847       1951.57774
EGADS    :     14     Yes                0       1953.45847                0
EGADS    :     15     Yes       2040.21562                0       1951.57774
EGADS    :     16     Yes       2040.21562                0                0
EGADS    :     17     Yes       2040.21562       1953.45847       1951.57774
EGADS    :     18     Yes       2040.21562       1953.45847                0

EGADS    : Face and Edge Match Information

EGADS    : No Face Matches Found

AFLR4    : Surface Mesh Spacing Setup

AFLR4    : Max Bounding Box Length     = 3906.92
AFLR4    : Min Bounding Box Length     = 3906.92
AFLR4    : Max Ref Bounding Box Length = 195.346
AFLR4    : Min Ref Bounding Box Length = 13.1976
AFLR4    : Reference Length            = 21.7051
AFLR4    : BL Thickness                = 0
AFLR4    : FarField Spacing            = 2651.51
AFLR4    : Abs Min Surf Spacing        = 0.0542627
AFLR4    : Min Surf Spacing            = 0.108525
AFLR4    : Max Surf Spacing            = 2.17051
AFLR4    : Global Scale Factor         = 5

AFLR4    : Geometry Definition Information

AFLR4    : Definition              Definition   Composite             Grid BC
AFLR4    :         ID                    Type          ID                Type
AFLR4    :          0     glue-only composite           -                   -
AFLR4    :          1            CAD geometry           0            STD w/BL
AFLR4    :          2            CAD geometry           0            STD w/BL
AFLR4    :          3            CAD geometry           0            STD w/BL
AFLR4    :          4            CAD geometry           0            STD w/BL
AFLR4    :          5            CAD geometry           0            STD w/BL
AFLR4    :          6            CAD geometry           0            STD w/BL
AFLR4    :          7            CAD geometry           0            STD w/BL
AFLR4    :          8            CAD geometry           0            STD w/BL
AFLR4    :          9            CAD geometry           0            STD w/BL
AFLR4    :         10            CAD geometry           0            STD w/BL
AFLR4    :         11            CAD geometry           0            FARFIELD
AFLR4    :         12            CAD geometry           0            FARFIELD
AFLR4    :         13            CAD geometry           0            FARFIELD
AFLR4    :         14            CAD geometry           0            FARFIELD
AFLR4    :         15            CAD geometry           0            FARFIELD
AFLR4    :         16            CAD geometry           0            FARFIELD

AFLR4    : Define CAD surface definition 1
AFLR4    : Define CAD surface definition 2
AFLR4    : Define CAD surface definition 3
AFLR4    : Define CAD surface definition 4
AFLR4    : Define CAD surface definition 5
AFLR4    : Define CAD surface definition 6
AFLR4    : Define CAD surface definition 7
AFLR4    : Define CAD surface definition 8
AFLR4    : Define CAD surface definition 9
AFLR4    : Define CAD surface definition 10
AFLR4    : Define CAD surface definition 11
AFLR4    : Define CAD surface definition 12
AFLR4    : Define CAD surface definition 13
AFLR4    : Define CAD surface definition 14
AFLR4    : Define CAD surface definition 15
AFLR4    : Define CAD surface definition 16

AFLR4    : Surface Grid Generation

AFLR4    : Generate optimal mesh on surface definition 1
AFLR2    : Nodes, Trias,Quads=      2701      5174         0
AFLR4    : Nodes, Trias,Quads=      1493      2758         0

AFLR4    : Generate optimal mesh on surface definition 2
AFLR2    : Nodes, Trias,Quads=      3758      7177         0
AFLR4    : Nodes, Trias,Quads=      1589      2839         0

AFLR4    : Generate optimal mesh on surface definition 3
AFLR2    : Nodes, Trias,Quads=      2824      5420         0
AFLR4    : Nodes, Trias,Quads=      1415      2602         0

AFLR4    : Generate optimal mesh on surface definition 4
AFLR2    : Nodes, Trias,Quads=      3766      7193         0
AFLR4    : Nodes, Trias,Quads=      1566      2793         0

AFLR4    : Generate optimal mesh on surface definition 5
AFLR2    : Nodes, Trias,Quads=        32        40         0
AFLR4    : Nodes, Trias,Quads=        22        20         0

AFLR4    : Generate optimal mesh on surface definition 6
AFLR2    : Nodes, Trias,Quads=       583      1067         0
AFLR4    : Nodes, Trias,Quads=       453       807         0

AFLR4    : Generate optimal mesh on surface definition 7
AFLR2    : Nodes, Trias,Quads=       616      1125         0
AFLR4    : Nodes, Trias,Quads=       323       539         0

AFLR4    : Generate optimal mesh on surface definition 8
AFLR2    : Nodes, Trias,Quads=       595      1091         0
AFLR4    : Nodes, Trias,Quads=       439       779         0

AFLR4    : Generate optimal mesh on surface definition 9
AFLR2    : Nodes, Trias,Quads=       585      1063         0
AFLR4    : Nodes, Trias,Quads=       314       521         0

AFLR4    : Generate optimal mesh on surface definition 10
AFLR2    : Nodes, Trias,Quads=        11        12         0
AFLR4    : Nodes, Trias,Quads=         8         6         0

AFLR4    : Generate optimal mesh on surface definition 11
AFLR2    : Nodes, Trias,Quads=         5         4         0
AFLR4    : Nodes, Trias,Quads=         4         2         0

AFLR4    : Generate optimal mesh on surface definition 12
AFLR2    : Nodes, Trias,Quads=         5         4         0
AFLR4    : Nodes, Trias,Quads=         4         2         0

AFLR4    : Generate optimal mesh on surface definition 13
AFLR2    : Nodes, Trias,Quads=         5         4         0
AFLR4    : Nodes, Trias,Quads=         4         2         0

AFLR4    : Generate optimal mesh on surface definition 14
AFLR2    : Nodes, Trias,Quads=         5         4         0
AFLR4    : Nodes, Trias,Quads=         4         2         0

AFLR4    : Generate optimal mesh on surface definition 15
AFLR2    : Nodes, Trias,Quads=         5         4         0
AFLR4    : Nodes, Trias,Quads=         4         2         0

AFLR4    : Generate optimal mesh on surface definition 16
AFLR2    : Nodes, Trias,Quads=         5         4         0
AFLR4    : Nodes, Trias,Quads=         4         2         0

DGEOM    : Add surface definitions to composite definition 0
DGEOM    : Glue composite surface definition 0
DGEOM    : Nodes,Faces,BEdges=      6842     13676      1584

AFLR4    : Curvature BG Surface Grid Generation

AFLR4    : Nodes, Faces      =      6842     13676

AFLR4    : Surface Grid Generation

AFLR4    : Generate optimal mesh on surface definition 1
AFLR2    : Nodes, Trias,Quads=      2679      5130         0
AFLR4    : Nodes, Trias,Quads=      2106      3984         0

AFLR4    : Generate optimal mesh on surface definition 2
AFLR2    : Nodes, Trias,Quads=      3434      6540         0
AFLR4    : Nodes, Trias,Quads=      2925      5522         0

AFLR4    : Generate optimal mesh on surface definition 3
AFLR2    : Nodes, Trias,Quads=      2738      5248         0
AFLR4    : Nodes, Trias,Quads=      2089      3950         0

AFLR4    : Generate optimal mesh on surface definition 4
AFLR2    : Nodes, Trias,Quads=      3474      6620         0
AFLR4    : Nodes, Trias,Quads=      2895      5462         0

AFLR4    : Generate optimal mesh on surface definition 5
AFLR2    : Nodes, Trias,Quads=        34        44         0
AFLR4    : Nodes, Trias,Quads=        22        20         0

AFLR4    : Generate optimal mesh on surface definition 6
AFLR2    : Nodes, Trias,Quads=       659      1212         0
AFLR4    : Nodes, Trias,Quads=       565      1024         0

AFLR4    : Generate optimal mesh on surface definition 7
AFLR2    : Nodes, Trias,Quads=       636      1162         0
AFLR4    : Nodes, Trias,Quads=       481       852         0

AFLR4    : Generate optimal mesh on surface definition 8
AFLR2    : Nodes, Trias,Quads=       640      1175         0
AFLR4    : Nodes, Trias,Quads=       542       979         0

AFLR4    : Generate optimal mesh on surface definition 9
AFLR2    : Nodes, Trias,Quads=       608      1107         0
AFLR4    : Nodes, Trias,Quads=       462       815         0

AFLR4    : Generate optimal mesh on surface definition 10
AFLR2    : Nodes, Trias,Quads=        11        12         0
AFLR4    : Nodes, Trias,Quads=         8         6         0

AFLR4    : Generate optimal mesh on surface definition 11
AFLR2    : Nodes, Trias,Quads=        12        14         0
AFLR4    : Nodes, Trias,Quads=         8         6         0

AFLR4    : Generate optimal mesh on surface definition 12
AFLR2    : Nodes, Trias,Quads=        12        14         0
AFLR4    : Nodes, Trias,Quads=         8         6         0

AFLR4    : Generate optimal mesh on surface definition 13
AFLR2    : Nodes, Trias,Quads=        12        14         0
AFLR4    : Nodes, Trias,Quads=         8         6         0

AFLR4    : Generate optimal mesh on surface definition 14
AFLR2    : Nodes, Trias,Quads=        12        14         0
AFLR4    : Nodes, Trias,Quads=         8         6         0

AFLR4    : Generate optimal mesh on surface definition 15
AFLR2    : Nodes, Trias,Quads=        12        14         0
AFLR4    : Nodes, Trias,Quads=         8         6         0

AFLR4    : Generate optimal mesh on surface definition 16
AFLR2    : Nodes, Trias,Quads=        12        14         0
AFLR4    : Nodes, Trias,Quads=         8         6         0

DGEOM    : Add surface definitions to composite definition 0
DGEOM    : Glue composite surface definition 0
DGEOM    : Nodes,Faces,BEdges=     11329     22650      1604

OVERALL  : CPU Time          =     0.197   seconds
Body 1 (of 2)
Number of nodes    = 11309
Number of elements = 22614
Number of triangle elements      = 22614
Number of quadrilateral elements = 0
Body 2 (of 2)
Number of nodes    = 20
Number of elements = 36
Number of triangle elements      = 36
Number of quadrilateral elements = 0
----------------------------
Total number of nodes    = 11329
Total number of elements = 22650
Total number of triangle elements      = 22650
Total number of quadrilateral elements = 0

real	0m1.089s
user	0m0.961s
sys	0m0.437s
+ status=0
+ set +x

=================================================
data/session07/05_aflr4_ScaleFactor.py passed (as expected)
=================================================


=================================================
06_aflr4_Proximity.py test;
+ python 06_aflr4_Proximity.py
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/CAPS/training/2023/training.log

MESSAGE:: Building wingOml


MESSAGE:: Building nacelleOml

Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 3
	Name = Nacelle, index = 1
	Name = Wing, index = 2
	Name = Farfield, index = 3
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 4
	Name = Nacelle, index = 1
	Name = leftWing, index = 2
	Name = riteWing, index = 3
	Name = Farfield, index = 4

Getting mesh sizing parameters
	Mesh sizing name - Farfield
	Mesh sizing name - Nacelle
	Mesh sizing name - leftWing
	Done getting mesh sizing parameters
 
AFLR2    : ---------------------------------------
AFLR2    : AFLR2 LIBRARY
AFLR2    : ADVANCING-FRONT/LOCAL-RECONNECTION
AFLR2    : TRIA/QUAD GRID GENERATOR
AFLR2    : Version Number 9.18.1
AFLR2    : Version Date   06/11/24 @ 05:52PM
AFLR2    : Compile OS     Darwin 23.5.0 arm64
AFLR2    : Compile Date   06/11/24 @ 05:52PM
AFLR2    : Copyright 1994-2021, D.L. Marcum
AFLR2    : ---------------------------------------
 
AFLR4    : ---------------------------------------
AFLR4    : AFLR4 LIBRARY
AFLR4    : ADVANCING-FRONT/LOCAL-RECONNECTION
AFLR4    : TRIA/QUAD SURFACE GRID GENERATOR
AFLR4    : Version Number 11.5.15
AFLR4    : Version Date   07/19/24 @ 07:04PM
AFLR4    : Compile OS     Darwin 23.5.0 arm64
AFLR4    : Compile Date   07/19/24 @ 07:06PM
AFLR4    : Copyright 1994-2021, D.L. Marcum
AFLR4    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.8.1
EGADS    : ---------------------------------------

EGADS    : EGADS CAD Geometry Setup

EGADS    : Model has 4 Active Bodies

EGADS    : Body 0 is a SolidBody
EGADS    : Body 0 has 1 Shells
EGADS    : Body 0 has 4 Faces
EGADS    : Body 0 has 8 Edges
EGADS    : Body 0 has 4 Loops
EGADS    : Body 0 has 4 Nodes
EGADS    : Body 1 is a SolidBody
EGADS    : Body 1 has 1 Shells
EGADS    : Body 1 has 4 Faces
EGADS    : Body 1 has 8 Edges
EGADS    : Body 1 has 4 Loops
EGADS    : Body 1 has 4 Nodes
EGADS    : Body 2 is a SolidBody
EGADS    : Body 2 has 1 Shells
EGADS    : Body 2 has 10 Faces
EGADS    : Body 2 has 18 Edges
EGADS    : Body 2 has 10 Loops
EGADS    : Body 2 has 10 Nodes
EGADS    : Body 3 is a SolidBody
EGADS    : Body 3 has 1 Shells
EGADS    : Body 3 has 6 Faces
EGADS    : Body 3 has 12 Edges
EGADS    : Body 3 has 6 Loops
EGADS    : Body 3 has 8 Nodes

EGADS    : Check Grid BCs

EGADS    : Grid BCs are OK

EGADS    : Face Neighbor-Faces Information

EGADS    : QC  = Face Quad Combination Flag
EGADS    : IER = Face Isolated Edge Refinement Flag
EGADS    : ER  = Face Edge Refinement Factor
EGADS    :       Not applicable for Faces with a FarField Grid BC.
EGADS    : SF  = Face Scale Factor
EGADS    :       Not applicable for Faces with a FarField Grid BC.

EGADS    :   Face          Body    QC   IER       ER    Scale   Neighbor
EGADS    :     ID  Active    ID  Flag  Flag   Weight   Factor   Faces
EGADS    :      1     Yes     0     0     1        0      0.5   2 3
EGADS    :      2     Yes     0     0     1        0      0.5   1 4
EGADS    :      3     Yes     0     0     1        0      0.5   1 4
EGADS    :      4     Yes     0     0     1        0      0.5   2 3
EGADS    :      5     Yes     1     0     1        0      0.5   6 7
EGADS    :      6     Yes     1     0     1        0      0.5   5 8
EGADS    :      7     Yes     1     0     1        0      0.5   5 8
EGADS    :      8     Yes     1     0     1        0      0.5   6 7
EGADS    :      9     Yes     2     0     1        0       50   10 11 14
EGADS    :     10     Yes     2     0     1        0       50   9 12 13
EGADS    :     11     Yes     2     0     1        0       50   9 12 16
EGADS    :     12     Yes     2     0     1        0       50   10 11 13
EGADS    :     13     Yes     2     0     1        0       50   10 12
EGADS    :     14     Yes     2     0     1        0        1   9 15 16
EGADS    :     15     Yes     2     0     1        0        1   14 17 18
EGADS    :     16     Yes     2     0     1        0        1   11 14 17
EGADS    :     17     Yes     2     0     1        0        1   15 16 18
EGADS    :     18     Yes     2     0     1        0        1   15 17
EGADS    :     19     Yes     3     0     1       NA       NA   21 22 23 24
EGADS    :     20     Yes     3     0     1       NA       NA   21 22 23 24
EGADS    :     21     Yes     3     0     1       NA       NA   19 20 23 24
EGADS    :     22     Yes     3     0     1       NA       NA   19 20 23 24
EGADS    :     23     Yes     3     0     1       NA       NA   19 20 21 22
EGADS    :     24     Yes     3     0     1       NA       NA   19 20 21 22

EGADS    : Face Edges Information

EGADS    :   Face   Edges
EGADS    :      1   -1 3 2 -4
EGADS    :      2   -2 5 1 -6
EGADS    :      3   7 4 -8 -3
EGADS    :      4   8 6 -7 -5
EGADS    :      5   9 12 -10 -11
EGADS    :      6   10 14 -9 -13
EGADS    :      7   -15 11 16 -12
EGADS    :      8   -16 13 15 -14
EGADS    :      9   -17 18 19 -20
EGADS    :     10   -21 20 22 -23
EGADS    :     11   -19 24 17 -25
EGADS    :     12   -22 25 21 -26
EGADS    :     13   23 26
EGADS    :     14   27 29 -28 -18
EGADS    :     15   30 32 -31 -29
EGADS    :     16   28 33 -27 -24
EGADS    :     17   31 34 -30 -33
EGADS    :     18   -32 -34
EGADS    :     19   35 36 -37 -38
EGADS    :     20   -39 42 41 -40
EGADS    :     21   43 39 -44 -35
EGADS    :     22   -45 37 46 -41
EGADS    :     23   38 45 -42 -43
EGADS    :     24   -36 44 40 -46

EGADS    : Face Loops Information

EGADS    :   Face   Loops
EGADS    :      1   1
EGADS    :      2   2
EGADS    :      3   3
EGADS    :      4   4
EGADS    :      5   5
EGADS    :      6   6
EGADS    :      7   7
EGADS    :      8   8
EGADS    :      9   9
EGADS    :     10   10
EGADS    :     11   11
EGADS    :     12   12
EGADS    :     13   13
EGADS    :     14   14
EGADS    :     15   15
EGADS    :     16   16
EGADS    :     17   17
EGADS    :     18   18
EGADS    :     19   19
EGADS    :     20   20
EGADS    :     21   21
EGADS    :     22   22
EGADS    :     23   23
EGADS    :     24   24

EGADS    : Loop Edges Information

EGADS    :   Loop  Active   Edges
EGADS    :      1     Yes   -1 3 2 -4
EGADS    :      2     Yes   -2 5 1 -6
EGADS    :      3     Yes   7 4 -8 -3
EGADS    :      4     Yes   8 6 -7 -5
EGADS    :      5     Yes   9 12 -10 -11
EGADS    :      6     Yes   10 14 -9 -13
EGADS    :      7     Yes   -15 11 16 -12
EGADS    :      8     Yes   -16 13 15 -14
EGADS    :      9     Yes   -17 18 19 -20
EGADS    :     10     Yes   -21 20 22 -23
EGADS    :     11     Yes   -19 24 17 -25
EGADS    :     12     Yes   -22 25 21 -26
EGADS    :     13     Yes   23 26
EGADS    :     14     Yes   27 29 -28 -18
EGADS    :     15     Yes   30 32 -31 -29
EGADS    :     16     Yes   28 33 -27 -24
EGADS    :     17     Yes   31 34 -30 -33
EGADS    :     18     Yes   -32 -34
EGADS    :     19     Yes   35 36 -37 -38
EGADS    :     20     Yes   -39 42 41 -40
EGADS    :     21     Yes   43 39 -44 -35
EGADS    :     22     Yes   -45 37 46 -41
EGADS    :     23     Yes   38 45 -42 -43
EGADS    :     24     Yes   -36 44 40 -46

EGADS    : Edge Node, Scale Factor, and Neighbor-Faces Information

EGADS    : ESF = Edge Scale Factor
EGADS    :       Not applicable for DEGENERATE Edges or Edges with a FarField
EGADS    :       Grid BC Neighbor Face.

EGADS    :                                             Neighbor
EGADS    :   Edge  Body  Active Node1 Node2      ESF   Faces
EGADS    :      1     0     Yes     1     2        1   1 2
EGADS    :      2     0     Yes     3     4        1   1 2
EGADS    :      3     0     Yes     1     3        1   1 3
EGADS    :      4     0     Yes     2     4        1   1 3
EGADS    :      5     0     Yes     3     1        1   2 4
EGADS    :      6     0     Yes     4     2        1   2 4
EGADS    :      7     0     Yes     1     2        1   3 4
EGADS    :      8     0     Yes     3     4        1   3 4
EGADS    :      9     1     Yes     5     6        1   5 6
EGADS    :     10     1     Yes     7     8        1   5 6
EGADS    :     11     1     Yes     5     7        1   5 7
EGADS    :     12     1     Yes     6     8        1   5 7
EGADS    :     13     1     Yes     7     5        1   6 8
EGADS    :     14     1     Yes     8     6        1   6 8
EGADS    :     15     1     Yes     5     6        1   7 8
EGADS    :     16     1     Yes     7     8        1   7 8
EGADS    :     17     2     Yes     9    10        1   9 11
EGADS    :     18     2     Yes     9    11        1   9 14
EGADS    :     19     2     Yes    11    12        1   9 11
EGADS    :     20     2     Yes    10    12        1   9 10
EGADS    :     21     2     Yes    10    13        1   10 12
EGADS    :     22     2     Yes    12    14        1   10 12
EGADS    :     23     2     Yes    13    14        1   10 13
EGADS    :     24     2     Yes    11     9        1   11 16
EGADS    :     25     2     Yes    12    10        1   11 12
EGADS    :     26     2     Yes    14    13        1   12 13
EGADS    :     27     2     Yes     9    15        1   14 16
EGADS    :     28     2     Yes    11    16        1   14 16
EGADS    :     29     2     Yes    15    16        1   14 15
EGADS    :     30     2     Yes    15    17        1   15 17
EGADS    :     31     2     Yes    16    18        1   15 17
EGADS    :     32     2     Yes    17    18        1   15 18
EGADS    :     33     2     Yes    16    15        1   16 17
EGADS    :     34     2     Yes    18    17        1   17 18
EGADS    :     35     3     Yes    20    19       NA   19 21
EGADS    :     36     3     Yes    19    21       NA   19 24
EGADS    :     37     3     Yes    22    21       NA   19 22
EGADS    :     38     3     Yes    20    22       NA   19 23
EGADS    :     39     3     Yes    24    23       NA   20 21
EGADS    :     40     3     Yes    23    25       NA   20 24
EGADS    :     41     3     Yes    26    25       NA   20 22
EGADS    :     42     3     Yes    24    26       NA   20 23
EGADS    :     43     3     Yes    20    24       NA   21 23
EGADS    :     44     3     Yes    19    23       NA   21 24
EGADS    :     45     3     Yes    22    26       NA   22 23
EGADS    :     46     3     Yes    21    25       NA   22 24

EGADS    : Node Information

EGADS    :   Node  Active      Coordinates
EGADS    :      1     Yes       90.5173952                0                0
EGADS    :      2     Yes       90.5173952                0                0
EGADS    :      3     Yes       60.5173952                0                0
EGADS    :      4     Yes       60.5173952                0                0
EGADS    :      5     Yes       90.5173952       29.3018771                0
EGADS    :      6     Yes       90.5173952       29.3018771                0
EGADS    :      7     Yes       60.5173952       29.3018771                0
EGADS    :      8     Yes       60.5173952       29.3018771                0
EGADS    :      9     Yes       97.2007855                0                0
EGADS    :     10     Yes       97.9335611                0                0
EGADS    :     11     Yes               50                0                0
EGADS    :     12     Yes       75.3047874                0                0
EGADS    :     13     Yes       123.552357                0        4.7180639
EGADS    :     14     Yes       118.391317                0       3.99272703
EGADS    :     15     Yes       97.9335611       36.1389817                0
EGADS    :     16     Yes       75.3047874       36.1389817                0
EGADS    :     17     Yes       123.552357       97.6729236        4.7180639
EGADS    :     18     Yes       118.391317       97.6729236       3.99272703
EGADS    :     19     Yes                0                0       1947.05079
EGADS    :     20     Yes                0                0                0
EGADS    :     21     Yes                0       1953.45847       1947.05079
EGADS    :     22     Yes                0       1953.45847                0
EGADS    :     23     Yes       2040.21562                0       1947.05079
EGADS    :     24     Yes       2040.21562                0                0
EGADS    :     25     Yes       2040.21562       1953.45847       1947.05079
EGADS    :     26     Yes       2040.21562       1953.45847                0

EGADS    : Face and Edge Match Information

EGADS    : No Face Matches Found

AFLR4    : Surface Mesh Spacing Setup

AFLR4    : Max Bounding Box Length     = 3906.92
AFLR4    : Min Bounding Box Length     = 3906.92
AFLR4    : Max Ref Bounding Box Length = 195.346
AFLR4    : Min Ref Bounding Box Length = 22.2515
AFLR4    : Reference Length            = 21.7051
AFLR4    : BL Thickness                = 0
AFLR4    : FarField Spacing            = 530.302
AFLR4    : Abs Min Surf Spacing        = 0.0542627
AFLR4    : Min Surf Spacing            = 0.108525
AFLR4    : Max Surf Spacing            = 2.17051
AFLR4    : Global Scale Factor         = 1

AFLR4    : Geometry Definition Information

AFLR4    : Definition              Definition   Composite             Grid BC
AFLR4    :         ID                    Type          ID                Type
AFLR4    :          0     glue-only composite           -                   -
AFLR4    :          1            CAD geometry           0            STD w/BL
AFLR4    :          2            CAD geometry           0            STD w/BL
AFLR4    :          3            CAD geometry           0            STD w/BL
AFLR4    :          4            CAD geometry           0            STD w/BL
AFLR4    :          5            CAD geometry           0            STD w/BL
AFLR4    :          6            CAD geometry           0            STD w/BL
AFLR4    :          7            CAD geometry           0            STD w/BL
AFLR4    :          8            CAD geometry           0            STD w/BL
AFLR4    :          9            CAD geometry           0            STD w/BL
AFLR4    :         10            CAD geometry           0            STD w/BL
AFLR4    :         11            CAD geometry           0            STD w/BL
AFLR4    :         12            CAD geometry           0            STD w/BL
AFLR4    :         13            CAD geometry           0            STD w/BL
AFLR4    :         14            CAD geometry           0            STD w/BL
AFLR4    :         15            CAD geometry           0            STD w/BL
AFLR4    :         16            CAD geometry           0            STD w/BL
AFLR4    :         17            CAD geometry           0            STD w/BL
AFLR4    :         18            CAD geometry           0            STD w/BL
AFLR4    :         19            CAD geometry           0            FARFIELD
AFLR4    :         20            CAD geometry           0            FARFIELD
AFLR4    :         21            CAD geometry           0            FARFIELD
AFLR4    :         22            CAD geometry           0            FARFIELD
AFLR4    :         23            CAD geometry           0            FARFIELD
AFLR4    :         24            CAD geometry           0            FARFIELD

AFLR4    : Case has 2 Proximity Checking Components

AFLR4    : Component 1 includes Definitions 9 10 11 12 13 14 15 16 17 18
AFLR4    : Component 2 includes Definitions 1 2 3 4 5 6 7 8

AFLR4    : Define CAD surface definition 1
AFLR4    : Define CAD surface definition 2
AFLR4    : Define CAD surface definition 3
AFLR4    : Define CAD surface definition 4
AFLR4    : Define CAD surface definition 5
AFLR4    : Define CAD surface definition 6
AFLR4    : Define CAD surface definition 7
AFLR4    : Define CAD surface definition 8
AFLR4    : Define CAD surface definition 9
AFLR4    : Define CAD surface definition 10
AFLR4    : Define CAD surface definition 11
AFLR4    : Define CAD surface definition 12
AFLR4    : Define CAD surface definition 13
AFLR4    : Define CAD surface definition 14
AFLR4    : Define CAD surface definition 15
AFLR4    : Define CAD surface definition 16
AFLR4    : Define CAD surface definition 17
AFLR4    : Define CAD surface definition 18
AFLR4    : Define CAD surface definition 19
AFLR4    : Define CAD surface definition 20
AFLR4    : Define CAD surface definition 21
AFLR4    : Define CAD surface definition 22
AFLR4    : Define CAD surface definition 23
AFLR4    : Define CAD surface definition 24

AFLR4    : Surface Grid Generation

AFLR4    : Generate optimal mesh on surface definition 1
AFLR2    : Nodes, Trias,Quads=     13740     26927         0
AFLR4    : Nodes, Trias,Quads=     13723     26893         0

AFLR4    : Generate optimal mesh on surface definition 2
AFLR2    : Nodes, Trias,Quads=     18558     36477         0
AFLR4    : Nodes, Trias,Quads=     16589     32539         0

AFLR4    : Generate optimal mesh on surface definition 3
AFLR2    : Nodes, Trias,Quads=     13776     26999         0
AFLR4    : Nodes, Trias,Quads=     13736     26919         0

AFLR4    : Generate optimal mesh on surface definition 4
AFLR2    : Nodes, Trias,Quads=     18524     36409         0
AFLR4    : Nodes, Trias,Quads=     16538     32437         0

AFLR4    : Generate optimal mesh on surface definition 5
AFLR2    : Nodes, Trias,Quads=     13776     26999         0
AFLR4    : Nodes, Trias,Quads=     13736     26919         0

AFLR4    : Generate optimal mesh on surface definition 6
AFLR2    : Nodes, Trias,Quads=     18524     36409         0
AFLR4    : Nodes, Trias,Quads=     16538     32437         0

AFLR4    : Generate optimal mesh on surface definition 7
AFLR2    : Nodes, Trias,Quads=     13740     26927         0
AFLR4    : Nodes, Trias,Quads=     13723     26893         0

AFLR4    : Generate optimal mesh on surface definition 8
AFLR2    : Nodes, Trias,Quads=     18558     36477         0
AFLR4    : Nodes, Trias,Quads=     16589     32539         0

AFLR4    : Generate optimal mesh on surface definition 9
AFLR2    : Nodes, Trias,Quads=       502       907         0
AFLR4    : Nodes, Trias,Quads=       423       749         0

AFLR4    : Generate optimal mesh on surface definition 10
AFLR2    : Nodes, Trias,Quads=        85       133         0
AFLR4    : Nodes, Trias,Quads=        56        75         0

AFLR4    : Generate optimal mesh on surface definition 11
AFLR2    : Nodes, Trias,Quads=       502       907         0
AFLR4    : Nodes, Trias,Quads=       399       701         0

AFLR4    : Generate optimal mesh on surface definition 12
AFLR2    : Nodes, Trias,Quads=        84       131         0
AFLR4    : Nodes, Trias,Quads=        55        73         0

AFLR4    : Generate optimal mesh on surface definition 13
AFLR2    : Nodes, Trias,Quads=         5         4         0
AFLR4    : Nodes, Trias,Quads=         4         2         0

AFLR4    : Generate optimal mesh on surface definition 14
AFLR2    : Nodes, Trias,Quads=      8705     16905         0
AFLR4    : Nodes, Trias,Quads=      5312     10119         0

AFLR4    : Generate optimal mesh on surface definition 15
AFLR2    : Nodes, Trias,Quads=     17908     35030         0
AFLR4    : Nodes, Trias,Quads=      5567     10348         0

AFLR4    : Generate optimal mesh on surface definition 16
AFLR2    : Nodes, Trias,Quads=      8823     17141         0
AFLR4    : Nodes, Trias,Quads=      4980      9455         0

AFLR4    : Generate optimal mesh on surface definition 17
AFLR2    : Nodes, Trias,Quads=     16876     32967         0
AFLR4    : Nodes, Trias,Quads=      5357      9929         0

AFLR4    : Generate optimal mesh on surface definition 18
AFLR2    : Nodes, Trias,Quads=        55        71         0
AFLR4    : Nodes, Trias,Quads=        46        53         0

AFLR4    : Generate optimal mesh on surface definition 19
AFLR2    : Nodes, Trias,Quads=        73       116         0
AFLR4    : Nodes, Trias,Quads=        68       106         0

AFLR4    : Generate optimal mesh on surface definition 20
AFLR2    : Nodes, Trias,Quads=        73       116         0
AFLR4    : Nodes, Trias,Quads=        68       106         0

AFLR4    : Generate optimal mesh on surface definition 21
AFLR2    : Nodes, Trias,Quads=        73       116         0
AFLR4    : Nodes, Trias,Quads=        68       106         0

AFLR4    : Generate optimal mesh on surface definition 22
AFLR2    : Nodes, Trias,Quads=        73       116         0
AFLR4    : Nodes, Trias,Quads=        68       106         0

AFLR4    : Generate optimal mesh on surface definition 23
AFLR2    : Nodes, Trias,Quads=        73       116         0
AFLR4    : Nodes, Trias,Quads=        68       106         0

AFLR4    : Generate optimal mesh on surface definition 24
AFLR2    : Nodes, Trias,Quads=        73       116         0
AFLR4    : Nodes, Trias,Quads=        68       106         0

DGEOM    : Add surface definitions to composite definition 0
DGEOM    : Glue composite surface definition 0
DGEOM    : Nodes,Faces,BEdges=    139862    279716      7794

AFLR4    : Curvature BG Surface Grid Generation

AFLR4    : Nodes, Faces      =    139862    279716

AFLR4    : Surface Grid Generation

AFLR4    : Generate optimal mesh on surface definition 1
AFLR2    : Nodes, Trias,Quads=     13776     26996         0
AFLR4    : Nodes, Trias,Quads=     13887     27218         0

AFLR4    : Generate optimal mesh on surface definition 2
AFLR2    : Nodes, Trias,Quads=     18675     36709         0
AFLR4    : Nodes, Trias,Quads=     16689     32737         0

AFLR4    : Generate optimal mesh on surface definition 3
AFLR2    : Nodes, Trias,Quads=     13883     27210         0
AFLR4    : Nodes, Trias,Quads=     13963     27370         0

AFLR4    : Generate optimal mesh on surface definition 4
AFLR2    : Nodes, Trias,Quads=     18667     36693         0
AFLR4    : Nodes, Trias,Quads=     16618     32595         0

AFLR4    : Generate optimal mesh on surface definition 5
AFLR2    : Nodes, Trias,Quads=     13883     27210         0
AFLR4    : Nodes, Trias,Quads=     13963     27370         0

AFLR4    : Generate optimal mesh on surface definition 6
AFLR2    : Nodes, Trias,Quads=     18667     36693         0
AFLR4    : Nodes, Trias,Quads=     16618     32595         0

AFLR4    : Generate optimal mesh on surface definition 7
AFLR2    : Nodes, Trias,Quads=     13776     26996         0
AFLR4    : Nodes, Trias,Quads=     13887     27218         0

AFLR4    : Generate optimal mesh on surface definition 8
AFLR2    : Nodes, Trias,Quads=     18675     36709         0
AFLR4    : Nodes, Trias,Quads=     16689     32737         0

AFLR4    : Generate optimal mesh on surface definition 9
AFLR2    : Nodes, Trias,Quads=       525       950         0
AFLR4    : Nodes, Trias,Quads=       470       840         0

AFLR4    : Generate optimal mesh on surface definition 10
AFLR2    : Nodes, Trias,Quads=        91       144         0
AFLR4    : Nodes, Trias,Quads=        59        80         0

AFLR4    : Generate optimal mesh on surface definition 11
AFLR2    : Nodes, Trias,Quads=       538       976         0
AFLR4    : Nodes, Trias,Quads=       443       786         0

AFLR4    : Generate optimal mesh on surface definition 12
AFLR2    : Nodes, Trias,Quads=        90       142         0
AFLR4    : Nodes, Trias,Quads=        58        78         0

AFLR4    : Generate optimal mesh on surface definition 13
AFLR2    : Nodes, Trias,Quads=         5         4         0
AFLR4    : Nodes, Trias,Quads=         4         2         0

AFLR4    : Generate optimal mesh on surface definition 14
AFLR2    : Nodes, Trias,Quads=      8695     16888         0
AFLR4    : Nodes, Trias,Quads=      6539     12576         0

AFLR4    : Generate optimal mesh on surface definition 15
AFLR2    : Nodes, Trias,Quads=     13624     26478         0
AFLR4    : Nodes, Trias,Quads=      9963     19156         0

AFLR4    : Generate optimal mesh on surface definition 16
AFLR2    : Nodes, Trias,Quads=      8700     16899         0
AFLR4    : Nodes, Trias,Quads=      6656     12811         0

AFLR4    : Generate optimal mesh on surface definition 17
AFLR2    : Nodes, Trias,Quads=     13534     26300         0
AFLR4    : Nodes, Trias,Quads=      9965     19162         0

AFLR4    : Generate optimal mesh on surface definition 18
AFLR2    : Nodes, Trias,Quads=        60        79         0
AFLR4    : Nodes, Trias,Quads=        49        57         0

AFLR4    : Generate optimal mesh on surface definition 19
AFLR2    : Nodes, Trias,Quads=        73       116         0
AFLR4    : Nodes, Trias,Quads=        68       106         0

AFLR4    : Generate optimal mesh on surface definition 20
AFLR2    : Nodes, Trias,Quads=        73       116         0
AFLR4    : Nodes, Trias,Quads=        68       106         0

AFLR4    : Generate optimal mesh on surface definition 21
AFLR2    : Nodes, Trias,Quads=        73       116         0
AFLR4    : Nodes, Trias,Quads=        68       106         0

AFLR4    : Generate optimal mesh on surface definition 22
AFLR2    : Nodes, Trias,Quads=        73       116         0
AFLR4    : Nodes, Trias,Quads=        68       106         0

AFLR4    : Generate optimal mesh on surface definition 23
AFLR2    : Nodes, Trias,Quads=        73       116         0
AFLR4    : Nodes, Trias,Quads=        68       106         0

AFLR4    : Generate optimal mesh on surface definition 24
AFLR2    : Nodes, Trias,Quads=        73       116         0
AFLR4    : Nodes, Trias,Quads=        68       106         0

DGEOM    : Add surface definitions to composite definition 0
DGEOM    : Glue composite surface definition 0
DGEOM    : Nodes,Faces,BEdges=    153016    306024      7784

AFLR4    : Proximity BG Surface Grid Generation

AFLR4    : Nodes, Trias      =    153404    306800

AFLR4    : Surface Grid Generation

AFLR4    : Generate optimal mesh on surface definition 1
AFLR2    : Nodes, Trias,Quads=     13935     27308         0
AFLR4    : Nodes, Trias,Quads=     13791     27020         0

AFLR4    : Generate optimal mesh on surface definition 2
AFLR2    : Nodes, Trias,Quads=     18710     36774         0
AFLR4    : Nodes, Trias,Quads=     16564     32482         0

AFLR4    : Generate optimal mesh on surface definition 3
AFLR2    : Nodes, Trias,Quads=     13945     27328         0
AFLR4    : Nodes, Trias,Quads=     13842     27122         0

AFLR4    : Generate optimal mesh on surface definition 4
AFLR2    : Nodes, Trias,Quads=     18677     36708         0
AFLR4    : Nodes, Trias,Quads=     16540     32434         0

AFLR4    : Generate optimal mesh on surface definition 5
AFLR2    : Nodes, Trias,Quads=     13945     27328         0
AFLR4    : Nodes, Trias,Quads=     13842     27122         0

AFLR4    : Generate optimal mesh on surface definition 6
AFLR2    : Nodes, Trias,Quads=     18677     36708         0
AFLR4    : Nodes, Trias,Quads=     16540     32434         0

AFLR4    : Generate optimal mesh on surface definition 7
AFLR2    : Nodes, Trias,Quads=     13935     27308         0
AFLR4    : Nodes, Trias,Quads=     13791     27020         0

AFLR4    : Generate optimal mesh on surface definition 8
AFLR2    : Nodes, Trias,Quads=     18710     36774         0
AFLR4    : Nodes, Trias,Quads=     16564     32482         0

AFLR4    : Generate optimal mesh on surface definition 9
AFLR2    : Nodes, Trias,Quads=       699      1265         0
AFLR4    : Nodes, Trias,Quads=       814      1495         0

AFLR4    : Generate optimal mesh on surface definition 10
AFLR2    : Nodes, Trias,Quads=       103       166         0
AFLR4    : Nodes, Trias,Quads=        63        86         0

AFLR4    : Generate optimal mesh on surface definition 11
AFLR2    : Nodes, Trias,Quads=      1127      2108         0
AFLR4    : Nodes, Trias,Quads=      1745      3344         0

AFLR4    : Generate optimal mesh on surface definition 12
AFLR2    : Nodes, Trias,Quads=       146       239         0
AFLR4    : Nodes, Trias,Quads=       186       319         0

AFLR4    : Generate optimal mesh on surface definition 13
AFLR2    : Nodes, Trias,Quads=         5         4         0
AFLR4    : Nodes, Trias,Quads=         4         2         0

AFLR4    : Generate optimal mesh on surface definition 14
AFLR2    : Nodes, Trias,Quads=      8840     17170         0
AFLR4    : Nodes, Trias,Quads=      7153     13796         0

AFLR4    : Generate optimal mesh on surface definition 15
AFLR2    : Nodes, Trias,Quads=     15659     30521         0
AFLR4    : Nodes, Trias,Quads=     11063     21329         0

AFLR4    : Generate optimal mesh on surface definition 16
AFLR2    : Nodes, Trias,Quads=      9010     17511         0
AFLR4    : Nodes, Trias,Quads=      7795     15081         0

AFLR4    : Generate optimal mesh on surface definition 17
AFLR2    : Nodes, Trias,Quads=     15522     30248         0
AFLR4    : Nodes, Trias,Quads=     11035     21274         0

AFLR4    : Generate optimal mesh on surface definition 18
AFLR2    : Nodes, Trias,Quads=        61        80         0
AFLR4    : Nodes, Trias,Quads=        50        58         0

AFLR4    : Generate optimal mesh on surface definition 19
AFLR2    : Nodes, Trias,Quads=        73       116         0
AFLR4    : Nodes, Trias,Quads=        68       106         0

AFLR4    : Generate optimal mesh on surface definition 20
AFLR2    : Nodes, Trias,Quads=        73       116         0
AFLR4    : Nodes, Trias,Quads=        68       106         0

AFLR4    : Generate optimal mesh on surface definition 21
AFLR2    : Nodes, Trias,Quads=        73       116         0
AFLR4    : Nodes, Trias,Quads=        68       106         0

AFLR4    : Generate optimal mesh on surface definition 22
AFLR2    : Nodes, Trias,Quads=        73       116         0
AFLR4    : Nodes, Trias,Quads=        68       106         0

AFLR4    : Generate optimal mesh on surface definition 23
AFLR2    : Nodes, Trias,Quads=        73       116         0
AFLR4    : Nodes, Trias,Quads=        68       106         0

AFLR4    : Generate optimal mesh on surface definition 24
AFLR2    : Nodes, Trias,Quads=        73       116         0
AFLR4    : Nodes, Trias,Quads=        68       106         0

DGEOM    : Add surface definitions to composite definition 0
DGEOM    : Glue composite surface definition 0
DGEOM    : Nodes,Faces,BEdges=    157772    315536      7996

OVERALL  : CPU Time          =     4.553   seconds
Body 1 (of 4)
Number of nodes    = 59529
Number of elements = 119058
Number of triangle elements      = 119058
Number of quadrilateral elements = 0
Body 2 (of 4)
Number of nodes    = 59529
Number of elements = 119058
Number of triangle elements      = 119058
Number of quadrilateral elements = 0
Body 3 (of 4)
Number of nodes    = 38394
Number of elements = 76784
Number of triangle elements      = 76784
Number of quadrilateral elements = 0
Body 4 (of 4)
Number of nodes    = 320
Number of elements = 636
Number of triangle elements      = 636
Number of quadrilateral elements = 0
----------------------------
Total number of nodes    = 157772
Total number of elements = 315536
Total number of triangle elements      = 315536
Total number of quadrilateral elements = 0

real	0m7.587s
user	0m7.358s
sys	0m0.504s
+ status=0
+ set +x

=================================================
data/session07/06_aflr4_Proximity.py passed (as expected)
=================================================


=================================================
07_aflr4_ProximityComponents.py test;
+ python 07_aflr4_ProximityComponents.py
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/CAPS/training/2023/training.log

MESSAGE:: Building wingOml


MESSAGE:: Building pylonOml


MESSAGE:: Building nacelleOml

Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 4
	Name = Wing, index = 1
	Name = Pylon, index = 2
	Name = Nacelle, index = 3
	Name = Farfield, index = 4
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 5
	Name = leftWing, index = 1
	Name = riteWing, index = 2
	Name = Pylon, index = 3
	Name = Nacelle, index = 4
	Name = Farfield, index = 5

Getting mesh sizing parameters
	Mesh sizing name - Farfield
	Mesh sizing name - Nacelle
	Mesh sizing name - Pylon
	Mesh sizing name - leftWing
	Done getting mesh sizing parameters
 
AFLR2    : ---------------------------------------
AFLR2    : AFLR2 LIBRARY
AFLR2    : ADVANCING-FRONT/LOCAL-RECONNECTION
AFLR2    : TRIA/QUAD GRID GENERATOR
AFLR2    : Version Number 9.18.1
AFLR2    : Version Date   06/11/24 @ 05:52PM
AFLR2    : Compile OS     Darwin 23.5.0 arm64
AFLR2    : Compile Date   06/11/24 @ 05:52PM
AFLR2    : Copyright 1994-2021, D.L. Marcum
AFLR2    : ---------------------------------------
 
AFLR4    : ---------------------------------------
AFLR4    : AFLR4 LIBRARY
AFLR4    : ADVANCING-FRONT/LOCAL-RECONNECTION
AFLR4    : TRIA/QUAD SURFACE GRID GENERATOR
AFLR4    : Version Number 11.5.15
AFLR4    : Version Date   07/19/24 @ 07:04PM
AFLR4    : Compile OS     Darwin 23.5.0 arm64
AFLR4    : Compile Date   07/19/24 @ 07:06PM
AFLR4    : Copyright 1994-2021, D.L. Marcum
AFLR4    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.8.1
EGADS    : ---------------------------------------

EGADS    : EGADS CAD Geometry Setup

EGADS    : Model has 2 Active Bodies

EGADS    : Body 0 is a SolidBody
EGADS    : Body 0 has 1 Shells
EGADS    : Body 0 has 22 Faces
EGADS    : Body 0 has 48 Edges
EGADS    : Body 0 has 24 Loops
EGADS    : Body 0 has 26 Nodes
EGADS    : Body 1 is a SolidBody
EGADS    : Body 1 has 1 Shells
EGADS    : Body 1 has 6 Faces
EGADS    : Body 1 has 12 Edges
EGADS    : Body 1 has 6 Loops
EGADS    : Body 1 has 8 Nodes

EGADS    : Check Grid BCs

EGADS    : Grid BCs are OK

EGADS    : Face Neighbor-Faces Information

EGADS    : QC  = Face Quad Combination Flag
EGADS    : IER = Face Isolated Edge Refinement Flag
EGADS    : ER  = Face Edge Refinement Factor
EGADS    :       Not applicable for Faces with a FarField Grid BC.
EGADS    : SF  = Face Scale Factor
EGADS    :       Not applicable for Faces with a FarField Grid BC.

EGADS    :   Face          Body    QC   IER       ER    Scale   Neighbor
EGADS    :     ID  Active    ID  Flag  Flag   Weight   Factor   Faces
EGADS    :      1     Yes     0     0     1        0       50   2 3 4
EGADS    :      2     Yes     0     0     1        0       50   1 5 6 7 8
EGADS    :      3     Yes     0     0     1        0        1   1 5 9
EGADS    :      4     Yes     0     0     1        0       50   1 6 10
EGADS    :      5     Yes     0     0     1        0        1   2 3 11 12 13
EGADS    :      6     Yes     0     0     1        0       50   2 4 10
EGADS    :      7     Yes     0     0     1        0       10   2 8 14
EGADS    :      8     Yes     0     0     1        0       10   2 7 15
EGADS    :      9     Yes     0     0     1        0        1   3 11 16
EGADS    :     10     Yes     0     0     1        0       50   4 6
EGADS    :     11     Yes     0     0     1        0        1   5 9 16
EGADS    :     12     Yes     0     0     1        0       10   5 13 17
EGADS    :     13     Yes     0     0     1        0       10   5 12 18
EGADS    :     14     Yes     0     0     1        0      0.5   7 15 19
EGADS    :     15     Yes     0     0     1        0      0.5   8 14 20
EGADS    :     16     Yes     0     0     1        0        1   9 11
EGADS    :     17     Yes     0     0     1        0      0.5   12 18 21
EGADS    :     18     Yes     0     0     1        0      0.5   13 17 22
EGADS    :     19     Yes     0     0     1        0      0.5   14 20
EGADS    :     20     Yes     0     0     1        0      0.5   15 19
EGADS    :     21     Yes     0     0     1        0      0.5   17 22
EGADS    :     22     Yes     0     0     1        0      0.5   18 21
EGADS    :     23     Yes     1     0     1       NA       NA   25 26 27 28
EGADS    :     24     Yes     1     0     1       NA       NA   25 26 27 28
EGADS    :     25     Yes     1     0     1       NA       NA   23 24 27 28
EGADS    :     26     Yes     1     0     1       NA       NA   23 24 27 28
EGADS    :     27     Yes     1     0     1       NA       NA   23 24 25 26
EGADS    :     28     Yes     1     0     1       NA       NA   23 24 25 26

EGADS    : Face Edges Information

EGADS    :   Face   Edges
EGADS    :      1   -1 2 3 -4
EGADS    :      2   -3 5 1 -6 7 8
EGADS    :      3   9 11 -10 -2
EGADS    :      4   -12 4 13 -14
EGADS    :      5   10 15 -9 -5 16 17
EGADS    :      6   -13 6 12 -18
EGADS    :      7   19 20 -7 -21
EGADS    :      8   21 -8 -20 -22
EGADS    :      9   23 25 -24 -11
EGADS    :     10   14 18
EGADS    :     11   24 26 -23 -15
EGADS    :     12   -27 29 -16 -28
EGADS    :     13   -29 30 28 -17
EGADS    :     14   31 -19 32 33 -34 -35
EGADS    :     15   -31 37 34 -36 -32 22
EGADS    :     16   -25 -26
EGADS    :     17   38 27 39 40 -41 -42
EGADS    :     18   -38 44 41 -43 -39 -30
EGADS    :     19   -33 45 35 -46
EGADS    :     20   36 46 -37 -45
EGADS    :     21   -40 47 42 -48
EGADS    :     22   43 48 -44 -47
EGADS    :     23   49 50 -51 -52
EGADS    :     24   -53 56 55 -54
EGADS    :     25   57 53 -58 -49
EGADS    :     26   -59 51 60 -55
EGADS    :     27   52 59 -56 -57
EGADS    :     28   -50 58 54 -60

EGADS    : Face Loops Information

EGADS    :   Face   Loops
EGADS    :      1   1
EGADS    :      2   2 3
EGADS    :      3   4
EGADS    :      4   5
EGADS    :      5   6 7
EGADS    :      6   8
EGADS    :      7   9
EGADS    :      8   10
EGADS    :      9   11
EGADS    :     10   12
EGADS    :     11   13
EGADS    :     12   14
EGADS    :     13   15
EGADS    :     14   16
EGADS    :     15   17
EGADS    :     16   18
EGADS    :     17   19
EGADS    :     18   20
EGADS    :     19   21
EGADS    :     20   22
EGADS    :     21   23
EGADS    :     22   24
EGADS    :     23   25
EGADS    :     24   26
EGADS    :     25   27
EGADS    :     26   28
EGADS    :     27   29
EGADS    :     28   30

EGADS    : Loop Edges Information

EGADS    :   Loop  Active   Edges
EGADS    :      1     Yes   -1 2 3 -4
EGADS    :      2     Yes   -3 5 1 -6
EGADS    :      3     Yes   7 8
EGADS    :      4     Yes   9 11 -10 -2
EGADS    :      5     Yes   -12 4 13 -14
EGADS    :      6     Yes   10 15 -9 -5
EGADS    :      7     Yes   16 17
EGADS    :      8     Yes   -13 6 12 -18
EGADS    :      9     Yes   19 20 -7 -21
EGADS    :     10     Yes   21 -8 -20 -22
EGADS    :     11     Yes   23 25 -24 -11
EGADS    :     12     Yes   14 18
EGADS    :     13     Yes   24 26 -23 -15
EGADS    :     14     Yes   -27 29 -16 -28
EGADS    :     15     Yes   -29 30 28 -17
EGADS    :     16     Yes   31 -19 32 33 -34 -35
EGADS    :     17     Yes   -31 37 34 -36 -32 22
EGADS    :     18     Yes   -25 -26
EGADS    :     19     Yes   38 27 39 40 -41 -42
EGADS    :     20     Yes   -38 44 41 -43 -39 -30
EGADS    :     21     Yes   -33 45 35 -46
EGADS    :     22     Yes   36 46 -37 -45
EGADS    :     23     Yes   -40 47 42 -48
EGADS    :     24     Yes   43 48 -44 -47
EGADS    :     25     Yes   49 50 -51 -52
EGADS    :     26     Yes   -53 56 55 -54
EGADS    :     27     Yes   57 53 -58 -49
EGADS    :     28     Yes   -59 51 60 -55
EGADS    :     29     Yes   52 59 -56 -57
EGADS    :     30     Yes   -50 58 54 -60

EGADS    : Edge Node, Scale Factor, and Neighbor-Faces Information

EGADS    : ESF = Edge Scale Factor
EGADS    :       Not applicable for DEGENERATE Edges or Edges with a FarField
EGADS    :       Grid BC Neighbor Face.

EGADS    :                                             Neighbor
EGADS    :   Edge  Body  Active Node1 Node2      ESF   Faces
EGADS    :      1     0     Yes     1     2        1   1 2
EGADS    :      2     0     Yes     1     3        1   1 3
EGADS    :      3     0     Yes     3     4        1   1 2
EGADS    :      4     0     Yes     2     4        1   1 4
EGADS    :      5     0     Yes     3     1        1   2 5
EGADS    :      6     0     Yes     4     2        1   2 6
EGADS    :      7     0     Yes     5     6        1   2 7
EGADS    :      8     0     Yes     6     5        1   2 8
EGADS    :      9     0     Yes     1     7        1   3 5
EGADS    :     10     0     Yes     3     8        1   3 5
EGADS    :     11     0     Yes     7     8        1   3 9
EGADS    :     12     0     Yes     2     9        1   4 6
EGADS    :     13     0     Yes     4    10        1   4 6
EGADS    :     14     0     Yes     9    10        1   4 10
EGADS    :     15     0     Yes     8     7        1   5 11
EGADS    :     16     0     Yes    11    12        1   5 12
EGADS    :     17     0     Yes    12    11        1   5 13
EGADS    :     18     0     Yes    10     9        1   6 10
EGADS    :     19     0     Yes    13    14        1   7 14
EGADS    :     20     0     Yes    14     6        1   7 8
EGADS    :     21     0     Yes    13     5        1   7 8
EGADS    :     22     0     Yes    13    14        1   8 15
EGADS    :     23     0     Yes     7    15        1   9 11
EGADS    :     24     0     Yes     8    16        1   9 11
EGADS    :     25     0     Yes    15    16        1   9 16
EGADS    :     26     0     Yes    16    15        1   11 16
EGADS    :     27     0     Yes    17    18        1   12 17
EGADS    :     28     0     Yes    18    11        1   12 13
EGADS    :     29     0     Yes    17    12        1   12 13
EGADS    :     30     0     Yes    17    18        1   13 18
EGADS    :     31     0     Yes    19    14        1   14 15
EGADS    :     32     0     Yes    13    20        1   14 15
EGADS    :     33     0     Yes    20    21        1   14 19
EGADS    :     34     0     Yes    22    21        1   14 15
EGADS    :     35     0     Yes    19    22        1   14 19
EGADS    :     36     0     Yes    20    21        1   15 20
EGADS    :     37     0     Yes    19    22        1   15 20
EGADS    :     38     0     Yes    23    17        1   17 18
EGADS    :     39     0     Yes    18    24        1   17 18
EGADS    :     40     0     Yes    24    25        1   17 21
EGADS    :     41     0     Yes    26    25        1   17 18
EGADS    :     42     0     Yes    23    26        1   17 21
EGADS    :     43     0     Yes    24    25        1   18 22
EGADS    :     44     0     Yes    23    26        1   18 22
EGADS    :     45     0     Yes    20    19        1   19 20
EGADS    :     46     0     Yes    21    22        1   19 20
EGADS    :     47     0     Yes    24    23        1   21 22
EGADS    :     48     0     Yes    25    26        1   21 22
EGADS    :     49     1     Yes    28    27       NA   23 25
EGADS    :     50     1     Yes    27    29       NA   23 28
EGADS    :     51     1     Yes    30    29       NA   23 26
EGADS    :     52     1     Yes    28    30       NA   23 27
EGADS    :     53     1     Yes    32    31       NA   24 25
EGADS    :     54     1     Yes    31    33       NA   24 28
EGADS    :     55     1     Yes    34    33       NA   24 26
EGADS    :     56     1     Yes    32    34       NA   24 27
EGADS    :     57     1     Yes    28    32       NA   25 27
EGADS    :     58     1     Yes    27    31       NA   25 28
EGADS    :     59     1     Yes    30    34       NA   26 27
EGADS    :     60     1     Yes    29    33       NA   26 28

EGADS    : Node Information

EGADS    :   Node  Active      Coordinates
EGADS    :      1     Yes       97.2007855                0                0
EGADS    :      2     Yes       97.9335611                0                0
EGADS    :      3     Yes               50                0                0
EGADS    :      4     Yes       75.3047874                0                0
EGADS    :      5     Yes       72.4759225                0                0
EGADS    :      6     Yes       83.5054156                0                0
EGADS    :      7     Yes       97.9335611       36.1389817                0
EGADS    :      8     Yes       75.3047874       36.1389817                0
EGADS    :      9     Yes       123.552357                0        4.7180639
EGADS    :     10     Yes       118.391317                0       3.99272703
EGADS    :     11     Yes       72.4759225       29.3018771                0
EGADS    :     12     Yes       83.5054156       29.3018771                0
EGADS    :     13     Yes        70.524066                0                0
EGADS    :     14     Yes       79.4370049                0                0
EGADS    :     15     Yes       123.552357       97.6729236        4.7180639
EGADS    :     16     Yes       118.391317       97.6729236       3.99272703
EGADS    :     17     Yes       79.4370049       29.3018771                0
EGADS    :     18     Yes        70.524066       29.3018771                0
EGADS    :     19     Yes       90.5173952                0                0
EGADS    :     20     Yes       60.5173952                0                0
EGADS    :     21     Yes       60.5173952                0                0
EGADS    :     22     Yes       90.5173952                0                0
EGADS    :     23     Yes       90.5173952       29.3018771                0
EGADS    :     24     Yes       60.5173952       29.3018771                0
EGADS    :     25     Yes       60.5173952       29.3018771                0
EGADS    :     26     Yes       90.5173952       29.3018771                0
EGADS    :     27     Yes                0                0       1947.05079
EGADS    :     28     Yes                0                0                0
EGADS    :     29     Yes                0       1953.45847       1947.05079
EGADS    :     30     Yes                0       1953.45847                0
EGADS    :     31     Yes       2040.21562                0       1947.05079
EGADS    :     32     Yes       2040.21562                0                0
EGADS    :     33     Yes       2040.21562       1953.45847       1947.05079
EGADS    :     34     Yes       2040.21562       1953.45847                0

EGADS    : Face and Edge Match Information

EGADS    : No Face Matches Found

AFLR4    : Surface Mesh Spacing Setup

AFLR4    : Max Bounding Box Length     = 3906.92
AFLR4    : Min Bounding Box Length     = 3906.92
AFLR4    : Max Ref Bounding Box Length = 195.346
AFLR4    : Min Ref Bounding Box Length = 22.2515
AFLR4    : Reference Length            = 21.7051
AFLR4    : BL Thickness                = 0
AFLR4    : FarField Spacing            = 530.302
AFLR4    : Abs Min Surf Spacing        = 0.0542627
AFLR4    : Min Surf Spacing            = 0.108525
AFLR4    : Max Surf Spacing            = 2.17051
AFLR4    : Global Scale Factor         = 1

AFLR4    : Geometry Definition Information

AFLR4    : Definition              Definition   Composite             Grid BC
AFLR4    :         ID                    Type          ID                Type
AFLR4    :          0     glue-only composite           -                   -
AFLR4    :          1            CAD geometry           0            STD w/BL
AFLR4    :          2            CAD geometry           0            STD w/BL
AFLR4    :          3            CAD geometry           0            STD w/BL
AFLR4    :          4            CAD geometry           0            STD w/BL
AFLR4    :          5            CAD geometry           0            STD w/BL
AFLR4    :          6            CAD geometry           0            STD w/BL
AFLR4    :          7            CAD geometry           0            STD w/BL
AFLR4    :          8            CAD geometry           0            STD w/BL
AFLR4    :          9            CAD geometry           0            STD w/BL
AFLR4    :         10            CAD geometry           0            STD w/BL
AFLR4    :         11            CAD geometry           0            STD w/BL
AFLR4    :         12            CAD geometry           0            STD w/BL
AFLR4    :         13            CAD geometry           0            STD w/BL
AFLR4    :         14            CAD geometry           0            STD w/BL
AFLR4    :         15            CAD geometry           0            STD w/BL
AFLR4    :         16            CAD geometry           0            STD w/BL
AFLR4    :         17            CAD geometry           0            STD w/BL
AFLR4    :         18            CAD geometry           0            STD w/BL
AFLR4    :         19            CAD geometry           0            STD w/BL
AFLR4    :         20            CAD geometry           0            STD w/BL
AFLR4    :         21            CAD geometry           0            STD w/BL
AFLR4    :         22            CAD geometry           0            STD w/BL
AFLR4    :         23            CAD geometry           0            FARFIELD
AFLR4    :         24            CAD geometry           0            FARFIELD
AFLR4    :         25            CAD geometry           0            FARFIELD
AFLR4    :         26            CAD geometry           0            FARFIELD
AFLR4    :         27            CAD geometry           0            FARFIELD
AFLR4    :         28            CAD geometry           0            FARFIELD

AFLR4    : Case has 3 Proximity Checking Components

AFLR4    : Component 1 includes Definitions 1 2 3 4 5 6 9 10 11 16
AFLR4    : Component 2 includes Definitions 14 15 17 18 19 20 21 22
AFLR4    : Component 3 includes Definitions 7 8 12 13

AFLR4    : Define CAD surface definition 1
AFLR4    : Define CAD surface definition 2
AFLR4    : Define CAD surface definition 3
AFLR4    : Define CAD surface definition 4
AFLR4    : Define CAD surface definition 5
AFLR4    : Define CAD surface definition 6
AFLR4    : Define CAD surface definition 7
AFLR4    : Define CAD surface definition 8
AFLR4    : Define CAD surface definition 9
AFLR4    : Define CAD surface definition 10
AFLR4    : Define CAD surface definition 11
AFLR4    : Define CAD surface definition 12
AFLR4    : Define CAD surface definition 13
AFLR4    : Define CAD surface definition 14
AFLR4    : Define CAD surface definition 15
AFLR4    : Define CAD surface definition 16
AFLR4    : Define CAD surface definition 17
AFLR4    : Define CAD surface definition 18
AFLR4    : Define CAD surface definition 19
AFLR4    : Define CAD surface definition 20
AFLR4    : Define CAD surface definition 21
AFLR4    : Define CAD surface definition 22
AFLR4    : Define CAD surface definition 23
AFLR4    : Define CAD surface definition 24
AFLR4    : Define CAD surface definition 25
AFLR4    : Define CAD surface definition 26
AFLR4    : Define CAD surface definition 27
AFLR4    : Define CAD surface definition 28

AFLR4    : Surface Grid Generation

AFLR4    : Generate optimal mesh on surface definition 1
AFLR2    : Nodes, Trias,Quads=       502       907         0
AFLR4    : Nodes, Trias,Quads=       423       749         0

AFLR4    : Generate optimal mesh on surface definition 2
AFLR2    : Nodes, Trias,Quads=       769      1416         0
AFLR4    : Nodes, Trias,Quads=       579      1036         0

AFLR4    : Generate optimal mesh on surface definition 3
AFLR2    : Nodes, Trias,Quads=      8705     16905         0
AFLR4    : Nodes, Trias,Quads=      5312     10119         0

AFLR4    : Generate optimal mesh on surface definition 4
AFLR2    : Nodes, Trias,Quads=        85       133         0
AFLR4    : Nodes, Trias,Quads=        56        75         0

AFLR4    : Generate optimal mesh on surface definition 5
AFLR2    : Nodes, Trias,Quads=      9412     18267         0
AFLR4    : Nodes, Trias,Quads=      5160      9763         0

AFLR4    : Generate optimal mesh on surface definition 6
AFLR2    : Nodes, Trias,Quads=        84       131         0
AFLR4    : Nodes, Trias,Quads=        55        73         0

AFLR4    : Generate optimal mesh on surface definition 7
AFLR2    : Nodes, Trias,Quads=       382       673         0
AFLR4    : Nodes, Trias,Quads=       221       351         0

AFLR4    : Generate optimal mesh on surface definition 8
AFLR2    : Nodes, Trias,Quads=       377       662         0
AFLR4    : Nodes, Trias,Quads=       227       362         0

AFLR4    : Generate optimal mesh on surface definition 9
AFLR2    : Nodes, Trias,Quads=     17908     35030         0
AFLR4    : Nodes, Trias,Quads=      5567     10348         0

AFLR4    : Generate optimal mesh on surface definition 10
AFLR2    : Nodes, Trias,Quads=         5         4         0
AFLR4    : Nodes, Trias,Quads=         4         2         0

AFLR4    : Generate optimal mesh on surface definition 11
AFLR2    : Nodes, Trias,Quads=     16876     32967         0
AFLR4    : Nodes, Trias,Quads=      5357      9929         0

AFLR4    : Generate optimal mesh on surface definition 12
AFLR2    : Nodes, Trias,Quads=       536       964         0
AFLR4    : Nodes, Trias,Quads=       324       540         0

AFLR4    : Generate optimal mesh on surface definition 13
AFLR2    : Nodes, Trias,Quads=       530       952         0
AFLR4    : Nodes, Trias,Quads=       325       542         0

AFLR4    : Generate optimal mesh on surface definition 14
AFLR2    : Nodes, Trias,Quads=     14942     29305         0
AFLR4    : Nodes, Trias,Quads=     14513     28447         0

AFLR4    : Generate optimal mesh on surface definition 15
AFLR2    : Nodes, Trias,Quads=     14940     29301         0
AFLR4    : Nodes, Trias,Quads=     14427     28275         0

AFLR4    : Generate optimal mesh on surface definition 16
AFLR2    : Nodes, Trias,Quads=        55        71         0
AFLR4    : Nodes, Trias,Quads=        46        53         0

AFLR4    : Generate optimal mesh on surface definition 17
AFLR2    : Nodes, Trias,Quads=     14942     29305         0
AFLR4    : Nodes, Trias,Quads=     14513     28447         0

AFLR4    : Generate optimal mesh on surface definition 18
AFLR2    : Nodes, Trias,Quads=     14928     29277         0
AFLR4    : Nodes, Trias,Quads=     14400     28221         0

AFLR4    : Generate optimal mesh on surface definition 19
AFLR2    : Nodes, Trias,Quads=     18558     36477         0
AFLR4    : Nodes, Trias,Quads=     16589     32539         0

AFLR4    : Generate optimal mesh on surface definition 20
AFLR2    : Nodes, Trias,Quads=     18524     36409         0
AFLR4    : Nodes, Trias,Quads=     16538     32437         0

AFLR4    : Generate optimal mesh on surface definition 21
AFLR2    : Nodes, Trias,Quads=     18558     36477         0
AFLR4    : Nodes, Trias,Quads=     16589     32539         0

AFLR4    : Generate optimal mesh on surface definition 22
AFLR2    : Nodes, Trias,Quads=     18524     36409         0
AFLR4    : Nodes, Trias,Quads=     16538     32437         0

AFLR4    : Generate optimal mesh on surface definition 23
AFLR2    : Nodes, Trias,Quads=        73       116         0
AFLR4    : Nodes, Trias,Quads=        68       106         0

AFLR4    : Generate optimal mesh on surface definition 24
AFLR2    : Nodes, Trias,Quads=        73       116         0
AFLR4    : Nodes, Trias,Quads=        68       106         0

AFLR4    : Generate optimal mesh on surface definition 25
AFLR2    : Nodes, Trias,Quads=        73       116         0
AFLR4    : Nodes, Trias,Quads=        68       106         0

AFLR4    : Generate optimal mesh on surface definition 26
AFLR2    : Nodes, Trias,Quads=        73       116         0
AFLR4    : Nodes, Trias,Quads=        68       106         0

AFLR4    : Generate optimal mesh on surface definition 27
AFLR2    : Nodes, Trias,Quads=        73       116         0
AFLR4    : Nodes, Trias,Quads=        68       106         0

AFLR4    : Generate optimal mesh on surface definition 28
AFLR2    : Nodes, Trias,Quads=        73       116         0
AFLR4    : Nodes, Trias,Quads=        68       106         0

DGEOM    : Add surface definitions to composite definition 0
DGEOM    : Glue composite surface definition 0
DGEOM    : Nodes,Faces,BEdges=    143960    287920      8370

AFLR4    : Curvature BG Surface Grid Generation

AFLR4    : Nodes, Faces      =    143960    287920

AFLR4    : Surface Grid Generation

AFLR4    : Generate optimal mesh on surface definition 1
AFLR2    : Nodes, Trias,Quads=       552      1002         0
AFLR4    : Nodes, Trias,Quads=       474       846         0

AFLR4    : Generate optimal mesh on surface definition 2
AFLR2    : Nodes, Trias,Quads=       803      1479         0
AFLR4    : Nodes, Trias,Quads=       727      1327         0

AFLR4    : Generate optimal mesh on surface definition 3
AFLR2    : Nodes, Trias,Quads=      8664     16826         0
AFLR4    : Nodes, Trias,Quads=      6539     12576         0

AFLR4    : Generate optimal mesh on surface definition 4
AFLR2    : Nodes, Trias,Quads=        94       149         0
AFLR4    : Nodes, Trias,Quads=        60        81         0

AFLR4    : Generate optimal mesh on surface definition 5
AFLR2    : Nodes, Trias,Quads=      9289     18022         0
AFLR4    : Nodes, Trias,Quads=      6959     13362         0

AFLR4    : Generate optimal mesh on surface definition 6
AFLR2    : Nodes, Trias,Quads=        92       145         0
AFLR4    : Nodes, Trias,Quads=        59        79         0

AFLR4    : Generate optimal mesh on surface definition 7
AFLR2    : Nodes, Trias,Quads=       375       660         0
AFLR4    : Nodes, Trias,Quads=       275       460         0

AFLR4    : Generate optimal mesh on surface definition 8
AFLR2    : Nodes, Trias,Quads=       386       681         0
AFLR4    : Nodes, Trias,Quads=       270       449         0

AFLR4    : Generate optimal mesh on surface definition 9
AFLR2    : Nodes, Trias,Quads=     13624     26478         0
AFLR4    : Nodes, Trias,Quads=      9963     19156         0

AFLR4    : Generate optimal mesh on surface definition 10
AFLR2    : Nodes, Trias,Quads=         5         4         0
AFLR4    : Nodes, Trias,Quads=         4         2         0

AFLR4    : Generate optimal mesh on surface definition 11
AFLR2    : Nodes, Trias,Quads=     13541     26314         0
AFLR4    : Nodes, Trias,Quads=      9963     19158         0

AFLR4    : Generate optimal mesh on surface definition 12
AFLR2    : Nodes, Trias,Quads=       573      1036         0
AFLR4    : Nodes, Trias,Quads=       363       616         0

AFLR4    : Generate optimal mesh on surface definition 13
AFLR2    : Nodes, Trias,Quads=       580      1049         0
AFLR4    : Nodes, Trias,Quads=       370       629         0

AFLR4    : Generate optimal mesh on surface definition 14
AFLR2    : Nodes, Trias,Quads=     15123     29666         0
AFLR4    : Nodes, Trias,Quads=     14640     28700         0

AFLR4    : Generate optimal mesh on surface definition 15
AFLR2    : Nodes, Trias,Quads=     15402     30224         0
AFLR4    : Nodes, Trias,Quads=     14606     28632         0

AFLR4    : Generate optimal mesh on surface definition 16
AFLR2    : Nodes, Trias,Quads=        60        79         0
AFLR4    : Nodes, Trias,Quads=        49        57         0

AFLR4    : Generate optimal mesh on surface definition 17
AFLR2    : Nodes, Trias,Quads=     15284     29986         0
AFLR4    : Nodes, Trias,Quads=     14698     28814         0

AFLR4    : Generate optimal mesh on surface definition 18
AFLR2    : Nodes, Trias,Quads=     15598     30614         0
AFLR4    : Nodes, Trias,Quads=     14616     28650         0

AFLR4    : Generate optimal mesh on surface definition 19
AFLR2    : Nodes, Trias,Quads=     18664     36687         0
AFLR4    : Nodes, Trias,Quads=     16684     32727         0

AFLR4    : Generate optimal mesh on surface definition 20
AFLR2    : Nodes, Trias,Quads=     18711     36781         0
AFLR4    : Nodes, Trias,Quads=     16625     32609         0

AFLR4    : Generate optimal mesh on surface definition 21
AFLR2    : Nodes, Trias,Quads=     18664     36687         0
AFLR4    : Nodes, Trias,Quads=     16684     32727         0

AFLR4    : Generate optimal mesh on surface definition 22
AFLR2    : Nodes, Trias,Quads=     18712     36783         0
AFLR4    : Nodes, Trias,Quads=     16612     32583         0

AFLR4    : Generate optimal mesh on surface definition 23
AFLR2    : Nodes, Trias,Quads=        73       116         0
AFLR4    : Nodes, Trias,Quads=        68       106         0

AFLR4    : Generate optimal mesh on surface definition 24
AFLR2    : Nodes, Trias,Quads=        73       116         0
AFLR4    : Nodes, Trias,Quads=        68       106         0

AFLR4    : Generate optimal mesh on surface definition 25
AFLR2    : Nodes, Trias,Quads=        73       116         0
AFLR4    : Nodes, Trias,Quads=        68       106         0

AFLR4    : Generate optimal mesh on surface definition 26
AFLR2    : Nodes, Trias,Quads=        73       116         0
AFLR4    : Nodes, Trias,Quads=        68       106         0

AFLR4    : Generate optimal mesh on surface definition 27
AFLR2    : Nodes, Trias,Quads=        73       116         0
AFLR4    : Nodes, Trias,Quads=        68       106         0

AFLR4    : Generate optimal mesh on surface definition 28
AFLR2    : Nodes, Trias,Quads=        73       116         0
AFLR4    : Nodes, Trias,Quads=        68       106         0

DGEOM    : Add surface definitions to composite definition 0
DGEOM    : Glue composite surface definition 0
DGEOM    : Nodes,Faces,BEdges=    157438    314876      8368

AFLR4    : Proximity BG Surface Grid Generation

AFLR4    : Nodes, Trias      =    159278    318556
AFLR4    : Nodes, Trias      =    159698    319396

AFLR4    : Surface Grid Generation

AFLR4    : Generate optimal mesh on surface definition 1
AFLR2    : Nodes, Trias,Quads=      1086      2020         0
AFLR4    : Nodes, Trias,Quads=       962      1772         0

AFLR4    : Generate optimal mesh on surface definition 2
AFLR2    : Nodes, Trias,Quads=      2773      5270         0
AFLR4    : Nodes, Trias,Quads=      2793      5310         0

AFLR4    : Generate optimal mesh on surface definition 3
AFLR2    : Nodes, Trias,Quads=      8880     17250         0
AFLR4    : Nodes, Trias,Quads=      7147     13784         0

AFLR4    : Generate optimal mesh on surface definition 4
AFLR2    : Nodes, Trias,Quads=       184       310         0
AFLR4    : Nodes, Trias,Quads=       138       218         0

AFLR4    : Generate optimal mesh on surface definition 5
AFLR2    : Nodes, Trias,Quads=     16222     31763         0
AFLR4    : Nodes, Trias,Quads=      9485     18289         0

AFLR4    : Generate optimal mesh on surface definition 6
AFLR2    : Nodes, Trias,Quads=       232       397         0
AFLR4    : Nodes, Trias,Quads=       221       375         0

AFLR4    : Generate optimal mesh on surface definition 7
AFLR2    : Nodes, Trias,Quads=      1413      2643         0
AFLR4    : Nodes, Trias,Quads=       911      1639         0

AFLR4    : Generate optimal mesh on surface definition 8
AFLR2    : Nodes, Trias,Quads=      1587      2978         0
AFLR4    : Nodes, Trias,Quads=      1002      1808         0

AFLR4    : Generate optimal mesh on surface definition 9
AFLR2    : Nodes, Trias,Quads=     15659     30521         0
AFLR4    : Nodes, Trias,Quads=     11061     21325         0

AFLR4    : Generate optimal mesh on surface definition 10
AFLR2    : Nodes, Trias,Quads=         5         4         0
AFLR4    : Nodes, Trias,Quads=         4         2         0

AFLR4    : Generate optimal mesh on surface definition 11
AFLR2    : Nodes, Trias,Quads=     15529     30262         0
AFLR4    : Nodes, Trias,Quads=     11050     21304         0

AFLR4    : Generate optimal mesh on surface definition 12
AFLR2    : Nodes, Trias,Quads=      2345      4452         0
AFLR4    : Nodes, Trias,Quads=      1526      2814         0

AFLR4    : Generate optimal mesh on surface definition 13
AFLR2    : Nodes, Trias,Quads=      2241      4252         0
AFLR4    : Nodes, Trias,Quads=      1462      2694         0

AFLR4    : Generate optimal mesh on surface definition 14
AFLR2    : Nodes, Trias,Quads=     17583     34542         0
AFLR4    : Nodes, Trias,Quads=     14782     28940         0

AFLR4    : Generate optimal mesh on surface definition 15
AFLR2    : Nodes, Trias,Quads=     17575     34524         0
AFLR4    : Nodes, Trias,Quads=     14759     28892         0

AFLR4    : Generate optimal mesh on surface definition 16
AFLR2    : Nodes, Trias,Quads=        61        80         0
AFLR4    : Nodes, Trias,Quads=        50        58         0

AFLR4    : Generate optimal mesh on surface definition 17
AFLR2    : Nodes, Trias,Quads=     19924     39212         0
AFLR4    : Nodes, Trias,Quads=     14954     29272         0

AFLR4    : Generate optimal mesh on surface definition 18
AFLR2    : Nodes, Trias,Quads=     18844     37054         0
AFLR4    : Nodes, Trias,Quads=     14853     29072         0

AFLR4    : Generate optimal mesh on surface definition 19
AFLR2    : Nodes, Trias,Quads=     18691     36736         0
AFLR4    : Nodes, Trias,Quads=     16527     32408         0

AFLR4    : Generate optimal mesh on surface definition 20
AFLR2    : Nodes, Trias,Quads=     18718     36790         0
AFLR4    : Nodes, Trias,Quads=     16525     32404         0

AFLR4    : Generate optimal mesh on surface definition 21
AFLR2    : Nodes, Trias,Quads=     18691     36736         0
AFLR4    : Nodes, Trias,Quads=     16527     32408         0

AFLR4    : Generate optimal mesh on surface definition 22
AFLR2    : Nodes, Trias,Quads=     18709     36772         0
AFLR4    : Nodes, Trias,Quads=     16535     32424         0

AFLR4    : Generate optimal mesh on surface definition 23
AFLR2    : Nodes, Trias,Quads=        73       116         0
AFLR4    : Nodes, Trias,Quads=        68       106         0

AFLR4    : Generate optimal mesh on surface definition 24
AFLR2    : Nodes, Trias,Quads=        73       116         0
AFLR4    : Nodes, Trias,Quads=        68       106         0

AFLR4    : Generate optimal mesh on surface definition 25
AFLR2    : Nodes, Trias,Quads=        73       116         0
AFLR4    : Nodes, Trias,Quads=        68       106         0

AFLR4    : Generate optimal mesh on surface definition 26
AFLR2    : Nodes, Trias,Quads=        73       116         0
AFLR4    : Nodes, Trias,Quads=        68       106         0

AFLR4    : Generate optimal mesh on surface definition 27
AFLR2    : Nodes, Trias,Quads=        73       116         0
AFLR4    : Nodes, Trias,Quads=        68       106         0

AFLR4    : Generate optimal mesh on surface definition 28
AFLR2    : Nodes, Trias,Quads=        73       116         0
AFLR4    : Nodes, Trias,Quads=        68       106         0

DGEOM    : Add surface definitions to composite definition 0
DGEOM    : Glue composite surface definition 0
DGEOM    : Nodes,Faces,BEdges=    168924    337848      9464

OVERALL  : CPU Time          =     6.153   seconds
Body 1 (of 2)
Number of nodes    = 168604
Number of elements = 337212
Number of triangle elements      = 337212
Number of quadrilateral elements = 0
Body 2 (of 2)
Number of nodes    = 320
Number of elements = 636
Number of triangle elements      = 636
Number of quadrilateral elements = 0
----------------------------
Total number of nodes    = 168924
Total number of elements = 337848
Total number of triangle elements      = 337848
Total number of quadrilateral elements = 0

real	0m11.632s
user	0m13.473s
sys	0m1.775s
+ status=0
+ set +x

=================================================
data/session07/07_aflr4_ProximityComponents.py passed (as expected)
=================================================


=================================================
08_aflr4_InviscidTransport.py test;
+ python 08_aflr4_InviscidTransport.py
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/CAPS/training/2023/training.log

MESSAGE:: Building wingOml


MESSAGE:: Building wingHinges


MESSAGE:: Building nacelleOml


MESSAGE:: Building htailOml


MESSAGE:: Building htailHinges


MESSAGE:: Building vtailOml


MESSAGE:: Building vtailHinges


MESSAGE:: Building fuseOml

Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 6
	Name = Nacelle, index = 1
	Name = Vtail, index = 2
	Name = Htail, index = 3
	Name = Fuselage, index = 4
	Name = Wing, index = 5
	Name = Farfield, index = 6
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 7
	Name = Nacelle, index = 1
	Name = Vtail, index = 2
	Name = Htail, index = 3
	Name = Fuselage, index = 4
	Name = riteWing, index = 5
	Name = leftWing, index = 6
	Name = Farfield, index = 7

Getting mesh sizing parameters
	Mesh sizing name - Farfield
	Mesh sizing name - Htail
	Mesh sizing name - Nacelle
	Mesh sizing name - Vtail
	Mesh sizing name - leftWing
	Mesh sizing name - riteWing
	Done getting mesh sizing parameters
 
AFLR2    : ---------------------------------------
AFLR2    : AFLR2 LIBRARY
AFLR2    : ADVANCING-FRONT/LOCAL-RECONNECTION
AFLR2    : TRIA/QUAD GRID GENERATOR
AFLR2    : Version Number 9.18.1
AFLR2    : Version Date   06/11/24 @ 05:52PM
AFLR2    : Compile OS     Darwin 23.5.0 arm64
AFLR2    : Compile Date   06/11/24 @ 05:52PM
AFLR2    : Copyright 1994-2021, D.L. Marcum
AFLR2    : ---------------------------------------
 
AFLR4    : ---------------------------------------
AFLR4    : AFLR4 LIBRARY
AFLR4    : ADVANCING-FRONT/LOCAL-RECONNECTION
AFLR4    : TRIA/QUAD SURFACE GRID GENERATOR
AFLR4    : Version Number 11.5.15
AFLR4    : Version Date   07/19/24 @ 07:04PM
AFLR4    : Compile OS     Darwin 23.5.0 arm64
AFLR4    : Compile Date   07/19/24 @ 07:06PM
AFLR4    : Copyright 1994-2021, D.L. Marcum
AFLR4    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.8.1
EGADS    : ---------------------------------------

EGADS    : EGADS CAD Geometry Setup

EGADS    : Model has 4 Active Bodies

EGADS    : Body 0 is a SolidBody
EGADS    : Body 0 has 1 Shells
EGADS    : Body 0 has 4 Faces
EGADS    : Body 0 has 8 Edges
EGADS    : Body 0 has 4 Loops
EGADS    : Body 0 has 4 Nodes
EGADS    : Body 1 is a SolidBody
EGADS    : Body 1 has 1 Shells
EGADS    : Body 1 has 4 Faces
EGADS    : Body 1 has 8 Edges
EGADS    : Body 1 has 4 Loops
EGADS    : Body 1 has 4 Nodes
EGADS    : Body 2 is a SolidBody
EGADS    : Body 2 has 1 Shells
EGADS    : Body 2 has 100 Faces
EGADS    : Body 2 has 245 Edges
EGADS    : Body 2 has 102 Loops
EGADS    : Body 2 has 145 Nodes
EGADS    : Body 3 is a SolidBody
EGADS    : Body 3 has 1 Shells
EGADS    : Body 3 has 6 Faces
EGADS    : Body 3 has 12 Edges
EGADS    : Body 3 has 6 Loops
EGADS    : Body 3 has 8 Nodes

EGADS    : Check Grid BCs

EGADS    : Grid BCs are OK

EGADS    : Face Neighbor-Faces Information

EGADS    : QC  = Face Quad Combination Flag
EGADS    : IER = Face Isolated Edge Refinement Flag
EGADS    : ER  = Face Edge Refinement Factor
EGADS    :       Not applicable for Faces with a FarField Grid BC.
EGADS    : SF  = Face Scale Factor
EGADS    :       Not applicable for Faces with a FarField Grid BC.

EGADS    :   Face          Body    QC   IER       ER    Scale   Neighbor
EGADS    :     ID  Active    ID  Flag  Flag   Weight   Factor   Faces
EGADS    :      1     Yes     0     0     1        0        5   2 3
EGADS    :      2     Yes     0     0     1        0        5   1 4
EGADS    :      3     Yes     0     0     1        0        5   1 4
EGADS    :      4     Yes     0     0     1        0        5   2 3
EGADS    :      5     Yes     1     0     1        0        5   6 7
EGADS    :      6     Yes     1     0     1        0        5   5 8
EGADS    :      7     Yes     1     0     1        0        5   5 8
EGADS    :      8     Yes     1     0     1        0        5   6 7
EGADS    :      9     Yes     2     0     1        0        4   10 14 32 107
EGADS    :     10     Yes     2     0     1        0        4   9 11 39 108
EGADS    :     11     Yes     2     0     1        0        4   10 12 39 108
EGADS    :     12     Yes     2     0     1        0        4   11 13 39 108
EGADS    :     13     Yes     2     0     1        0        4   12 14 32 107
EGADS    :     14     Yes     2     0     1        0        4   9 13 32 107
EGADS    :     15     Yes     2     0     1        0        4   16 17 18 19
EGADS    :     16     Yes     2     0     1        0        4   15 17 20 21 22
EGADS    :                                                      23 24
EGADS    :     17     Yes     2     0     1        0        4   15 16 18 22
EGADS    :     18     Yes     2     0     1        0        4   15 17 22 25
EGADS    :     19     Yes     2     0     1        0        4   15 20 25 26
EGADS    :     20     Yes     2     0     1        0        4   16 19 21 23 24
EGADS    :                                                      26 27
EGADS    :     21     Yes     2     0     1        0        4   16 20
EGADS    :     22     Yes     2     0     1        0        4   16 17 18 27
EGADS    :     23     Yes     2     0     1        0        1   16 20 24 28 29
EGADS    :                                                      30
EGADS    :     24     Yes     2     0     1        0        1   16 20 23 29 31
EGADS    :                                                      32 33
EGADS    :     25     Yes     2     0     1        0        4   18 19 26 27
EGADS    :     26     Yes     2     0     1        0        4   19 20 25 27
EGADS    :     27     Yes     2     0     1        0        4   20 22 25 26
EGADS    :     28     Yes     2     0     1        0        1   23 29 31 34 35
EGADS    :                                                      36
EGADS    :     29     Yes     2     0     1        0        1   23 24 28 31
EGADS    :     30     Yes     2     0     1        0        1   23 33 36 37 38
EGADS    :     31     Yes     2     0     1        0        1   24 28 29 34 35
EGADS    :                                                      39 40
EGADS    :     32     Yes     2     0     1        0        4   9 13 14 24 39 41
EGADS    :     33     Yes     2     0     1        0        1   24 30 40
EGADS    :     34     Yes     2     0     1        0        4   28 31 35 42 43
EGADS    :                                                      44 45
EGADS    :     35     Yes     2     0     1        0        4   28 31 34 42 46
EGADS    :                                                      47 48
EGADS    :     36     Yes     2     0     1        0        1   28 30 40 49 50
EGADS    :     37     Yes     2     0     1        0        4   30 38 51 52 53
EGADS    :                                                      54
EGADS    :     38     Yes     2     0     1        0        4   30 37 55 56 57
EGADS    :                                                      58
EGADS    :     39     Yes     2     0     1        0        4   10 11 12 31 32
EGADS    :                                                      41
EGADS    :     40     Yes     2     0     1        0        1   31 33 36
EGADS    :     41     Yes     2     0     1        0        4   32 39
EGADS    :     42     Yes     2     0     1        0        4   34 35
EGADS    :     43     Yes     2     0     1        0        4   34 44 48 59
EGADS    :     44     Yes     2     0     1        0        4   34 43 45 59
EGADS    :     45     Yes     2     0     1        0        4   34 44 46 59
EGADS    :     46     Yes     2     0     1        0        4   35 45 47 60
EGADS    :     47     Yes     2     0     1        0        4   35 46 48 60
EGADS    :     48     Yes     2     0     1        0        4   35 43 47 60
EGADS    :     49     Yes     2     0     1        0        4   36 50 61 62 63
EGADS    :                                                      64
EGADS    :     50     Yes     2     0     1        0        4   36 49 65 66 67
EGADS    :                                                      68
EGADS    :     51     Yes     2     0     1        0        4   37 52 58 69
EGADS    :     52     Yes     2     0     1        0        4   37 51 53 69
EGADS    :     53     Yes     2     0     1        0        4   37 52 56 69
EGADS    :     54     Yes     2     0     1        0        4   37 55 70 71 72
EGADS    :                                                      73 74 75 76
EGADS    :     55     Yes     2     0     1        0        4   38 54 76 77 78
EGADS    :                                                      79 80 81 82
EGADS    :     56     Yes     2     0     1        0        4   38 53 57 83
EGADS    :     57     Yes     2     0     1        0        4   38 56 58 83
EGADS    :     58     Yes     2     0     1        0        4   38 51 57 83
EGADS    :     59     Yes     2     0     1        0        4   43 44 45 60
EGADS    :     60     Yes     2     0     1        0        4   46 47 48 59
EGADS    :     61     Yes     2     0     1        0        4   49 68 84 85 86
EGADS    :                                                      87 88 89 90
EGADS    :     62     Yes     2     0     1        0        4   49 63 67 91
EGADS    :     63     Yes     2     0     1        0        4   49 62 64 91
EGADS    :     64     Yes     2     0     1        0        4   49 63 65 91
EGADS    :     65     Yes     2     0     1        0        4   50 64 66 92
EGADS    :     66     Yes     2     0     1        0        4   50 65 67 92
EGADS    :     67     Yes     2     0     1        0        4   50 62 66 92
EGADS    :     68     Yes     2     0     1        0        4   50 61 84 93 94
EGADS    :                                                      95 96 97 98
EGADS    :     69     Yes     2     0     1        0        4   51 52 53 83
EGADS    :     70     Yes     2     0     1        0        4   54 71 82 99
EGADS    :     71     Yes     2     0     1        0        4   54 70 72 99
EGADS    :     72     Yes     2     0     1        0        4   54 71 80 99
EGADS    :     73     Yes     2     0     1        0        4   54 74 79 100
EGADS    :     74     Yes     2     0     1        0        4   54 73 75 100
EGADS    :     75     Yes     2     0     1        0        4   54 74 77 100
EGADS    :     76     Yes     2     0     1        0        4   54 55
EGADS    :     77     Yes     2     0     1        0        4   55 75 78 101
EGADS    :     78     Yes     2     0     1        0        4   55 77 79 101
EGADS    :     79     Yes     2     0     1        0        4   55 73 78 101
EGADS    :     80     Yes     2     0     1        0        4   55 72 81 102
EGADS    :     81     Yes     2     0     1        0        4   55 80 82 102
EGADS    :     82     Yes     2     0     1        0        4   55 70 81 102
EGADS    :     83     Yes     2     0     1        0        4   56 57 58 69
EGADS    :     84     Yes     2     0     1        0        4   61 68
EGADS    :     85     Yes     2     0     1        0        4   61 86 98 103
EGADS    :     86     Yes     2     0     1        0        4   61 85 87 103
EGADS    :     87     Yes     2     0     1        0        4   61 86 96 103
EGADS    :     88     Yes     2     0     1        0        4   61 89 95 104
EGADS    :     89     Yes     2     0     1        0        4   61 88 90 104
EGADS    :     90     Yes     2     0     1        0        4   61 89 93 104
EGADS    :     91     Yes     2     0     1        0        4   62 63 64 92
EGADS    :     92     Yes     2     0     1        0        4   65 66 67 91
EGADS    :     93     Yes     2     0     1        0        4   68 90 94 105
EGADS    :     94     Yes     2     0     1        0        4   68 93 95 105
EGADS    :     95     Yes     2     0     1        0        4   68 88 94 105
EGADS    :     96     Yes     2     0     1        0        4   68 87 97 106
EGADS    :     97     Yes     2     0     1        0        4   68 96 98 106
EGADS    :     98     Yes     2     0     1        0        4   68 85 97 106
EGADS    :     99     Yes     2     0     1        0        4   70 71 72 102
EGADS    :    100     Yes     2     0     1        0        4   73 74 75 101
EGADS    :    101     Yes     2     0     1        0        4   77 78 79 100
EGADS    :    102     Yes     2     0     1        0        4   80 81 82 99
EGADS    :    103     Yes     2     0     1        0        4   85 86 87 106
EGADS    :    104     Yes     2     0     1        0        4   88 89 90 105
EGADS    :    105     Yes     2     0     1        0        4   93 94 95 104
EGADS    :    106     Yes     2     0     1        0        4   96 97 98 103
EGADS    :    107     Yes     2     0     1        0        4   9 13 14 108
EGADS    :    108     Yes     2     0     1        0        4   10 11 12 107
EGADS    :    109     Yes     3     0     1       NA       NA   111 112 113 114
EGADS    :    110     Yes     3     0     1       NA       NA   111 112 113 114
EGADS    :    111     Yes     3     0     1       NA       NA   109 110 113 114
EGADS    :    112     Yes     3     0     1       NA       NA   109 110 113 114
EGADS    :    113     Yes     3     0     1       NA       NA   109 110 111 112
EGADS    :    114     Yes     3     0     1       NA       NA   109 110 111 112

EGADS    : Face Edges Information

EGADS    :   Face   Edges
EGADS    :      1   -1 3 2 -4
EGADS    :      2   -2 5 1 -6
EGADS    :      3   7 4 -8 -3
EGADS    :      4   8 6 -7 -5
EGADS    :      5   9 12 -10 -11
EGADS    :      6   10 14 -9 -13
EGADS    :      7   -15 11 16 -12
EGADS    :      8   -16 13 15 -14
EGADS    :      9   -17 20 19 -18
EGADS    :     10   -21 18 23 -22
EGADS    :     11   -24 22 26 -25
EGADS    :     12   27 25 -28 -29
EGADS    :     13   30 29 -31 -32
EGADS    :     14   33 32 -34 -20
EGADS    :     15   35 36 -37 -38
EGADS    :     16   39 40 -41 42 -43 -35 -44 45 46
EGADS    :     17   43 47 -48 -36
EGADS    :     18   -49 37 48 -50
EGADS    :     19   51 38 -52 -53
EGADS    :     20   44 -51 54 55 41 56 -39 57 58
EGADS    :     21   -56 -40
EGADS    :     22   -42 59 50 -47
EGADS    :     23   -60 64 63 -45 -58 62 -61
EGADS    :     24   -63 69 68 67 66 -65 -62 -57 -46
EGADS    :     25   49 -70 -71 52
EGADS    :     26   -54 53 71 -72
EGADS    :     27   -55 72 70 -59
EGADS    :     28   -73 78 60 -77 -76 75 74
EGADS    :     29   61 65 79 77
EGADS    :     30   -80 82 81 -64 -83 -84
EGADS    :     31   -68 88 73 87 86 76 -79 -66 85
EGADS    :     32   -89 -67 92 -91 -90 -30 -33 17
EGADS    :     33   -81 93 94 -69
EGADS    :     34   -95 -87 -74 101 100 99 -98 97 -96
EGADS    :     35   -101 -75 -86 95 -105 -97 -104 -103 102
EGADS    :     36   -106 107 80 -78 108 109
EGADS    :     37   110 -111 112 113 114 115 -116 83
EGADS    :     38   116 117 -114 118 -119 -120 -110 84
EGADS    :     39   -92 -85 89 21 24 -27 90 -121
EGADS    :     40   -94 122 106 -88
EGADS    :     41   91 121
EGADS    :     42   105 96
EGADS    :     43   98 123 -124 -125
EGADS    :     44   -99 127 126 -123
EGADS    :     45   -100 129 128 -127
EGADS    :     46   -102 131 130 -129
EGADS    :     47   103 132 -133 -131
EGADS    :     48   104 125 -134 -132
EGADS    :     49   -135 -108 141 140 139 -138 137 -136
EGADS    :     50   -141 -109 135 -145 -137 -144 -143 142
EGADS    :     51   111 146 -147 -148
EGADS    :     52   -112 148 150 -149
EGADS    :     53   -113 149 152 -151
EGADS    :     54   153 -154 155 156 157 -158 159 160 161 162 -163 -115
EGADS    :     55   163 164 -161 165 -166 -167 -157 168 -169 -170 -153 -117
EGADS    :     56   -118 151 172 -171
EGADS    :     57   119 171 -173 -174
EGADS    :     58   120 174 -175 -146
EGADS    :     59   176 124 -126 -128
EGADS    :     60   -176 -130 133 134
EGADS    :     61   -177 136 187 186 185 -184 183 182 181 -180 179 -178
EGADS    :     62   138 188 -189 -190
EGADS    :     63   -139 192 191 -188
EGADS    :     64   -140 194 193 -192
EGADS    :     65   -142 196 195 -194
EGADS    :     66   143 197 -198 -196
EGADS    :     67   144 190 -199 -197
EGADS    :     68   -187 145 177 -206 -179 -205 -204 203 -183 -202 -201 200
EGADS    :     69   207 -152 -150 147
EGADS    :     70   154 208 -209 -210
EGADS    :     71   -155 210 212 -211
EGADS    :     72   -156 211 214 -213
EGADS    :     73   158 215 -216 -217
EGADS    :     74   -159 217 219 -218
EGADS    :     75   -160 218 221 -220
EGADS    :     76   -162 -164
EGADS    :     77   -165 220 223 -222
EGADS    :     78   166 222 -224 -225
EGADS    :     79   167 225 -226 -215
EGADS    :     80   -168 213 228 -227
EGADS    :     81   169 227 -229 -230
EGADS    :     82   170 230 -231 -208
EGADS    :     83   175 173 -172 -207
EGADS    :     84   206 178
EGADS    :     85   180 232 -233 -234
EGADS    :     86   -181 236 235 -232
EGADS    :     87   -182 238 237 -236
EGADS    :     88   184 239 -240 -241
EGADS    :     89   -185 243 242 -239
EGADS    :     90   -186 245 244 -243
EGADS    :     91   -193 246 189 -191
EGADS    :     92   -246 -195 198 199
EGADS    :     93   -200 248 247 -245
EGADS    :     94   201 249 -250 -248
EGADS    :     95   202 241 -251 -249
EGADS    :     96   -203 253 252 -238
EGADS    :     97   204 254 -255 -253
EGADS    :     98   205 234 -256 -254
EGADS    :     99   257 -214 -212 209
EGADS    :    100   -221 -219 216 258
EGADS    :    101   -258 226 224 -223
EGADS    :    102   231 229 -228 -257
EGADS    :    103   -237 259 233 -235
EGADS    :    104   -244 260 240 -242
EGADS    :    105   -260 -247 250 251
EGADS    :    106   -259 -252 255 256
EGADS    :    107   -261 -19 34 31
EGADS    :    108   -23 261 28 -26
EGADS    :    109   262 263 -264 -265
EGADS    :    110   -266 269 268 -267
EGADS    :    111   270 266 -271 -262
EGADS    :    112   -272 264 273 -268
EGADS    :    113   265 272 -269 -270
EGADS    :    114   -263 271 267 -273

EGADS    : Face Loops Information

EGADS    :   Face   Loops
EGADS    :      1   1
EGADS    :      2   2
EGADS    :      3   3
EGADS    :      4   4
EGADS    :      5   5
EGADS    :      6   6
EGADS    :      7   7
EGADS    :      8   8
EGADS    :      9   9
EGADS    :     10   10
EGADS    :     11   11
EGADS    :     12   12
EGADS    :     13   13
EGADS    :     14   14
EGADS    :     15   15
EGADS    :     16   16
EGADS    :     17   17
EGADS    :     18   18
EGADS    :     19   19
EGADS    :     20   20
EGADS    :     21   21
EGADS    :     22   22
EGADS    :     23   23
EGADS    :     24   24
EGADS    :     25   25
EGADS    :     26   26
EGADS    :     27   27
EGADS    :     28   28
EGADS    :     29   29
EGADS    :     30   30 31
EGADS    :     31   32
EGADS    :     32   33
EGADS    :     33   34
EGADS    :     34   35
EGADS    :     35   36
EGADS    :     36   37 38
EGADS    :     37   39
EGADS    :     38   40
EGADS    :     39   41
EGADS    :     40   42
EGADS    :     41   43
EGADS    :     42   44
EGADS    :     43   45
EGADS    :     44   46
EGADS    :     45   47
EGADS    :     46   48
EGADS    :     47   49
EGADS    :     48   50
EGADS    :     49   51
EGADS    :     50   52
EGADS    :     51   53
EGADS    :     52   54
EGADS    :     53   55
EGADS    :     54   56
EGADS    :     55   57
EGADS    :     56   58
EGADS    :     57   59
EGADS    :     58   60
EGADS    :     59   61
EGADS    :     60   62
EGADS    :     61   63
EGADS    :     62   64
EGADS    :     63   65
EGADS    :     64   66
EGADS    :     65   67
EGADS    :     66   68
EGADS    :     67   69
EGADS    :     68   70
EGADS    :     69   71
EGADS    :     70   72
EGADS    :     71   73
EGADS    :     72   74
EGADS    :     73   75
EGADS    :     74   76
EGADS    :     75   77
EGADS    :     76   78
EGADS    :     77   79
EGADS    :     78   80
EGADS    :     79   81
EGADS    :     80   82
EGADS    :     81   83
EGADS    :     82   84
EGADS    :     83   85
EGADS    :     84   86
EGADS    :     85   87
EGADS    :     86   88
EGADS    :     87   89
EGADS    :     88   90
EGADS    :     89   91
EGADS    :     90   92
EGADS    :     91   93
EGADS    :     92   94
EGADS    :     93   95
EGADS    :     94   96
EGADS    :     95   97
EGADS    :     96   98
EGADS    :     97   99
EGADS    :     98   100
EGADS    :     99   101
EGADS    :    100   102
EGADS    :    101   103
EGADS    :    102   104
EGADS    :    103   105
EGADS    :    104   106
EGADS    :    105   107
EGADS    :    106   108
EGADS    :    107   109
EGADS    :    108   110
EGADS    :    109   111
EGADS    :    110   112
EGADS    :    111   113
EGADS    :    112   114
EGADS    :    113   115
EGADS    :    114   116

EGADS    : Loop Edges Information

EGADS    :   Loop  Active   Edges
EGADS    :      1     Yes   -1 3 2 -4
EGADS    :      2     Yes   -2 5 1 -6
EGADS    :      3     Yes   7 4 -8 -3
EGADS    :      4     Yes   8 6 -7 -5
EGADS    :      5     Yes   9 12 -10 -11
EGADS    :      6     Yes   10 14 -9 -13
EGADS    :      7     Yes   -15 11 16 -12
EGADS    :      8     Yes   -16 13 15 -14
EGADS    :      9     Yes   -17 20 19 -18
EGADS    :     10     Yes   -21 18 23 -22
EGADS    :     11     Yes   -24 22 26 -25
EGADS    :     12     Yes   27 25 -28 -29
EGADS    :     13     Yes   30 29 -31 -32
EGADS    :     14     Yes   33 32 -34 -20
EGADS    :     15     Yes   35 36 -37 -38
EGADS    :     16     Yes   39 40 -41 42 -43 -35 -44 45 46
EGADS    :     17     Yes   43 47 -48 -36
EGADS    :     18     Yes   -49 37 48 -50
EGADS    :     19     Yes   51 38 -52 -53
EGADS    :     20     Yes   44 -51 54 55 41 56 -39 57 58
EGADS    :     21     Yes   -56 -40
EGADS    :     22     Yes   -42 59 50 -47
EGADS    :     23     Yes   -60 64 63 -45 -58 62 -61
EGADS    :     24     Yes   -63 69 68 67 66 -65 -62 -57 -46
EGADS    :     25     Yes   49 -70 -71 52
EGADS    :     26     Yes   -54 53 71 -72
EGADS    :     27     Yes   -55 72 70 -59
EGADS    :     28     Yes   -73 78 60 -77 -76 75 74
EGADS    :     29     Yes   61 65 79 77
EGADS    :     30     Yes   -80 82 81 -64
EGADS    :     31     Yes   -83 -84
EGADS    :     32     Yes   -68 88 73 87 86 76 -79 -66 85
EGADS    :     33     Yes   -89 -67 92 -91 -90 -30 -33 17
EGADS    :     34     Yes   -81 93 94 -69
EGADS    :     35     Yes   -95 -87 -74 101 100 99 -98 97 -96
EGADS    :     36     Yes   -101 -75 -86 95 -105 -97 -104 -103 102
EGADS    :     37     Yes   -106 107 80 -78
EGADS    :     38     Yes   108 109
EGADS    :     39     Yes   110 -111 112 113 114 115 -116 83
EGADS    :     40     Yes   116 117 -114 118 -119 -120 -110 84
EGADS    :     41     Yes   -92 -85 89 21 24 -27 90 -121
EGADS    :     42     Yes   -94 122 106 -88
EGADS    :     43     Yes   91 121
EGADS    :     44     Yes   105 96
EGADS    :     45     Yes   98 123 -124 -125
EGADS    :     46     Yes   -99 127 126 -123
EGADS    :     47     Yes   -100 129 128 -127
EGADS    :     48     Yes   -102 131 130 -129
EGADS    :     49     Yes   103 132 -133 -131
EGADS    :     50     Yes   104 125 -134 -132
EGADS    :     51     Yes   -135 -108 141 140 139 -138 137 -136
EGADS    :     52     Yes   -141 -109 135 -145 -137 -144 -143 142
EGADS    :     53     Yes   111 146 -147 -148
EGADS    :     54     Yes   -112 148 150 -149
EGADS    :     55     Yes   -113 149 152 -151
EGADS    :     56     Yes   153 -154 155 156 157 -158 159 160 161 162 -163 -115
EGADS    :     57     Yes   163 164 -161 165 -166 -167 -157 168 -169 -170 -153
EGADS    :                        -117
EGADS    :     58     Yes   -118 151 172 -171
EGADS    :     59     Yes   119 171 -173 -174
EGADS    :     60     Yes   120 174 -175 -146
EGADS    :     61     Yes   176 124 -126 -128
EGADS    :     62     Yes   -176 -130 133 134
EGADS    :     63     Yes   -177 136 187 186 185 -184 183 182 181 -180 179 -178
EGADS    :     64     Yes   138 188 -189 -190
EGADS    :     65     Yes   -139 192 191 -188
EGADS    :     66     Yes   -140 194 193 -192
EGADS    :     67     Yes   -142 196 195 -194
EGADS    :     68     Yes   143 197 -198 -196
EGADS    :     69     Yes   144 190 -199 -197
EGADS    :     70     Yes   -187 145 177 -206 -179 -205 -204 203 -183 -202 -201
EGADS    :                        200
EGADS    :     71     Yes   207 -152 -150 147
EGADS    :     72     Yes   154 208 -209 -210
EGADS    :     73     Yes   -155 210 212 -211
EGADS    :     74     Yes   -156 211 214 -213
EGADS    :     75     Yes   158 215 -216 -217
EGADS    :     76     Yes   -159 217 219 -218
EGADS    :     77     Yes   -160 218 221 -220
EGADS    :     78     Yes   -162 -164
EGADS    :     79     Yes   -165 220 223 -222
EGADS    :     80     Yes   166 222 -224 -225
EGADS    :     81     Yes   167 225 -226 -215
EGADS    :     82     Yes   -168 213 228 -227
EGADS    :     83     Yes   169 227 -229 -230
EGADS    :     84     Yes   170 230 -231 -208
EGADS    :     85     Yes   175 173 -172 -207
EGADS    :     86     Yes   206 178
EGADS    :     87     Yes   180 232 -233 -234
EGADS    :     88     Yes   -181 236 235 -232
EGADS    :     89     Yes   -182 238 237 -236
EGADS    :     90     Yes   184 239 -240 -241
EGADS    :     91     Yes   -185 243 242 -239
EGADS    :     92     Yes   -186 245 244 -243
EGADS    :     93     Yes   -193 246 189 -191
EGADS    :     94     Yes   -246 -195 198 199
EGADS    :     95     Yes   -200 248 247 -245
EGADS    :     96     Yes   201 249 -250 -248
EGADS    :     97     Yes   202 241 -251 -249
EGADS    :     98     Yes   -203 253 252 -238
EGADS    :     99     Yes   204 254 -255 -253
EGADS    :    100     Yes   205 234 -256 -254
EGADS    :    101     Yes   257 -214 -212 209
EGADS    :    102     Yes   -221 -219 216 258
EGADS    :    103     Yes   -258 226 224 -223
EGADS    :    104     Yes   231 229 -228 -257
EGADS    :    105     Yes   -237 259 233 -235
EGADS    :    106     Yes   -244 260 240 -242
EGADS    :    107     Yes   -260 -247 250 251
EGADS    :    108     Yes   -259 -252 255 256
EGADS    :    109     Yes   -261 -19 34 31
EGADS    :    110     Yes   -23 261 28 -26
EGADS    :    111     Yes   262 263 -264 -265
EGADS    :    112     Yes   -266 269 268 -267
EGADS    :    113     Yes   270 266 -271 -262
EGADS    :    114     Yes   -272 264 273 -268
EGADS    :    115     Yes   265 272 -269 -270
EGADS    :    116     Yes   -263 271 267 -273

EGADS    : Edge Node, Scale Factor, and Neighbor-Faces Information

EGADS    : ESF = Edge Scale Factor
EGADS    :       Not applicable for DEGENERATE Edges or Edges with a FarField
EGADS    :       Grid BC Neighbor Face.

EGADS    :                                             Neighbor
EGADS    :   Edge  Body  Active Node1 Node2      ESF   Faces
EGADS    :      1     0     Yes     1     2        1   1 2
EGADS    :      2     0     Yes     3     4        1   1 2
EGADS    :      3     0     Yes     1     3        1   1 3
EGADS    :      4     0     Yes     2     4        1   1 3
EGADS    :      5     0     Yes     3     1        1   2 4
EGADS    :      6     0     Yes     4     2        1   2 4
EGADS    :      7     0     Yes     1     2        1   3 4
EGADS    :      8     0     Yes     3     4        1   3 4
EGADS    :      9     1     Yes     5     6        1   5 6
EGADS    :     10     1     Yes     7     8        1   5 6
EGADS    :     11     1     Yes     5     7        1   5 7
EGADS    :     12     1     Yes     6     8        1   5 7
EGADS    :     13     1     Yes     7     5        1   6 8
EGADS    :     14     1     Yes     8     6        1   6 8
EGADS    :     15     1     Yes     5     6        1   7 8
EGADS    :     16     1     Yes     7     8        1   7 8
EGADS    :     17     2     Yes     9    10        1   9 32
EGADS    :     18     2     Yes    10    11        1   9 10
EGADS    :     19     2     Yes    12    11        1   9 107
EGADS    :     20     2     Yes     9    12        1   9 14
EGADS    :     21     2     Yes    10    13        1   10 39
EGADS    :     22     2     Yes    13    14        1   10 11
EGADS    :     23     2     Yes    11    14        1   10 108
EGADS    :     24     2     Yes    13    15        1   11 39
EGADS    :     25     2     Yes    15    16        1   11 12
EGADS    :     26     2     Yes    14    16        1   11 108
EGADS    :     27     2     Yes    17    15        1   12 39
EGADS    :     28     2     Yes    18    16        1   12 108
EGADS    :     29     2     Yes    17    18        1   12 13
EGADS    :     30     2     Yes    19    17        1   13 32
EGADS    :     31     2     Yes    20    18        1   13 107
EGADS    :     32     2     Yes    19    20        1   13 14
EGADS    :     33     2     Yes     9    19        1   14 32
EGADS    :     34     2     Yes    12    20        1   14 107
EGADS    :     35     2     Yes    21    22        1   15 16
EGADS    :     36     2     Yes    22    23        1   15 17
EGADS    :     37     2     Yes    24    23        1   15 18
EGADS    :     38     2     Yes    21    24        1   15 19
EGADS    :     39     2     Yes    25    26        1   16 20
EGADS    :     40     2     Yes    26    27        1   16 21
EGADS    :     41     2     Yes    28    27        1   16 20
EGADS    :     42     2     Yes    28    29        1   16 22
EGADS    :     43     2     Yes    22    29        1   16 17
EGADS    :     44     2     Yes    30    21        1   16 20
EGADS    :     45     2     Yes    30    31        1   16 23
EGADS    :     46     2     Yes    31    25        1   16 24
EGADS    :     47     2     Yes    29    32        1   17 22
EGADS    :     48     2     Yes    23    32        1   17 18
EGADS    :     49     2     Yes    24    33        1   18 25
EGADS    :     50     2     Yes    33    32        1   18 22
EGADS    :     51     2     Yes    34    21        1   19 20
EGADS    :     52     2     Yes    35    24        1   19 25
EGADS    :     53     2     Yes    34    35        1   19 26
EGADS    :     54     2     Yes    34    36        1   20 26
EGADS    :     55     2     Yes    36    28        1   20 27
EGADS    :     56     2     Yes    27    26        1   20 21
EGADS    :     57     2     Yes    25    37        1   20 24
EGADS    :     58     2     Yes    37    30        1   20 23
EGADS    :     59     2     Yes    28    33        1   22 27
EGADS    :     60     2     Yes    38    39        1   23 28
EGADS    :     61     2     Yes    39    40        1   23 29
EGADS    :     62     2     Yes    37    40        1   23 24
EGADS    :     63     2     Yes    41    31        1   23 24
EGADS    :     64     2     Yes    38    41        1   23 30
EGADS    :     65     2     Yes    40    42        1   24 29
EGADS    :     66     2     Yes    43    42        1   24 31
EGADS    :     67     2     Yes    44    43        1   24 32
EGADS    :     68     2     Yes    45    44        1   24 31
EGADS    :     69     2     Yes    41    45        1   24 33
EGADS    :     70     2     Yes    46    33        1   25 27
EGADS    :     71     2     Yes    35    46        1   25 26
EGADS    :     72     2     Yes    36    46        1   26 27
EGADS    :     73     2     Yes    47    48        1   28 31
EGADS    :     74     2     Yes    49    48        1   28 34
EGADS    :     75     2     Yes    50    49        1   28 35
EGADS    :     76     2     Yes    50    51        1   28 31
EGADS    :     77     2     Yes    51    39        1   28 29
EGADS    :     78     2     Yes    47    38        1   28 36
EGADS    :     79     2     Yes    42    51        1   29 31
EGADS    :     80     2     Yes    52    38        1   30 36
EGADS    :     81     2     Yes    52    41        1   30 33
EGADS    :     82     2   DEGEN    52    52        -   30
EGADS    :     83     2     Yes    53    54        1   30 37
EGADS    :     84     2     Yes    54    53        1   30 38
EGADS    :     85     2     Yes    43    44        1   31 39
EGADS    :     86     2     Yes    55    50        1   31 35
EGADS    :     87     2     Yes    48    55        1   31 34
EGADS    :     88     2     Yes    45    47        1   31 40
EGADS    :     89     2     Yes    43    10        1   32 39
EGADS    :     90     2     Yes    17    56        1   32 39
EGADS    :     91     2     Yes    56    57        1   32 41
EGADS    :     92     2     Yes    44    57        1   32 39
EGADS    :     93     2   DEGEN    52    52        -   33
EGADS    :     94     2     Yes    52    45        1   33 40
EGADS    :     95     2     Yes    55    58        1   34 35
EGADS    :     96     2     Yes    58    59        1   34 42
EGADS    :     97     2     Yes    60    59        1   34 35
EGADS    :     98     2     Yes    60    61        1   34 43
EGADS    :     99     2     Yes    62    61        1   34 44
EGADS    :    100     2     Yes    63    62        1   34 45
EGADS    :    101     2     Yes    49    63        1   34 35
EGADS    :    102     2     Yes    64    63        1   35 46
EGADS    :    103     2     Yes    64    65        1   35 47
EGADS    :    104     2     Yes    65    60        1   35 48
EGADS    :    105     2     Yes    59    58        1   35 42
EGADS    :    106     2     Yes    52    47        1   36 40
EGADS    :    107     2   DEGEN    52    52        -   36
EGADS    :    108     2     Yes    66    67        1   36 49
EGADS    :    109     2     Yes    67    66        1   36 50
EGADS    :    110     2     Yes    54    68        1   37 38
EGADS    :    111     2     Yes    69    68        1   37 51
EGADS    :    112     2     Yes    69    70        1   37 52
EGADS    :    113     2     Yes    70    71        1   37 53
EGADS    :    114     2     Yes    71    72        1   37 38
EGADS    :    115     2     Yes    72    73        1   37 54
EGADS    :    116     2     Yes    53    73        1   37 38
EGADS    :    117     2     Yes    73    72        1   38 55
EGADS    :    118     2     Yes    71    74        1   38 56
EGADS    :    119     2     Yes    75    74        1   38 57
EGADS    :    120     2     Yes    68    75        1   38 58
EGADS    :    121     2     Yes    57    56        1   39 41
EGADS    :    122     2   DEGEN    52    52        -   40
EGADS    :    123     2     Yes    61    76        1   43 44
EGADS    :    124     2     Yes    77    76        1   43 59
EGADS    :    125     2     Yes    60    77        1   43 48
EGADS    :    126     2     Yes    78    76        1   44 59
EGADS    :    127     2     Yes    62    78        1   44 45
EGADS    :    128     2     Yes    79    78        1   45 59
EGADS    :    129     2     Yes    63    79        1   45 46
EGADS    :    130     2     Yes    80    79        1   46 60
EGADS    :    131     2     Yes    64    80        1   46 47
EGADS    :    132     2     Yes    65    81        1   47 48
EGADS    :    133     2     Yes    80    81        1   47 60
EGADS    :    134     2     Yes    81    77        1   48 60
EGADS    :    135     2     Yes    67    82        1   49 50
EGADS    :    136     2     Yes    82    83        1   49 61
EGADS    :    137     2     Yes    84    83        1   49 50
EGADS    :    138     2     Yes    84    85        1   49 62
EGADS    :    139     2     Yes    86    85        1   49 63
EGADS    :    140     2     Yes    87    86        1   49 64
EGADS    :    141     2     Yes    66    87        1   49 50
EGADS    :    142     2     Yes    88    87        1   50 65
EGADS    :    143     2     Yes    88    89        1   50 66
EGADS    :    144     2     Yes    89    84        1   50 67
EGADS    :    145     2     Yes    83    82        1   50 68
EGADS    :    146     2     Yes    68    90        1   51 58
EGADS    :    147     2     Yes    91    90        1   51 69
EGADS    :    148     2     Yes    69    91        1   51 52
EGADS    :    149     2     Yes    70    92        1   52 53
EGADS    :    150     2     Yes    91    92        1   52 69
EGADS    :    151     2     Yes    71    93        1   53 56
EGADS    :    152     2     Yes    92    93        1   53 69
EGADS    :    153     2     Yes    72    94        1   54 55
EGADS    :    154     2     Yes    95    94        1   54 70
EGADS    :    155     2     Yes    95    96        1   54 71
EGADS    :    156     2     Yes    96    97        1   54 72
EGADS    :    157     2     Yes    97    98        1   54 55
EGADS    :    158     2     Yes    99    98        1   54 73
EGADS    :    159     2     Yes    99   100        1   54 74
EGADS    :    160     2     Yes   100   101        1   54 75
EGADS    :    161     2     Yes   101   102        1   54 55
EGADS    :    162     2     Yes   102   103        1   54 76
EGADS    :    163     2     Yes    73   103        1   54 55
EGADS    :    164     2     Yes   103   102        1   55 76
EGADS    :    165     2     Yes   101   104        1   55 77
EGADS    :    166     2     Yes   105   104        1   55 78
EGADS    :    167     2     Yes    98   105        1   55 79
EGADS    :    168     2     Yes    97   106        1   55 80
EGADS    :    169     2     Yes   107   106        1   55 81
EGADS    :    170     2     Yes    94   107        1   55 82
EGADS    :    171     2     Yes    74   108        1   56 57
EGADS    :    172     2     Yes    93   108        1   56 83
EGADS    :    173     2     Yes   109   108        1   57 83
EGADS    :    174     2     Yes    75   109        1   57 58
EGADS    :    175     2     Yes    90   109        1   58 83
EGADS    :    176     2     Yes    79    77        1   59 60
EGADS    :    177     2     Yes    82   110        1   61 68
EGADS    :    178     2     Yes   110   111        1   61 84
EGADS    :    179     2     Yes   112   111        1   61 68
EGADS    :    180     2     Yes   112   113        1   61 85
EGADS    :    181     2     Yes   114   113        1   61 86
EGADS    :    182     2     Yes   115   114        1   61 87
EGADS    :    183     2     Yes   116   115        1   61 68
EGADS    :    184     2     Yes   116   117        1   61 88
EGADS    :    185     2     Yes   118   117        1   61 89
EGADS    :    186     2     Yes   119   118        1   61 90
EGADS    :    187     2     Yes    83   119        1   61 68
EGADS    :    188     2     Yes    85   120        1   62 63
EGADS    :    189     2     Yes   121   120        1   62 91
EGADS    :    190     2     Yes    84   121        1   62 67
EGADS    :    191     2     Yes   122   120        1   63 91
EGADS    :    192     2     Yes    86   122        1   63 64
EGADS    :    193     2     Yes   123   122        1   64 91
EGADS    :    194     2     Yes    87   123        1   64 65
EGADS    :    195     2     Yes   124   123        1   65 92
EGADS    :    196     2     Yes    88   124        1   65 66
EGADS    :    197     2     Yes    89   125        1   66 67
EGADS    :    198     2     Yes   124   125        1   66 92
EGADS    :    199     2     Yes   125   121        1   67 92
EGADS    :    200     2     Yes   126   119        1   68 93
EGADS    :    201     2     Yes   126   127        1   68 94
EGADS    :    202     2     Yes   127   116        1   68 95
EGADS    :    203     2     Yes   128   115        1   68 96
EGADS    :    204     2     Yes   128   129        1   68 97
EGADS    :    205     2     Yes   129   112        1   68 98
EGADS    :    206     2     Yes   111   110        1   68 84
EGADS    :    207     2     Yes    90    93        1   69 83
EGADS    :    208     2     Yes    94   130        1   70 82
EGADS    :    209     2     Yes   131   130        1   70 99
EGADS    :    210     2     Yes    95   131        1   70 71
EGADS    :    211     2     Yes    96   132        1   71 72
EGADS    :    212     2     Yes   131   132        1   71 99
EGADS    :    213     2     Yes    97   133        1   72 80
EGADS    :    214     2     Yes   132   133        1   72 99
EGADS    :    215     2     Yes    98   134        1   73 79
EGADS    :    216     2     Yes   135   134        1   73 100
EGADS    :    217     2     Yes    99   135        1   73 74
EGADS    :    218     2     Yes   100   136        1   74 75
EGADS    :    219     2     Yes   135   136        1   74 100
EGADS    :    220     2     Yes   101   137        1   75 77
EGADS    :    221     2     Yes   136   137        1   75 100
EGADS    :    222     2     Yes   104   138        1   77 78
EGADS    :    223     2     Yes   137   138        1   77 101
EGADS    :    224     2     Yes   139   138        1   78 101
EGADS    :    225     2     Yes   105   139        1   78 79
EGADS    :    226     2     Yes   134   139        1   79 101
EGADS    :    227     2     Yes   106   140        1   80 81
EGADS    :    228     2     Yes   133   140        1   80 102
EGADS    :    229     2     Yes   141   140        1   81 102
EGADS    :    230     2     Yes   107   141        1   81 82
EGADS    :    231     2     Yes   130   141        1   82 102
EGADS    :    232     2     Yes   113   142        1   85 86
EGADS    :    233     2     Yes   143   142        1   85 103
EGADS    :    234     2     Yes   112   143        1   85 98
EGADS    :    235     2     Yes   144   142        1   86 103
EGADS    :    236     2     Yes   114   144        1   86 87
EGADS    :    237     2     Yes   145   144        1   87 103
EGADS    :    238     2     Yes   115   145        1   87 96
EGADS    :    239     2     Yes   117   146        1   88 89
EGADS    :    240     2     Yes   147   146        1   88 104
EGADS    :    241     2     Yes   116   147        1   88 95
EGADS    :    242     2     Yes   148   146        1   89 104
EGADS    :    243     2     Yes   118   148        1   89 90
EGADS    :    244     2     Yes   149   148        1   90 104
EGADS    :    245     2     Yes   119   149        1   90 93
EGADS    :    246     2     Yes   123   121        1   91 92
EGADS    :    247     2     Yes   150   149        1   93 105
EGADS    :    248     2     Yes   126   150        1   93 94
EGADS    :    249     2     Yes   127   151        1   94 95
EGADS    :    250     2     Yes   150   151        1   94 105
EGADS    :    251     2     Yes   151   147        1   95 105
EGADS    :    252     2     Yes   152   145        1   96 106
EGADS    :    253     2     Yes   128   152        1   96 97
EGADS    :    254     2     Yes   129   153        1   97 98
EGADS    :    255     2     Yes   152   153        1   97 106
EGADS    :    256     2     Yes   153   143        1   98 106
EGADS    :    257     2     Yes   130   133        1   99 102
EGADS    :    258     2     Yes   134   137        1   100 101
EGADS    :    259     2     Yes   145   143        1   103 106
EGADS    :    260     2     Yes   149   147        1   104 105
EGADS    :    261     2     Yes    11    18        1   107 108
EGADS    :    262     3     Yes   155   154       NA   109 111
EGADS    :    263     3     Yes   154   156       NA   109 114
EGADS    :    264     3     Yes   157   156       NA   109 112
EGADS    :    265     3     Yes   155   157       NA   109 113
EGADS    :    266     3     Yes   159   158       NA   110 111
EGADS    :    267     3     Yes   158   160       NA   110 114
EGADS    :    268     3     Yes   161   160       NA   110 112
EGADS    :    269     3     Yes   159   161       NA   110 113
EGADS    :    270     3     Yes   155   159       NA   111 113
EGADS    :    271     3     Yes   154   158       NA   111 114
EGADS    :    272     3     Yes   157   161       NA   112 113
EGADS    :    273     3     Yes   156   160       NA   112 114

EGADS    : Node Information

EGADS    :   Node  Active      Coordinates
EGADS    :      1     Yes       90.5173952                0                0
EGADS    :      2     Yes       90.5173952                0                0
EGADS    :      3     Yes       60.5173952                0                0
EGADS    :      4     Yes       60.5173952                0                0
EGADS    :      5     Yes       90.5173952       29.3018771                0
EGADS    :      6     Yes       90.5173952       29.3018771                0
EGADS    :      7     Yes       60.5173952       29.3018771                0
EGADS    :      8     Yes       60.5173952       29.3018771                0
EGADS    :      9     Yes       155.279418      0.556318046       17.8486974
EGADS    :     10     Yes       162.754076                0       17.8179957
EGADS    :     11     Yes       162.923819                0       18.2706428
EGADS    :     12     Yes       156.044413      0.521348839       18.2706428
EGADS    :     13     Yes       155.279418                0       17.8486974
EGADS    :     14     Yes       156.044413                0       18.2706428
EGADS    :     15     Yes       166.073363                0       35.1119946
EGADS    :     16     Yes       166.308339                0       34.6929244
EGADS    :     17     Yes       169.251074                0       35.1433216
EGADS    :     18     Yes       169.082175                0       34.6929244
EGADS    :     19     Yes       166.073363      0.227596794       35.1119946
EGADS    :     20     Yes       166.308339      0.210212312       34.6929244
EGADS    :     21     Yes       162.505711        6.6926087       7.42255789
EGADS    :     22     Yes       153.264796       6.72114619       6.73834001
EGADS    :     23     Yes       153.930225         7.199099       6.86796425
EGADS    :     24     Yes       162.623387       7.31455844       6.87508685
EGADS    :     25     Yes       139.227902       5.03861756       7.07099122
EGADS    :     26     Yes        165.02399        35.781198       13.6055284
EGADS    :     27     Yes       173.282633        35.781198       13.6055284
EGADS    :     28     Yes       172.798165       34.4735419       13.3275775
EGADS    :     29     Yes       168.724656       34.4225125       13.0211892
EGADS    :     30     Yes       160.457816       1.16501909       6.24763245
EGADS    :     31     Yes       152.092394       3.29252447       6.00142548
EGADS    :     32     Yes       168.960236       34.0035224       12.9505074
EGADS    :     33     Yes       172.609156        34.051986        12.953497
EGADS    :     34     Yes       153.264796       6.72114619       8.11890743
EGADS    :     35     Yes       154.029174       7.14485531       8.17706386
EGADS    :     36     Yes       168.724656       34.4225125       13.6122726
EGADS    :     37     Yes       156.577382       2.32417494       6.86784347
EGADS    :     38     Yes       121.026192                0                0
EGADS    :     39     Yes       165.026192                0                7
EGADS    :     40     Yes       165.026192              0.5              8.5
EGADS    :     41     Yes       121.026192               10                0
EGADS    :     42     Yes       165.026192                0               10
EGADS    :     43     Yes       159.822328                0               10
EGADS    :     44     Yes       137.454662                0               10
EGADS    :     45     Yes       121.026192                0               10
EGADS    :     46     Yes        169.00177       33.9807538       13.4999966
EGADS    :     47     Yes       121.026192                0                0
EGADS    :     48     Yes       152.092394                0       6.00142548
EGADS    :     49     Yes       160.457816                0       6.24763245
EGADS    :     50     Yes       156.577382                0       6.86784347
EGADS    :     51     Yes       165.026192                0              8.5
EGADS    :     52     Yes                0                0                0
EGADS    :     53     Yes       54.9020417       7.00084115                0
EGADS    :     54     Yes        97.361045       7.90366896                0
EGADS    :     55     Yes       139.227902                0       7.07099122
EGADS    :     56     Yes        169.38016                0        35.487551
EGADS    :     57     Yes       162.942213                0        35.487551
EGADS    :     58     Yes        165.02399                0       13.6055284
EGADS    :     59     Yes       173.282633                0       13.6055284
EGADS    :     60     Yes       172.798165                0       13.3275775
EGADS    :     61     Yes       168.724656                0       13.0211892
EGADS    :     62     Yes       153.264796                0       6.73834001
EGADS    :     63     Yes       162.505711                0       7.42255789
EGADS    :     64     Yes       153.264796                0       8.11890743
EGADS    :     65     Yes       168.724656                0       13.6122726
EGADS    :     66     Yes        97.361045                0                0
EGADS    :     67     Yes       54.9020417                0                0
EGADS    :     68     Yes       97.4729837       13.4242561                0
EGADS    :     69     Yes       93.4471586       13.4242631                0
EGADS    :     70     Yes       93.8409288        32.482011                0
EGADS    :     71     Yes       97.8594104        32.482018                0
EGADS    :     72     Yes       97.9335611       36.1389817                0
EGADS    :     73     Yes       75.3047874       36.1389817                0
EGADS    :     74     Yes       93.8409288        32.482011                0
EGADS    :     75     Yes       93.4471586       13.4242631                0
EGADS    :     76     Yes       168.960236                0       12.9505074
EGADS    :     77     Yes       172.609156                0        12.953497
EGADS    :     78     Yes       153.930225                0       6.86796425
EGADS    :     79     Yes       162.623387                0       6.87508685
EGADS    :     80     Yes       154.029174                0       8.17706386
EGADS    :     81     Yes        169.00177                0       13.4999966
EGADS    :     82     Yes       75.3047874                0                0
EGADS    :     83     Yes       97.9335611                0                0
EGADS    :     84     Yes       97.8594104                0                0
EGADS    :     85     Yes       93.8409288                0                0
EGADS    :     86     Yes       93.4471586                0                0
EGADS    :     87     Yes       97.4729837                0                0
EGADS    :     88     Yes       93.4471586                0                0
EGADS    :     89     Yes       93.8409288                0                0
EGADS    :     90     Yes       97.1624342       13.7926169                0
EGADS    :     91     Yes       93.8265357       13.6735644                0
EGADS    :     92     Yes       94.2099771       32.2314198                0
EGADS    :     93     Yes       97.6079776       32.3498916                0
EGADS    :     94     Yes       100.278023       41.7701593                0
EGADS    :     95     Yes       94.7972887       41.7748561                0
EGADS    :     96     Yes       107.397556       67.6186586       1.83668579
EGADS    :     97     Yes       111.041954       67.6241096       1.25345146
EGADS    :     98     Yes       111.257254       68.1412393       1.31307624
EGADS    :     99     Yes       107.654637        68.146711       1.88687506
EGADS    :    100     Yes       121.207308       95.9421381       4.50820234
EGADS    :    101     Yes       122.837313       95.9554542       4.52004059
EGADS    :    102     Yes       123.552357       97.6729236        4.7180639
EGADS    :    103     Yes       118.391317       97.6729236       3.99272703
EGADS    :    104     Yes       121.207308       95.9421381       4.21444802
EGADS    :    105     Yes       107.654637        68.146711      0.876544084
EGADS    :    106     Yes       107.397556       67.6186586      0.813033541
EGADS    :    107     Yes       94.7972887       41.7748561                0
EGADS    :    108     Yes       93.9108835       32.2329728                0
EGADS    :    109     Yes       93.5781103       13.6748542                0
EGADS    :    110     Yes       118.391317                0       3.99272703
EGADS    :    111     Yes       123.552357                0        4.7180639
EGADS    :    112     Yes       122.837313                0       4.52004059
EGADS    :    113     Yes       121.207308                0       4.21444802
EGADS    :    114     Yes       107.654637                0      0.876544084
EGADS    :    115     Yes       111.257254                0       1.31307624
EGADS    :    116     Yes       111.041954                0       1.25345146
EGADS    :    117     Yes       107.397556                0      0.813033541
EGADS    :    118     Yes       94.7972887                0                0
EGADS    :    119     Yes       100.278023                0                0
EGADS    :    120     Yes       93.9108835                0                0
EGADS    :    121     Yes       97.6079776                0                0
EGADS    :    122     Yes       93.5781103                0                0
EGADS    :    123     Yes       97.1624342                0                0
EGADS    :    124     Yes       93.8265357                0                0
EGADS    :    125     Yes       94.2099771                0                0
EGADS    :    126     Yes       94.7972887                0                0
EGADS    :    127     Yes       107.397556                0       1.83668579
EGADS    :    128     Yes       107.654637                0       1.88687506
EGADS    :    129     Yes       121.207308                0       4.50820234
EGADS    :    130     Yes       100.219054       42.1509694                0
EGADS    :    131     Yes       95.2324957        41.963173                0
EGADS    :    132     Yes       107.613646       67.3581332       1.77910017
EGADS    :    133     Yes       110.892704       67.4707526      0.699981401
EGADS    :    134     Yes       111.247925        68.471101      0.828432723
EGADS    :    135     Yes       108.034544       68.3613138       1.87771912
EGADS    :    136     Yes        121.36809       95.7097324       4.49194275
EGADS    :    137     Yes       122.742135       95.7387605        4.2753035
EGADS    :    138     Yes       121.327393       95.7291979       4.23513353
EGADS    :    139     Yes        107.88707       68.4318513      0.947114671
EGADS    :    140     Yes       107.462349       67.4305014       0.82436964
EGADS    :    141     Yes       94.9817282       42.0831197                0
EGADS    :    142     Yes       121.367879                0       4.23512504
EGADS    :    143     Yes       122.701966                0       4.70778241
EGADS    :    144     Yes       108.034333                0      0.936789144
EGADS    :    145     Yes       111.269456                0       1.85592771
EGADS    :    146     Yes       107.462349                0       0.82436964
EGADS    :    147     Yes       110.892704                0      0.699981401
EGADS    :    148     Yes       94.9817282                0                0
EGADS    :    149     Yes       100.219054                0                0
EGADS    :    150     Yes       95.2324957                0                0
EGADS    :    151     Yes       107.613646                0       1.77910017
EGADS    :    152     Yes       107.888388                0       1.86745513
EGADS    :    153     Yes       121.327604                0       4.49195125
EGADS    :    154     Yes                0                0       1962.43554
EGADS    :    155     Yes                0                0                0
EGADS    :    156     Yes                0       1953.45847       1962.43554
EGADS    :    157     Yes                0       1953.45847                0
EGADS    :    158     Yes       2040.09979                0       1962.43554
EGADS    :    159     Yes       2040.09979                0                0
EGADS    :    160     Yes       2040.09979       1953.45847       1962.43554
EGADS    :    161     Yes       2040.09979       1953.45847                0

EGADS    : Face and Edge Match Information

EGADS    : No Face Matches Found

AFLR4    : Surface Mesh Spacing Setup

AFLR4    : Max Bounding Box Length     = 3906.92
AFLR4    : Min Bounding Box Length     = 3906.92
AFLR4    : Max Ref Bounding Box Length = 195.346
AFLR4    : Min Ref Bounding Box Length = 53.021
AFLR4    : Reference Length            = 21.7051
AFLR4    : BL Thickness                = 0
AFLR4    : FarField Spacing            = 530.302
AFLR4    : Abs Min Surf Spacing        = 0.0542627
AFLR4    : Min Surf Spacing            = 0.108525
AFLR4    : Max Surf Spacing            = 2.17051
AFLR4    : Global Scale Factor         = 1

AFLR4    : Geometry Definition Information

AFLR4    : Definition              Definition   Composite             Grid BC
AFLR4    :         ID                    Type          ID                Type
AFLR4    :          0     glue-only composite           -                   -
AFLR4    :          1            CAD geometry           0            STD w/BL
AFLR4    :          2            CAD geometry           0            STD w/BL
AFLR4    :          3            CAD geometry           0            STD w/BL
AFLR4    :          4            CAD geometry           0            STD w/BL
AFLR4    :          5            CAD geometry           0            STD w/BL
AFLR4    :          6            CAD geometry           0            STD w/BL
AFLR4    :          7            CAD geometry           0            STD w/BL
AFLR4    :          8            CAD geometry           0            STD w/BL
AFLR4    :          9            CAD geometry           0            STD w/BL
AFLR4    :         10            CAD geometry           0            STD w/BL
AFLR4    :         11            CAD geometry           0            STD w/BL
AFLR4    :         12            CAD geometry           0            STD w/BL
AFLR4    :         13            CAD geometry           0            STD w/BL
AFLR4    :         14            CAD geometry           0            STD w/BL
AFLR4    :         15            CAD geometry           0            STD w/BL
AFLR4    :         16            CAD geometry           0            STD w/BL
AFLR4    :         17            CAD geometry           0            STD w/BL
AFLR4    :         18            CAD geometry           0            STD w/BL
AFLR4    :         19            CAD geometry           0            STD w/BL
AFLR4    :         20            CAD geometry           0            STD w/BL
AFLR4    :         21            CAD geometry           0            STD w/BL
AFLR4    :         22            CAD geometry           0            STD w/BL
AFLR4    :         23            CAD geometry           0            STD w/BL
AFLR4    :         24            CAD geometry           0            STD w/BL
AFLR4    :         25            CAD geometry           0            STD w/BL
AFLR4    :         26            CAD geometry           0            STD w/BL
AFLR4    :         27            CAD geometry           0            STD w/BL
AFLR4    :         28            CAD geometry           0            STD w/BL
AFLR4    :         29            CAD geometry           0            STD w/BL
AFLR4    :         30            CAD geometry           0            STD w/BL
AFLR4    :         31            CAD geometry           0            STD w/BL
AFLR4    :         32            CAD geometry           0            STD w/BL
AFLR4    :         33            CAD geometry           0            STD w/BL
AFLR4    :         34            CAD geometry           0            STD w/BL
AFLR4    :         35            CAD geometry           0            STD w/BL
AFLR4    :         36            CAD geometry           0            STD w/BL
AFLR4    :         37            CAD geometry           0            STD w/BL
AFLR4    :         38            CAD geometry           0            STD w/BL
AFLR4    :         39            CAD geometry           0            STD w/BL
AFLR4    :         40            CAD geometry           0            STD w/BL
AFLR4    :         41            CAD geometry           0            STD w/BL
AFLR4    :         42            CAD geometry           0            STD w/BL
AFLR4    :         43            CAD geometry           0            STD w/BL
AFLR4    :         44            CAD geometry           0            STD w/BL
AFLR4    :         45            CAD geometry           0            STD w/BL
AFLR4    :         46            CAD geometry           0            STD w/BL
AFLR4    :         47            CAD geometry           0            STD w/BL
AFLR4    :         48            CAD geometry           0            STD w/BL
AFLR4    :         49            CAD geometry           0            STD w/BL
AFLR4    :         50            CAD geometry           0            STD w/BL
AFLR4    :         51            CAD geometry           0            STD w/BL
AFLR4    :         52            CAD geometry           0            STD w/BL
AFLR4    :         53            CAD geometry           0            STD w/BL
AFLR4    :         54            CAD geometry           0            STD w/BL
AFLR4    :         55            CAD geometry           0            STD w/BL
AFLR4    :         56            CAD geometry           0            STD w/BL
AFLR4    :         57            CAD geometry           0            STD w/BL
AFLR4    :         58            CAD geometry           0            STD w/BL
AFLR4    :         59            CAD geometry           0            STD w/BL
AFLR4    :         60            CAD geometry           0            STD w/BL
AFLR4    :         61            CAD geometry           0            STD w/BL
AFLR4    :         62            CAD geometry           0            STD w/BL
AFLR4    :         63            CAD geometry           0            STD w/BL
AFLR4    :         64            CAD geometry           0            STD w/BL
AFLR4    :         65            CAD geometry           0            STD w/BL
AFLR4    :         66            CAD geometry           0            STD w/BL
AFLR4    :         67            CAD geometry           0            STD w/BL
AFLR4    :         68            CAD geometry           0            STD w/BL
AFLR4    :         69            CAD geometry           0            STD w/BL
AFLR4    :         70            CAD geometry           0            STD w/BL
AFLR4    :         71            CAD geometry           0            STD w/BL
AFLR4    :         72            CAD geometry           0            STD w/BL
AFLR4    :         73            CAD geometry           0            STD w/BL
AFLR4    :         74            CAD geometry           0            STD w/BL
AFLR4    :         75            CAD geometry           0            STD w/BL
AFLR4    :         76            CAD geometry           0            STD w/BL
AFLR4    :         77            CAD geometry           0            STD w/BL
AFLR4    :         78            CAD geometry           0            STD w/BL
AFLR4    :         79            CAD geometry           0            STD w/BL
AFLR4    :         80            CAD geometry           0            STD w/BL
AFLR4    :         81            CAD geometry           0            STD w/BL
AFLR4    :         82            CAD geometry           0            STD w/BL
AFLR4    :         83            CAD geometry           0            STD w/BL
AFLR4    :         84            CAD geometry           0            STD w/BL
AFLR4    :         85            CAD geometry           0            STD w/BL
AFLR4    :         86            CAD geometry           0            STD w/BL
AFLR4    :         87            CAD geometry           0            STD w/BL
AFLR4    :         88            CAD geometry           0            STD w/BL
AFLR4    :         89            CAD geometry           0            STD w/BL
AFLR4    :         90            CAD geometry           0            STD w/BL
AFLR4    :         91            CAD geometry           0            STD w/BL
AFLR4    :         92            CAD geometry           0            STD w/BL
AFLR4    :         93            CAD geometry           0            STD w/BL
AFLR4    :         94            CAD geometry           0            STD w/BL
AFLR4    :         95            CAD geometry           0            STD w/BL
AFLR4    :         96            CAD geometry           0            STD w/BL
AFLR4    :         97            CAD geometry           0            STD w/BL
AFLR4    :         98            CAD geometry           0            STD w/BL
AFLR4    :         99            CAD geometry           0            STD w/BL
AFLR4    :        100            CAD geometry           0            STD w/BL
AFLR4    :        101            CAD geometry           0            STD w/BL
AFLR4    :        102            CAD geometry           0            STD w/BL
AFLR4    :        103            CAD geometry           0            STD w/BL
AFLR4    :        104            CAD geometry           0            STD w/BL
AFLR4    :        105            CAD geometry           0            STD w/BL
AFLR4    :        106            CAD geometry           0            STD w/BL
AFLR4    :        107            CAD geometry           0            STD w/BL
AFLR4    :        108            CAD geometry           0            STD w/BL
AFLR4    :        109            CAD geometry           0            FARFIELD
AFLR4    :        110            CAD geometry           0            FARFIELD
AFLR4    :        111            CAD geometry           0            FARFIELD
AFLR4    :        112            CAD geometry           0            FARFIELD
AFLR4    :        113            CAD geometry           0            FARFIELD
AFLR4    :        114            CAD geometry           0            FARFIELD

AFLR4    : Case has 5 Proximity Checking Components

AFLR4    : Component 1 includes Definitions 23 24 28 29 30 31 33 36 40
AFLR4    : Component 2 includes Definitions 37 38 49 50 51 52 53 54 55 56 57 58
AFLR4    :                                  61 62 63 64 65 66 67 68 69 70 71 72
AFLR4    :                                  73 74 75 76 77 78 79 80 81 82 83 84
AFLR4    :                                  85 86 87 88 89 90 91 92 93 94 95 96
AFLR4    :                                  97 98 99 100 101 102 103 104 105 106
AFLR4    : Component 3 includes Definitions 15 16 17 18 19 20 21 22 25 26 27 34
AFLR4    :                                  35 42 43 44 45 46 47 48 59 60
AFLR4    : Component 4 includes Definitions 9 10 11 12 13 14 32 39 41 107 108
AFLR4    : Component 5 includes Definitions 1 2 3 4 5 6 7 8

AFLR4    : Define CAD surface definition 1
AFLR4    : Define CAD surface definition 2
AFLR4    : Define CAD surface definition 3
AFLR4    : Define CAD surface definition 4
AFLR4    : Define CAD surface definition 5
AFLR4    : Define CAD surface definition 6
AFLR4    : Define CAD surface definition 7
AFLR4    : Define CAD surface definition 8
AFLR4    : Define CAD surface definition 9
AFLR4    : Define CAD surface definition 10
AFLR4    : Define CAD surface definition 11
AFLR4    : Define CAD surface definition 12
AFLR4    : Define CAD surface definition 13
AFLR4    : Define CAD surface definition 14
AFLR4    : Define CAD surface definition 15
AFLR4    : Define CAD surface definition 16
AFLR4    : Define CAD surface definition 17
AFLR4    : Define CAD surface definition 18
AFLR4    : Define CAD surface definition 19
AFLR4    : Define CAD surface definition 20
AFLR4    : Define CAD surface definition 21
AFLR4    : Define CAD surface definition 22
AFLR4    : Define CAD surface definition 23
AFLR4    : Define CAD surface definition 24
AFLR4    : Define CAD surface definition 25
AFLR4    : Define CAD surface definition 26
AFLR4    : Define CAD surface definition 27
AFLR4    : Define CAD surface definition 28
AFLR4    : Define CAD surface definition 29
AFLR4    : Define CAD surface definition 30
AFLR4    : Define CAD surface definition 31
AFLR4    : Define CAD surface definition 32
AFLR4    : Define CAD surface definition 33
AFLR4    : Define CAD surface definition 34
AFLR4    : Define CAD surface definition 35
AFLR4    : Define CAD surface definition 36
AFLR4    : Define CAD surface definition 37
AFLR4    : Define CAD surface definition 38
AFLR4    : Define CAD surface definition 39
AFLR4    : Define CAD surface definition 40
AFLR4    : Define CAD surface definition 41
AFLR4    : Define CAD surface definition 42
AFLR4    : Define CAD surface definition 43
AFLR4    : Define CAD surface definition 44
AFLR4    : Define CAD surface definition 45
AFLR4    : Define CAD surface definition 46
AFLR4    : Define CAD surface definition 47
AFLR4    : Define CAD surface definition 48
AFLR4    : Define CAD surface definition 49
AFLR4    : Define CAD surface definition 50
AFLR4    : Define CAD surface definition 51
AFLR4    : Define CAD surface definition 52
AFLR4    : Define CAD surface definition 53
AFLR4    : Define CAD surface definition 54
AFLR4    : Define CAD surface definition 55
AFLR4    : Define CAD surface definition 56
AFLR4    : Define CAD surface definition 57
AFLR4    : Define CAD surface definition 58
AFLR4    : Define CAD surface definition 59
AFLR4    : Define CAD surface definition 60
AFLR4    : Define CAD surface definition 61
AFLR4    : Define CAD surface definition 62
AFLR4    : Define CAD surface definition 63
AFLR4    : Define CAD surface definition 64
AFLR4    : Define CAD surface definition 65
AFLR4    : Define CAD surface definition 66
AFLR4    : Define CAD surface definition 67
AFLR4    : Define CAD surface definition 68
AFLR4    : Define CAD surface definition 69
AFLR4    : Define CAD surface definition 70
AFLR4    : Define CAD surface definition 71
AFLR4    : Define CAD surface definition 72
AFLR4    : Define CAD surface definition 73
AFLR4    : Define CAD surface definition 74
AFLR4    : Define CAD surface definition 75
AFLR4    : Define CAD surface definition 76
AFLR4    : Define CAD surface definition 77
AFLR4    : Define CAD surface definition 78
AFLR4    : Define CAD surface definition 79
AFLR4    : Define CAD surface definition 80
AFLR4    : Define CAD surface definition 81
AFLR4    : Define CAD surface definition 82
AFLR4    : Define CAD surface definition 83
AFLR4    : Define CAD surface definition 84
AFLR4    : Define CAD surface definition 85
AFLR4    : Define CAD surface definition 86
AFLR4    : Define CAD surface definition 87
AFLR4    : Define CAD surface definition 88
AFLR4    : Define CAD surface definition 89
AFLR4    : Define CAD surface definition 90
AFLR4    : Define CAD surface definition 91
AFLR4    : Define CAD surface definition 92
AFLR4    : Define CAD surface definition 93
AFLR4    : Define CAD surface definition 94
AFLR4    : Define CAD surface definition 95
AFLR4    : Define CAD surface definition 96
AFLR4    : Define CAD surface definition 97
AFLR4    : Define CAD surface definition 98
AFLR4    : Define CAD surface definition 99
AFLR4    : Define CAD surface definition 100
AFLR4    : Define CAD surface definition 101
AFLR4    : Define CAD surface definition 102
AFLR4    : Define CAD surface definition 103
AFLR4    : Define CAD surface definition 104
AFLR4    : Define CAD surface definition 105
AFLR4    : Define CAD surface definition 106
AFLR4    : Define CAD surface definition 107
AFLR4    : Define CAD surface definition 108
AFLR4    : Define CAD surface definition 109
AFLR4    : Define CAD surface definition 110
AFLR4    : Define CAD surface definition 111
AFLR4    : Define CAD surface definition 112
AFLR4    : Define CAD surface definition 113
AFLR4    : Define CAD surface definition 114

AFLR4    : Surface Grid Generation

AFLR4    : Generate optimal mesh on surface definition 1
AFLR2    : Nodes, Trias,Quads=       339       605         0
AFLR4    : Nodes, Trias,Quads=       362       651         0

AFLR4    : Generate optimal mesh on surface definition 2
AFLR2    : Nodes, Trias,Quads=       319       563         0
AFLR4    : Nodes, Trias,Quads=       284       493         0

AFLR4    : Generate optimal mesh on surface definition 3
AFLR2    : Nodes, Trias,Quads=       340       607         0
AFLR4    : Nodes, Trias,Quads=       362       651         0

AFLR4    : Generate optimal mesh on surface definition 4
AFLR2    : Nodes, Trias,Quads=       321       567         0
AFLR4    : Nodes, Trias,Quads=       284       493         0

AFLR4    : Generate optimal mesh on surface definition 5
AFLR2    : Nodes, Trias,Quads=       340       607         0
AFLR4    : Nodes, Trias,Quads=       362       651         0

AFLR4    : Generate optimal mesh on surface definition 6
AFLR2    : Nodes, Trias,Quads=       321       567         0
AFLR4    : Nodes, Trias,Quads=       284       493         0

AFLR4    : Generate optimal mesh on surface definition 7
AFLR2    : Nodes, Trias,Quads=       339       605         0
AFLR4    : Nodes, Trias,Quads=       362       651         0

AFLR4    : Generate optimal mesh on surface definition 8
AFLR2    : Nodes, Trias,Quads=       319       563         0
AFLR4    : Nodes, Trias,Quads=       284       493         0

AFLR4    : Generate optimal mesh on surface definition 9
AFLR2    : Nodes, Trias,Quads=        15        19         0
AFLR4    : Nodes, Trias,Quads=         9         7         0

AFLR4    : Generate optimal mesh on surface definition 10
AFLR2    : Nodes, Trias,Quads=        15        19         0
AFLR4    : Nodes, Trias,Quads=         9         7         0

AFLR4    : Generate optimal mesh on surface definition 11
AFLR2    : Nodes, Trias,Quads=        47        65         0
AFLR4    : Nodes, Trias,Quads=        27        25         0

AFLR4    : Generate optimal mesh on surface definition 12
AFLR2    : Nodes, Trias,Quads=        24        31         0
AFLR4    : Nodes, Trias,Quads=        23        29         0

AFLR4    : Generate optimal mesh on surface definition 13
AFLR2    : Nodes, Trias,Quads=        24        31         0
AFLR4    : Nodes, Trias,Quads=        22        27         0

AFLR4    : Generate optimal mesh on surface definition 14
AFLR2    : Nodes, Trias,Quads=        47        65         0
AFLR4    : Nodes, Trias,Quads=        27        25         0

AFLR4    : Generate optimal mesh on surface definition 15
AFLR2    : Nodes, Trias,Quads=        51        67         0
AFLR4    : Nodes, Trias,Quads=        58        81         0

AFLR4    : Generate optimal mesh on surface definition 16
AFLR2    : Nodes, Trias,Quads=      1615      3003         0
AFLR4    : Nodes, Trias,Quads=      1188      2149         0

AFLR4    : Generate optimal mesh on surface definition 17
AFLR2    : Nodes, Trias,Quads=        90       127         0
AFLR4    : Nodes, Trias,Quads=        51        49         0

AFLR4    : Generate optimal mesh on surface definition 18
AFLR2    : Nodes, Trias,Quads=       216       367         0
AFLR4    : Nodes, Trias,Quads=       174       283         0

AFLR4    : Generate optimal mesh on surface definition 19
AFLR2    : Nodes, Trias,Quads=        51        67         0
AFLR4    : Nodes, Trias,Quads=        51        67         0

AFLR4    : Generate optimal mesh on surface definition 20
AFLR2    : Nodes, Trias,Quads=      1677      3126         0
AFLR4    : Nodes, Trias,Quads=      1210      2192         0

AFLR4    : Generate optimal mesh on surface definition 21
AFLR2    : Nodes, Trias,Quads=        35        44         0
AFLR4    : Nodes, Trias,Quads=        24        22         0

AFLR4    : Generate optimal mesh on surface definition 22
AFLR2    : Nodes, Trias,Quads=        11        13         0
AFLR4    : Nodes, Trias,Quads=         9         9         0

AFLR4    : Generate optimal mesh on surface definition 23
AFLR2    : Nodes, Trias,Quads=       907      1650         0
AFLR4    : Nodes, Trias,Quads=       569       974         0

AFLR4    : Generate optimal mesh on surface definition 24
AFLR2    : Nodes, Trias,Quads=      3270      6232         0
AFLR4    : Nodes, Trias,Quads=      1907      3506         0

AFLR4    : Generate optimal mesh on surface definition 25
AFLR2    : Nodes, Trias,Quads=       220       375         0
AFLR4    : Nodes, Trias,Quads=       176       287         0

AFLR4    : Generate optimal mesh on surface definition 26
AFLR2    : Nodes, Trias,Quads=        80       108         0
AFLR4    : Nodes, Trias,Quads=        50        48         0

AFLR4    : Generate optimal mesh on surface definition 27
AFLR2    : Nodes, Trias,Quads=        12        14         0
AFLR4    : Nodes, Trias,Quads=        12        14         0

AFLR4    : Generate optimal mesh on surface definition 28
AFLR2    : Nodes, Trias,Quads=       902      1640         0
AFLR4    : Nodes, Trias,Quads=       561       958         0

AFLR4    : Generate optimal mesh on surface definition 29
AFLR2    : Nodes, Trias,Quads=       106       170         0
AFLR4    : Nodes, Trias,Quads=       106       170         0

AFLR4    : Generate optimal mesh on surface definition 30
AFLR2    : Nodes, Trias,Quads=      1586      2835         0
AFLR4    : Nodes, Trias,Quads=      1651      2965         0

AFLR4    : Generate optimal mesh on surface definition 31
AFLR2    : Nodes, Trias,Quads=      3418      6528         0
AFLR4    : Nodes, Trias,Quads=      1888      3468         0

AFLR4    : Generate optimal mesh on surface definition 32
AFLR2    : Nodes, Trias,Quads=      1868      3486         0
AFLR4    : Nodes, Trias,Quads=      1347      2444         0

AFLR4    : Generate optimal mesh on surface definition 33
AFLR2    : Nodes, Trias,Quads=      1026      1838         0
AFLR4    : Nodes, Trias,Quads=      1211      2208         0

AFLR4    : Generate optimal mesh on surface definition 34
AFLR2    : Nodes, Trias,Quads=      1436      2654         0
AFLR4    : Nodes, Trias,Quads=       979      1740         0

AFLR4    : Generate optimal mesh on surface definition 35
AFLR2    : Nodes, Trias,Quads=      1684      3140         0
AFLR4    : Nodes, Trias,Quads=      1216      2204         0

AFLR4    : Generate optimal mesh on surface definition 36
AFLR2    : Nodes, Trias,Quads=      1580      2823         0
AFLR4    : Nodes, Trias,Quads=      1646      2955         0

AFLR4    : Generate optimal mesh on surface definition 37
AFLR2    : Nodes, Trias,Quads=      2154      4060         0
AFLR4    : Nodes, Trias,Quads=      2140      4032         0

AFLR4    : Generate optimal mesh on surface definition 38
AFLR2    : Nodes, Trias,Quads=      2585      4915         0
AFLR4    : Nodes, Trias,Quads=      2189      4123         0

AFLR4    : Generate optimal mesh on surface definition 39
AFLR2    : Nodes, Trias,Quads=      1916      3582         0
AFLR4    : Nodes, Trias,Quads=      1367      2484         0

AFLR4    : Generate optimal mesh on surface definition 40
AFLR2    : Nodes, Trias,Quads=      1026      1838         0
AFLR4    : Nodes, Trias,Quads=      1215      2216         0

AFLR4    : Generate optimal mesh on surface definition 41
AFLR2    : Nodes, Trias,Quads=        47        60         0
AFLR4    : Nodes, Trias,Quads=        32        30         0

AFLR4    : Generate optimal mesh on surface definition 42
AFLR2    : Nodes, Trias,Quads=        35        44         0
AFLR4    : Nodes, Trias,Quads=        24        22         0

AFLR4    : Generate optimal mesh on surface definition 43
AFLR2    : Nodes, Trias,Quads=        11        13         0
AFLR4    : Nodes, Trias,Quads=         9         9         0

AFLR4    : Generate optimal mesh on surface definition 44
AFLR2    : Nodes, Trias,Quads=        59        84         0
AFLR4    : Nodes, Trias,Quads=        32        30         0

AFLR4    : Generate optimal mesh on surface definition 45
AFLR2    : Nodes, Trias,Quads=        41        53         0
AFLR4    : Nodes, Trias,Quads=        48        67         0

AFLR4    : Generate optimal mesh on surface definition 46
AFLR2    : Nodes, Trias,Quads=        51        67         0
AFLR4    : Nodes, Trias,Quads=        50        65         0

AFLR4    : Generate optimal mesh on surface definition 47
AFLR2    : Nodes, Trias,Quads=        80       108         0
AFLR4    : Nodes, Trias,Quads=        50        48         0

AFLR4    : Generate optimal mesh on surface definition 48
AFLR2    : Nodes, Trias,Quads=        12        14         0
AFLR4    : Nodes, Trias,Quads=        12        14         0

AFLR4    : Generate optimal mesh on surface definition 49
AFLR2    : Nodes, Trias,Quads=      2582      4909         0
AFLR4    : Nodes, Trias,Quads=      2199      4143         0

AFLR4    : Generate optimal mesh on surface definition 50
AFLR2    : Nodes, Trias,Quads=      2158      4068         0
AFLR4    : Nodes, Trias,Quads=      2139      4030         0

AFLR4    : Generate optimal mesh on surface definition 51
AFLR2    : Nodes, Trias,Quads=        46        65         0
AFLR4    : Nodes, Trias,Quads=        39        51         0

AFLR4    : Generate optimal mesh on surface definition 52
AFLR2    : Nodes, Trias,Quads=       108       144         0
AFLR4    : Nodes, Trias,Quads=       102       132         0

AFLR4    : Generate optimal mesh on surface definition 53
AFLR2    : Nodes, Trias,Quads=        46        65         0
AFLR4    : Nodes, Trias,Quads=        39        51         0

AFLR4    : Generate optimal mesh on surface definition 54
AFLR2    : Nodes, Trias,Quads=      3787      7224         0
AFLR4    : Nodes, Trias,Quads=      2368      4386         0

AFLR4    : Generate optimal mesh on surface definition 55
AFLR2    : Nodes, Trias,Quads=      3490      6642         0
AFLR4    : Nodes, Trias,Quads=      2094      3850         0

AFLR4    : Generate optimal mesh on surface definition 56
AFLR2    : Nodes, Trias,Quads=        74       114         0
AFLR4    : Nodes, Trias,Quads=        49        64         0

AFLR4    : Generate optimal mesh on surface definition 57
AFLR2    : Nodes, Trias,Quads=       148       206         0
AFLR4    : Nodes, Trias,Quads=       111       132         0

AFLR4    : Generate optimal mesh on surface definition 58
AFLR2    : Nodes, Trias,Quads=        70       107         0
AFLR4    : Nodes, Trias,Quads=        49        65         0

AFLR4    : Generate optimal mesh on surface definition 59
AFLR2    : Nodes, Trias,Quads=       130       209         0
AFLR4    : Nodes, Trias,Quads=        94       137         0

AFLR4    : Generate optimal mesh on surface definition 60
AFLR2    : Nodes, Trias,Quads=       215       365         0
AFLR4    : Nodes, Trias,Quads=       176       287         0

AFLR4    : Generate optimal mesh on surface definition 61
AFLR2    : Nodes, Trias,Quads=      3536      6729         0
AFLR4    : Nodes, Trias,Quads=      2180      4017         0

AFLR4    : Generate optimal mesh on surface definition 62
AFLR2    : Nodes, Trias,Quads=        74       114         0
AFLR4    : Nodes, Trias,Quads=        48        62         0

AFLR4    : Generate optimal mesh on surface definition 63
AFLR2    : Nodes, Trias,Quads=       148       206         0
AFLR4    : Nodes, Trias,Quads=       111       132         0

AFLR4    : Generate optimal mesh on surface definition 64
AFLR2    : Nodes, Trias,Quads=        70       107         0
AFLR4    : Nodes, Trias,Quads=        49        65         0

AFLR4    : Generate optimal mesh on surface definition 65
AFLR2    : Nodes, Trias,Quads=        46        65         0
AFLR4    : Nodes, Trias,Quads=        39        51         0

AFLR4    : Generate optimal mesh on surface definition 66
AFLR2    : Nodes, Trias,Quads=       108       144         0
AFLR4    : Nodes, Trias,Quads=        94       116         0

AFLR4    : Generate optimal mesh on surface definition 67
AFLR2    : Nodes, Trias,Quads=        46        65         0
AFLR4    : Nodes, Trias,Quads=        39        51         0

AFLR4    : Generate optimal mesh on surface definition 68
AFLR2    : Nodes, Trias,Quads=      3573      6801         0
AFLR4    : Nodes, Trias,Quads=      2281      4217         0

AFLR4    : Generate optimal mesh on surface definition 69
AFLR2    : Nodes, Trias,Quads=       245       414         0
AFLR4    : Nodes, Trias,Quads=       224       372         0

AFLR4    : Generate optimal mesh on surface definition 70
AFLR2    : Nodes, Trias,Quads=        50        67         0
AFLR4    : Nodes, Trias,Quads=        51        69         0

AFLR4    : Generate optimal mesh on surface definition 71
AFLR2    : Nodes, Trias,Quads=       114       155         0
AFLR4    : Nodes, Trias,Quads=        78        83         0

AFLR4    : Generate optimal mesh on surface definition 72
AFLR2    : Nodes, Trias,Quads=        28        36         0
AFLR4    : Nodes, Trias,Quads=        31        42         0

AFLR4    : Generate optimal mesh on surface definition 73
AFLR2    : Nodes, Trias,Quads=        39        50         0
AFLR4    : Nodes, Trias,Quads=        42        56         0

AFLR4    : Generate optimal mesh on surface definition 74
AFLR2    : Nodes, Trias,Quads=       157       216         0
AFLR4    : Nodes, Trias,Quads=       141       184         0

AFLR4    : Generate optimal mesh on surface definition 75
AFLR2    : Nodes, Trias,Quads=        31        39         0
AFLR4    : Nodes, Trias,Quads=        32        41         0

AFLR4    : Generate optimal mesh on surface definition 76
AFLR2    : Nodes, Trias,Quads=        36        49         0
AFLR4    : Nodes, Trias,Quads=        21        19         0

AFLR4    : Generate optimal mesh on surface definition 77
AFLR2    : Nodes, Trias,Quads=        32        40         0
AFLR4    : Nodes, Trias,Quads=        34        44         0

AFLR4    : Generate optimal mesh on surface definition 78
AFLR2    : Nodes, Trias,Quads=       148       208         0
AFLR4    : Nodes, Trias,Quads=        86        84         0

AFLR4    : Generate optimal mesh on surface definition 79
AFLR2    : Nodes, Trias,Quads=        31        40         0
AFLR4    : Nodes, Trias,Quads=        33        44         0

AFLR4    : Generate optimal mesh on surface definition 80
AFLR2    : Nodes, Trias,Quads=        28        36         0
AFLR4    : Nodes, Trias,Quads=        30        40         0

AFLR4    : Generate optimal mesh on surface definition 81
AFLR2    : Nodes, Trias,Quads=       111       158         0
AFLR4    : Nodes, Trias,Quads=        65        66         0

AFLR4    : Generate optimal mesh on surface definition 82
AFLR2    : Nodes, Trias,Quads=        33        41         0
AFLR4    : Nodes, Trias,Quads=        40        55         0

AFLR4    : Generate optimal mesh on surface definition 83
AFLR2    : Nodes, Trias,Quads=       328       564         0
AFLR4    : Nodes, Trias,Quads=       305       518         0

AFLR4    : Generate optimal mesh on surface definition 84
AFLR2    : Nodes, Trias,Quads=        36        49         0
AFLR4    : Nodes, Trias,Quads=        21        19         0

AFLR4    : Generate optimal mesh on surface definition 85
AFLR2    : Nodes, Trias,Quads=        32        41         0
AFLR4    : Nodes, Trias,Quads=        34        45         0

AFLR4    : Generate optimal mesh on surface definition 86
AFLR2    : Nodes, Trias,Quads=       157       216         0
AFLR4    : Nodes, Trias,Quads=       119       140         0

AFLR4    : Generate optimal mesh on surface definition 87
AFLR2    : Nodes, Trias,Quads=        39        51         0
AFLR4    : Nodes, Trias,Quads=        43        59         0

AFLR4    : Generate optimal mesh on surface definition 88
AFLR2    : Nodes, Trias,Quads=        28        36         0
AFLR4    : Nodes, Trias,Quads=        30        40         0

AFLR4    : Generate optimal mesh on surface definition 89
AFLR2    : Nodes, Trias,Quads=       111       158         0
AFLR4    : Nodes, Trias,Quads=        65        66         0

AFLR4    : Generate optimal mesh on surface definition 90
AFLR2    : Nodes, Trias,Quads=        33        41         0
AFLR4    : Nodes, Trias,Quads=        40        55         0

AFLR4    : Generate optimal mesh on surface definition 91
AFLR2    : Nodes, Trias,Quads=       329       566         0
AFLR4    : Nodes, Trias,Quads=       305       518         0

AFLR4    : Generate optimal mesh on surface definition 92
AFLR2    : Nodes, Trias,Quads=       245       414         0
AFLR4    : Nodes, Trias,Quads=       225       374         0

AFLR4    : Generate optimal mesh on surface definition 93
AFLR2    : Nodes, Trias,Quads=        50        67         0
AFLR4    : Nodes, Trias,Quads=        51        69         0

AFLR4    : Generate optimal mesh on surface definition 94
AFLR2    : Nodes, Trias,Quads=       114       155         0
AFLR4    : Nodes, Trias,Quads=        78        83         0

AFLR4    : Generate optimal mesh on surface definition 95
AFLR2    : Nodes, Trias,Quads=        28        36         0
AFLR4    : Nodes, Trias,Quads=        31        42         0

AFLR4    : Generate optimal mesh on surface definition 96
AFLR2    : Nodes, Trias,Quads=        32        41         0
AFLR4    : Nodes, Trias,Quads=        35        47         0

AFLR4    : Generate optimal mesh on surface definition 97
AFLR2    : Nodes, Trias,Quads=       148       208         0
AFLR4    : Nodes, Trias,Quads=       112       136         0

AFLR4    : Generate optimal mesh on surface definition 98
AFLR2    : Nodes, Trias,Quads=        33        42         0
AFLR4    : Nodes, Trias,Quads=        34        44         0

AFLR4    : Generate optimal mesh on surface definition 99
AFLR2    : Nodes, Trias,Quads=       251       422         0
AFLR4    : Nodes, Trias,Quads=       208       336         0

AFLR4    : Generate optimal mesh on surface definition 100
AFLR2    : Nodes, Trias,Quads=       332       556         0
AFLR4    : Nodes, Trias,Quads=       250       392         0

AFLR4    : Generate optimal mesh on surface definition 101
AFLR2    : Nodes, Trias,Quads=       295       490         0
AFLR4    : Nodes, Trias,Quads=       216       332         0

AFLR4    : Generate optimal mesh on surface definition 102
AFLR2    : Nodes, Trias,Quads=       207       341         0
AFLR4    : Nodes, Trias,Quads=       174       275         0

AFLR4    : Generate optimal mesh on surface definition 103
AFLR2    : Nodes, Trias,Quads=       327       547         0
AFLR4    : Nodes, Trias,Quads=       240       373         0

AFLR4    : Generate optimal mesh on surface definition 104
AFLR2    : Nodes, Trias,Quads=       208       343         0
AFLR4    : Nodes, Trias,Quads=       173       273         0

AFLR4    : Generate optimal mesh on surface definition 105
AFLR2    : Nodes, Trias,Quads=       248       416         0
AFLR4    : Nodes, Trias,Quads=       208       336         0

AFLR4    : Generate optimal mesh on surface definition 106
AFLR2    : Nodes, Trias,Quads=       297       493         0
AFLR4    : Nodes, Trias,Quads=       225       349         0

AFLR4    : Generate optimal mesh on surface definition 107
AFLR2    : Nodes, Trias,Quads=        40        57         0
AFLR4    : Nodes, Trias,Quads=        30        37         0

AFLR4    : Generate optimal mesh on surface definition 108
AFLR2    : Nodes, Trias,Quads=        40        57         0
AFLR4    : Nodes, Trias,Quads=        31        39         0

AFLR4    : Generate optimal mesh on surface definition 109
AFLR2    : Nodes, Trias,Quads=        73       116         0
AFLR4    : Nodes, Trias,Quads=        68       106         0

AFLR4    : Generate optimal mesh on surface definition 110
AFLR2    : Nodes, Trias,Quads=        73       116         0
AFLR4    : Nodes, Trias,Quads=        68       106         0

AFLR4    : Generate optimal mesh on surface definition 111
AFLR2    : Nodes, Trias,Quads=        73       116         0
AFLR4    : Nodes, Trias,Quads=        68       106         0

AFLR4    : Generate optimal mesh on surface definition 112
AFLR2    : Nodes, Trias,Quads=        73       116         0
AFLR4    : Nodes, Trias,Quads=        68       106         0

AFLR4    : Generate optimal mesh on surface definition 113
AFLR2    : Nodes, Trias,Quads=        73       116         0
AFLR4    : Nodes, Trias,Quads=        68       106         0

AFLR4    : Generate optimal mesh on surface definition 114
AFLR2    : Nodes, Trias,Quads=        73       116         0
AFLR4    : Nodes, Trias,Quads=        68       106         0

DGEOM    : Add surface definitions to composite definition 0
DGEOM    : Glue composite surface definition 0
DGEOM    : Nodes,Faces,BEdges=     39754     79500      9980

AFLR4    : Curvature BG Surface Grid Generation

AFLR4    : Nodes, Faces      =     39754     79500

AFLR4    : Surface Grid Generation

AFLR4    : Generate optimal mesh on surface definition 1
AFLR2    : Nodes, Trias,Quads=       397       713         0
AFLR4    : Nodes, Trias,Quads=       416       751         0

AFLR4    : Generate optimal mesh on surface definition 2
AFLR2    : Nodes, Trias,Quads=       387       691         0
AFLR4    : Nodes, Trias,Quads=       346       609         0

AFLR4    : Generate optimal mesh on surface definition 3
AFLR2    : Nodes, Trias,Quads=       396       711         0
AFLR4    : Nodes, Trias,Quads=       417       753         0

AFLR4    : Generate optimal mesh on surface definition 4
AFLR2    : Nodes, Trias,Quads=       388       693         0
AFLR4    : Nodes, Trias,Quads=       344       605         0

AFLR4    : Generate optimal mesh on surface definition 5
AFLR2    : Nodes, Trias,Quads=       395       709         0
AFLR4    : Nodes, Trias,Quads=       416       751         0

AFLR4    : Generate optimal mesh on surface definition 6
AFLR2    : Nodes, Trias,Quads=       388       693         0
AFLR4    : Nodes, Trias,Quads=       344       605         0

AFLR4    : Generate optimal mesh on surface definition 7
AFLR2    : Nodes, Trias,Quads=       395       709         0
AFLR4    : Nodes, Trias,Quads=       416       751         0

AFLR4    : Generate optimal mesh on surface definition 8
AFLR2    : Nodes, Trias,Quads=       387       691         0
AFLR4    : Nodes, Trias,Quads=       346       609         0

AFLR4    : Generate optimal mesh on surface definition 9
AFLR2    : Nodes, Trias,Quads=        18        23         0
AFLR4    : Nodes, Trias,Quads=        11         9         0

AFLR4    : Generate optimal mesh on surface definition 10
AFLR2    : Nodes, Trias,Quads=        18        23         0
AFLR4    : Nodes, Trias,Quads=        11         9         0

AFLR4    : Generate optimal mesh on surface definition 11
AFLR2    : Nodes, Trias,Quads=        56        77         0
AFLR4    : Nodes, Trias,Quads=        33        31         0

AFLR4    : Generate optimal mesh on surface definition 12
AFLR2    : Nodes, Trias,Quads=        28        37         0
AFLR4    : Nodes, Trias,Quads=        25        31         0

AFLR4    : Generate optimal mesh on surface definition 13
AFLR2    : Nodes, Trias,Quads=        29        38         0
AFLR4    : Nodes, Trias,Quads=        28        36         0

AFLR4    : Generate optimal mesh on surface definition 14
AFLR2    : Nodes, Trias,Quads=        56        77         0
AFLR4    : Nodes, Trias,Quads=        33        31         0

AFLR4    : Generate optimal mesh on surface definition 15
AFLR2    : Nodes, Trias,Quads=        60        80         0
AFLR4    : Nodes, Trias,Quads=        59        78         0

AFLR4    : Generate optimal mesh on surface definition 16
AFLR2    : Nodes, Trias,Quads=      1730      3226         0
AFLR4    : Nodes, Trias,Quads=      1387      2540         0

AFLR4    : Generate optimal mesh on surface definition 17
AFLR2    : Nodes, Trias,Quads=       100       140         0
AFLR4    : Nodes, Trias,Quads=        58        56         0

AFLR4    : Generate optimal mesh on surface definition 18
AFLR2    : Nodes, Trias,Quads=       271       470         0
AFLR4    : Nodes, Trias,Quads=       208       344         0

AFLR4    : Generate optimal mesh on surface definition 19
AFLR2    : Nodes, Trias,Quads=        57        75         0
AFLR4    : Nodes, Trias,Quads=        61        83         0

AFLR4    : Generate optimal mesh on surface definition 20
AFLR2    : Nodes, Trias,Quads=      1821      3408         0
AFLR4    : Nodes, Trias,Quads=      1413      2592         0

AFLR4    : Generate optimal mesh on surface definition 21
AFLR2    : Nodes, Trias,Quads=        38        49         0
AFLR4    : Nodes, Trias,Quads=        25        23         0

AFLR4    : Generate optimal mesh on surface definition 22
AFLR2    : Nodes, Trias,Quads=        15        19         0
AFLR4    : Nodes, Trias,Quads=        15        19         0

AFLR4    : Generate optimal mesh on surface definition 23
AFLR2    : Nodes, Trias,Quads=      1020      1868         0
AFLR4    : Nodes, Trias,Quads=      1567      2962         0

AFLR4    : Generate optimal mesh on surface definition 24
AFLR2    : Nodes, Trias,Quads=      3285      6257         0
AFLR4    : Nodes, Trias,Quads=      2655      4997         0

AFLR4    : Generate optimal mesh on surface definition 25
AFLR2    : Nodes, Trias,Quads=       268       463         0
AFLR4    : Nodes, Trias,Quads=       211       349         0

AFLR4    : Generate optimal mesh on surface definition 26
AFLR2    : Nodes, Trias,Quads=        96       133         0
AFLR4    : Nodes, Trias,Quads=        57        55         0

AFLR4    : Generate optimal mesh on surface definition 27
AFLR2    : Nodes, Trias,Quads=        15        18         0
AFLR4    : Nodes, Trias,Quads=        15        18         0

AFLR4    : Generate optimal mesh on surface definition 28
AFLR2    : Nodes, Trias,Quads=      1004      1837         0
AFLR4    : Nodes, Trias,Quads=      1549      2927         0

AFLR4    : Generate optimal mesh on surface definition 29
AFLR2    : Nodes, Trias,Quads=       106       170         0
AFLR4    : Nodes, Trias,Quads=       116       190         0

AFLR4    : Generate optimal mesh on surface definition 30
AFLR2    : Nodes, Trias,Quads=      1642      2942         0
AFLR4    : Nodes, Trias,Quads=      3189      6036         0

AFLR4    : Generate optimal mesh on surface definition 31
AFLR2    : Nodes, Trias,Quads=      3518      6723         0
AFLR4    : Nodes, Trias,Quads=      2629      4945         0

AFLR4    : Generate optimal mesh on surface definition 32
AFLR2    : Nodes, Trias,Quads=      2078      3899         0
AFLR4    : Nodes, Trias,Quads=      1693      3129         0

AFLR4    : Generate optimal mesh on surface definition 33
AFLR2    : Nodes, Trias,Quads=      1089      1958         0
AFLR4    : Nodes, Trias,Quads=      2728      5236         0

AFLR4    : Generate optimal mesh on surface definition 34
AFLR2    : Nodes, Trias,Quads=      1551      2878         0
AFLR4    : Nodes, Trias,Quads=      1231      2238         0

AFLR4    : Generate optimal mesh on surface definition 35
AFLR2    : Nodes, Trias,Quads=      1791      3350         0
AFLR4    : Nodes, Trias,Quads=      1414      2596         0

AFLR4    : Generate optimal mesh on surface definition 36
AFLR2    : Nodes, Trias,Quads=      1643      2944         0
AFLR4    : Nodes, Trias,Quads=      3170      5998         0

AFLR4    : Generate optimal mesh on surface definition 37
AFLR2    : Nodes, Trias,Quads=      2194      4132         0
AFLR4    : Nodes, Trias,Quads=      2357      4458         0

AFLR4    : Generate optimal mesh on surface definition 38
AFLR2    : Nodes, Trias,Quads=      3014      5761         0
AFLR4    : Nodes, Trias,Quads=      2581      4895         0

AFLR4    : Generate optimal mesh on surface definition 39
AFLR2    : Nodes, Trias,Quads=      2124      3993         0
AFLR4    : Nodes, Trias,Quads=      1733      3211         0

AFLR4    : Generate optimal mesh on surface definition 40
AFLR2    : Nodes, Trias,Quads=      1090      1960         0
AFLR4    : Nodes, Trias,Quads=      2713      5206         0

AFLR4    : Generate optimal mesh on surface definition 41
AFLR2    : Nodes, Trias,Quads=        60        81         0
AFLR4    : Nodes, Trias,Quads=        37        35         0

AFLR4    : Generate optimal mesh on surface definition 42
AFLR2    : Nodes, Trias,Quads=        37        47         0
AFLR4    : Nodes, Trias,Quads=        25        23         0

AFLR4    : Generate optimal mesh on surface definition 43
AFLR2    : Nodes, Trias,Quads=        15        18         0
AFLR4    : Nodes, Trias,Quads=        16        20         0

AFLR4    : Generate optimal mesh on surface definition 44
AFLR2    : Nodes, Trias,Quads=        71       100         0
AFLR4    : Nodes, Trias,Quads=        40        38         0

AFLR4    : Generate optimal mesh on surface definition 45
AFLR2    : Nodes, Trias,Quads=        48        63         0
AFLR4    : Nodes, Trias,Quads=        51        69         0

AFLR4    : Generate optimal mesh on surface definition 46
AFLR2    : Nodes, Trias,Quads=        57        75         0
AFLR4    : Nodes, Trias,Quads=        62        85         0

AFLR4    : Generate optimal mesh on surface definition 47
AFLR2    : Nodes, Trias,Quads=        85       111         0
AFLR4    : Nodes, Trias,Quads=        57        55         0

AFLR4    : Generate optimal mesh on surface definition 48
AFLR2    : Nodes, Trias,Quads=        15        18         0
AFLR4    : Nodes, Trias,Quads=        15        18         0

AFLR4    : Generate optimal mesh on surface definition 49
AFLR2    : Nodes, Trias,Quads=      3046      5824         0
AFLR4    : Nodes, Trias,Quads=      2604      4940         0

AFLR4    : Generate optimal mesh on surface definition 50
AFLR2    : Nodes, Trias,Quads=      2207      4159         0
AFLR4    : Nodes, Trias,Quads=      2346      4437         0

AFLR4    : Generate optimal mesh on surface definition 51
AFLR2    : Nodes, Trias,Quads=        53        77         0
AFLR4    : Nodes, Trias,Quads=        41        53         0

AFLR4    : Generate optimal mesh on surface definition 52
AFLR2    : Nodes, Trias,Quads=       121       160         0
AFLR4    : Nodes, Trias,Quads=        99       116         0

AFLR4    : Generate optimal mesh on surface definition 53
AFLR2    : Nodes, Trias,Quads=        55        80         0
AFLR4    : Nodes, Trias,Quads=        44        58         0

AFLR4    : Generate optimal mesh on surface definition 54
AFLR2    : Nodes, Trias,Quads=      4380      8388         0
AFLR4    : Nodes, Trias,Quads=      2756      5140         0

AFLR4    : Generate optimal mesh on surface definition 55
AFLR2    : Nodes, Trias,Quads=      3999      7641         0
AFLR4    : Nodes, Trias,Quads=      2398      4439         0

AFLR4    : Generate optimal mesh on surface definition 56
AFLR2    : Nodes, Trias,Quads=        78       120         0
AFLR4    : Nodes, Trias,Quads=        51        66         0

AFLR4    : Generate optimal mesh on surface definition 57
AFLR2    : Nodes, Trias,Quads=       164       223         0
AFLR4    : Nodes, Trias,Quads=       162       219         0

AFLR4    : Generate optimal mesh on surface definition 58
AFLR2    : Nodes, Trias,Quads=        73       112         0
AFLR4    : Nodes, Trias,Quads=        48        62         0

AFLR4    : Generate optimal mesh on surface definition 59
AFLR2    : Nodes, Trias,Quads=       175       291         0
AFLR4    : Nodes, Trias,Quads=       161       263         0

AFLR4    : Generate optimal mesh on surface definition 60
AFLR2    : Nodes, Trias,Quads=       260       448         0
AFLR4    : Nodes, Trias,Quads=       208       344         0

AFLR4    : Generate optimal mesh on surface definition 61
AFLR2    : Nodes, Trias,Quads=      4125      7885         0
AFLR4    : Nodes, Trias,Quads=      2506      4647         0

AFLR4    : Generate optimal mesh on surface definition 62
AFLR2    : Nodes, Trias,Quads=        78       120         0
AFLR4    : Nodes, Trias,Quads=        51        66         0

AFLR4    : Generate optimal mesh on surface definition 63
AFLR2    : Nodes, Trias,Quads=       175       244         0
AFLR4    : Nodes, Trias,Quads=       163       220         0

AFLR4    : Generate optimal mesh on surface definition 64
AFLR2    : Nodes, Trias,Quads=        73       112         0
AFLR4    : Nodes, Trias,Quads=        48        62         0

AFLR4    : Generate optimal mesh on surface definition 65
AFLR2    : Nodes, Trias,Quads=        53        77         0
AFLR4    : Nodes, Trias,Quads=        41        53         0

AFLR4    : Generate optimal mesh on surface definition 66
AFLR2    : Nodes, Trias,Quads=       124       169         0
AFLR4    : Nodes, Trias,Quads=       111       143         0

AFLR4    : Generate optimal mesh on surface definition 67
AFLR2    : Nodes, Trias,Quads=        56        82         0
AFLR4    : Nodes, Trias,Quads=        43        56         0

AFLR4    : Generate optimal mesh on surface definition 68
AFLR2    : Nodes, Trias,Quads=      4113      7862         0
AFLR4    : Nodes, Trias,Quads=      2649      4934         0

AFLR4    : Generate optimal mesh on surface definition 69
AFLR2    : Nodes, Trias,Quads=       300       515         0
AFLR4    : Nodes, Trias,Quads=       283       481         0

AFLR4    : Generate optimal mesh on surface definition 70
AFLR2    : Nodes, Trias,Quads=        57        78         0
AFLR4    : Nodes, Trias,Quads=        55        74         0

AFLR4    : Generate optimal mesh on surface definition 71
AFLR2    : Nodes, Trias,Quads=       135       188         0
AFLR4    : Nodes, Trias,Quads=        87        92         0

AFLR4    : Generate optimal mesh on surface definition 72
AFLR2    : Nodes, Trias,Quads=        33        42         0
AFLR4    : Nodes, Trias,Quads=        36        48         0

AFLR4    : Generate optimal mesh on surface definition 73
AFLR2    : Nodes, Trias,Quads=        43        55         0
AFLR4    : Nodes, Trias,Quads=        44        57         0

AFLR4    : Generate optimal mesh on surface definition 74
AFLR2    : Nodes, Trias,Quads=       186       257         0
AFLR4    : Nodes, Trias,Quads=       180       245         0

AFLR4    : Generate optimal mesh on surface definition 75
AFLR2    : Nodes, Trias,Quads=        31        39         0
AFLR4    : Nodes, Trias,Quads=        31        39         0

AFLR4    : Generate optimal mesh on surface definition 76
AFLR2    : Nodes, Trias,Quads=        39        53         0
AFLR4    : Nodes, Trias,Quads=        23        21         0

AFLR4    : Generate optimal mesh on surface definition 77
AFLR2    : Nodes, Trias,Quads=        32        40         0
AFLR4    : Nodes, Trias,Quads=        32        40         0

AFLR4    : Generate optimal mesh on surface definition 78
AFLR2    : Nodes, Trias,Quads=       169       238         0
AFLR4    : Nodes, Trias,Quads=       101       102         0

AFLR4    : Generate optimal mesh on surface definition 79
AFLR2    : Nodes, Trias,Quads=        34        44         0
AFLR4    : Nodes, Trias,Quads=        36        48         0

AFLR4    : Generate optimal mesh on surface definition 80
AFLR2    : Nodes, Trias,Quads=        33        43         0
AFLR4    : Nodes, Trias,Quads=        36        49         0

AFLR4    : Generate optimal mesh on surface definition 81
AFLR2    : Nodes, Trias,Quads=       132       188         0
AFLR4    : Nodes, Trias,Quads=        79        82         0

AFLR4    : Generate optimal mesh on surface definition 82
AFLR2    : Nodes, Trias,Quads=        40        51         0
AFLR4    : Nodes, Trias,Quads=        45        61         0

AFLR4    : Generate optimal mesh on surface definition 83
AFLR2    : Nodes, Trias,Quads=       402       701         0
AFLR4    : Nodes, Trias,Quads=       405       707         0

AFLR4    : Generate optimal mesh on surface definition 84
AFLR2    : Nodes, Trias,Quads=        39        53         0
AFLR4    : Nodes, Trias,Quads=        23        21         0

AFLR4    : Generate optimal mesh on surface definition 85
AFLR2    : Nodes, Trias,Quads=        32        41         0
AFLR4    : Nodes, Trias,Quads=        31        39         0

AFLR4    : Generate optimal mesh on surface definition 86
AFLR2    : Nodes, Trias,Quads=       186       260         0
AFLR4    : Nodes, Trias,Quads=       140       168         0

AFLR4    : Generate optimal mesh on surface definition 87
AFLR2    : Nodes, Trias,Quads=        42        54         0
AFLR4    : Nodes, Trias,Quads=        48        66         0

AFLR4    : Generate optimal mesh on surface definition 88
AFLR2    : Nodes, Trias,Quads=        34        44         0
AFLR4    : Nodes, Trias,Quads=        37        50         0

AFLR4    : Generate optimal mesh on surface definition 89
AFLR2    : Nodes, Trias,Quads=       132       188         0
AFLR4    : Nodes, Trias,Quads=        79        82         0

AFLR4    : Generate optimal mesh on surface definition 90
AFLR2    : Nodes, Trias,Quads=        40        51         0
AFLR4    : Nodes, Trias,Quads=        45        61         0

AFLR4    : Generate optimal mesh on surface definition 91
AFLR2    : Nodes, Trias,Quads=       401       699         0
AFLR4    : Nodes, Trias,Quads=       404       705         0

AFLR4    : Generate optimal mesh on surface definition 92
AFLR2    : Nodes, Trias,Quads=       293       502         0
AFLR4    : Nodes, Trias,Quads=       277       470         0

AFLR4    : Generate optimal mesh on surface definition 93
AFLR2    : Nodes, Trias,Quads=        57        78         0
AFLR4    : Nodes, Trias,Quads=        55        74         0

AFLR4    : Generate optimal mesh on surface definition 94
AFLR2    : Nodes, Trias,Quads=       135       188         0
AFLR4    : Nodes, Trias,Quads=        87        92         0

AFLR4    : Generate optimal mesh on surface definition 95
AFLR2    : Nodes, Trias,Quads=        32        41         0
AFLR4    : Nodes, Trias,Quads=        35        47         0

AFLR4    : Generate optimal mesh on surface definition 96
AFLR2    : Nodes, Trias,Quads=        34        43         0
AFLR4    : Nodes, Trias,Quads=        36        47         0

AFLR4    : Generate optimal mesh on surface definition 97
AFLR2    : Nodes, Trias,Quads=       175       245         0
AFLR4    : Nodes, Trias,Quads=       139       173         0

AFLR4    : Generate optimal mesh on surface definition 98
AFLR2    : Nodes, Trias,Quads=        32        40         0
AFLR4    : Nodes, Trias,Quads=        32        40         0

AFLR4    : Generate optimal mesh on surface definition 99
AFLR2    : Nodes, Trias,Quads=       303       516         0
AFLR4    : Nodes, Trias,Quads=       258       426         0

AFLR4    : Generate optimal mesh on surface definition 100
AFLR2    : Nodes, Trias,Quads=       380       642         0
AFLR4    : Nodes, Trias,Quads=       285       452         0

AFLR4    : Generate optimal mesh on surface definition 101
AFLR2    : Nodes, Trias,Quads=       334       560         0
AFLR4    : Nodes, Trias,Quads=       242       376         0

AFLR4    : Generate optimal mesh on surface definition 102
AFLR2    : Nodes, Trias,Quads=       271       457         0
AFLR4    : Nodes, Trias,Quads=       222       359         0

AFLR4    : Generate optimal mesh on surface definition 103
AFLR2    : Nodes, Trias,Quads=       369       622         0
AFLR4    : Nodes, Trias,Quads=       275       434         0

AFLR4    : Generate optimal mesh on surface definition 104
AFLR2    : Nodes, Trias,Quads=       272       459         0
AFLR4    : Nodes, Trias,Quads=       220       355         0

AFLR4    : Generate optimal mesh on surface definition 105
AFLR2    : Nodes, Trias,Quads=       303       516         0
AFLR4    : Nodes, Trias,Quads=       258       426         0

AFLR4    : Generate optimal mesh on surface definition 106
AFLR2    : Nodes, Trias,Quads=       353       594         0
AFLR4    : Nodes, Trias,Quads=       266       420         0

AFLR4    : Generate optimal mesh on surface definition 107
AFLR2    : Nodes, Trias,Quads=        72       113         0
AFLR4    : Nodes, Trias,Quads=        47        63         0

AFLR4    : Generate optimal mesh on surface definition 108
AFLR2    : Nodes, Trias,Quads=        70       109         0
AFLR4    : Nodes, Trias,Quads=        49        67         0

AFLR4    : Generate optimal mesh on surface definition 109
AFLR2    : Nodes, Trias,Quads=        73       116         0
AFLR4    : Nodes, Trias,Quads=        68       106         0

AFLR4    : Generate optimal mesh on surface definition 110
AFLR2    : Nodes, Trias,Quads=        73       116         0
AFLR4    : Nodes, Trias,Quads=        68       106         0

AFLR4    : Generate optimal mesh on surface definition 111
AFLR2    : Nodes, Trias,Quads=        73       116         0
AFLR4    : Nodes, Trias,Quads=        68       106         0

AFLR4    : Generate optimal mesh on surface definition 112
AFLR2    : Nodes, Trias,Quads=        73       116         0
AFLR4    : Nodes, Trias,Quads=        68       106         0

AFLR4    : Generate optimal mesh on surface definition 113
AFLR2    : Nodes, Trias,Quads=        73       116         0
AFLR4    : Nodes, Trias,Quads=        68       106         0

AFLR4    : Generate optimal mesh on surface definition 114
AFLR2    : Nodes, Trias,Quads=        73       116         0
AFLR4    : Nodes, Trias,Quads=        68       106         0

DGEOM    : Add surface definitions to composite definition 0
DGEOM    : Glue composite surface definition 0
DGEOM    : Nodes,Faces,BEdges=     54863    109718     10706

AFLR4    : Proximity BG Surface Grid Generation

AFLR4    : Nodes, Trias      =     57095    114182
AFLR4    : Nodes, Trias      =     57402    114796

AFLR4    : Surface Grid Generation

AFLR4    : Generate optimal mesh on surface definition 1
AFLR2    : Nodes, Trias,Quads=       779      1451         0
AFLR4    : Nodes, Trias,Quads=       643      1179         0

AFLR4    : Generate optimal mesh on surface definition 2
AFLR2    : Nodes, Trias,Quads=       399       711         0
AFLR4    : Nodes, Trias,Quads=       375       663         0

AFLR4    : Generate optimal mesh on surface definition 3
AFLR2    : Nodes, Trias,Quads=       753      1402         0
AFLR4    : Nodes, Trias,Quads=       682      1260         0

AFLR4    : Generate optimal mesh on surface definition 4
AFLR2    : Nodes, Trias,Quads=       388       692         0
AFLR4    : Nodes, Trias,Quads=       357       630         0

AFLR4    : Generate optimal mesh on surface definition 5
AFLR2    : Nodes, Trias,Quads=       773      1439         0
AFLR4    : Nodes, Trias,Quads=       640      1173         0

AFLR4    : Generate optimal mesh on surface definition 6
AFLR2    : Nodes, Trias,Quads=       400       713         0
AFLR4    : Nodes, Trias,Quads=       372       657         0

AFLR4    : Generate optimal mesh on surface definition 7
AFLR2    : Nodes, Trias,Quads=       751      1398         0
AFLR4    : Nodes, Trias,Quads=       681      1258         0

AFLR4    : Generate optimal mesh on surface definition 8
AFLR2    : Nodes, Trias,Quads=       388       692         0
AFLR4    : Nodes, Trias,Quads=       358       632         0

AFLR4    : Generate optimal mesh on surface definition 9
AFLR2    : Nodes, Trias,Quads=        21        27         0
AFLR4    : Nodes, Trias,Quads=        18        21         0

AFLR4    : Generate optimal mesh on surface definition 10
AFLR2    : Nodes, Trias,Quads=        21        27         0
AFLR4    : Nodes, Trias,Quads=        20        25         0

AFLR4    : Generate optimal mesh on surface definition 11
AFLR2    : Nodes, Trias,Quads=        66        90         0
AFLR4    : Nodes, Trias,Quads=        40        38         0

AFLR4    : Generate optimal mesh on surface definition 12
AFLR2    : Nodes, Trias,Quads=        32        43         0
AFLR4    : Nodes, Trias,Quads=        29        37         0

AFLR4    : Generate optimal mesh on surface definition 13
AFLR2    : Nodes, Trias,Quads=        32        43         0
AFLR4    : Nodes, Trias,Quads=        28        35         0

AFLR4    : Generate optimal mesh on surface definition 14
AFLR2    : Nodes, Trias,Quads=        65        89         0
AFLR4    : Nodes, Trias,Quads=        39        37         0

AFLR4    : Generate optimal mesh on surface definition 15
AFLR2    : Nodes, Trias,Quads=        61        80         0
AFLR4    : Nodes, Trias,Quads=        62        82         0

AFLR4    : Generate optimal mesh on surface definition 16
AFLR2    : Nodes, Trias,Quads=      2575      4845         0
AFLR4    : Nodes, Trias,Quads=      2031      3757         0

AFLR4    : Generate optimal mesh on surface definition 17
AFLR2    : Nodes, Trias,Quads=       109       150         0
AFLR4    : Nodes, Trias,Quads=        66        64         0

AFLR4    : Generate optimal mesh on surface definition 18
AFLR2    : Nodes, Trias,Quads=       298       518         0
AFLR4    : Nodes, Trias,Quads=       228       378         0

AFLR4    : Generate optimal mesh on surface definition 19
AFLR2    : Nodes, Trias,Quads=        62        81         0
AFLR4    : Nodes, Trias,Quads=        62        81         0

AFLR4    : Generate optimal mesh on surface definition 20
AFLR2    : Nodes, Trias,Quads=      2647      4991         0
AFLR4    : Nodes, Trias,Quads=      2128      3953         0

AFLR4    : Generate optimal mesh on surface definition 21
AFLR2    : Nodes, Trias,Quads=        39        50         0
AFLR4    : Nodes, Trias,Quads=        26        24         0

AFLR4    : Generate optimal mesh on surface definition 22
AFLR2    : Nodes, Trias,Quads=        19        25         0
AFLR4    : Nodes, Trias,Quads=        19        25         0

AFLR4    : Generate optimal mesh on surface definition 23
AFLR2    : Nodes, Trias,Quads=      2173      4081         0
AFLR4    : Nodes, Trias,Quads=      1920      3575         0

AFLR4    : Generate optimal mesh on surface definition 24
AFLR2    : Nodes, Trias,Quads=      4843      9261         0
AFLR4    : Nodes, Trias,Quads=      3472      6519         0

AFLR4    : Generate optimal mesh on surface definition 25
AFLR2    : Nodes, Trias,Quads=       310       540         0
AFLR4    : Nodes, Trias,Quads=       242       404         0

AFLR4    : Generate optimal mesh on surface definition 26
AFLR2    : Nodes, Trias,Quads=       106       145         0
AFLR4    : Nodes, Trias,Quads=        65        63         0

AFLR4    : Generate optimal mesh on surface definition 27
AFLR2    : Nodes, Trias,Quads=        18        22         0
AFLR4    : Nodes, Trias,Quads=        19        24         0

AFLR4    : Generate optimal mesh on surface definition 28
AFLR2    : Nodes, Trias,Quads=      2233      4200         0
AFLR4    : Nodes, Trias,Quads=      1939      3612         0

AFLR4    : Generate optimal mesh on surface definition 29
AFLR2    : Nodes, Trias,Quads=       106       170         0
AFLR4    : Nodes, Trias,Quads=       120       198         0

AFLR4    : Generate optimal mesh on surface definition 30
AFLR2    : Nodes, Trias,Quads=      3806      7035         0
AFLR4    : Nodes, Trias,Quads=      4864      9151         0

AFLR4    : Generate optimal mesh on surface definition 31
AFLR2    : Nodes, Trias,Quads=      4917      9413         0
AFLR4    : Nodes, Trias,Quads=      3455      6489         0

AFLR4    : Generate optimal mesh on surface definition 32
AFLR2    : Nodes, Trias,Quads=      2589      4890         0
AFLR4    : Nodes, Trias,Quads=      1963      3638         0

AFLR4    : Generate optimal mesh on surface definition 33
AFLR2    : Nodes, Trias,Quads=      2220      4140         0
AFLR4    : Nodes, Trias,Quads=      2591      4882         0

AFLR4    : Generate optimal mesh on surface definition 34
AFLR2    : Nodes, Trias,Quads=      2344      4396         0
AFLR4    : Nodes, Trias,Quads=      1845      3398         0

AFLR4    : Generate optimal mesh on surface definition 35
AFLR2    : Nodes, Trias,Quads=      2659      5015         0
AFLR4    : Nodes, Trias,Quads=      2130      3957         0

AFLR4    : Generate optimal mesh on surface definition 36
AFLR2    : Nodes, Trias,Quads=      3827      7075         0
AFLR4    : Nodes, Trias,Quads=      4860      9141         0

AFLR4    : Generate optimal mesh on surface definition 37
AFLR2    : Nodes, Trias,Quads=      5597     10778         0
AFLR4    : Nodes, Trias,Quads=      3975      7534         0

AFLR4    : Generate optimal mesh on surface definition 38
AFLR2    : Nodes, Trias,Quads=      3935      7561         0
AFLR4    : Nodes, Trias,Quads=      2905      5501         0

AFLR4    : Generate optimal mesh on surface definition 39
AFLR2    : Nodes, Trias,Quads=      2618      4948         0
AFLR4    : Nodes, Trias,Quads=      2017      3746         0

AFLR4    : Generate optimal mesh on surface definition 40
AFLR2    : Nodes, Trias,Quads=      2224      4148         0
AFLR4    : Nodes, Trias,Quads=      2603      4906         0

AFLR4    : Generate optimal mesh on surface definition 41
AFLR2    : Nodes, Trias,Quads=        62        83         0
AFLR4    : Nodes, Trias,Quads=        39        37         0

AFLR4    : Generate optimal mesh on surface definition 42
AFLR2    : Nodes, Trias,Quads=        39        50         0
AFLR4    : Nodes, Trias,Quads=        26        24         0

AFLR4    : Generate optimal mesh on surface definition 43
AFLR2    : Nodes, Trias,Quads=        18        22         0
AFLR4    : Nodes, Trias,Quads=        19        24         0

AFLR4    : Generate optimal mesh on surface definition 44
AFLR2    : Nodes, Trias,Quads=        86       119         0
AFLR4    : Nodes, Trias,Quads=        51        49         0

AFLR4    : Generate optimal mesh on surface definition 45
AFLR2    : Nodes, Trias,Quads=        54        71         0
AFLR4    : Nodes, Trias,Quads=        58        79         0

AFLR4    : Generate optimal mesh on surface definition 46
AFLR2    : Nodes, Trias,Quads=        61        80         0
AFLR4    : Nodes, Trias,Quads=        62        82         0

AFLR4    : Generate optimal mesh on surface definition 47
AFLR2    : Nodes, Trias,Quads=       106       145         0
AFLR4    : Nodes, Trias,Quads=        65        63         0

AFLR4    : Generate optimal mesh on surface definition 48
AFLR2    : Nodes, Trias,Quads=        18        22         0
AFLR4    : Nodes, Trias,Quads=        19        24         0

AFLR4    : Generate optimal mesh on surface definition 49
AFLR2    : Nodes, Trias,Quads=      3946      7581         0
AFLR4    : Nodes, Trias,Quads=      2941      5571         0

AFLR4    : Generate optimal mesh on surface definition 50
AFLR2    : Nodes, Trias,Quads=      5413     10408         0
AFLR4    : Nodes, Trias,Quads=      3958      7498         0

AFLR4    : Generate optimal mesh on surface definition 51
AFLR2    : Nodes, Trias,Quads=        62        92         0
AFLR4    : Nodes, Trias,Quads=        45        58         0

AFLR4    : Generate optimal mesh on surface definition 52
AFLR2    : Nodes, Trias,Quads=       127       168         0
AFLR4    : Nodes, Trias,Quads=       120       154         0

AFLR4    : Generate optimal mesh on surface definition 53
AFLR2    : Nodes, Trias,Quads=        58        85         0
AFLR4    : Nodes, Trias,Quads=        44        57         0

AFLR4    : Generate optimal mesh on surface definition 54
AFLR2    : Nodes, Trias,Quads=      5057      9716         0
AFLR4    : Nodes, Trias,Quads=      2994      5590         0

AFLR4    : Generate optimal mesh on surface definition 55
AFLR2    : Nodes, Trias,Quads=      4633      8888         0
AFLR4    : Nodes, Trias,Quads=      2620      4862         0

AFLR4    : Generate optimal mesh on surface definition 56
AFLR2    : Nodes, Trias,Quads=        88       138         0
AFLR4    : Nodes, Trias,Quads=        54        70         0

AFLR4    : Generate optimal mesh on surface definition 57
AFLR2    : Nodes, Trias,Quads=       198       270         0
AFLR4    : Nodes, Trias,Quads=       204       282         0

AFLR4    : Generate optimal mesh on surface definition 58
AFLR2    : Nodes, Trias,Quads=        76       117         0
AFLR4    : Nodes, Trias,Quads=        49        63         0

AFLR4    : Generate optimal mesh on surface definition 59
AFLR2    : Nodes, Trias,Quads=       234       399         0
AFLR4    : Nodes, Trias,Quads=       188       307         0

AFLR4    : Generate optimal mesh on surface definition 60
AFLR2    : Nodes, Trias,Quads=       294       509         0
AFLR4    : Nodes, Trias,Quads=       234       389         0

AFLR4    : Generate optimal mesh on surface definition 61
AFLR2    : Nodes, Trias,Quads=      4681      8974         0
AFLR4    : Nodes, Trias,Quads=      2722      5056         0

AFLR4    : Generate optimal mesh on surface definition 62
AFLR2    : Nodes, Trias,Quads=        87       136         0
AFLR4    : Nodes, Trias,Quads=        54        70         0

AFLR4    : Generate optimal mesh on surface definition 63
AFLR2    : Nodes, Trias,Quads=       205       284         0
AFLR4    : Nodes, Trias,Quads=       195       264         0

AFLR4    : Generate optimal mesh on surface definition 64
AFLR2    : Nodes, Trias,Quads=        76       117         0
AFLR4    : Nodes, Trias,Quads=        50        65         0

AFLR4    : Generate optimal mesh on surface definition 65
AFLR2    : Nodes, Trias,Quads=        62        92         0
AFLR4    : Nodes, Trias,Quads=        46        60         0

AFLR4    : Generate optimal mesh on surface definition 66
AFLR2    : Nodes, Trias,Quads=       138       190         0
AFLR4    : Nodes, Trias,Quads=       127       168         0

AFLR4    : Generate optimal mesh on surface definition 67
AFLR2    : Nodes, Trias,Quads=        62        92         0
AFLR4    : Nodes, Trias,Quads=        46        60         0

AFLR4    : Generate optimal mesh on surface definition 68
AFLR2    : Nodes, Trias,Quads=      4678      8970         0
AFLR4    : Nodes, Trias,Quads=      2893      5400         0

AFLR4    : Generate optimal mesh on surface definition 69
AFLR2    : Nodes, Trias,Quads=       350       608         0
AFLR4    : Nodes, Trias,Quads=       324       556         0

AFLR4    : Generate optimal mesh on surface definition 70
AFLR2    : Nodes, Trias,Quads=        70       101         0
AFLR4    : Nodes, Trias,Quads=        62        85         0

AFLR4    : Generate optimal mesh on surface definition 71
AFLR2    : Nodes, Trias,Quads=       149       207         0
AFLR4    : Nodes, Trias,Quads=        95        99         0

AFLR4    : Generate optimal mesh on surface definition 72
AFLR2    : Nodes, Trias,Quads=        36        46         0
AFLR4    : Nodes, Trias,Quads=        38        50         0

AFLR4    : Generate optimal mesh on surface definition 73
AFLR2    : Nodes, Trias,Quads=        50        67         0
AFLR4    : Nodes, Trias,Quads=        48        63         0

AFLR4    : Generate optimal mesh on surface definition 74
AFLR2    : Nodes, Trias,Quads=       220       305         0
AFLR4    : Nodes, Trias,Quads=       209       283         0

AFLR4    : Generate optimal mesh on surface definition 75
AFLR2    : Nodes, Trias,Quads=        31        39         0
AFLR4    : Nodes, Trias,Quads=        31        39         0

AFLR4    : Generate optimal mesh on surface definition 76
AFLR2    : Nodes, Trias,Quads=        39        50         0
AFLR4    : Nodes, Trias,Quads=        26        24         0

AFLR4    : Generate optimal mesh on surface definition 77
AFLR2    : Nodes, Trias,Quads=        32        40         0
AFLR4    : Nodes, Trias,Quads=        33        42         0

AFLR4    : Generate optimal mesh on surface definition 78
AFLR2    : Nodes, Trias,Quads=       196       279         0
AFLR4    : Nodes, Trias,Quads=       113       113         0

AFLR4    : Generate optimal mesh on surface definition 79
AFLR2    : Nodes, Trias,Quads=        35        45         0
AFLR4    : Nodes, Trias,Quads=        38        51         0

AFLR4    : Generate optimal mesh on surface definition 80
AFLR2    : Nodes, Trias,Quads=        36        46         0
AFLR4    : Nodes, Trias,Quads=        36        46         0

AFLR4    : Generate optimal mesh on surface definition 81
AFLR2    : Nodes, Trias,Quads=       157       225         0
AFLR4    : Nodes, Trias,Quads=        95       101         0

AFLR4    : Generate optimal mesh on surface definition 82
AFLR2    : Nodes, Trias,Quads=        47        63         0
AFLR4    : Nodes, Trias,Quads=        46        61         0

AFLR4    : Generate optimal mesh on surface definition 83
AFLR2    : Nodes, Trias,Quads=       520       923         0
AFLR4    : Nodes, Trias,Quads=       508       899         0

AFLR4    : Generate optimal mesh on surface definition 84
AFLR2    : Nodes, Trias,Quads=        39        50         0
AFLR4    : Nodes, Trias,Quads=        26        24         0

AFLR4    : Generate optimal mesh on surface definition 85
AFLR2    : Nodes, Trias,Quads=        32        41         0
AFLR4    : Nodes, Trias,Quads=        31        39         0

AFLR4    : Generate optimal mesh on surface definition 86
AFLR2    : Nodes, Trias,Quads=       199       273         0
AFLR4    : Nodes, Trias,Quads=       152       179         0

AFLR4    : Generate optimal mesh on surface definition 87
AFLR2    : Nodes, Trias,Quads=        51        69         0
AFLR4    : Nodes, Trias,Quads=        48        63         0

AFLR4    : Generate optimal mesh on surface definition 88
AFLR2    : Nodes, Trias,Quads=        37        47         0
AFLR4    : Nodes, Trias,Quads=        41        55         0

AFLR4    : Generate optimal mesh on surface definition 89
AFLR2    : Nodes, Trias,Quads=       159       229         0
AFLR4    : Nodes, Trias,Quads=        95       101         0

AFLR4    : Generate optimal mesh on surface definition 90
AFLR2    : Nodes, Trias,Quads=        46        61         0
AFLR4    : Nodes, Trias,Quads=        46        61         0

AFLR4    : Generate optimal mesh on surface definition 91
AFLR2    : Nodes, Trias,Quads=       516       915         0
AFLR4    : Nodes, Trias,Quads=       504       891         0

AFLR4    : Generate optimal mesh on surface definition 92
AFLR2    : Nodes, Trias,Quads=       354       616         0
AFLR4    : Nodes, Trias,Quads=       320       548         0

AFLR4    : Generate optimal mesh on surface definition 93
AFLR2    : Nodes, Trias,Quads=        70       101         0
AFLR4    : Nodes, Trias,Quads=        62        85         0

AFLR4    : Generate optimal mesh on surface definition 94
AFLR2    : Nodes, Trias,Quads=       140       190         0
AFLR4    : Nodes, Trias,Quads=        96       102         0

AFLR4    : Generate optimal mesh on surface definition 95
AFLR2    : Nodes, Trias,Quads=        34        44         0
AFLR4    : Nodes, Trias,Quads=        35        46         0

AFLR4    : Generate optimal mesh on surface definition 96
AFLR2    : Nodes, Trias,Quads=        36        47         0
AFLR4    : Nodes, Trias,Quads=        37        49         0

AFLR4    : Generate optimal mesh on surface definition 97
AFLR2    : Nodes, Trias,Quads=       204       286         0
AFLR4    : Nodes, Trias,Quads=       165       208         0

AFLR4    : Generate optimal mesh on surface definition 98
AFLR2    : Nodes, Trias,Quads=        32        40         0
AFLR4    : Nodes, Trias,Quads=        34        44         0

AFLR4    : Generate optimal mesh on surface definition 99
AFLR2    : Nodes, Trias,Quads=       344       591         0
AFLR4    : Nodes, Trias,Quads=       292       487         0

AFLR4    : Generate optimal mesh on surface definition 100
AFLR2    : Nodes, Trias,Quads=       442       755         0
AFLR4    : Nodes, Trias,Quads=       340       551         0

AFLR4    : Generate optimal mesh on surface definition 101
AFLR2    : Nodes, Trias,Quads=       377       638         0
AFLR4    : Nodes, Trias,Quads=       268       420         0

AFLR4    : Generate optimal mesh on surface definition 102
AFLR2    : Nodes, Trias,Quads=       327       559         0
AFLR4    : Nodes, Trias,Quads=       273       451         0

AFLR4    : Generate optimal mesh on surface definition 103
AFLR2    : Nodes, Trias,Quads=       419       714         0
AFLR4    : Nodes, Trias,Quads=       304       484         0

AFLR4    : Generate optimal mesh on surface definition 104
AFLR2    : Nodes, Trias,Quads=       326       557         0
AFLR4    : Nodes, Trias,Quads=       271       447         0

AFLR4    : Generate optimal mesh on surface definition 105
AFLR2    : Nodes, Trias,Quads=       345       593         0
AFLR4    : Nodes, Trias,Quads=       292       487         0

AFLR4    : Generate optimal mesh on surface definition 106
AFLR2    : Nodes, Trias,Quads=       409       698         0
AFLR4    : Nodes, Trias,Quads=       301       482         0

AFLR4    : Generate optimal mesh on surface definition 107
AFLR2    : Nodes, Trias,Quads=        89       141         0
AFLR4    : Nodes, Trias,Quads=        66        95         0

AFLR4    : Generate optimal mesh on surface definition 108
AFLR2    : Nodes, Trias,Quads=        94       150         0
AFLR4    : Nodes, Trias,Quads=        67        96         0

AFLR4    : Generate optimal mesh on surface definition 109
AFLR2    : Nodes, Trias,Quads=        73       116         0
AFLR4    : Nodes, Trias,Quads=        68       106         0

AFLR4    : Generate optimal mesh on surface definition 110
AFLR2    : Nodes, Trias,Quads=        73       116         0
AFLR4    : Nodes, Trias,Quads=        68       106         0

AFLR4    : Generate optimal mesh on surface definition 111
AFLR2    : Nodes, Trias,Quads=        73       116         0
AFLR4    : Nodes, Trias,Quads=        68       106         0

AFLR4    : Generate optimal mesh on surface definition 112
AFLR2    : Nodes, Trias,Quads=        73       116         0
AFLR4    : Nodes, Trias,Quads=        68       106         0

AFLR4    : Generate optimal mesh on surface definition 113
AFLR2    : Nodes, Trias,Quads=        73       116         0
AFLR4    : Nodes, Trias,Quads=        68       106         0

AFLR4    : Generate optimal mesh on surface definition 114
AFLR2    : Nodes, Trias,Quads=        73       116         0
AFLR4    : Nodes, Trias,Quads=        68       106         0

DGEOM    : Add surface definitions to composite definition 0
DGEOM    : Glue composite surface definition 0
DGEOM    : Nodes,Faces,BEdges=     69412    138816     13136

OVERALL  : CPU Time          =     3.604   seconds
Body 1 (of 4)
Number of nodes    = 1866
Number of elements = 3732
Number of triangle elements      = 3732
Number of quadrilateral elements = 0
Body 2 (of 4)
Number of nodes    = 1860
Number of elements = 3720
Number of triangle elements      = 3720
Number of quadrilateral elements = 0
Body 3 (of 4)
Number of nodes    = 65366
Number of elements = 130728
Number of triangle elements      = 130728
Number of quadrilateral elements = 0
Body 4 (of 4)
Number of nodes    = 320
Number of elements = 636
Number of triangle elements      = 636
Number of quadrilateral elements = 0
----------------------------
Total number of nodes    = 69412
Total number of elements = 138816
Total number of triangle elements      = 138816
Total number of quadrilateral elements = 0

real	0m39.132s
user	0m44.103s
sys	0m9.326s
+ status=0
+ set +x

=================================================
data/session07/08_aflr4_InviscidTransport.py passed (as expected)
=================================================


=================================================
09_aflr4_aflr3_InviscidWing.py test;
+ python 09_aflr4_aflr3_InviscidWing.py
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/CAPS/training/2023/training.log

MESSAGE:: Building wingOml


MESSAGE:: Building nacelleOml

Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 3
	Name = Nacelle, index = 1
	Name = Wing, index = 2
	Name = Farfield, index = 3
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 4
	Name = Nacelle, index = 1
	Name = leftWing, index = 2
	Name = riteWing, index = 3
	Name = Farfield, index = 4

Getting mesh sizing parameters
	Mesh sizing name - Farfield
	Mesh sizing name - leftWing
	Mesh sizing name - riteWing
	Done getting mesh sizing parameters
 
AFLR2    : ---------------------------------------
AFLR2    : AFLR2 LIBRARY
AFLR2    : ADVANCING-FRONT/LOCAL-RECONNECTION
AFLR2    : TRIA/QUAD GRID GENERATOR
AFLR2    : Version Number 9.18.1
AFLR2    : Version Date   06/11/24 @ 05:52PM
AFLR2    : Compile OS     Darwin 23.5.0 arm64
AFLR2    : Compile Date   06/11/24 @ 05:52PM
AFLR2    : Copyright 1994-2021, D.L. Marcum
AFLR2    : ---------------------------------------
 
AFLR4    : ---------------------------------------
AFLR4    : AFLR4 LIBRARY
AFLR4    : ADVANCING-FRONT/LOCAL-RECONNECTION
AFLR4    : TRIA/QUAD SURFACE GRID GENERATOR
AFLR4    : Version Number 11.5.15
AFLR4    : Version Date   07/19/24 @ 07:04PM
AFLR4    : Compile OS     Darwin 23.5.0 arm64
AFLR4    : Compile Date   07/19/24 @ 07:06PM
AFLR4    : Copyright 1994-2021, D.L. Marcum
AFLR4    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.8.1
EGADS    : ---------------------------------------

EGADS    : EGADS CAD Geometry Setup

EGADS    : Model has 4 Active Bodies

EGADS    : Body 0 is a SolidBody
EGADS    : Body 0 has 1 Shells
EGADS    : Body 0 has 4 Faces
EGADS    : Body 0 has 8 Edges
EGADS    : Body 0 has 4 Loops
EGADS    : Body 0 has 4 Nodes
EGADS    : Body 1 is a SolidBody
EGADS    : Body 1 has 1 Shells
EGADS    : Body 1 has 4 Faces
EGADS    : Body 1 has 8 Edges
EGADS    : Body 1 has 4 Loops
EGADS    : Body 1 has 4 Nodes
EGADS    : Body 2 is a SolidBody
EGADS    : Body 2 has 1 Shells
EGADS    : Body 2 has 10 Faces
EGADS    : Body 2 has 18 Edges
EGADS    : Body 2 has 10 Loops
EGADS    : Body 2 has 10 Nodes
EGADS    : Body 3 is a SolidBody
EGADS    : Body 3 has 1 Shells
EGADS    : Body 3 has 6 Faces
EGADS    : Body 3 has 12 Edges
EGADS    : Body 3 has 6 Loops
EGADS    : Body 3 has 8 Nodes

EGADS    : Check Grid BCs

EGADS    : Grid BCs are OK

EGADS    : Face Neighbor-Faces Information

EGADS    : QC  = Face Quad Combination Flag
EGADS    : IER = Face Isolated Edge Refinement Flag
EGADS    : ER  = Face Edge Refinement Factor
EGADS    :       Not applicable for Faces with a FarField Grid BC.
EGADS    : SF  = Face Scale Factor
EGADS    :       Not applicable for Faces with a FarField Grid BC.

EGADS    :   Face          Body    QC   IER       ER    Scale   Neighbor
EGADS    :     ID  Active    ID  Flag  Flag   Weight   Factor   Faces
EGADS    :      1     Yes     0     0     1        0        1   2 3
EGADS    :      2     Yes     0     0     1        0        1   1 4
EGADS    :      3     Yes     0     0     1        0        1   1 4
EGADS    :      4     Yes     0     0     1        0        1   2 3
EGADS    :      5     Yes     1     0     1        0        1   6 7
EGADS    :      6     Yes     1     0     1        0        1   5 8
EGADS    :      7     Yes     1     0     1        0        1   5 8
EGADS    :      8     Yes     1     0     1        0        1   6 7
EGADS    :      9     Yes     2     0     1        1        1   10 11 14
EGADS    :     10     Yes     2     0     1        1        1   9 12 13
EGADS    :     11     Yes     2     0     1        1        1   9 12 16
EGADS    :     12     Yes     2     0     1        1        1   10 11 13
EGADS    :     13     Yes     2     0     1        1        1   10 12
EGADS    :     14     Yes     2     0     1        1        1   9 15 16
EGADS    :     15     Yes     2     0     1        1        1   14 17 18
EGADS    :     16     Yes     2     0     1        1        1   11 14 17
EGADS    :     17     Yes     2     0     1        1        1   15 16 18
EGADS    :     18     Yes     2     0     1        1        1   15 17
EGADS    :     19     Yes     3     0     1       NA       NA   21 22 23 24
EGADS    :     20     Yes     3     0     1       NA       NA   21 22 23 24
EGADS    :     21     Yes     3     0     1       NA       NA   19 20 23 24
EGADS    :     22     Yes     3     0     1       NA       NA   19 20 23 24
EGADS    :     23     Yes     3     0     1       NA       NA   19 20 21 22
EGADS    :     24     Yes     3     0     1       NA       NA   19 20 21 22

EGADS    : Face Edges Information

EGADS    :   Face   Edges
EGADS    :      1   -1 3 2 -4
EGADS    :      2   -2 5 1 -6
EGADS    :      3   7 4 -8 -3
EGADS    :      4   8 6 -7 -5
EGADS    :      5   9 12 -10 -11
EGADS    :      6   10 14 -9 -13
EGADS    :      7   -15 11 16 -12
EGADS    :      8   -16 13 15 -14
EGADS    :      9   -17 18 19 -20
EGADS    :     10   -21 20 22 -23
EGADS    :     11   -19 24 17 -25
EGADS    :     12   -22 25 21 -26
EGADS    :     13   23 26
EGADS    :     14   27 29 -28 -18
EGADS    :     15   30 32 -31 -29
EGADS    :     16   28 33 -27 -24
EGADS    :     17   31 34 -30 -33
EGADS    :     18   -32 -34
EGADS    :     19   35 36 -37 -38
EGADS    :     20   -39 42 41 -40
EGADS    :     21   43 39 -44 -35
EGADS    :     22   -45 37 46 -41
EGADS    :     23   38 45 -42 -43
EGADS    :     24   -36 44 40 -46

EGADS    : Face Loops Information

EGADS    :   Face   Loops
EGADS    :      1   1
EGADS    :      2   2
EGADS    :      3   3
EGADS    :      4   4
EGADS    :      5   5
EGADS    :      6   6
EGADS    :      7   7
EGADS    :      8   8
EGADS    :      9   9
EGADS    :     10   10
EGADS    :     11   11
EGADS    :     12   12
EGADS    :     13   13
EGADS    :     14   14
EGADS    :     15   15
EGADS    :     16   16
EGADS    :     17   17
EGADS    :     18   18
EGADS    :     19   19
EGADS    :     20   20
EGADS    :     21   21
EGADS    :     22   22
EGADS    :     23   23
EGADS    :     24   24

EGADS    : Loop Edges Information

EGADS    :   Loop  Active   Edges
EGADS    :      1     Yes   -1 3 2 -4
EGADS    :      2     Yes   -2 5 1 -6
EGADS    :      3     Yes   7 4 -8 -3
EGADS    :      4     Yes   8 6 -7 -5
EGADS    :      5     Yes   9 12 -10 -11
EGADS    :      6     Yes   10 14 -9 -13
EGADS    :      7     Yes   -15 11 16 -12
EGADS    :      8     Yes   -16 13 15 -14
EGADS    :      9     Yes   -17 18 19 -20
EGADS    :     10     Yes   -21 20 22 -23
EGADS    :     11     Yes   -19 24 17 -25
EGADS    :     12     Yes   -22 25 21 -26
EGADS    :     13     Yes   23 26
EGADS    :     14     Yes   27 29 -28 -18
EGADS    :     15     Yes   30 32 -31 -29
EGADS    :     16     Yes   28 33 -27 -24
EGADS    :     17     Yes   31 34 -30 -33
EGADS    :     18     Yes   -32 -34
EGADS    :     19     Yes   35 36 -37 -38
EGADS    :     20     Yes   -39 42 41 -40
EGADS    :     21     Yes   43 39 -44 -35
EGADS    :     22     Yes   -45 37 46 -41
EGADS    :     23     Yes   38 45 -42 -43
EGADS    :     24     Yes   -36 44 40 -46

EGADS    : Edge Node, Scale Factor, and Neighbor-Faces Information

EGADS    : ESF = Edge Scale Factor
EGADS    :       Not applicable for DEGENERATE Edges or Edges with a FarField
EGADS    :       Grid BC Neighbor Face.

EGADS    :                                             Neighbor
EGADS    :   Edge  Body  Active Node1 Node2      ESF   Faces
EGADS    :      1     0     Yes     1     2        1   1 2
EGADS    :      2     0     Yes     3     4        1   1 2
EGADS    :      3     0     Yes     1     3        1   1 3
EGADS    :      4     0     Yes     2     4        1   1 3
EGADS    :      5     0     Yes     3     1        1   2 4
EGADS    :      6     0     Yes     4     2        1   2 4
EGADS    :      7     0     Yes     1     2        1   3 4
EGADS    :      8     0     Yes     3     4        1   3 4
EGADS    :      9     1     Yes     5     6        1   5 6
EGADS    :     10     1     Yes     7     8        1   5 6
EGADS    :     11     1     Yes     5     7        1   5 7
EGADS    :     12     1     Yes     6     8        1   5 7
EGADS    :     13     1     Yes     7     5        1   6 8
EGADS    :     14     1     Yes     8     6        1   6 8
EGADS    :     15     1     Yes     5     6        1   7 8
EGADS    :     16     1     Yes     7     8        1   7 8
EGADS    :     17     2     Yes     9    10        1   9 11
EGADS    :     18     2     Yes     9    11        1   9 14
EGADS    :     19     2     Yes    11    12        1   9 11
EGADS    :     20     2     Yes    10    12        1   9 10
EGADS    :     21     2     Yes    10    13        1   10 12
EGADS    :     22     2     Yes    12    14        1   10 12
EGADS    :     23     2     Yes    13    14        1   10 13
EGADS    :     24     2     Yes    11     9        1   11 16
EGADS    :     25     2     Yes    12    10        1   11 12
EGADS    :     26     2     Yes    14    13        1   12 13
EGADS    :     27     2     Yes     9    15        1   14 16
EGADS    :     28     2     Yes    11    16        1   14 16
EGADS    :     29     2     Yes    15    16        1   14 15
EGADS    :     30     2     Yes    15    17        1   15 17
EGADS    :     31     2     Yes    16    18        1   15 17
EGADS    :     32     2     Yes    17    18        1   15 18
EGADS    :     33     2     Yes    16    15        1   16 17
EGADS    :     34     2     Yes    18    17        1   17 18
EGADS    :     35     3     Yes    20    19       NA   19 21
EGADS    :     36     3     Yes    19    21       NA   19 24
EGADS    :     37     3     Yes    22    21       NA   19 22
EGADS    :     38     3     Yes    20    22       NA   19 23
EGADS    :     39     3     Yes    24    23       NA   20 21
EGADS    :     40     3     Yes    23    25       NA   20 24
EGADS    :     41     3     Yes    26    25       NA   20 22
EGADS    :     42     3     Yes    24    26       NA   20 23
EGADS    :     43     3     Yes    20    24       NA   21 23
EGADS    :     44     3     Yes    19    23       NA   21 24
EGADS    :     45     3     Yes    22    26       NA   22 23
EGADS    :     46     3     Yes    21    25       NA   22 24

EGADS    : Node Information

EGADS    :   Node  Active      Coordinates
EGADS    :      1     Yes       90.5173952                0                0
EGADS    :      2     Yes       90.5173952                0                0
EGADS    :      3     Yes       60.5173952                0                0
EGADS    :      4     Yes       60.5173952                0                0
EGADS    :      5     Yes       90.5173952       29.3018771                0
EGADS    :      6     Yes       90.5173952       29.3018771                0
EGADS    :      7     Yes       60.5173952       29.3018771                0
EGADS    :      8     Yes       60.5173952       29.3018771                0
EGADS    :      9     Yes       97.2007855                0                0
EGADS    :     10     Yes       97.9335611                0                0
EGADS    :     11     Yes               50                0                0
EGADS    :     12     Yes       75.3047874                0                0
EGADS    :     13     Yes       123.552357                0        4.7180639
EGADS    :     14     Yes       118.391317                0       3.99272703
EGADS    :     15     Yes       97.9335611       36.1389817                0
EGADS    :     16     Yes       75.3047874       36.1389817                0
EGADS    :     17     Yes       123.552357       97.6729236        4.7180639
EGADS    :     18     Yes       118.391317       97.6729236       3.99272703
EGADS    :     19     Yes                0                0       1947.05079
EGADS    :     20     Yes                0                0                0
EGADS    :     21     Yes                0       1953.45847       1947.05079
EGADS    :     22     Yes                0       1953.45847                0
EGADS    :     23     Yes       2040.21562                0       1947.05079
EGADS    :     24     Yes       2040.21562                0                0
EGADS    :     25     Yes       2040.21562       1953.45847       1947.05079
EGADS    :     26     Yes       2040.21562       1953.45847                0

EGADS    : Face and Edge Match Information

EGADS    : No Face Matches Found

AFLR4    : Surface Mesh Spacing Setup

AFLR4    : Max Bounding Box Length     = 3906.92
AFLR4    : Min Bounding Box Length     = 3906.92
AFLR4    : Max Ref Bounding Box Length = 195.346
AFLR4    : Min Ref Bounding Box Length = 22.2515
AFLR4    : Reference Length            = 21.7051
AFLR4    : BL Thickness                = 0
AFLR4    : FarField Spacing            = 2651.51
AFLR4    : Abs Min Surf Spacing        = 0.0542627
AFLR4    : Min Surf Spacing            = 0.108525
AFLR4    : Max Surf Spacing            = 2.17051
AFLR4    : Global Scale Factor         = 5

AFLR4    : Geometry Definition Information

AFLR4    : Definition              Definition   Composite             Grid BC
AFLR4    :         ID                    Type          ID                Type
AFLR4    :          0     glue-only composite           -                   -
AFLR4    :          1            CAD geometry           0            STD w/BL
AFLR4    :          2            CAD geometry           0            STD w/BL
AFLR4    :          3            CAD geometry           0            STD w/BL
AFLR4    :          4            CAD geometry           0            STD w/BL
AFLR4    :          5            CAD geometry           0            STD w/BL
AFLR4    :          6            CAD geometry           0            STD w/BL
AFLR4    :          7            CAD geometry           0            STD w/BL
AFLR4    :          8            CAD geometry           0            STD w/BL
AFLR4    :          9            CAD geometry           0            STD w/BL
AFLR4    :         10            CAD geometry           0            STD w/BL
AFLR4    :         11            CAD geometry           0            STD w/BL
AFLR4    :         12            CAD geometry           0            STD w/BL
AFLR4    :         13            CAD geometry           0            STD w/BL
AFLR4    :         14            CAD geometry           0            STD w/BL
AFLR4    :         15            CAD geometry           0            STD w/BL
AFLR4    :         16            CAD geometry           0            STD w/BL
AFLR4    :         17            CAD geometry           0            STD w/BL
AFLR4    :         18            CAD geometry           0            STD w/BL
AFLR4    :         19            CAD geometry           0            FARFIELD
AFLR4    :         20            CAD geometry           0            FARFIELD
AFLR4    :         21            CAD geometry           0            FARFIELD
AFLR4    :         22            CAD geometry           0            FARFIELD
AFLR4    :         23            CAD geometry           0            FARFIELD
AFLR4    :         24            CAD geometry           0            FARFIELD

AFLR4    : Case has 2 Proximity Checking Components

AFLR4    : Component 1 includes Definitions 9 10 11 12 13 14 15 16 17 18
AFLR4    : Component 2 includes Definitions 1 2 3 4 5 6 7 8

AFLR4    : Define CAD surface definition 1
AFLR4    : Define CAD surface definition 2
AFLR4    : Define CAD surface definition 3
AFLR4    : Define CAD surface definition 4
AFLR4    : Define CAD surface definition 5
AFLR4    : Define CAD surface definition 6
AFLR4    : Define CAD surface definition 7
AFLR4    : Define CAD surface definition 8
AFLR4    : Define CAD surface definition 9
AFLR4    : Define CAD surface definition 10
AFLR4    : Define CAD surface definition 11
AFLR4    : Define CAD surface definition 12
AFLR4    : Define CAD surface definition 13
AFLR4    : Define CAD surface definition 14
AFLR4    : Define CAD surface definition 15
AFLR4    : Define CAD surface definition 16
AFLR4    : Define CAD surface definition 17
AFLR4    : Define CAD surface definition 18
AFLR4    : Define CAD surface definition 19
AFLR4    : Define CAD surface definition 20
AFLR4    : Define CAD surface definition 21
AFLR4    : Define CAD surface definition 22
AFLR4    : Define CAD surface definition 23
AFLR4    : Define CAD surface definition 24

AFLR4    : Surface Grid Generation

AFLR4    : Generate optimal mesh on surface definition 1
AFLR2    : Nodes, Trias,Quads=       339       605         0
AFLR4    : Nodes, Trias,Quads=       362       651         0

AFLR4    : Generate optimal mesh on surface definition 2
AFLR2    : Nodes, Trias,Quads=       319       563         0
AFLR4    : Nodes, Trias,Quads=       284       493         0

AFLR4    : Generate optimal mesh on surface definition 3
AFLR2    : Nodes, Trias,Quads=       340       607         0
AFLR4    : Nodes, Trias,Quads=       362       651         0

AFLR4    : Generate optimal mesh on surface definition 4
AFLR2    : Nodes, Trias,Quads=       321       567         0
AFLR4    : Nodes, Trias,Quads=       284       493         0

AFLR4    : Generate optimal mesh on surface definition 5
AFLR2    : Nodes, Trias,Quads=       340       607         0
AFLR4    : Nodes, Trias,Quads=       362       651         0

AFLR4    : Generate optimal mesh on surface definition 6
AFLR2    : Nodes, Trias,Quads=       321       567         0
AFLR4    : Nodes, Trias,Quads=       284       493         0

AFLR4    : Generate optimal mesh on surface definition 7
AFLR2    : Nodes, Trias,Quads=       339       605         0
AFLR4    : Nodes, Trias,Quads=       362       651         0

AFLR4    : Generate optimal mesh on surface definition 8
AFLR2    : Nodes, Trias,Quads=       319       563         0
AFLR4    : Nodes, Trias,Quads=       284       493         0

AFLR4    : Generate optimal mesh on surface definition 9
AFLR2    : Nodes, Trias,Quads=      1107      2082         0
AFLR4    : Nodes, Trias,Quads=       685      1238         0

AFLR4    : Generate optimal mesh on surface definition 10
AFLR2    : Nodes, Trias,Quads=      1473      2759         0
AFLR4    : Nodes, Trias,Quads=       721      1255         0

AFLR4    : Generate optimal mesh on surface definition 11
AFLR2    : Nodes, Trias,Quads=      1116      2100         0
AFLR4    : Nodes, Trias,Quads=       671      1210         0

AFLR4    : Generate optimal mesh on surface definition 12
AFLR2    : Nodes, Trias,Quads=      1458      2729         0
AFLR4    : Nodes, Trias,Quads=       714      1241         0

AFLR4    : Generate optimal mesh on surface definition 13
AFLR2    : Nodes, Trias,Quads=        20        24         0
AFLR4    : Nodes, Trias,Quads=        14        12         0

AFLR4    : Generate optimal mesh on surface definition 14
AFLR2    : Nodes, Trias,Quads=      1108      2084         0
AFLR4    : Nodes, Trias,Quads=       683      1234         0

AFLR4    : Generate optimal mesh on surface definition 15
AFLR2    : Nodes, Trias,Quads=      1488      2789         0
AFLR4    : Nodes, Trias,Quads=       714      1241         0

AFLR4    : Generate optimal mesh on surface definition 16
AFLR2    : Nodes, Trias,Quads=      1112      2092         0
AFLR4    : Nodes, Trias,Quads=       653      1174         0

AFLR4    : Generate optimal mesh on surface definition 17
AFLR2    : Nodes, Trias,Quads=      1456      2725         0
AFLR4    : Nodes, Trias,Quads=       708      1229         0

AFLR4    : Generate optimal mesh on surface definition 18
AFLR2    : Nodes, Trias,Quads=        20        24         0
AFLR4    : Nodes, Trias,Quads=        14        12         0

AFLR4    : Generate optimal mesh on surface definition 19
AFLR2    : Nodes, Trias,Quads=         5         4         0
AFLR4    : Nodes, Trias,Quads=         4         2         0

AFLR4    : Generate optimal mesh on surface definition 20
AFLR2    : Nodes, Trias,Quads=         5         4         0
AFLR4    : Nodes, Trias,Quads=         4         2         0

AFLR4    : Generate optimal mesh on surface definition 21
AFLR2    : Nodes, Trias,Quads=         5         4         0
AFLR4    : Nodes, Trias,Quads=         4         2         0

AFLR4    : Generate optimal mesh on surface definition 22
AFLR2    : Nodes, Trias,Quads=         5         4         0
AFLR4    : Nodes, Trias,Quads=         4         2         0

AFLR4    : Generate optimal mesh on surface definition 23
AFLR2    : Nodes, Trias,Quads=         5         4         0
AFLR4    : Nodes, Trias,Quads=         4         2         0

AFLR4    : Generate optimal mesh on surface definition 24
AFLR2    : Nodes, Trias,Quads=         5         4         0
AFLR4    : Nodes, Trias,Quads=         4         2         0

DGEOM    : Add surface definitions to composite definition 0
DGEOM    : Glue composite surface definition 0
DGEOM    : Nodes,Faces,BEdges=      7221     14434      1888

AFLR4    : Curvature BG Surface Grid Generation

AFLR4    : Nodes, Faces      =      7221     14434

AFLR4    : Surface Grid Generation

AFLR4    : Generate optimal mesh on surface definition 1
AFLR2    : Nodes, Trias,Quads=       397       713         0
AFLR4    : Nodes, Trias,Quads=       416       751         0

AFLR4    : Generate optimal mesh on surface definition 2
AFLR2    : Nodes, Trias,Quads=       387       691         0
AFLR4    : Nodes, Trias,Quads=       346       609         0

AFLR4    : Generate optimal mesh on surface definition 3
AFLR2    : Nodes, Trias,Quads=       396       711         0
AFLR4    : Nodes, Trias,Quads=       417       753         0

AFLR4    : Generate optimal mesh on surface definition 4
AFLR2    : Nodes, Trias,Quads=       388       693         0
AFLR4    : Nodes, Trias,Quads=       344       605         0

AFLR4    : Generate optimal mesh on surface definition 5
AFLR2    : Nodes, Trias,Quads=       395       709         0
AFLR4    : Nodes, Trias,Quads=       416       751         0

AFLR4    : Generate optimal mesh on surface definition 6
AFLR2    : Nodes, Trias,Quads=       388       693         0
AFLR4    : Nodes, Trias,Quads=       344       605         0

AFLR4    : Generate optimal mesh on surface definition 7
AFLR2    : Nodes, Trias,Quads=       395       709         0
AFLR4    : Nodes, Trias,Quads=       416       751         0

AFLR4    : Generate optimal mesh on surface definition 8
AFLR2    : Nodes, Trias,Quads=       387       691         0
AFLR4    : Nodes, Trias,Quads=       346       609         0

AFLR4    : Generate optimal mesh on surface definition 9
AFLR2    : Nodes, Trias,Quads=     12796     24695         0
AFLR4    : Nodes, Trias,Quads=      7764     14631         0

AFLR4    : Generate optimal mesh on surface definition 10
AFLR2    : Nodes, Trias,Quads=     29251     57087         0
AFLR4    : Nodes, Trias,Quads=     12448     23481         0

AFLR4    : Generate optimal mesh on surface definition 11
AFLR2    : Nodes, Trias,Quads=     12136     23411         0
AFLR4    : Nodes, Trias,Quads=      7447     14033         0

AFLR4    : Generate optimal mesh on surface definition 12
AFLR2    : Nodes, Trias,Quads=     29424     57435         0
AFLR4    : Nodes, Trias,Quads=     12399     23385         0

AFLR4    : Generate optimal mesh on surface definition 13
AFLR2    : Nodes, Trias,Quads=       196       293         0
AFLR4    : Nodes, Trias,Quads=       188       277         0

AFLR4    : Generate optimal mesh on surface definition 14
AFLR2    : Nodes, Trias,Quads=     12819     24741         0
AFLR4    : Nodes, Trias,Quads=      7725     14553         0

AFLR4    : Generate optimal mesh on surface definition 15
AFLR2    : Nodes, Trias,Quads=     29437     57459         0
AFLR4    : Nodes, Trias,Quads=     12412     23409         0

AFLR4    : Generate optimal mesh on surface definition 16
AFLR2    : Nodes, Trias,Quads=     12144     23427         0
AFLR4    : Nodes, Trias,Quads=      7471     14081         0

AFLR4    : Generate optimal mesh on surface definition 17
AFLR2    : Nodes, Trias,Quads=     29445     57477         0
AFLR4    : Nodes, Trias,Quads=     12478     23543         0

AFLR4    : Generate optimal mesh on surface definition 18
AFLR2    : Nodes, Trias,Quads=       196       293         0
AFLR4    : Nodes, Trias,Quads=       188       277         0

AFLR4    : Generate optimal mesh on surface definition 19
AFLR2    : Nodes, Trias,Quads=        12        14         0
AFLR4    : Nodes, Trias,Quads=         8         6         0

AFLR4    : Generate optimal mesh on surface definition 20
AFLR2    : Nodes, Trias,Quads=        12        14         0
AFLR4    : Nodes, Trias,Quads=         8         6         0

AFLR4    : Generate optimal mesh on surface definition 21
AFLR2    : Nodes, Trias,Quads=        12        14         0
AFLR4    : Nodes, Trias,Quads=         8         6         0

AFLR4    : Generate optimal mesh on surface definition 22
AFLR2    : Nodes, Trias,Quads=        12        14         0
AFLR4    : Nodes, Trias,Quads=         8         6         0

AFLR4    : Generate optimal mesh on surface definition 23
AFLR2    : Nodes, Trias,Quads=        12        14         0
AFLR4    : Nodes, Trias,Quads=         8         6         0

AFLR4    : Generate optimal mesh on surface definition 24
AFLR2    : Nodes, Trias,Quads=        12        14         0
AFLR4    : Nodes, Trias,Quads=         8         6         0

DGEOM    : Add surface definitions to composite definition 0
DGEOM    : Glue composite surface definition 0
DGEOM    : Nodes,Faces,BEdges=     78574    157140     10038

AFLR4    : Proximity BG Surface Grid Generation

AFLR4    : Nodes, Trias      =     78960    157912

AFLR4    : Surface Grid Generation

AFLR4    : Generate optimal mesh on surface definition 1
AFLR2    : Nodes, Trias,Quads=       850      1593         0
AFLR4    : Nodes, Trias,Quads=       754      1401         0

AFLR4    : Generate optimal mesh on surface definition 2
AFLR2    : Nodes, Trias,Quads=       384       685         0
AFLR4    : Nodes, Trias,Quads=       354       625         0

AFLR4    : Generate optimal mesh on surface definition 3
AFLR2    : Nodes, Trias,Quads=       842      1577         0
AFLR4    : Nodes, Trias,Quads=       803      1499         0

AFLR4    : Generate optimal mesh on surface definition 4
AFLR2    : Nodes, Trias,Quads=       384       685         0
AFLR4    : Nodes, Trias,Quads=       351       619         0

AFLR4    : Generate optimal mesh on surface definition 5
AFLR2    : Nodes, Trias,Quads=       837      1566         0
AFLR4    : Nodes, Trias,Quads=       755      1402         0

AFLR4    : Generate optimal mesh on surface definition 6
AFLR2    : Nodes, Trias,Quads=       384       685         0
AFLR4    : Nodes, Trias,Quads=       351       619         0

AFLR4    : Generate optimal mesh on surface definition 7
AFLR2    : Nodes, Trias,Quads=       834      1560         0
AFLR4    : Nodes, Trias,Quads=       806      1504         0

AFLR4    : Generate optimal mesh on surface definition 8
AFLR2    : Nodes, Trias,Quads=       384       685         0
AFLR4    : Nodes, Trias,Quads=       354       625         0

AFLR4    : Generate optimal mesh on surface definition 9
AFLR2    : Nodes, Trias,Quads=     11687     22537         0
AFLR4    : Nodes, Trias,Quads=      9244     17651         0

AFLR4    : Generate optimal mesh on surface definition 10
AFLR2    : Nodes, Trias,Quads=     22265     43205         0
AFLR4    : Nodes, Trias,Quads=     14799     28273         0

AFLR4    : Generate optimal mesh on surface definition 11
AFLR2    : Nodes, Trias,Quads=     11200     21594         0
AFLR4    : Nodes, Trias,Quads=      8943     17080         0

AFLR4    : Generate optimal mesh on surface definition 12
AFLR2    : Nodes, Trias,Quads=     22072     42820         0
AFLR4    : Nodes, Trias,Quads=     14774     28224         0

AFLR4    : Generate optimal mesh on surface definition 13
AFLR2    : Nodes, Trias,Quads=       184       274         0
AFLR4    : Nodes, Trias,Quads=       178       262         0

AFLR4    : Generate optimal mesh on surface definition 14
AFLR2    : Nodes, Trias,Quads=     11697     22557         0
AFLR4    : Nodes, Trias,Quads=      9237     17637         0

AFLR4    : Generate optimal mesh on surface definition 15
AFLR2    : Nodes, Trias,Quads=     22389     43453         0
AFLR4    : Nodes, Trias,Quads=     14717     28109         0

AFLR4    : Generate optimal mesh on surface definition 16
AFLR2    : Nodes, Trias,Quads=     11243     21680         0
AFLR4    : Nodes, Trias,Quads=      8970     17134         0

AFLR4    : Generate optimal mesh on surface definition 17
AFLR2    : Nodes, Trias,Quads=     22230     43136         0
AFLR4    : Nodes, Trias,Quads=     14757     28190         0

AFLR4    : Generate optimal mesh on surface definition 18
AFLR2    : Nodes, Trias,Quads=       184       274         0
AFLR4    : Nodes, Trias,Quads=       178       262         0

AFLR4    : Generate optimal mesh on surface definition 19
AFLR2    : Nodes, Trias,Quads=        12        14         0
AFLR4    : Nodes, Trias,Quads=         8         6         0

AFLR4    : Generate optimal mesh on surface definition 20
AFLR2    : Nodes, Trias,Quads=        12        14         0
AFLR4    : Nodes, Trias,Quads=         8         6         0

AFLR4    : Generate optimal mesh on surface definition 21
AFLR2    : Nodes, Trias,Quads=        12        14         0
AFLR4    : Nodes, Trias,Quads=         8         6         0

AFLR4    : Generate optimal mesh on surface definition 22
AFLR2    : Nodes, Trias,Quads=        12        14         0
AFLR4    : Nodes, Trias,Quads=         8         6         0

AFLR4    : Generate optimal mesh on surface definition 23
AFLR2    : Nodes, Trias,Quads=        12        14         0
AFLR4    : Nodes, Trias,Quads=         8         6         0

AFLR4    : Generate optimal mesh on surface definition 24
AFLR2    : Nodes, Trias,Quads=        12        14         0
AFLR4    : Nodes, Trias,Quads=         8         6         0

DGEOM    : Add surface definitions to composite definition 0
DGEOM    : Glue composite surface definition 0
DGEOM    : Nodes,Faces,BEdges=     95580    191152      9546

OVERALL  : CPU Time          =     2.483   seconds
Body 1 (of 4)
Number of nodes    = 2072
Number of elements = 4144
Number of triangle elements      = 4144
Number of quadrilateral elements = 0
Body 2 (of 4)
Number of nodes    = 2075
Number of elements = 4150
Number of triangle elements      = 4150
Number of quadrilateral elements = 0
Body 3 (of 4)
Number of nodes    = 91413
Number of elements = 182822
Number of triangle elements      = 182822
Number of quadrilateral elements = 0
Body 4 (of 4)
Number of nodes    = 20
Number of elements = 36
Number of triangle elements      = 36
Number of quadrilateral elements = 0
----------------------------
Total number of nodes    = 95580
Total number of elements = 191152
Total number of triangle elements      = 191152
Total number of quadrilateral elements = 0

Writing vtk file ....

Writing vtk surface file ....

capsGroups found:
  1: Nacelle
  2: Wing
  3: Farfield
Finished writing vtk file

Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 4
	Name = Nacelle, index = 1
	Name = leftWing, index = 2
	Name = riteWing, index = 3
	Name = Farfield, index = 4
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 3
	Name = Nacelle, index = 1
	Name = Wing, index = 2
	Name = Farfield, index = 3
Getting volume mesh
 
UG PARAM : SETTING INPUT PARAMETERS FROM ARGUMENT VECTOR
 
UG PARAM : mrecm                       = 3         
UG PARAM : mrecqm                      = 3         
UG PARAM : mpfrmt                      = 0         
 
AFLR2    : ---------------------------------------
AFLR2    : AFLR2 LIBRARY
AFLR2    : ADVANCING-FRONT/LOCAL-RECONNECTION
AFLR2    : TRIA/QUAD GRID GENERATOR
AFLR2    : Version Number 9.18.1
AFLR2    : Version Date   06/11/24 @ 05:52PM
AFLR2    : Compile OS     Darwin 23.5.0 arm64
AFLR2    : Compile Date   06/11/24 @ 05:52PM
AFLR2    : Copyright 1994-2021, D.L. Marcum
AFLR2    : ---------------------------------------
 
AFLR4    : ---------------------------------------
AFLR4    : AFLR4 LIBRARY
AFLR4    : ADVANCING-FRONT/LOCAL-RECONNECTION
AFLR4    : TRIA/QUAD SURFACE GRID GENERATOR
AFLR4    : Version Number 11.5.15
AFLR4    : Version Date   07/19/24 @ 07:04PM
AFLR4    : Compile OS     Darwin 23.5.0 arm64
AFLR4    : Compile Date   07/19/24 @ 07:06PM
AFLR4    : Copyright 1994-2021, D.L. Marcum
AFLR4    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.8.1
EGADS    : ---------------------------------------

EGADS    : EGADS CAD Geometry Setup

EGADS    : Model has 4 Active Bodies

EGADS    : Body 0 is a SolidBody
EGADS    : Body 0 has 1 Shells
EGADS    : Body 0 has 4 Faces
EGADS    : Body 0 has 8 Edges
EGADS    : Body 0 has 4 Loops
EGADS    : Body 0 has 4 Nodes
EGADS    : Body 1 is a SolidBody
EGADS    : Body 1 has 1 Shells
EGADS    : Body 1 has 4 Faces
EGADS    : Body 1 has 8 Edges
EGADS    : Body 1 has 4 Loops
EGADS    : Body 1 has 4 Nodes
EGADS    : Body 2 is a SolidBody
EGADS    : Body 2 has 1 Shells
EGADS    : Body 2 has 10 Faces
EGADS    : Body 2 has 18 Edges
EGADS    : Body 2 has 10 Loops
EGADS    : Body 2 has 10 Nodes
EGADS    : Body 3 is a SolidBody
EGADS    : Body 3 has 1 Shells
EGADS    : Body 3 has 6 Faces
EGADS    : Body 3 has 12 Edges
EGADS    : Body 3 has 6 Loops
EGADS    : Body 3 has 8 Nodes

EGADS    : Check Grid BCs

EGADS    : Grid BCs are OK

EGADS    : Face Neighbor-Faces Information

EGADS    : QC  = Face Quad Combination Flag
EGADS    : IER = Face Isolated Edge Refinement Flag
EGADS    : ER  = Face Edge Refinement Factor
EGADS    :       Not applicable for Faces with a FarField Grid BC.
EGADS    : SF  = Face Scale Factor
EGADS    :       Not applicable for Faces with a FarField Grid BC.

EGADS    :   Face          Body    QC   IER       ER    Scale   Neighbor
EGADS    :     ID  Active    ID  Flag  Flag   Weight   Factor   Faces
EGADS    :      1     Yes     0     0     1        0        1   2 3
EGADS    :      2     Yes     0     0     1        0        1   1 4
EGADS    :      3     Yes     0     0     1        0        1   1 4
EGADS    :      4     Yes     0     0     1        0        1   2 3
EGADS    :      5     Yes     1     0     1        0        1   6 7
EGADS    :      6     Yes     1     0     1        0        1   5 8
EGADS    :      7     Yes     1     0     1        0        1   5 8
EGADS    :      8     Yes     1     0     1        0        1   6 7
EGADS    :      9     Yes     2     0     1        1        1   10 11 14
EGADS    :     10     Yes     2     0     1        1        1   9 12 13
EGADS    :     11     Yes     2     0     1        1        1   9 12 16
EGADS    :     12     Yes     2     0     1        1        1   10 11 13
EGADS    :     13     Yes     2     0     1        1        1   10 12
EGADS    :     14     Yes     2     0     1        1        1   9 15 16
EGADS    :     15     Yes     2     0     1        1        1   14 17 18
EGADS    :     16     Yes     2     0     1        1        1   11 14 17
EGADS    :     17     Yes     2     0     1        1        1   15 16 18
EGADS    :     18     Yes     2     0     1        1        1   15 17
EGADS    :     19     Yes     3     0     1       NA       NA   21 22 23 24
EGADS    :     20     Yes     3     0     1       NA       NA   21 22 23 24
EGADS    :     21     Yes     3     0     1       NA       NA   19 20 23 24
EGADS    :     22     Yes     3     0     1       NA       NA   19 20 23 24
EGADS    :     23     Yes     3     0     1       NA       NA   19 20 21 22
EGADS    :     24     Yes     3     0     1       NA       NA   19 20 21 22

EGADS    : Face Edges Information

EGADS    :   Face   Edges
EGADS    :      1   -1 3 2 -4
EGADS    :      2   -2 5 1 -6
EGADS    :      3   7 4 -8 -3
EGADS    :      4   8 6 -7 -5
EGADS    :      5   9 12 -10 -11
EGADS    :      6   10 14 -9 -13
EGADS    :      7   -15 11 16 -12
EGADS    :      8   -16 13 15 -14
EGADS    :      9   -17 18 19 -20
EGADS    :     10   -21 20 22 -23
EGADS    :     11   -19 24 17 -25
EGADS    :     12   -22 25 21 -26
EGADS    :     13   23 26
EGADS    :     14   27 29 -28 -18
EGADS    :     15   30 32 -31 -29
EGADS    :     16   28 33 -27 -24
EGADS    :     17   31 34 -30 -33
EGADS    :     18   -32 -34
EGADS    :     19   35 36 -37 -38
EGADS    :     20   -39 42 41 -40
EGADS    :     21   43 39 -44 -35
EGADS    :     22   -45 37 46 -41
EGADS    :     23   38 45 -42 -43
EGADS    :     24   -36 44 40 -46

EGADS    : Face Loops Information

EGADS    :   Face   Loops
EGADS    :      1   1
EGADS    :      2   2
EGADS    :      3   3
EGADS    :      4   4
EGADS    :      5   5
EGADS    :      6   6
EGADS    :      7   7
EGADS    :      8   8
EGADS    :      9   9
EGADS    :     10   10
EGADS    :     11   11
EGADS    :     12   12
EGADS    :     13   13
EGADS    :     14   14
EGADS    :     15   15
EGADS    :     16   16
EGADS    :     17   17
EGADS    :     18   18
EGADS    :     19   19
EGADS    :     20   20
EGADS    :     21   21
EGADS    :     22   22
EGADS    :     23   23
EGADS    :     24   24

EGADS    : Loop Edges Information

EGADS    :   Loop  Active   Edges
EGADS    :      1     Yes   -1 3 2 -4
EGADS    :      2     Yes   -2 5 1 -6
EGADS    :      3     Yes   7 4 -8 -3
EGADS    :      4     Yes   8 6 -7 -5
EGADS    :      5     Yes   9 12 -10 -11
EGADS    :      6     Yes   10 14 -9 -13
EGADS    :      7     Yes   -15 11 16 -12
EGADS    :      8     Yes   -16 13 15 -14
EGADS    :      9     Yes   -17 18 19 -20
EGADS    :     10     Yes   -21 20 22 -23
EGADS    :     11     Yes   -19 24 17 -25
EGADS    :     12     Yes   -22 25 21 -26
EGADS    :     13     Yes   23 26
EGADS    :     14     Yes   27 29 -28 -18
EGADS    :     15     Yes   30 32 -31 -29
EGADS    :     16     Yes   28 33 -27 -24
EGADS    :     17     Yes   31 34 -30 -33
EGADS    :     18     Yes   -32 -34
EGADS    :     19     Yes   35 36 -37 -38
EGADS    :     20     Yes   -39 42 41 -40
EGADS    :     21     Yes   43 39 -44 -35
EGADS    :     22     Yes   -45 37 46 -41
EGADS    :     23     Yes   38 45 -42 -43
EGADS    :     24     Yes   -36 44 40 -46

EGADS    : Edge Node, Scale Factor, and Neighbor-Faces Information

EGADS    : ESF = Edge Scale Factor
EGADS    :       Not applicable for DEGENERATE Edges or Edges with a FarField
EGADS    :       Grid BC Neighbor Face.

EGADS    :                                             Neighbor
EGADS    :   Edge  Body  Active Node1 Node2      ESF   Faces
EGADS    :      1     0     Yes     1     2        1   1 2
EGADS    :      2     0     Yes     3     4        1   1 2
EGADS    :      3     0     Yes     1     3        1   1 3
EGADS    :      4     0     Yes     2     4        1   1 3
EGADS    :      5     0     Yes     3     1        1   2 4
EGADS    :      6     0     Yes     4     2        1   2 4
EGADS    :      7     0     Yes     1     2        1   3 4
EGADS    :      8     0     Yes     3     4        1   3 4
EGADS    :      9     1     Yes     5     6        1   5 6
EGADS    :     10     1     Yes     7     8        1   5 6
EGADS    :     11     1     Yes     5     7        1   5 7
EGADS    :     12     1     Yes     6     8        1   5 7
EGADS    :     13     1     Yes     7     5        1   6 8
EGADS    :     14     1     Yes     8     6        1   6 8
EGADS    :     15     1     Yes     5     6        1   7 8
EGADS    :     16     1     Yes     7     8        1   7 8
EGADS    :     17     2     Yes     9    10        1   9 11
EGADS    :     18     2     Yes     9    11        1   9 14
EGADS    :     19     2     Yes    11    12        1   9 11
EGADS    :     20     2     Yes    10    12        1   9 10
EGADS    :     21     2     Yes    10    13        1   10 12
EGADS    :     22     2     Yes    12    14        1   10 12
EGADS    :     23     2     Yes    13    14        1   10 13
EGADS    :     24     2     Yes    11     9        1   11 16
EGADS    :     25     2     Yes    12    10        1   11 12
EGADS    :     26     2     Yes    14    13        1   12 13
EGADS    :     27     2     Yes     9    15        1   14 16
EGADS    :     28     2     Yes    11    16        1   14 16
EGADS    :     29     2     Yes    15    16        1   14 15
EGADS    :     30     2     Yes    15    17        1   15 17
EGADS    :     31     2     Yes    16    18        1   15 17
EGADS    :     32     2     Yes    17    18        1   15 18
EGADS    :     33     2     Yes    16    15        1   16 17
EGADS    :     34     2     Yes    18    17        1   17 18
EGADS    :     35     3     Yes    20    19       NA   19 21
EGADS    :     36     3     Yes    19    21       NA   19 24
EGADS    :     37     3     Yes    22    21       NA   19 22
EGADS    :     38     3     Yes    20    22       NA   19 23
EGADS    :     39     3     Yes    24    23       NA   20 21
EGADS    :     40     3     Yes    23    25       NA   20 24
EGADS    :     41     3     Yes    26    25       NA   20 22
EGADS    :     42     3     Yes    24    26       NA   20 23
EGADS    :     43     3     Yes    20    24       NA   21 23
EGADS    :     44     3     Yes    19    23       NA   21 24
EGADS    :     45     3     Yes    22    26       NA   22 23
EGADS    :     46     3     Yes    21    25       NA   22 24

EGADS    : Node Information

EGADS    :   Node  Active      Coordinates
EGADS    :      1     Yes       90.5173952                0                0
EGADS    :      2     Yes       90.5173952                0                0
EGADS    :      3     Yes       60.5173952                0                0
EGADS    :      4     Yes       60.5173952                0                0
EGADS    :      5     Yes       90.5173952       29.3018771                0
EGADS    :      6     Yes       90.5173952       29.3018771                0
EGADS    :      7     Yes       60.5173952       29.3018771                0
EGADS    :      8     Yes       60.5173952       29.3018771                0
EGADS    :      9     Yes       97.2007855                0                0
EGADS    :     10     Yes       97.9335611                0                0
EGADS    :     11     Yes               50                0                0
EGADS    :     12     Yes       75.3047874                0                0
EGADS    :     13     Yes       123.552357                0        4.7180639
EGADS    :     14     Yes       118.391317                0       3.99272703
EGADS    :     15     Yes       97.9335611       36.1389817                0
EGADS    :     16     Yes       75.3047874       36.1389817                0
EGADS    :     17     Yes       123.552357       97.6729236        4.7180639
EGADS    :     18     Yes       118.391317       97.6729236       3.99272703
EGADS    :     19     Yes                0                0       1947.05079
EGADS    :     20     Yes                0                0                0
EGADS    :     21     Yes                0       1953.45847       1947.05079
EGADS    :     22     Yes                0       1953.45847                0
EGADS    :     23     Yes       2040.21562                0       1947.05079
EGADS    :     24     Yes       2040.21562                0                0
EGADS    :     25     Yes       2040.21562       1953.45847       1947.05079
EGADS    :     26     Yes       2040.21562       1953.45847                0

EGADS    : Face and Edge Match Information

EGADS    : No Face Matches Found

AFLR4    : Surface Mesh Spacing Setup

AFLR4    : Max Bounding Box Length     = 3906.92
AFLR4    : Min Bounding Box Length     = 3906.92
AFLR4    : Max Ref Bounding Box Length = 195.346
AFLR4    : Min Ref Bounding Box Length = 22.2515
AFLR4    : Reference Length            = 22.2515
AFLR4    : BL Thickness                = 0
AFLR4    : FarField Spacing            = 428.344
AFLR4    : Abs Min Surf Spacing        = 0.0556287
AFLR4    : Min Surf Spacing            = 0.111257
AFLR4    : Max Surf Spacing            = 2.22515
AFLR4    : Global Scale Factor         = 1

AFLR4    : Geometry Definition Information

AFLR4    : Definition              Definition   Composite             Grid BC
AFLR4    :         ID                    Type          ID                Type
AFLR4    :          0     glue-only composite           -                   -
AFLR4    :          1            CAD geometry           0                 STD
AFLR4    :          2            CAD geometry           0                 STD
AFLR4    :          3            CAD geometry           0                 STD
AFLR4    :          4            CAD geometry           0                 STD
AFLR4    :          5            CAD geometry           0                 STD
AFLR4    :          6            CAD geometry           0                 STD
AFLR4    :          7            CAD geometry           0                 STD
AFLR4    :          8            CAD geometry           0                 STD
AFLR4    :          9            CAD geometry           0                 STD
AFLR4    :         10            CAD geometry           0                 STD
AFLR4    :         11            CAD geometry           0                 STD
AFLR4    :         12            CAD geometry           0                 STD
AFLR4    :         13            CAD geometry           0                 STD
AFLR4    :         14            CAD geometry           0                 STD
AFLR4    :         15            CAD geometry           0                 STD
AFLR4    :         16            CAD geometry           0                 STD
AFLR4    :         17            CAD geometry           0                 STD
AFLR4    :         18            CAD geometry           0                 STD
AFLR4    :         19            CAD geometry           0            FARFIELD
AFLR4    :         20            CAD geometry           0            FARFIELD
AFLR4    :         21            CAD geometry           0            FARFIELD
AFLR4    :         22            CAD geometry           0            FARFIELD
AFLR4    :         23            CAD geometry           0            FARFIELD
AFLR4    :         24            CAD geometry           0            FARFIELD

AFLR4    : Case has 2 Proximity Checking Components

AFLR4    : Component 1 includes Definitions 9 10 11 12 13 14 15 16 17 18
AFLR4    : Component 2 includes Definitions 1 2 3 4 5 6 7 8

AFLR4    : Define CAD surface definition 1
AFLR4    : Define CAD surface definition 2
AFLR4    : Define CAD surface definition 3
AFLR4    : Define CAD surface definition 4
AFLR4    : Define CAD surface definition 5
AFLR4    : Define CAD surface definition 6
AFLR4    : Define CAD surface definition 7
AFLR4    : Define CAD surface definition 8
AFLR4    : Define CAD surface definition 9
AFLR4    : Define CAD surface definition 10
AFLR4    : Define CAD surface definition 11
AFLR4    : Define CAD surface definition 12
AFLR4    : Define CAD surface definition 13
AFLR4    : Define CAD surface definition 14
AFLR4    : Define CAD surface definition 15
AFLR4    : Define CAD surface definition 16
AFLR4    : Define CAD surface definition 17
AFLR4    : Define CAD surface definition 18
AFLR4    : Define CAD surface definition 19
AFLR4    : Define CAD surface definition 20
AFLR4    : Define CAD surface definition 21
AFLR4    : Define CAD surface definition 22
AFLR4    : Define CAD surface definition 23
AFLR4    : Define CAD surface definition 24
 
AFLR43   : INPUT SURFACE MESH FROM TESS
 
AFLR43   : Quad Surface Faces=         0
AFLR43   : Tria Surface Faces=    191152
AFLR43   : Nodes             =     95580
 
 
UG PARAM : SETTING INPUT PARAMETERS FROM ARGUMENT VECTOR
 
UG PARAM : mrecm                       = 3         
UG PARAM : mrecqm                      = 3         
UG PARAM : mpfrmt                      = 0         
 
AFLR3    : ---------------------------------------
AFLR3    : AFLR3 LIBRARY
AFLR3    : ADVANCING-FRONT/LOCAL-RECONNECTION
AFLR3    : TETRAHEDRAL GRID GENERATOR
AFLR3    : Version Number 16.32.50
AFLR3    : Version Date   10/31/23 @ 06:31PM
AFLR3    : Compile OS     Darwin 23.3.0 arm64
AFLR3    : Compile Date   02/08/24 @ 04:22PM
AFLR3    : Copyright 1994-2021, D.L. Marcum
AFLR3    : ---------------------------------------
 
AFLR3 IC : INPUT SURFACE GRID CHECK
 
AFLR3 IC : Nodes, Elements   =     95580         0

UG3      : Boundary Conditions

UG3      :  B-Face ID            Boundary Condition
UG3      :          1                         Solid
UG3      :          2                         Solid
UG3      :          3                         Solid
UG3      :          4                         Solid
UG3      :          5                         Solid
UG3      :          6                         Solid
UG3      :          7                         Solid
UG3      :          8                         Solid
UG3      :          9                         Solid
UG3      :         10                         Solid
UG3      :         11                         Solid
UG3      :         12                         Solid
UG3      :         13                         Solid
UG3      :         14                         Solid
UG3      :         15                         Solid
UG3      :         16                         Solid
UG3      :         17                         Solid
UG3      :         18                         Solid
UG3      :         19                      FarField
UG3      :         20                      FarField
UG3      :         21                      FarField
UG3      :         22                      FarField
UG3      :         23                      FarField
UG3      :         24                      FarField
 
AFLR3    : CPU Time          =     0.109   seconds
 
AFLR3 IG : INITIAL VOLUME GRID GENERATION
 
AFLR3 IG : Nodes, Elements   =     95580         0
AFLR3 IG : Nodes, Elements   =         8        10
AFLR3 IG : Nodes, Elements   =     19118    113387
AFLR3 IG : Nodes, Elements   =     38236    247740
AFLR3 IG : Nodes, Elements   =     57354    368381
AFLR3 IG : Nodes, Elements   =     76472    521305
AFLR3 IG : Nodes, Elements   =     95587    673125
AFLR3 IG : Nodes, Elements   =     95587    671793
AFLR3 IG : Nodes, Elements   =     95587    671843
AFLR3 IG : Nodes, Elements   =     95587    671732
AFLR3 IG : Nodes, Elements   =     95587    671730
AFLR3 IG : Nodes, Elements   =     95580    378556
AFLR3 IG : Nodes, Elements   =     95580    378785
AFLR3 IG : Nodes, Elements   =     95580    306254
AFLR3 IG : Nodes, Elements   =     95580    287815
 
AFLR3    : CPU Time          =     3.643   seconds
 
AFLR3 GG : ISOTROPIC VOLUME GRID GENERATION
 
AFLR3 GG : Nodes, Elements   =     95580    287815
AFLR3 GGi: Nodes, Elements   =     95581    287818
AFLR3 GGi: Nodes, Elements   =     95581    287829
AFLR3 GGi: Nodes, Elements   =     95581    287828
AFLR3 GGi: Nodes, Elements   =     95583    287834
AFLR3 GGi: Nodes, Elements   =     95583    287890
AFLR3 GGi: Nodes, Elements   =     95583    287912
AFLR3 GG : Nodes, Elements   =    136678    411938
AFLR3 GG : Nodes, Elements   =    136678    577044
AFLR3 GG : Nodes, Elements   =    136678    536154
AFLR3 GG : Nodes, Elements   =    171128    640568
AFLR3 GG : Nodes, Elements   =    171128    776304
AFLR3 GG : Nodes, Elements   =    171128    734094
AFLR3 GG : Nodes, Elements   =    206400    840686
AFLR3 GG : Nodes, Elements   =    206400    979875
AFLR3 GG : Nodes, Elements   =    206400    937908
AFLR3 GG : Nodes, Elements   =    241646   1044099
AFLR3 GG : Nodes, Elements   =    241646   1188395
AFLR3 GG : Nodes, Elements   =    241646   1146956
AFLR3 GG : Nodes, Elements   =    241646   1137722
AFLR3 GG : Nodes, Elements   =    276767   1243501
AFLR3 GG : Nodes, Elements   =    276767   1395480
AFLR3 GG : Nodes, Elements   =    276767   1354454
AFLR3 GG : Nodes, Elements   =    311737   1459784
AFLR3 GG : Nodes, Elements   =    311737   1601038
AFLR3 GG : Nodes, Elements   =    311737   1562741
AFLR3 GG : Nodes, Elements   =    346382   1667060
AFLR3 GG : Nodes, Elements   =    346382   1803912
AFLR3 GG : Nodes, Elements   =    346382   1767981
AFLR3 GG : Nodes, Elements   =    379866   1868797
AFLR3 GG : Nodes, Elements   =    379866   2001420
AFLR3 GG : Nodes, Elements   =    379866   1966993
AFLR3 GG : Nodes, Elements   =    412236   2064483
AFLR3 GG : Nodes, Elements   =    412236   2190563
AFLR3 GG : Nodes, Elements   =    412236   2159284
AFLR3 GG : Nodes, Elements   =    443624   2253761
AFLR3 GG : Nodes, Elements   =    443624   2375880
AFLR3 GG : Nodes, Elements   =    443624   2345639
AFLR3 GG : Nodes, Elements   =    473758   2436345
AFLR3 GG : Nodes, Elements   =    473758   2553524
AFLR3 GG : Nodes, Elements   =    473758   2524504
AFLR3 GG : Nodes, Elements   =    502809   2611934
AFLR3 GG : Nodes, Elements   =    502809   2725931
AFLR3 GG : Nodes, Elements   =    502809   2696981
AFLR3 GG : Nodes, Elements   =    530466   2780197
AFLR3 GG : Nodes, Elements   =    530466   2889393
AFLR3 GG : Nodes, Elements   =    530466   2861633
AFLR3 GG : Nodes, Elements   =    557117   2941852
AFLR3 GG : Nodes, Elements   =    557117   3045248
AFLR3 GG : Nodes, Elements   =    557117   3019721
AFLR3 GG : Nodes, Elements   =    582598   3096375
AFLR3 GG : Nodes, Elements   =    582598   3195656
AFLR3 GG : Nodes, Elements   =    582598   3171187
AFLR3 GG : Nodes, Elements   =    607120   3245004
AFLR3 GG : Nodes, Elements   =    607120   3341157
AFLR3 GG : Nodes, Elements   =    607120   3316708
AFLR3 GG : Nodes, Elements   =    630670   3387605
AFLR3 GG : Nodes, Elements   =    630670   3480180
AFLR3 GG : Nodes, Elements   =    630670   3456797
AFLR3 GG : Nodes, Elements   =    653200   3524630
AFLR3 GG : Nodes, Elements   =    653200   3613020
AFLR3 GG : Nodes, Elements   =    653200   3590696
AFLR3 GG : Nodes, Elements   =    675084   3656585
AFLR3 GG : Nodes, Elements   =    675084   3741278
AFLR3 GG : Nodes, Elements   =    675084   3720774
AFLR3 GG : Nodes, Elements   =    696108   3784042
AFLR3 GG : Nodes, Elements   =    696108   3866035
AFLR3 GG : Nodes, Elements   =    696108   3845633
AFLR3 GG : Nodes, Elements   =    716356   3906549
AFLR3 GG : Nodes, Elements   =    716356   3984761
AFLR3 GG : Nodes, Elements   =    716356   3965561
AFLR3 GG : Nodes, Elements   =    735889   4024306
AFLR3 GG : Nodes, Elements   =    735889   4100723
AFLR3 GG : Nodes, Elements   =    735889   4081584
AFLR3 GG : Nodes, Elements   =    754458   4137443
AFLR3 GG : Nodes, Elements   =    754458   4209831
AFLR3 GG : Nodes, Elements   =    754458   4191783
AFLR3 GG : Nodes, Elements   =    772291   4245412
AFLR3 GG : Nodes, Elements   =    772291   4315501
AFLR3 GG : Nodes, Elements   =    772291   4297710
AFLR3 GG : Nodes, Elements   =    789443   4349276
AFLR3 GG : Nodes, Elements   =    789443   4416475
AFLR3 GG : Nodes, Elements   =    789443   4399563
AFLR3 GG : Nodes, Elements   =    806051   4449471
AFLR3 GG : Nodes, Elements   =    806051   4514571
AFLR3 GG : Nodes, Elements   =    806051   4498171
AFLR3 GG : Nodes, Elements   =    821873   4545711
AFLR3 GG : Nodes, Elements   =    821873   4607158
AFLR3 GG : Nodes, Elements   =    821873   4592064
AFLR3 GG : Nodes, Elements   =    837118   4637853
AFLR3 GG : Nodes, Elements   =    837118   4697402
AFLR3 GG : Nodes, Elements   =    837118   4682546
AFLR3 GG : Nodes, Elements   =    851739   4726464
AFLR3 GG : Nodes, Elements   =    851739   4782603
AFLR3 GG : Nodes, Elements   =    851739   4769065
AFLR3 GG : Nodes, Elements   =    865824   4811353
AFLR3 GG : Nodes, Elements   =    865824   4866088
AFLR3 GG : Nodes, Elements   =    865824   4852550
AFLR3 GG : Nodes, Elements   =    879359   4893188
AFLR3 GG : Nodes, Elements   =    879359   4945198
AFLR3 GG : Nodes, Elements   =    879359   4932618
AFLR3 GG : Nodes, Elements   =    892295   4971462
AFLR3 GG : Nodes, Elements   =    892295   5021252
AFLR3 GG : Nodes, Elements   =    892295   5009183
AFLR3 GG : Nodes, Elements   =    904796   5046719
AFLR3 GG : Nodes, Elements   =    904796   5094609
AFLR3 GG : Nodes, Elements   =    904796   5082935
AFLR3 GG : Nodes, Elements   =    917006   5119589
AFLR3 GG : Nodes, Elements   =    917006   5167108
AFLR3 GG : Nodes, Elements   =    917006   5155238
AFLR3 GG : Nodes, Elements   =    928945   5191076
AFLR3 GG : Nodes, Elements   =    928945   5236714
AFLR3 GG : Nodes, Elements   =    928945   5225614
AFLR3 GG : Nodes, Elements   =    940659   5260766
AFLR3 GG : Nodes, Elements   =    940659   5306192
AFLR3 GG : Nodes, Elements   =    940659   5294917
AFLR3 GG : Nodes, Elements   =    952358   5330036
AFLR3 GG : Nodes, Elements   =    952358   5374827
AFLR3 GG : Nodes, Elements   =    952358   5364090
AFLR3 GG : Nodes, Elements   =    963772   5398344
AFLR3 GG : Nodes, Elements   =    963772   5442371
AFLR3 GG : Nodes, Elements   =    963772   5431527
AFLR3 GG : Nodes, Elements   =    975235   5465936
AFLR3 GG : Nodes, Elements   =    975235   5510168
AFLR3 GG : Nodes, Elements   =    975235   5499163
AFLR3 GG : Nodes, Elements   =    986552   5533128
AFLR3 GG : Nodes, Elements   =    986552   5576100
AFLR3 GG : Nodes, Elements   =    986552   5565791
AFLR3 GG : Nodes, Elements   =    997689   5599215
AFLR3 GG : Nodes, Elements   =    997689   5641662
AFLR3 GG : Nodes, Elements   =    997689   5631301
AFLR3 GG : Nodes, Elements   =   1008693   5664321
AFLR3 GG : Nodes, Elements   =   1008693   5706246
AFLR3 GG : Nodes, Elements   =   1008693   5696151
AFLR3 GG : Nodes, Elements   =   1019592   5728860
AFLR3 GG : Nodes, Elements   =   1019592   5771162
AFLR3 GG : Nodes, Elements   =   1019592   5760605
AFLR3 GG : Nodes, Elements   =   1030418   5793103
AFLR3 GG : Nodes, Elements   =   1030418   5834841
AFLR3 GG : Nodes, Elements   =   1030418   5824463
AFLR3 GG : Nodes, Elements   =   1040850   5855769
AFLR3 GG : Nodes, Elements   =   1040850   5895951
AFLR3 GG : Nodes, Elements   =   1040850   5885943
AFLR3 GG : Nodes, Elements   =   1051188   5916972
AFLR3 GG : Nodes, Elements   =   1051188   5957000
AFLR3 GG : Nodes, Elements   =   1051188   5946966
AFLR3 GG : Nodes, Elements   =   1061495   5977893
AFLR3 GG : Nodes, Elements   =   1061495   6017359
AFLR3 GG : Nodes, Elements   =   1061495   6007786
AFLR3 GG : Nodes, Elements   =   1071564   6038008
AFLR3 GG : Nodes, Elements   =   1071564   6076351
AFLR3 GG : Nodes, Elements   =   1071564   6067022
AFLR3 GG : Nodes, Elements   =   1081243   6096066
AFLR3 GG : Nodes, Elements   =   1081243   6133873
AFLR3 GG : Nodes, Elements   =   1081243   6124235
AFLR3 GG : Nodes, Elements   =   1090504   6152024
AFLR3 GG : Nodes, Elements   =   1090504   6188229
AFLR3 GG : Nodes, Elements   =   1090504   6178954
AFLR3 GG : Nodes, Elements   =   1099257   6205218
AFLR3 GG : Nodes, Elements   =   1099257   6239457
AFLR3 GG : Nodes, Elements   =   1099257   6230836
AFLR3 GG : Nodes, Elements   =   1107059   6254252
AFLR3 GG : Nodes, Elements   =   1107059   6284884
AFLR3 GG : Nodes, Elements   =   1107059   6276999
AFLR3 GG : Nodes, Elements   =   1113848   6297377
AFLR3 GG : Nodes, Elements   =   1113848   6323612
AFLR3 GG : Nodes, Elements   =   1113848   6316993
AFLR3 GG : Nodes, Elements   =   1119760   6334736
AFLR3 GG : Nodes, Elements   =   1119760   6358254
AFLR3 GG : Nodes, Elements   =   1119760   6351947
AFLR3 GG : Nodes, Elements   =   1124553   6366331
AFLR3 GG : Nodes, Elements   =   1124553   6385564
AFLR3 GG : Nodes, Elements   =   1124553   6380400
AFLR3 GG : Nodes, Elements   =   1128268   6391547
AFLR3 GG : Nodes, Elements   =   1128268   6406066
AFLR3 GG : Nodes, Elements   =   1128268   6402254
AFLR3 GG : Nodes, Elements   =   1130923   6410221
AFLR3 GG : Nodes, Elements   =   1130923   6421060
AFLR3 GG : Nodes, Elements   =   1130923   6417908
AFLR3 GG : Nodes, Elements   =   1132691   6423216
AFLR3 GG : Nodes, Elements   =   1132691   6430239
AFLR3 GG : Nodes, Elements   =   1132691   6428275
AFLR3 GG : Nodes, Elements   =   1133857   6431773
AFLR3 GG : Nodes, Elements   =   1133857   6436705
AFLR3 GG : Nodes, Elements   =   1133857   6435176
AFLR3 GG : Nodes, Elements   =   1134481   6437048
AFLR3 GG : Nodes, Elements   =   1134481   6439565
AFLR3 GG : Nodes, Elements   =   1134481   6438803
AFLR3 GG : Nodes, Elements   =   1134784   6439712
AFLR3 GG : Nodes, Elements   =   1134784   6440912
AFLR3 GG : Nodes, Elements   =   1134784   6440547
AFLR3 GG : Nodes, Elements   =   1134914   6440937
AFLR3 GG : Nodes, Elements   =   1134914   6441430
AFLR3 GG : Nodes, Elements   =   1134914   6441281
AFLR3 GG : Nodes, Elements   =   1134969   6441446
AFLR3 GG : Nodes, Elements   =   1134969   6441682
AFLR3 GG : Nodes, Elements   =   1134969   6441599
AFLR3 GG : Nodes, Elements   =   1134985   6441647
AFLR3 GG : Nodes, Elements   =   1134985   6441720
AFLR3 GG : Nodes, Elements   =   1134985   6441692
AFLR3 GG : Nodes, Elements   =   1134992   6441713
AFLR3 GG : Nodes, Elements   =   1134992   6441745
AFLR3 GG : Nodes, Elements   =   1134992   6441730
AFLR3 GG : Nodes, Elements   =   1134993   6441733
AFLR3 GG : Nodes, Elements   =   1134993   6441738
AFLR3 GG : Nodes, Elements   =   1134993   6441736
AFLR3 GG : Nodes, Elements   =   1135116   6442105
AFLR3 GG : Nodes, Elements   =   1135116   6442576
AFLR3 GG : Nodes, Elements   =   1135116   6442430
AFLR3 GG : Nodes, Elements   =   1135150   6442532
AFLR3 GG : Nodes, Elements   =   1135150   6442653
AFLR3 GG : Nodes, Elements   =   1135150   6442602
AFLR3 GG : Nodes, Elements   =   1135162   6442638
AFLR3 GG : Nodes, Elements   =   1135162   6442684
AFLR3 GG : Nodes, Elements   =   1135162   6442668
AFLR3 GG : Nodes, Elements   =   1135164   6442674
AFLR3 GG : Nodes, Elements   =   1135164   6442683
AFLR3 GG : Nodes, Elements   =   1135164   6442680
AFLR3 GG : Nodes, Elements   =   1135166   6442686
AFLR3 GG : Nodes, Elements   =   1135166   6442692
AFLR3 GG : Nodes, Elements   =   1135166   6442691
AFLR3 GG : Nodes, Elements   =   1135167   6442694
AFLR3 GG : Nodes, Elements   =   1135167   6442697
AFLR3 GG : Nodes, Elements   =   1135167   6442696
 
AFLR3    : CPU Time          =     1.056   minutes
 
AFLR3 QI : QUALITY IMPROVEMENT
 
AFLR3 QI : Nodes, Elements   =   1135167   6442696
AFLR3 QI : Nodes, Elements   =   1129670   6411684
AFLR3 QI : Nodes, Elements   =   1128689   6406154
AFLR3 QI : Nodes, Elements   =   1128464   6404899
AFLR3 QI : Nodes, Elements   =   1128424   6404669
AFLR3 QI : Nodes, Elements   =   1128409   6404587
AFLR3 QI : Nodes, Elements   =   1128407   6404575
AFLR3 QI : Nodes, Elements   =   1128406   6404568
AFLR3 QI : Nodes, Elements   =   1128405   6404563
AFLR3 QI : Nodes, Elements   =   1128405   6427353
AFLR3 QI : Nodes, Elements   =   1128405   6402765
AFLR3 QI : Nodes, Elements   =   1128405   6391678
AFLR3 QI : Nodes, Elements   =   1128405   6408644
AFLR3 QI : Nodes, Elements   =   1128405   6391271
AFLR3 QI : Nodes, Elements   =   1128405   6390811
AFLR3 QI : Nodes, Elements   =   1128405   6406750
AFLR3 QI : Nodes, Elements   =   1128405   6390982
AFLR3 QI : Nodes, Elements   =   1128405   6390667
AFLR3 QI : Nodes, Elements   =   1128405   6395803
AFLR3 QI : Nodes, Elements   =   1128405   6389758
AFLR3 QI : Nodes, Elements   =   1128405   6389206
AFLR3 QI : Nodes, Elements   =   1128405   6391898
AFLR3 QI : Nodes, Elements   =   1128405   6388765
AFLR3 QI : Nodes, Elements   =   1128405   6388419
 
AFLR3    : CPU Time          =    14.565   seconds
 
AFLR3 QRG: QUALITY GRID RE-GENERATION
 
AFLR3 QRG: Nodes, Elements   =   1128405   6388419
AFLR3 QRG: Nodes, Elements   =   1128425   6388539
 
AFLR3    : CPU Time          =     0.592   seconds
 
AFLR3    : DONE

UG3      : DIHEDRAL ANGLE CHECK

UG3      : No. Tet Elems     =   6388539
UG3      : Min, Max Ang      =     3.386     162.2
UG3      : Average Angle     =      70.2
UG3      : No. Angle&gt;160.0   =         5
UG3      : No. Angle&gt;179.9   =         0

UG3      : VOL CHECK

UG3      : Total-Volume      =  5.96e+10

UG3      : No. Tet Elems     =   6388539
UG3      : Min Vol           =  1.42e-05
UG3      : Average Vol       =  9.33e+03
UG3      : Total-Tet-Vol     =  5.96e+10
UG3      : No. Vol&lt;TOL       =         0

UG3      : Q VOL-LENGTH-RATIO CHECK
                      2/3        2
UG3      : Q = c * Vol   / sum( L  )
UG3      : 0 &lt;= Q &lt;= 1

UG3      : No. Tet Elems     =   6388539
UG3      : Min, Max Q        =    0.0232         1
UG3      : Average Q         =     0.894
UG3      : No. Q&lt;       0.1  =       205
UG3      : No. Q&lt;      0.01  =         0

OVERALL  : CPU Time          =     1.394   minutes

UG3      : DIHEDRAL ANGLE CHECK

UG3      : No. Tet Elems     =   6388539
UG3      : Min, Max Ang      =     3.386     162.2
UG3      : Average Angle     =      70.2
UG3      : No. Angle&gt;160.0   =         5
UG3      : No. Angle&gt;179.9   =         0

UG3      : VOL CHECK

UG3      : Total-Volume      =  5.96e+10

UG3      : No. Tet Elems     =   6388539
UG3      : Min Vol           =  1.42e-05
UG3      : Average Vol       =  9.33e+03
UG3      : Total-Tet-Vol     =  5.96e+10
UG3      : No. Vol&lt;TOL       =         0

UG3      : Q VOL-LENGTH-RATIO CHECK
                      2/3        2
UG3      : Q = c * Vol   / sum( L  )
UG3      : 0 &lt;= Q &lt;= 1
UG3      : Note that L includes scaling for BL-aspect=ratio

UG3      : No. Tet Elems     =   6388539
UG3      : Min, Max Q        =     0.142         1
UG3      : Average Q         =     0.857
UG3      : No. Q&lt;       0.1  =         0
UG3      : No. Q&lt;      0.01  =         0

UG3      : CPU Time          =     0.000   seconds

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.8.1
EGADS    : ---------------------------------------

EGADS    : CREATE EGADS TESS FROM AFLR3 DATA

EGADS    : CREATING TESSELLATION FOR BODY 0 EDGE 1
EGADS    : CREATING TESSELLATION FOR BODY 0 EDGE 2
EGADS    : CREATING TESSELLATION FOR BODY 0 EDGE 3
EGADS    : CREATING TESSELLATION FOR BODY 0 EDGE 4
EGADS    : CREATING TESSELLATION FOR BODY 0 EDGE 5
EGADS    : CREATING TESSELLATION FOR BODY 0 EDGE 6
EGADS    : CREATING TESSELLATION FOR BODY 0 EDGE 7
EGADS    : CREATING TESSELLATION FOR BODY 0 EDGE 8

EGADS    : CREATING TESSELLATION FOR BODY 0 FACE 1
EGADS    : CREATING TESSELLATION FOR BODY 0 FACE 2
EGADS    : CREATING TESSELLATION FOR BODY 0 FACE 3
EGADS    : CREATING TESSELLATION FOR BODY 0 FACE 4

EGADS    : CREATING TESSELLATION FOR BODY 1 EDGE 9
EGADS    : CREATING TESSELLATION FOR BODY 1 EDGE 10
EGADS    : CREATING TESSELLATION FOR BODY 1 EDGE 11
EGADS    : CREATING TESSELLATION FOR BODY 1 EDGE 12
EGADS    : CREATING TESSELLATION FOR BODY 1 EDGE 13
EGADS    : CREATING TESSELLATION FOR BODY 1 EDGE 14
EGADS    : CREATING TESSELLATION FOR BODY 1 EDGE 15
EGADS    : CREATING TESSELLATION FOR BODY 1 EDGE 16

EGADS    : CREATING TESSELLATION FOR BODY 1 FACE 5
EGADS    : CREATING TESSELLATION FOR BODY 1 FACE 6
EGADS    : CREATING TESSELLATION FOR BODY 1 FACE 7
EGADS    : CREATING TESSELLATION FOR BODY 1 FACE 8

EGADS    : CREATING TESSELLATION FOR BODY 2 EDGE 17
EGADS    : CREATING TESSELLATION FOR BODY 2 EDGE 18
EGADS    : CREATING TESSELLATION FOR BODY 2 EDGE 19
EGADS    : CREATING TESSELLATION FOR BODY 2 EDGE 20
EGADS    : CREATING TESSELLATION FOR BODY 2 EDGE 21
EGADS    : CREATING TESSELLATION FOR BODY 2 EDGE 22
EGADS    : CREATING TESSELLATION FOR BODY 2 EDGE 23
EGADS    : CREATING TESSELLATION FOR BODY 2 EDGE 24
EGADS    : CREATING TESSELLATION FOR BODY 2 EDGE 25
EGADS    : CREATING TESSELLATION FOR BODY 2 EDGE 26
EGADS    : CREATING TESSELLATION FOR BODY 2 EDGE 27
EGADS    : CREATING TESSELLATION FOR BODY 2 EDGE 28
EGADS    : CREATING TESSELLATION FOR BODY 2 EDGE 29
EGADS    : CREATING TESSELLATION FOR BODY 2 EDGE 30
EGADS    : CREATING TESSELLATION FOR BODY 2 EDGE 31
EGADS    : CREATING TESSELLATION FOR BODY 2 EDGE 32
EGADS    : CREATING TESSELLATION FOR BODY 2 EDGE 33
EGADS    : CREATING TESSELLATION FOR BODY 2 EDGE 34

EGADS    : CREATING TESSELLATION FOR BODY 2 FACE 9
EGADS    : CREATING TESSELLATION FOR BODY 2 FACE 10
EGADS    : CREATING TESSELLATION FOR BODY 2 FACE 11
EGADS    : CREATING TESSELLATION FOR BODY 2 FACE 12
EGADS    : CREATING TESSELLATION FOR BODY 2 FACE 13
EGADS    : CREATING TESSELLATION FOR BODY 2 FACE 14
EGADS    : CREATING TESSELLATION FOR BODY 2 FACE 15
EGADS    : CREATING TESSELLATION FOR BODY 2 FACE 16
EGADS    : CREATING TESSELLATION FOR BODY 2 FACE 17
EGADS    : CREATING TESSELLATION FOR BODY 2 FACE 18

EGADS    : CREATING TESSELLATION FOR BODY 3 EDGE 35
EGADS    : CREATING TESSELLATION FOR BODY 3 EDGE 36
EGADS    : CREATING TESSELLATION FOR BODY 3 EDGE 37
EGADS    : CREATING TESSELLATION FOR BODY 3 EDGE 38
EGADS    : CREATING TESSELLATION FOR BODY 3 EDGE 39
EGADS    : CREATING TESSELLATION FOR BODY 3 EDGE 40
EGADS    : CREATING TESSELLATION FOR BODY 3 EDGE 41
EGADS    : CREATING TESSELLATION FOR BODY 3 EDGE 42
EGADS    : CREATING TESSELLATION FOR BODY 3 EDGE 43
EGADS    : CREATING TESSELLATION FOR BODY 3 EDGE 44
EGADS    : CREATING TESSELLATION FOR BODY 3 EDGE 45
EGADS    : CREATING TESSELLATION FOR BODY 3 EDGE 46

EGADS    : CREATING TESSELLATION FOR BODY 3 FACE 19
EGADS    : CREATING TESSELLATION FOR BODY 3 FACE 20
EGADS    : CREATING TESSELLATION FOR BODY 3 FACE 21
EGADS    : CREATING TESSELLATION FOR BODY 3 FACE 22
EGADS    : CREATING TESSELLATION FOR BODY 3 FACE 23
EGADS    : CREATING TESSELLATION FOR BODY 3 FACE 24

EGADS    : EGADS TESS CREATED

EGADS    : CHECK TESS FACE NODE MAP

EGADS    : CHECKING NODE MAP FOR BODY 0 FACE 1
EGADS    : CHECKING NODE MAP FOR BODY 0 FACE 2
EGADS    : CHECKING NODE MAP FOR BODY 0 FACE 3
EGADS    : CHECKING NODE MAP FOR BODY 0 FACE 4
EGADS    : CHECKING NODE MAP FOR BODY 1 FACE 5
EGADS    : CHECKING NODE MAP FOR BODY 1 FACE 6
EGADS    : CHECKING NODE MAP FOR BODY 1 FACE 7
EGADS    : CHECKING NODE MAP FOR BODY 1 FACE 8
EGADS    : CHECKING NODE MAP FOR BODY 2 FACE 9
EGADS    : CHECKING NODE MAP FOR BODY 2 FACE 10
EGADS    : CHECKING NODE MAP FOR BODY 2 FACE 11
EGADS    : CHECKING NODE MAP FOR BODY 2 FACE 12
EGADS    : CHECKING NODE MAP FOR BODY 2 FACE 13
EGADS    : CHECKING NODE MAP FOR BODY 2 FACE 14
EGADS    : CHECKING NODE MAP FOR BODY 2 FACE 15
EGADS    : CHECKING NODE MAP FOR BODY 2 FACE 16
EGADS    : CHECKING NODE MAP FOR BODY 2 FACE 17
EGADS    : CHECKING NODE MAP FOR BODY 2 FACE 18
EGADS    : CHECKING NODE MAP FOR BODY 3 FACE 19
EGADS    : CHECKING NODE MAP FOR BODY 3 FACE 20
EGADS    : CHECKING NODE MAP FOR BODY 3 FACE 21
EGADS    : CHECKING NODE MAP FOR BODY 3 FACE 22
EGADS    : CHECKING NODE MAP FOR BODY 3 FACE 23
EGADS    : CHECKING NODE MAP FOR BODY 3 FACE 24
Volume mesh:
	Number of nodes          = 1128425
	Number of elements       = 6579691
	Number of triangles      = 191152
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 6388539
	Number of pyramids       = 0
	Number of prisms         = 0
	Number of hexahedrals    = 0

Writing vtk file ....

Writing vtk general file ....
Finished writing vtk file


real	1m36.987s
user	1m35.915s
sys	0m1.161s
+ status=0
+ set +x

=================================================
data/session07/09_aflr4_aflr3_InviscidWing.py passed (as expected)
=================================================


=================================================
10_aflr4_aflr3_ViscousWing.py test;
+ python 10_aflr4_aflr3_ViscousWing.py
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/CAPS/training/2023/training.log

MESSAGE:: Building wingOml

Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 2
	Name = Wing, index = 1
	Name = Farfield, index = 2
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 3
	Name = leftWing, index = 1
	Name = riteWing, index = 2
	Name = Farfield, index = 3

Getting mesh sizing parameters
	Mesh sizing name - Farfield
	Done getting mesh sizing parameters
 
AFLR2    : ---------------------------------------
AFLR2    : AFLR2 LIBRARY
AFLR2    : ADVANCING-FRONT/LOCAL-RECONNECTION
AFLR2    : TRIA/QUAD GRID GENERATOR
AFLR2    : Version Number 9.18.1
AFLR2    : Version Date   06/11/24 @ 05:52PM
AFLR2    : Compile OS     Darwin 23.5.0 arm64
AFLR2    : Compile Date   06/11/24 @ 05:52PM
AFLR2    : Copyright 1994-2021, D.L. Marcum
AFLR2    : ---------------------------------------
 
AFLR4    : ---------------------------------------
AFLR4    : AFLR4 LIBRARY
AFLR4    : ADVANCING-FRONT/LOCAL-RECONNECTION
AFLR4    : TRIA/QUAD SURFACE GRID GENERATOR
AFLR4    : Version Number 11.5.15
AFLR4    : Version Date   07/19/24 @ 07:04PM
AFLR4    : Compile OS     Darwin 23.5.0 arm64
AFLR4    : Compile Date   07/19/24 @ 07:06PM
AFLR4    : Copyright 1994-2021, D.L. Marcum
AFLR4    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.8.1
EGADS    : ---------------------------------------

EGADS    : EGADS CAD Geometry Setup

EGADS    : Model has 2 Active Bodies

EGADS    : Body 0 is a SolidBody
EGADS    : Body 0 has 1 Shells
EGADS    : Body 0 has 10 Faces
EGADS    : Body 0 has 18 Edges
EGADS    : Body 0 has 10 Loops
EGADS    : Body 0 has 10 Nodes
EGADS    : Body 1 is a SolidBody
EGADS    : Body 1 has 1 Shells
EGADS    : Body 1 has 6 Faces
EGADS    : Body 1 has 12 Edges
EGADS    : Body 1 has 6 Loops
EGADS    : Body 1 has 8 Nodes

EGADS    : Check Grid BCs

EGADS    : Grid BCs are OK

EGADS    : Face Neighbor-Faces Information

EGADS    : QC  = Face Quad Combination Flag
EGADS    : IER = Face Isolated Edge Refinement Flag
EGADS    : ER  = Face Edge Refinement Factor
EGADS    :       Not applicable for Faces with a FarField Grid BC.
EGADS    : SF  = Face Scale Factor
EGADS    :       Not applicable for Faces with a FarField Grid BC.

EGADS    :   Face          Body    QC   IER       ER    Scale   Neighbor
EGADS    :     ID  Active    ID  Flag  Flag   Weight   Factor   Faces
EGADS    :      1     Yes     0     0     1        0        1   2 3 6
EGADS    :      2     Yes     0     0     1        0        1   1 4 5
EGADS    :      3     Yes     0     0     1        0        1   1 4 8
EGADS    :      4     Yes     0     0     1        0        1   2 3 5
EGADS    :      5     Yes     0     0     1        0        1   2 4
EGADS    :      6     Yes     0     0     1        0        1   1 7 8
EGADS    :      7     Yes     0     0     1        0        1   6 9 10
EGADS    :      8     Yes     0     0     1        0        1   3 6 9
EGADS    :      9     Yes     0     0     1        0        1   7 8 10
EGADS    :     10     Yes     0     0     1        0        1   7 9
EGADS    :     11     Yes     1     0     1       NA       NA   13 14 15 16
EGADS    :     12     Yes     1     0     1       NA       NA   13 14 15 16
EGADS    :     13     Yes     1     0     1       NA       NA   11 12 15 16
EGADS    :     14     Yes     1     0     1       NA       NA   11 12 15 16
EGADS    :     15     Yes     1     0     1       NA       NA   11 12 13 14
EGADS    :     16     Yes     1     0     1       NA       NA   11 12 13 14

EGADS    : Face Edges Information

EGADS    :   Face   Edges
EGADS    :      1   -1 2 3 -4
EGADS    :      2   -5 4 6 -7
EGADS    :      3   -3 8 1 -9
EGADS    :      4   -6 9 5 -10
EGADS    :      5   7 10
EGADS    :      6   11 13 -12 -2
EGADS    :      7   14 16 -15 -13
EGADS    :      8   12 17 -11 -8
EGADS    :      9   15 18 -14 -17
EGADS    :     10   -16 -18
EGADS    :     11   19 20 -21 -22
EGADS    :     12   -23 26 25 -24
EGADS    :     13   27 23 -28 -19
EGADS    :     14   -29 21 30 -25
EGADS    :     15   22 29 -26 -27
EGADS    :     16   -20 28 24 -30

EGADS    : Face Loops Information

EGADS    :   Face   Loops
EGADS    :      1   1
EGADS    :      2   2
EGADS    :      3   3
EGADS    :      4   4
EGADS    :      5   5
EGADS    :      6   6
EGADS    :      7   7
EGADS    :      8   8
EGADS    :      9   9
EGADS    :     10   10
EGADS    :     11   11
EGADS    :     12   12
EGADS    :     13   13
EGADS    :     14   14
EGADS    :     15   15
EGADS    :     16   16

EGADS    : Loop Edges Information

EGADS    :   Loop  Active   Edges
EGADS    :      1     Yes   -1 2 3 -4
EGADS    :      2     Yes   -5 4 6 -7
EGADS    :      3     Yes   -3 8 1 -9
EGADS    :      4     Yes   -6 9 5 -10
EGADS    :      5     Yes   7 10
EGADS    :      6     Yes   11 13 -12 -2
EGADS    :      7     Yes   14 16 -15 -13
EGADS    :      8     Yes   12 17 -11 -8
EGADS    :      9     Yes   15 18 -14 -17
EGADS    :     10     Yes   -16 -18
EGADS    :     11     Yes   19 20 -21 -22
EGADS    :     12     Yes   -23 26 25 -24
EGADS    :     13     Yes   27 23 -28 -19
EGADS    :     14     Yes   -29 21 30 -25
EGADS    :     15     Yes   22 29 -26 -27
EGADS    :     16     Yes   -20 28 24 -30

EGADS    : Edge Node, Scale Factor, and Neighbor-Faces Information

EGADS    : ESF = Edge Scale Factor
EGADS    :       Not applicable for DEGENERATE Edges or Edges with a FarField
EGADS    :       Grid BC Neighbor Face.

EGADS    :                                             Neighbor
EGADS    :   Edge  Body  Active Node1 Node2      ESF   Faces
EGADS    :      1     0     Yes     1     2        1   1 3
EGADS    :      2     0     Yes     1     3        1   1 6
EGADS    :      3     0     Yes     3     4        1   1 3
EGADS    :      4     0     Yes     2     4        1   1 2
EGADS    :      5     0     Yes     2     5        1   2 4
EGADS    :      6     0     Yes     4     6        1   2 4
EGADS    :      7     0     Yes     5     6        1   2 5
EGADS    :      8     0     Yes     3     1        1   3 8
EGADS    :      9     0     Yes     4     2        1   3 4
EGADS    :     10     0     Yes     6     5        1   4 5
EGADS    :     11     0     Yes     1     7        1   6 8
EGADS    :     12     0     Yes     3     8        1   6 8
EGADS    :     13     0     Yes     7     8        1   6 7
EGADS    :     14     0     Yes     7     9        1   7 9
EGADS    :     15     0     Yes     8    10        1   7 9
EGADS    :     16     0     Yes     9    10        1   7 10
EGADS    :     17     0     Yes     8     7        1   8 9
EGADS    :     18     0     Yes    10     9        1   9 10
EGADS    :     19     1     Yes    12    11       NA   11 13
EGADS    :     20     1     Yes    11    13       NA   11 16
EGADS    :     21     1     Yes    14    13       NA   11 14
EGADS    :     22     1     Yes    12    14       NA   11 15
EGADS    :     23     1     Yes    16    15       NA   12 13
EGADS    :     24     1     Yes    15    17       NA   12 16
EGADS    :     25     1     Yes    18    17       NA   12 14
EGADS    :     26     1     Yes    16    18       NA   12 15
EGADS    :     27     1     Yes    12    16       NA   13 15
EGADS    :     28     1     Yes    11    15       NA   13 16
EGADS    :     29     1     Yes    14    18       NA   14 15
EGADS    :     30     1     Yes    13    17       NA   14 16

EGADS    : Node Information

EGADS    :   Node  Active      Coordinates
EGADS    :      1     Yes       97.2007855                0                0
EGADS    :      2     Yes       97.9335611                0                0
EGADS    :      3     Yes               50                0                0
EGADS    :      4     Yes       75.3047874                0                0
EGADS    :      5     Yes       123.552357                0        4.7180639
EGADS    :      6     Yes       118.391317                0       3.99272703
EGADS    :      7     Yes       97.9335611       36.1389817                0
EGADS    :      8     Yes       75.3047874       36.1389817                0
EGADS    :      9     Yes       123.552357       97.6729236        4.7180639
EGADS    :     10     Yes       118.391317       97.6729236       3.99272703
EGADS    :     11     Yes                0                0       1951.57774
EGADS    :     12     Yes                0                0                0
EGADS    :     13     Yes                0       1953.45847       1951.57774
EGADS    :     14     Yes                0       1953.45847                0
EGADS    :     15     Yes       2040.21562                0       1951.57774
EGADS    :     16     Yes       2040.21562                0                0
EGADS    :     17     Yes       2040.21562       1953.45847       1951.57774
EGADS    :     18     Yes       2040.21562       1953.45847                0

EGADS    : Face and Edge Match Information

EGADS    : No Face Matches Found

AFLR4    : Surface Mesh Spacing Setup

AFLR4    : Max Bounding Box Length     = 3906.92
AFLR4    : Min Bounding Box Length     = 3906.92
AFLR4    : Max Ref Bounding Box Length = 195.346
AFLR4    : Min Ref Bounding Box Length = 13.1976
AFLR4    : Reference Length            = 21.7051
AFLR4    : BL Thickness                = 0
AFLR4    : FarField Spacing            = 2651.51
AFLR4    : Abs Min Surf Spacing        = 0.0542627
AFLR4    : Min Surf Spacing            = 0.108525
AFLR4    : Max Surf Spacing            = 2.17051
AFLR4    : Global Scale Factor         = 5

AFLR4    : Geometry Definition Information

AFLR4    : Definition              Definition   Composite             Grid BC
AFLR4    :         ID                    Type          ID                Type
AFLR4    :          0     glue-only composite           -                   -
AFLR4    :          1            CAD geometry           0            STD w/BL
AFLR4    :          2            CAD geometry           0            STD w/BL
AFLR4    :          3            CAD geometry           0            STD w/BL
AFLR4    :          4            CAD geometry           0            STD w/BL
AFLR4    :          5            CAD geometry           0            STD w/BL
AFLR4    :          6            CAD geometry           0            STD w/BL
AFLR4    :          7            CAD geometry           0            STD w/BL
AFLR4    :          8            CAD geometry           0            STD w/BL
AFLR4    :          9            CAD geometry           0            STD w/BL
AFLR4    :         10            CAD geometry           0            STD w/BL
AFLR4    :         11            CAD geometry           0            FARFIELD
AFLR4    :         12            CAD geometry           0            FARFIELD
AFLR4    :         13            CAD geometry           0            FARFIELD
AFLR4    :         14            CAD geometry           0            FARFIELD
AFLR4    :         15            CAD geometry           0            FARFIELD
AFLR4    :         16            CAD geometry           0            FARFIELD

AFLR4    : Define CAD surface definition 1
AFLR4    : Define CAD surface definition 2
AFLR4    : Define CAD surface definition 3
AFLR4    : Define CAD surface definition 4
AFLR4    : Define CAD surface definition 5
AFLR4    : Define CAD surface definition 6
AFLR4    : Define CAD surface definition 7
AFLR4    : Define CAD surface definition 8
AFLR4    : Define CAD surface definition 9
AFLR4    : Define CAD surface definition 10
AFLR4    : Define CAD surface definition 11
AFLR4    : Define CAD surface definition 12
AFLR4    : Define CAD surface definition 13
AFLR4    : Define CAD surface definition 14
AFLR4    : Define CAD surface definition 15
AFLR4    : Define CAD surface definition 16

AFLR4    : Surface Grid Generation

AFLR4    : Generate optimal mesh on surface definition 1
AFLR2    : Nodes, Trias,Quads=      1107      2082         0
AFLR4    : Nodes, Trias,Quads=       685      1238         0

AFLR4    : Generate optimal mesh on surface definition 2
AFLR2    : Nodes, Trias,Quads=      1473      2759         0
AFLR4    : Nodes, Trias,Quads=       721      1255         0

AFLR4    : Generate optimal mesh on surface definition 3
AFLR2    : Nodes, Trias,Quads=      1116      2100         0
AFLR4    : Nodes, Trias,Quads=       671      1210         0

AFLR4    : Generate optimal mesh on surface definition 4
AFLR2    : Nodes, Trias,Quads=      1458      2729         0
AFLR4    : Nodes, Trias,Quads=       714      1241         0

AFLR4    : Generate optimal mesh on surface definition 5
AFLR2    : Nodes, Trias,Quads=        20        24         0
AFLR4    : Nodes, Trias,Quads=        14        12         0

AFLR4    : Generate optimal mesh on surface definition 6
AFLR2    : Nodes, Trias,Quads=      1108      2084         0
AFLR4    : Nodes, Trias,Quads=       683      1234         0

AFLR4    : Generate optimal mesh on surface definition 7
AFLR2    : Nodes, Trias,Quads=      1488      2789         0
AFLR4    : Nodes, Trias,Quads=       714      1241         0

AFLR4    : Generate optimal mesh on surface definition 8
AFLR2    : Nodes, Trias,Quads=      1112      2092         0
AFLR4    : Nodes, Trias,Quads=       653      1174         0

AFLR4    : Generate optimal mesh on surface definition 9
AFLR2    : Nodes, Trias,Quads=      1456      2725         0
AFLR4    : Nodes, Trias,Quads=       708      1229         0

AFLR4    : Generate optimal mesh on surface definition 10
AFLR2    : Nodes, Trias,Quads=        20        24         0
AFLR4    : Nodes, Trias,Quads=        14        12         0

AFLR4    : Generate optimal mesh on surface definition 11
AFLR2    : Nodes, Trias,Quads=         5         4         0
AFLR4    : Nodes, Trias,Quads=         4         2         0

AFLR4    : Generate optimal mesh on surface definition 12
AFLR2    : Nodes, Trias,Quads=         5         4         0
AFLR4    : Nodes, Trias,Quads=         4         2         0

AFLR4    : Generate optimal mesh on surface definition 13
AFLR2    : Nodes, Trias,Quads=         5         4         0
AFLR4    : Nodes, Trias,Quads=         4         2         0

AFLR4    : Generate optimal mesh on surface definition 14
AFLR2    : Nodes, Trias,Quads=         5         4         0
AFLR4    : Nodes, Trias,Quads=         4         2         0

AFLR4    : Generate optimal mesh on surface definition 15
AFLR2    : Nodes, Trias,Quads=         5         4         0
AFLR4    : Nodes, Trias,Quads=         4         2         0

AFLR4    : Generate optimal mesh on surface definition 16
AFLR2    : Nodes, Trias,Quads=         5         4         0
AFLR4    : Nodes, Trias,Quads=         4         2         0

DGEOM    : Add surface definitions to composite definition 0
DGEOM    : Glue composite surface definition 0
DGEOM    : Nodes,Faces,BEdges=      4933      9858      1312

AFLR4    : Curvature BG Surface Grid Generation

AFLR4    : Nodes, Faces      =      4933      9858

AFLR4    : Surface Grid Generation

AFLR4    : Generate optimal mesh on surface definition 1
AFLR2    : Nodes, Trias,Quads=      1115      2096         0
AFLR4    : Nodes, Trias,Quads=       948      1762         0

AFLR4    : Generate optimal mesh on surface definition 2
AFLR2    : Nodes, Trias,Quads=      1450      2716         0
AFLR4    : Nodes, Trias,Quads=      1183      2182         0

AFLR4    : Generate optimal mesh on surface definition 3
AFLR2    : Nodes, Trias,Quads=      1125      2116         0
AFLR4    : Nodes, Trias,Quads=       936      1738         0

AFLR4    : Generate optimal mesh on surface definition 4
AFLR2    : Nodes, Trias,Quads=      1477      2769         0
AFLR4    : Nodes, Trias,Quads=      1165      2145         0

AFLR4    : Generate optimal mesh on surface definition 5
AFLR2    : Nodes, Trias,Quads=        26        35         0
AFLR4    : Nodes, Trias,Quads=        15        13         0

AFLR4    : Generate optimal mesh on surface definition 6
AFLR2    : Nodes, Trias,Quads=      1106      2078         0
AFLR4    : Nodes, Trias,Quads=       957      1780         0

AFLR4    : Generate optimal mesh on surface definition 7
AFLR2    : Nodes, Trias,Quads=      1453      2723         0
AFLR4    : Nodes, Trias,Quads=      1179      2175         0

AFLR4    : Generate optimal mesh on surface definition 8
AFLR2    : Nodes, Trias,Quads=      1118      2102         0
AFLR4    : Nodes, Trias,Quads=       953      1772         0

AFLR4    : Generate optimal mesh on surface definition 9
AFLR2    : Nodes, Trias,Quads=      1477      2770         0
AFLR4    : Nodes, Trias,Quads=      1147      2110         0

AFLR4    : Generate optimal mesh on surface definition 10
AFLR2    : Nodes, Trias,Quads=        26        35         0
AFLR4    : Nodes, Trias,Quads=        15        13         0

AFLR4    : Generate optimal mesh on surface definition 11
AFLR2    : Nodes, Trias,Quads=        12        14         0
AFLR4    : Nodes, Trias,Quads=         8         6         0

AFLR4    : Generate optimal mesh on surface definition 12
AFLR2    : Nodes, Trias,Quads=        12        14         0
AFLR4    : Nodes, Trias,Quads=         8         6         0

AFLR4    : Generate optimal mesh on surface definition 13
AFLR2    : Nodes, Trias,Quads=        12        14         0
AFLR4    : Nodes, Trias,Quads=         8         6         0

AFLR4    : Generate optimal mesh on surface definition 14
AFLR2    : Nodes, Trias,Quads=        12        14         0
AFLR4    : Nodes, Trias,Quads=         8         6         0

AFLR4    : Generate optimal mesh on surface definition 15
AFLR2    : Nodes, Trias,Quads=        12        14         0
AFLR4    : Nodes, Trias,Quads=         8         6         0

AFLR4    : Generate optimal mesh on surface definition 16
AFLR2    : Nodes, Trias,Quads=        12        14         0
AFLR4    : Nodes, Trias,Quads=         8         6         0

DGEOM    : Add surface definitions to composite definition 0
DGEOM    : Glue composite surface definition 0
DGEOM    : Nodes,Faces,BEdges=      7867     15726      1334

OVERALL  : CPU Time          =     0.150   seconds
Body 1 (of 2)
Number of nodes    = 7847
Number of elements = 15690
Number of triangle elements      = 15690
Number of quadrilateral elements = 0
Body 2 (of 2)
Number of nodes    = 20
Number of elements = 36
Number of triangle elements      = 36
Number of quadrilateral elements = 0
----------------------------
Total number of nodes    = 7867
Total number of elements = 15726
Total number of triangle elements      = 15726
Total number of quadrilateral elements = 0

Writing vtk file ....

Writing vtk surface file ....

capsGroups found:
  1: Wing
  2: Farfield
Finished writing vtk file

Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 3
	Name = leftWing, index = 1
	Name = riteWing, index = 2
	Name = Farfield, index = 3
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 2
	Name = Wing, index = 1
	Name = Farfield, index = 2
Getting volume mesh
 
UG PARAM : SETTING INPUT PARAMETERS FROM ARGUMENT VECTOR
 
UG PARAM : mbl                         = 1         
UG PARAM : nbl                         = 10        
UG PARAM : mblelc                      = 2         
UG PARAM : mrecm                       = 3         
UG PARAM : mrecqm                      = 3         
UG PARAM : mbl                         = 1         
UG PARAM : mrecm                       = 3         
UG PARAM : mrecqm                      = 3         
UG PARAM : mblelc                      = 1         
UG PARAM : BC_IDs                  [ 0]= 1         
UG PARAM : BC_IDs                  [ 1]= 2         
UG PARAM : BC_IDs                  [ 2]= 3         
UG PARAM : BC_IDs                  [ 3]= 4         
UG PARAM : BC_IDs                  [ 4]= 5         
UG PARAM : BC_IDs                  [ 5]= 6         
UG PARAM : BC_IDs                  [ 6]= 7         
UG PARAM : BC_IDs                  [ 7]= 8         
UG PARAM : BC_IDs                  [ 8]= 9         
UG PARAM : BC_IDs                  [ 9]= 10        
UG PARAM : BC_IDs                  [10]= 11        
UG PARAM : BC_IDs                  [11]= 12        
UG PARAM : BC_IDs                  [12]= 13        
UG PARAM : BC_IDs                  [13]= 14        
UG PARAM : BC_IDs                  [14]= 15        
UG PARAM : BC_IDs                  [15]= 16        
UG PARAM : BL_DS                   [ 0]= 0.217051  
UG PARAM : BL_DS                   [ 1]= 0.217051  
UG PARAM : BL_DS                   [ 2]= 0.217051  
UG PARAM : BL_DS                   [ 3]= 0.217051  
UG PARAM : BL_DS                   [ 4]= 0.217051  
UG PARAM : BL_DS                   [ 5]= 0.217051  
UG PARAM : BL_DS                   [ 6]= 0.217051  
UG PARAM : BL_DS                   [ 7]= 0.217051  
UG PARAM : BL_DS                   [ 8]= 0.217051  
UG PARAM : BL_DS                   [ 9]= 0.217051  
UG PARAM : BL_DS                   [10]= 0.217051  
UG PARAM : BL_DS                   [11]= 0.217051  
UG PARAM : BL_DS                   [12]= 0.217051  
UG PARAM : BL_DS                   [13]= 0.217051  
UG PARAM : BL_DS                   [14]= 0.217051  
UG PARAM : BL_DS                   [15]= 0.217051  
UG PARAM : BL_DEL                  [ 0]= 2.17051   
UG PARAM : BL_DEL                  [ 1]= 2.17051   
UG PARAM : BL_DEL                  [ 2]= 2.17051   
UG PARAM : BL_DEL                  [ 3]= 2.17051   
UG PARAM : BL_DEL                  [ 4]= 2.17051   
UG PARAM : BL_DEL                  [ 5]= 2.17051   
UG PARAM : BL_DEL                  [ 6]= 2.17051   
UG PARAM : BL_DEL                  [ 7]= 2.17051   
UG PARAM : BL_DEL                  [ 8]= 2.17051   
UG PARAM : BL_DEL                  [ 9]= 2.17051   
UG PARAM : BL_DEL                  [10]= 2.17051   
UG PARAM : BL_DEL                  [11]= 2.17051   
UG PARAM : BL_DEL                  [12]= 2.17051   
UG PARAM : BL_DEL                  [13]= 2.17051   
UG PARAM : BL_DEL                  [14]= 2.17051   
UG PARAM : BL_DEL                  [15]= 2.17051   
UG PARAM : mpfrmt                      = 0         
 
AFLR2    : ---------------------------------------
AFLR2    : AFLR2 LIBRARY
AFLR2    : ADVANCING-FRONT/LOCAL-RECONNECTION
AFLR2    : TRIA/QUAD GRID GENERATOR
AFLR2    : Version Number 9.18.1
AFLR2    : Version Date   06/11/24 @ 05:52PM
AFLR2    : Compile OS     Darwin 23.5.0 arm64
AFLR2    : Compile Date   06/11/24 @ 05:52PM
AFLR2    : Copyright 1994-2021, D.L. Marcum
AFLR2    : ---------------------------------------
 
AFLR4    : ---------------------------------------
AFLR4    : AFLR4 LIBRARY
AFLR4    : ADVANCING-FRONT/LOCAL-RECONNECTION
AFLR4    : TRIA/QUAD SURFACE GRID GENERATOR
AFLR4    : Version Number 11.5.15
AFLR4    : Version Date   07/19/24 @ 07:04PM
AFLR4    : Compile OS     Darwin 23.5.0 arm64
AFLR4    : Compile Date   07/19/24 @ 07:06PM
AFLR4    : Copyright 1994-2021, D.L. Marcum
AFLR4    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.8.1
EGADS    : ---------------------------------------

EGADS    : EGADS CAD Geometry Setup

EGADS    : Model has 2 Active Bodies

EGADS    : Body 0 is a SolidBody
EGADS    : Body 0 has 1 Shells
EGADS    : Body 0 has 10 Faces
EGADS    : Body 0 has 18 Edges
EGADS    : Body 0 has 10 Loops
EGADS    : Body 0 has 10 Nodes
EGADS    : Body 1 is a SolidBody
EGADS    : Body 1 has 1 Shells
EGADS    : Body 1 has 6 Faces
EGADS    : Body 1 has 12 Edges
EGADS    : Body 1 has 6 Loops
EGADS    : Body 1 has 8 Nodes

EGADS    : Check Grid BCs

EGADS    : Grid BCs are OK

EGADS    : Face Neighbor-Faces Information

EGADS    : QC  = Face Quad Combination Flag
EGADS    : IER = Face Isolated Edge Refinement Flag
EGADS    : ER  = Face Edge Refinement Factor
EGADS    :       Not applicable for Faces with a FarField Grid BC.
EGADS    : SF  = Face Scale Factor
EGADS    :       Not applicable for Faces with a FarField Grid BC.

EGADS    :   Face          Body    QC   IER       ER    Scale   Neighbor
EGADS    :     ID  Active    ID  Flag  Flag   Weight   Factor   Faces
EGADS    :      1     Yes     0     0     1        0        1   2 3 6
EGADS    :      2     Yes     0     0     1        0        1   1 4 5
EGADS    :      3     Yes     0     0     1        0        1   1 4 8
EGADS    :      4     Yes     0     0     1        0        1   2 3 5
EGADS    :      5     Yes     0     0     1        0        1   2 4
EGADS    :      6     Yes     0     0     1        0        1   1 7 8
EGADS    :      7     Yes     0     0     1        0        1   6 9 10
EGADS    :      8     Yes     0     0     1        0        1   3 6 9
EGADS    :      9     Yes     0     0     1        0        1   7 8 10
EGADS    :     10     Yes     0     0     1        0        1   7 9
EGADS    :     11     Yes     1     0     1       NA       NA   13 14 15 16
EGADS    :     12     Yes     1     0     1       NA       NA   13 14 15 16
EGADS    :     13     Yes     1     0     1       NA       NA   11 12 15 16
EGADS    :     14     Yes     1     0     1       NA       NA   11 12 15 16
EGADS    :     15     Yes     1     0     1       NA       NA   11 12 13 14
EGADS    :     16     Yes     1     0     1       NA       NA   11 12 13 14

EGADS    : Face Edges Information

EGADS    :   Face   Edges
EGADS    :      1   -1 2 3 -4
EGADS    :      2   -5 4 6 -7
EGADS    :      3   -3 8 1 -9
EGADS    :      4   -6 9 5 -10
EGADS    :      5   7 10
EGADS    :      6   11 13 -12 -2
EGADS    :      7   14 16 -15 -13
EGADS    :      8   12 17 -11 -8
EGADS    :      9   15 18 -14 -17
EGADS    :     10   -16 -18
EGADS    :     11   19 20 -21 -22
EGADS    :     12   -23 26 25 -24
EGADS    :     13   27 23 -28 -19
EGADS    :     14   -29 21 30 -25
EGADS    :     15   22 29 -26 -27
EGADS    :     16   -20 28 24 -30

EGADS    : Face Loops Information

EGADS    :   Face   Loops
EGADS    :      1   1
EGADS    :      2   2
EGADS    :      3   3
EGADS    :      4   4
EGADS    :      5   5
EGADS    :      6   6
EGADS    :      7   7
EGADS    :      8   8
EGADS    :      9   9
EGADS    :     10   10
EGADS    :     11   11
EGADS    :     12   12
EGADS    :     13   13
EGADS    :     14   14
EGADS    :     15   15
EGADS    :     16   16

EGADS    : Loop Edges Information

EGADS    :   Loop  Active   Edges
EGADS    :      1     Yes   -1 2 3 -4
EGADS    :      2     Yes   -5 4 6 -7
EGADS    :      3     Yes   -3 8 1 -9
EGADS    :      4     Yes   -6 9 5 -10
EGADS    :      5     Yes   7 10
EGADS    :      6     Yes   11 13 -12 -2
EGADS    :      7     Yes   14 16 -15 -13
EGADS    :      8     Yes   12 17 -11 -8
EGADS    :      9     Yes   15 18 -14 -17
EGADS    :     10     Yes   -16 -18
EGADS    :     11     Yes   19 20 -21 -22
EGADS    :     12     Yes   -23 26 25 -24
EGADS    :     13     Yes   27 23 -28 -19
EGADS    :     14     Yes   -29 21 30 -25
EGADS    :     15     Yes   22 29 -26 -27
EGADS    :     16     Yes   -20 28 24 -30

EGADS    : Edge Node, Scale Factor, and Neighbor-Faces Information

EGADS    : ESF = Edge Scale Factor
EGADS    :       Not applicable for DEGENERATE Edges or Edges with a FarField
EGADS    :       Grid BC Neighbor Face.

EGADS    :                                             Neighbor
EGADS    :   Edge  Body  Active Node1 Node2      ESF   Faces
EGADS    :      1     0     Yes     1     2        1   1 3
EGADS    :      2     0     Yes     1     3        1   1 6
EGADS    :      3     0     Yes     3     4        1   1 3
EGADS    :      4     0     Yes     2     4        1   1 2
EGADS    :      5     0     Yes     2     5        1   2 4
EGADS    :      6     0     Yes     4     6        1   2 4
EGADS    :      7     0     Yes     5     6        1   2 5
EGADS    :      8     0     Yes     3     1        1   3 8
EGADS    :      9     0     Yes     4     2        1   3 4
EGADS    :     10     0     Yes     6     5        1   4 5
EGADS    :     11     0     Yes     1     7        1   6 8
EGADS    :     12     0     Yes     3     8        1   6 8
EGADS    :     13     0     Yes     7     8        1   6 7
EGADS    :     14     0     Yes     7     9        1   7 9
EGADS    :     15     0     Yes     8    10        1   7 9
EGADS    :     16     0     Yes     9    10        1   7 10
EGADS    :     17     0     Yes     8     7        1   8 9
EGADS    :     18     0     Yes    10     9        1   9 10
EGADS    :     19     1     Yes    12    11       NA   11 13
EGADS    :     20     1     Yes    11    13       NA   11 16
EGADS    :     21     1     Yes    14    13       NA   11 14
EGADS    :     22     1     Yes    12    14       NA   11 15
EGADS    :     23     1     Yes    16    15       NA   12 13
EGADS    :     24     1     Yes    15    17       NA   12 16
EGADS    :     25     1     Yes    18    17       NA   12 14
EGADS    :     26     1     Yes    16    18       NA   12 15
EGADS    :     27     1     Yes    12    16       NA   13 15
EGADS    :     28     1     Yes    11    15       NA   13 16
EGADS    :     29     1     Yes    14    18       NA   14 15
EGADS    :     30     1     Yes    13    17       NA   14 16

EGADS    : Node Information

EGADS    :   Node  Active      Coordinates
EGADS    :      1     Yes       97.2007855                0                0
EGADS    :      2     Yes       97.9335611                0                0
EGADS    :      3     Yes               50                0                0
EGADS    :      4     Yes       75.3047874                0                0
EGADS    :      5     Yes       123.552357                0        4.7180639
EGADS    :      6     Yes       118.391317                0       3.99272703
EGADS    :      7     Yes       97.9335611       36.1389817                0
EGADS    :      8     Yes       75.3047874       36.1389817                0
EGADS    :      9     Yes       123.552357       97.6729236        4.7180639
EGADS    :     10     Yes       118.391317       97.6729236       3.99272703
EGADS    :     11     Yes                0                0       1951.57774
EGADS    :     12     Yes                0                0                0
EGADS    :     13     Yes                0       1953.45847       1951.57774
EGADS    :     14     Yes                0       1953.45847                0
EGADS    :     15     Yes       2040.21562                0       1951.57774
EGADS    :     16     Yes       2040.21562                0                0
EGADS    :     17     Yes       2040.21562       1953.45847       1951.57774
EGADS    :     18     Yes       2040.21562       1953.45847                0

EGADS    : Face and Edge Match Information

EGADS    : No Face Matches Found

AFLR4    : Surface Mesh Spacing Setup

AFLR4    : Max Bounding Box Length     = 3906.92
AFLR4    : Min Bounding Box Length     = 3906.92
AFLR4    : Max Ref Bounding Box Length = 195.346
AFLR4    : Min Ref Bounding Box Length = 13.1976
AFLR4    : Reference Length            = 13.1976
AFLR4    : BL Thickness                = 0
AFLR4    : FarField Spacing            = 428.309
AFLR4    : Abs Min Surf Spacing        = 0.032994
AFLR4    : Min Surf Spacing            = 0.065988
AFLR4    : Max Surf Spacing            = 1.31976
AFLR4    : Global Scale Factor         = 1

AFLR4    : Geometry Definition Information

AFLR4    : Definition              Definition   Composite             Grid BC
AFLR4    :         ID                    Type          ID                Type
AFLR4    :          0     glue-only composite           -                   -
AFLR4    :          1            CAD geometry           0            STD w/BL
AFLR4    :          2            CAD geometry           0            STD w/BL
AFLR4    :          3            CAD geometry           0            STD w/BL
AFLR4    :          4            CAD geometry           0            STD w/BL
AFLR4    :          5            CAD geometry           0            STD w/BL
AFLR4    :          6            CAD geometry           0            STD w/BL
AFLR4    :          7            CAD geometry           0            STD w/BL
AFLR4    :          8            CAD geometry           0            STD w/BL
AFLR4    :          9            CAD geometry           0            STD w/BL
AFLR4    :         10            CAD geometry           0            STD w/BL
AFLR4    :         11            CAD geometry           0            FARFIELD
AFLR4    :         12            CAD geometry           0            FARFIELD
AFLR4    :         13            CAD geometry           0            FARFIELD
AFLR4    :         14            CAD geometry           0            FARFIELD
AFLR4    :         15            CAD geometry           0            FARFIELD
AFLR4    :         16            CAD geometry           0            FARFIELD

AFLR4    : Define CAD surface definition 1
AFLR4    : Define CAD surface definition 2
AFLR4    : Define CAD surface definition 3
AFLR4    : Define CAD surface definition 4
AFLR4    : Define CAD surface definition 5
AFLR4    : Define CAD surface definition 6
AFLR4    : Define CAD surface definition 7
AFLR4    : Define CAD surface definition 8
AFLR4    : Define CAD surface definition 9
AFLR4    : Define CAD surface definition 10
AFLR4    : Define CAD surface definition 11
AFLR4    : Define CAD surface definition 12
AFLR4    : Define CAD surface definition 13
AFLR4    : Define CAD surface definition 14
AFLR4    : Define CAD surface definition 15
AFLR4    : Define CAD surface definition 16
 
AFLR43   : INPUT SURFACE MESH FROM TESS
 
AFLR43   : Quad Surface Faces=         0
AFLR43   : Tria Surface Faces=     15726
AFLR43   : Nodes             =      7867
 
 
UG PARAM : SETTING INPUT PARAMETERS FROM ARGUMENT VECTOR
 
UG PARAM : mbl                         = 1         
UG PARAM : nbl                         = 10        
UG PARAM : mblelc                      = 2         
UG PARAM : mrecm                       = 3         
UG PARAM : mrecqm                      = 3         
UG PARAM : mbl                         = 1         
UG PARAM : mrecm                       = 3         
UG PARAM : mrecqm                      = 3         
UG PARAM : mblelc                      = 1         
UG PARAM : BC_IDs                  [ 0]= 1         
UG PARAM : BC_IDs                  [ 1]= 2         
UG PARAM : BC_IDs                  [ 2]= 3         
UG PARAM : BC_IDs                  [ 3]= 4         
UG PARAM : BC_IDs                  [ 4]= 5         
UG PARAM : BC_IDs                  [ 5]= 6         
UG PARAM : BC_IDs                  [ 6]= 7         
UG PARAM : BC_IDs                  [ 7]= 8         
UG PARAM : BC_IDs                  [ 8]= 9         
UG PARAM : BC_IDs                  [ 9]= 10        
UG PARAM : BC_IDs                  [10]= 11        
UG PARAM : BC_IDs                  [11]= 12        
UG PARAM : BC_IDs                  [12]= 13        
UG PARAM : BC_IDs                  [13]= 14        
UG PARAM : BC_IDs                  [14]= 15        
UG PARAM : BC_IDs                  [15]= 16        
UG PARAM : BL_DS                   [ 0]= 0.217051  
UG PARAM : BL_DS                   [ 1]= 0.217051  
UG PARAM : BL_DS                   [ 2]= 0.217051  
UG PARAM : BL_DS                   [ 3]= 0.217051  
UG PARAM : BL_DS                   [ 4]= 0.217051  
UG PARAM : BL_DS                   [ 5]= 0.217051  
UG PARAM : BL_DS                   [ 6]= 0.217051  
UG PARAM : BL_DS                   [ 7]= 0.217051  
UG PARAM : BL_DS                   [ 8]= 0.217051  
UG PARAM : BL_DS                   [ 9]= 0.217051  
UG PARAM : BL_DS                   [10]= 0.217051  
UG PARAM : BL_DS                   [11]= 0.217051  
UG PARAM : BL_DS                   [12]= 0.217051  
UG PARAM : BL_DS                   [13]= 0.217051  
UG PARAM : BL_DS                   [14]= 0.217051  
UG PARAM : BL_DS                   [15]= 0.217051  
UG PARAM : BL_DEL                  [ 0]= 2.17051   
UG PARAM : BL_DEL                  [ 1]= 2.17051   
UG PARAM : BL_DEL                  [ 2]= 2.17051   
UG PARAM : BL_DEL                  [ 3]= 2.17051   
UG PARAM : BL_DEL                  [ 4]= 2.17051   
UG PARAM : BL_DEL                  [ 5]= 2.17051   
UG PARAM : BL_DEL                  [ 6]= 2.17051   
UG PARAM : BL_DEL                  [ 7]= 2.17051   
UG PARAM : BL_DEL                  [ 8]= 2.17051   
UG PARAM : BL_DEL                  [ 9]= 2.17051   
UG PARAM : BL_DEL                  [10]= 2.17051   
UG PARAM : BL_DEL                  [11]= 2.17051   
UG PARAM : BL_DEL                  [12]= 2.17051   
UG PARAM : BL_DEL                  [13]= 2.17051   
UG PARAM : BL_DEL                  [14]= 2.17051   
UG PARAM : BL_DEL                  [15]= 2.17051   
UG PARAM : mpfrmt                      = 0         
 
AFLR3    : ---------------------------------------
AFLR3    : AFLR3 LIBRARY
AFLR3    : ADVANCING-FRONT/LOCAL-RECONNECTION
AFLR3    : TETRAHEDRAL GRID GENERATOR
AFLR3    : Version Number 16.32.50
AFLR3    : Version Date   10/31/23 @ 06:31PM
AFLR3    : Compile OS     Darwin 23.3.0 arm64
AFLR3    : Compile Date   02/08/24 @ 04:22PM
AFLR3    : Copyright 1994-2021, D.L. Marcum
AFLR3    : ---------------------------------------
 
AFLR3 IC : INPUT SURFACE GRID CHECK
 
AFLR3 IC : Nodes, Elements   =      7867         0

UG3      : Boundary Conditions

UG3      :  B-Face ID            Boundary Condition
UG3      :          1                    Solid w/BL
UG3      :          2                    Solid w/BL
UG3      :          3                    Solid w/BL
UG3      :          4                    Solid w/BL
UG3      :          5                    Solid w/BL
UG3      :          6                    Solid w/BL
UG3      :          7                    Solid w/BL
UG3      :          8                    Solid w/BL
UG3      :          9                    Solid w/BL
UG3      :         10                    Solid w/BL
UG3      :         11                      FarField
UG3      :         12                      FarField
UG3      :         13                      FarField
UG3      :         14                      FarField
UG3      :         15                      FarField
UG3      :         16                      FarField
 
AFLR3    : CPU Time          =     0.009   seconds
 
AFLR3    : DONE
 
ANBL3    : ---------------------------------------
ANBL3    : ANBL3 LIBRARY
ANBL3    : ADVANCING-NORMAL
ANBL3    : BOUNDARY-LAYER (BL)
ANBL3    : STRUCTURED-LAYER (SL)
ANBL3    : SPECIFIED NORMAL SPACING (SNS)
ANBL3    : TETRAHEDRAL/PENTAHEDRAL GRID GENERATOR
ANBL3    : Version Number 9.34.2
ANBL3    : Version Date   03/10/23 @ 04:32PM
ANBL3    : Compile OS     Darwin 23.3.0 arm64
ANBL3    : Compile Date   02/08/24 @ 04:22PM
ANBL3    : Copyright 1994-2021, D.L. Marcum
ANBL3    : ---------------------------------------
 
ANBL3 BLC: BL BOUNDARY CONDITIONS CHECK
 
ANBL3 BLC: Nodes, Elements   =      7867         0
 
ANBL3    : CPU Time          =     0.008   seconds
 
ANBL3    : DONE
 
ANBL3 BLG: BL NODE GENERATION
 
ANBL3 BLG: Nodes, Layer      =         0         0
ANBL3 BLG: Nodes, Layer      =     15694         2
ANBL3 BLG: Nodes, Layer      =     23541         3
ANBL3 BLG: Nodes, Layer      =     31384         4
ANBL3 BLG: Nodes, Layer      =     39209         5
ANBL3 BLG: Nodes, Layer      =     47034         6
ANBL3 BLG: Nodes, Layer      =     62668         8
ANBL3 BLG: Nodes, Layer      =     70485         9
ANBL3 BLG: Nodes, Layer      =     78298        10
ANBL3 BLG: Nodes, Layer      =     86108        11
 
ANBL3    : CPU Time          =     1.689   seconds
 
ANBL3    : DONE
 
AFLR3 IC : INPUT SURFACE GRID CHECK
 
AFLR3 IC : Nodes, Elements   =      7867         0
 
AFLR3    : CPU Time          =     0.005   seconds
 
AFLR3 IG : INITIAL VOLUME GRID GENERATION
 
AFLR3 IG : Nodes, Elements   =      7867         0
AFLR3 IG : Nodes, Elements   =         8        10
AFLR3 IG : Nodes, Elements   =      1574     11548
AFLR3 IG : Nodes, Elements   =      3148     23433
AFLR3 IG : Nodes, Elements   =      4722     34747
AFLR3 IG : Nodes, Elements   =      6296     47989
AFLR3 IG : Nodes, Elements   =      7870     61732
AFLR3 IG : Nodes, Elements   =      7874     61705
AFLR3 IG : Nodes, Elements   =      7874     61706
AFLR3 IG : Nodes, Elements   =      7874     61623
AFLR3 IG : Nodes, Elements   =      7874     61706
AFLR3 IG : Nodes, Elements   =      7874     61496
AFLR3 IG : Nodes, Elements   =      7874     61498
AFLR3 IG : Nodes, Elements   =      7867     38596
AFLR3 IG : Nodes, Elements   =      7867     38782
AFLR3 IG : Nodes, Elements   =      7867     29831
AFLR3 IG : Nodes, Elements   =      7867     25823
 
AFLR3    : CPU Time          =     0.129   seconds
 
AFLR3 GG : ISOTROPIC VOLUME GRID GENERATION
 
AFLR3 GG : Nodes, Elements   =      7867     25823
AFLR3 GG : Nodes, Elements   =     10946     35182
AFLR3 GG : Nodes, Elements   =     10946     47516
AFLR3 GG : Nodes, Elements   =     10946     43444
AFLR3 GG : Nodes, Elements   =     13492     51414
AFLR3 GG : Nodes, Elements   =     13492     61230
AFLR3 GG : Nodes, Elements   =     13492     57306
AFLR3 GG : Nodes, Elements   =     16631     66944
AFLR3 GG : Nodes, Elements   =     16631     79377
AFLR3 GG : Nodes, Elements   =     16631     75560
AFLR3 GG : Nodes, Elements   =     19759     85053
AFLR3 GG : Nodes, Elements   =     19759     98029
AFLR3 GG : Nodes, Elements   =     19759     94286
AFLR3 GG : Nodes, Elements   =     22986    104051
AFLR3 GG : Nodes, Elements   =     22986    116794
AFLR3 GG : Nodes, Elements   =     22986    113401
AFLR3 GG : Nodes, Elements   =     26089    122790
AFLR3 GG : Nodes, Elements   =     26089    135033
AFLR3 GG : Nodes, Elements   =     26089    131747
AFLR3 GG : Nodes, Elements   =     29272    141349
AFLR3 GG : Nodes, Elements   =     29272    153867
AFLR3 GG : Nodes, Elements   =     29272    150645
AFLR3 GG : Nodes, Elements   =     32276    159688
AFLR3 GG : Nodes, Elements   =     32276    171615
AFLR3 GG : Nodes, Elements   =     32276    168520
AFLR3 GG : Nodes, Elements   =     35203    177336
AFLR3 GG : Nodes, Elements   =     35203    188654
AFLR3 GG : Nodes, Elements   =     35203    185837
AFLR3 GG : Nodes, Elements   =     38011    194280
AFLR3 GG : Nodes, Elements   =     38011    205443
AFLR3 GG : Nodes, Elements   =     38011    202533
AFLR3 GG : Nodes, Elements   =     40671    210539
AFLR3 GG : Nodes, Elements   =     40671    221055
AFLR3 GG : Nodes, Elements   =     40671    218360
AFLR3 GG : Nodes, Elements   =     43226    226045
AFLR3 GG : Nodes, Elements   =     43226    236088
AFLR3 GG : Nodes, Elements   =     43226    233582
AFLR3 GG : Nodes, Elements   =     45650    240880
AFLR3 GG : Nodes, Elements   =     45650    250374
AFLR3 GG : Nodes, Elements   =     45650    247948
AFLR3 GG : Nodes, Elements   =     47957    254895
AFLR3 GG : Nodes, Elements   =     47957    263946
AFLR3 GG : Nodes, Elements   =     47957    261694
AFLR3 GG : Nodes, Elements   =     50132    268238
AFLR3 GG : Nodes, Elements   =     50132    276829
AFLR3 GG : Nodes, Elements   =     50132    274612
AFLR3 GG : Nodes, Elements   =     52187    280792
AFLR3 GG : Nodes, Elements   =     52187    288902
AFLR3 GG : Nodes, Elements   =     52187    286919
AFLR3 GG : Nodes, Elements   =     54105    292688
AFLR3 GG : Nodes, Elements   =     54105    300236
AFLR3 GG : Nodes, Elements   =     54105    298298
AFLR3 GG : Nodes, Elements   =     55940    303816
AFLR3 GG : Nodes, Elements   =     55940    310917
AFLR3 GG : Nodes, Elements   =     55940    309193
AFLR3 GG : Nodes, Elements   =     57654    314342
AFLR3 GG : Nodes, Elements   =     57654    321069
AFLR3 GG : Nodes, Elements   =     57654    319375
AFLR3 GG : Nodes, Elements   =     59279    324265
AFLR3 GG : Nodes, Elements   =     59279    330695
AFLR3 GG : Nodes, Elements   =     59279    329079
AFLR3 GG : Nodes, Elements   =     60784    333605
AFLR3 GG : Nodes, Elements   =     60784    339419
AFLR3 GG : Nodes, Elements   =     60784    337937
AFLR3 GG : Nodes, Elements   =     62170    342102
AFLR3 GG : Nodes, Elements   =     62170    347580
AFLR3 GG : Nodes, Elements   =     62170    346147
AFLR3 GG : Nodes, Elements   =     63504    350156
AFLR3 GG : Nodes, Elements   =     63504    355349
AFLR3 GG : Nodes, Elements   =     63504    354090
AFLR3 GG : Nodes, Elements   =     64737    357794
AFLR3 GG : Nodes, Elements   =     64737    362614
AFLR3 GG : Nodes, Elements   =     64737    361426
AFLR3 GG : Nodes, Elements   =     65857    364795
AFLR3 GG : Nodes, Elements   =     65857    369203
AFLR3 GG : Nodes, Elements   =     65857    368093
AFLR3 GG : Nodes, Elements   =     66873    371147
AFLR3 GG : Nodes, Elements   =     66873    375105
AFLR3 GG : Nodes, Elements   =     66873    374112
AFLR3 GG : Nodes, Elements   =     67797    376889
AFLR3 GG : Nodes, Elements   =     67797    380498
AFLR3 GG : Nodes, Elements   =     67797    379624
AFLR3 GG : Nodes, Elements   =     68597    382025
AFLR3 GG : Nodes, Elements   =     68597    385186
AFLR3 GG : Nodes, Elements   =     68597    384331
AFLR3 GG : Nodes, Elements   =     69317    386493
AFLR3 GG : Nodes, Elements   =     69317    389307
AFLR3 GG : Nodes, Elements   =     69317    388598
AFLR3 GG : Nodes, Elements   =     69895    390335
AFLR3 GG : Nodes, Elements   =     69895    392606
AFLR3 GG : Nodes, Elements   =     69895    392001
AFLR3 GG : Nodes, Elements   =     70383    393465
AFLR3 GG : Nodes, Elements   =     70383    395436
AFLR3 GG : Nodes, Elements   =     70383    394902
AFLR3 GG : Nodes, Elements   =     70736    395962
AFLR3 GG : Nodes, Elements   =     70736    397400
AFLR3 GG : Nodes, Elements   =     70736    396998
AFLR3 GG : Nodes, Elements   =     70989    397758
AFLR3 GG : Nodes, Elements   =     70989    398775
AFLR3 GG : Nodes, Elements   =     70989    398490
AFLR3 GG : Nodes, Elements   =     71138    398937
AFLR3 GG : Nodes, Elements   =     71138    399558
AFLR3 GG : Nodes, Elements   =     71138    399361
AFLR3 GG : Nodes, Elements   =     71220    399607
AFLR3 GG : Nodes, Elements   =     71220    399968
AFLR3 GG : Nodes, Elements   =     71220    399831
AFLR3 GG : Nodes, Elements   =     71262    399957
AFLR3 GG : Nodes, Elements   =     71262    400154
AFLR3 GG : Nodes, Elements   =     71262    400076
AFLR3 GG : Nodes, Elements   =     71279    400127
AFLR3 GG : Nodes, Elements   =     71279    400221
AFLR3 GG : Nodes, Elements   =     71279    400173
AFLR3 GG : Nodes, Elements   =     71289    400203
AFLR3 GG : Nodes, Elements   =     71289    400245
AFLR3 GG : Nodes, Elements   =     71289    400227
AFLR3 GG : Nodes, Elements   =     71291    400233
AFLR3 GG : Nodes, Elements   =     71291    400239
AFLR3 GG : Nodes, Elements   =     71291    400238
AFLR3 GG : Nodes, Elements   =     71298    400259
AFLR3 GG : Nodes, Elements   =     71298    400281
AFLR3 GG : Nodes, Elements   =     71298    400277
AFLR3 GG : Nodes, Elements   =     71299    400280
AFLR3 GG : Nodes, Elements   =     71299    400284
AFLR3 GG : Nodes, Elements   =     71299    400282
 
AFLR3    : CPU Time          =     1.601   seconds
 
AFLR3 QI : QUALITY IMPROVEMENT
 
AFLR3 QI : Nodes, Elements   =     71299    400282
AFLR3 QI : Nodes, Elements   =     70927    398220
AFLR3 QI : Nodes, Elements   =     70888    397997
AFLR3 QI : Nodes, Elements   =     70881    397960
AFLR3 QI : Nodes, Elements   =     70881    400024
AFLR3 QI : Nodes, Elements   =     70881    397740
AFLR3 QI : Nodes, Elements   =     70881    396743
AFLR3 QI : Nodes, Elements   =     70881    397455
AFLR3 QI : Nodes, Elements   =     70881    396626
AFLR3 QI : Nodes, Elements   =     70881    396480
AFLR3 QI : Nodes, Elements   =     70881    397096
AFLR3 QI : Nodes, Elements   =     70881    396492
AFLR3 QI : Nodes, Elements   =     70881    396420
AFLR3 QI : Nodes, Elements   =     70881    397002
AFLR3 QI : Nodes, Elements   =     70881    396451
AFLR3 QI : Nodes, Elements   =     70881    396396
AFLR3 QI : Nodes, Elements   =     70881    396956
AFLR3 QI : Nodes, Elements   =     70881    396418
AFLR3 QI : Nodes, Elements   =     70881    396375
AFLR3 QI : Nodes, Elements   =     70881    396368
 
AFLR3    : CPU Time          =     0.466   seconds
 
AFLR3    : DONE
 
ANBL3 BLM: BL VOLUME GRID MERGE
 
ANBL3 BLM: Nodes, Elements   =     70881    396368
 
UG3      : OUTPUT GRID
 
UG3      : Grid File Name    = .tmp.b8.ugrid
UG3      : Quad Surface Faces=         0
UG3      : Tria Surface Faces=     15726
UG3      : Nodes             =    149142
UG3      : Total Elements    =    552989
UG3      : Hex Elements      =         0
UG3      : Pent_5 Elements   =       147
UG3      : Pent_6 Elements   =    156367
UG3      : Tet Elements      =    396475
 
ANBL3 BLM: Nodes, Elements   =    149142    865870
ANBL3 BLM: Nodes, Elements   =    149142       107
 
ANBL3    : CPU Time          =     0.082   seconds
 
ANBL3    : DONE

OVERALL  : CPU Time          =     4.011   seconds

UG3      : DIHEDRAL ANGLE CHECK

UG3      : No. Tet Elems     =    396475
UG3      : Min, Max Ang      =     1.996     172.9
UG3      : Average Angle     =      70.2
UG3      : No. Angle&gt;160.0   =        13
UG3      : No. Angle&gt;179.9   =         0

UG3      : No. Pyramid Elems =       147
UG3      : Min, Max Ang      =     8.861     172.3
UG3      : Average Angle     =      80.9
UG3      : No. Angle&gt;160.0   =        12
UG3      : No. Angle&gt;179.9   =         0

UG3      : No. Prism Elems   =    156367
UG3      : Min, Max Ang      =     9.482     174.2
UG3      : Average Angle     =        80
UG3      : No. Angle&gt;160.0   =       421
UG3      : No. Angle&gt;179.9   =         0

UG3      : VOL CHECK

UG3      : Total-Volume      =  5.96e+10

UG3      : No. Tet Elems     =    396475
UG3      : Min Vol           =   0.00131
UG3      : Average Vol       =   1.5e+05
UG3      : Total-Tet-Vol     =  5.96e+10
UG3      : No. Vol&lt;TOL       =         0

UG3      : No. Pyramid Elems =       147
UG3      : Min Vol           =   0.00545
UG3      : Average Vol       =     0.074
UG3      : Total-Pyramid-Vol =      10.9
UG3      : No. Vol&lt;TOL       =         0

UG3      : No. Prism Elems   =    156367
UG3      : Min Vol           =    0.0139
UG3      : Average Vol       =     0.165
UG3      : Total-Prism-Vol   =  2.58e+04
UG3      : No. Vol&lt;TOL       =         0

UG3      : Q VOL-LENGTH-RATIO CHECK
                      2/3        2
UG3      : Q = c * Vol   / sum( L  )
UG3      : 0 &lt;= Q &lt;= 1
UG3      : Note that L includes scaling for BL-aspect=ratio

UG3      : No. Tet Elems     =    396475
UG3      : Min, Max Q        =     0.137         1
UG3      : Average Q         =     0.856
UG3      : No. Q&lt;       0.1  =         0
UG3      : No. Q&lt;      0.01  =         0

UG3      : No. Pyramid Elems =       147
UG3      : Min, Max Q        =     0.259         1
UG3      : Average Q         =     0.754
UG3      : No. Q&lt;       0.1  =         0
UG3      : No. Q&lt;      0.01  =         0

UG3      : No. Prism Elems   =    156367
UG3      : Min, Max Q        =     0.353         1
UG3      : Average Q         =     0.907
UG3      : No. Q&lt;       0.1  =         0
UG3      : No. Q&lt;      0.01  =         0

UG3      : CPU Time          =     0.000   seconds

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.8.1
EGADS    : ---------------------------------------

EGADS    : CREATE EGADS TESS FROM AFLR3 DATA

EGADS    : CREATING TESSELLATION FOR BODY 0 EDGE 1
EGADS    : CREATING TESSELLATION FOR BODY 0 EDGE 2
EGADS    : CREATING TESSELLATION FOR BODY 0 EDGE 3
EGADS    : CREATING TESSELLATION FOR BODY 0 EDGE 4
EGADS    : CREATING TESSELLATION FOR BODY 0 EDGE 5
EGADS    : CREATING TESSELLATION FOR BODY 0 EDGE 6
EGADS    : CREATING TESSELLATION FOR BODY 0 EDGE 7
EGADS    : CREATING TESSELLATION FOR BODY 0 EDGE 8
EGADS    : CREATING TESSELLATION FOR BODY 0 EDGE 9
EGADS    : CREATING TESSELLATION FOR BODY 0 EDGE 10
EGADS    : CREATING TESSELLATION FOR BODY 0 EDGE 11
EGADS    : CREATING TESSELLATION FOR BODY 0 EDGE 12
EGADS    : CREATING TESSELLATION FOR BODY 0 EDGE 13
EGADS    : CREATING TESSELLATION FOR BODY 0 EDGE 14
EGADS    : CREATING TESSELLATION FOR BODY 0 EDGE 15
EGADS    : CREATING TESSELLATION FOR BODY 0 EDGE 16
EGADS    : CREATING TESSELLATION FOR BODY 0 EDGE 17
EGADS    : CREATING TESSELLATION FOR BODY 0 EDGE 18

EGADS    : CREATING TESSELLATION FOR BODY 0 FACE 1
EGADS    : CREATING TESSELLATION FOR BODY 0 FACE 2
EGADS    : CREATING TESSELLATION FOR BODY 0 FACE 3
EGADS    : CREATING TESSELLATION FOR BODY 0 FACE 4
EGADS    : CREATING TESSELLATION FOR BODY 0 FACE 5
EGADS    : CREATING TESSELLATION FOR BODY 0 FACE 6
EGADS    : CREATING TESSELLATION FOR BODY 0 FACE 7
EGADS    : CREATING TESSELLATION FOR BODY 0 FACE 8
EGADS    : CREATING TESSELLATION FOR BODY 0 FACE 9
EGADS    : CREATING TESSELLATION FOR BODY 0 FACE 10

EGADS    : CREATING TESSELLATION FOR BODY 1 EDGE 19
EGADS    : CREATING TESSELLATION FOR BODY 1 EDGE 20
EGADS    : CREATING TESSELLATION FOR BODY 1 EDGE 21
EGADS    : CREATING TESSELLATION FOR BODY 1 EDGE 22
EGADS    : CREATING TESSELLATION FOR BODY 1 EDGE 23
EGADS    : CREATING TESSELLATION FOR BODY 1 EDGE 24
EGADS    : CREATING TESSELLATION FOR BODY 1 EDGE 25
EGADS    : CREATING TESSELLATION FOR BODY 1 EDGE 26
EGADS    : CREATING TESSELLATION FOR BODY 1 EDGE 27
EGADS    : CREATING TESSELLATION FOR BODY 1 EDGE 28
EGADS    : CREATING TESSELLATION FOR BODY 1 EDGE 29
EGADS    : CREATING TESSELLATION FOR BODY 1 EDGE 30

EGADS    : CREATING TESSELLATION FOR BODY 1 FACE 11
EGADS    : CREATING TESSELLATION FOR BODY 1 FACE 12
EGADS    : CREATING TESSELLATION FOR BODY 1 FACE 13
EGADS    : CREATING TESSELLATION FOR BODY 1 FACE 14
EGADS    : CREATING TESSELLATION FOR BODY 1 FACE 15
EGADS    : CREATING TESSELLATION FOR BODY 1 FACE 16

EGADS    : EGADS TESS CREATED

EGADS    : CHECK TESS FACE NODE MAP

EGADS    : CHECKING NODE MAP FOR BODY 0 FACE 1
EGADS    : CHECKING NODE MAP FOR BODY 0 FACE 2
EGADS    : CHECKING NODE MAP FOR BODY 0 FACE 3
EGADS    : CHECKING NODE MAP FOR BODY 0 FACE 4
EGADS    : CHECKING NODE MAP FOR BODY 0 FACE 5
EGADS    : CHECKING NODE MAP FOR BODY 0 FACE 6
EGADS    : CHECKING NODE MAP FOR BODY 0 FACE 7
EGADS    : CHECKING NODE MAP FOR BODY 0 FACE 8
EGADS    : CHECKING NODE MAP FOR BODY 0 FACE 9
EGADS    : CHECKING NODE MAP FOR BODY 0 FACE 10
EGADS    : CHECKING NODE MAP FOR BODY 1 FACE 11
EGADS    : CHECKING NODE MAP FOR BODY 1 FACE 12
EGADS    : CHECKING NODE MAP FOR BODY 1 FACE 13
EGADS    : CHECKING NODE MAP FOR BODY 1 FACE 14
EGADS    : CHECKING NODE MAP FOR BODY 1 FACE 15
EGADS    : CHECKING NODE MAP FOR BODY 1 FACE 16
Volume mesh:
	Number of nodes          = 149142
	Number of elements       = 568715
	Number of triangles      = 15726
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 396475
	Number of pyramids       = 147
	Number of prisms         = 156367
	Number of hexahedrals    = 0

Writing vtk file ....

Writing vtk general file ....
Finished writing vtk file


real	0m5.788s
user	0m5.361s
sys	0m0.726s
+ status=0
+ set +x

=================================================
data/session07/10_aflr4_aflr3_ViscousWing.py passed (as expected)
=================================================


=================================================
11_aflr4_aflr3_ViscousWingPod.py test;
+ python 11_aflr4_aflr3_ViscousWingPod.py
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/CAPS/training/2023/training.log

MESSAGE:: Building wingOml


MESSAGE:: Building nacelleOml

Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 3
	Name = Nacelle, index = 1
	Name = Wing, index = 2
	Name = Farfield, index = 3
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 4
	Name = Nacelle, index = 1
	Name = leftWing, index = 2
	Name = riteWing, index = 3
	Name = Farfield, index = 4

Getting mesh sizing parameters
	Mesh sizing name - Farfield
	Done getting mesh sizing parameters
 
AFLR2    : ---------------------------------------
AFLR2    : AFLR2 LIBRARY
AFLR2    : ADVANCING-FRONT/LOCAL-RECONNECTION
AFLR2    : TRIA/QUAD GRID GENERATOR
AFLR2    : Version Number 9.18.1
AFLR2    : Version Date   06/11/24 @ 05:52PM
AFLR2    : Compile OS     Darwin 23.5.0 arm64
AFLR2    : Compile Date   06/11/24 @ 05:52PM
AFLR2    : Copyright 1994-2021, D.L. Marcum
AFLR2    : ---------------------------------------
 
AFLR4    : ---------------------------------------
AFLR4    : AFLR4 LIBRARY
AFLR4    : ADVANCING-FRONT/LOCAL-RECONNECTION
AFLR4    : TRIA/QUAD SURFACE GRID GENERATOR
AFLR4    : Version Number 11.5.15
AFLR4    : Version Date   07/19/24 @ 07:04PM
AFLR4    : Compile OS     Darwin 23.5.0 arm64
AFLR4    : Compile Date   07/19/24 @ 07:06PM
AFLR4    : Copyright 1994-2021, D.L. Marcum
AFLR4    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.8.1
EGADS    : ---------------------------------------

EGADS    : EGADS CAD Geometry Setup

EGADS    : Model has 4 Active Bodies

EGADS    : Body 0 is a SolidBody
EGADS    : Body 0 has 1 Shells
EGADS    : Body 0 has 4 Faces
EGADS    : Body 0 has 8 Edges
EGADS    : Body 0 has 4 Loops
EGADS    : Body 0 has 4 Nodes
EGADS    : Body 1 is a SolidBody
EGADS    : Body 1 has 1 Shells
EGADS    : Body 1 has 4 Faces
EGADS    : Body 1 has 8 Edges
EGADS    : Body 1 has 4 Loops
EGADS    : Body 1 has 4 Nodes
EGADS    : Body 2 is a SolidBody
EGADS    : Body 2 has 1 Shells
EGADS    : Body 2 has 10 Faces
EGADS    : Body 2 has 18 Edges
EGADS    : Body 2 has 10 Loops
EGADS    : Body 2 has 10 Nodes
EGADS    : Body 3 is a SolidBody
EGADS    : Body 3 has 1 Shells
EGADS    : Body 3 has 6 Faces
EGADS    : Body 3 has 12 Edges
EGADS    : Body 3 has 6 Loops
EGADS    : Body 3 has 8 Nodes

EGADS    : Check Grid BCs

EGADS    : Grid BCs are OK

EGADS    : Face Neighbor-Faces Information

EGADS    : QC  = Face Quad Combination Flag
EGADS    : IER = Face Isolated Edge Refinement Flag
EGADS    : ER  = Face Edge Refinement Factor
EGADS    :       Not applicable for Faces with a FarField Grid BC.
EGADS    : SF  = Face Scale Factor
EGADS    :       Not applicable for Faces with a FarField Grid BC.

EGADS    :   Face          Body    QC   IER       ER    Scale   Neighbor
EGADS    :     ID  Active    ID  Flag  Flag   Weight   Factor   Faces
EGADS    :      1     Yes     0     0     1        0        1   2 3
EGADS    :      2     Yes     0     0     1        0        1   1 4
EGADS    :      3     Yes     0     0     1        0        1   1 4
EGADS    :      4     Yes     0     0     1        0        1   2 3
EGADS    :      5     Yes     1     0     1        0        1   6 7
EGADS    :      6     Yes     1     0     1        0        1   5 8
EGADS    :      7     Yes     1     0     1        0        1   5 8
EGADS    :      8     Yes     1     0     1        0        1   6 7
EGADS    :      9     Yes     2     0     1        0        1   10 11 14
EGADS    :     10     Yes     2     0     1        0        1   9 12 13
EGADS    :     11     Yes     2     0     1        0        1   9 12 16
EGADS    :     12     Yes     2     0     1        0        1   10 11 13
EGADS    :     13     Yes     2     0     1        0        1   10 12
EGADS    :     14     Yes     2     0     1        0        1   9 15 16
EGADS    :     15     Yes     2     0     1        0        1   14 17 18
EGADS    :     16     Yes     2     0     1        0        1   11 14 17
EGADS    :     17     Yes     2     0     1        0        1   15 16 18
EGADS    :     18     Yes     2     0     1        0        1   15 17
EGADS    :     19     Yes     3     0     1       NA       NA   21 22 23 24
EGADS    :     20     Yes     3     0     1       NA       NA   21 22 23 24
EGADS    :     21     Yes     3     0     1       NA       NA   19 20 23 24
EGADS    :     22     Yes     3     0     1       NA       NA   19 20 23 24
EGADS    :     23     Yes     3     0     1       NA       NA   19 20 21 22
EGADS    :     24     Yes     3     0     1       NA       NA   19 20 21 22

EGADS    : Face Edges Information

EGADS    :   Face   Edges
EGADS    :      1   -1 3 2 -4
EGADS    :      2   -2 5 1 -6
EGADS    :      3   7 4 -8 -3
EGADS    :      4   8 6 -7 -5
EGADS    :      5   9 12 -10 -11
EGADS    :      6   10 14 -9 -13
EGADS    :      7   -15 11 16 -12
EGADS    :      8   -16 13 15 -14
EGADS    :      9   -17 18 19 -20
EGADS    :     10   -21 20 22 -23
EGADS    :     11   -19 24 17 -25
EGADS    :     12   -22 25 21 -26
EGADS    :     13   23 26
EGADS    :     14   27 29 -28 -18
EGADS    :     15   30 32 -31 -29
EGADS    :     16   28 33 -27 -24
EGADS    :     17   31 34 -30 -33
EGADS    :     18   -32 -34
EGADS    :     19   35 36 -37 -38
EGADS    :     20   -39 42 41 -40
EGADS    :     21   43 39 -44 -35
EGADS    :     22   -45 37 46 -41
EGADS    :     23   38 45 -42 -43
EGADS    :     24   -36 44 40 -46

EGADS    : Face Loops Information

EGADS    :   Face   Loops
EGADS    :      1   1
EGADS    :      2   2
EGADS    :      3   3
EGADS    :      4   4
EGADS    :      5   5
EGADS    :      6   6
EGADS    :      7   7
EGADS    :      8   8
EGADS    :      9   9
EGADS    :     10   10
EGADS    :     11   11
EGADS    :     12   12
EGADS    :     13   13
EGADS    :     14   14
EGADS    :     15   15
EGADS    :     16   16
EGADS    :     17   17
EGADS    :     18   18
EGADS    :     19   19
EGADS    :     20   20
EGADS    :     21   21
EGADS    :     22   22
EGADS    :     23   23
EGADS    :     24   24

EGADS    : Loop Edges Information

EGADS    :   Loop  Active   Edges
EGADS    :      1     Yes   -1 3 2 -4
EGADS    :      2     Yes   -2 5 1 -6
EGADS    :      3     Yes   7 4 -8 -3
EGADS    :      4     Yes   8 6 -7 -5
EGADS    :      5     Yes   9 12 -10 -11
EGADS    :      6     Yes   10 14 -9 -13
EGADS    :      7     Yes   -15 11 16 -12
EGADS    :      8     Yes   -16 13 15 -14
EGADS    :      9     Yes   -17 18 19 -20
EGADS    :     10     Yes   -21 20 22 -23
EGADS    :     11     Yes   -19 24 17 -25
EGADS    :     12     Yes   -22 25 21 -26
EGADS    :     13     Yes   23 26
EGADS    :     14     Yes   27 29 -28 -18
EGADS    :     15     Yes   30 32 -31 -29
EGADS    :     16     Yes   28 33 -27 -24
EGADS    :     17     Yes   31 34 -30 -33
EGADS    :     18     Yes   -32 -34
EGADS    :     19     Yes   35 36 -37 -38
EGADS    :     20     Yes   -39 42 41 -40
EGADS    :     21     Yes   43 39 -44 -35
EGADS    :     22     Yes   -45 37 46 -41
EGADS    :     23     Yes   38 45 -42 -43
EGADS    :     24     Yes   -36 44 40 -46

EGADS    : Edge Node, Scale Factor, and Neighbor-Faces Information

EGADS    : ESF = Edge Scale Factor
EGADS    :       Not applicable for DEGENERATE Edges or Edges with a FarField
EGADS    :       Grid BC Neighbor Face.

EGADS    :                                             Neighbor
EGADS    :   Edge  Body  Active Node1 Node2      ESF   Faces
EGADS    :      1     0     Yes     1     2        1   1 2
EGADS    :      2     0     Yes     3     4        1   1 2
EGADS    :      3     0     Yes     1     3        1   1 3
EGADS    :      4     0     Yes     2     4        1   1 3
EGADS    :      5     0     Yes     3     1        1   2 4
EGADS    :      6     0     Yes     4     2        1   2 4
EGADS    :      7     0     Yes     1     2        1   3 4
EGADS    :      8     0     Yes     3     4        1   3 4
EGADS    :      9     1     Yes     5     6        1   5 6
EGADS    :     10     1     Yes     7     8        1   5 6
EGADS    :     11     1     Yes     5     7        1   5 7
EGADS    :     12     1     Yes     6     8        1   5 7
EGADS    :     13     1     Yes     7     5        1   6 8
EGADS    :     14     1     Yes     8     6        1   6 8
EGADS    :     15     1     Yes     5     6        1   7 8
EGADS    :     16     1     Yes     7     8        1   7 8
EGADS    :     17     2     Yes     9    10        1   9 11
EGADS    :     18     2     Yes     9    11        1   9 14
EGADS    :     19     2     Yes    11    12        1   9 11
EGADS    :     20     2     Yes    10    12        1   9 10
EGADS    :     21     2     Yes    10    13        1   10 12
EGADS    :     22     2     Yes    12    14        1   10 12
EGADS    :     23     2     Yes    13    14        1   10 13
EGADS    :     24     2     Yes    11     9        1   11 16
EGADS    :     25     2     Yes    12    10        1   11 12
EGADS    :     26     2     Yes    14    13        1   12 13
EGADS    :     27     2     Yes     9    15        1   14 16
EGADS    :     28     2     Yes    11    16        1   14 16
EGADS    :     29     2     Yes    15    16        1   14 15
EGADS    :     30     2     Yes    15    17        1   15 17
EGADS    :     31     2     Yes    16    18        1   15 17
EGADS    :     32     2     Yes    17    18        1   15 18
EGADS    :     33     2     Yes    16    15        1   16 17
EGADS    :     34     2     Yes    18    17        1   17 18
EGADS    :     35     3     Yes    20    19       NA   19 21
EGADS    :     36     3     Yes    19    21       NA   19 24
EGADS    :     37     3     Yes    22    21       NA   19 22
EGADS    :     38     3     Yes    20    22       NA   19 23
EGADS    :     39     3     Yes    24    23       NA   20 21
EGADS    :     40     3     Yes    23    25       NA   20 24
EGADS    :     41     3     Yes    26    25       NA   20 22
EGADS    :     42     3     Yes    24    26       NA   20 23
EGADS    :     43     3     Yes    20    24       NA   21 23
EGADS    :     44     3     Yes    19    23       NA   21 24
EGADS    :     45     3     Yes    22    26       NA   22 23
EGADS    :     46     3     Yes    21    25       NA   22 24

EGADS    : Node Information

EGADS    :   Node  Active      Coordinates
EGADS    :      1     Yes       90.5173952                0                0
EGADS    :      2     Yes       90.5173952                0                0
EGADS    :      3     Yes       60.5173952                0                0
EGADS    :      4     Yes       60.5173952                0                0
EGADS    :      5     Yes       90.5173952       29.3018771                0
EGADS    :      6     Yes       90.5173952       29.3018771                0
EGADS    :      7     Yes       60.5173952       29.3018771                0
EGADS    :      8     Yes       60.5173952       29.3018771                0
EGADS    :      9     Yes       97.2007855                0                0
EGADS    :     10     Yes       97.9335611                0                0
EGADS    :     11     Yes               50                0                0
EGADS    :     12     Yes       75.3047874                0                0
EGADS    :     13     Yes       123.552357                0        4.7180639
EGADS    :     14     Yes       118.391317                0       3.99272703
EGADS    :     15     Yes       97.9335611       36.1389817                0
EGADS    :     16     Yes       75.3047874       36.1389817                0
EGADS    :     17     Yes       123.552357       97.6729236        4.7180639
EGADS    :     18     Yes       118.391317       97.6729236       3.99272703
EGADS    :     19     Yes                0                0       1947.05079
EGADS    :     20     Yes                0                0                0
EGADS    :     21     Yes                0       1953.45847       1947.05079
EGADS    :     22     Yes                0       1953.45847                0
EGADS    :     23     Yes       2040.21562                0       1947.05079
EGADS    :     24     Yes       2040.21562                0                0
EGADS    :     25     Yes       2040.21562       1953.45847       1947.05079
EGADS    :     26     Yes       2040.21562       1953.45847                0

EGADS    : Face and Edge Match Information

EGADS    : No Face Matches Found

AFLR4    : Surface Mesh Spacing Setup

AFLR4    : Max Bounding Box Length     = 3906.92
AFLR4    : Min Bounding Box Length     = 3906.92
AFLR4    : Max Ref Bounding Box Length = 195.346
AFLR4    : Min Ref Bounding Box Length = 22.2515
AFLR4    : Reference Length            = 21.7051
AFLR4    : BL Thickness                = 0
AFLR4    : FarField Spacing            = 5303.02
AFLR4    : Abs Min Surf Spacing        = 0.0542627
AFLR4    : Min Surf Spacing            = 0.108525
AFLR4    : Max Surf Spacing            = 2.17051
AFLR4    : Global Scale Factor         = 10

AFLR4    : Geometry Definition Information

AFLR4    : Definition              Definition   Composite             Grid BC
AFLR4    :         ID                    Type          ID                Type
AFLR4    :          0     glue-only composite           -                   -
AFLR4    :          1            CAD geometry           0            STD w/BL
AFLR4    :          2            CAD geometry           0            STD w/BL
AFLR4    :          3            CAD geometry           0            STD w/BL
AFLR4    :          4            CAD geometry           0            STD w/BL
AFLR4    :          5            CAD geometry           0            STD w/BL
AFLR4    :          6            CAD geometry           0            STD w/BL
AFLR4    :          7            CAD geometry           0            STD w/BL
AFLR4    :          8            CAD geometry           0            STD w/BL
AFLR4    :          9            CAD geometry           0            STD w/BL
AFLR4    :         10            CAD geometry           0            STD w/BL
AFLR4    :         11            CAD geometry           0            STD w/BL
AFLR4    :         12            CAD geometry           0            STD w/BL
AFLR4    :         13            CAD geometry           0            STD w/BL
AFLR4    :         14            CAD geometry           0            STD w/BL
AFLR4    :         15            CAD geometry           0            STD w/BL
AFLR4    :         16            CAD geometry           0            STD w/BL
AFLR4    :         17            CAD geometry           0            STD w/BL
AFLR4    :         18            CAD geometry           0            STD w/BL
AFLR4    :         19            CAD geometry           0            FARFIELD
AFLR4    :         20            CAD geometry           0            FARFIELD
AFLR4    :         21            CAD geometry           0            FARFIELD
AFLR4    :         22            CAD geometry           0            FARFIELD
AFLR4    :         23            CAD geometry           0            FARFIELD
AFLR4    :         24            CAD geometry           0            FARFIELD

AFLR4    : Case has 2 Proximity Checking Components

AFLR4    : Component 1 includes Definitions 9 10 11 12 13 14 15 16 17 18
AFLR4    : Component 2 includes Definitions 1 2 3 4 5 6 7 8

AFLR4    : Define CAD surface definition 1
AFLR4    : Define CAD surface definition 2
AFLR4    : Define CAD surface definition 3
AFLR4    : Define CAD surface definition 4
AFLR4    : Define CAD surface definition 5
AFLR4    : Define CAD surface definition 6
AFLR4    : Define CAD surface definition 7
AFLR4    : Define CAD surface definition 8
AFLR4    : Define CAD surface definition 9
AFLR4    : Define CAD surface definition 10
AFLR4    : Define CAD surface definition 11
AFLR4    : Define CAD surface definition 12
AFLR4    : Define CAD surface definition 13
AFLR4    : Define CAD surface definition 14
AFLR4    : Define CAD surface definition 15
AFLR4    : Define CAD surface definition 16
AFLR4    : Define CAD surface definition 17
AFLR4    : Define CAD surface definition 18
AFLR4    : Define CAD surface definition 19
AFLR4    : Define CAD surface definition 20
AFLR4    : Define CAD surface definition 21
AFLR4    : Define CAD surface definition 22
AFLR4    : Define CAD surface definition 23
AFLR4    : Define CAD surface definition 24

AFLR4    : Surface Grid Generation

AFLR4    : Generate optimal mesh on surface definition 1
AFLR2    : Nodes, Trias,Quads=       146       247         0
AFLR4    : Nodes, Trias,Quads=       151       257         0

AFLR4    : Generate optimal mesh on surface definition 2
AFLR2    : Nodes, Trias,Quads=       129       213         0
AFLR4    : Nodes, Trias,Quads=       115       185         0

AFLR4    : Generate optimal mesh on surface definition 3
AFLR2    : Nodes, Trias,Quads=       146       247         0
AFLR4    : Nodes, Trias,Quads=       150       255         0

AFLR4    : Generate optimal mesh on surface definition 4
AFLR2    : Nodes, Trias,Quads=       129       213         0
AFLR4    : Nodes, Trias,Quads=       116       187         0

AFLR4    : Generate optimal mesh on surface definition 5
AFLR2    : Nodes, Trias,Quads=       146       247         0
AFLR4    : Nodes, Trias,Quads=       150       255         0

AFLR4    : Generate optimal mesh on surface definition 6
AFLR2    : Nodes, Trias,Quads=       129       213         0
AFLR4    : Nodes, Trias,Quads=       116       187         0

AFLR4    : Generate optimal mesh on surface definition 7
AFLR2    : Nodes, Trias,Quads=       146       247         0
AFLR4    : Nodes, Trias,Quads=       151       257         0

AFLR4    : Generate optimal mesh on surface definition 8
AFLR2    : Nodes, Trias,Quads=       129       213         0
AFLR4    : Nodes, Trias,Quads=       115       185         0

AFLR4    : Generate optimal mesh on surface definition 9
AFLR2    : Nodes, Trias,Quads=       427       774         0
AFLR4    : Nodes, Trias,Quads=       333       586         0

AFLR4    : Generate optimal mesh on surface definition 10
AFLR2    : Nodes, Trias,Quads=       610      1113         0
AFLR4    : Nodes, Trias,Quads=       325       543         0

AFLR4    : Generate optimal mesh on surface definition 11
AFLR2    : Nodes, Trias,Quads=       457       833         0
AFLR4    : Nodes, Trias,Quads=       324       567         0

AFLR4    : Generate optimal mesh on surface definition 12
AFLR2    : Nodes, Trias,Quads=       586      1065         0
AFLR4    : Nodes, Trias,Quads=       313       519         0

AFLR4    : Generate optimal mesh on surface definition 13
AFLR2    : Nodes, Trias,Quads=        11        12         0
AFLR4    : Nodes, Trias,Quads=         8         6         0

AFLR4    : Generate optimal mesh on surface definition 14
AFLR2    : Nodes, Trias,Quads=       428       776         0
AFLR4    : Nodes, Trias,Quads=       336       592         0

AFLR4    : Generate optimal mesh on surface definition 15
AFLR2    : Nodes, Trias,Quads=       616      1125         0
AFLR4    : Nodes, Trias,Quads=       323       539         0

AFLR4    : Generate optimal mesh on surface definition 16
AFLR2    : Nodes, Trias,Quads=       456       831         0
AFLR4    : Nodes, Trias,Quads=       332       583         0

AFLR4    : Generate optimal mesh on surface definition 17
AFLR2    : Nodes, Trias,Quads=       585      1063         0
AFLR4    : Nodes, Trias,Quads=       314       521         0

AFLR4    : Generate optimal mesh on surface definition 18
AFLR2    : Nodes, Trias,Quads=        11        12         0
AFLR4    : Nodes, Trias,Quads=         8         6         0

AFLR4    : Generate optimal mesh on surface definition 19
AFLR2    : Nodes, Trias,Quads=         5         4         0
AFLR4    : Nodes, Trias,Quads=         4         2         0

AFLR4    : Generate optimal mesh on surface definition 20
AFLR2    : Nodes, Trias,Quads=         5         4         0
AFLR4    : Nodes, Trias,Quads=         4         2         0

AFLR4    : Generate optimal mesh on surface definition 21
AFLR2    : Nodes, Trias,Quads=         5         4         0
AFLR4    : Nodes, Trias,Quads=         4         2         0

AFLR4    : Generate optimal mesh on surface definition 22
AFLR2    : Nodes, Trias,Quads=         5         4         0
AFLR4    : Nodes, Trias,Quads=         4         2         0

AFLR4    : Generate optimal mesh on surface definition 23
AFLR2    : Nodes, Trias,Quads=         5         4         0
AFLR4    : Nodes, Trias,Quads=         4         2         0

AFLR4    : Generate optimal mesh on surface definition 24
AFLR2    : Nodes, Trias,Quads=         5         4         0
AFLR4    : Nodes, Trias,Quads=         4         2         0

DGEOM    : Add surface definitions to composite definition 0
DGEOM    : Glue composite surface definition 0
DGEOM    : Nodes,Faces,BEdges=      3125      6242      1118

AFLR4    : Curvature BG Surface Grid Generation

AFLR4    : Nodes, Faces      =      3125      6242

AFLR4    : Surface Grid Generation

AFLR4    : Generate optimal mesh on surface definition 1
AFLR2    : Nodes, Trias,Quads=       220       383         0
AFLR4    : Nodes, Trias,Quads=       219       381         0

AFLR4    : Generate optimal mesh on surface definition 2
AFLR2    : Nodes, Trias,Quads=       204       351         0
AFLR4    : Nodes, Trias,Quads=       177       297         0

AFLR4    : Generate optimal mesh on surface definition 3
AFLR2    : Nodes, Trias,Quads=       224       391         0
AFLR4    : Nodes, Trias,Quads=       219       381         0

AFLR4    : Generate optimal mesh on surface definition 4
AFLR2    : Nodes, Trias,Quads=       205       353         0
AFLR4    : Nodes, Trias,Quads=       178       299         0

AFLR4    : Generate optimal mesh on surface definition 5
AFLR2    : Nodes, Trias,Quads=       224       391         0
AFLR4    : Nodes, Trias,Quads=       219       381         0

AFLR4    : Generate optimal mesh on surface definition 6
AFLR2    : Nodes, Trias,Quads=       205       353         0
AFLR4    : Nodes, Trias,Quads=       178       299         0

AFLR4    : Generate optimal mesh on surface definition 7
AFLR2    : Nodes, Trias,Quads=       220       383         0
AFLR4    : Nodes, Trias,Quads=       219       381         0

AFLR4    : Generate optimal mesh on surface definition 8
AFLR2    : Nodes, Trias,Quads=       204       351         0
AFLR4    : Nodes, Trias,Quads=       177       297         0

AFLR4    : Generate optimal mesh on surface definition 9
AFLR2    : Nodes, Trias,Quads=       504       921         0
AFLR4    : Nodes, Trias,Quads=       447       807         0

AFLR4    : Generate optimal mesh on surface definition 10
AFLR2    : Nodes, Trias,Quads=       638      1166         0
AFLR4    : Nodes, Trias,Quads=       470       830         0

AFLR4    : Generate optimal mesh on surface definition 11
AFLR2    : Nodes, Trias,Quads=       522       956         0
AFLR4    : Nodes, Trias,Quads=       452       816         0

AFLR4    : Generate optimal mesh on surface definition 12
AFLR2    : Nodes, Trias,Quads=       609      1109         0
AFLR4    : Nodes, Trias,Quads=       463       817         0

AFLR4    : Generate optimal mesh on surface definition 13
AFLR2    : Nodes, Trias,Quads=        11        12         0
AFLR4    : Nodes, Trias,Quads=         8         6         0

AFLR4    : Generate optimal mesh on surface definition 14
AFLR2    : Nodes, Trias,Quads=       500       913         0
AFLR4    : Nodes, Trias,Quads=       451       815         0

AFLR4    : Generate optimal mesh on surface definition 15
AFLR2    : Nodes, Trias,Quads=       637      1164         0
AFLR4    : Nodes, Trias,Quads=       481       852         0

AFLR4    : Generate optimal mesh on surface definition 16
AFLR2    : Nodes, Trias,Quads=       521       954         0
AFLR4    : Nodes, Trias,Quads=       452       816         0

AFLR4    : Generate optimal mesh on surface definition 17
AFLR2    : Nodes, Trias,Quads=       609      1109         0
AFLR4    : Nodes, Trias,Quads=       462       815         0

AFLR4    : Generate optimal mesh on surface definition 18
AFLR2    : Nodes, Trias,Quads=        11        12         0
AFLR4    : Nodes, Trias,Quads=         8         6         0

AFLR4    : Generate optimal mesh on surface definition 19
AFLR2    : Nodes, Trias,Quads=        12        14         0
AFLR4    : Nodes, Trias,Quads=         8         6         0

AFLR4    : Generate optimal mesh on surface definition 20
AFLR2    : Nodes, Trias,Quads=        12        14         0
AFLR4    : Nodes, Trias,Quads=         8         6         0

AFLR4    : Generate optimal mesh on surface definition 21
AFLR2    : Nodes, Trias,Quads=        12        14         0
AFLR4    : Nodes, Trias,Quads=         8         6         0

AFLR4    : Generate optimal mesh on surface definition 22
AFLR2    : Nodes, Trias,Quads=        12        14         0
AFLR4    : Nodes, Trias,Quads=         8         6         0

AFLR4    : Generate optimal mesh on surface definition 23
AFLR2    : Nodes, Trias,Quads=        12        14         0
AFLR4    : Nodes, Trias,Quads=         8         6         0

AFLR4    : Generate optimal mesh on surface definition 24
AFLR2    : Nodes, Trias,Quads=        12        14         0
AFLR4    : Nodes, Trias,Quads=         8         6         0

DGEOM    : Add surface definitions to composite definition 0
DGEOM    : Glue composite surface definition 0
DGEOM    : Nodes,Faces,BEdges=      4670      9332      1276

AFLR4    : Proximity BG Surface Grid Generation

AFLR4    : Nodes, Trias      =      5096     10184
AFLR4    : Nodes, Trias      =      5178     10348
AFLR4    : Nodes, Trias      =      5178     10348

AFLR4    : Surface Grid Generation

AFLR4    : Generate optimal mesh on surface definition 1
AFLR2    : Nodes, Trias,Quads=       525       968         0
AFLR4    : Nodes, Trias,Quads=       454       826         0

AFLR4    : Generate optimal mesh on surface definition 2
AFLR2    : Nodes, Trias,Quads=       200       342         0
AFLR4    : Nodes, Trias,Quads=       189       320         0

AFLR4    : Generate optimal mesh on surface definition 3
AFLR2    : Nodes, Trias,Quads=       517       952         0
AFLR4    : Nodes, Trias,Quads=       522       962         0

AFLR4    : Generate optimal mesh on surface definition 4
AFLR2    : Nodes, Trias,Quads=       200       342         0
AFLR4    : Nodes, Trias,Quads=       192       326         0

AFLR4    : Generate optimal mesh on surface definition 5
AFLR2    : Nodes, Trias,Quads=       516       950         0
AFLR4    : Nodes, Trias,Quads=       455       828         0

AFLR4    : Generate optimal mesh on surface definition 6
AFLR2    : Nodes, Trias,Quads=       200       342         0
AFLR4    : Nodes, Trias,Quads=       192       326         0

AFLR4    : Generate optimal mesh on surface definition 7
AFLR2    : Nodes, Trias,Quads=       523       964         0
AFLR4    : Nodes, Trias,Quads=       518       954         0

AFLR4    : Generate optimal mesh on surface definition 8
AFLR2    : Nodes, Trias,Quads=       200       342         0
AFLR4    : Nodes, Trias,Quads=       190       322         0

AFLR4    : Generate optimal mesh on surface definition 9
AFLR2    : Nodes, Trias,Quads=       578      1062         0
AFLR4    : Nodes, Trias,Quads=       525       956         0

AFLR4    : Generate optimal mesh on surface definition 10
AFLR2    : Nodes, Trias,Quads=       742      1369         0
AFLR4    : Nodes, Trias,Quads=       509       903         0

AFLR4    : Generate optimal mesh on surface definition 11
AFLR2    : Nodes, Trias,Quads=       579      1064         0
AFLR4    : Nodes, Trias,Quads=       758      1422         0

AFLR4    : Generate optimal mesh on surface definition 12
AFLR2    : Nodes, Trias,Quads=       708      1302         0
AFLR4    : Nodes, Trias,Quads=       508       902         0

AFLR4    : Generate optimal mesh on surface definition 13
AFLR2    : Nodes, Trias,Quads=        12        14         0
AFLR4    : Nodes, Trias,Quads=         8         6         0

AFLR4    : Generate optimal mesh on surface definition 14
AFLR2    : Nodes, Trias,Quads=       575      1056         0
AFLR4    : Nodes, Trias,Quads=       528       962         0

AFLR4    : Generate optimal mesh on surface definition 15
AFLR2    : Nodes, Trias,Quads=       722      1330         0
AFLR4    : Nodes, Trias,Quads=       529       944         0

AFLR4    : Generate optimal mesh on surface definition 16
AFLR2    : Nodes, Trias,Quads=       580      1066         0
AFLR4    : Nodes, Trias,Quads=       749      1404         0

AFLR4    : Generate optimal mesh on surface definition 17
AFLR2    : Nodes, Trias,Quads=       694      1275         0
AFLR4    : Nodes, Trias,Quads=       498       883         0

AFLR4    : Generate optimal mesh on surface definition 18
AFLR2    : Nodes, Trias,Quads=        12        14         0
AFLR4    : Nodes, Trias,Quads=         8         6         0

AFLR4    : Generate optimal mesh on surface definition 19
AFLR2    : Nodes, Trias,Quads=        12        14         0
AFLR4    : Nodes, Trias,Quads=         8         6         0

AFLR4    : Generate optimal mesh on surface definition 20
AFLR2    : Nodes, Trias,Quads=        12        14         0
AFLR4    : Nodes, Trias,Quads=         8         6         0

AFLR4    : Generate optimal mesh on surface definition 21
AFLR2    : Nodes, Trias,Quads=        12        14         0
AFLR4    : Nodes, Trias,Quads=         8         6         0

AFLR4    : Generate optimal mesh on surface definition 22
AFLR2    : Nodes, Trias,Quads=        12        14         0
AFLR4    : Nodes, Trias,Quads=         8         6         0

AFLR4    : Generate optimal mesh on surface definition 23
AFLR2    : Nodes, Trias,Quads=        12        14         0
AFLR4    : Nodes, Trias,Quads=         8         6         0

AFLR4    : Generate optimal mesh on surface definition 24
AFLR2    : Nodes, Trias,Quads=        12        14         0
AFLR4    : Nodes, Trias,Quads=         8         6         0

DGEOM    : Add surface definitions to composite definition 0
DGEOM    : Glue composite surface definition 0
DGEOM    : Nodes,Faces,BEdges=      6648     13288      1424

OVERALL  : CPU Time          =     0.447   seconds
Body 1 (of 4)
Number of nodes    = 1217
Number of elements = 2434
Number of triangle elements      = 2434
Number of quadrilateral elements = 0
Body 2 (of 4)
Number of nodes    = 1215
Number of elements = 2430
Number of triangle elements      = 2430
Number of quadrilateral elements = 0
Body 3 (of 4)
Number of nodes    = 4196
Number of elements = 8388
Number of triangle elements      = 8388
Number of quadrilateral elements = 0
Body 4 (of 4)
Number of nodes    = 20
Number of elements = 36
Number of triangle elements      = 36
Number of quadrilateral elements = 0
----------------------------
Total number of nodes    = 6648
Total number of elements = 13288
Total number of triangle elements      = 13288
Total number of quadrilateral elements = 0

Writing vtk file ....

Writing vtk surface file ....

capsGroups found:
  1: Nacelle
  2: Wing
  3: Farfield
Finished writing vtk file

Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 4
	Name = Nacelle, index = 1
	Name = leftWing, index = 2
	Name = riteWing, index = 3
	Name = Farfield, index = 4
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 3
	Name = Nacelle, index = 1
	Name = Wing, index = 2
	Name = Farfield, index = 3

Getting mesh sizing parameters
	Mesh sizing name - Nacelle
	Mesh sizing name - leftWing
	Mesh sizing name - riteWing
	Done getting mesh sizing parameters
Getting volume mesh
 
UG PARAM : SETTING INPUT PARAMETERS FROM ARGUMENT VECTOR
 
UG PARAM : mbl                         = 1         
UG PARAM : nbl                         = 10        
UG PARAM : mblelc                      = 2         
UG PARAM : mrecm                       = 3         
UG PARAM : mrecqm                      = 3         
UG PARAM : mbl                         = 1         
UG PARAM : mrecm                       = 3         
UG PARAM : mrecqm                      = 3         
UG PARAM : mblelc                      = 1         
UG PARAM : BC_IDs                  [ 0]= 1         
UG PARAM : BC_IDs                  [ 1]= 2         
UG PARAM : BC_IDs                  [ 2]= 3         
UG PARAM : BC_IDs                  [ 3]= 4         
UG PARAM : BC_IDs                  [ 4]= 5         
UG PARAM : BC_IDs                  [ 5]= 6         
UG PARAM : BC_IDs                  [ 6]= 7         
UG PARAM : BC_IDs                  [ 7]= 8         
UG PARAM : BC_IDs                  [ 8]= 9         
UG PARAM : BC_IDs                  [ 9]= 10        
UG PARAM : BC_IDs                  [10]= 11        
UG PARAM : BC_IDs                  [11]= 12        
UG PARAM : BC_IDs                  [12]= 13        
UG PARAM : BC_IDs                  [13]= 14        
UG PARAM : BC_IDs                  [14]= 15        
UG PARAM : BC_IDs                  [15]= 16        
UG PARAM : BC_IDs                  [16]= 17        
UG PARAM : BC_IDs                  [17]= 18        
UG PARAM : BC_IDs                  [18]= 19        
UG PARAM : BC_IDs                  [19]= 20        
UG PARAM : BC_IDs                  [20]= 21        
UG PARAM : BC_IDs                  [21]= 22        
UG PARAM : BC_IDs                  [22]= 23        
UG PARAM : BC_IDs                  [23]= 24        
UG PARAM : BL_DS                   [ 0]= 0.434102  
UG PARAM : BL_DS                   [ 1]= 0.434102  
UG PARAM : BL_DS                   [ 2]= 0.434102  
UG PARAM : BL_DS                   [ 3]= 0.434102  
UG PARAM : BL_DS                   [ 4]= 0.434102  
UG PARAM : BL_DS                   [ 5]= 0.434102  
UG PARAM : BL_DS                   [ 6]= 0.434102  
UG PARAM : BL_DS                   [ 7]= 0.434102  
UG PARAM : BL_DS                   [ 8]= 0.217051  
UG PARAM : BL_DS                   [ 9]= 0.217051  
UG PARAM : BL_DS                   [10]= 0.217051  
UG PARAM : BL_DS                   [11]= 0.217051  
UG PARAM : BL_DS                   [12]= 0.217051  
UG PARAM : BL_DS                   [13]= 0.217051  
UG PARAM : BL_DS                   [14]= 0.217051  
UG PARAM : BL_DS                   [15]= 0.217051  
UG PARAM : BL_DS                   [16]= 0.217051  
UG PARAM : BL_DS                   [17]= 0.217051  
UG PARAM : BL_DS                   [18]= 0         
UG PARAM : BL_DS                   [19]= 0         
UG PARAM : BL_DS                   [20]= 0         
UG PARAM : BL_DS                   [21]= 0         
UG PARAM : BL_DS                   [22]= 0         
UG PARAM : BL_DS                   [23]= 0         
UG PARAM : BL_DEL                  [ 0]= 2.17051   
UG PARAM : BL_DEL                  [ 1]= 2.17051   
UG PARAM : BL_DEL                  [ 2]= 2.17051   
UG PARAM : BL_DEL                  [ 3]= 2.17051   
UG PARAM : BL_DEL                  [ 4]= 2.17051   
UG PARAM : BL_DEL                  [ 5]= 2.17051   
UG PARAM : BL_DEL                  [ 6]= 2.17051   
UG PARAM : BL_DEL                  [ 7]= 2.17051   
UG PARAM : BL_DEL                  [ 8]= 2.17051   
UG PARAM : BL_DEL                  [ 9]= 2.17051   
UG PARAM : BL_DEL                  [10]= 2.17051   
UG PARAM : BL_DEL                  [11]= 2.17051   
UG PARAM : BL_DEL                  [12]= 2.17051   
UG PARAM : BL_DEL                  [13]= 2.17051   
UG PARAM : BL_DEL                  [14]= 2.17051   
UG PARAM : BL_DEL                  [15]= 2.17051   
UG PARAM : BL_DEL                  [16]= 2.17051   
UG PARAM : BL_DEL                  [17]= 2.17051   
UG PARAM : BL_DEL                  [18]= 0         
UG PARAM : BL_DEL                  [19]= 0         
UG PARAM : BL_DEL                  [20]= 0         
UG PARAM : BL_DEL                  [21]= 0         
UG PARAM : BL_DEL                  [22]= 0         
UG PARAM : BL_DEL                  [23]= 0         
UG PARAM : mpfrmt                      = 0         
 
AFLR2    : ---------------------------------------
AFLR2    : AFLR2 LIBRARY
AFLR2    : ADVANCING-FRONT/LOCAL-RECONNECTION
AFLR2    : TRIA/QUAD GRID GENERATOR
AFLR2    : Version Number 9.18.1
AFLR2    : Version Date   06/11/24 @ 05:52PM
AFLR2    : Compile OS     Darwin 23.5.0 arm64
AFLR2    : Compile Date   06/11/24 @ 05:52PM
AFLR2    : Copyright 1994-2021, D.L. Marcum
AFLR2    : ---------------------------------------
 
AFLR4    : ---------------------------------------
AFLR4    : AFLR4 LIBRARY
AFLR4    : ADVANCING-FRONT/LOCAL-RECONNECTION
AFLR4    : TRIA/QUAD SURFACE GRID GENERATOR
AFLR4    : Version Number 11.5.15
AFLR4    : Version Date   07/19/24 @ 07:04PM
AFLR4    : Compile OS     Darwin 23.5.0 arm64
AFLR4    : Compile Date   07/19/24 @ 07:06PM
AFLR4    : Copyright 1994-2021, D.L. Marcum
AFLR4    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.8.1
EGADS    : ---------------------------------------

EGADS    : EGADS CAD Geometry Setup

EGADS    : Model has 4 Active Bodies

EGADS    : Body 0 is a SolidBody
EGADS    : Body 0 has 1 Shells
EGADS    : Body 0 has 4 Faces
EGADS    : Body 0 has 8 Edges
EGADS    : Body 0 has 4 Loops
EGADS    : Body 0 has 4 Nodes
EGADS    : Body 1 is a SolidBody
EGADS    : Body 1 has 1 Shells
EGADS    : Body 1 has 4 Faces
EGADS    : Body 1 has 8 Edges
EGADS    : Body 1 has 4 Loops
EGADS    : Body 1 has 4 Nodes
EGADS    : Body 2 is a SolidBody
EGADS    : Body 2 has 1 Shells
EGADS    : Body 2 has 10 Faces
EGADS    : Body 2 has 18 Edges
EGADS    : Body 2 has 10 Loops
EGADS    : Body 2 has 10 Nodes
EGADS    : Body 3 is a SolidBody
EGADS    : Body 3 has 1 Shells
EGADS    : Body 3 has 6 Faces
EGADS    : Body 3 has 12 Edges
EGADS    : Body 3 has 6 Loops
EGADS    : Body 3 has 8 Nodes

EGADS    : Check Grid BCs

EGADS    : Grid BCs are OK

EGADS    : Face Neighbor-Faces Information

EGADS    : QC  = Face Quad Combination Flag
EGADS    : IER = Face Isolated Edge Refinement Flag
EGADS    : ER  = Face Edge Refinement Factor
EGADS    :       Not applicable for Faces with a FarField Grid BC.
EGADS    : SF  = Face Scale Factor
EGADS    :       Not applicable for Faces with a FarField Grid BC.

EGADS    :   Face          Body    QC   IER       ER    Scale   Neighbor
EGADS    :     ID  Active    ID  Flag  Flag   Weight   Factor   Faces
EGADS    :      1     Yes     0     0     1        0        1   2 3
EGADS    :      2     Yes     0     0     1        0        1   1 4
EGADS    :      3     Yes     0     0     1        0        1   1 4
EGADS    :      4     Yes     0     0     1        0        1   2 3
EGADS    :      5     Yes     1     0     1        0        1   6 7
EGADS    :      6     Yes     1     0     1        0        1   5 8
EGADS    :      7     Yes     1     0     1        0        1   5 8
EGADS    :      8     Yes     1     0     1        0        1   6 7
EGADS    :      9     Yes     2     0     1        0        1   10 11 14
EGADS    :     10     Yes     2     0     1        0        1   9 12 13
EGADS    :     11     Yes     2     0     1        0        1   9 12 16
EGADS    :     12     Yes     2     0     1        0        1   10 11 13
EGADS    :     13     Yes     2     0     1        0        1   10 12
EGADS    :     14     Yes     2     0     1        0        1   9 15 16
EGADS    :     15     Yes     2     0     1        0        1   14 17 18
EGADS    :     16     Yes     2     0     1        0        1   11 14 17
EGADS    :     17     Yes     2     0     1        0        1   15 16 18
EGADS    :     18     Yes     2     0     1        0        1   15 17
EGADS    :     19     Yes     3     0     1       NA       NA   21 22 23 24
EGADS    :     20     Yes     3     0     1       NA       NA   21 22 23 24
EGADS    :     21     Yes     3     0     1       NA       NA   19 20 23 24
EGADS    :     22     Yes     3     0     1       NA       NA   19 20 23 24
EGADS    :     23     Yes     3     0     1       NA       NA   19 20 21 22
EGADS    :     24     Yes     3     0     1       NA       NA   19 20 21 22

EGADS    : Face Edges Information

EGADS    :   Face   Edges
EGADS    :      1   -1 3 2 -4
EGADS    :      2   -2 5 1 -6
EGADS    :      3   7 4 -8 -3
EGADS    :      4   8 6 -7 -5
EGADS    :      5   9 12 -10 -11
EGADS    :      6   10 14 -9 -13
EGADS    :      7   -15 11 16 -12
EGADS    :      8   -16 13 15 -14
EGADS    :      9   -17 18 19 -20
EGADS    :     10   -21 20 22 -23
EGADS    :     11   -19 24 17 -25
EGADS    :     12   -22 25 21 -26
EGADS    :     13   23 26
EGADS    :     14   27 29 -28 -18
EGADS    :     15   30 32 -31 -29
EGADS    :     16   28 33 -27 -24
EGADS    :     17   31 34 -30 -33
EGADS    :     18   -32 -34
EGADS    :     19   35 36 -37 -38
EGADS    :     20   -39 42 41 -40
EGADS    :     21   43 39 -44 -35
EGADS    :     22   -45 37 46 -41
EGADS    :     23   38 45 -42 -43
EGADS    :     24   -36 44 40 -46

EGADS    : Face Loops Information

EGADS    :   Face   Loops
EGADS    :      1   1
EGADS    :      2   2
EGADS    :      3   3
EGADS    :      4   4
EGADS    :      5   5
EGADS    :      6   6
EGADS    :      7   7
EGADS    :      8   8
EGADS    :      9   9
EGADS    :     10   10
EGADS    :     11   11
EGADS    :     12   12
EGADS    :     13   13
EGADS    :     14   14
EGADS    :     15   15
EGADS    :     16   16
EGADS    :     17   17
EGADS    :     18   18
EGADS    :     19   19
EGADS    :     20   20
EGADS    :     21   21
EGADS    :     22   22
EGADS    :     23   23
EGADS    :     24   24

EGADS    : Loop Edges Information

EGADS    :   Loop  Active   Edges
EGADS    :      1     Yes   -1 3 2 -4
EGADS    :      2     Yes   -2 5 1 -6
EGADS    :      3     Yes   7 4 -8 -3
EGADS    :      4     Yes   8 6 -7 -5
EGADS    :      5     Yes   9 12 -10 -11
EGADS    :      6     Yes   10 14 -9 -13
EGADS    :      7     Yes   -15 11 16 -12
EGADS    :      8     Yes   -16 13 15 -14
EGADS    :      9     Yes   -17 18 19 -20
EGADS    :     10     Yes   -21 20 22 -23
EGADS    :     11     Yes   -19 24 17 -25
EGADS    :     12     Yes   -22 25 21 -26
EGADS    :     13     Yes   23 26
EGADS    :     14     Yes   27 29 -28 -18
EGADS    :     15     Yes   30 32 -31 -29
EGADS    :     16     Yes   28 33 -27 -24
EGADS    :     17     Yes   31 34 -30 -33
EGADS    :     18     Yes   -32 -34
EGADS    :     19     Yes   35 36 -37 -38
EGADS    :     20     Yes   -39 42 41 -40
EGADS    :     21     Yes   43 39 -44 -35
EGADS    :     22     Yes   -45 37 46 -41
EGADS    :     23     Yes   38 45 -42 -43
EGADS    :     24     Yes   -36 44 40 -46

EGADS    : Edge Node, Scale Factor, and Neighbor-Faces Information

EGADS    : ESF = Edge Scale Factor
EGADS    :       Not applicable for DEGENERATE Edges or Edges with a FarField
EGADS    :       Grid BC Neighbor Face.

EGADS    :                                             Neighbor
EGADS    :   Edge  Body  Active Node1 Node2      ESF   Faces
EGADS    :      1     0     Yes     1     2        1   1 2
EGADS    :      2     0     Yes     3     4        1   1 2
EGADS    :      3     0     Yes     1     3        1   1 3
EGADS    :      4     0     Yes     2     4        1   1 3
EGADS    :      5     0     Yes     3     1        1   2 4
EGADS    :      6     0     Yes     4     2        1   2 4
EGADS    :      7     0     Yes     1     2        1   3 4
EGADS    :      8     0     Yes     3     4        1   3 4
EGADS    :      9     1     Yes     5     6        1   5 6
EGADS    :     10     1     Yes     7     8        1   5 6
EGADS    :     11     1     Yes     5     7        1   5 7
EGADS    :     12     1     Yes     6     8        1   5 7
EGADS    :     13     1     Yes     7     5        1   6 8
EGADS    :     14     1     Yes     8     6        1   6 8
EGADS    :     15     1     Yes     5     6        1   7 8
EGADS    :     16     1     Yes     7     8        1   7 8
EGADS    :     17     2     Yes     9    10        1   9 11
EGADS    :     18     2     Yes     9    11        1   9 14
EGADS    :     19     2     Yes    11    12        1   9 11
EGADS    :     20     2     Yes    10    12        1   9 10
EGADS    :     21     2     Yes    10    13        1   10 12
EGADS    :     22     2     Yes    12    14        1   10 12
EGADS    :     23     2     Yes    13    14        1   10 13
EGADS    :     24     2     Yes    11     9        1   11 16
EGADS    :     25     2     Yes    12    10        1   11 12
EGADS    :     26     2     Yes    14    13        1   12 13
EGADS    :     27     2     Yes     9    15        1   14 16
EGADS    :     28     2     Yes    11    16        1   14 16
EGADS    :     29     2     Yes    15    16        1   14 15
EGADS    :     30     2     Yes    15    17        1   15 17
EGADS    :     31     2     Yes    16    18        1   15 17
EGADS    :     32     2     Yes    17    18        1   15 18
EGADS    :     33     2     Yes    16    15        1   16 17
EGADS    :     34     2     Yes    18    17        1   17 18
EGADS    :     35     3     Yes    20    19       NA   19 21
EGADS    :     36     3     Yes    19    21       NA   19 24
EGADS    :     37     3     Yes    22    21       NA   19 22
EGADS    :     38     3     Yes    20    22       NA   19 23
EGADS    :     39     3     Yes    24    23       NA   20 21
EGADS    :     40     3     Yes    23    25       NA   20 24
EGADS    :     41     3     Yes    26    25       NA   20 22
EGADS    :     42     3     Yes    24    26       NA   20 23
EGADS    :     43     3     Yes    20    24       NA   21 23
EGADS    :     44     3     Yes    19    23       NA   21 24
EGADS    :     45     3     Yes    22    26       NA   22 23
EGADS    :     46     3     Yes    21    25       NA   22 24

EGADS    : Node Information

EGADS    :   Node  Active      Coordinates
EGADS    :      1     Yes       90.5173952                0                0
EGADS    :      2     Yes       90.5173952                0                0
EGADS    :      3     Yes       60.5173952                0                0
EGADS    :      4     Yes       60.5173952                0                0
EGADS    :      5     Yes       90.5173952       29.3018771                0
EGADS    :      6     Yes       90.5173952       29.3018771                0
EGADS    :      7     Yes       60.5173952       29.3018771                0
EGADS    :      8     Yes       60.5173952       29.3018771                0
EGADS    :      9     Yes       97.2007855                0                0
EGADS    :     10     Yes       97.9335611                0                0
EGADS    :     11     Yes               50                0                0
EGADS    :     12     Yes       75.3047874                0                0
EGADS    :     13     Yes       123.552357                0        4.7180639
EGADS    :     14     Yes       118.391317                0       3.99272703
EGADS    :     15     Yes       97.9335611       36.1389817                0
EGADS    :     16     Yes       75.3047874       36.1389817                0
EGADS    :     17     Yes       123.552357       97.6729236        4.7180639
EGADS    :     18     Yes       118.391317       97.6729236       3.99272703
EGADS    :     19     Yes                0                0       1947.05079
EGADS    :     20     Yes                0                0                0
EGADS    :     21     Yes                0       1953.45847       1947.05079
EGADS    :     22     Yes                0       1953.45847                0
EGADS    :     23     Yes       2040.21562                0       1947.05079
EGADS    :     24     Yes       2040.21562                0                0
EGADS    :     25     Yes       2040.21562       1953.45847       1947.05079
EGADS    :     26     Yes       2040.21562       1953.45847                0

EGADS    : Face and Edge Match Information

EGADS    : No Face Matches Found

AFLR4    : Surface Mesh Spacing Setup

AFLR4    : Max Bounding Box Length     = 3906.92
AFLR4    : Min Bounding Box Length     = 3906.92
AFLR4    : Max Ref Bounding Box Length = 195.346
AFLR4    : Min Ref Bounding Box Length = 22.2515
AFLR4    : Reference Length            = 22.2515
AFLR4    : BL Thickness                = 0
AFLR4    : FarField Spacing            = 428.344
AFLR4    : Abs Min Surf Spacing        = 0.0556287
AFLR4    : Min Surf Spacing            = 0.111257
AFLR4    : Max Surf Spacing            = 2.22515
AFLR4    : Global Scale Factor         = 1

AFLR4    : Geometry Definition Information

AFLR4    : Definition              Definition   Composite             Grid BC
AFLR4    :         ID                    Type          ID                Type
AFLR4    :          0     glue-only composite           -                   -
AFLR4    :          1            CAD geometry           0            STD w/BL
AFLR4    :          2            CAD geometry           0            STD w/BL
AFLR4    :          3            CAD geometry           0            STD w/BL
AFLR4    :          4            CAD geometry           0            STD w/BL
AFLR4    :          5            CAD geometry           0            STD w/BL
AFLR4    :          6            CAD geometry           0            STD w/BL
AFLR4    :          7            CAD geometry           0            STD w/BL
AFLR4    :          8            CAD geometry           0            STD w/BL
AFLR4    :          9            CAD geometry           0            STD w/BL
AFLR4    :         10            CAD geometry           0            STD w/BL
AFLR4    :         11            CAD geometry           0            STD w/BL
AFLR4    :         12            CAD geometry           0            STD w/BL
AFLR4    :         13            CAD geometry           0            STD w/BL
AFLR4    :         14            CAD geometry           0            STD w/BL
AFLR4    :         15            CAD geometry           0            STD w/BL
AFLR4    :         16            CAD geometry           0            STD w/BL
AFLR4    :         17            CAD geometry           0            STD w/BL
AFLR4    :         18            CAD geometry           0            STD w/BL
AFLR4    :         19            CAD geometry           0            FARFIELD
AFLR4    :         20            CAD geometry           0            FARFIELD
AFLR4    :         21            CAD geometry           0            FARFIELD
AFLR4    :         22            CAD geometry           0            FARFIELD
AFLR4    :         23            CAD geometry           0            FARFIELD
AFLR4    :         24            CAD geometry           0            FARFIELD

AFLR4    : Case has 2 Proximity Checking Components

AFLR4    : Component 1 includes Definitions 9 10 11 12 13 14 15 16 17 18
AFLR4    : Component 2 includes Definitions 1 2 3 4 5 6 7 8

AFLR4    : Define CAD surface definition 1
AFLR4    : Define CAD surface definition 2
AFLR4    : Define CAD surface definition 3
AFLR4    : Define CAD surface definition 4
AFLR4    : Define CAD surface definition 5
AFLR4    : Define CAD surface definition 6
AFLR4    : Define CAD surface definition 7
AFLR4    : Define CAD surface definition 8
AFLR4    : Define CAD surface definition 9
AFLR4    : Define CAD surface definition 10
AFLR4    : Define CAD surface definition 11
AFLR4    : Define CAD surface definition 12
AFLR4    : Define CAD surface definition 13
AFLR4    : Define CAD surface definition 14
AFLR4    : Define CAD surface definition 15
AFLR4    : Define CAD surface definition 16
AFLR4    : Define CAD surface definition 17
AFLR4    : Define CAD surface definition 18
AFLR4    : Define CAD surface definition 19
AFLR4    : Define CAD surface definition 20
AFLR4    : Define CAD surface definition 21
AFLR4    : Define CAD surface definition 22
AFLR4    : Define CAD surface definition 23
AFLR4    : Define CAD surface definition 24
 
AFLR43   : INPUT SURFACE MESH FROM TESS
 
AFLR43   : Quad Surface Faces=         0
AFLR43   : Tria Surface Faces=     13288
AFLR43   : Nodes             =      6648
 
 
UG PARAM : SETTING INPUT PARAMETERS FROM ARGUMENT VECTOR
 
UG PARAM : mbl                         = 1         
UG PARAM : nbl                         = 10        
UG PARAM : mblelc                      = 2         
UG PARAM : mrecm                       = 3         
UG PARAM : mrecqm                      = 3         
UG PARAM : mbl                         = 1         
UG PARAM : mrecm                       = 3         
UG PARAM : mrecqm                      = 3         
UG PARAM : mblelc                      = 1         
UG PARAM : BC_IDs                  [ 0]= 1         
UG PARAM : BC_IDs                  [ 1]= 2         
UG PARAM : BC_IDs                  [ 2]= 3         
UG PARAM : BC_IDs                  [ 3]= 4         
UG PARAM : BC_IDs                  [ 4]= 5         
UG PARAM : BC_IDs                  [ 5]= 6         
UG PARAM : BC_IDs                  [ 6]= 7         
UG PARAM : BC_IDs                  [ 7]= 8         
UG PARAM : BC_IDs                  [ 8]= 9         
UG PARAM : BC_IDs                  [ 9]= 10        
UG PARAM : BC_IDs                  [10]= 11        
UG PARAM : BC_IDs                  [11]= 12        
UG PARAM : BC_IDs                  [12]= 13        
UG PARAM : BC_IDs                  [13]= 14        
UG PARAM : BC_IDs                  [14]= 15        
UG PARAM : BC_IDs                  [15]= 16        
UG PARAM : BC_IDs                  [16]= 17        
UG PARAM : BC_IDs                  [17]= 18        
UG PARAM : BC_IDs                  [18]= 19        
UG PARAM : BC_IDs                  [19]= 20        
UG PARAM : BC_IDs                  [20]= 21        
UG PARAM : BC_IDs                  [21]= 22        
UG PARAM : BC_IDs                  [22]= 23        
UG PARAM : BC_IDs                  [23]= 24        
UG PARAM : BL_DS                   [ 0]= 0.434102  
UG PARAM : BL_DS                   [ 1]= 0.434102  
UG PARAM : BL_DS                   [ 2]= 0.434102  
UG PARAM : BL_DS                   [ 3]= 0.434102  
UG PARAM : BL_DS                   [ 4]= 0.434102  
UG PARAM : BL_DS                   [ 5]= 0.434102  
UG PARAM : BL_DS                   [ 6]= 0.434102  
UG PARAM : BL_DS                   [ 7]= 0.434102  
UG PARAM : BL_DS                   [ 8]= 0.217051  
UG PARAM : BL_DS                   [ 9]= 0.217051  
UG PARAM : BL_DS                   [10]= 0.217051  
UG PARAM : BL_DS                   [11]= 0.217051  
UG PARAM : BL_DS                   [12]= 0.217051  
UG PARAM : BL_DS                   [13]= 0.217051  
UG PARAM : BL_DS                   [14]= 0.217051  
UG PARAM : BL_DS                   [15]= 0.217051  
UG PARAM : BL_DS                   [16]= 0.217051  
UG PARAM : BL_DS                   [17]= 0.217051  
UG PARAM : BL_DS                   [18]= 0         
UG PARAM : BL_DS                   [19]= 0         
UG PARAM : BL_DS                   [20]= 0         
UG PARAM : BL_DS                   [21]= 0         
UG PARAM : BL_DS                   [22]= 0         
UG PARAM : BL_DS                   [23]= 0         
UG PARAM : BL_DEL                  [ 0]= 2.17051   
UG PARAM : BL_DEL                  [ 1]= 2.17051   
UG PARAM : BL_DEL                  [ 2]= 2.17051   
UG PARAM : BL_DEL                  [ 3]= 2.17051   
UG PARAM : BL_DEL                  [ 4]= 2.17051   
UG PARAM : BL_DEL                  [ 5]= 2.17051   
UG PARAM : BL_DEL                  [ 6]= 2.17051   
UG PARAM : BL_DEL                  [ 7]= 2.17051   
UG PARAM : BL_DEL                  [ 8]= 2.17051   
UG PARAM : BL_DEL                  [ 9]= 2.17051   
UG PARAM : BL_DEL                  [10]= 2.17051   
UG PARAM : BL_DEL                  [11]= 2.17051   
UG PARAM : BL_DEL                  [12]= 2.17051   
UG PARAM : BL_DEL                  [13]= 2.17051   
UG PARAM : BL_DEL                  [14]= 2.17051   
UG PARAM : BL_DEL                  [15]= 2.17051   
UG PARAM : BL_DEL                  [16]= 2.17051   
UG PARAM : BL_DEL                  [17]= 2.17051   
UG PARAM : BL_DEL                  [18]= 0         
UG PARAM : BL_DEL                  [19]= 0         
UG PARAM : BL_DEL                  [20]= 0         
UG PARAM : BL_DEL                  [21]= 0         
UG PARAM : BL_DEL                  [22]= 0         
UG PARAM : BL_DEL                  [23]= 0         
UG PARAM : mpfrmt                      = 0         
 
AFLR3    : ---------------------------------------
AFLR3    : AFLR3 LIBRARY
AFLR3    : ADVANCING-FRONT/LOCAL-RECONNECTION
AFLR3    : TETRAHEDRAL GRID GENERATOR
AFLR3    : Version Number 16.32.50
AFLR3    : Version Date   10/31/23 @ 06:31PM
AFLR3    : Compile OS     Darwin 23.3.0 arm64
AFLR3    : Compile Date   02/08/24 @ 04:22PM
AFLR3    : Copyright 1994-2021, D.L. Marcum
AFLR3    : ---------------------------------------
 
AFLR3 IC : INPUT SURFACE GRID CHECK
 
AFLR3 IC : Nodes, Elements   =      6648         0

UG3      : Boundary Conditions

UG3      :  B-Face ID            Boundary Condition
UG3      :          1                    Solid w/BL
UG3      :          2                    Solid w/BL
UG3      :          3                    Solid w/BL
UG3      :          4                    Solid w/BL
UG3      :          5                    Solid w/BL
UG3      :          6                    Solid w/BL
UG3      :          7                    Solid w/BL
UG3      :          8                    Solid w/BL
UG3      :          9                    Solid w/BL
UG3      :         10                    Solid w/BL
UG3      :         11                    Solid w/BL
UG3      :         12                    Solid w/BL
UG3      :         13                    Solid w/BL
UG3      :         14                    Solid w/BL
UG3      :         15                    Solid w/BL
UG3      :         16                    Solid w/BL
UG3      :         17                    Solid w/BL
UG3      :         18                    Solid w/BL
UG3      :         19                      FarField
UG3      :         20                      FarField
UG3      :         21                      FarField
UG3      :         22                      FarField
UG3      :         23                      FarField
UG3      :         24                      FarField
 
AFLR3    : CPU Time          =     0.008   seconds
 
AFLR3    : DONE
 
ANBL3    : ---------------------------------------
ANBL3    : ANBL3 LIBRARY
ANBL3    : ADVANCING-NORMAL
ANBL3    : BOUNDARY-LAYER (BL)
ANBL3    : STRUCTURED-LAYER (SL)
ANBL3    : SPECIFIED NORMAL SPACING (SNS)
ANBL3    : TETRAHEDRAL/PENTAHEDRAL GRID GENERATOR
ANBL3    : Version Number 9.34.2
ANBL3    : Version Date   03/10/23 @ 04:32PM
ANBL3    : Compile OS     Darwin 23.3.0 arm64
ANBL3    : Compile Date   02/08/24 @ 04:22PM
ANBL3    : Copyright 1994-2021, D.L. Marcum
ANBL3    : ---------------------------------------
 
ANBL3 BLC: BL BOUNDARY CONDITIONS CHECK
 
ANBL3 BLC: Nodes, Elements   =      6648         0
 
ANBL3    : CPU Time          =     0.007   seconds
 
ANBL3    : DONE
 
ANBL3 BLG: BL NODE GENERATION
 
ANBL3 BLG: Nodes, Layer      =         0         0
ANBL3 BLG: Nodes, Layer      =     13236         2
ANBL3 BLG: Nodes, Layer      =     19803         3
ANBL3 BLG: Nodes, Layer      =     25869         4
ANBL3 BLG: Nodes, Layer      =     31554         5
ANBL3 BLG: Nodes, Layer      =     37022         6
ANBL3 BLG: Nodes, Layer      =     42307         7
ANBL3 BLG: Nodes, Layer      =     47280         8
ANBL3 BLG: Nodes, Layer      =     51732         9
ANBL3 BLG: Nodes, Layer      =     55961        10
ANBL3 BLG: Nodes, Layer      =     60010        11
 
ANBL3    : CPU Time          =     1.858   seconds
 
ANBL3    : DONE
 
AFLR3 IC : INPUT SURFACE GRID CHECK
 
AFLR3 IC : Nodes, Elements   =      6648         0
 
AFLR3    : CPU Time          =     0.004   seconds
 
AFLR3 IG : INITIAL VOLUME GRID GENERATION
 
AFLR3 IG : Nodes, Elements   =      6648         0
AFLR3 IG : Nodes, Elements   =         8        10
AFLR3 IG : Nodes, Elements   =      1332      8500
AFLR3 IG : Nodes, Elements   =      2664     17268
AFLR3 IG : Nodes, Elements   =      3996     25716
AFLR3 IG : Nodes, Elements   =      5328     35137
AFLR3 IG : Nodes, Elements   =      6655     45683
AFLR3 IG : Nodes, Elements   =      6655     45689
AFLR3 IG : Nodes, Elements   =      6655     45677
AFLR3 IG : Nodes, Elements   =      6655     47451
AFLR3 IG : Nodes, Elements   =      6655     45089
AFLR3 IG : Nodes, Elements   =      6655     45152
AFLR3 IG : Nodes, Elements   =      6655     45155
AFLR3 IG : Nodes, Elements   =      6655     45739
AFLR3 IG : Nodes, Elements   =      6655     45709
AFLR3 IG : Nodes, Elements   =      6655     44362
AFLR3 IG : Nodes, Elements   =      6655     44363
AFLR3 IG : Nodes, Elements   =      6655     44745
AFLR3 IG : Nodes, Elements   =      6655     44391
AFLR3 IG : Nodes, Elements   =      6655     44392
AFLR3 IG : Nodes, Elements   =      6655     44666
AFLR3 IG : Nodes, Elements   =      6655     44653
AFLR3 IG : Nodes, Elements   =      6655     44286
AFLR3 IG : Nodes, Elements   =      6655     44288
AFLR3 IG : Nodes, Elements   =      6655     44497
AFLR3 IG : Nodes, Elements   =      6655     44291
AFLR3 IG : Nodes, Elements   =      6655     44292
AFLR3 IG : Nodes, Elements   =      6655     44436
AFLR3 IG : Nodes, Elements   =      6655     44426
AFLR3 IG : Nodes, Elements   =      6655     44281
AFLR3 IG : Nodes, Elements   =      6655     44434
AFLR3 IG : Nodes, Elements   =      6655     44279
AFLR3 IG : Nodes, Elements   =      6655     44417
AFLR3 IG : Nodes, Elements   =      6655     44408
AFLR3 IG : Nodes, Elements   =      6655     44262
AFLR3 IG : Nodes, Elements   =      6655     44396
AFLR3 IG : Nodes, Elements   =      6655     44274
AFLR3 IG : Nodes, Elements   =      6655     44373
AFLR3 IG : Nodes, Elements   =      6655     44366
AFLR3 IG : Nodes, Elements   =      6655     44260
AFLR3 IG : Nodes, Elements   =      6655     44402
AFLR3 IG : Nodes, Elements   =      6655     44273
AFLR3 IG : Nodes, Elements   =      6655     44369
AFLR3 IG : Nodes, Elements   =      6655     44364
AFLR3 IG : Nodes, Elements   =      6655     44256
AFLR3 IG : Nodes, Elements   =      6655     44375
AFLR3 IG : Nodes, Elements   =      6655     44262
AFLR3 IG : Nodes, Elements   =      6655     44369
AFLR3 IG : Nodes, Elements   =      6655     44366
AFLR3 IG : Nodes, Elements   =      6655     44258
AFLR3 IG : Nodes, Elements   =      6655     44257
AFLR3 IG : Nodes, Elements   =      6655     44380
AFLR3 IG : Nodes, Elements   =      6655     44263
AFLR3 IG : Nodes, Elements   =      6655     44363
AFLR3 IG : Nodes, Elements   =      6655     44362
AFLR3 IG : Nodes, Elements   =      6655     44270
AFLR3 IG : Nodes, Elements   =      6655     44271
AFLR3 IG : Nodes, Elements   =      6655     44270
AFLR3 IG : Nodes, Elements   =      6655     44321
AFLR3 IG : Nodes, Elements   =      6655     44263
AFLR3 IG : Nodes, Elements   =      6655     44317
AFLR3 IG : Nodes, Elements   =      6655     44314
AFLR3 IG : Nodes, Elements   =      6655     44262
AFLR3 IG : Nodes, Elements   =      6655     44263
AFLR3 IG : Nodes, Elements   =      6655     44320
AFLR3 IG : Nodes, Elements   =      6655     44269
AFLR3 IG : Nodes, Elements   =      6655     44310
AFLR3 IG : Nodes, Elements   =      6655     44308
AFLR3 IG : Nodes, Elements   =      6655     44264
AFLR3 IG : Nodes, Elements   =      6655     44320
AFLR3 IG : Nodes, Elements   =      6655     44266
AFLR3 IG : Nodes, Elements   =      6655     44311
AFLR3 IG : Nodes, Elements   =      6655     44309
AFLR3 IG : Nodes, Elements   =      6655     44258
AFLR3 IG : Nodes, Elements   =      6655     44317
AFLR3 IG : Nodes, Elements   =      6655     44265
AFLR3 IG : Nodes, Elements   =      6655     44267
AFLR3 IG : Nodes, Elements   =      6648     24989
AFLR3 IG : Nodes, Elements   =      6648     26288
AFLR3 IG : Nodes, Elements   =      6648     23110
AFLR3 IG : Nodes, Elements   =      6648     22265
 
AFLR3    : CPU Time          =     0.594   seconds
 
AFLR3 GG : ISOTROPIC VOLUME GRID GENERATION
 
AFLR3 GG : Nodes, Elements   =      6648     22265
AFLR3 GG : Nodes, Elements   =      8375     27503
AFLR3 GG : Nodes, Elements   =      8375     32736
AFLR3 GG : Nodes, Elements   =      8375     30893
AFLR3 GG : Nodes, Elements   =      8375     30460
AFLR3 GG : Nodes, Elements   =     10055     35588
AFLR3 GG : Nodes, Elements   =     10055     42754
AFLR3 GG : Nodes, Elements   =     10055     40597
AFLR3 GG : Nodes, Elements   =     10055     40211
AFLR3 GG : Nodes, Elements   =     11867     45701
AFLR3 GG : Nodes, Elements   =     11867     53702
AFLR3 GG : Nodes, Elements   =     11867     51495
AFLR3 GG : Nodes, Elements   =     11867     51102
AFLR3 GG : Nodes, Elements   =     13742     56777
AFLR3 GG : Nodes, Elements   =     13742     64748
AFLR3 GG : Nodes, Elements   =     13742     62622
AFLR3 GG : Nodes, Elements   =     13742     62184
AFLR3 GG : Nodes, Elements   =     15637     67903
AFLR3 GG : Nodes, Elements   =     15637     75943
AFLR3 GG : Nodes, Elements   =     15637     73853
AFLR3 GG : Nodes, Elements   =     15637     73429
AFLR3 GG : Nodes, Elements   =     17497     79063
AFLR3 GG : Nodes, Elements   =     17497     86929
AFLR3 GG : Nodes, Elements   =     17497     84822
AFLR3 GG : Nodes, Elements   =     17497     84453
AFLR3 GG : Nodes, Elements   =     19358     90074
AFLR3 GG : Nodes, Elements   =     19358     97979
AFLR3 GG : Nodes, Elements   =     19358     95900
AFLR3 GG : Nodes, Elements   =     19358     95501
AFLR3 GG : Nodes, Elements   =     21182    101014
AFLR3 GG : Nodes, Elements   =     21182    108824
AFLR3 GG : Nodes, Elements   =     21182    106721
AFLR3 GG : Nodes, Elements   =     21182    106371
AFLR3 GG : Nodes, Elements   =     22953    111712
AFLR3 GG : Nodes, Elements   =     22953    119193
AFLR3 GG : Nodes, Elements   =     22953    117260
AFLR3 GG : Nodes, Elements   =     22953    116902
AFLR3 GG : Nodes, Elements   =     24659    122062
AFLR3 GG : Nodes, Elements   =     24659    129358
AFLR3 GG : Nodes, Elements   =     24659    127471
AFLR3 GG : Nodes, Elements   =     24659    127125
AFLR3 GG : Nodes, Elements   =     26322    132156
AFLR3 GG : Nodes, Elements   =     26322    139187
AFLR3 GG : Nodes, Elements   =     26322    137339
AFLR3 GG : Nodes, Elements   =     26322    137016
AFLR3 GG : Nodes, Elements   =     27964    141980
AFLR3 GG : Nodes, Elements   =     27964    148896
AFLR3 GG : Nodes, Elements   =     27964    147162
AFLR3 GG : Nodes, Elements   =     27964    146829
AFLR3 GG : Nodes, Elements   =     29507    151482
AFLR3 GG : Nodes, Elements   =     29507    158031
AFLR3 GG : Nodes, Elements   =     29507    156288
AFLR3 GG : Nodes, Elements   =     29507    156010
AFLR3 GG : Nodes, Elements   =     30967    160420
AFLR3 GG : Nodes, Elements   =     30967    166634
AFLR3 GG : Nodes, Elements   =     30967    165028
AFLR3 GG : Nodes, Elements   =     30967    164732
AFLR3 GG : Nodes, Elements   =     32405    169071
AFLR3 GG : Nodes, Elements   =     32405    175152
AFLR3 GG : Nodes, Elements   =     32405    173590
AFLR3 GG : Nodes, Elements   =     32405    173285
AFLR3 GG : Nodes, Elements   =     33780    177430
AFLR3 GG : Nodes, Elements   =     33780    183224
AFLR3 GG : Nodes, Elements   =     33780    181755
AFLR3 GG : Nodes, Elements   =     33780    181476
AFLR3 GG : Nodes, Elements   =     35079    185397
AFLR3 GG : Nodes, Elements   =     35079    190895
AFLR3 GG : Nodes, Elements   =     35079    189447
AFLR3 GG : Nodes, Elements   =     35079    189199
AFLR3 GG : Nodes, Elements   =     36329    192971
AFLR3 GG : Nodes, Elements   =     36329    198346
AFLR3 GG : Nodes, Elements   =     36329    196915
AFLR3 GG : Nodes, Elements   =     36329    196673
AFLR3 GG : Nodes, Elements   =     37476    200134
AFLR3 GG : Nodes, Elements   =     37476    204990
AFLR3 GG : Nodes, Elements   =     37476    203770
AFLR3 GG : Nodes, Elements   =     37476    203524
AFLR3 GG : Nodes, Elements   =     38613    206952
AFLR3 GG : Nodes, Elements   =     38613    211807
AFLR3 GG : Nodes, Elements   =     38613    210525
AFLR3 GG : Nodes, Elements   =     38613    210316
AFLR3 GG : Nodes, Elements   =     39698    213589
AFLR3 GG : Nodes, Elements   =     39698    218183
AFLR3 GG : Nodes, Elements   =     39698    216999
AFLR3 GG : Nodes, Elements   =     39698    216798
AFLR3 GG : Nodes, Elements   =     40722    219880
AFLR3 GG : Nodes, Elements   =     40722    224289
AFLR3 GG : Nodes, Elements   =     40722    223146
AFLR3 GG : Nodes, Elements   =     40722    222914
AFLR3 GG : Nodes, Elements   =     41692    225847
AFLR3 GG : Nodes, Elements   =     41692    229994
AFLR3 GG : Nodes, Elements   =     41692    228881
AFLR3 GG : Nodes, Elements   =     41692    228678
AFLR3 GG : Nodes, Elements   =     42632    231517
AFLR3 GG : Nodes, Elements   =     42632    235510
AFLR3 GG : Nodes, Elements   =     42632    234465
AFLR3 GG : Nodes, Elements   =     42632    234274
AFLR3 GG : Nodes, Elements   =     43525    236967
AFLR3 GG : Nodes, Elements   =     43525    240785
AFLR3 GG : Nodes, Elements   =     43525    239799
AFLR3 GG : Nodes, Elements   =     43525    239632
AFLR3 GG : Nodes, Elements   =     44366    242171
AFLR3 GG : Nodes, Elements   =     44366    245783
AFLR3 GG : Nodes, Elements   =     44366    244832
AFLR3 GG : Nodes, Elements   =     44366    244673
AFLR3 GG : Nodes, Elements   =     45212    247225
AFLR3 GG : Nodes, Elements   =     45212    250840
AFLR3 GG : Nodes, Elements   =     45212    249921
AFLR3 GG : Nodes, Elements   =     45212    249733
AFLR3 GG : Nodes, Elements   =     46019    252159
AFLR3 GG : Nodes, Elements   =     46019    255571
AFLR3 GG : Nodes, Elements   =     46019    254706
AFLR3 GG : Nodes, Elements   =     46019    254531
AFLR3 GG : Nodes, Elements   =     46782    256832
AFLR3 GG : Nodes, Elements   =     46782    260007
AFLR3 GG : Nodes, Elements   =     46782    259193
AFLR3 GG : Nodes, Elements   =     46782    259050
AFLR3 GG : Nodes, Elements   =     47515    261256
AFLR3 GG : Nodes, Elements   =     47515    264385
AFLR3 GG : Nodes, Elements   =     47515    263599
AFLR3 GG : Nodes, Elements   =     47515    263462
AFLR3 GG : Nodes, Elements   =     48219    265591
AFLR3 GG : Nodes, Elements   =     48219    268520
AFLR3 GG : Nodes, Elements   =     48219    267779
AFLR3 GG : Nodes, Elements   =     48219    267634
AFLR3 GG : Nodes, Elements   =     48868    269588
AFLR3 GG : Nodes, Elements   =     48868    272401
AFLR3 GG : Nodes, Elements   =     48868    271655
AFLR3 GG : Nodes, Elements   =     48868    271521
AFLR3 GG : Nodes, Elements   =     49496    273408
AFLR3 GG : Nodes, Elements   =     49496    276093
AFLR3 GG : Nodes, Elements   =     49496    275400
AFLR3 GG : Nodes, Elements   =     49496    275273
AFLR3 GG : Nodes, Elements   =     50132    277186
AFLR3 GG : Nodes, Elements   =     50132    279854
AFLR3 GG : Nodes, Elements   =     50132    279158
AFLR3 GG : Nodes, Elements   =     50132    279016
AFLR3 GG : Nodes, Elements   =     50722    280790
AFLR3 GG : Nodes, Elements   =     50722    283311
AFLR3 GG : Nodes, Elements   =     50722    282683
AFLR3 GG : Nodes, Elements   =     50722    282569
AFLR3 GG : Nodes, Elements   =     51297    284306
AFLR3 GG : Nodes, Elements   =     51297    286734
AFLR3 GG : Nodes, Elements   =     51297    286091
AFLR3 GG : Nodes, Elements   =     51297    285960
AFLR3 GG : Nodes, Elements   =     51844    287606
AFLR3 GG : Nodes, Elements   =     51844    289979
AFLR3 GG : Nodes, Elements   =     51844    289361
AFLR3 GG : Nodes, Elements   =     51844    289242
AFLR3 GG : Nodes, Elements   =     52368    290818
AFLR3 GG : Nodes, Elements   =     52368    293059
AFLR3 GG : Nodes, Elements   =     52368    292486
AFLR3 GG : Nodes, Elements   =     52368    292373
AFLR3 GG : Nodes, Elements   =     52915    294020
AFLR3 GG : Nodes, Elements   =     52915    296322
AFLR3 GG : Nodes, Elements   =     52915    295765
AFLR3 GG : Nodes, Elements   =     52915    295629
AFLR3 GG : Nodes, Elements   =     53422    297154
AFLR3 GG : Nodes, Elements   =     53422    299240
AFLR3 GG : Nodes, Elements   =     53422    298743
AFLR3 GG : Nodes, Elements   =     53422    298637
AFLR3 GG : Nodes, Elements   =     53905    300091
AFLR3 GG : Nodes, Elements   =     53905    302157
AFLR3 GG : Nodes, Elements   =     53905    301625
AFLR3 GG : Nodes, Elements   =     53905    301517
AFLR3 GG : Nodes, Elements   =     54391    302978
AFLR3 GG : Nodes, Elements   =     54391    305036
AFLR3 GG : Nodes, Elements   =     54391    304505
AFLR3 GG : Nodes, Elements   =     54391    304418
AFLR3 GG : Nodes, Elements   =     54858    305820
AFLR3 GG : Nodes, Elements   =     54858    307759
AFLR3 GG : Nodes, Elements   =     54858    307291
AFLR3 GG : Nodes, Elements   =     54858    307211
AFLR3 GG : Nodes, Elements   =     55329    308626
AFLR3 GG : Nodes, Elements   =     55329    310589
AFLR3 GG : Nodes, Elements   =     55329    310096
AFLR3 GG : Nodes, Elements   =     55329    309998
AFLR3 GG : Nodes, Elements   =     55782    311357
AFLR3 GG : Nodes, Elements   =     55782    313295
AFLR3 GG : Nodes, Elements   =     55782    312764
AFLR3 GG : Nodes, Elements   =     55782    312661
AFLR3 GG : Nodes, Elements   =     56186    313876
AFLR3 GG : Nodes, Elements   =     56186    315608
AFLR3 GG : Nodes, Elements   =     56186    315151
AFLR3 GG : Nodes, Elements   =     56186    315085
AFLR3 GG : Nodes, Elements   =     56544    316160
AFLR3 GG : Nodes, Elements   =     56544    317734
AFLR3 GG : Nodes, Elements   =     56544    317296
AFLR3 GG : Nodes, Elements   =     56544    317198
AFLR3 GG : Nodes, Elements   =     56846    318106
AFLR3 GG : Nodes, Elements   =     56846    319464
AFLR3 GG : Nodes, Elements   =     56846    319071
AFLR3 GG : Nodes, Elements   =     56846    318991
AFLR3 GG : Nodes, Elements   =     57102    319761
AFLR3 GG : Nodes, Elements   =     57102    320905
AFLR3 GG : Nodes, Elements   =     57102    320579
AFLR3 GG : Nodes, Elements   =     57102    320508
AFLR3 GG : Nodes, Elements   =     57309    321130
AFLR3 GG : Nodes, Elements   =     57309    322085
AFLR3 GG : Nodes, Elements   =     57309    321780
AFLR3 GG : Nodes, Elements   =     57309    321722
AFLR3 GG : Nodes, Elements   =     57479    322233
AFLR3 GG : Nodes, Elements   =     57479    323050
AFLR3 GG : Nodes, Elements   =     57479    322789
AFLR3 GG : Nodes, Elements   =     57479    322708
AFLR3 GG : Nodes, Elements   =     57600    323071
AFLR3 GG : Nodes, Elements   =     57600    323642
AFLR3 GG : Nodes, Elements   =     57600    323464
AFLR3 GG : Nodes, Elements   =     57600    323424
AFLR3 GG : Nodes, Elements   =     57703    323733
AFLR3 GG : Nodes, Elements   =     57703    324242
AFLR3 GG : Nodes, Elements   =     57703    324072
AFLR3 GG : Nodes, Elements   =     57703    324030
AFLR3 GG : Nodes, Elements   =     57778    324257
AFLR3 GG : Nodes, Elements   =     57778    324643
AFLR3 GG : Nodes, Elements   =     57778    324499
AFLR3 GG : Nodes, Elements   =     57778    324471
AFLR3 GG : Nodes, Elements   =     57851    324690
AFLR3 GG : Nodes, Elements   =     57851    325062
AFLR3 GG : Nodes, Elements   =     57851    324933
AFLR3 GG : Nodes, Elements   =     57851    324909
AFLR3 GG : Nodes, Elements   =     57904    325069
AFLR3 GG : Nodes, Elements   =     57904    325333
AFLR3 GG : Nodes, Elements   =     57904    325251
AFLR3 GG : Nodes, Elements   =     57904    325221
AFLR3 GG : Nodes, Elements   =     57949    325356
AFLR3 GG : Nodes, Elements   =     57949    325584
AFLR3 GG : Nodes, Elements   =     57949    325504
AFLR3 GG : Nodes, Elements   =     57949    325485
AFLR3 GG : Nodes, Elements   =     57985    325594
AFLR3 GG : Nodes, Elements   =     57985    325778
AFLR3 GG : Nodes, Elements   =     57985    325705
AFLR3 GG : Nodes, Elements   =     57985    325688
AFLR3 GG : Nodes, Elements   =     58001    325736
AFLR3 GG : Nodes, Elements   =     58001    325828
AFLR3 GG : Nodes, Elements   =     58001    325788
AFLR3 GG : Nodes, Elements   =     58001    325774
AFLR3 GG : Nodes, Elements   =     58009    325798
AFLR3 GG : Nodes, Elements   =     58009    325847
AFLR3 GG : Nodes, Elements   =     58009    325826
AFLR3 GG : Nodes, Elements   =     58009    325818
AFLR3 GG : Nodes, Elements   =     58020    325851
AFLR3 GG : Nodes, Elements   =     58020    325936
AFLR3 GG : Nodes, Elements   =     58020    325892
AFLR3 GG : Nodes, Elements   =     58020    325885
AFLR3 GG : Nodes, Elements   =     58026    325903
AFLR3 GG : Nodes, Elements   =     58026    325935
AFLR3 GG : Nodes, Elements   =     58026    325917
AFLR3 GG : Nodes, Elements   =     58026    325914
AFLR3 GG : Nodes, Elements   =     58027    325917
AFLR3 GG : Nodes, Elements   =     58027    325927
AFLR3 GG : Nodes, Elements   =     58027    325921
AFLR3 GG : Nodes, Elements   =     58027    325920
AFLR3 GG : Nodes, Elements   =     58036    325947
AFLR3 GG : Nodes, Elements   =     58036    325999
AFLR3 GG : Nodes, Elements   =     58036    325971
AFLR3 GG : Nodes, Elements   =     58036    325968
AFLR3 GG : Nodes, Elements   =     58039    325977
AFLR3 GG : Nodes, Elements   =     58039    325996
AFLR3 GG : Nodes, Elements   =     58039    325987
AFLR3 GG : Nodes, Elements   =     58039    325985
 
AFLR3    : CPU Time          =     1.750   seconds
 
AFLR3 QI : QUALITY IMPROVEMENT
 
AFLR3 QI : Nodes, Elements   =     58039    325985
AFLR3 QI : Nodes, Elements   =     56680    318324
AFLR3 QI : Nodes, Elements   =     56461    317092
AFLR3 QI : Nodes, Elements   =     56451    317038
AFLR3 QI : Nodes, Elements   =     56451    320862
AFLR3 QI : Nodes, Elements   =     56451    316961
AFLR3 QI : Nodes, Elements   =     56451    316386
AFLR3 QI : Nodes, Elements   =     56451    319172
AFLR3 QI : Nodes, Elements   =     56451    316595
AFLR3 QI : Nodes, Elements   =     56451    316339
AFLR3 QI : Nodes, Elements   =     56451    317390
AFLR3 QI : Nodes, Elements   =     56451    316353
AFLR3 QI : Nodes, Elements   =     56451    316100
AFLR3 QI : Nodes, Elements   =     56451    317003
AFLR3 QI : Nodes, Elements   =     56451    316235
AFLR3 QI : Nodes, Elements   =     56451    316055
AFLR3 QI : Nodes, Elements   =     56451    316917
AFLR3 QI : Nodes, Elements   =     56451    316196
AFLR3 QI : Nodes, Elements   =     56451    316021
AFLR3 QI : Nodes, Elements   =     56451    315999
AFLR3 QI : Nodes, Elements   =     56466    316064
AFLR3 QI : Nodes, Elements   =     56466    316885
AFLR3 QI : Nodes, Elements   =     56466    316214
AFLR3 QI : Nodes, Elements   =     56466    316073
AFLR3 QI : Nodes, Elements   =     56466    316859
AFLR3 QI : Nodes, Elements   =     56466    316205
AFLR3 QI : Nodes, Elements   =     56466    316062
 
AFLR3    : CPU Time          =     0.609   seconds
 
AFLR3 QRG: QUALITY GRID RE-GENERATION
 
AFLR3 QRG: Nodes, Elements   =     56466    316062
AFLR3 QRG: Nodes, Elements   =     56471    316086
AFLR3 QRG: Nodes, Elements   =     56497    316220
AFLR3 QRG: Nodes, Elements   =     56501    316237
AFLR3 QRG: Nodes, Elements   =     56504    316251
 
AFLR3    : CPU Time          =     0.024   seconds
 
AFLR3    : DONE
 
ANBL3 BLM: BL VOLUME GRID MERGE
 
ANBL3 BLM: Nodes, Elements   =     56504    316251
 
UG3      : OUTPUT GRID
 
UG3      : Grid File Name    = .tmp.b8.ugrid
UG3      : Quad Surface Faces=         0
UG3      : Tria Surface Faces=     13288
UG3      : Nodes             =    109886
UG3      : Total Elements    =    425661
UG3      : Hex Elements      =         0
UG3      : Pent_5 Elements   =      2793
UG3      : Pent_6 Elements   =    104033
UG3      : Tet Elements      =    318835
 
ANBL3 BLM: Nodes, Elements   =    109886    636520
ANBL3 BLM: Nodes, Elements   =    109886      2584
 
ANBL3    : CPU Time          =     0.064   seconds
 
ANBL3    : DONE

OVERALL  : CPU Time          =     5.087   seconds

UG3      : DIHEDRAL ANGLE CHECK

UG3      : No. Tet Elems     =    318835
UG3      : Min, Max Ang      =    0.8537     178.7
UG3      : Average Angle     =      70.1
UG3      : No. Angle&gt;160.0   =       293
UG3      : No. Angle&gt;179.9   =         0

UG3      : No. Pyramid Elems =      2793
UG3      : Min, Max Ang      =     7.032     171.7
UG3      : Average Angle     =      82.6
UG3      : No. Angle&gt;160.0   =        56
UG3      : No. Angle&gt;179.9   =         0

UG3      : No. Prism Elems   =    104033
UG3      : Min, Max Ang      =     6.792     174.6
UG3      : Average Angle     =      80.1
UG3      : No. Angle&gt;160.0   =       561
UG3      : No. Angle&gt;179.9   =         0

UG3      : VOL CHECK

UG3      : Total-Volume      =  5.96e+10

UG3      : No. Tet Elems     =    318835
UG3      : Min Vol           =  0.000481
UG3      : Average Vol       =  1.87e+05
UG3      : Total-Tet-Vol     =  5.96e+10
UG3      : No. Vol&lt;TOL       =         0

UG3      : No. Pyramid Elems =      2793
UG3      : Min Vol           =    0.0167
UG3      : Average Vol       =      0.25
UG3      : Total-Pyramid-Vol =       699
UG3      : No. Vol&lt;TOL       =         0

UG3      : No. Prism Elems   =    104033
UG3      : Min Vol           =    0.0144
UG3      : Average Vol       =      0.37
UG3      : Total-Prism-Vol   =  3.84e+04
UG3      : No. Vol&lt;TOL       =         0

UG3      : Q VOL-LENGTH-RATIO CHECK
                      2/3        2
UG3      : Q = c * Vol   / sum( L  )
UG3      : 0 &lt;= Q &lt;= 1
UG3      : Note that L includes scaling for BL-aspect=ratio

UG3      : No. Tet Elems     =    318835
UG3      : Min, Max Q        =    0.0647         1
UG3      : Average Q         =     0.851
UG3      : No. Q&lt;       0.1  =        24
UG3      : No. Q&lt;      0.01  =         0

UG3      : No. Pyramid Elems =      2793
UG3      : Min, Max Q        =      0.26         1
UG3      : Average Q         =     0.792
UG3      : No. Q&lt;       0.1  =         0
UG3      : No. Q&lt;      0.01  =         0

UG3      : No. Prism Elems   =    104033
UG3      : Min, Max Q        =     0.279         1
UG3      : Average Q         =     0.902
UG3      : No. Q&lt;       0.1  =         0
UG3      : No. Q&lt;      0.01  =         0

UG3      : CPU Time          =     0.000   seconds

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.8.1
EGADS    : ---------------------------------------

EGADS    : CREATE EGADS TESS FROM AFLR3 DATA

EGADS    : CREATING TESSELLATION FOR BODY 0 EDGE 1
EGADS    : CREATING TESSELLATION FOR BODY 0 EDGE 2
EGADS    : CREATING TESSELLATION FOR BODY 0 EDGE 3
EGADS    : CREATING TESSELLATION FOR BODY 0 EDGE 4
EGADS    : CREATING TESSELLATION FOR BODY 0 EDGE 5
EGADS    : CREATING TESSELLATION FOR BODY 0 EDGE 6
EGADS    : CREATING TESSELLATION FOR BODY 0 EDGE 7
EGADS    : CREATING TESSELLATION FOR BODY 0 EDGE 8

EGADS    : CREATING TESSELLATION FOR BODY 0 FACE 1
EGADS    : CREATING TESSELLATION FOR BODY 0 FACE 2
EGADS    : CREATING TESSELLATION FOR BODY 0 FACE 3
EGADS    : CREATING TESSELLATION FOR BODY 0 FACE 4

EGADS    : CREATING TESSELLATION FOR BODY 1 EDGE 9
EGADS    : CREATING TESSELLATION FOR BODY 1 EDGE 10
EGADS    : CREATING TESSELLATION FOR BODY 1 EDGE 11
EGADS    : CREATING TESSELLATION FOR BODY 1 EDGE 12
EGADS    : CREATING TESSELLATION FOR BODY 1 EDGE 13
EGADS    : CREATING TESSELLATION FOR BODY 1 EDGE 14
EGADS    : CREATING TESSELLATION FOR BODY 1 EDGE 15
EGADS    : CREATING TESSELLATION FOR BODY 1 EDGE 16

EGADS    : CREATING TESSELLATION FOR BODY 1 FACE 5
EGADS    : CREATING TESSELLATION FOR BODY 1 FACE 6
EGADS    : CREATING TESSELLATION FOR BODY 1 FACE 7
EGADS    : CREATING TESSELLATION FOR BODY 1 FACE 8

EGADS    : CREATING TESSELLATION FOR BODY 2 EDGE 17
EGADS    : CREATING TESSELLATION FOR BODY 2 EDGE 18
EGADS    : CREATING TESSELLATION FOR BODY 2 EDGE 19
EGADS    : CREATING TESSELLATION FOR BODY 2 EDGE 20
EGADS    : CREATING TESSELLATION FOR BODY 2 EDGE 21
EGADS    : CREATING TESSELLATION FOR BODY 2 EDGE 22
EGADS    : CREATING TESSELLATION FOR BODY 2 EDGE 23
EGADS    : CREATING TESSELLATION FOR BODY 2 EDGE 24
EGADS    : CREATING TESSELLATION FOR BODY 2 EDGE 25
EGADS    : CREATING TESSELLATION FOR BODY 2 EDGE 26
EGADS    : CREATING TESSELLATION FOR BODY 2 EDGE 27
EGADS    : CREATING TESSELLATION FOR BODY 2 EDGE 28
EGADS    : CREATING TESSELLATION FOR BODY 2 EDGE 29
EGADS    : CREATING TESSELLATION FOR BODY 2 EDGE 30
EGADS    : CREATING TESSELLATION FOR BODY 2 EDGE 31
EGADS    : CREATING TESSELLATION FOR BODY 2 EDGE 32
EGADS    : CREATING TESSELLATION FOR BODY 2 EDGE 33
EGADS    : CREATING TESSELLATION FOR BODY 2 EDGE 34

EGADS    : CREATING TESSELLATION FOR BODY 2 FACE 9
EGADS    : CREATING TESSELLATION FOR BODY 2 FACE 10
EGADS    : CREATING TESSELLATION FOR BODY 2 FACE 11
EGADS    : CREATING TESSELLATION FOR BODY 2 FACE 12
EGADS    : CREATING TESSELLATION FOR BODY 2 FACE 13
EGADS    : CREATING TESSELLATION FOR BODY 2 FACE 14
EGADS    : CREATING TESSELLATION FOR BODY 2 FACE 15
EGADS    : CREATING TESSELLATION FOR BODY 2 FACE 16
EGADS    : CREATING TESSELLATION FOR BODY 2 FACE 17
EGADS    : CREATING TESSELLATION FOR BODY 2 FACE 18

EGADS    : CREATING TESSELLATION FOR BODY 3 EDGE 35
EGADS    : CREATING TESSELLATION FOR BODY 3 EDGE 36
EGADS    : CREATING TESSELLATION FOR BODY 3 EDGE 37
EGADS    : CREATING TESSELLATION FOR BODY 3 EDGE 38
EGADS    : CREATING TESSELLATION FOR BODY 3 EDGE 39
EGADS    : CREATING TESSELLATION FOR BODY 3 EDGE 40
EGADS    : CREATING TESSELLATION FOR BODY 3 EDGE 41
EGADS    : CREATING TESSELLATION FOR BODY 3 EDGE 42
EGADS    : CREATING TESSELLATION FOR BODY 3 EDGE 43
EGADS    : CREATING TESSELLATION FOR BODY 3 EDGE 44
EGADS    : CREATING TESSELLATION FOR BODY 3 EDGE 45
EGADS    : CREATING TESSELLATION FOR BODY 3 EDGE 46

EGADS    : CREATING TESSELLATION FOR BODY 3 FACE 19
EGADS    : CREATING TESSELLATION FOR BODY 3 FACE 20
EGADS    : CREATING TESSELLATION FOR BODY 3 FACE 21
EGADS    : CREATING TESSELLATION FOR BODY 3 FACE 22
EGADS    : CREATING TESSELLATION FOR BODY 3 FACE 23
EGADS    : CREATING TESSELLATION FOR BODY 3 FACE 24

EGADS    : EGADS TESS CREATED

EGADS    : CHECK TESS FACE NODE MAP

EGADS    : CHECKING NODE MAP FOR BODY 0 FACE 1
EGADS    : CHECKING NODE MAP FOR BODY 0 FACE 2
EGADS    : CHECKING NODE MAP FOR BODY 0 FACE 3
EGADS    : CHECKING NODE MAP FOR BODY 0 FACE 4
EGADS    : CHECKING NODE MAP FOR BODY 1 FACE 5
EGADS    : CHECKING NODE MAP FOR BODY 1 FACE 6
EGADS    : CHECKING NODE MAP FOR BODY 1 FACE 7
EGADS    : CHECKING NODE MAP FOR BODY 1 FACE 8
EGADS    : CHECKING NODE MAP FOR BODY 2 FACE 9
EGADS    : CHECKING NODE MAP FOR BODY 2 FACE 10
EGADS    : CHECKING NODE MAP FOR BODY 2 FACE 11
EGADS    : CHECKING NODE MAP FOR BODY 2 FACE 12
EGADS    : CHECKING NODE MAP FOR BODY 2 FACE 13
EGADS    : CHECKING NODE MAP FOR BODY 2 FACE 14
EGADS    : CHECKING NODE MAP FOR BODY 2 FACE 15
EGADS    : CHECKING NODE MAP FOR BODY 2 FACE 16
EGADS    : CHECKING NODE MAP FOR BODY 2 FACE 17
EGADS    : CHECKING NODE MAP FOR BODY 2 FACE 18
EGADS    : CHECKING NODE MAP FOR BODY 3 FACE 19
EGADS    : CHECKING NODE MAP FOR BODY 3 FACE 20
EGADS    : CHECKING NODE MAP FOR BODY 3 FACE 21
EGADS    : CHECKING NODE MAP FOR BODY 3 FACE 22
EGADS    : CHECKING NODE MAP FOR BODY 3 FACE 23
EGADS    : CHECKING NODE MAP FOR BODY 3 FACE 24
Volume mesh:
	Number of nodes          = 109886
	Number of elements       = 438949
	Number of triangles      = 13288
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 318835
	Number of pyramids       = 2793
	Number of prisms         = 104033
	Number of hexahedrals    = 0

Writing vtk file ....

Writing vtk general file ....
Finished writing vtk file


real	0m7.574s
user	0m7.144s
sys	0m0.710s
+ status=0
+ set +x

=================================================
data/session07/11_aflr4_aflr3_ViscousWingPod.py passed (as expected)
=================================================


=================================================
12_aflr4_aflr3_ViscousTransport.py test;
+ python 12_aflr4_aflr3_ViscousTransport.py
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/CAPS/training/2023/training.log

MESSAGE:: Building wingOml


MESSAGE:: Building wingHinges


MESSAGE:: Building pylonOml


MESSAGE:: Building nacelleOml


MESSAGE:: Building htailOml


MESSAGE:: Building htailHinges


MESSAGE:: Building vtailOml


MESSAGE:: Building vtailHinges


MESSAGE:: Building fuseOml

Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 8
	Name = Fuselage, index = 1
	Name = Wing, index = 2
	Name = Htail, index = 3
	Name = Pylon, index = 4
	Name = Vtail, index = 5
	Name = Nacelle, index = 6
	Name = Control, index = 7
	Name = Farfield, index = 8
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 9
	Name = Fuselage, index = 1
	Name = riteWing, index = 2
	Name = leftWing, index = 3
	Name = Htail, index = 4
	Name = Pylon, index = 5
	Name = Vtail, index = 6
	Name = Nacelle, index = 7
	Name = Control, index = 8
	Name = Farfield, index = 9

Getting mesh sizing parameters
	Mesh sizing name - Farfield
	Done getting mesh sizing parameters
 
AFLR2    : ---------------------------------------
AFLR2    : AFLR2 LIBRARY
AFLR2    : ADVANCING-FRONT/LOCAL-RECONNECTION
AFLR2    : TRIA/QUAD GRID GENERATOR
AFLR2    : Version Number 9.18.1
AFLR2    : Version Date   06/11/24 @ 05:52PM
AFLR2    : Compile OS     Darwin 23.5.0 arm64
AFLR2    : Compile Date   06/11/24 @ 05:52PM
AFLR2    : Copyright 1994-2021, D.L. Marcum
AFLR2    : ---------------------------------------
 
AFLR4    : ---------------------------------------
AFLR4    : AFLR4 LIBRARY
AFLR4    : ADVANCING-FRONT/LOCAL-RECONNECTION
AFLR4    : TRIA/QUAD SURFACE GRID GENERATOR
AFLR4    : Version Number 11.5.15
AFLR4    : Version Date   07/19/24 @ 07:04PM
AFLR4    : Compile OS     Darwin 23.5.0 arm64
AFLR4    : Compile Date   07/19/24 @ 07:06PM
AFLR4    : Copyright 1994-2021, D.L. Marcum
AFLR4    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.8.1
EGADS    : ---------------------------------------

EGADS    : EGADS CAD Geometry Setup

EGADS    : Model has 11 Active Bodies

EGADS    : Body 0 is a SolidBody
EGADS    : Body 0 has 1 Shells
EGADS    : Body 0 has 67 Faces
EGADS    : Body 0 has 176 Edges
EGADS    : Body 0 has 71 Loops
EGADS    : Body 0 has 107 Nodes
EGADS    : Body 1 is a SolidBody
EGADS    : Body 1 has 1 Shells
EGADS    : Body 1 has 5 Faces
EGADS    : Body 1 has 9 Edges
EGADS    : Body 1 has 5 Loops
EGADS    : Body 1 has 6 Nodes
EGADS    : Body 2 is a SolidBody
EGADS    : Body 2 has 1 Shells
EGADS    : Body 2 has 5 Faces
EGADS    : Body 2 has 9 Edges
EGADS    : Body 2 has 5 Loops
EGADS    : Body 2 has 6 Nodes
EGADS    : Body 3 is a SolidBody
EGADS    : Body 3 has 1 Shells
EGADS    : Body 3 has 5 Faces
EGADS    : Body 3 has 9 Edges
EGADS    : Body 3 has 5 Loops
EGADS    : Body 3 has 6 Nodes
EGADS    : Body 4 is a SolidBody
EGADS    : Body 4 has 1 Shells
EGADS    : Body 4 has 5 Faces
EGADS    : Body 4 has 9 Edges
EGADS    : Body 4 has 5 Loops
EGADS    : Body 4 has 6 Nodes
EGADS    : Body 5 is a SolidBody
EGADS    : Body 5 has 1 Shells
EGADS    : Body 5 has 5 Faces
EGADS    : Body 5 has 9 Edges
EGADS    : Body 5 has 5 Loops
EGADS    : Body 5 has 6 Nodes
EGADS    : Body 6 is a SolidBody
EGADS    : Body 6 has 1 Shells
EGADS    : Body 6 has 5 Faces
EGADS    : Body 6 has 9 Edges
EGADS    : Body 6 has 5 Loops
EGADS    : Body 6 has 6 Nodes
EGADS    : Body 7 is a SolidBody
EGADS    : Body 7 has 1 Shells
EGADS    : Body 7 has 5 Faces
EGADS    : Body 7 has 9 Edges
EGADS    : Body 7 has 5 Loops
EGADS    : Body 7 has 6 Nodes
EGADS    : Body 8 is a SolidBody
EGADS    : Body 8 has 1 Shells
EGADS    : Body 8 has 5 Faces
EGADS    : Body 8 has 9 Edges
EGADS    : Body 8 has 5 Loops
EGADS    : Body 8 has 6 Nodes
EGADS    : Body 9 is a SolidBody
EGADS    : Body 9 has 1 Shells
EGADS    : Body 9 has 5 Faces
EGADS    : Body 9 has 9 Edges
EGADS    : Body 9 has 5 Loops
EGADS    : Body 9 has 6 Nodes
EGADS    : Body 10 is a SolidBody
EGADS    : Body 10 has 1 Shells
EGADS    : Body 10 has 6 Faces
EGADS    : Body 10 has 12 Edges
EGADS    : Body 10 has 6 Loops
EGADS    : Body 10 has 8 Nodes

EGADS    : Check Grid BCs

EGADS    : Grid BCs are OK

EGADS    : Face Neighbor-Faces Information

EGADS    : QC  = Face Quad Combination Flag
EGADS    : IER = Face Isolated Edge Refinement Flag
EGADS    : ER  = Face Edge Refinement Factor
EGADS    :       Not applicable for Faces with a FarField Grid BC.
EGADS    : SF  = Face Scale Factor
EGADS    :       Not applicable for Faces with a FarField Grid BC.

EGADS    :   Face          Body    QC   IER       ER    Scale   Neighbor
EGADS    :     ID  Active    ID  Flag  Flag   Weight   Factor   Faces
EGADS    :      1     Yes     0     0     1        0        1   2 3 4 5 6
EGADS    :      2     Yes     0     0     1        0        1   1 7 8 9 10
EGADS    :      3     Yes     0     0     1        0        1   1 8 11 12 13 14
EGADS    :      4     Yes     0     0     1        0        1   1 7 12
EGADS    :      5     Yes     0     0     1        0        1   1 6 15 16 17 18
EGADS    :      6     Yes     0     0     1        0        1   1 5 15 16 17 19
EGADS    :                                                      20 21
EGADS    :      7     Yes     0     0     1        0        1   2 4 22
EGADS    :      8     Yes     0     0     1        0        1   2 3 11 22 23 24
EGADS    :      9     Yes     0     0     1        0        1   2 10 25 26 27 28
EGADS    :                                                      29 30
EGADS    :     10     Yes     0     0     1        0        1   2 9 26 27 28 31
EGADS    :     11     Yes     0     0     1        0        1   3 8 12 22
EGADS    :     12     Yes     0     0     1        0        1   3 4 11 13 14 22
EGADS    :                                                      32
EGADS    :     13     Yes     0     0     1        0        1   3 12 14 33 34 35
EGADS    :                                                      36
EGADS    :     14     Yes     0     0     1        0        1   3 12 13 33 34 35
EGADS    :                                                      36
EGADS    :     15     Yes     0     0     1        0        1   5 6 16
EGADS    :     16     Yes     0     0     1        0        1   5 6 15 17
EGADS    :     17     Yes     0     0     1        0        1   5 6 16
EGADS    :     18     Yes     0     0     1        0        1   5 19 37 38 39 40
EGADS    :                                                      41 42 43
EGADS    :     19     Yes     0     0     1        0        1   6 18 37 38 39 40
EGADS    :                                                      41 42 43
EGADS    :     20     Yes     0     0     1        0        1   6 21 44
EGADS    :     21     Yes     0     0     1        0        1   6 20 45
EGADS    :     22     Yes     0     0     1        0        1   7 8 11 12 23 24
EGADS    :                                                      46
EGADS    :     23     Yes     0     0     1        0        1   8 22 24 47 48 49
EGADS    :                                                      50
EGADS    :     24     Yes     0     0     1        0        1   8 22 23 47 48 49
EGADS    :                                                      50
EGADS    :     25     Yes     0     0     1        0        1   9 31 51 52 53 54
EGADS    :                                                      55 56 57
EGADS    :     26     Yes     0     0     1        0        1   9 10 27
EGADS    :     27     Yes     0     0     1        0        1   9 10 26 28
EGADS    :     28     Yes     0     0     1        0        1   9 10 27
EGADS    :     29     Yes     0     0     1        0        1   9 30 58
EGADS    :     30     Yes     0     0     1        0        1   9 29 59
EGADS    :     31     Yes     0     0     1        0        1   10 25 51 52 53
EGADS    :                                                      54 55 56 57
EGADS    :     32     Yes     0     0     1        0        1   12 46 60 61 62
EGADS    :                                                      63
EGADS    :     33     Yes     0     0     1        0        1   13 14 34
EGADS    :     34     Yes     0     0     1        0        1   13 14 33 35
EGADS    :     35     Yes     0     0     1        0        1   13 14 34
EGADS    :     36     Yes     0     0     1        0        1   13 14
EGADS    :     37     Yes     0     0     1        0        1   18 19 38
EGADS    :     38     Yes     0     0     1        0        1   18 19 37 39
EGADS    :     39     Yes     0     0     1        0        1   18 19 38
EGADS    :     40     Yes     0     0     1        0        1   18 19 41
EGADS    :     41     Yes     0     0     1        0        1   18 19 40 42
EGADS    :     42     Yes     0     0     1        0        1   18 19 41
EGADS    :     43     Yes     0     0     1        0        1   18 19
EGADS    :     44     Yes     0     0     1        0        1   20 45 64
EGADS    :     45     Yes     0     0     1        0        1   21 44 65
EGADS    :     46     Yes     0     0     1        0        1   22 32 60 61 62
EGADS    :                                                      63
EGADS    :     47     Yes     0     0     1        0        1   23 24
EGADS    :     48     Yes     0     0     1        0        1   23 24 49
EGADS    :     49     Yes     0     0     1        0        1   23 24 48 50
EGADS    :     50     Yes     0     0     1        0        1   23 24 49
EGADS    :     51     Yes     0     0     1        0        1   25 31
EGADS    :     52     Yes     0     0     1        0        1   25 31 53
EGADS    :     53     Yes     0     0     1        0        1   25 31 52 54
EGADS    :     54     Yes     0     0     1        0        1   25 31 53
EGADS    :     55     Yes     0     0     1        0        1   25 31 56
EGADS    :     56     Yes     0     0     1        0        1   25 31 55 57
EGADS    :     57     Yes     0     0     1        0        1   25 31 56
EGADS    :     58     Yes     0     0     1        0        1   29 59 66
EGADS    :     59     Yes     0     0     1        0        1   30 58 67
EGADS    :     60     Yes     0     0     1        0        1   32 46 61
EGADS    :     61     Yes     0     0     1        0        1   32 46 60 62
EGADS    :     62     Yes     0     0     1        0        1   32 46 61
EGADS    :     63     Yes     0     0     1        0        1   32 46
EGADS    :     64     Yes     0     0     1        0        1   44 65
EGADS    :     65     Yes     0     0     1        0        1   45 64
EGADS    :     66     Yes     0     0     1        0        1   58 67
EGADS    :     67     Yes     0     0     1        0        1   59 66
EGADS    :     68     Yes     1     0     1        0        1   69 70 71 72
EGADS    :     69     Yes     1     0     1        0        1   68 70 72
EGADS    :     70     Yes     1     0     1        0        1   68 69 71 72
EGADS    :     71     Yes     1     0     1        0        1   68 70 72
EGADS    :     72     Yes     1     0     1        0        1   68 69 70 71
EGADS    :     73     Yes     2     0     1        0        1   74 75 76 77
EGADS    :     74     Yes     2     0     1        0        1   73 75 77
EGADS    :     75     Yes     2     0     1        0        1   73 74 76 77
EGADS    :     76     Yes     2     0     1        0        1   73 75 77
EGADS    :     77     Yes     2     0     1        0        1   73 74 75 76
EGADS    :     78     Yes     3     0     1        0        1   79 80 81 82
EGADS    :     79     Yes     3     0     1        0        1   78 80 82
EGADS    :     80     Yes     3     0     1        0        1   78 79 81 82
EGADS    :     81     Yes     3     0     1        0        1   78 80 82
EGADS    :     82     Yes     3     0     1        0        1   78 79 80 81
EGADS    :     83     Yes     4     0     1        0        1   84 85 86 87
EGADS    :     84     Yes     4     0     1        0        1   83 85 86 87
EGADS    :     85     Yes     4     0     1        0        1   83 84 86
EGADS    :     86     Yes     4     0     1        0        1   83 84 85 87
EGADS    :     87     Yes     4     0     1        0        1   83 84 86
EGADS    :     88     Yes     5     0     1        0        1   89 90 91 92
EGADS    :     89     Yes     5     0     1        0        1   88 90 91 92
EGADS    :     90     Yes     5     0     1        0        1   88 89 91
EGADS    :     91     Yes     5     0     1        0        1   88 89 90 92
EGADS    :     92     Yes     5     0     1        0        1   88 89 91
EGADS    :     93     Yes     6     0     1        0        1   94 95 96 97
EGADS    :     94     Yes     6     0     1        0        1   93 95 97
EGADS    :     95     Yes     6     0     1        0        1   93 94 96 97
EGADS    :     96     Yes     6     0     1        0        1   93 95 97
EGADS    :     97     Yes     6     0     1        0        1   93 94 95 96
EGADS    :     98     Yes     7     0     1        0        1   99 100 101 102
EGADS    :     99     Yes     7     0     1        0        1   98 100 101 102
EGADS    :    100     Yes     7     0     1        0        1   98 99 101
EGADS    :    101     Yes     7     0     1        0        1   98 99 100 102
EGADS    :    102     Yes     7     0     1        0        1   98 99 101
EGADS    :    103     Yes     8     0     1        0        1   104 105 106 107
EGADS    :    104     Yes     8     0     1        0        1   103 105 106 107
EGADS    :    105     Yes     8     0     1        0        1   103 104 106
EGADS    :    106     Yes     8     0     1        0        1   103 104 105 107
EGADS    :    107     Yes     8     0     1        0        1   103 104 106
EGADS    :    108     Yes     9     0     1        0        1   109 110 111 112
EGADS    :    109     Yes     9     0     1        0        1   108 110 111 112
EGADS    :    110     Yes     9     0     1        0        1   108 109 111
EGADS    :    111     Yes     9     0     1        0        1   108 109 110 112
EGADS    :    112     Yes     9     0     1        0        1   108 109 111
EGADS    :    113     Yes    10     0     1       NA       NA   115 116 117 118
EGADS    :    114     Yes    10     0     1       NA       NA   115 116 117 118
EGADS    :    115     Yes    10     0     1       NA       NA   113 114 117 118
EGADS    :    116     Yes    10     0     1       NA       NA   113 114 117 118
EGADS    :    117     Yes    10     0     1       NA       NA   113 114 115 116
EGADS    :    118     Yes    10     0     1       NA       NA   113 114 115 116

EGADS    : Face Edges Information

EGADS    :   Face   Edges
EGADS    :      1   -1 4 3 -2 -5 -6
EGADS    :      2   -7 9 1 -8 10 11
EGADS    :      3   -12 2 17 -16 -15 14 -13
EGADS    :      4   -3 18 19 -20
EGADS    :      5   21 -22 23 24 25 26 -27 5
EGADS    :      6   27 28 -25 29 -30 -31 -21 6 32 33
EGADS    :      7   -19 34 7 -35
EGADS    :      8   -36 8 12 -40 -39 38 37
EGADS    :      9   -41 -10 47 46 45 -44 43 -42 48 49
EGADS    :     10   -47 -11 41 -53 -43 -52 -51 50
EGADS    :     11   13 54 55 40
EGADS    :     12   -17 20 60 59 58 -54 -14 -57 -56
EGADS    :     13   61 -62 63 64 65 66 -67 57 15
EGADS    :     14   67 68 -65 69 -70 -71 -61 16 56
EGADS    :     15   31 72 22
EGADS    :     16   30 73 -23 -72
EGADS    :     17   -73 -29 -24
EGADS    :     18   74 -75 76 77 78 -79 80 81 82 83 -84 -26
EGADS    :     19   84 85 -82 86 -87 -88 -78 89 -90 -91 -74 -28
EGADS    :     20   -92 94 -32 -93
EGADS    :     21   -94 95 93 -33
EGADS    :     22   -60 35 36 98 97 39 -55 -58 96
EGADS    :     23   -99 -98 -37 105 104 103 -102 101 -100
EGADS    :     24   -105 -38 -97 99 -109 -101 -108 -107 106
EGADS    :     25   -110 42 120 119 118 -117 116 115 114 -113 112 -111
EGADS    :     26   44 121 52
EGADS    :     27   -45 122 51 -121
EGADS    :     28   -122 -46 -50
EGADS    :     29   123 124 -48 -125
EGADS    :     30   125 -49 -124 -126
EGADS    :     31   -120 53 110 -133 -112 -132 -131 130 -116 -129 -128 127
EGADS    :     32   -134 -59 140 -139 -138 -137 -136 135
EGADS    :     33   71 141 62
EGADS    :     34   70 142 -63 -141
EGADS    :     35   -142 -69 -64
EGADS    :     36   -66 -68
EGADS    :     37   91 143 75
EGADS    :     38   90 144 -76 -143
EGADS    :     39   -144 -89 -77
EGADS    :     40   88 145 79
EGADS    :     41   87 146 -80 -145
EGADS    :     42   -146 -86 -81
EGADS    :     43   -83 -85
EGADS    :     44   147 92 148 149 -150 -151
EGADS    :     45   -147 153 150 -152 -148 -95
EGADS    :     46   -140 -96 134 157 156 -155 138 -154
EGADS    :     47   109 100
EGADS    :     48   102 158 108
EGADS    :     49   -103 159 107 -158
EGADS    :     50   -159 -104 -106
EGADS    :     51   133 111
EGADS    :     52   113 160 132
EGADS    :     53   -114 161 131 -160
EGADS    :     54   -161 -115 -130
EGADS    :     55   117 162 129
EGADS    :     56   -118 163 128 -162
EGADS    :     57   -163 -119 -127
EGADS    :     58   164 -123 165 166 -167 -168
EGADS    :     59   -164 170 167 -169 -165 126
EGADS    :     60   -135 171 -157
EGADS    :     61   136 172 -156 -171
EGADS    :     62   -172 137 155
EGADS    :     63   139 154
EGADS    :     64   -149 173 151 -174
EGADS    :     65   152 174 -153 -173
EGADS    :     66   -166 175 168 -176
EGADS    :     67   169 176 -170 -175
EGADS    :     68   -177 180 179 -178
EGADS    :     69   181 182 177
EGADS    :     70   178 183 -184 -181
EGADS    :     71   -179 -185 -183
EGADS    :     72   -180 -182 184 185
EGADS    :     73   -186 189 188 -187
EGADS    :     74   190 191 186
EGADS    :     75   187 192 -193 -190
EGADS    :     76   -188 -194 -192
EGADS    :     77   -189 -191 193 194
EGADS    :     78   -195 198 197 -196
EGADS    :     79   199 200 195
EGADS    :     80   196 201 -202 -199
EGADS    :     81   -197 -203 -201
EGADS    :     82   -198 -200 202 203
EGADS    :     83   204 -205 -206 207
EGADS    :     84   208 209 -210 -204
EGADS    :     85   211 205 210
EGADS    :     86   -209 212 206 -211
EGADS    :     87   -208 -207 -212
EGADS    :     88   213 -214 -215 216
EGADS    :     89   217 218 -219 -213
EGADS    :     90   220 214 219
EGADS    :     91   -218 221 215 -220
EGADS    :     92   -217 -216 -221
EGADS    :     93   -222 -223 224 225
EGADS    :     94   226 222 227
EGADS    :     95   -228 229 223 -226
EGADS    :     96   -230 -224 -229
EGADS    :     97   -225 230 228 -227
EGADS    :     98   231 234 -233 -232
EGADS    :     99   -231 -237 236 235
EGADS    :    100   238 237 232
EGADS    :    101   233 239 -236 -238
EGADS    :    102   -234 -235 -239
EGADS    :    103   240 -241 -242 243
EGADS    :    104   -240 244 245 -246
EGADS    :    105   247 241 246
EGADS    :    106   -245 248 242 -247
EGADS    :    107   -244 -243 -248
EGADS    :    108   -249 -252 251 250
EGADS    :    109   -253 249 255 -254
EGADS    :    110   256 -255 -250
EGADS    :    111   -251 257 254 -256
EGADS    :    112   252 253 -257
EGADS    :    113   258 259 -260 -261
EGADS    :    114   -262 265 264 -263
EGADS    :    115   266 262 -267 -258
EGADS    :    116   -268 260 269 -264
EGADS    :    117   261 268 -265 -266
EGADS    :    118   -259 267 263 -269

EGADS    : Face Loops Information

EGADS    :   Face   Loops
EGADS    :      1   1 2
EGADS    :      2   3 4
EGADS    :      3   5
EGADS    :      4   6
EGADS    :      5   7
EGADS    :      6   8 9
EGADS    :      7   10
EGADS    :      8   11
EGADS    :      9   12 13
EGADS    :     10   14
EGADS    :     11   15
EGADS    :     12   16
EGADS    :     13   17
EGADS    :     14   18
EGADS    :     15   19
EGADS    :     16   20
EGADS    :     17   21
EGADS    :     18   22
EGADS    :     19   23
EGADS    :     20   24
EGADS    :     21   25
EGADS    :     22   26
EGADS    :     23   27
EGADS    :     24   28
EGADS    :     25   29
EGADS    :     26   30
EGADS    :     27   31
EGADS    :     28   32
EGADS    :     29   33
EGADS    :     30   34
EGADS    :     31   35
EGADS    :     32   36
EGADS    :     33   37
EGADS    :     34   38
EGADS    :     35   39
EGADS    :     36   40
EGADS    :     37   41
EGADS    :     38   42
EGADS    :     39   43
EGADS    :     40   44
EGADS    :     41   45
EGADS    :     42   46
EGADS    :     43   47
EGADS    :     44   48
EGADS    :     45   49
EGADS    :     46   50
EGADS    :     47   51
EGADS    :     48   52
EGADS    :     49   53
EGADS    :     50   54
EGADS    :     51   55
EGADS    :     52   56
EGADS    :     53   57
EGADS    :     54   58
EGADS    :     55   59
EGADS    :     56   60
EGADS    :     57   61
EGADS    :     58   62
EGADS    :     59   63
EGADS    :     60   64
EGADS    :     61   65
EGADS    :     62   66
EGADS    :     63   67
EGADS    :     64   68
EGADS    :     65   69
EGADS    :     66   70
EGADS    :     67   71
EGADS    :     68   72
EGADS    :     69   73
EGADS    :     70   74
EGADS    :     71   75
EGADS    :     72   76
EGADS    :     73   77
EGADS    :     74   78
EGADS    :     75   79
EGADS    :     76   80
EGADS    :     77   81
EGADS    :     78   82
EGADS    :     79   83
EGADS    :     80   84
EGADS    :     81   85
EGADS    :     82   86
EGADS    :     83   87
EGADS    :     84   88
EGADS    :     85   89
EGADS    :     86   90
EGADS    :     87   91
EGADS    :     88   92
EGADS    :     89   93
EGADS    :     90   94
EGADS    :     91   95
EGADS    :     92   96
EGADS    :     93   97
EGADS    :     94   98
EGADS    :     95   99
EGADS    :     96   100
EGADS    :     97   101
EGADS    :     98   102
EGADS    :     99   103
EGADS    :    100   104
EGADS    :    101   105
EGADS    :    102   106
EGADS    :    103   107
EGADS    :    104   108
EGADS    :    105   109
EGADS    :    106   110
EGADS    :    107   111
EGADS    :    108   112
EGADS    :    109   113
EGADS    :    110   114
EGADS    :    111   115
EGADS    :    112   116
EGADS    :    113   117
EGADS    :    114   118
EGADS    :    115   119
EGADS    :    116   120
EGADS    :    117   121
EGADS    :    118   122

EGADS    : Loop Edges Information

EGADS    :   Loop  Active   Edges
EGADS    :      1     Yes   -1 4 3 -2
EGADS    :      2     Yes   -5 -6
EGADS    :      3     Yes   -7 9 1 -8
EGADS    :      4     Yes   10 11
EGADS    :      5     Yes   -12 2 17 -16 -15 14 -13
EGADS    :      6     Yes   -3 18 19 -20
EGADS    :      7     Yes   21 -22 23 24 25 26 -27 5
EGADS    :      8     Yes   27 28 -25 29 -30 -31 -21 6
EGADS    :      9     Yes   32 33
EGADS    :     10     Yes   -19 34 7 -35
EGADS    :     11     Yes   -36 8 12 -40 -39 38 37
EGADS    :     12     Yes   -41 -10 47 46 45 -44 43 -42
EGADS    :     13     Yes   48 49
EGADS    :     14     Yes   -47 -11 41 -53 -43 -52 -51 50
EGADS    :     15     Yes   13 54 55 40
EGADS    :     16     Yes   -17 20 60 59 58 -54 -14 -57 -56
EGADS    :     17     Yes   61 -62 63 64 65 66 -67 57 15
EGADS    :     18     Yes   67 68 -65 69 -70 -71 -61 16 56
EGADS    :     19     Yes   31 72 22
EGADS    :     20     Yes   30 73 -23 -72
EGADS    :     21     Yes   -73 -29 -24
EGADS    :     22     Yes   74 -75 76 77 78 -79 80 81 82 83 -84 -26
EGADS    :     23     Yes   84 85 -82 86 -87 -88 -78 89 -90 -91 -74 -28
EGADS    :     24     Yes   -92 94 -32 -93
EGADS    :     25     Yes   -94 95 93 -33
EGADS    :     26     Yes   -60 35 36 98 97 39 -55 -58 96
EGADS    :     27     Yes   -99 -98 -37 105 104 103 -102 101 -100
EGADS    :     28     Yes   -105 -38 -97 99 -109 -101 -108 -107 106
EGADS    :     29     Yes   -110 42 120 119 118 -117 116 115 114 -113 112 -111
EGADS    :     30     Yes   44 121 52
EGADS    :     31     Yes   -45 122 51 -121
EGADS    :     32     Yes   -122 -46 -50
EGADS    :     33     Yes   123 124 -48 -125
EGADS    :     34     Yes   125 -49 -124 -126
EGADS    :     35     Yes   -120 53 110 -133 -112 -132 -131 130 -116 -129 -128
EGADS    :                        127
EGADS    :     36     Yes   -134 -59 140 -139 -138 -137 -136 135
EGADS    :     37     Yes   71 141 62
EGADS    :     38     Yes   70 142 -63 -141
EGADS    :     39     Yes   -142 -69 -64
EGADS    :     40     Yes   -66 -68
EGADS    :     41     Yes   91 143 75
EGADS    :     42     Yes   90 144 -76 -143
EGADS    :     43     Yes   -144 -89 -77
EGADS    :     44     Yes   88 145 79
EGADS    :     45     Yes   87 146 -80 -145
EGADS    :     46     Yes   -146 -86 -81
EGADS    :     47     Yes   -83 -85
EGADS    :     48     Yes   147 92 148 149 -150 -151
EGADS    :     49     Yes   -147 153 150 -152 -148 -95
EGADS    :     50     Yes   -140 -96 134 157 156 -155 138 -154
EGADS    :     51     Yes   109 100
EGADS    :     52     Yes   102 158 108
EGADS    :     53     Yes   -103 159 107 -158
EGADS    :     54     Yes   -159 -104 -106
EGADS    :     55     Yes   133 111
EGADS    :     56     Yes   113 160 132
EGADS    :     57     Yes   -114 161 131 -160
EGADS    :     58     Yes   -161 -115 -130
EGADS    :     59     Yes   117 162 129
EGADS    :     60     Yes   -118 163 128 -162
EGADS    :     61     Yes   -163 -119 -127
EGADS    :     62     Yes   164 -123 165 166 -167 -168
EGADS    :     63     Yes   -164 170 167 -169 -165 126
EGADS    :     64     Yes   -135 171 -157
EGADS    :     65     Yes   136 172 -156 -171
EGADS    :     66     Yes   -172 137 155
EGADS    :     67     Yes   139 154
EGADS    :     68     Yes   -149 173 151 -174
EGADS    :     69     Yes   152 174 -153 -173
EGADS    :     70     Yes   -166 175 168 -176
EGADS    :     71     Yes   169 176 -170 -175
EGADS    :     72     Yes   -177 180 179 -178
EGADS    :     73     Yes   181 182 177
EGADS    :     74     Yes   178 183 -184 -181
EGADS    :     75     Yes   -179 -185 -183
EGADS    :     76     Yes   -180 -182 184 185
EGADS    :     77     Yes   -186 189 188 -187
EGADS    :     78     Yes   190 191 186
EGADS    :     79     Yes   187 192 -193 -190
EGADS    :     80     Yes   -188 -194 -192
EGADS    :     81     Yes   -189 -191 193 194
EGADS    :     82     Yes   -195 198 197 -196
EGADS    :     83     Yes   199 200 195
EGADS    :     84     Yes   196 201 -202 -199
EGADS    :     85     Yes   -197 -203 -201
EGADS    :     86     Yes   -198 -200 202 203
EGADS    :     87     Yes   204 -205 -206 207
EGADS    :     88     Yes   208 209 -210 -204
EGADS    :     89     Yes   211 205 210
EGADS    :     90     Yes   -209 212 206 -211
EGADS    :     91     Yes   -208 -207 -212
EGADS    :     92     Yes   213 -214 -215 216
EGADS    :     93     Yes   217 218 -219 -213
EGADS    :     94     Yes   220 214 219
EGADS    :     95     Yes   -218 221 215 -220
EGADS    :     96     Yes   -217 -216 -221
EGADS    :     97     Yes   -222 -223 224 225
EGADS    :     98     Yes   226 222 227
EGADS    :     99     Yes   -228 229 223 -226
EGADS    :    100     Yes   -230 -224 -229
EGADS    :    101     Yes   -225 230 228 -227
EGADS    :    102     Yes   231 234 -233 -232
EGADS    :    103     Yes   -231 -237 236 235
EGADS    :    104     Yes   238 237 232
EGADS    :    105     Yes   233 239 -236 -238
EGADS    :    106     Yes   -234 -235 -239
EGADS    :    107     Yes   240 -241 -242 243
EGADS    :    108     Yes   -240 244 245 -246
EGADS    :    109     Yes   247 241 246
EGADS    :    110     Yes   -245 248 242 -247
EGADS    :    111     Yes   -244 -243 -248
EGADS    :    112     Yes   -249 -252 251 250
EGADS    :    113     Yes   -253 249 255 -254
EGADS    :    114     Yes   256 -255 -250
EGADS    :    115     Yes   -251 257 254 -256
EGADS    :    116     Yes   252 253 -257
EGADS    :    117     Yes   258 259 -260 -261
EGADS    :    118     Yes   -262 265 264 -263
EGADS    :    119     Yes   266 262 -267 -258
EGADS    :    120     Yes   -268 260 269 -264
EGADS    :    121     Yes   261 268 -265 -266
EGADS    :    122     Yes   -259 267 263 -269

EGADS    : Edge Node, Scale Factor, and Neighbor-Faces Information

EGADS    : ESF = Edge Scale Factor
EGADS    :       Not applicable for DEGENERATE Edges or Edges with a FarField
EGADS    :       Grid BC Neighbor Face.

EGADS    :                                             Neighbor
EGADS    :   Edge  Body  Active Node1 Node2      ESF   Faces
EGADS    :      1     0     Yes     1     2        1   1 2
EGADS    :      2     0     Yes     2     3        1   1 3
EGADS    :      3     0     Yes     1     3        1   1 4
EGADS    :      4     0   DEGEN     1     1        -   1
EGADS    :      5     0     Yes     4     5        1   1 5
EGADS    :      6     0     Yes     5     4        1   1 6
EGADS    :      7     0     Yes     1     6        1   2 7
EGADS    :      8     0     Yes     6     2        1   2 8
EGADS    :      9     0   DEGEN     1     1        -   2
EGADS    :     10     0     Yes     7     8        1   2 9
EGADS    :     11     0     Yes     8     7        1   2 10
EGADS    :     12     0     Yes     2     9        1   3 8
EGADS    :     13     0     Yes     9    10        1   3 11
EGADS    :     14     0     Yes    11    10        1   3 12
EGADS    :     15     0     Yes    11    12        1   3 13
EGADS    :     16     0     Yes    12    13        1   3 14
EGADS    :     17     0     Yes     3    13        1   3 12
EGADS    :     18     0   DEGEN     1     1        -   4
EGADS    :     19     0     Yes     1    14        1   4 7
EGADS    :     20     0     Yes     3    14        1   4 12
EGADS    :     21     0     Yes     5    15        1   5 6
EGADS    :     22     0     Yes    16    15        1   5 15
EGADS    :     23     0     Yes    16    17        1   5 16
EGADS    :     24     0     Yes    17    18        1   5 17
EGADS    :     25     0     Yes    18    19        1   5 6
EGADS    :     26     0     Yes    19    20        1   5 18
EGADS    :     27     0     Yes     4    20        1   5 6
EGADS    :     28     0     Yes    20    19        1   6 19
EGADS    :     29     0     Yes    18    21        1   6 17
EGADS    :     30     0     Yes    22    21        1   6 16
EGADS    :     31     0     Yes    15    22        1   6 15
EGADS    :     32     0     Yes    23    24        1   6 20
EGADS    :     33     0     Yes    24    23        1   6 21
EGADS    :     34     0   DEGEN     1     1        -   7
EGADS    :     35     0     Yes    14     6        1   7 22
EGADS    :     36     0     Yes     6    25        1   8 22
EGADS    :     37     0     Yes    26    25        1   8 23
EGADS    :     38     0     Yes    27    26        1   8 24
EGADS    :     39     0     Yes    27    28        1   8 22
EGADS    :     40     0     Yes    28     9        1   8 11
EGADS    :     41     0     Yes     8    29        1   9 10
EGADS    :     42     0     Yes    29    30        1   9 25
EGADS    :     43     0     Yes    31    30        1   9 10
EGADS    :     44     0     Yes    31    32        1   9 26
EGADS    :     45     0     Yes    33    32        1   9 27
EGADS    :     46     0     Yes    34    33        1   9 28
EGADS    :     47     0     Yes     7    34        1   9 10
EGADS    :     48     0     Yes    35    36        1   9 29
EGADS    :     49     0     Yes    36    35        1   9 30
EGADS    :     50     0     Yes    37    34        1   10 28
EGADS    :     51     0     Yes    37    38        1   10 27
EGADS    :     52     0     Yes    38    31        1   10 26
EGADS    :     53     0     Yes    30    29        1   10 31
EGADS    :     54     0     Yes    10    39        1   11 12
EGADS    :     55     0     Yes    39    28        1   11 22
EGADS    :     56     0     Yes    13    40        1   12 14
EGADS    :     57     0     Yes    40    11        1   12 13
EGADS    :     58     0     Yes    41    39        1   12 22
EGADS    :     59     0     Yes    42    41        1   12 32
EGADS    :     60     0     Yes    14    42        1   12 22
EGADS    :     61     0     Yes    12    43        1   13 14
EGADS    :     62     0     Yes    44    43        1   13 33
EGADS    :     63     0     Yes    44    45        1   13 34
EGADS    :     64     0     Yes    45    46        1   13 35
EGADS    :     65     0     Yes    46    47        1   13 14
EGADS    :     66     0     Yes    47    48        1   13 36
EGADS    :     67     0     Yes    40    48        1   13 14
EGADS    :     68     0     Yes    48    47        1   14 36
EGADS    :     69     0     Yes    46    49        1   14 35
EGADS    :     70     0     Yes    50    49        1   14 34
EGADS    :     71     0     Yes    43    50        1   14 33
EGADS    :     72     0     Yes    22    16        1   15 16
EGADS    :     73     0     Yes    21    17        1   16 17
EGADS    :     74     0     Yes    19    51        1   18 19
EGADS    :     75     0     Yes    52    51        1   18 37
EGADS    :     76     0     Yes    52    53        1   18 38
EGADS    :     77     0     Yes    53    54        1   18 39
EGADS    :     78     0     Yes    54    55        1   18 19
EGADS    :     79     0     Yes    56    55        1   18 40
EGADS    :     80     0     Yes    56    57        1   18 41
EGADS    :     81     0     Yes    57    58        1   18 42
EGADS    :     82     0     Yes    58    59        1   18 19
EGADS    :     83     0     Yes    59    60        1   18 43
EGADS    :     84     0     Yes    20    60        1   18 19
EGADS    :     85     0     Yes    60    59        1   19 43
EGADS    :     86     0     Yes    58    61        1   19 42
EGADS    :     87     0     Yes    62    61        1   19 41
EGADS    :     88     0     Yes    55    62        1   19 40
EGADS    :     89     0     Yes    54    63        1   19 39
EGADS    :     90     0     Yes    64    63        1   19 38
EGADS    :     91     0     Yes    51    64        1   19 37
EGADS    :     92     0     Yes    65    66        1   20 44
EGADS    :     93     0     Yes    66    23        1   20 21
EGADS    :     94     0     Yes    65    24        1   20 21
EGADS    :     95     0     Yes    65    66        1   21 45
EGADS    :     96     0     Yes    41    42        1   22 46
EGADS    :     97     0     Yes    67    27        1   22 24
EGADS    :     98     0     Yes    25    67        1   22 23
EGADS    :     99     0     Yes    67    68        1   23 24
EGADS    :    100     0     Yes    68    69        1   23 47
EGADS    :    101     0     Yes    70    69        1   23 24
EGADS    :    102     0     Yes    70    71        1   23 48
EGADS    :    103     0     Yes    72    71        1   23 49
EGADS    :    104     0     Yes    73    72        1   23 50
EGADS    :    105     0     Yes    26    73        1   23 24
EGADS    :    106     0     Yes    74    73        1   24 50
EGADS    :    107     0     Yes    74    75        1   24 49
EGADS    :    108     0     Yes    75    70        1   24 48
EGADS    :    109     0     Yes    69    68        1   24 47
EGADS    :    110     0     Yes    29    76        1   25 31
EGADS    :    111     0     Yes    76    77        1   25 51
EGADS    :    112     0     Yes    78    77        1   25 31
EGADS    :    113     0     Yes    78    79        1   25 52
EGADS    :    114     0     Yes    80    79        1   25 53
EGADS    :    115     0     Yes    81    80        1   25 54
EGADS    :    116     0     Yes    82    81        1   25 31
EGADS    :    117     0     Yes    82    83        1   25 55
EGADS    :    118     0     Yes    84    83        1   25 56
EGADS    :    119     0     Yes    85    84        1   25 57
EGADS    :    120     0     Yes    30    85        1   25 31
EGADS    :    121     0     Yes    32    38        1   26 27
EGADS    :    122     0     Yes    33    37        1   27 28
EGADS    :    123     0     Yes    86    87        1   29 58
EGADS    :    124     0     Yes    87    36        1   29 30
EGADS    :    125     0     Yes    86    35        1   29 30
EGADS    :    126     0     Yes    86    87        1   30 59
EGADS    :    127     0     Yes    88    85        1   31 57
EGADS    :    128     0     Yes    88    89        1   31 56
EGADS    :    129     0     Yes    89    82        1   31 55
EGADS    :    130     0     Yes    90    81        1   31 54
EGADS    :    131     0     Yes    90    91        1   31 53
EGADS    :    132     0     Yes    91    78        1   31 52
EGADS    :    133     0     Yes    77    76        1   31 51
EGADS    :    134     0     Yes    41    92        1   32 46
EGADS    :    135     0     Yes    93    92        1   32 60
EGADS    :    136     0     Yes    93    94        1   32 61
EGADS    :    137     0     Yes    94    95        1   32 62
EGADS    :    138     0     Yes    95    96        1   32 46
EGADS    :    139     0     Yes    96    97        1   32 63
EGADS    :    140     0     Yes    42    97        1   32 46
EGADS    :    141     0     Yes    50    44        1   33 34
EGADS    :    142     0     Yes    49    45        1   34 35
EGADS    :    143     0     Yes    64    52        1   37 38
EGADS    :    144     0     Yes    63    53        1   38 39
EGADS    :    145     0     Yes    62    56        1   40 41
EGADS    :    146     0     Yes    61    57        1   41 42
EGADS    :    147     0     Yes    98    65        1   44 45
EGADS    :    148     0     Yes    66    99        1   44 45
EGADS    :    149     0     Yes    99   100        1   44 64
EGADS    :    150     0     Yes   101   100        1   44 45
EGADS    :    151     0     Yes    98   101        1   44 64
EGADS    :    152     0     Yes    99   100        1   45 65
EGADS    :    153     0     Yes    98   101        1   45 65
EGADS    :    154     0     Yes    97    96        1   46 63
EGADS    :    155     0     Yes    95   102        1   46 62
EGADS    :    156     0     Yes   103   102        1   46 61
EGADS    :    157     0     Yes    92   103        1   46 60
EGADS    :    158     0     Yes    71    75        1   48 49
EGADS    :    159     0     Yes    72    74        1   49 50
EGADS    :    160     0     Yes    79    91        1   52 53
EGADS    :    161     0     Yes    80    90        1   53 54
EGADS    :    162     0     Yes    83    89        1   55 56
EGADS    :    163     0     Yes    84    88        1   56 57
EGADS    :    164     0     Yes   104    87        1   58 59
EGADS    :    165     0     Yes    86   105        1   58 59
EGADS    :    166     0     Yes   105   106        1   58 66
EGADS    :    167     0     Yes   107   106        1   58 59
EGADS    :    168     0     Yes   104   107        1   58 66
EGADS    :    169     0     Yes   105   106        1   59 67
EGADS    :    170     0     Yes   104   107        1   59 67
EGADS    :    171     0     Yes    93   103        1   60 61
EGADS    :    172     0     Yes    94   102        1   61 62
EGADS    :    173     0     Yes    99    98        1   64 65
EGADS    :    174     0     Yes   100   101        1   64 65
EGADS    :    175     0     Yes   105   104        1   66 67
EGADS    :    176     0     Yes   106   107        1   66 67
EGADS    :    177     1     Yes   108   109        1   68 69
EGADS    :    178     1     Yes   109   110        1   68 70
EGADS    :    179     1     Yes   111   110        1   68 71
EGADS    :    180     1     Yes   108   111        1   68 72
EGADS    :    181     1     Yes   109   112        1   69 70
EGADS    :    182     1     Yes   112   108        1   69 72
EGADS    :    183     1     Yes   110   113        1   70 71
EGADS    :    184     1     Yes   112   113        1   70 72
EGADS    :    185     1     Yes   113   111        1   71 72
EGADS    :    186     2     Yes   114   115        1   73 74
EGADS    :    187     2     Yes   115   116        1   73 75
EGADS    :    188     2     Yes   117   116        1   73 76
EGADS    :    189     2     Yes   114   117        1   73 77
EGADS    :    190     2     Yes   115   118        1   74 75
EGADS    :    191     2     Yes   118   114        1   74 77
EGADS    :    192     2     Yes   116   119        1   75 76
EGADS    :    193     2     Yes   118   119        1   75 77
EGADS    :    194     2     Yes   119   117        1   76 77
EGADS    :    195     3     Yes   120   121        1   78 79
EGADS    :    196     3     Yes   121   122        1   78 80
EGADS    :    197     3     Yes   123   122        1   78 81
EGADS    :    198     3     Yes   120   123        1   78 82
EGADS    :    199     3     Yes   121   124        1   79 80
EGADS    :    200     3     Yes   124   120        1   79 82
EGADS    :    201     3     Yes   122   125        1   80 81
EGADS    :    202     3     Yes   124   125        1   80 82
EGADS    :    203     3     Yes   125   123        1   81 82
EGADS    :    204     4     Yes   126   127        1   83 84
EGADS    :    205     4     Yes   128   127        1   83 85
EGADS    :    206     4     Yes   129   128        1   83 86
EGADS    :    207     4     Yes   129   126        1   83 87
EGADS    :    208     4     Yes   126   130        1   84 87
EGADS    :    209     4     Yes   130   131        1   84 86
EGADS    :    210     4     Yes   127   131        1   84 85
EGADS    :    211     4     Yes   131   128        1   85 86
EGADS    :    212     4     Yes   130   129        1   86 87
EGADS    :    213     5     Yes   132   133        1   88 89
EGADS    :    214     5     Yes   134   133        1   88 90
EGADS    :    215     5     Yes   135   134        1   88 91
EGADS    :    216     5     Yes   135   132        1   88 92
EGADS    :    217     5     Yes   132   136        1   89 92
EGADS    :    218     5     Yes   136   137        1   89 91
EGADS    :    219     5     Yes   133   137        1   89 90
EGADS    :    220     5     Yes   137   134        1   90 91
EGADS    :    221     5     Yes   136   135        1   91 92
EGADS    :    222     6     Yes   138   139        1   93 94
EGADS    :    223     6     Yes   140   138        1   93 95
EGADS    :    224     6     Yes   140   141        1   93 96
EGADS    :    225     6     Yes   141   139        1   93 97
EGADS    :    226     6     Yes   142   138        1   94 95
EGADS    :    227     6     Yes   139   142        1   94 97
EGADS    :    228     6     Yes   143   142        1   95 97
EGADS    :    229     6     Yes   143   140        1   95 96
EGADS    :    230     6     Yes   141   143        1   96 97
EGADS    :    231     7     Yes   144   145        1   98 99
EGADS    :    232     7     Yes   144   146        1   98 100
EGADS    :    233     7     Yes   146   147        1   98 101
EGADS    :    234     7     Yes   145   147        1   98 102
EGADS    :    235     7     Yes   148   145        1   99 102
EGADS    :    236     7     Yes   149   148        1   99 101
EGADS    :    237     7     Yes   149   144        1   99 100
EGADS    :    238     7     Yes   146   149        1   100 101
EGADS    :    239     7     Yes   147   148        1   101 102
EGADS    :    240     8     Yes   150   151        1   103 104
EGADS    :    241     8     Yes   152   151        1   103 105
EGADS    :    242     8     Yes   153   152        1   103 106
EGADS    :    243     8     Yes   153   150        1   103 107
EGADS    :    244     8     Yes   150   154        1   104 107
EGADS    :    245     8     Yes   154   155        1   104 106
EGADS    :    246     8     Yes   151   155        1   104 105
EGADS    :    247     8     Yes   155   152        1   105 106
EGADS    :    248     8     Yes   154   153        1   106 107
EGADS    :    249     9     Yes   156   157        1   108 109
EGADS    :    250     9     Yes   158   157        1   108 110
EGADS    :    251     9     Yes   159   158        1   108 111
EGADS    :    252     9     Yes   159   156        1   108 112
EGADS    :    253     9     Yes   156   160        1   109 112
EGADS    :    254     9     Yes   160   161        1   109 111
EGADS    :    255     9     Yes   157   161        1   109 110
EGADS    :    256     9     Yes   158   161        1   110 111
EGADS    :    257     9     Yes   159   160        1   111 112
EGADS    :    258    10     Yes   163   162       NA   113 115
EGADS    :    259    10     Yes   162   164       NA   113 118
EGADS    :    260    10     Yes   165   164       NA   113 116
EGADS    :    261    10     Yes   163   165       NA   113 117
EGADS    :    262    10     Yes   167   166       NA   114 115
EGADS    :    263    10     Yes   166   168       NA   114 118
EGADS    :    264    10     Yes   169   168       NA   114 116
EGADS    :    265    10     Yes   167   169       NA   114 117
EGADS    :    266    10     Yes   163   167       NA   115 117
EGADS    :    267    10     Yes   162   166       NA   115 118
EGADS    :    268    10     Yes   165   169       NA   116 117
EGADS    :    269    10     Yes   164   168       NA   116 118

EGADS    : Node Information

EGADS    :   Node  Active      Coordinates
EGADS    :      1     Yes                0                0                0
EGADS    :      2     Yes       121.026192                0                0
EGADS    :      3     Yes       121.026192               10                0
EGADS    :      4     Yes       54.9020417       7.00084115                0
EGADS    :      5     Yes        97.361045       7.90366896                0
EGADS    :      6     Yes       121.026192                0                0
EGADS    :      7     Yes        97.361045                0                0
EGADS    :      8     Yes       54.9020417                0                0
EGADS    :      9     Yes       165.026192                0                7
EGADS    :     10     Yes       165.026192              0.5              8.5
EGADS    :     11     Yes       156.577382       2.32417494       6.86784347
EGADS    :     12     Yes       160.457816       1.16501909       6.24763245
EGADS    :     13     Yes       152.092394       3.29252447       6.00142548
EGADS    :     14     Yes       121.026192                0               10
EGADS    :     15     Yes       97.4729828       13.4242093                0
EGADS    :     16     Yes       93.4296648       13.4242093                0
EGADS    :     17     Yes        93.813734       32.4820648                0
EGADS    :     18     Yes       97.8594113       32.4820648                0
EGADS    :     19     Yes       97.9335611       36.1389817                0
EGADS    :     20     Yes       75.3047874       36.1389817                0
EGADS    :     21     Yes        93.813734       32.4820648                0
EGADS    :     22     Yes       93.4296648       13.4242093                0
EGADS    :     23     Yes       72.4759225       29.3018771                0
EGADS    :     24     Yes       83.5054156       29.3018771                0
EGADS    :     25     Yes       152.092394                0       6.00142548
EGADS    :     26     Yes       160.457816                0       6.24763245
EGADS    :     27     Yes       156.577382                0       6.86784347
EGADS    :     28     Yes       165.026192                0              8.5
EGADS    :     29     Yes       75.3047874                0                0
EGADS    :     30     Yes       97.9335611                0                0
EGADS    :     31     Yes       97.8594113                0                0
EGADS    :     32     Yes        93.813734                0                0
EGADS    :     33     Yes       93.4296648                0                0
EGADS    :     34     Yes       97.4729828                0                0
EGADS    :     35     Yes       72.4759225                0                0
EGADS    :     36     Yes       83.5054156                0                0
EGADS    :     37     Yes       93.4296648                0                0
EGADS    :     38     Yes        93.813734                0                0
EGADS    :     39     Yes       165.026192                0               10
EGADS    :     40     Yes       139.227902       5.03861756       7.07099122
EGADS    :     41     Yes       159.822328                0               10
EGADS    :     42     Yes       137.454662                0               10
EGADS    :     43     Yes       162.492237        6.6562396        7.4148274
EGADS    :     44     Yes       153.156875        6.6562396       8.10980625
EGADS    :     45     Yes       168.687412       34.4921381       13.6297335
EGADS    :     46     Yes       172.805054       34.4921381       13.3315303
EGADS    :     47     Yes       173.282633        35.781198       13.6055284
EGADS    :     48     Yes        165.02399        35.781198       13.6055284
EGADS    :     49     Yes       168.687412       34.4921381        13.033327
EGADS    :     50     Yes       153.156875        6.6562396       6.71984855
EGADS    :     51     Yes       100.269362       41.7493571                0
EGADS    :     52     Yes       94.7284993       41.7493571                0
EGADS    :     53     Yes       107.349293       67.6443173       1.84589548
EGADS    :     54     Yes       111.050367       67.6443173       1.25578139
EGADS    :     55     Yes       111.248847       68.1210465       1.31074802
EGADS    :     56     Yes       107.581644       68.1210465       1.89111513
EGADS    :     57     Yes       121.153699       95.9694651       4.50848923
EGADS    :     58     Yes       122.843146       95.9694651       4.52165604
EGADS    :     59     Yes       123.552357       97.6729236        4.7180639
EGADS    :     60     Yes       118.391317       97.6729236       3.99272703
EGADS    :     61     Yes       121.153699       95.9694651       4.20550678
EGADS    :     62     Yes       107.581644       68.1210465      0.865881946
EGADS    :     63     Yes       107.349293       67.6443173      0.808537183
EGADS    :     64     Yes       94.7284993       41.7493571                0
EGADS    :     65     Yes       79.4370049       29.3018771                0
EGADS    :     66     Yes        70.524066       29.3018771                0
EGADS    :     67     Yes       139.227902                0       7.07099122
EGADS    :     68     Yes        165.02399                0       13.6055284
EGADS    :     69     Yes       173.282633                0       13.6055284
EGADS    :     70     Yes       172.805054                0       13.3315303
EGADS    :     71     Yes       168.687412                0        13.033327
EGADS    :     72     Yes       153.156875                0       6.71984855
EGADS    :     73     Yes       162.492237                0        7.4148274
EGADS    :     74     Yes       153.156875                0       8.10980625
EGADS    :     75     Yes       168.687412                0       13.6297335
EGADS    :     76     Yes       118.391317                0       3.99272703
EGADS    :     77     Yes       123.552357                0        4.7180639
EGADS    :     78     Yes       122.843146                0       4.52165604
EGADS    :     79     Yes       121.153699                0       4.20550678
EGADS    :     80     Yes       107.581644                0      0.865881946
EGADS    :     81     Yes       111.248847                0       1.31074802
EGADS    :     82     Yes       111.050367                0       1.25578139
EGADS    :     83     Yes       107.349293                0      0.808537183
EGADS    :     84     Yes       94.7284993                0                0
EGADS    :     85     Yes       100.269362                0                0
EGADS    :     86     Yes        70.524066                0                0
EGADS    :     87     Yes       79.4370049                0                0
EGADS    :     88     Yes       94.7284993                0                0
EGADS    :     89     Yes       107.349293                0       1.84589548
EGADS    :     90     Yes       107.581644                0       1.89111513
EGADS    :     91     Yes       121.153699                0       4.50848923
EGADS    :     92     Yes       160.542569                0       11.9206428
EGADS    :     93     Yes       151.486032      0.673415422       11.9206428
EGADS    :     94     Yes       165.862466      0.235428105       34.9229244
EGADS    :     95     Yes       169.168425                0       34.9229244
EGADS    :     96     Yes        169.38016                0        35.487551
EGADS    :     97     Yes       162.942213                0        35.487551
EGADS    :     98     Yes       90.5173952       29.3018771                0
EGADS    :     99     Yes       60.5173952       29.3018771                0
EGADS    :    100     Yes       60.5173952       29.3018771                0
EGADS    :    101     Yes       90.5173952       29.3018771                0
EGADS    :    102     Yes       165.862466                0       34.9229244
EGADS    :    103     Yes       151.486032                0       11.9206428
EGADS    :    104     Yes       90.5173952                0                0
EGADS    :    105     Yes       60.5173952                0                0
EGADS    :    106     Yes       60.5173952                0                0
EGADS    :    107     Yes       90.5173952                0                0
EGADS    :    108     Yes       111.321903                0       1.86654259
EGADS    :    109     Yes       108.055298                0       0.93793256
EGADS    :    110     Yes        121.33061                0       4.22828065
EGADS    :    111     Yes       122.700876                0       4.71377572
EGADS    :    112     Yes       107.907885                0       1.87632098
EGADS    :    113     Yes       121.289329                0       4.49106118
EGADS    :    114     Yes       100.394138                0                0
EGADS    :    115     Yes       95.1284577                0                0
EGADS    :    116     Yes       107.505559                0      0.813039939
EGADS    :    117     Yes       110.968457                0      0.689237814
EGADS    :    118     Yes       95.3800953                0                0
EGADS    :    119     Yes       107.657908                0       1.77558767
EGADS    :    120     Yes       97.2857328                0                0
EGADS    :    121     Yes       93.6847537                0                0
EGADS    :    122     Yes       94.0587466                0                0
EGADS    :    123     Yes       97.7824572                0                0
EGADS    :    124     Yes       93.9345512                0                0
EGADS    :    125     Yes       94.3601422                0                0
EGADS    :    126     Yes       97.2857328       13.7821489                0
EGADS    :    127     Yes       97.7824572       32.3393376                0
EGADS    :    128     Yes       94.3601422       32.2302343                0
EGADS    :    129     Yes       93.9345512       13.6726922                0
EGADS    :    130     Yes       93.6847537       13.6742093                0
EGADS    :    131     Yes       94.0587466       32.2320648                0
EGADS    :    132     Yes       100.394138       42.0879216                0
EGADS    :    133     Yes       110.968457       67.4483237      0.689237814
EGADS    :    134     Yes       107.657908       67.3218336       1.77558767
EGADS    :    135     Yes       95.3800953       41.8796344                0
EGADS    :    136     Yes       95.1284577       41.9993571                0
EGADS    :    137     Yes       107.505559       67.3943173      0.813039939
EGADS    :    138     Yes       121.330781       95.7095395       4.49106118
EGADS    :    139     Yes       122.742253       95.7419985       4.26970731
EGADS    :    140     Yes       108.055908       68.3356022       1.87632098
EGADS    :    141     Yes       111.300912       68.4526045      0.818951249
EGADS    :    142     Yes       121.289158       95.7293907       4.22828065
EGADS    :    143     Yes       107.907275       68.4064908       0.93793256
EGADS    :    144     Yes       162.652062                0       6.87525931
EGADS    :    145     Yes       172.609142                0       12.9541609
EGADS    :    146     Yes       153.959016                0       6.86654493
EGADS    :    147     Yes       168.960275                0        12.950503
EGADS    :    148     Yes       169.001731                0        13.500001
EGADS    :    149     Yes        154.05778                0       8.17566644
EGADS    :    150     Yes       162.652062       7.30770007       6.87525931
EGADS    :    151     Yes       172.609142       34.0557129       12.9541609
EGADS    :    152     Yes       169.001731        33.980789        13.500001
EGADS    :    153     Yes        154.05778       7.12920153       8.17566644
EGADS    :    154     Yes       153.959016       7.18327767       6.86654493
EGADS    :    155     Yes       168.960275       34.0034872        12.950503
EGADS    :    156     Yes       160.730069                0       12.4206428
EGADS    :    157     Yes       168.980925                0       34.4229244
EGADS    :    158     Yes       166.139589      0.215327731       34.4229244
EGADS    :    159     Yes       152.388156      0.632183325       12.4206428
EGADS    :    160     Yes       152.388156                0       12.4206428
EGADS    :    161     Yes       166.139589                0       34.4229244
EGADS    :    162     Yes                0                0       1962.43554
EGADS    :    163     Yes                0                0                0
EGADS    :    164     Yes                0       1953.45847       1962.43554
EGADS    :    165     Yes                0       1953.45847                0
EGADS    :    166     Yes       2040.09979                0       1962.43554
EGADS    :    167     Yes       2040.09979                0                0
EGADS    :    168     Yes       2040.09979       1953.45847       1962.43554
EGADS    :    169     Yes       2040.09979       1953.45847                0

EGADS    : Face and Edge Match Information

EGADS    : No Face Matches Found

AFLR4    : Surface Mesh Spacing Setup

AFLR4    : Max Bounding Box Length     = 3906.92
AFLR4    : Min Bounding Box Length     = 3906.92
AFLR4    : Max Ref Bounding Box Length = 195.346
AFLR4    : Min Ref Bounding Box Length = 53.021
AFLR4    : Reference Length            = 21.7051
AFLR4    : BL Thickness                = 0
AFLR4    : FarField Spacing            = 3181.81
AFLR4    : Abs Min Surf Spacing        = 0.0542627
AFLR4    : Min Surf Spacing            = 0.108525
AFLR4    : Max Surf Spacing            = 2.17051
AFLR4    : Global Scale Factor         = 6

AFLR4    : Geometry Definition Information

AFLR4    : Definition              Definition   Composite             Grid BC
AFLR4    :         ID                    Type          ID                Type
AFLR4    :          0     glue-only composite           -                   -
AFLR4    :          1            CAD geometry           0            STD w/BL
AFLR4    :          2            CAD geometry           0            STD w/BL
AFLR4    :          3            CAD geometry           0            STD w/BL
AFLR4    :          4            CAD geometry           0            STD w/BL
AFLR4    :          5            CAD geometry           0            STD w/BL
AFLR4    :          6            CAD geometry           0            STD w/BL
AFLR4    :          7            CAD geometry           0            STD w/BL
AFLR4    :          8            CAD geometry           0            STD w/BL
AFLR4    :          9            CAD geometry           0            STD w/BL
AFLR4    :         10            CAD geometry           0            STD w/BL
AFLR4    :         11            CAD geometry           0            STD w/BL
AFLR4    :         12            CAD geometry           0            STD w/BL
AFLR4    :         13            CAD geometry           0            STD w/BL
AFLR4    :         14            CAD geometry           0            STD w/BL
AFLR4    :         15            CAD geometry           0            STD w/BL
AFLR4    :         16            CAD geometry           0            STD w/BL
AFLR4    :         17            CAD geometry           0            STD w/BL
AFLR4    :         18            CAD geometry           0            STD w/BL
AFLR4    :         19            CAD geometry           0            STD w/BL
AFLR4    :         20            CAD geometry           0            STD w/BL
AFLR4    :         21            CAD geometry           0            STD w/BL
AFLR4    :         22            CAD geometry           0            STD w/BL
AFLR4    :         23            CAD geometry           0            STD w/BL
AFLR4    :         24            CAD geometry           0            STD w/BL
AFLR4    :         25            CAD geometry           0            STD w/BL
AFLR4    :         26            CAD geometry           0            STD w/BL
AFLR4    :         27            CAD geometry           0            STD w/BL
AFLR4    :         28            CAD geometry           0            STD w/BL
AFLR4    :         29            CAD geometry           0            STD w/BL
AFLR4    :         30            CAD geometry           0            STD w/BL
AFLR4    :         31            CAD geometry           0            STD w/BL
AFLR4    :         32            CAD geometry           0            STD w/BL
AFLR4    :         33            CAD geometry           0            STD w/BL
AFLR4    :         34            CAD geometry           0            STD w/BL
AFLR4    :         35            CAD geometry           0            STD w/BL
AFLR4    :         36            CAD geometry           0            STD w/BL
AFLR4    :         37            CAD geometry           0            STD w/BL
AFLR4    :         38            CAD geometry           0            STD w/BL
AFLR4    :         39            CAD geometry           0            STD w/BL
AFLR4    :         40            CAD geometry           0            STD w/BL
AFLR4    :         41            CAD geometry           0            STD w/BL
AFLR4    :         42            CAD geometry           0            STD w/BL
AFLR4    :         43            CAD geometry           0            STD w/BL
AFLR4    :         44            CAD geometry           0            STD w/BL
AFLR4    :         45            CAD geometry           0            STD w/BL
AFLR4    :         46            CAD geometry           0            STD w/BL
AFLR4    :         47            CAD geometry           0            STD w/BL
AFLR4    :         48            CAD geometry           0            STD w/BL
AFLR4    :         49            CAD geometry           0            STD w/BL
AFLR4    :         50            CAD geometry           0            STD w/BL
AFLR4    :         51            CAD geometry           0            STD w/BL
AFLR4    :         52            CAD geometry           0            STD w/BL
AFLR4    :         53            CAD geometry           0            STD w/BL
AFLR4    :         54            CAD geometry           0            STD w/BL
AFLR4    :         55            CAD geometry           0            STD w/BL
AFLR4    :         56            CAD geometry           0            STD w/BL
AFLR4    :         57            CAD geometry           0            STD w/BL
AFLR4    :         58            CAD geometry           0            STD w/BL
AFLR4    :         59            CAD geometry           0            STD w/BL
AFLR4    :         60            CAD geometry           0            STD w/BL
AFLR4    :         61            CAD geometry           0            STD w/BL
AFLR4    :         62            CAD geometry           0            STD w/BL
AFLR4    :         63            CAD geometry           0            STD w/BL
AFLR4    :         64            CAD geometry           0            STD w/BL
AFLR4    :         65            CAD geometry           0            STD w/BL
AFLR4    :         66            CAD geometry           0            STD w/BL
AFLR4    :         67            CAD geometry           0            STD w/BL
AFLR4    :         68            CAD geometry           0            STD w/BL
AFLR4    :         69            CAD geometry           0            STD w/BL
AFLR4    :         70            CAD geometry           0            STD w/BL
AFLR4    :         71            CAD geometry           0            STD w/BL
AFLR4    :         72            CAD geometry           0            STD w/BL
AFLR4    :         73            CAD geometry           0            STD w/BL
AFLR4    :         74            CAD geometry           0            STD w/BL
AFLR4    :         75            CAD geometry           0            STD w/BL
AFLR4    :         76            CAD geometry           0            STD w/BL
AFLR4    :         77            CAD geometry           0            STD w/BL
AFLR4    :         78            CAD geometry           0            STD w/BL
AFLR4    :         79            CAD geometry           0            STD w/BL
AFLR4    :         80            CAD geometry           0            STD w/BL
AFLR4    :         81            CAD geometry           0            STD w/BL
AFLR4    :         82            CAD geometry           0            STD w/BL
AFLR4    :         83            CAD geometry           0            STD w/BL
AFLR4    :         84            CAD geometry           0            STD w/BL
AFLR4    :         85            CAD geometry           0            STD w/BL
AFLR4    :         86            CAD geometry           0            STD w/BL
AFLR4    :         87            CAD geometry           0            STD w/BL
AFLR4    :         88            CAD geometry           0            STD w/BL
AFLR4    :         89            CAD geometry           0            STD w/BL
AFLR4    :         90            CAD geometry           0            STD w/BL
AFLR4    :         91            CAD geometry           0            STD w/BL
AFLR4    :         92            CAD geometry           0            STD w/BL
AFLR4    :         93            CAD geometry           0            STD w/BL
AFLR4    :         94            CAD geometry           0            STD w/BL
AFLR4    :         95            CAD geometry           0            STD w/BL
AFLR4    :         96            CAD geometry           0            STD w/BL
AFLR4    :         97            CAD geometry           0            STD w/BL
AFLR4    :         98            CAD geometry           0            STD w/BL
AFLR4    :         99            CAD geometry           0            STD w/BL
AFLR4    :        100            CAD geometry           0            STD w/BL
AFLR4    :        101            CAD geometry           0            STD w/BL
AFLR4    :        102            CAD geometry           0            STD w/BL
AFLR4    :        103            CAD geometry           0            STD w/BL
AFLR4    :        104            CAD geometry           0            STD w/BL
AFLR4    :        105            CAD geometry           0            STD w/BL
AFLR4    :        106            CAD geometry           0            STD w/BL
AFLR4    :        107            CAD geometry           0            STD w/BL
AFLR4    :        108            CAD geometry           0            STD w/BL
AFLR4    :        109            CAD geometry           0            STD w/BL
AFLR4    :        110            CAD geometry           0            STD w/BL
AFLR4    :        111            CAD geometry           0            STD w/BL
AFLR4    :        112            CAD geometry           0            STD w/BL
AFLR4    :        113            CAD geometry           0            FARFIELD
AFLR4    :        114            CAD geometry           0            FARFIELD
AFLR4    :        115            CAD geometry           0            FARFIELD
AFLR4    :        116            CAD geometry           0            FARFIELD
AFLR4    :        117            CAD geometry           0            FARFIELD
AFLR4    :        118            CAD geometry           0            FARFIELD

AFLR4    : Case has 10 Proximity Checking Components

AFLR4    : Component 1 includes Definitions 1 2 3 4 7 8 11 12 22
AFLR4    : Component 2 includes Definitions 5 6 9 10 15 16 17 18 19 25 26 27 28
AFLR4    :                                  31 37 38 39 40 41 42 43 51 52 53 54
AFLR4    :                                  55 56 57 68 69 70 71 72 73 77 78 82
AFLR4    :                                  83 84 88 89 93 97
AFLR4    : Component 3 includes Definitions 13 14 23 24 33 34 35 36 47 48 49 50
AFLR4    :                                  74 75 76 98 99 103 104
AFLR4    : Component 4 includes Definitions 32 46 60 61 62 63 79 80 81 108 109
AFLR4    : Component 5 includes Definitions 44 45 58 59 64 65 66 67 85 86 87
AFLR4    : Component 6 includes Definitions 20 21 29 30 90 91 92
AFLR4    : Component 7 includes Definitions 94 95 96
AFLR4    : Component 8 includes Definitions 100 101 102
AFLR4    : Component 9 includes Definitions 105 106 107
AFLR4    : Component 10 includes Definitions 110 111 112

AFLR4    : Define CAD surface definition 1
AFLR4    : Define CAD surface definition 2
AFLR4    : Define CAD surface definition 3
AFLR4    : Define CAD surface definition 4
AFLR4    : Define CAD surface definition 5
AFLR4    : Define CAD surface definition 6
AFLR4    : Define CAD surface definition 7
AFLR4    : Define CAD surface definition 8
AFLR4    : Define CAD surface definition 9
AFLR4    : Define CAD surface definition 10
AFLR4    : Define CAD surface definition 11
AFLR4    : Define CAD surface definition 12
AFLR4    : Define CAD surface definition 13
AFLR4    : Define CAD surface definition 14
AFLR4    : Define CAD surface definition 15
AFLR4    : Define CAD surface definition 16
AFLR4    : Define CAD surface definition 17
AFLR4    : Define CAD surface definition 18
AFLR4    : Define CAD surface definition 19
AFLR4    : Define CAD surface definition 20
AFLR4    : Define CAD surface definition 21
AFLR4    : Define CAD surface definition 22
AFLR4    : Define CAD surface definition 23
AFLR4    : Define CAD surface definition 24
AFLR4    : Define CAD surface definition 25
AFLR4    : Define CAD surface definition 26
AFLR4    : Define CAD surface definition 27
AFLR4    : Define CAD surface definition 28
AFLR4    : Define CAD surface definition 29
AFLR4    : Define CAD surface definition 30
AFLR4    : Define CAD surface definition 31
AFLR4    : Define CAD surface definition 32
AFLR4    : Define CAD surface definition 33
AFLR4    : Define CAD surface definition 34
AFLR4    : Define CAD surface definition 35
AFLR4    : Define CAD surface definition 36
AFLR4    : Define CAD surface definition 37
AFLR4    : Define CAD surface definition 38
AFLR4    : Define CAD surface definition 39
AFLR4    : Define CAD surface definition 40
AFLR4    : Define CAD surface definition 41
AFLR4    : Define CAD surface definition 42
AFLR4    : Define CAD surface definition 43
AFLR4    : Define CAD surface definition 44
AFLR4    : Define CAD surface definition 45
AFLR4    : Define CAD surface definition 46
AFLR4    : Define CAD surface definition 47
AFLR4    : Define CAD surface definition 48
AFLR4    : Define CAD surface definition 49
AFLR4    : Define CAD surface definition 50
AFLR4    : Define CAD surface definition 51
AFLR4    : Define CAD surface definition 52
AFLR4    : Define CAD surface definition 53
AFLR4    : Define CAD surface definition 54
AFLR4    : Define CAD surface definition 55
AFLR4    : Define CAD surface definition 56
AFLR4    : Define CAD surface definition 57
AFLR4    : Define CAD surface definition 58
AFLR4    : Define CAD surface definition 59
AFLR4    : Define CAD surface definition 60
AFLR4    : Define CAD surface definition 61
AFLR4    : Define CAD surface definition 62
AFLR4    : Define CAD surface definition 63
AFLR4    : Define CAD surface definition 64
AFLR4    : Define CAD surface definition 65
AFLR4    : Define CAD surface definition 66
AFLR4    : Define CAD surface definition 67
AFLR4    : Define CAD surface definition 68
AFLR4    : Define CAD surface definition 69
AFLR4    : Define CAD surface definition 70
AFLR4    : Define CAD surface definition 71
AFLR4    : Define CAD surface definition 72
AFLR4    : Define CAD surface definition 73
AFLR4    : Define CAD surface definition 74
AFLR4    : Define CAD surface definition 75
AFLR4    : Define CAD surface definition 76
AFLR4    : Define CAD surface definition 77
AFLR4    : Define CAD surface definition 78
AFLR4    : Define CAD surface definition 79
AFLR4    : Define CAD surface definition 80
AFLR4    : Define CAD surface definition 81
AFLR4    : Define CAD surface definition 82
AFLR4    : Define CAD surface definition 83
AFLR4    : Define CAD surface definition 84
AFLR4    : Define CAD surface definition 85
AFLR4    : Define CAD surface definition 86
AFLR4    : Define CAD surface definition 87
AFLR4    : Define CAD surface definition 88
AFLR4    : Define CAD surface definition 89
AFLR4    : Define CAD surface definition 90
AFLR4    : Define CAD surface definition 91
AFLR4    : Define CAD surface definition 92
AFLR4    : Define CAD surface definition 93
AFLR4    : Define CAD surface definition 94
AFLR4    : Define CAD surface definition 95
AFLR4    : Define CAD surface definition 96
AFLR4    : Define CAD surface definition 97
AFLR4    : Define CAD surface definition 98
AFLR4    : Define CAD surface definition 99
AFLR4    : Define CAD surface definition 100
AFLR4    : Define CAD surface definition 101
AFLR4    : Define CAD surface definition 102
AFLR4    : Define CAD surface definition 103
AFLR4    : Define CAD surface definition 104
AFLR4    : Define CAD surface definition 105
AFLR4    : Define CAD surface definition 106
AFLR4    : Define CAD surface definition 107
AFLR4    : Define CAD surface definition 108
AFLR4    : Define CAD surface definition 109
AFLR4    : Define CAD surface definition 110
AFLR4    : Define CAD surface definition 111
AFLR4    : Define CAD surface definition 112
AFLR4    : Define CAD surface definition 113
AFLR4    : Define CAD surface definition 114
AFLR4    : Define CAD surface definition 115
AFLR4    : Define CAD surface definition 116
AFLR4    : Define CAD surface definition 117
AFLR4    : Define CAD surface definition 118

AFLR4    : Surface Grid Generation

AFLR4    : Generate optimal mesh on surface definition 1
AFLR2    : Nodes, Trias,Quads=       201       301         0
AFLR4    : Nodes, Trias,Quads=       184       267         0

AFLR4    : Generate optimal mesh on surface definition 2
AFLR2    : Nodes, Trias,Quads=       201       301         0
AFLR4    : Nodes, Trias,Quads=       183       265         0

AFLR4    : Generate optimal mesh on surface definition 3
AFLR2    : Nodes, Trias,Quads=       148       243         0
AFLR4    : Nodes, Trias,Quads=        92       131         0

AFLR4    : Generate optimal mesh on surface definition 4
AFLR2    : Nodes, Trias,Quads=       125       184         0
AFLR4    : Nodes, Trias,Quads=       134       202         0

AFLR4    : Generate optimal mesh on surface definition 5
AFLR2    : Nodes, Trias,Quads=       730      1326         0
AFLR4    : Nodes, Trias,Quads=       627      1120         0

AFLR4    : Generate optimal mesh on surface definition 6
AFLR2    : Nodes, Trias,Quads=       868      1583         0
AFLR4    : Nodes, Trias,Quads=       655      1157         0

AFLR4    : Generate optimal mesh on surface definition 7
AFLR2    : Nodes, Trias,Quads=       125       184         0
AFLR4    : Nodes, Trias,Quads=       133       200         0

AFLR4    : Generate optimal mesh on surface definition 8
AFLR2    : Nodes, Trias,Quads=       148       243         0
AFLR4    : Nodes, Trias,Quads=        91       129         0

AFLR4    : Generate optimal mesh on surface definition 9
AFLR2    : Nodes, Trias,Quads=       860      1567         0
AFLR4    : Nodes, Trias,Quads=       651      1149         0

AFLR4    : Generate optimal mesh on surface definition 10
AFLR2    : Nodes, Trias,Quads=       728      1322         0
AFLR4    : Nodes, Trias,Quads=       631      1128         0

AFLR4    : Generate optimal mesh on surface definition 11
AFLR2    : Nodes, Trias,Quads=        17        20         0
AFLR4    : Nodes, Trias,Quads=        12        10         0

AFLR4    : Generate optimal mesh on surface definition 12
AFLR2    : Nodes, Trias,Quads=       334       576         0
AFLR4    : Nodes, Trias,Quads=       211       330         0

AFLR4    : Generate optimal mesh on surface definition 13
AFLR2    : Nodes, Trias,Quads=       851      1557         0
AFLR4    : Nodes, Trias,Quads=       537       929         0

AFLR4    : Generate optimal mesh on surface definition 14
AFLR2    : Nodes, Trias,Quads=       833      1521         0
AFLR4    : Nodes, Trias,Quads=       543       941         0

AFLR4    : Generate optimal mesh on surface definition 15
AFLR2    : Nodes, Trias,Quads=        22        28         0
AFLR4    : Nodes, Trias,Quads=        14        12         0

AFLR4    : Generate optimal mesh on surface definition 16
AFLR2    : Nodes, Trias,Quads=        67        88         0
AFLR4    : Nodes, Trias,Quads=        46        46         0

AFLR4    : Generate optimal mesh on surface definition 17
AFLR2    : Nodes, Trias,Quads=        18        22         0
AFLR4    : Nodes, Trias,Quads=        12        10         0

AFLR4    : Generate optimal mesh on surface definition 18
AFLR2    : Nodes, Trias,Quads=      1997      3751         0
AFLR4    : Nodes, Trias,Quads=      1162      2081         0

AFLR4    : Generate optimal mesh on surface definition 19
AFLR2    : Nodes, Trias,Quads=      2014      3782         0
AFLR4    : Nodes, Trias,Quads=      1149      2052         0

AFLR4    : Generate optimal mesh on surface definition 20
AFLR2    : Nodes, Trias,Quads=        51        73         0
AFLR4    : Nodes, Trias,Quads=        44        59         0

AFLR4    : Generate optimal mesh on surface definition 21
AFLR2    : Nodes, Trias,Quads=        48        68         0
AFLR4    : Nodes, Trias,Quads=        43        58         0

AFLR4    : Generate optimal mesh on surface definition 22
AFLR2    : Nodes, Trias,Quads=       355       618         0
AFLR4    : Nodes, Trias,Quads=       213       334         0

AFLR4    : Generate optimal mesh on surface definition 23
AFLR2    : Nodes, Trias,Quads=       820      1495         0
AFLR4    : Nodes, Trias,Quads=       540       935         0

AFLR4    : Generate optimal mesh on surface definition 24
AFLR2    : Nodes, Trias,Quads=       861      1577         0
AFLR4    : Nodes, Trias,Quads=       543       941         0

AFLR4    : Generate optimal mesh on surface definition 25
AFLR2    : Nodes, Trias,Quads=      2005      3764         0
AFLR4    : Nodes, Trias,Quads=      1146      2046         0

AFLR4    : Generate optimal mesh on surface definition 26
AFLR2    : Nodes, Trias,Quads=        18        22         0
AFLR4    : Nodes, Trias,Quads=        12        10         0

AFLR4    : Generate optimal mesh on surface definition 27
AFLR2    : Nodes, Trias,Quads=        66        86         0
AFLR4    : Nodes, Trias,Quads=        46        46         0

AFLR4    : Generate optimal mesh on surface definition 28
AFLR2    : Nodes, Trias,Quads=        22        28         0
AFLR4    : Nodes, Trias,Quads=        14        12         0

AFLR4    : Generate optimal mesh on surface definition 29
AFLR2    : Nodes, Trias,Quads=        47        66         0
AFLR4    : Nodes, Trias,Quads=        43        58         0

AFLR4    : Generate optimal mesh on surface definition 30
AFLR2    : Nodes, Trias,Quads=        49        69         0
AFLR4    : Nodes, Trias,Quads=        44        59         0

AFLR4    : Generate optimal mesh on surface definition 31
AFLR2    : Nodes, Trias,Quads=      1993      3743         0
AFLR4    : Nodes, Trias,Quads=      1177      2111         0

AFLR4    : Generate optimal mesh on surface definition 32
AFLR2    : Nodes, Trias,Quads=       728      1310         0
AFLR4    : Nodes, Trias,Quads=       449       752         0

AFLR4    : Generate optimal mesh on surface definition 33
AFLR2    : Nodes, Trias,Quads=        31        40         0
AFLR4    : Nodes, Trias,Quads=        21        20         0

AFLR4    : Generate optimal mesh on surface definition 34
AFLR2    : Nodes, Trias,Quads=       100       132         0
AFLR4    : Nodes, Trias,Quads=        67        66         0

AFLR4    : Generate optimal mesh on surface definition 35
AFLR2    : Nodes, Trias,Quads=        30        38         0
AFLR4    : Nodes, Trias,Quads=        20        18         0

AFLR4    : Generate optimal mesh on surface definition 36
AFLR2    : Nodes, Trias,Quads=        29        36         0
AFLR4    : Nodes, Trias,Quads=        20        18         0

AFLR4    : Generate optimal mesh on surface definition 37
AFLR2    : Nodes, Trias,Quads=        18        22         0
AFLR4    : Nodes, Trias,Quads=        12        10         0

AFLR4    : Generate optimal mesh on surface definition 38
AFLR2    : Nodes, Trias,Quads=        79       105         0
AFLR4    : Nodes, Trias,Quads=        54        55         0

AFLR4    : Generate optimal mesh on surface definition 39
AFLR2    : Nodes, Trias,Quads=        35        47         0
AFLR4    : Nodes, Trias,Quads=        24        25         0

AFLR4    : Generate optimal mesh on surface definition 40
AFLR2    : Nodes, Trias,Quads=        35        47         0
AFLR4    : Nodes, Trias,Quads=        24        25         0

AFLR4    : Generate optimal mesh on surface definition 41
AFLR2    : Nodes, Trias,Quads=       121       160         0
AFLR4    : Nodes, Trias,Quads=        83        84         0

AFLR4    : Generate optimal mesh on surface definition 42
AFLR2    : Nodes, Trias,Quads=        28        36         0
AFLR4    : Nodes, Trias,Quads=        18        16         0

AFLR4    : Generate optimal mesh on surface definition 43
AFLR2    : Nodes, Trias,Quads=        17        20         0
AFLR4    : Nodes, Trias,Quads=        12        10         0

AFLR4    : Generate optimal mesh on surface definition 44
AFLR2    : Nodes, Trias,Quads=       361       650         0
AFLR4    : Nodes, Trias,Quads=       381       690         0

AFLR4    : Generate optimal mesh on surface definition 45
AFLR2    : Nodes, Trias,Quads=       363       654         0
AFLR4    : Nodes, Trias,Quads=       378       684         0

AFLR4    : Generate optimal mesh on surface definition 46
AFLR2    : Nodes, Trias,Quads=       725      1304         0
AFLR4    : Nodes, Trias,Quads=       446       746         0

AFLR4    : Generate optimal mesh on surface definition 47
AFLR2    : Nodes, Trias,Quads=        29        36         0
AFLR4    : Nodes, Trias,Quads=        20        18         0

AFLR4    : Generate optimal mesh on surface definition 48
AFLR2    : Nodes, Trias,Quads=        30        38         0
AFLR4    : Nodes, Trias,Quads=        20        18         0

AFLR4    : Generate optimal mesh on surface definition 49
AFLR2    : Nodes, Trias,Quads=       100       132         0
AFLR4    : Nodes, Trias,Quads=        67        66         0

AFLR4    : Generate optimal mesh on surface definition 50
AFLR2    : Nodes, Trias,Quads=        31        40         0
AFLR4    : Nodes, Trias,Quads=        21        20         0

AFLR4    : Generate optimal mesh on surface definition 51
AFLR2    : Nodes, Trias,Quads=        17        20         0
AFLR4    : Nodes, Trias,Quads=        12        10         0

AFLR4    : Generate optimal mesh on surface definition 52
AFLR2    : Nodes, Trias,Quads=        28        36         0
AFLR4    : Nodes, Trias,Quads=        18        16         0

AFLR4    : Generate optimal mesh on surface definition 53
AFLR2    : Nodes, Trias,Quads=       121       160         0
AFLR4    : Nodes, Trias,Quads=        83        84         0

AFLR4    : Generate optimal mesh on surface definition 54
AFLR2    : Nodes, Trias,Quads=        35        47         0
AFLR4    : Nodes, Trias,Quads=        24        25         0

AFLR4    : Generate optimal mesh on surface definition 55
AFLR2    : Nodes, Trias,Quads=        35        47         0
AFLR4    : Nodes, Trias,Quads=        24        25         0

AFLR4    : Generate optimal mesh on surface definition 56
AFLR2    : Nodes, Trias,Quads=        79       105         0
AFLR4    : Nodes, Trias,Quads=        54        55         0

AFLR4    : Generate optimal mesh on surface definition 57
AFLR2    : Nodes, Trias,Quads=        18        22         0
AFLR4    : Nodes, Trias,Quads=        12        10         0

AFLR4    : Generate optimal mesh on surface definition 58
AFLR2    : Nodes, Trias,Quads=       360       648         0
AFLR4    : Nodes, Trias,Quads=       380       688         0

AFLR4    : Generate optimal mesh on surface definition 59
AFLR2    : Nodes, Trias,Quads=       360       648         0
AFLR4    : Nodes, Trias,Quads=       379       686         0

AFLR4    : Generate optimal mesh on surface definition 60
AFLR2    : Nodes, Trias,Quads=        30        38         0
AFLR4    : Nodes, Trias,Quads=        20        18         0

AFLR4    : Generate optimal mesh on surface definition 61
AFLR2    : Nodes, Trias,Quads=        97       128         0
AFLR4    : Nodes, Trias,Quads=        65        64         0

AFLR4    : Generate optimal mesh on surface definition 62
AFLR2    : Nodes, Trias,Quads=        42        54         0
AFLR4    : Nodes, Trias,Quads=        32        34         0

AFLR4    : Generate optimal mesh on surface definition 63
AFLR2    : Nodes, Trias,Quads=        35        44         0
AFLR4    : Nodes, Trias,Quads=        24        22         0

AFLR4    : Generate optimal mesh on surface definition 64
AFLR2    : Nodes, Trias,Quads=       235       406         0
AFLR4    : Nodes, Trias,Quads=       211       358         0

AFLR4    : Generate optimal mesh on surface definition 65
AFLR2    : Nodes, Trias,Quads=       235       406         0
AFLR4    : Nodes, Trias,Quads=       212       360         0

AFLR4    : Generate optimal mesh on surface definition 66
AFLR2    : Nodes, Trias,Quads=       235       406         0
AFLR4    : Nodes, Trias,Quads=       211       358         0

AFLR4    : Generate optimal mesh on surface definition 67
AFLR2    : Nodes, Trias,Quads=       235       406         0
AFLR4    : Nodes, Trias,Quads=       212       360         0

AFLR4    : Generate optimal mesh on surface definition 68
AFLR2    : Nodes, Trias,Quads=       206       330         0
AFLR4    : Nodes, Trias,Quads=       151       220         0

AFLR4    : Generate optimal mesh on surface definition 69
AFLR2    : Nodes, Trias,Quads=        22        29         0
AFLR4    : Nodes, Trias,Quads=        13        11         0

AFLR4    : Generate optimal mesh on surface definition 70
AFLR2    : Nodes, Trias,Quads=       127       168         0
AFLR4    : Nodes, Trias,Quads=        87        88         0

AFLR4    : Generate optimal mesh on surface definition 71
AFLR2    : Nodes, Trias,Quads=        25        32         0
AFLR4    : Nodes, Trias,Quads=        16        14         0

AFLR4    : Generate optimal mesh on surface definition 72
AFLR2    : Nodes, Trias,Quads=       208       333         0
AFLR4    : Nodes, Trias,Quads=       157       231         0

AFLR4    : Generate optimal mesh on surface definition 73
AFLR2    : Nodes, Trias,Quads=       119       185         0
AFLR4    : Nodes, Trias,Quads=        98       143         0

AFLR4    : Generate optimal mesh on surface definition 74
AFLR2    : Nodes, Trias,Quads=        18        22         0
AFLR4    : Nodes, Trias,Quads=        12        10         0

AFLR4    : Generate optimal mesh on surface definition 75
AFLR2    : Nodes, Trias,Quads=        79       104         0
AFLR4    : Nodes, Trias,Quads=        55        56         0

AFLR4    : Generate optimal mesh on surface definition 76
AFLR2    : Nodes, Trias,Quads=        18        22         0
AFLR4    : Nodes, Trias,Quads=        12        10         0

AFLR4    : Generate optimal mesh on surface definition 77
AFLR2    : Nodes, Trias,Quads=       119       185         0
AFLR4    : Nodes, Trias,Quads=       100       147         0

AFLR4    : Generate optimal mesh on surface definition 78
AFLR2    : Nodes, Trias,Quads=       106       165         0
AFLR4    : Nodes, Trias,Quads=        97       147         0

AFLR4    : Generate optimal mesh on surface definition 79
AFLR2    : Nodes, Trias,Quads=        22        28         0
AFLR4    : Nodes, Trias,Quads=        14        12         0

AFLR4    : Generate optimal mesh on surface definition 80
AFLR2    : Nodes, Trias,Quads=        68        89         0
AFLR4    : Nodes, Trias,Quads=        47        47         0

AFLR4    : Generate optimal mesh on surface definition 81
AFLR2    : Nodes, Trias,Quads=        18        22         0
AFLR4    : Nodes, Trias,Quads=        12        10         0

AFLR4    : Generate optimal mesh on surface definition 82
AFLR2    : Nodes, Trias,Quads=       111       174         0
AFLR4    : Nodes, Trias,Quads=       103       158         0

AFLR4    : Generate optimal mesh on surface definition 83
AFLR2    : Nodes, Trias,Quads=       110       172         0
AFLR4    : Nodes, Trias,Quads=       103       158         0

AFLR4    : Generate optimal mesh on surface definition 84
AFLR2    : Nodes, Trias,Quads=       106       165         0
AFLR4    : Nodes, Trias,Quads=        97       147         0

AFLR4    : Generate optimal mesh on surface definition 85
AFLR2    : Nodes, Trias,Quads=        18        22         0
AFLR4    : Nodes, Trias,Quads=        12        10         0

AFLR4    : Generate optimal mesh on surface definition 86
AFLR2    : Nodes, Trias,Quads=        69        91         0
AFLR4    : Nodes, Trias,Quads=        47        47         0

AFLR4    : Generate optimal mesh on surface definition 87
AFLR2    : Nodes, Trias,Quads=        22        28         0
AFLR4    : Nodes, Trias,Quads=        14        12         0

AFLR4    : Generate optimal mesh on surface definition 88
AFLR2    : Nodes, Trias,Quads=       119       185         0
AFLR4    : Nodes, Trias,Quads=       100       147         0

AFLR4    : Generate optimal mesh on surface definition 89
AFLR2    : Nodes, Trias,Quads=       120       187         0
AFLR4    : Nodes, Trias,Quads=        98       143         0

AFLR4    : Generate optimal mesh on surface definition 90
AFLR2    : Nodes, Trias,Quads=        18        22         0
AFLR4    : Nodes, Trias,Quads=        12        10         0

AFLR4    : Generate optimal mesh on surface definition 91
AFLR2    : Nodes, Trias,Quads=        79       104         0
AFLR4    : Nodes, Trias,Quads=        55        56         0

AFLR4    : Generate optimal mesh on surface definition 92
AFLR2    : Nodes, Trias,Quads=        18        22         0
AFLR4    : Nodes, Trias,Quads=        12        10         0

AFLR4    : Generate optimal mesh on surface definition 93
AFLR2    : Nodes, Trias,Quads=       207       331         0
AFLR4    : Nodes, Trias,Quads=       155       227         0

AFLR4    : Generate optimal mesh on surface definition 94
AFLR2    : Nodes, Trias,Quads=        25        32         0
AFLR4    : Nodes, Trias,Quads=        16        14         0

AFLR4    : Generate optimal mesh on surface definition 95
AFLR2    : Nodes, Trias,Quads=       127       168         0
AFLR4    : Nodes, Trias,Quads=        87        88         0

AFLR4    : Generate optimal mesh on surface definition 96
AFLR2    : Nodes, Trias,Quads=        22        29         0
AFLR4    : Nodes, Trias,Quads=        13        11         0

AFLR4    : Generate optimal mesh on surface definition 97
AFLR2    : Nodes, Trias,Quads=       207       332         0
AFLR4    : Nodes, Trias,Quads=       152       222         0

AFLR4    : Generate optimal mesh on surface definition 98
AFLR2    : Nodes, Trias,Quads=       229       388         0
AFLR4    : Nodes, Trias,Quads=       171       272         0

AFLR4    : Generate optimal mesh on surface definition 99
AFLR2    : Nodes, Trias,Quads=       227       384         0
AFLR4    : Nodes, Trias,Quads=       172       274         0

AFLR4    : Generate optimal mesh on surface definition 100
AFLR2    : Nodes, Trias,Quads=        30        38         0
AFLR4    : Nodes, Trias,Quads=        21        20         0

AFLR4    : Generate optimal mesh on surface definition 101
AFLR2    : Nodes, Trias,Quads=       100       132         0
AFLR4    : Nodes, Trias,Quads=        67        66         0

AFLR4    : Generate optimal mesh on surface definition 102
AFLR2    : Nodes, Trias,Quads=        30        38         0
AFLR4    : Nodes, Trias,Quads=        21        20         0

AFLR4    : Generate optimal mesh on surface definition 103
AFLR2    : Nodes, Trias,Quads=       225       380         0
AFLR4    : Nodes, Trias,Quads=       172       274         0

AFLR4    : Generate optimal mesh on surface definition 104
AFLR2    : Nodes, Trias,Quads=       228       386         0
AFLR4    : Nodes, Trias,Quads=       172       274         0

AFLR4    : Generate optimal mesh on surface definition 105
AFLR2    : Nodes, Trias,Quads=        30        38         0
AFLR4    : Nodes, Trias,Quads=        21        20         0

AFLR4    : Generate optimal mesh on surface definition 106
AFLR2    : Nodes, Trias,Quads=       100       132         0
AFLR4    : Nodes, Trias,Quads=        67        66         0

AFLR4    : Generate optimal mesh on surface definition 107
AFLR2    : Nodes, Trias,Quads=        30        38         0
AFLR4    : Nodes, Trias,Quads=        21        20         0

AFLR4    : Generate optimal mesh on surface definition 108
AFLR2    : Nodes, Trias,Quads=       244       418         0
AFLR4    : Nodes, Trias,Quads=       180       290         0

AFLR4    : Generate optimal mesh on surface definition 109
AFLR2    : Nodes, Trias,Quads=       245       420         0
AFLR4    : Nodes, Trias,Quads=       180       290         0

AFLR4    : Generate optimal mesh on surface definition 110
AFLR2    : Nodes, Trias,Quads=        30        38         0
AFLR4    : Nodes, Trias,Quads=        21        20         0

AFLR4    : Generate optimal mesh on surface definition 111
AFLR2    : Nodes, Trias,Quads=       100       132         0
AFLR4    : Nodes, Trias,Quads=        67        66         0

AFLR4    : Generate optimal mesh on surface definition 112
AFLR2    : Nodes, Trias,Quads=        30        38         0
AFLR4    : Nodes, Trias,Quads=        21        20         0

AFLR4    : Generate optimal mesh on surface definition 113
AFLR2    : Nodes, Trias,Quads=         5         4         0
AFLR4    : Nodes, Trias,Quads=         4         2         0

AFLR4    : Generate optimal mesh on surface definition 114
AFLR2    : Nodes, Trias,Quads=         5         4         0
AFLR4    : Nodes, Trias,Quads=         4         2         0

AFLR4    : Generate optimal mesh on surface definition 115
AFLR2    : Nodes, Trias,Quads=         5         4         0
AFLR4    : Nodes, Trias,Quads=         4         2         0

AFLR4    : Generate optimal mesh on surface definition 116
AFLR2    : Nodes, Trias,Quads=         5         4         0
AFLR4    : Nodes, Trias,Quads=         4         2         0

AFLR4    : Generate optimal mesh on surface definition 117
AFLR2    : Nodes, Trias,Quads=         5         4         0
AFLR4    : Nodes, Trias,Quads=         4         2         0

AFLR4    : Generate optimal mesh on surface definition 118
AFLR2    : Nodes, Trias,Quads=         5         4         0
AFLR4    : Nodes, Trias,Quads=         4         2         0

DGEOM    : Add surface definitions to composite definition 0
DGEOM    : Glue composite surface definition 0
DGEOM    : Nodes,Faces,BEdges=     14994     29952      6594

AFLR4    : Curvature BG Surface Grid Generation

AFLR4    : Nodes, Faces      =     14994     29952

AFLR4    : Surface Grid Generation

AFLR4    : Generate optimal mesh on surface definition 1
AFLR2    : Nodes, Trias,Quads=       221       333         0
AFLR4    : Nodes, Trias,Quads=       306       503         0

AFLR4    : Generate optimal mesh on surface definition 2
AFLR2    : Nodes, Trias,Quads=       217       326         0
AFLR4    : Nodes, Trias,Quads=       291       474         0

AFLR4    : Generate optimal mesh on surface definition 3
AFLR2    : Nodes, Trias,Quads=       193       323         0
AFLR4    : Nodes, Trias,Quads=       128       193         0

AFLR4    : Generate optimal mesh on surface definition 4
AFLR2    : Nodes, Trias,Quads=       149       226         0
AFLR4    : Nodes, Trias,Quads=       165       258         0

AFLR4    : Generate optimal mesh on surface definition 5
AFLR2    : Nodes, Trias,Quads=       764      1394         0
AFLR4    : Nodes, Trias,Quads=       758      1382         0

AFLR4    : Generate optimal mesh on surface definition 6
AFLR2    : Nodes, Trias,Quads=       882      1611         0
AFLR4    : Nodes, Trias,Quads=       823      1493         0

AFLR4    : Generate optimal mesh on surface definition 7
AFLR2    : Nodes, Trias,Quads=       150       228         0
AFLR4    : Nodes, Trias,Quads=       161       250         0

AFLR4    : Generate optimal mesh on surface definition 8
AFLR2    : Nodes, Trias,Quads=       192       321         0
AFLR4    : Nodes, Trias,Quads=       124       185         0

AFLR4    : Generate optimal mesh on surface definition 9
AFLR2    : Nodes, Trias,Quads=       855      1559         0
AFLR4    : Nodes, Trias,Quads=       812      1473         0

AFLR4    : Generate optimal mesh on surface definition 10
AFLR2    : Nodes, Trias,Quads=       764      1395         0
AFLR4    : Nodes, Trias,Quads=       760      1387         0

AFLR4    : Generate optimal mesh on surface definition 11
AFLR2    : Nodes, Trias,Quads=        18        22         0
AFLR4    : Nodes, Trias,Quads=        14        14         0

AFLR4    : Generate optimal mesh on surface definition 12
AFLR2    : Nodes, Trias,Quads=       399       695         0
AFLR4    : Nodes, Trias,Quads=       325       547         0

AFLR4    : Generate optimal mesh on surface definition 13
AFLR2    : Nodes, Trias,Quads=       873      1599         0
AFLR4    : Nodes, Trias,Quads=       615      1083         0

AFLR4    : Generate optimal mesh on surface definition 14
AFLR2    : Nodes, Trias,Quads=       858      1570         0
AFLR4    : Nodes, Trias,Quads=       606      1066         0

AFLR4    : Generate optimal mesh on surface definition 15
AFLR2    : Nodes, Trias,Quads=        21        26         0
AFLR4    : Nodes, Trias,Quads=        14        12         0

AFLR4    : Generate optimal mesh on surface definition 16
AFLR2    : Nodes, Trias,Quads=        62        80         0
AFLR4    : Nodes, Trias,Quads=        42        40         0

AFLR4    : Generate optimal mesh on surface definition 17
AFLR2    : Nodes, Trias,Quads=        18        22         0
AFLR4    : Nodes, Trias,Quads=        12        10         0

AFLR4    : Generate optimal mesh on surface definition 18
AFLR2    : Nodes, Trias,Quads=      2052      3855         0
AFLR4    : Nodes, Trias,Quads=      1330      2411         0

AFLR4    : Generate optimal mesh on surface definition 19
AFLR2    : Nodes, Trias,Quads=      2043      3837         0
AFLR4    : Nodes, Trias,Quads=      1290      2331         0

AFLR4    : Generate optimal mesh on surface definition 20
AFLR2    : Nodes, Trias,Quads=        75       115         0
AFLR4    : Nodes, Trias,Quads=        52        69         0

AFLR4    : Generate optimal mesh on surface definition 21
AFLR2    : Nodes, Trias,Quads=        70       106         0
AFLR4    : Nodes, Trias,Quads=        50        66         0

AFLR4    : Generate optimal mesh on surface definition 22
AFLR2    : Nodes, Trias,Quads=       433       763         0
AFLR4    : Nodes, Trias,Quads=       326       549         0

AFLR4    : Generate optimal mesh on surface definition 23
AFLR2    : Nodes, Trias,Quads=       851      1556         0
AFLR4    : Nodes, Trias,Quads=       602      1058         0

AFLR4    : Generate optimal mesh on surface definition 24
AFLR2    : Nodes, Trias,Quads=       880      1613         0
AFLR4    : Nodes, Trias,Quads=       627      1107         0

AFLR4    : Generate optimal mesh on surface definition 25
AFLR2    : Nodes, Trias,Quads=      2033      3817         0
AFLR4    : Nodes, Trias,Quads=      1281      2313         0

AFLR4    : Generate optimal mesh on surface definition 26
AFLR2    : Nodes, Trias,Quads=        18        22         0
AFLR4    : Nodes, Trias,Quads=        12        10         0

AFLR4    : Generate optimal mesh on surface definition 27
AFLR2    : Nodes, Trias,Quads=        61        79         0
AFLR4    : Nodes, Trias,Quads=        41        39         0

AFLR4    : Generate optimal mesh on surface definition 28
AFLR2    : Nodes, Trias,Quads=        20        25         0
AFLR4    : Nodes, Trias,Quads=        13        11         0

AFLR4    : Generate optimal mesh on surface definition 29
AFLR2    : Nodes, Trias,Quads=        64        96         0
AFLR4    : Nodes, Trias,Quads=        47        62         0

AFLR4    : Generate optimal mesh on surface definition 30
AFLR2    : Nodes, Trias,Quads=        66        99         0
AFLR4    : Nodes, Trias,Quads=        49        65         0

AFLR4    : Generate optimal mesh on surface definition 31
AFLR2    : Nodes, Trias,Quads=      2044      3840         0
AFLR4    : Nodes, Trias,Quads=      1321      2394         0

AFLR4    : Generate optimal mesh on surface definition 32
AFLR2    : Nodes, Trias,Quads=       749      1351         0
AFLR4    : Nodes, Trias,Quads=       492       837         0

AFLR4    : Generate optimal mesh on surface definition 33
AFLR2    : Nodes, Trias,Quads=        31        40         0
AFLR4    : Nodes, Trias,Quads=        20        18         0

AFLR4    : Generate optimal mesh on surface definition 34
AFLR2    : Nodes, Trias,Quads=       102       137         0
AFLR4    : Nodes, Trias,Quads=        65        63         0

AFLR4    : Generate optimal mesh on surface definition 35
AFLR2    : Nodes, Trias,Quads=        28        36         0
AFLR4    : Nodes, Trias,Quads=        18        16         0

AFLR4    : Generate optimal mesh on surface definition 36
AFLR2    : Nodes, Trias,Quads=        34        44         0
AFLR4    : Nodes, Trias,Quads=        22        20         0

AFLR4    : Generate optimal mesh on surface definition 37
AFLR2    : Nodes, Trias,Quads=        18        22         0
AFLR4    : Nodes, Trias,Quads=        12        10         0

AFLR4    : Generate optimal mesh on surface definition 38
AFLR2    : Nodes, Trias,Quads=        79       105         0
AFLR4    : Nodes, Trias,Quads=        52        51         0

AFLR4    : Generate optimal mesh on surface definition 39
AFLR2    : Nodes, Trias,Quads=        34        44         0
AFLR4    : Nodes, Trias,Quads=        25        26         0

AFLR4    : Generate optimal mesh on surface definition 40
AFLR2    : Nodes, Trias,Quads=        34        44         0
AFLR4    : Nodes, Trias,Quads=        25        26         0

AFLR4    : Generate optimal mesh on surface definition 41
AFLR2    : Nodes, Trias,Quads=       133       181         0
AFLR4    : Nodes, Trias,Quads=        84        83         0

AFLR4    : Generate optimal mesh on surface definition 42
AFLR2    : Nodes, Trias,Quads=        25        32         0
AFLR4    : Nodes, Trias,Quads=        16        14         0

AFLR4    : Generate optimal mesh on surface definition 43
AFLR2    : Nodes, Trias,Quads=        21        26         0
AFLR4    : Nodes, Trias,Quads=        14        12         0

AFLR4    : Generate optimal mesh on surface definition 44
AFLR2    : Nodes, Trias,Quads=       490       896         0
AFLR4    : Nodes, Trias,Quads=       448       812         0

AFLR4    : Generate optimal mesh on surface definition 45
AFLR2    : Nodes, Trias,Quads=       486       888         0
AFLR4    : Nodes, Trias,Quads=       442       800         0

AFLR4    : Generate optimal mesh on surface definition 46
AFLR2    : Nodes, Trias,Quads=       739      1330         0
AFLR4    : Nodes, Trias,Quads=       479       810         0

AFLR4    : Generate optimal mesh on surface definition 47
AFLR2    : Nodes, Trias,Quads=        34        44         0
AFLR4    : Nodes, Trias,Quads=        22        20         0

AFLR4    : Generate optimal mesh on surface definition 48
AFLR2    : Nodes, Trias,Quads=        27        34         0
AFLR4    : Nodes, Trias,Quads=        18        16         0

AFLR4    : Generate optimal mesh on surface definition 49
AFLR2    : Nodes, Trias,Quads=        97       127         0
AFLR4    : Nodes, Trias,Quads=        65        63         0

AFLR4    : Generate optimal mesh on surface definition 50
AFLR2    : Nodes, Trias,Quads=        31        40         0
AFLR4    : Nodes, Trias,Quads=        20        18         0

AFLR4    : Generate optimal mesh on surface definition 51
AFLR2    : Nodes, Trias,Quads=        21        26         0
AFLR4    : Nodes, Trias,Quads=        14        12         0

AFLR4    : Generate optimal mesh on surface definition 52
AFLR2    : Nodes, Trias,Quads=        23        29         0
AFLR4    : Nodes, Trias,Quads=        15        13         0

AFLR4    : Generate optimal mesh on surface definition 53
AFLR2    : Nodes, Trias,Quads=       133       183         0
AFLR4    : Nodes, Trias,Quads=        82        81         0

AFLR4    : Generate optimal mesh on surface definition 54
AFLR2    : Nodes, Trias,Quads=        34        44         0
AFLR4    : Nodes, Trias,Quads=        25        26         0

AFLR4    : Generate optimal mesh on surface definition 55
AFLR2    : Nodes, Trias,Quads=        34        44         0
AFLR4    : Nodes, Trias,Quads=        25        26         0

AFLR4    : Generate optimal mesh on surface definition 56
AFLR2    : Nodes, Trias,Quads=        80       107         0
AFLR4    : Nodes, Trias,Quads=        53        53         0

AFLR4    : Generate optimal mesh on surface definition 57
AFLR2    : Nodes, Trias,Quads=        18        22         0
AFLR4    : Nodes, Trias,Quads=        12        10         0

AFLR4    : Generate optimal mesh on surface definition 58
AFLR2    : Nodes, Trias,Quads=       456       830         0
AFLR4    : Nodes, Trias,Quads=       432       782         0

AFLR4    : Generate optimal mesh on surface definition 59
AFLR2    : Nodes, Trias,Quads=       452       822         0
AFLR4    : Nodes, Trias,Quads=       419       756         0

AFLR4    : Generate optimal mesh on surface definition 60
AFLR2    : Nodes, Trias,Quads=        31        40         0
AFLR4    : Nodes, Trias,Quads=        20        18         0

AFLR4    : Generate optimal mesh on surface definition 61
AFLR2    : Nodes, Trias,Quads=        89       117         0
AFLR4    : Nodes, Trias,Quads=        59        57         0

AFLR4    : Generate optimal mesh on surface definition 62
AFLR2    : Nodes, Trias,Quads=        37        47         0
AFLR4    : Nodes, Trias,Quads=        28        29         0

AFLR4    : Generate optimal mesh on surface definition 63
AFLR2    : Nodes, Trias,Quads=        45        61         0
AFLR4    : Nodes, Trias,Quads=        27        25         0

AFLR4    : Generate optimal mesh on surface definition 64
AFLR2    : Nodes, Trias,Quads=       316       558         0
AFLR4    : Nodes, Trias,Quads=       274       474         0

AFLR4    : Generate optimal mesh on surface definition 65
AFLR2    : Nodes, Trias,Quads=       315       556         0
AFLR4    : Nodes, Trias,Quads=       275       476         0

AFLR4    : Generate optimal mesh on surface definition 66
AFLR2    : Nodes, Trias,Quads=       316       558         0
AFLR4    : Nodes, Trias,Quads=       274       474         0

AFLR4    : Generate optimal mesh on surface definition 67
AFLR2    : Nodes, Trias,Quads=       315       556         0
AFLR4    : Nodes, Trias,Quads=       275       476         0

AFLR4    : Generate optimal mesh on surface definition 68
AFLR2    : Nodes, Trias,Quads=       224       362         0
AFLR4    : Nodes, Trias,Quads=       175       264         0

AFLR4    : Generate optimal mesh on surface definition 69
AFLR2    : Nodes, Trias,Quads=        22        29         0
AFLR4    : Nodes, Trias,Quads=        13        11         0

AFLR4    : Generate optimal mesh on surface definition 70
AFLR2    : Nodes, Trias,Quads=       147       205         0
AFLR4    : Nodes, Trias,Quads=        88        87         0

AFLR4    : Generate optimal mesh on surface definition 71
AFLR2    : Nodes, Trias,Quads=        25        32         0
AFLR4    : Nodes, Trias,Quads=        16        14         0

AFLR4    : Generate optimal mesh on surface definition 72
AFLR2    : Nodes, Trias,Quads=       234       380         0
AFLR4    : Nodes, Trias,Quads=       187       286         0

AFLR4    : Generate optimal mesh on surface definition 73
AFLR2    : Nodes, Trias,Quads=       122       191         0
AFLR4    : Nodes, Trias,Quads=       107       161         0

AFLR4    : Generate optimal mesh on surface definition 74
AFLR2    : Nodes, Trias,Quads=        19        24         0
AFLR4    : Nodes, Trias,Quads=        12        10         0

AFLR4    : Generate optimal mesh on surface definition 75
AFLR2    : Nodes, Trias,Quads=        78       103         0
AFLR4    : Nodes, Trias,Quads=        52        51         0

AFLR4    : Generate optimal mesh on surface definition 76
AFLR2    : Nodes, Trias,Quads=        18        22         0
AFLR4    : Nodes, Trias,Quads=        12        10         0

AFLR4    : Generate optimal mesh on surface definition 77
AFLR2    : Nodes, Trias,Quads=       126       198         0
AFLR4    : Nodes, Trias,Quads=       112       170         0

AFLR4    : Generate optimal mesh on surface definition 78
AFLR2    : Nodes, Trias,Quads=       116       183         0
AFLR4    : Nodes, Trias,Quads=       109       169         0

AFLR4    : Generate optimal mesh on surface definition 79
AFLR2    : Nodes, Trias,Quads=        22        28         0
AFLR4    : Nodes, Trias,Quads=        14        12         0

AFLR4    : Generate optimal mesh on surface definition 80
AFLR2    : Nodes, Trias,Quads=        68        90         0
AFLR4    : Nodes, Trias,Quads=        47        48         0

AFLR4    : Generate optimal mesh on surface definition 81
AFLR2    : Nodes, Trias,Quads=        19        24         0
AFLR4    : Nodes, Trias,Quads=        12        10         0

AFLR4    : Generate optimal mesh on surface definition 82
AFLR2    : Nodes, Trias,Quads=       118       187         0
AFLR4    : Nodes, Trias,Quads=       111       173         0

AFLR4    : Generate optimal mesh on surface definition 83
AFLR2    : Nodes, Trias,Quads=       117       185         0
AFLR4    : Nodes, Trias,Quads=       111       173         0

AFLR4    : Generate optimal mesh on surface definition 84
AFLR2    : Nodes, Trias,Quads=       115       181         0
AFLR4    : Nodes, Trias,Quads=       109       169         0

AFLR4    : Generate optimal mesh on surface definition 85
AFLR2    : Nodes, Trias,Quads=        19        24         0
AFLR4    : Nodes, Trias,Quads=        12        10         0

AFLR4    : Generate optimal mesh on surface definition 86
AFLR2    : Nodes, Trias,Quads=        68        90         0
AFLR4    : Nodes, Trias,Quads=        47        48         0

AFLR4    : Generate optimal mesh on surface definition 87
AFLR2    : Nodes, Trias,Quads=        22        28         0
AFLR4    : Nodes, Trias,Quads=        14        12         0

AFLR4    : Generate optimal mesh on surface definition 88
AFLR2    : Nodes, Trias,Quads=       125       196         0
AFLR4    : Nodes, Trias,Quads=       111       168         0

AFLR4    : Generate optimal mesh on surface definition 89
AFLR2    : Nodes, Trias,Quads=       122       191         0
AFLR4    : Nodes, Trias,Quads=       107       161         0

AFLR4    : Generate optimal mesh on surface definition 90
AFLR2    : Nodes, Trias,Quads=        18        22         0
AFLR4    : Nodes, Trias,Quads=        12        10         0

AFLR4    : Generate optimal mesh on surface definition 91
AFLR2    : Nodes, Trias,Quads=        78       103         0
AFLR4    : Nodes, Trias,Quads=        52        51         0

AFLR4    : Generate optimal mesh on surface definition 92
AFLR2    : Nodes, Trias,Quads=        19        24         0
AFLR4    : Nodes, Trias,Quads=        12        10         0

AFLR4    : Generate optimal mesh on surface definition 93
AFLR2    : Nodes, Trias,Quads=       233       378         0
AFLR4    : Nodes, Trias,Quads=       187       286         0

AFLR4    : Generate optimal mesh on surface definition 94
AFLR2    : Nodes, Trias,Quads=        25        32         0
AFLR4    : Nodes, Trias,Quads=        16        14         0

AFLR4    : Generate optimal mesh on surface definition 95
AFLR2    : Nodes, Trias,Quads=       148       207         0
AFLR4    : Nodes, Trias,Quads=        88        87         0

AFLR4    : Generate optimal mesh on surface definition 96
AFLR2    : Nodes, Trias,Quads=        22        29         0
AFLR4    : Nodes, Trias,Quads=        13        11         0

AFLR4    : Generate optimal mesh on surface definition 97
AFLR2    : Nodes, Trias,Quads=       229       372         0
AFLR4    : Nodes, Trias,Quads=       175       264         0

AFLR4    : Generate optimal mesh on surface definition 98
AFLR2    : Nodes, Trias,Quads=       236       401         0
AFLR4    : Nodes, Trias,Quads=       200       329         0

AFLR4    : Generate optimal mesh on surface definition 99
AFLR2    : Nodes, Trias,Quads=       243       414         0
AFLR4    : Nodes, Trias,Quads=       204       336         0

AFLR4    : Generate optimal mesh on surface definition 100
AFLR2    : Nodes, Trias,Quads=        31        40         0
AFLR4    : Nodes, Trias,Quads=        20        18         0

AFLR4    : Generate optimal mesh on surface definition 101
AFLR2    : Nodes, Trias,Quads=       108       149         0
AFLR4    : Nodes, Trias,Quads=        66        65         0

AFLR4    : Generate optimal mesh on surface definition 102
AFLR2    : Nodes, Trias,Quads=        31        40         0
AFLR4    : Nodes, Trias,Quads=        20        18         0

AFLR4    : Generate optimal mesh on surface definition 103
AFLR2    : Nodes, Trias,Quads=       241       410         0
AFLR4    : Nodes, Trias,Quads=       204       336         0

AFLR4    : Generate optimal mesh on surface definition 104
AFLR2    : Nodes, Trias,Quads=       238       405         0
AFLR4    : Nodes, Trias,Quads=       201       331         0

AFLR4    : Generate optimal mesh on surface definition 105
AFLR2    : Nodes, Trias,Quads=        31        40         0
AFLR4    : Nodes, Trias,Quads=        20        18         0

AFLR4    : Generate optimal mesh on surface definition 106
AFLR2    : Nodes, Trias,Quads=       108       149         0
AFLR4    : Nodes, Trias,Quads=        66        65         0

AFLR4    : Generate optimal mesh on surface definition 107
AFLR2    : Nodes, Trias,Quads=        31        40         0
AFLR4    : Nodes, Trias,Quads=        20        18         0

AFLR4    : Generate optimal mesh on surface definition 108
AFLR2    : Nodes, Trias,Quads=       241       412         0
AFLR4    : Nodes, Trias,Quads=       200       330         0

AFLR4    : Generate optimal mesh on surface definition 109
AFLR2    : Nodes, Trias,Quads=       243       416         0
AFLR4    : Nodes, Trias,Quads=       202       334         0

AFLR4    : Generate optimal mesh on surface definition 110
AFLR2    : Nodes, Trias,Quads=        31        40         0
AFLR4    : Nodes, Trias,Quads=        20        18         0

AFLR4    : Generate optimal mesh on surface definition 111
AFLR2    : Nodes, Trias,Quads=        97       128         0
AFLR4    : Nodes, Trias,Quads=        64        62         0

AFLR4    : Generate optimal mesh on surface definition 112
AFLR2    : Nodes, Trias,Quads=        31        40         0
AFLR4    : Nodes, Trias,Quads=        20        18         0

AFLR4    : Generate optimal mesh on surface definition 113
AFLR2    : Nodes, Trias,Quads=        12        14         0
AFLR4    : Nodes, Trias,Quads=         8         6         0

AFLR4    : Generate optimal mesh on surface definition 114
AFLR2    : Nodes, Trias,Quads=        12        14         0
AFLR4    : Nodes, Trias,Quads=         8         6         0

AFLR4    : Generate optimal mesh on surface definition 115
AFLR2    : Nodes, Trias,Quads=        12        14         0
AFLR4    : Nodes, Trias,Quads=         8         6         0

AFLR4    : Generate optimal mesh on surface definition 116
AFLR2    : Nodes, Trias,Quads=        12        14         0
AFLR4    : Nodes, Trias,Quads=         8         6         0

AFLR4    : Generate optimal mesh on surface definition 117
AFLR2    : Nodes, Trias,Quads=        12        14         0
AFLR4    : Nodes, Trias,Quads=         8         6         0

AFLR4    : Generate optimal mesh on surface definition 118
AFLR2    : Nodes, Trias,Quads=        12        14         0
AFLR4    : Nodes, Trias,Quads=         8         6         0

DGEOM    : Add surface definitions to composite definition 0
DGEOM    : Glue composite surface definition 0
DGEOM    : Nodes,Faces,BEdges=     17838     35640      6838

AFLR4    : Proximity BG Surface Grid Generation

AFLR4    : Nodes, Trias      =     19585     39134
AFLR4    : Nodes, Trias      =     20717     41398
AFLR4    : Nodes, Trias      =     21827     43618
AFLR4    : Nodes, Trias      =     22761     45486
AFLR4    : Nodes, Trias      =     23519     47002
AFLR4    : Nodes, Trias      =     23918     47800
AFLR4    : Nodes, Trias      =     24002     47968

AFLR4    : Surface Grid Generation

AFLR4    : Generate optimal mesh on surface definition 1
AFLR2    : Nodes, Trias,Quads=       799      1346         0
AFLR4    : Nodes, Trias,Quads=      1156      2060         0

AFLR4    : Generate optimal mesh on surface definition 2
AFLR2    : Nodes, Trias,Quads=       696      1157         0
AFLR4    : Nodes, Trias,Quads=       935      1635         0

AFLR4    : Generate optimal mesh on surface definition 3
AFLR2    : Nodes, Trias,Quads=       610      1103         0
AFLR4    : Nodes, Trias,Quads=       437       757         0

AFLR4    : Generate optimal mesh on surface definition 4
AFLR2    : Nodes, Trias,Quads=       366       622         0
AFLR4    : Nodes, Trias,Quads=       483       856         0

AFLR4    : Generate optimal mesh on surface definition 5
AFLR2    : Nodes, Trias,Quads=      2301      4380         0
AFLR4    : Nodes, Trias,Quads=      1586      2950         0

AFLR4    : Generate optimal mesh on surface definition 6
AFLR2    : Nodes, Trias,Quads=      2447      4630         0
AFLR4    : Nodes, Trias,Quads=      2254      4244         0

AFLR4    : Generate optimal mesh on surface definition 7
AFLR2    : Nodes, Trias,Quads=       364       618         0
AFLR4    : Nodes, Trias,Quads=       481       852         0

AFLR4    : Generate optimal mesh on surface definition 8
AFLR2    : Nodes, Trias,Quads=       605      1093         0
AFLR4    : Nodes, Trias,Quads=       430       743         0

AFLR4    : Generate optimal mesh on surface definition 9
AFLR2    : Nodes, Trias,Quads=      1819      3421         0
AFLR4    : Nodes, Trias,Quads=      1634      3051         0

AFLR4    : Generate optimal mesh on surface definition 10
AFLR2    : Nodes, Trias,Quads=      2023      3844         0
AFLR4    : Nodes, Trias,Quads=      1336      2470         0

AFLR4    : Generate optimal mesh on surface definition 11
AFLR2    : Nodes, Trias,Quads=        18        22         0
AFLR4    : Nodes, Trias,Quads=        14        14         0

AFLR4    : Generate optimal mesh on surface definition 12
AFLR2    : Nodes, Trias,Quads=      1422      2644         0
AFLR4    : Nodes, Trias,Quads=       870      1540         0

AFLR4    : Generate optimal mesh on surface definition 13
AFLR2    : Nodes, Trias,Quads=      1664      3096         0
AFLR4    : Nodes, Trias,Quads=      1398      2564         0

AFLR4    : Generate optimal mesh on surface definition 14
AFLR2    : Nodes, Trias,Quads=      1898      3542         0
AFLR4    : Nodes, Trias,Quads=      1705      3156         0

AFLR4    : Generate optimal mesh on surface definition 15
AFLR2    : Nodes, Trias,Quads=        21        26         0
AFLR4    : Nodes, Trias,Quads=        14        12         0

AFLR4    : Generate optimal mesh on surface definition 16
AFLR2    : Nodes, Trias,Quads=       238       386         0
AFLR4    : Nodes, Trias,Quads=       285       480         0

AFLR4    : Generate optimal mesh on surface definition 17
AFLR2    : Nodes, Trias,Quads=        21        27         0
AFLR4    : Nodes, Trias,Quads=        14        13         0

AFLR4    : Generate optimal mesh on surface definition 18
AFLR2    : Nodes, Trias,Quads=      2433      4570         0
AFLR4    : Nodes, Trias,Quads=      1882      3468         0

AFLR4    : Generate optimal mesh on surface definition 19
AFLR2    : Nodes, Trias,Quads=      2560      4813         0
AFLR4    : Nodes, Trias,Quads=      2080      3853         0

AFLR4    : Generate optimal mesh on surface definition 20
AFLR2    : Nodes, Trias,Quads=       539       977         0
AFLR4    : Nodes, Trias,Quads=       320       539         0

AFLR4    : Generate optimal mesh on surface definition 21
AFLR2    : Nodes, Trias,Quads=       463       833         0
AFLR4    : Nodes, Trias,Quads=       270       447         0

AFLR4    : Generate optimal mesh on surface definition 22
AFLR2    : Nodes, Trias,Quads=      1538      2877         0
AFLR4    : Nodes, Trias,Quads=       860      1521         0

AFLR4    : Generate optimal mesh on surface definition 23
AFLR2    : Nodes, Trias,Quads=      1881      3508         0
AFLR4    : Nodes, Trias,Quads=      1684      3114         0

AFLR4    : Generate optimal mesh on surface definition 24
AFLR2    : Nodes, Trias,Quads=      1853      3463         0
AFLR4    : Nodes, Trias,Quads=      1608      2973         0

AFLR4    : Generate optimal mesh on surface definition 25
AFLR2    : Nodes, Trias,Quads=      2397      4507         0
AFLR4    : Nodes, Trias,Quads=      1662      3037         0

AFLR4    : Generate optimal mesh on surface definition 26
AFLR2    : Nodes, Trias,Quads=        21        27         0
AFLR4    : Nodes, Trias,Quads=        14        13         0

AFLR4    : Generate optimal mesh on surface definition 27
AFLR2    : Nodes, Trias,Quads=        60        78         0
AFLR4    : Nodes, Trias,Quads=        41        40         0

AFLR4    : Generate optimal mesh on surface definition 28
AFLR2    : Nodes, Trias,Quads=        20        25         0
AFLR4    : Nodes, Trias,Quads=        13        11         0

AFLR4    : Generate optimal mesh on surface definition 29
AFLR2    : Nodes, Trias,Quads=       485       875         0
AFLR4    : Nodes, Trias,Quads=       288       481         0

AFLR4    : Generate optimal mesh on surface definition 30
AFLR2    : Nodes, Trias,Quads=       514       928         0
AFLR4    : Nodes, Trias,Quads=       306       512         0

AFLR4    : Generate optimal mesh on surface definition 31
AFLR2    : Nodes, Trias,Quads=      2168      4078         0
AFLR4    : Nodes, Trias,Quads=      1399      2540         0

AFLR4    : Generate optimal mesh on surface definition 32
AFLR2    : Nodes, Trias,Quads=      1770      3290         0
AFLR4    : Nodes, Trias,Quads=      1381      2512         0

AFLR4    : Generate optimal mesh on surface definition 33
AFLR2    : Nodes, Trias,Quads=       222       379         0
AFLR4    : Nodes, Trias,Quads=       332       599         0

AFLR4    : Generate optimal mesh on surface definition 34
AFLR2    : Nodes, Trias,Quads=       266       407         0
AFLR4    : Nodes, Trias,Quads=       330       535         0

AFLR4    : Generate optimal mesh on surface definition 35
AFLR2    : Nodes, Trias,Quads=        46        63         0
AFLR4    : Nodes, Trias,Quads=        31        33         0

AFLR4    : Generate optimal mesh on surface definition 36
AFLR2    : Nodes, Trias,Quads=        37        48         0
AFLR4    : Nodes, Trias,Quads=        24        22         0

AFLR4    : Generate optimal mesh on surface definition 37
AFLR2    : Nodes, Trias,Quads=        20        25         0
AFLR4    : Nodes, Trias,Quads=        14        13         0

AFLR4    : Generate optimal mesh on surface definition 38
AFLR2    : Nodes, Trias,Quads=        82       109         0
AFLR4    : Nodes, Trias,Quads=        65        75         0

AFLR4    : Generate optimal mesh on surface definition 39
AFLR2    : Nodes, Trias,Quads=        73       108         0
AFLR4    : Nodes, Trias,Quads=       113       188         0

AFLR4    : Generate optimal mesh on surface definition 40
AFLR2    : Nodes, Trias,Quads=        72       105         0
AFLR4    : Nodes, Trias,Quads=       112       185         0

AFLR4    : Generate optimal mesh on surface definition 41
AFLR2    : Nodes, Trias,Quads=       309       473         0
AFLR4    : Nodes, Trias,Quads=       356       567         0

AFLR4    : Generate optimal mesh on surface definition 42
AFLR2    : Nodes, Trias,Quads=        51        70         0
AFLR4    : Nodes, Trias,Quads=        47        62         0

AFLR4    : Generate optimal mesh on surface definition 43
AFLR2    : Nodes, Trias,Quads=        27        34         0
AFLR4    : Nodes, Trias,Quads=        18        16         0

AFLR4    : Generate optimal mesh on surface definition 44
AFLR2    : Nodes, Trias,Quads=      1065      2004         0
AFLR4    : Nodes, Trias,Quads=       926      1726         0

AFLR4    : Generate optimal mesh on surface definition 45
AFLR2    : Nodes, Trias,Quads=       965      1808         0
AFLR4    : Nodes, Trias,Quads=       885      1648         0

AFLR4    : Generate optimal mesh on surface definition 46
AFLR2    : Nodes, Trias,Quads=      1738      3231         0
AFLR4    : Nodes, Trias,Quads=      1352      2459         0

AFLR4    : Generate optimal mesh on surface definition 47
AFLR2    : Nodes, Trias,Quads=        37        48         0
AFLR4    : Nodes, Trias,Quads=        24        22         0

AFLR4    : Generate optimal mesh on surface definition 48
AFLR2    : Nodes, Trias,Quads=        46        63         0
AFLR4    : Nodes, Trias,Quads=        32        35         0

AFLR4    : Generate optimal mesh on surface definition 49
AFLR2    : Nodes, Trias,Quads=       374       609         0
AFLR4    : Nodes, Trias,Quads=       524       909         0

AFLR4    : Generate optimal mesh on surface definition 50
AFLR2    : Nodes, Trias,Quads=       187       313         0
AFLR4    : Nodes, Trias,Quads=       268       475         0

AFLR4    : Generate optimal mesh on surface definition 51
AFLR2    : Nodes, Trias,Quads=        26        32         0
AFLR4    : Nodes, Trias,Quads=        18        16         0

AFLR4    : Generate optimal mesh on surface definition 52
AFLR2    : Nodes, Trias,Quads=        23        29         0
AFLR4    : Nodes, Trias,Quads=        15        13         0

AFLR4    : Generate optimal mesh on surface definition 53
AFLR2    : Nodes, Trias,Quads=       145       204         0
AFLR4    : Nodes, Trias,Quads=        85        84         0

AFLR4    : Generate optimal mesh on surface definition 54
AFLR2    : Nodes, Trias,Quads=        35        45         0
AFLR4    : Nodes, Trias,Quads=        26        27         0

AFLR4    : Generate optimal mesh on surface definition 55
AFLR2    : Nodes, Trias,Quads=       101       154         0
AFLR4    : Nodes, Trias,Quads=       138       228         0

AFLR4    : Generate optimal mesh on surface definition 56
AFLR2    : Nodes, Trias,Quads=       125       175         0
AFLR4    : Nodes, Trias,Quads=       131       187         0

AFLR4    : Generate optimal mesh on surface definition 57
AFLR2    : Nodes, Trias,Quads=        20        25         0
AFLR4    : Nodes, Trias,Quads=        14        13         0

AFLR4    : Generate optimal mesh on surface definition 58
AFLR2    : Nodes, Trias,Quads=      1009      1895         0
AFLR4    : Nodes, Trias,Quads=       903      1683         0

AFLR4    : Generate optimal mesh on surface definition 59
AFLR2    : Nodes, Trias,Quads=      1035      1945         0
AFLR4    : Nodes, Trias,Quads=       919      1713         0

AFLR4    : Generate optimal mesh on surface definition 60
AFLR2    : Nodes, Trias,Quads=       232       398         0
AFLR4    : Nodes, Trias,Quads=       358       650         0

AFLR4    : Generate optimal mesh on surface definition 61
AFLR2    : Nodes, Trias,Quads=       347       567         0
AFLR4    : Nodes, Trias,Quads=       474       821         0

AFLR4    : Generate optimal mesh on surface definition 62
AFLR2    : Nodes, Trias,Quads=        44        60         0
AFLR4    : Nodes, Trias,Quads=        30        32         0

AFLR4    : Generate optimal mesh on surface definition 63
AFLR2    : Nodes, Trias,Quads=        48        64         0
AFLR4    : Nodes, Trias,Quads=        30        28         0

AFLR4    : Generate optimal mesh on surface definition 64
AFLR2    : Nodes, Trias,Quads=       314       553         0
AFLR4    : Nodes, Trias,Quads=       288       501         0

AFLR4    : Generate optimal mesh on surface definition 65
AFLR2    : Nodes, Trias,Quads=       316       557         0
AFLR4    : Nodes, Trias,Quads=       295       515         0

AFLR4    : Generate optimal mesh on surface definition 66
AFLR2    : Nodes, Trias,Quads=       315       555         0
AFLR4    : Nodes, Trias,Quads=       287       499         0

AFLR4    : Generate optimal mesh on surface definition 67
AFLR2    : Nodes, Trias,Quads=       316       557         0
AFLR4    : Nodes, Trias,Quads=       296       517         0

AFLR4    : Generate optimal mesh on surface definition 68
AFLR2    : Nodes, Trias,Quads=       237       385         0
AFLR4    : Nodes, Trias,Quads=       183       277         0

AFLR4    : Generate optimal mesh on surface definition 69
AFLR2    : Nodes, Trias,Quads=        22        29         0
AFLR4    : Nodes, Trias,Quads=        13        11         0

AFLR4    : Generate optimal mesh on surface definition 70
AFLR2    : Nodes, Trias,Quads=       152       215         0
AFLR4    : Nodes, Trias,Quads=        87        85         0

AFLR4    : Generate optimal mesh on surface definition 71
AFLR2    : Nodes, Trias,Quads=        25        32         0
AFLR4    : Nodes, Trias,Quads=        16        14         0

AFLR4    : Generate optimal mesh on surface definition 72
AFLR2    : Nodes, Trias,Quads=       252       413         0
AFLR4    : Nodes, Trias,Quads=       197       303         0

AFLR4    : Generate optimal mesh on surface definition 73
AFLR2    : Nodes, Trias,Quads=       728      1314         0
AFLR4    : Nodes, Trias,Quads=       730      1318         0

AFLR4    : Generate optimal mesh on surface definition 74
AFLR2    : Nodes, Trias,Quads=       112       179         0
AFLR4    : Nodes, Trias,Quads=       109       173         0

AFLR4    : Generate optimal mesh on surface definition 75
AFLR2    : Nodes, Trias,Quads=       678      1184         0
AFLR4    : Nodes, Trias,Quads=       654      1136         0

AFLR4    : Generate optimal mesh on surface definition 76
AFLR2    : Nodes, Trias,Quads=       380       680         0
AFLR4    : Nodes, Trias,Quads=       374       668         0

AFLR4    : Generate optimal mesh on surface definition 77
AFLR2    : Nodes, Trias,Quads=       722      1303         0
AFLR4    : Nodes, Trias,Quads=       733      1325         0

AFLR4    : Generate optimal mesh on surface definition 78
AFLR2    : Nodes, Trias,Quads=       259       441         0
AFLR4    : Nodes, Trias,Quads=       274       471         0

AFLR4    : Generate optimal mesh on surface definition 79
AFLR2    : Nodes, Trias,Quads=        25        32         0
AFLR4    : Nodes, Trias,Quads=        17        16         0

AFLR4    : Generate optimal mesh on surface definition 80
AFLR2    : Nodes, Trias,Quads=       175       268         0
AFLR4    : Nodes, Trias,Quads=       152       222         0

AFLR4    : Generate optimal mesh on surface definition 81
AFLR2    : Nodes, Trias,Quads=        90       140         0
AFLR4    : Nodes, Trias,Quads=        85       130         0

AFLR4    : Generate optimal mesh on surface definition 82
AFLR2    : Nodes, Trias,Quads=       264       451         0
AFLR4    : Nodes, Trias,Quads=       273       469         0

AFLR4    : Generate optimal mesh on surface definition 83
AFLR2    : Nodes, Trias,Quads=       557       997         0
AFLR4    : Nodes, Trias,Quads=       599      1081         0

AFLR4    : Generate optimal mesh on surface definition 84
AFLR2    : Nodes, Trias,Quads=       498       880         0
AFLR4    : Nodes, Trias,Quads=       589      1062         0

AFLR4    : Generate optimal mesh on surface definition 85
AFLR2    : Nodes, Trias,Quads=        89       138         0
AFLR4    : Nodes, Trias,Quads=        85       130         0

AFLR4    : Generate optimal mesh on surface definition 86
AFLR2    : Nodes, Trias,Quads=       508       870         0
AFLR4    : Nodes, Trias,Quads=       467       788         0

AFLR4    : Generate optimal mesh on surface definition 87
AFLR2    : Nodes, Trias,Quads=       104       163         0
AFLR4    : Nodes, Trias,Quads=        94       143         0

AFLR4    : Generate optimal mesh on surface definition 88
AFLR2    : Nodes, Trias,Quads=       716      1291         0
AFLR4    : Nodes, Trias,Quads=       728      1315         0

AFLR4    : Generate optimal mesh on surface definition 89
AFLR2    : Nodes, Trias,Quads=       742      1342         0
AFLR4    : Nodes, Trias,Quads=       735      1328         0

AFLR4    : Generate optimal mesh on surface definition 90
AFLR2    : Nodes, Trias,Quads=       377       674         0
AFLR4    : Nodes, Trias,Quads=       374       668         0

AFLR4    : Generate optimal mesh on surface definition 91
AFLR2    : Nodes, Trias,Quads=       679      1186         0
AFLR4    : Nodes, Trias,Quads=       654      1136         0

AFLR4    : Generate optimal mesh on surface definition 92
AFLR2    : Nodes, Trias,Quads=       114       183         0
AFLR4    : Nodes, Trias,Quads=       109       173         0

AFLR4    : Generate optimal mesh on surface definition 93
AFLR2    : Nodes, Trias,Quads=       804      1439         0
AFLR4    : Nodes, Trias,Quads=       683      1197         0

AFLR4    : Generate optimal mesh on surface definition 94
AFLR2    : Nodes, Trias,Quads=        68        98         0
AFLR4    : Nodes, Trias,Quads=        59        80         0

AFLR4    : Generate optimal mesh on surface definition 95
AFLR2    : Nodes, Trias,Quads=       689      1178         0
AFLR4    : Nodes, Trias,Quads=       600      1000         0

AFLR4    : Generate optimal mesh on surface definition 96
AFLR2    : Nodes, Trias,Quads=       348       619         0
AFLR4    : Nodes, Trias,Quads=       343       609         0

AFLR4    : Generate optimal mesh on surface definition 97
AFLR2    : Nodes, Trias,Quads=       736      1300         0
AFLR4    : Nodes, Trias,Quads=       694      1216         0

AFLR4    : Generate optimal mesh on surface definition 98
AFLR2    : Nodes, Trias,Quads=      1092      2013         0
AFLR4    : Nodes, Trias,Quads=       863      1555         0

AFLR4    : Generate optimal mesh on surface definition 99
AFLR2    : Nodes, Trias,Quads=       997      1831         0
AFLR4    : Nodes, Trias,Quads=       824      1485         0

AFLR4    : Generate optimal mesh on surface definition 100
AFLR2    : Nodes, Trias,Quads=       617      1124         0
AFLR4    : Nodes, Trias,Quads=       634      1158         0

AFLR4    : Generate optimal mesh on surface definition 101
AFLR2    : Nodes, Trias,Quads=       773      1355         0
AFLR4    : Nodes, Trias,Quads=       701      1211         0

AFLR4    : Generate optimal mesh on surface definition 102
AFLR2    : Nodes, Trias,Quads=        80       117         0
AFLR4    : Nodes, Trias,Quads=        69        95         0

AFLR4    : Generate optimal mesh on surface definition 103
AFLR2    : Nodes, Trias,Quads=       908      1659         0
AFLR4    : Nodes, Trias,Quads=       765      1373         0

AFLR4    : Generate optimal mesh on surface definition 104
AFLR2    : Nodes, Trias,Quads=      1055      1943         0
AFLR4    : Nodes, Trias,Quads=       827      1487         0

AFLR4    : Generate optimal mesh on surface definition 105
AFLR2    : Nodes, Trias,Quads=        80       117         0
AFLR4    : Nodes, Trias,Quads=        69        95         0

AFLR4    : Generate optimal mesh on surface definition 106
AFLR2    : Nodes, Trias,Quads=       670      1159         0
AFLR4    : Nodes, Trias,Quads=       578       975         0

AFLR4    : Generate optimal mesh on surface definition 107
AFLR2    : Nodes, Trias,Quads=       616      1122         0
AFLR4    : Nodes, Trias,Quads=       632      1154         0

AFLR4    : Generate optimal mesh on surface definition 108
AFLR2    : Nodes, Trias,Quads=      1009      1861         0
AFLR4    : Nodes, Trias,Quads=       712      1267         0

AFLR4    : Generate optimal mesh on surface definition 109
AFLR2    : Nodes, Trias,Quads=      1012      1867         0
AFLR4    : Nodes, Trias,Quads=       709      1261         0

AFLR4    : Generate optimal mesh on surface definition 110
AFLR2    : Nodes, Trias,Quads=        51        69         0
AFLR4    : Nodes, Trias,Quads=        41        49         0

AFLR4    : Generate optimal mesh on surface definition 111
AFLR2    : Nodes, Trias,Quads=       734      1294         0
AFLR4    : Nodes, Trias,Quads=       744      1314         0

AFLR4    : Generate optimal mesh on surface definition 112
AFLR2    : Nodes, Trias,Quads=       565      1023         0
AFLR4    : Nodes, Trias,Quads=       596      1085         0

AFLR4    : Generate optimal mesh on surface definition 113
AFLR2    : Nodes, Trias,Quads=        12        14         0
AFLR4    : Nodes, Trias,Quads=         8         6         0

AFLR4    : Generate optimal mesh on surface definition 114
AFLR2    : Nodes, Trias,Quads=        12        14         0
AFLR4    : Nodes, Trias,Quads=         8         6         0

AFLR4    : Generate optimal mesh on surface definition 115
AFLR2    : Nodes, Trias,Quads=        12        14         0
AFLR4    : Nodes, Trias,Quads=         8         6         0

AFLR4    : Generate optimal mesh on surface definition 116
AFLR2    : Nodes, Trias,Quads=        12        14         0
AFLR4    : Nodes, Trias,Quads=         8         6         0

AFLR4    : Generate optimal mesh on surface definition 117
AFLR2    : Nodes, Trias,Quads=        12        14         0
AFLR4    : Nodes, Trias,Quads=         8         6         0

AFLR4    : Generate optimal mesh on surface definition 118
AFLR2    : Nodes, Trias,Quads=        12        14         0
AFLR4    : Nodes, Trias,Quads=         8         6         0

DGEOM    : Add surface definitions to composite definition 0
DGEOM    : Glue composite surface definition 0
DGEOM    : Nodes,Faces,BEdges=     51867    103698     12318

OVERALL  : CPU Time          =     3.233   seconds
Body 1 (of 11)
Number of nodes    = 34775
Number of elements = 69554
Number of triangle elements      = 69554
Number of quadrilateral elements = 0
Body 2 (of 11)
Number of nodes    = 347
Number of elements = 690
Number of triangle elements      = 690
Number of quadrilateral elements = 0
Body 3 (of 11)
Number of nodes    = 2312
Number of elements = 4620
Number of triangle elements      = 4620
Number of quadrilateral elements = 0
Body 4 (of 11)
Number of nodes    = 656
Number of elements = 1308
Number of triangle elements      = 1308
Number of quadrilateral elements = 0
Body 5 (of 11)
Number of nodes    = 1604
Number of elements = 3204
Number of triangle elements      = 3204
Number of quadrilateral elements = 0
Body 6 (of 11)
Number of nodes    = 2312
Number of elements = 4620
Number of triangle elements      = 4620
Number of quadrilateral elements = 0
Body 7 (of 11)
Number of nodes    = 2053
Number of elements = 4102
Number of triangle elements      = 4102
Number of quadrilateral elements = 0
Body 8 (of 11)
Number of nodes    = 2754
Number of elements = 5504
Number of triangle elements      = 5504
Number of quadrilateral elements = 0
Body 9 (of 11)
Number of nodes    = 2544
Number of elements = 5084
Number of triangle elements      = 5084
Number of quadrilateral elements = 0
Body 10 (of 11)
Number of nodes    = 2490
Number of elements = 4976
Number of triangle elements      = 4976
Number of quadrilateral elements = 0
Body 11 (of 11)
Number of nodes    = 20
Number of elements = 36
Number of triangle elements      = 36
Number of quadrilateral elements = 0
----------------------------
Total number of nodes    = 51867
Total number of elements = 103698
Total number of triangle elements      = 103698
Total number of quadrilateral elements = 0

Writing vtk file ....

Writing vtk surface file ....

capsGroups found:
  1: Fuselage
  2: Wing
  3: Htail
  4: Pylon
  5: Vtail
  6: Nacelle
  7: Control
  8: Farfield
Finished writing vtk file

Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 9
	Name = Fuselage, index = 1
	Name = riteWing, index = 2
	Name = leftWing, index = 3
	Name = Htail, index = 4
	Name = Pylon, index = 5
	Name = Vtail, index = 6
	Name = Nacelle, index = 7
	Name = Control, index = 8
	Name = Farfield, index = 9
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 8
	Name = Fuselage, index = 1
	Name = Wing, index = 2
	Name = Htail, index = 3
	Name = Pylon, index = 4
	Name = Vtail, index = 5
	Name = Nacelle, index = 6
	Name = Control, index = 7
	Name = Farfield, index = 8

Getting mesh sizing parameters
	Mesh sizing name - Control
	Mesh sizing name - Fuselage
	Mesh sizing name - Htail
	Mesh sizing name - Nacelle
	Mesh sizing name - Pylon
	Mesh sizing name - Vtail
	Mesh sizing name - leftWing
	Mesh sizing name - riteWing
	Done getting mesh sizing parameters
Getting volume mesh
 
UG PARAM : SETTING INPUT PARAMETERS FROM ARGUMENT VECTOR
 
UG PARAM : mbl                         = 1         
UG PARAM : nbl                         = 5         
UG PARAM : mblelc                      = 2         
UG PARAM : mrecm                       = 3         
UG PARAM : mrecqm                      = 3         
UG PARAM : mbl                         = 1         
UG PARAM : mrecm                       = 3         
UG PARAM : mrecqm                      = 3         
UG PARAM : mblelc                      = 1         
UG PARAM : BC_IDs                  [ 0]= 1         
UG PARAM : BC_IDs                  [ 1]= 2         
UG PARAM : BC_IDs                  [ 2]= 3         
UG PARAM : BC_IDs                  [ 3]= 4         
UG PARAM : BC_IDs                  [ 4]= 5         
UG PARAM : BC_IDs                  [ 5]= 6         
UG PARAM : BC_IDs                  [ 6]= 7         
UG PARAM : BC_IDs                  [ 7]= 8         
UG PARAM : BC_IDs                  [ 8]= 9         
UG PARAM : BC_IDs                  [ 9]= 10        
UG PARAM : BC_IDs                  [10]= 11        
UG PARAM : BC_IDs                  [11]= 12        
UG PARAM : BC_IDs                  [12]= 13        
UG PARAM : BC_IDs                  [13]= 14        
UG PARAM : BC_IDs                  [14]= 15        
UG PARAM : BC_IDs                  [15]= 16        
UG PARAM : BC_IDs                  [16]= 17        
UG PARAM : BC_IDs                  [17]= 18        
UG PARAM : BC_IDs                  [18]= 19        
UG PARAM : BC_IDs                  [19]= 20        
UG PARAM : BC_IDs                  [20]= 21        
UG PARAM : BC_IDs                  [21]= 22        
UG PARAM : BC_IDs                  [22]= 23        
UG PARAM : BC_IDs                  [23]= 24        
UG PARAM : BC_IDs                  [24]= 25        
UG PARAM : BC_IDs                  [25]= 26        
UG PARAM : BC_IDs                  [26]= 27        
UG PARAM : BC_IDs                  [27]= 28        
UG PARAM : BC_IDs                  [28]= 29        
UG PARAM : BC_IDs                  [29]= 30        
UG PARAM : BC_IDs                  [30]= 31        
UG PARAM : BC_IDs                  [31]= 32        
UG PARAM : BC_IDs                  [32]= 33        
UG PARAM : BC_IDs                  [33]= 34        
UG PARAM : BC_IDs                  [34]= 35        
UG PARAM : BC_IDs                  [35]= 36        
UG PARAM : BC_IDs                  [36]= 37        
UG PARAM : BC_IDs                  [37]= 38        
UG PARAM : BC_IDs                  [38]= 39        
UG PARAM : BC_IDs                  [39]= 40        
UG PARAM : BC_IDs                  [40]= 41        
UG PARAM : BC_IDs                  [41]= 42        
UG PARAM : BC_IDs                  [42]= 43        
UG PARAM : BC_IDs                  [43]= 44        
UG PARAM : BC_IDs                  [44]= 45        
UG PARAM : BC_IDs                  [45]= 46        
UG PARAM : BC_IDs                  [46]= 47        
UG PARAM : BC_IDs                  [47]= 48        
UG PARAM : BC_IDs                  [48]= 49        
UG PARAM : BC_IDs                  [49]= 50        
UG PARAM : BC_IDs                  [50]= 51        
UG PARAM : BC_IDs                  [51]= 52        
UG PARAM : BC_IDs                  [52]= 53        
UG PARAM : BC_IDs                  [53]= 54        
UG PARAM : BC_IDs                  [54]= 55        
UG PARAM : BC_IDs                  [55]= 56        
UG PARAM : BC_IDs                  [56]= 57        
UG PARAM : BC_IDs                  [57]= 58        
UG PARAM : BC_IDs                  [58]= 59        
UG PARAM : BC_IDs                  [59]= 60        
UG PARAM : BC_IDs                  [60]= 61        
UG PARAM : BC_IDs                  [61]= 62        
UG PARAM : BC_IDs                  [62]= 63        
UG PARAM : BC_IDs                  [63]= 64        
UG PARAM : BC_IDs                  [64]= 65        
UG PARAM : BC_IDs                  [65]= 66        
UG PARAM : BC_IDs                  [66]= 67        
UG PARAM : BC_IDs                  [67]= 68        
UG PARAM : BC_IDs                  [68]= 69        
UG PARAM : BC_IDs                  [69]= 70        
UG PARAM : BC_IDs                  [70]= 71        
UG PARAM : BC_IDs                  [71]= 72        
UG PARAM : BC_IDs                  [72]= 73        
UG PARAM : BC_IDs                  [73]= 74        
UG PARAM : BC_IDs                  [74]= 75        
UG PARAM : BC_IDs                  [75]= 76        
UG PARAM : BC_IDs                  [76]= 77        
UG PARAM : BC_IDs                  [77]= 78        
UG PARAM : BC_IDs                  [78]= 79        
UG PARAM : BC_IDs                  [79]= 80        
UG PARAM : BC_IDs                  [80]= 81        
UG PARAM : BC_IDs                  [81]= 82        
UG PARAM : BC_IDs                  [82]= 83        
UG PARAM : BC_IDs                  [83]= 84        
UG PARAM : BC_IDs                  [84]= 85        
UG PARAM : BC_IDs                  [85]= 86        
UG PARAM : BC_IDs                  [86]= 87        
UG PARAM : BC_IDs                  [87]= 88        
UG PARAM : BC_IDs                  [88]= 89        
UG PARAM : BC_IDs                  [89]= 90        
UG PARAM : BC_IDs                  [90]= 91        
UG PARAM : BC_IDs                  [91]= 92        
UG PARAM : BC_IDs                  [92]= 93        
UG PARAM : BC_IDs                  [93]= 94        
UG PARAM : BC_IDs                  [94]= 95        
UG PARAM : BC_IDs                  [95]= 96        
UG PARAM : BC_IDs                  [96]= 97        
UG PARAM : BC_IDs                  [97]= 98        
UG PARAM : BC_IDs                  [98]= 99        
UG PARAM : BC_IDs                  [99]= 100       
UG PARAM : BC_IDs                  [117]= 118       
UG PARAM : BL_DS                   [ 0]= 0.434102  
UG PARAM : BL_DS                   [ 1]= 0.434102  
UG PARAM : BL_DS                   [ 2]= 0.434102  
UG PARAM : BL_DS                   [ 3]= 0.434102  
UG PARAM : BL_DS                   [ 4]= 0.434102  
UG PARAM : BL_DS                   [ 5]= 0.434102  
UG PARAM : BL_DS                   [ 6]= 0.434102  
UG PARAM : BL_DS                   [ 7]= 0.434102  
UG PARAM : BL_DS                   [ 8]= 0.434102  
UG PARAM : BL_DS                   [ 9]= 0.434102  
UG PARAM : BL_DS                   [10]= 0.434102  
UG PARAM : BL_DS                   [11]= 0.434102  
UG PARAM : BL_DS                   [12]= 0.434102  
UG PARAM : BL_DS                   [13]= 0.434102  
UG PARAM : BL_DS                   [14]= 0.434102  
UG PARAM : BL_DS                   [15]= 0.434102  
UG PARAM : BL_DS                   [16]= 0.434102  
UG PARAM : BL_DS                   [17]= 0.434102  
UG PARAM : BL_DS                   [18]= 0.434102  
UG PARAM : BL_DS                   [19]= 0.434102  
UG PARAM : BL_DS                   [20]= 0.434102  
UG PARAM : BL_DS                   [21]= 0.434102  
UG PARAM : BL_DS                   [22]= 0.434102  
UG PARAM : BL_DS                   [23]= 0.434102  
UG PARAM : BL_DS                   [24]= 0.434102  
UG PARAM : BL_DS                   [25]= 0.434102  
UG PARAM : BL_DS                   [26]= 0.434102  
UG PARAM : BL_DS                   [27]= 0.434102  
UG PARAM : BL_DS                   [28]= 0.434102  
UG PARAM : BL_DS                   [29]= 0.434102  
UG PARAM : BL_DS                   [30]= 0.434102  
UG PARAM : BL_DS                   [31]= 0.434102  
UG PARAM : BL_DS                   [32]= 0.434102  
UG PARAM : BL_DS                   [33]= 0.434102  
UG PARAM : BL_DS                   [34]= 0.434102  
UG PARAM : BL_DS                   [35]= 0.434102  
UG PARAM : BL_DS                   [36]= 0.434102  
UG PARAM : BL_DS                   [37]= 0.434102  
UG PARAM : BL_DS                   [38]= 0.434102  
UG PARAM : BL_DS                   [39]= 0.434102  
UG PARAM : BL_DS                   [40]= 0.434102  
UG PARAM : BL_DS                   [41]= 0.434102  
UG PARAM : BL_DS                   [42]= 0.434102  
UG PARAM : BL_DS                   [43]= 0.434102  
UG PARAM : BL_DS                   [44]= 0.434102  
UG PARAM : BL_DS                   [45]= 0.434102  
UG PARAM : BL_DS                   [46]= 0.434102  
UG PARAM : BL_DS                   [47]= 0.434102  
UG PARAM : BL_DS                   [48]= 0.434102  
UG PARAM : BL_DS                   [49]= 0.434102  
UG PARAM : BL_DS                   [50]= 0.434102  
UG PARAM : BL_DS                   [51]= 0.434102  
UG PARAM : BL_DS                   [52]= 0.434102  
UG PARAM : BL_DS                   [53]= 0.434102  
UG PARAM : BL_DS                   [54]= 0.434102  
UG PARAM : BL_DS                   [55]= 0.434102  
UG PARAM : BL_DS                   [56]= 0.434102  
UG PARAM : BL_DS                   [57]= 0.434102  
UG PARAM : BL_DS                   [58]= 0.434102  
UG PARAM : BL_DS                   [59]= 0.434102  
UG PARAM : BL_DS                   [60]= 0.434102  
UG PARAM : BL_DS                   [61]= 0.434102  
UG PARAM : BL_DS                   [62]= 0.434102  
UG PARAM : BL_DS                   [63]= 0.434102  
UG PARAM : BL_DS                   [64]= 0.434102  
UG PARAM : BL_DS                   [65]= 0.434102  
UG PARAM : BL_DS                   [66]= 0.434102  
UG PARAM : BL_DS                   [67]= 0.434102  
UG PARAM : BL_DS                   [68]= 0.217051  
UG PARAM : BL_DS                   [69]= 0.217051  
UG PARAM : BL_DS                   [70]= 0.217051  
UG PARAM : BL_DS                   [71]= 0.434102  
UG PARAM : BL_DS                   [72]= 0.434102  
UG PARAM : BL_DS                   [73]= 0.217051  
UG PARAM : BL_DS                   [74]= 0.217051  
UG PARAM : BL_DS                   [75]= 0.217051  
UG PARAM : BL_DS                   [76]= 0.434102  
UG PARAM : BL_DS                   [77]= 0.434102  
UG PARAM : BL_DS                   [78]= 0.217051  
UG PARAM : BL_DS                   [79]= 0.217051  
UG PARAM : BL_DS                   [80]= 0.217051  
UG PARAM : BL_DS                   [81]= 0.434102  
UG PARAM : BL_DS                   [82]= 0.434102  
UG PARAM : BL_DS                   [83]= 0.434102  
UG PARAM : BL_DS                   [84]= 0.217051  
UG PARAM : BL_DS                   [85]= 0.217051  
UG PARAM : BL_DS                   [86]= 0.217051  
UG PARAM : BL_DS                   [87]= 0.434102  
UG PARAM : BL_DS                   [88]= 0.434102  
UG PARAM : BL_DS                   [89]= 0.217051  
UG PARAM : BL_DS                   [90]= 0.217051  
UG PARAM : BL_DS                   [91]= 0.217051  
UG PARAM : BL_DS                   [92]= 0.434102  
UG PARAM : BL_DS                   [93]= 0.217051  
UG PARAM : BL_DS                   [94]= 0.217051  
UG PARAM : BL_DS                   [95]= 0.217051  
UG PARAM : BL_DS                   [96]= 0.434102  
UG PARAM : BL_DS                   [97]= 0.434102  
UG PARAM : BL_DS                   [98]= 0.434102  
UG PARAM : BL_DS                   [99]= 0.217051  
UG PARAM : BL_DS                   [117]= 0         
UG PARAM : BL_DEL                  [ 0]= 2.17051   
UG PARAM : BL_DEL                  [ 1]= 2.17051   
UG PARAM : BL_DEL                  [ 2]= 2.17051   
UG PARAM : BL_DEL                  [ 3]= 2.17051   
UG PARAM : BL_DEL                  [ 4]= 2.17051   
UG PARAM : BL_DEL                  [ 5]= 2.17051   
UG PARAM : BL_DEL                  [ 6]= 2.17051   
UG PARAM : BL_DEL                  [ 7]= 2.17051   
UG PARAM : BL_DEL                  [ 8]= 2.17051   
UG PARAM : BL_DEL                  [ 9]= 2.17051   
UG PARAM : BL_DEL                  [10]= 2.17051   
UG PARAM : BL_DEL                  [11]= 2.17051   
UG PARAM : BL_DEL                  [12]= 2.17051   
UG PARAM : BL_DEL                  [13]= 2.17051   
UG PARAM : BL_DEL                  [14]= 2.17051   
UG PARAM : BL_DEL                  [15]= 2.17051   
UG PARAM : BL_DEL                  [16]= 2.17051   
UG PARAM : BL_DEL                  [17]= 2.17051   
UG PARAM : BL_DEL                  [18]= 2.17051   
UG PARAM : BL_DEL                  [19]= 2.17051   
UG PARAM : BL_DEL                  [20]= 2.17051   
UG PARAM : BL_DEL                  [21]= 2.17051   
UG PARAM : BL_DEL                  [22]= 2.17051   
UG PARAM : BL_DEL                  [23]= 2.17051   
UG PARAM : BL_DEL                  [24]= 2.17051   
UG PARAM : BL_DEL                  [25]= 2.17051   
UG PARAM : BL_DEL                  [26]= 2.17051   
UG PARAM : BL_DEL                  [27]= 2.17051   
UG PARAM : BL_DEL                  [28]= 2.17051   
UG PARAM : BL_DEL                  [29]= 2.17051   
UG PARAM : BL_DEL                  [30]= 2.17051   
UG PARAM : BL_DEL                  [31]= 2.17051   
UG PARAM : BL_DEL                  [32]= 2.17051   
UG PARAM : BL_DEL                  [33]= 2.17051   
UG PARAM : BL_DEL                  [34]= 2.17051   
UG PARAM : BL_DEL                  [35]= 2.17051   
UG PARAM : BL_DEL                  [36]= 2.17051   
UG PARAM : BL_DEL                  [37]= 2.17051   
UG PARAM : BL_DEL                  [38]= 2.17051   
UG PARAM : BL_DEL                  [39]= 2.17051   
UG PARAM : BL_DEL                  [40]= 2.17051   
UG PARAM : BL_DEL                  [41]= 2.17051   
UG PARAM : BL_DEL                  [42]= 2.17051   
UG PARAM : BL_DEL                  [43]= 2.17051   
UG PARAM : BL_DEL                  [44]= 2.17051   
UG PARAM : BL_DEL                  [45]= 2.17051   
UG PARAM : BL_DEL                  [46]= 2.17051   
UG PARAM : BL_DEL                  [47]= 2.17051   
UG PARAM : BL_DEL                  [48]= 2.17051   
UG PARAM : BL_DEL                  [49]= 2.17051   
UG PARAM : BL_DEL                  [50]= 2.17051   
UG PARAM : BL_DEL                  [51]= 2.17051   
UG PARAM : BL_DEL                  [52]= 2.17051   
UG PARAM : BL_DEL                  [53]= 2.17051   
UG PARAM : BL_DEL                  [54]= 2.17051   
UG PARAM : BL_DEL                  [55]= 2.17051   
UG PARAM : BL_DEL                  [56]= 2.17051   
UG PARAM : BL_DEL                  [57]= 2.17051   
UG PARAM : BL_DEL                  [58]= 2.17051   
UG PARAM : BL_DEL                  [59]= 2.17051   
UG PARAM : BL_DEL                  [60]= 2.17051   
UG PARAM : BL_DEL                  [61]= 2.17051   
UG PARAM : BL_DEL                  [62]= 2.17051   
UG PARAM : BL_DEL                  [63]= 2.17051   
UG PARAM : BL_DEL                  [64]= 2.17051   
UG PARAM : BL_DEL                  [65]= 2.17051   
UG PARAM : BL_DEL                  [66]= 2.17051   
UG PARAM : BL_DEL                  [67]= 2.17051   
UG PARAM : BL_DEL                  [68]= 2.17051   
UG PARAM : BL_DEL                  [69]= 2.17051   
UG PARAM : BL_DEL                  [70]= 2.17051   
UG PARAM : BL_DEL                  [71]= 2.17051   
UG PARAM : BL_DEL                  [72]= 2.17051   
UG PARAM : BL_DEL                  [73]= 2.17051   
UG PARAM : BL_DEL                  [74]= 2.17051   
UG PARAM : BL_DEL                  [75]= 2.17051   
UG PARAM : BL_DEL                  [76]= 2.17051   
UG PARAM : BL_DEL                  [77]= 2.17051   
UG PARAM : BL_DEL                  [78]= 2.17051   
UG PARAM : BL_DEL                  [79]= 2.17051   
UG PARAM : BL_DEL                  [80]= 2.17051   
UG PARAM : BL_DEL                  [81]= 2.17051   
UG PARAM : BL_DEL                  [82]= 2.17051   
UG PARAM : BL_DEL                  [83]= 2.17051   
UG PARAM : BL_DEL                  [84]= 2.17051   
UG PARAM : BL_DEL                  [85]= 2.17051   
UG PARAM : BL_DEL                  [86]= 2.17051   
UG PARAM : BL_DEL                  [87]= 2.17051   
UG PARAM : BL_DEL                  [88]= 2.17051   
UG PARAM : BL_DEL                  [89]= 2.17051   
UG PARAM : BL_DEL                  [90]= 2.17051   
UG PARAM : BL_DEL                  [91]= 2.17051   
UG PARAM : BL_DEL                  [92]= 2.17051   
UG PARAM : BL_DEL                  [93]= 2.17051   
UG PARAM : BL_DEL                  [94]= 2.17051   
UG PARAM : BL_DEL                  [95]= 2.17051   
UG PARAM : BL_DEL                  [96]= 2.17051   
UG PARAM : BL_DEL                  [97]= 2.17051   
UG PARAM : BL_DEL                  [98]= 2.17051   
UG PARAM : BL_DEL                  [99]= 2.17051   
UG PARAM : BL_DEL                  [117]= 0         
UG PARAM : mpfrmt                      = 0         
 
AFLR2    : ---------------------------------------
AFLR2    : AFLR2 LIBRARY
AFLR2    : ADVANCING-FRONT/LOCAL-RECONNECTION
AFLR2    : TRIA/QUAD GRID GENERATOR
AFLR2    : Version Number 9.18.1
AFLR2    : Version Date   06/11/24 @ 05:52PM
AFLR2    : Compile OS     Darwin 23.5.0 arm64
AFLR2    : Compile Date   06/11/24 @ 05:52PM
AFLR2    : Copyright 1994-2021, D.L. Marcum
AFLR2    : ---------------------------------------
 
AFLR4    : ---------------------------------------
AFLR4    : AFLR4 LIBRARY
AFLR4    : ADVANCING-FRONT/LOCAL-RECONNECTION
AFLR4    : TRIA/QUAD SURFACE GRID GENERATOR
AFLR4    : Version Number 11.5.15
AFLR4    : Version Date   07/19/24 @ 07:04PM
AFLR4    : Compile OS     Darwin 23.5.0 arm64
AFLR4    : Compile Date   07/19/24 @ 07:06PM
AFLR4    : Copyright 1994-2021, D.L. Marcum
AFLR4    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.8.1
EGADS    : ---------------------------------------

EGADS    : EGADS CAD Geometry Setup

EGADS    : Model has 11 Active Bodies

EGADS    : Body 0 is a SolidBody
EGADS    : Body 0 has 1 Shells
EGADS    : Body 0 has 67 Faces
EGADS    : Body 0 has 176 Edges
EGADS    : Body 0 has 71 Loops
EGADS    : Body 0 has 107 Nodes
EGADS    : Body 1 is a SolidBody
EGADS    : Body 1 has 1 Shells
EGADS    : Body 1 has 5 Faces
EGADS    : Body 1 has 9 Edges
EGADS    : Body 1 has 5 Loops
EGADS    : Body 1 has 6 Nodes
EGADS    : Body 2 is a SolidBody
EGADS    : Body 2 has 1 Shells
EGADS    : Body 2 has 5 Faces
EGADS    : Body 2 has 9 Edges
EGADS    : Body 2 has 5 Loops
EGADS    : Body 2 has 6 Nodes
EGADS    : Body 3 is a SolidBody
EGADS    : Body 3 has 1 Shells
EGADS    : Body 3 has 5 Faces
EGADS    : Body 3 has 9 Edges
EGADS    : Body 3 has 5 Loops
EGADS    : Body 3 has 6 Nodes
EGADS    : Body 4 is a SolidBody
EGADS    : Body 4 has 1 Shells
EGADS    : Body 4 has 5 Faces
EGADS    : Body 4 has 9 Edges
EGADS    : Body 4 has 5 Loops
EGADS    : Body 4 has 6 Nodes
EGADS    : Body 5 is a SolidBody
EGADS    : Body 5 has 1 Shells
EGADS    : Body 5 has 5 Faces
EGADS    : Body 5 has 9 Edges
EGADS    : Body 5 has 5 Loops
EGADS    : Body 5 has 6 Nodes
EGADS    : Body 6 is a SolidBody
EGADS    : Body 6 has 1 Shells
EGADS    : Body 6 has 5 Faces
EGADS    : Body 6 has 9 Edges
EGADS    : Body 6 has 5 Loops
EGADS    : Body 6 has 6 Nodes
EGADS    : Body 7 is a SolidBody
EGADS    : Body 7 has 1 Shells
EGADS    : Body 7 has 5 Faces
EGADS    : Body 7 has 9 Edges
EGADS    : Body 7 has 5 Loops
EGADS    : Body 7 has 6 Nodes
EGADS    : Body 8 is a SolidBody
EGADS    : Body 8 has 1 Shells
EGADS    : Body 8 has 5 Faces
EGADS    : Body 8 has 9 Edges
EGADS    : Body 8 has 5 Loops
EGADS    : Body 8 has 6 Nodes
EGADS    : Body 9 is a SolidBody
EGADS    : Body 9 has 1 Shells
EGADS    : Body 9 has 5 Faces
EGADS    : Body 9 has 9 Edges
EGADS    : Body 9 has 5 Loops
EGADS    : Body 9 has 6 Nodes
EGADS    : Body 10 is a SolidBody
EGADS    : Body 10 has 1 Shells
EGADS    : Body 10 has 6 Faces
EGADS    : Body 10 has 12 Edges
EGADS    : Body 10 has 6 Loops
EGADS    : Body 10 has 8 Nodes

EGADS    : Check Grid BCs

EGADS    : Grid BCs are OK

EGADS    : Face Neighbor-Faces Information

EGADS    : QC  = Face Quad Combination Flag
EGADS    : IER = Face Isolated Edge Refinement Flag
EGADS    : ER  = Face Edge Refinement Factor
EGADS    :       Not applicable for Faces with a FarField Grid BC.
EGADS    : SF  = Face Scale Factor
EGADS    :       Not applicable for Faces with a FarField Grid BC.

EGADS    :   Face          Body    QC   IER       ER    Scale   Neighbor
EGADS    :     ID  Active    ID  Flag  Flag   Weight   Factor   Faces
EGADS    :      1     Yes     0     0     1        0        1   2 3 4 5 6
EGADS    :      2     Yes     0     0     1        0        1   1 7 8 9 10
EGADS    :      3     Yes     0     0     1        0        1   1 8 11 12 13 14
EGADS    :      4     Yes     0     0     1        0        1   1 7 12
EGADS    :      5     Yes     0     0     1        0        1   1 6 15 16 17 18
EGADS    :      6     Yes     0     0     1        0        1   1 5 15 16 17 19
EGADS    :                                                      20 21
EGADS    :      7     Yes     0     0     1        0        1   2 4 22
EGADS    :      8     Yes     0     0     1        0        1   2 3 11 22 23 24
EGADS    :      9     Yes     0     0     1        0        1   2 10 25 26 27 28
EGADS    :                                                      29 30
EGADS    :     10     Yes     0     0     1        0        1   2 9 26 27 28 31
EGADS    :     11     Yes     0     0     1        0        1   3 8 12 22
EGADS    :     12     Yes     0     0     1        0        1   3 4 11 13 14 22
EGADS    :                                                      32
EGADS    :     13     Yes     0     0     1        0        1   3 12 14 33 34 35
EGADS    :                                                      36
EGADS    :     14     Yes     0     0     1        0        1   3 12 13 33 34 35
EGADS    :                                                      36
EGADS    :     15     Yes     0     0     1        0        1   5 6 16
EGADS    :     16     Yes     0     0     1        0        1   5 6 15 17
EGADS    :     17     Yes     0     0     1        0        1   5 6 16
EGADS    :     18     Yes     0     0     1        0        1   5 19 37 38 39 40
EGADS    :                                                      41 42 43
EGADS    :     19     Yes     0     0     1        0        1   6 18 37 38 39 40
EGADS    :                                                      41 42 43
EGADS    :     20     Yes     0     0     1        0        1   6 21 44
EGADS    :     21     Yes     0     0     1        0        1   6 20 45
EGADS    :     22     Yes     0     0     1        0        1   7 8 11 12 23 24
EGADS    :                                                      46
EGADS    :     23     Yes     0     0     1        0        1   8 22 24 47 48 49
EGADS    :                                                      50
EGADS    :     24     Yes     0     0     1        0        1   8 22 23 47 48 49
EGADS    :                                                      50
EGADS    :     25     Yes     0     0     1        0        1   9 31 51 52 53 54
EGADS    :                                                      55 56 57
EGADS    :     26     Yes     0     0     1        0        1   9 10 27
EGADS    :     27     Yes     0     0     1        0        1   9 10 26 28
EGADS    :     28     Yes     0     0     1        0        1   9 10 27
EGADS    :     29     Yes     0     0     1        0        1   9 30 58
EGADS    :     30     Yes     0     0     1        0        1   9 29 59
EGADS    :     31     Yes     0     0     1        0        1   10 25 51 52 53
EGADS    :                                                      54 55 56 57
EGADS    :     32     Yes     0     0     1        0        1   12 46 60 61 62
EGADS    :                                                      63
EGADS    :     33     Yes     0     0     1        0        1   13 14 34
EGADS    :     34     Yes     0     0     1        0        1   13 14 33 35
EGADS    :     35     Yes     0     0     1        0        1   13 14 34
EGADS    :     36     Yes     0     0     1        0        1   13 14
EGADS    :     37     Yes     0     0     1        0        1   18 19 38
EGADS    :     38     Yes     0     0     1        0        1   18 19 37 39
EGADS    :     39     Yes     0     0     1        0        1   18 19 38
EGADS    :     40     Yes     0     0     1        0        1   18 19 41
EGADS    :     41     Yes     0     0     1        0        1   18 19 40 42
EGADS    :     42     Yes     0     0     1        0        1   18 19 41
EGADS    :     43     Yes     0     0     1        0        1   18 19
EGADS    :     44     Yes     0     0     1        0        1   20 45 64
EGADS    :     45     Yes     0     0     1        0        1   21 44 65
EGADS    :     46     Yes     0     0     1        0        1   22 32 60 61 62
EGADS    :                                                      63
EGADS    :     47     Yes     0     0     1        0        1   23 24
EGADS    :     48     Yes     0     0     1        0        1   23 24 49
EGADS    :     49     Yes     0     0     1        0        1   23 24 48 50
EGADS    :     50     Yes     0     0     1        0        1   23 24 49
EGADS    :     51     Yes     0     0     1        0        1   25 31
EGADS    :     52     Yes     0     0     1        0        1   25 31 53
EGADS    :     53     Yes     0     0     1        0        1   25 31 52 54
EGADS    :     54     Yes     0     0     1        0        1   25 31 53
EGADS    :     55     Yes     0     0     1        0        1   25 31 56
EGADS    :     56     Yes     0     0     1        0        1   25 31 55 57
EGADS    :     57     Yes     0     0     1        0        1   25 31 56
EGADS    :     58     Yes     0     0     1        0        1   29 59 66
EGADS    :     59     Yes     0     0     1        0        1   30 58 67
EGADS    :     60     Yes     0     0     1        0        1   32 46 61
EGADS    :     61     Yes     0     0     1        0        1   32 46 60 62
EGADS    :     62     Yes     0     0     1        0        1   32 46 61
EGADS    :     63     Yes     0     0     1        0        1   32 46
EGADS    :     64     Yes     0     0     1        0        1   44 65
EGADS    :     65     Yes     0     0     1        0        1   45 64
EGADS    :     66     Yes     0     0     1        0        1   58 67
EGADS    :     67     Yes     0     0     1        0        1   59 66
EGADS    :     68     Yes     1     0     1        0        1   69 70 71 72
EGADS    :     69     Yes     1     0     1        0        1   68 70 72
EGADS    :     70     Yes     1     0     1        0        1   68 69 71 72
EGADS    :     71     Yes     1     0     1        0        1   68 70 72
EGADS    :     72     Yes     1     0     1        0        1   68 69 70 71
EGADS    :     73     Yes     2     0     1        0        1   74 75 76 77
EGADS    :     74     Yes     2     0     1        0        1   73 75 77
EGADS    :     75     Yes     2     0     1        0        1   73 74 76 77
EGADS    :     76     Yes     2     0     1        0        1   73 75 77
EGADS    :     77     Yes     2     0     1        0        1   73 74 75 76
EGADS    :     78     Yes     3     0     1        0        1   79 80 81 82
EGADS    :     79     Yes     3     0     1        0        1   78 80 82
EGADS    :     80     Yes     3     0     1        0        1   78 79 81 82
EGADS    :     81     Yes     3     0     1        0        1   78 80 82
EGADS    :     82     Yes     3     0     1        0        1   78 79 80 81
EGADS    :     83     Yes     4     0     1        0        1   84 85 86 87
EGADS    :     84     Yes     4     0     1        0        1   83 85 86 87
EGADS    :     85     Yes     4     0     1        0        1   83 84 86
EGADS    :     86     Yes     4     0     1        0        1   83 84 85 87
EGADS    :     87     Yes     4     0     1        0        1   83 84 86
EGADS    :     88     Yes     5     0     1        0        1   89 90 91 92
EGADS    :     89     Yes     5     0     1        0        1   88 90 91 92
EGADS    :     90     Yes     5     0     1        0        1   88 89 91
EGADS    :     91     Yes     5     0     1        0        1   88 89 90 92
EGADS    :     92     Yes     5     0     1        0        1   88 89 91
EGADS    :     93     Yes     6     0     1        0        1   94 95 96 97
EGADS    :     94     Yes     6     0     1        0        1   93 95 97
EGADS    :     95     Yes     6     0     1        0        1   93 94 96 97
EGADS    :     96     Yes     6     0     1        0        1   93 95 97
EGADS    :     97     Yes     6     0     1        0        1   93 94 95 96
EGADS    :     98     Yes     7     0     1        0        1   99 100 101 102
EGADS    :     99     Yes     7     0     1        0        1   98 100 101 102
EGADS    :    100     Yes     7     0     1        0        1   98 99 101
EGADS    :    101     Yes     7     0     1        0        1   98 99 100 102
EGADS    :    102     Yes     7     0     1        0        1   98 99 101
EGADS    :    103     Yes     8     0     1        0        1   104 105 106 107
EGADS    :    104     Yes     8     0     1        0        1   103 105 106 107
EGADS    :    105     Yes     8     0     1        0        1   103 104 106
EGADS    :    106     Yes     8     0     1        0        1   103 104 105 107
EGADS    :    107     Yes     8     0     1        0        1   103 104 106
EGADS    :    108     Yes     9     0     1        0        1   109 110 111 112
EGADS    :    109     Yes     9     0     1        0        1   108 110 111 112
EGADS    :    110     Yes     9     0     1        0        1   108 109 111
EGADS    :    111     Yes     9     0     1        0        1   108 109 110 112
EGADS    :    112     Yes     9     0     1        0        1   108 109 111
EGADS    :    113     Yes    10     0     1       NA       NA   115 116 117 118
EGADS    :    114     Yes    10     0     1       NA       NA   115 116 117 118
EGADS    :    115     Yes    10     0     1       NA       NA   113 114 117 118
EGADS    :    116     Yes    10     0     1       NA       NA   113 114 117 118
EGADS    :    117     Yes    10     0     1       NA       NA   113 114 115 116
EGADS    :    118     Yes    10     0     1       NA       NA   113 114 115 116

EGADS    : Face Edges Information

EGADS    :   Face   Edges
EGADS    :      1   -1 4 3 -2 -5 -6
EGADS    :      2   -7 9 1 -8 10 11
EGADS    :      3   -12 2 17 -16 -15 14 -13
EGADS    :      4   -3 18 19 -20
EGADS    :      5   21 -22 23 24 25 26 -27 5
EGADS    :      6   27 28 -25 29 -30 -31 -21 6 32 33
EGADS    :      7   -19 34 7 -35
EGADS    :      8   -36 8 12 -40 -39 38 37
EGADS    :      9   -41 -10 47 46 45 -44 43 -42 48 49
EGADS    :     10   -47 -11 41 -53 -43 -52 -51 50
EGADS    :     11   13 54 55 40
EGADS    :     12   -17 20 60 59 58 -54 -14 -57 -56
EGADS    :     13   61 -62 63 64 65 66 -67 57 15
EGADS    :     14   67 68 -65 69 -70 -71 -61 16 56
EGADS    :     15   31 72 22
EGADS    :     16   30 73 -23 -72
EGADS    :     17   -73 -29 -24
EGADS    :     18   74 -75 76 77 78 -79 80 81 82 83 -84 -26
EGADS    :     19   84 85 -82 86 -87 -88 -78 89 -90 -91 -74 -28
EGADS    :     20   -92 94 -32 -93
EGADS    :     21   -94 95 93 -33
EGADS    :     22   -60 35 36 98 97 39 -55 -58 96
EGADS    :     23   -99 -98 -37 105 104 103 -102 101 -100
EGADS    :     24   -105 -38 -97 99 -109 -101 -108 -107 106
EGADS    :     25   -110 42 120 119 118 -117 116 115 114 -113 112 -111
EGADS    :     26   44 121 52
EGADS    :     27   -45 122 51 -121
EGADS    :     28   -122 -46 -50
EGADS    :     29   123 124 -48 -125
EGADS    :     30   125 -49 -124 -126
EGADS    :     31   -120 53 110 -133 -112 -132 -131 130 -116 -129 -128 127
EGADS    :     32   -134 -59 140 -139 -138 -137 -136 135
EGADS    :     33   71 141 62
EGADS    :     34   70 142 -63 -141
EGADS    :     35   -142 -69 -64
EGADS    :     36   -66 -68
EGADS    :     37   91 143 75
EGADS    :     38   90 144 -76 -143
EGADS    :     39   -144 -89 -77
EGADS    :     40   88 145 79
EGADS    :     41   87 146 -80 -145
EGADS    :     42   -146 -86 -81
EGADS    :     43   -83 -85
EGADS    :     44   147 92 148 149 -150 -151
EGADS    :     45   -147 153 150 -152 -148 -95
EGADS    :     46   -140 -96 134 157 156 -155 138 -154
EGADS    :     47   109 100
EGADS    :     48   102 158 108
EGADS    :     49   -103 159 107 -158
EGADS    :     50   -159 -104 -106
EGADS    :     51   133 111
EGADS    :     52   113 160 132
EGADS    :     53   -114 161 131 -160
EGADS    :     54   -161 -115 -130
EGADS    :     55   117 162 129
EGADS    :     56   -118 163 128 -162
EGADS    :     57   -163 -119 -127
EGADS    :     58   164 -123 165 166 -167 -168
EGADS    :     59   -164 170 167 -169 -165 126
EGADS    :     60   -135 171 -157
EGADS    :     61   136 172 -156 -171
EGADS    :     62   -172 137 155
EGADS    :     63   139 154
EGADS    :     64   -149 173 151 -174
EGADS    :     65   152 174 -153 -173
EGADS    :     66   -166 175 168 -176
EGADS    :     67   169 176 -170 -175
EGADS    :     68   -177 180 179 -178
EGADS    :     69   181 182 177
EGADS    :     70   178 183 -184 -181
EGADS    :     71   -179 -185 -183
EGADS    :     72   -180 -182 184 185
EGADS    :     73   -186 189 188 -187
EGADS    :     74   190 191 186
EGADS    :     75   187 192 -193 -190
EGADS    :     76   -188 -194 -192
EGADS    :     77   -189 -191 193 194
EGADS    :     78   -195 198 197 -196
EGADS    :     79   199 200 195
EGADS    :     80   196 201 -202 -199
EGADS    :     81   -197 -203 -201
EGADS    :     82   -198 -200 202 203
EGADS    :     83   204 -205 -206 207
EGADS    :     84   208 209 -210 -204
EGADS    :     85   211 205 210
EGADS    :     86   -209 212 206 -211
EGADS    :     87   -208 -207 -212
EGADS    :     88   213 -214 -215 216
EGADS    :     89   217 218 -219 -213
EGADS    :     90   220 214 219
EGADS    :     91   -218 221 215 -220
EGADS    :     92   -217 -216 -221
EGADS    :     93   -222 -223 224 225
EGADS    :     94   226 222 227
EGADS    :     95   -228 229 223 -226
EGADS    :     96   -230 -224 -229
EGADS    :     97   -225 230 228 -227
EGADS    :     98   231 234 -233 -232
EGADS    :     99   -231 -237 236 235
EGADS    :    100   238 237 232
EGADS    :    101   233 239 -236 -238
EGADS    :    102   -234 -235 -239
EGADS    :    103   240 -241 -242 243
EGADS    :    104   -240 244 245 -246
EGADS    :    105   247 241 246
EGADS    :    106   -245 248 242 -247
EGADS    :    107   -244 -243 -248
EGADS    :    108   -249 -252 251 250
EGADS    :    109   -253 249 255 -254
EGADS    :    110   256 -255 -250
EGADS    :    111   -251 257 254 -256
EGADS    :    112   252 253 -257
EGADS    :    113   258 259 -260 -261
EGADS    :    114   -262 265 264 -263
EGADS    :    115   266 262 -267 -258
EGADS    :    116   -268 260 269 -264
EGADS    :    117   261 268 -265 -266
EGADS    :    118   -259 267 263 -269

EGADS    : Face Loops Information

EGADS    :   Face   Loops
EGADS    :      1   1 2
EGADS    :      2   3 4
EGADS    :      3   5
EGADS    :      4   6
EGADS    :      5   7
EGADS    :      6   8 9
EGADS    :      7   10
EGADS    :      8   11
EGADS    :      9   12 13
EGADS    :     10   14
EGADS    :     11   15
EGADS    :     12   16
EGADS    :     13   17
EGADS    :     14   18
EGADS    :     15   19
EGADS    :     16   20
EGADS    :     17   21
EGADS    :     18   22
EGADS    :     19   23
EGADS    :     20   24
EGADS    :     21   25
EGADS    :     22   26
EGADS    :     23   27
EGADS    :     24   28
EGADS    :     25   29
EGADS    :     26   30
EGADS    :     27   31
EGADS    :     28   32
EGADS    :     29   33
EGADS    :     30   34
EGADS    :     31   35
EGADS    :     32   36
EGADS    :     33   37
EGADS    :     34   38
EGADS    :     35   39
EGADS    :     36   40
EGADS    :     37   41
EGADS    :     38   42
EGADS    :     39   43
EGADS    :     40   44
EGADS    :     41   45
EGADS    :     42   46
EGADS    :     43   47
EGADS    :     44   48
EGADS    :     45   49
EGADS    :     46   50
EGADS    :     47   51
EGADS    :     48   52
EGADS    :     49   53
EGADS    :     50   54
EGADS    :     51   55
EGADS    :     52   56
EGADS    :     53   57
EGADS    :     54   58
EGADS    :     55   59
EGADS    :     56   60
EGADS    :     57   61
EGADS    :     58   62
EGADS    :     59   63
EGADS    :     60   64
EGADS    :     61   65
EGADS    :     62   66
EGADS    :     63   67
EGADS    :     64   68
EGADS    :     65   69
EGADS    :     66   70
EGADS    :     67   71
EGADS    :     68   72
EGADS    :     69   73
EGADS    :     70   74
EGADS    :     71   75
EGADS    :     72   76
EGADS    :     73   77
EGADS    :     74   78
EGADS    :     75   79
EGADS    :     76   80
EGADS    :     77   81
EGADS    :     78   82
EGADS    :     79   83
EGADS    :     80   84
EGADS    :     81   85
EGADS    :     82   86
EGADS    :     83   87
EGADS    :     84   88
EGADS    :     85   89
EGADS    :     86   90
EGADS    :     87   91
EGADS    :     88   92
EGADS    :     89   93
EGADS    :     90   94
EGADS    :     91   95
EGADS    :     92   96
EGADS    :     93   97
EGADS    :     94   98
EGADS    :     95   99
EGADS    :     96   100
EGADS    :     97   101
EGADS    :     98   102
EGADS    :     99   103
EGADS    :    100   104
EGADS    :    101   105
EGADS    :    102   106
EGADS    :    103   107
EGADS    :    104   108
EGADS    :    105   109
EGADS    :    106   110
EGADS    :    107   111
EGADS    :    108   112
EGADS    :    109   113
EGADS    :    110   114
EGADS    :    111   115
EGADS    :    112   116
EGADS    :    113   117
EGADS    :    114   118
EGADS    :    115   119
EGADS    :    116   120
EGADS    :    117   121
EGADS    :    118   122

EGADS    : Loop Edges Information

EGADS    :   Loop  Active   Edges
EGADS    :      1     Yes   -1 4 3 -2
EGADS    :      2     Yes   -5 -6
EGADS    :      3     Yes   -7 9 1 -8
EGADS    :      4     Yes   10 11
EGADS    :      5     Yes   -12 2 17 -16 -15 14 -13
EGADS    :      6     Yes   -3 18 19 -20
EGADS    :      7     Yes   21 -22 23 24 25 26 -27 5
EGADS    :      8     Yes   27 28 -25 29 -30 -31 -21 6
EGADS    :      9     Yes   32 33
EGADS    :     10     Yes   -19 34 7 -35
EGADS    :     11     Yes   -36 8 12 -40 -39 38 37
EGADS    :     12     Yes   -41 -10 47 46 45 -44 43 -42
EGADS    :     13     Yes   48 49
EGADS    :     14     Yes   -47 -11 41 -53 -43 -52 -51 50
EGADS    :     15     Yes   13 54 55 40
EGADS    :     16     Yes   -17 20 60 59 58 -54 -14 -57 -56
EGADS    :     17     Yes   61 -62 63 64 65 66 -67 57 15
EGADS    :     18     Yes   67 68 -65 69 -70 -71 -61 16 56
EGADS    :     19     Yes   31 72 22
EGADS    :     20     Yes   30 73 -23 -72
EGADS    :     21     Yes   -73 -29 -24
EGADS    :     22     Yes   74 -75 76 77 78 -79 80 81 82 83 -84 -26
EGADS    :     23     Yes   84 85 -82 86 -87 -88 -78 89 -90 -91 -74 -28
EGADS    :     24     Yes   -92 94 -32 -93
EGADS    :     25     Yes   -94 95 93 -33
EGADS    :     26     Yes   -60 35 36 98 97 39 -55 -58 96
EGADS    :     27     Yes   -99 -98 -37 105 104 103 -102 101 -100
EGADS    :     28     Yes   -105 -38 -97 99 -109 -101 -108 -107 106
EGADS    :     29     Yes   -110 42 120 119 118 -117 116 115 114 -113 112 -111
EGADS    :     30     Yes   44 121 52
EGADS    :     31     Yes   -45 122 51 -121
EGADS    :     32     Yes   -122 -46 -50
EGADS    :     33     Yes   123 124 -48 -125
EGADS    :     34     Yes   125 -49 -124 -126
EGADS    :     35     Yes   -120 53 110 -133 -112 -132 -131 130 -116 -129 -128
EGADS    :                        127
EGADS    :     36     Yes   -134 -59 140 -139 -138 -137 -136 135
EGADS    :     37     Yes   71 141 62
EGADS    :     38     Yes   70 142 -63 -141
EGADS    :     39     Yes   -142 -69 -64
EGADS    :     40     Yes   -66 -68
EGADS    :     41     Yes   91 143 75
EGADS    :     42     Yes   90 144 -76 -143
EGADS    :     43     Yes   -144 -89 -77
EGADS    :     44     Yes   88 145 79
EGADS    :     45     Yes   87 146 -80 -145
EGADS    :     46     Yes   -146 -86 -81
EGADS    :     47     Yes   -83 -85
EGADS    :     48     Yes   147 92 148 149 -150 -151
EGADS    :     49     Yes   -147 153 150 -152 -148 -95
EGADS    :     50     Yes   -140 -96 134 157 156 -155 138 -154
EGADS    :     51     Yes   109 100
EGADS    :     52     Yes   102 158 108
EGADS    :     53     Yes   -103 159 107 -158
EGADS    :     54     Yes   -159 -104 -106
EGADS    :     55     Yes   133 111
EGADS    :     56     Yes   113 160 132
EGADS    :     57     Yes   -114 161 131 -160
EGADS    :     58     Yes   -161 -115 -130
EGADS    :     59     Yes   117 162 129
EGADS    :     60     Yes   -118 163 128 -162
EGADS    :     61     Yes   -163 -119 -127
EGADS    :     62     Yes   164 -123 165 166 -167 -168
EGADS    :     63     Yes   -164 170 167 -169 -165 126
EGADS    :     64     Yes   -135 171 -157
EGADS    :     65     Yes   136 172 -156 -171
EGADS    :     66     Yes   -172 137 155
EGADS    :     67     Yes   139 154
EGADS    :     68     Yes   -149 173 151 -174
EGADS    :     69     Yes   152 174 -153 -173
EGADS    :     70     Yes   -166 175 168 -176
EGADS    :     71     Yes   169 176 -170 -175
EGADS    :     72     Yes   -177 180 179 -178
EGADS    :     73     Yes   181 182 177
EGADS    :     74     Yes   178 183 -184 -181
EGADS    :     75     Yes   -179 -185 -183
EGADS    :     76     Yes   -180 -182 184 185
EGADS    :     77     Yes   -186 189 188 -187
EGADS    :     78     Yes   190 191 186
EGADS    :     79     Yes   187 192 -193 -190
EGADS    :     80     Yes   -188 -194 -192
EGADS    :     81     Yes   -189 -191 193 194
EGADS    :     82     Yes   -195 198 197 -196
EGADS    :     83     Yes   199 200 195
EGADS    :     84     Yes   196 201 -202 -199
EGADS    :     85     Yes   -197 -203 -201
EGADS    :     86     Yes   -198 -200 202 203
EGADS    :     87     Yes   204 -205 -206 207
EGADS    :     88     Yes   208 209 -210 -204
EGADS    :     89     Yes   211 205 210
EGADS    :     90     Yes   -209 212 206 -211
EGADS    :     91     Yes   -208 -207 -212
EGADS    :     92     Yes   213 -214 -215 216
EGADS    :     93     Yes   217 218 -219 -213
EGADS    :     94     Yes   220 214 219
EGADS    :     95     Yes   -218 221 215 -220
EGADS    :     96     Yes   -217 -216 -221
EGADS    :     97     Yes   -222 -223 224 225
EGADS    :     98     Yes   226 222 227
EGADS    :     99     Yes   -228 229 223 -226
EGADS    :    100     Yes   -230 -224 -229
EGADS    :    101     Yes   -225 230 228 -227
EGADS    :    102     Yes   231 234 -233 -232
EGADS    :    103     Yes   -231 -237 236 235
EGADS    :    104     Yes   238 237 232
EGADS    :    105     Yes   233 239 -236 -238
EGADS    :    106     Yes   -234 -235 -239
EGADS    :    107     Yes   240 -241 -242 243
EGADS    :    108     Yes   -240 244 245 -246
EGADS    :    109     Yes   247 241 246
EGADS    :    110     Yes   -245 248 242 -247
EGADS    :    111     Yes   -244 -243 -248
EGADS    :    112     Yes   -249 -252 251 250
EGADS    :    113     Yes   -253 249 255 -254
EGADS    :    114     Yes   256 -255 -250
EGADS    :    115     Yes   -251 257 254 -256
EGADS    :    116     Yes   252 253 -257
EGADS    :    117     Yes   258 259 -260 -261
EGADS    :    118     Yes   -262 265 264 -263
EGADS    :    119     Yes   266 262 -267 -258
EGADS    :    120     Yes   -268 260 269 -264
EGADS    :    121     Yes   261 268 -265 -266
EGADS    :    122     Yes   -259 267 263 -269

EGADS    : Edge Node, Scale Factor, and Neighbor-Faces Information

EGADS    : ESF = Edge Scale Factor
EGADS    :       Not applicable for DEGENERATE Edges or Edges with a FarField
EGADS    :       Grid BC Neighbor Face.

EGADS    :                                             Neighbor
EGADS    :   Edge  Body  Active Node1 Node2      ESF   Faces
EGADS    :      1     0     Yes     1     2        1   1 2
EGADS    :      2     0     Yes     2     3        1   1 3
EGADS    :      3     0     Yes     1     3        1   1 4
EGADS    :      4     0   DEGEN     1     1        -   1
EGADS    :      5     0     Yes     4     5        1   1 5
EGADS    :      6     0     Yes     5     4        1   1 6
EGADS    :      7     0     Yes     1     6        1   2 7
EGADS    :      8     0     Yes     6     2        1   2 8
EGADS    :      9     0   DEGEN     1     1        -   2
EGADS    :     10     0     Yes     7     8        1   2 9
EGADS    :     11     0     Yes     8     7        1   2 10
EGADS    :     12     0     Yes     2     9        1   3 8
EGADS    :     13     0     Yes     9    10        1   3 11
EGADS    :     14     0     Yes    11    10        1   3 12
EGADS    :     15     0     Yes    11    12        1   3 13
EGADS    :     16     0     Yes    12    13        1   3 14
EGADS    :     17     0     Yes     3    13        1   3 12
EGADS    :     18     0   DEGEN     1     1        -   4
EGADS    :     19     0     Yes     1    14        1   4 7
EGADS    :     20     0     Yes     3    14        1   4 12
EGADS    :     21     0     Yes     5    15        1   5 6
EGADS    :     22     0     Yes    16    15        1   5 15
EGADS    :     23     0     Yes    16    17        1   5 16
EGADS    :     24     0     Yes    17    18        1   5 17
EGADS    :     25     0     Yes    18    19        1   5 6
EGADS    :     26     0     Yes    19    20        1   5 18
EGADS    :     27     0     Yes     4    20        1   5 6
EGADS    :     28     0     Yes    20    19        1   6 19
EGADS    :     29     0     Yes    18    21        1   6 17
EGADS    :     30     0     Yes    22    21        1   6 16
EGADS    :     31     0     Yes    15    22        1   6 15
EGADS    :     32     0     Yes    23    24        1   6 20
EGADS    :     33     0     Yes    24    23        1   6 21
EGADS    :     34     0   DEGEN     1     1        -   7
EGADS    :     35     0     Yes    14     6        1   7 22
EGADS    :     36     0     Yes     6    25        1   8 22
EGADS    :     37     0     Yes    26    25        1   8 23
EGADS    :     38     0     Yes    27    26        1   8 24
EGADS    :     39     0     Yes    27    28        1   8 22
EGADS    :     40     0     Yes    28     9        1   8 11
EGADS    :     41     0     Yes     8    29        1   9 10
EGADS    :     42     0     Yes    29    30        1   9 25
EGADS    :     43     0     Yes    31    30        1   9 10
EGADS    :     44     0     Yes    31    32        1   9 26
EGADS    :     45     0     Yes    33    32        1   9 27
EGADS    :     46     0     Yes    34    33        1   9 28
EGADS    :     47     0     Yes     7    34        1   9 10
EGADS    :     48     0     Yes    35    36        1   9 29
EGADS    :     49     0     Yes    36    35        1   9 30
EGADS    :     50     0     Yes    37    34        1   10 28
EGADS    :     51     0     Yes    37    38        1   10 27
EGADS    :     52     0     Yes    38    31        1   10 26
EGADS    :     53     0     Yes    30    29        1   10 31
EGADS    :     54     0     Yes    10    39        1   11 12
EGADS    :     55     0     Yes    39    28        1   11 22
EGADS    :     56     0     Yes    13    40        1   12 14
EGADS    :     57     0     Yes    40    11        1   12 13
EGADS    :     58     0     Yes    41    39        1   12 22
EGADS    :     59     0     Yes    42    41        1   12 32
EGADS    :     60     0     Yes    14    42        1   12 22
EGADS    :     61     0     Yes    12    43        1   13 14
EGADS    :     62     0     Yes    44    43        1   13 33
EGADS    :     63     0     Yes    44    45        1   13 34
EGADS    :     64     0     Yes    45    46        1   13 35
EGADS    :     65     0     Yes    46    47        1   13 14
EGADS    :     66     0     Yes    47    48        1   13 36
EGADS    :     67     0     Yes    40    48        1   13 14
EGADS    :     68     0     Yes    48    47        1   14 36
EGADS    :     69     0     Yes    46    49        1   14 35
EGADS    :     70     0     Yes    50    49        1   14 34
EGADS    :     71     0     Yes    43    50        1   14 33
EGADS    :     72     0     Yes    22    16        1   15 16
EGADS    :     73     0     Yes    21    17        1   16 17
EGADS    :     74     0     Yes    19    51        1   18 19
EGADS    :     75     0     Yes    52    51        1   18 37
EGADS    :     76     0     Yes    52    53        1   18 38
EGADS    :     77     0     Yes    53    54        1   18 39
EGADS    :     78     0     Yes    54    55        1   18 19
EGADS    :     79     0     Yes    56    55        1   18 40
EGADS    :     80     0     Yes    56    57        1   18 41
EGADS    :     81     0     Yes    57    58        1   18 42
EGADS    :     82     0     Yes    58    59        1   18 19
EGADS    :     83     0     Yes    59    60        1   18 43
EGADS    :     84     0     Yes    20    60        1   18 19
EGADS    :     85     0     Yes    60    59        1   19 43
EGADS    :     86     0     Yes    58    61        1   19 42
EGADS    :     87     0     Yes    62    61        1   19 41
EGADS    :     88     0     Yes    55    62        1   19 40
EGADS    :     89     0     Yes    54    63        1   19 39
EGADS    :     90     0     Yes    64    63        1   19 38
EGADS    :     91     0     Yes    51    64        1   19 37
EGADS    :     92     0     Yes    65    66        1   20 44
EGADS    :     93     0     Yes    66    23        1   20 21
EGADS    :     94     0     Yes    65    24        1   20 21
EGADS    :     95     0     Yes    65    66        1   21 45
EGADS    :     96     0     Yes    41    42        1   22 46
EGADS    :     97     0     Yes    67    27        1   22 24
EGADS    :     98     0     Yes    25    67        1   22 23
EGADS    :     99     0     Yes    67    68        1   23 24
EGADS    :    100     0     Yes    68    69        1   23 47
EGADS    :    101     0     Yes    70    69        1   23 24
EGADS    :    102     0     Yes    70    71        1   23 48
EGADS    :    103     0     Yes    72    71        1   23 49
EGADS    :    104     0     Yes    73    72        1   23 50
EGADS    :    105     0     Yes    26    73        1   23 24
EGADS    :    106     0     Yes    74    73        1   24 50
EGADS    :    107     0     Yes    74    75        1   24 49
EGADS    :    108     0     Yes    75    70        1   24 48
EGADS    :    109     0     Yes    69    68        1   24 47
EGADS    :    110     0     Yes    29    76        1   25 31
EGADS    :    111     0     Yes    76    77        1   25 51
EGADS    :    112     0     Yes    78    77        1   25 31
EGADS    :    113     0     Yes    78    79        1   25 52
EGADS    :    114     0     Yes    80    79        1   25 53
EGADS    :    115     0     Yes    81    80        1   25 54
EGADS    :    116     0     Yes    82    81        1   25 31
EGADS    :    117     0     Yes    82    83        1   25 55
EGADS    :    118     0     Yes    84    83        1   25 56
EGADS    :    119     0     Yes    85    84        1   25 57
EGADS    :    120     0     Yes    30    85        1   25 31
EGADS    :    121     0     Yes    32    38        1   26 27
EGADS    :    122     0     Yes    33    37        1   27 28
EGADS    :    123     0     Yes    86    87        1   29 58
EGADS    :    124     0     Yes    87    36        1   29 30
EGADS    :    125     0     Yes    86    35        1   29 30
EGADS    :    126     0     Yes    86    87        1   30 59
EGADS    :    127     0     Yes    88    85        1   31 57
EGADS    :    128     0     Yes    88    89        1   31 56
EGADS    :    129     0     Yes    89    82        1   31 55
EGADS    :    130     0     Yes    90    81        1   31 54
EGADS    :    131     0     Yes    90    91        1   31 53
EGADS    :    132     0     Yes    91    78        1   31 52
EGADS    :    133     0     Yes    77    76        1   31 51
EGADS    :    134     0     Yes    41    92        1   32 46
EGADS    :    135     0     Yes    93    92        1   32 60
EGADS    :    136     0     Yes    93    94        1   32 61
EGADS    :    137     0     Yes    94    95        1   32 62
EGADS    :    138     0     Yes    95    96        1   32 46
EGADS    :    139     0     Yes    96    97        1   32 63
EGADS    :    140     0     Yes    42    97        1   32 46
EGADS    :    141     0     Yes    50    44        1   33 34
EGADS    :    142     0     Yes    49    45        1   34 35
EGADS    :    143     0     Yes    64    52        1   37 38
EGADS    :    144     0     Yes    63    53        1   38 39
EGADS    :    145     0     Yes    62    56        1   40 41
EGADS    :    146     0     Yes    61    57        1   41 42
EGADS    :    147     0     Yes    98    65        1   44 45
EGADS    :    148     0     Yes    66    99        1   44 45
EGADS    :    149     0     Yes    99   100        1   44 64
EGADS    :    150     0     Yes   101   100        1   44 45
EGADS    :    151     0     Yes    98   101        1   44 64
EGADS    :    152     0     Yes    99   100        1   45 65
EGADS    :    153     0     Yes    98   101        1   45 65
EGADS    :    154     0     Yes    97    96        1   46 63
EGADS    :    155     0     Yes    95   102        1   46 62
EGADS    :    156     0     Yes   103   102        1   46 61
EGADS    :    157     0     Yes    92   103        1   46 60
EGADS    :    158     0     Yes    71    75        1   48 49
EGADS    :    159     0     Yes    72    74        1   49 50
EGADS    :    160     0     Yes    79    91        1   52 53
EGADS    :    161     0     Yes    80    90        1   53 54
EGADS    :    162     0     Yes    83    89        1   55 56
EGADS    :    163     0     Yes    84    88        1   56 57
EGADS    :    164     0     Yes   104    87        1   58 59
EGADS    :    165     0     Yes    86   105        1   58 59
EGADS    :    166     0     Yes   105   106        1   58 66
EGADS    :    167     0     Yes   107   106        1   58 59
EGADS    :    168     0     Yes   104   107        1   58 66
EGADS    :    169     0     Yes   105   106        1   59 67
EGADS    :    170     0     Yes   104   107        1   59 67
EGADS    :    171     0     Yes    93   103        1   60 61
EGADS    :    172     0     Yes    94   102        1   61 62
EGADS    :    173     0     Yes    99    98        1   64 65
EGADS    :    174     0     Yes   100   101        1   64 65
EGADS    :    175     0     Yes   105   104        1   66 67
EGADS    :    176     0     Yes   106   107        1   66 67
EGADS    :    177     1     Yes   108   109        1   68 69
EGADS    :    178     1     Yes   109   110        1   68 70
EGADS    :    179     1     Yes   111   110        1   68 71
EGADS    :    180     1     Yes   108   111        1   68 72
EGADS    :    181     1     Yes   109   112        1   69 70
EGADS    :    182     1     Yes   112   108        1   69 72
EGADS    :    183     1     Yes   110   113        1   70 71
EGADS    :    184     1     Yes   112   113        1   70 72
EGADS    :    185     1     Yes   113   111        1   71 72
EGADS    :    186     2     Yes   114   115        1   73 74
EGADS    :    187     2     Yes   115   116        1   73 75
EGADS    :    188     2     Yes   117   116        1   73 76
EGADS    :    189     2     Yes   114   117        1   73 77
EGADS    :    190     2     Yes   115   118        1   74 75
EGADS    :    191     2     Yes   118   114        1   74 77
EGADS    :    192     2     Yes   116   119        1   75 76
EGADS    :    193     2     Yes   118   119        1   75 77
EGADS    :    194     2     Yes   119   117        1   76 77
EGADS    :    195     3     Yes   120   121        1   78 79
EGADS    :    196     3     Yes   121   122        1   78 80
EGADS    :    197     3     Yes   123   122        1   78 81
EGADS    :    198     3     Yes   120   123        1   78 82
EGADS    :    199     3     Yes   121   124        1   79 80
EGADS    :    200     3     Yes   124   120        1   79 82
EGADS    :    201     3     Yes   122   125        1   80 81
EGADS    :    202     3     Yes   124   125        1   80 82
EGADS    :    203     3     Yes   125   123        1   81 82
EGADS    :    204     4     Yes   126   127        1   83 84
EGADS    :    205     4     Yes   128   127        1   83 85
EGADS    :    206     4     Yes   129   128        1   83 86
EGADS    :    207     4     Yes   129   126        1   83 87
EGADS    :    208     4     Yes   126   130        1   84 87
EGADS    :    209     4     Yes   130   131        1   84 86
EGADS    :    210     4     Yes   127   131        1   84 85
EGADS    :    211     4     Yes   131   128        1   85 86
EGADS    :    212     4     Yes   130   129        1   86 87
EGADS    :    213     5     Yes   132   133        1   88 89
EGADS    :    214     5     Yes   134   133        1   88 90
EGADS    :    215     5     Yes   135   134        1   88 91
EGADS    :    216     5     Yes   135   132        1   88 92
EGADS    :    217     5     Yes   132   136        1   89 92
EGADS    :    218     5     Yes   136   137        1   89 91
EGADS    :    219     5     Yes   133   137        1   89 90
EGADS    :    220     5     Yes   137   134        1   90 91
EGADS    :    221     5     Yes   136   135        1   91 92
EGADS    :    222     6     Yes   138   139        1   93 94
EGADS    :    223     6     Yes   140   138        1   93 95
EGADS    :    224     6     Yes   140   141        1   93 96
EGADS    :    225     6     Yes   141   139        1   93 97
EGADS    :    226     6     Yes   142   138        1   94 95
EGADS    :    227     6     Yes   139   142        1   94 97
EGADS    :    228     6     Yes   143   142        1   95 97
EGADS    :    229     6     Yes   143   140        1   95 96
EGADS    :    230     6     Yes   141   143        1   96 97
EGADS    :    231     7     Yes   144   145        1   98 99
EGADS    :    232     7     Yes   144   146        1   98 100
EGADS    :    233     7     Yes   146   147        1   98 101
EGADS    :    234     7     Yes   145   147        1   98 102
EGADS    :    235     7     Yes   148   145        1   99 102
EGADS    :    236     7     Yes   149   148        1   99 101
EGADS    :    237     7     Yes   149   144        1   99 100
EGADS    :    238     7     Yes   146   149        1   100 101
EGADS    :    239     7     Yes   147   148        1   101 102
EGADS    :    240     8     Yes   150   151        1   103 104
EGADS    :    241     8     Yes   152   151        1   103 105
EGADS    :    242     8     Yes   153   152        1   103 106
EGADS    :    243     8     Yes   153   150        1   103 107
EGADS    :    244     8     Yes   150   154        1   104 107
EGADS    :    245     8     Yes   154   155        1   104 106
EGADS    :    246     8     Yes   151   155        1   104 105
EGADS    :    247     8     Yes   155   152        1   105 106
EGADS    :    248     8     Yes   154   153        1   106 107
EGADS    :    249     9     Yes   156   157        1   108 109
EGADS    :    250     9     Yes   158   157        1   108 110
EGADS    :    251     9     Yes   159   158        1   108 111
EGADS    :    252     9     Yes   159   156        1   108 112
EGADS    :    253     9     Yes   156   160        1   109 112
EGADS    :    254     9     Yes   160   161        1   109 111
EGADS    :    255     9     Yes   157   161        1   109 110
EGADS    :    256     9     Yes   158   161        1   110 111
EGADS    :    257     9     Yes   159   160        1   111 112
EGADS    :    258    10     Yes   163   162       NA   113 115
EGADS    :    259    10     Yes   162   164       NA   113 118
EGADS    :    260    10     Yes   165   164       NA   113 116
EGADS    :    261    10     Yes   163   165       NA   113 117
EGADS    :    262    10     Yes   167   166       NA   114 115
EGADS    :    263    10     Yes   166   168       NA   114 118
EGADS    :    264    10     Yes   169   168       NA   114 116
EGADS    :    265    10     Yes   167   169       NA   114 117
EGADS    :    266    10     Yes   163   167       NA   115 117
EGADS    :    267    10     Yes   162   166       NA   115 118
EGADS    :    268    10     Yes   165   169       NA   116 117
EGADS    :    269    10     Yes   164   168       NA   116 118

EGADS    : Node Information

EGADS    :   Node  Active      Coordinates
EGADS    :      1     Yes                0                0                0
EGADS    :      2     Yes       121.026192                0                0
EGADS    :      3     Yes       121.026192               10                0
EGADS    :      4     Yes       54.9020417       7.00084115                0
EGADS    :      5     Yes        97.361045       7.90366896                0
EGADS    :      6     Yes       121.026192                0                0
EGADS    :      7     Yes        97.361045                0                0
EGADS    :      8     Yes       54.9020417                0                0
EGADS    :      9     Yes       165.026192                0                7
EGADS    :     10     Yes       165.026192              0.5              8.5
EGADS    :     11     Yes       156.577382       2.32417494       6.86784347
EGADS    :     12     Yes       160.457816       1.16501909       6.24763245
EGADS    :     13     Yes       152.092394       3.29252447       6.00142548
EGADS    :     14     Yes       121.026192                0               10
EGADS    :     15     Yes       97.4729828       13.4242093                0
EGADS    :     16     Yes       93.4296648       13.4242093                0
EGADS    :     17     Yes        93.813734       32.4820648                0
EGADS    :     18     Yes       97.8594113       32.4820648                0
EGADS    :     19     Yes       97.9335611       36.1389817                0
EGADS    :     20     Yes       75.3047874       36.1389817                0
EGADS    :     21     Yes        93.813734       32.4820648                0
EGADS    :     22     Yes       93.4296648       13.4242093                0
EGADS    :     23     Yes       72.4759225       29.3018771                0
EGADS    :     24     Yes       83.5054156       29.3018771                0
EGADS    :     25     Yes       152.092394                0       6.00142548
EGADS    :     26     Yes       160.457816                0       6.24763245
EGADS    :     27     Yes       156.577382                0       6.86784347
EGADS    :     28     Yes       165.026192                0              8.5
EGADS    :     29     Yes       75.3047874                0                0
EGADS    :     30     Yes       97.9335611                0                0
EGADS    :     31     Yes       97.8594113                0                0
EGADS    :     32     Yes        93.813734                0                0
EGADS    :     33     Yes       93.4296648                0                0
EGADS    :     34     Yes       97.4729828                0                0
EGADS    :     35     Yes       72.4759225                0                0
EGADS    :     36     Yes       83.5054156                0                0
EGADS    :     37     Yes       93.4296648                0                0
EGADS    :     38     Yes        93.813734                0                0
EGADS    :     39     Yes       165.026192                0               10
EGADS    :     40     Yes       139.227902       5.03861756       7.07099122
EGADS    :     41     Yes       159.822328                0               10
EGADS    :     42     Yes       137.454662                0               10
EGADS    :     43     Yes       162.492237        6.6562396        7.4148274
EGADS    :     44     Yes       153.156875        6.6562396       8.10980625
EGADS    :     45     Yes       168.687412       34.4921381       13.6297335
EGADS    :     46     Yes       172.805054       34.4921381       13.3315303
EGADS    :     47     Yes       173.282633        35.781198       13.6055284
EGADS    :     48     Yes        165.02399        35.781198       13.6055284
EGADS    :     49     Yes       168.687412       34.4921381        13.033327
EGADS    :     50     Yes       153.156875        6.6562396       6.71984855
EGADS    :     51     Yes       100.269362       41.7493571                0
EGADS    :     52     Yes       94.7284993       41.7493571                0
EGADS    :     53     Yes       107.349293       67.6443173       1.84589548
EGADS    :     54     Yes       111.050367       67.6443173       1.25578139
EGADS    :     55     Yes       111.248847       68.1210465       1.31074802
EGADS    :     56     Yes       107.581644       68.1210465       1.89111513
EGADS    :     57     Yes       121.153699       95.9694651       4.50848923
EGADS    :     58     Yes       122.843146       95.9694651       4.52165604
EGADS    :     59     Yes       123.552357       97.6729236        4.7180639
EGADS    :     60     Yes       118.391317       97.6729236       3.99272703
EGADS    :     61     Yes       121.153699       95.9694651       4.20550678
EGADS    :     62     Yes       107.581644       68.1210465      0.865881946
EGADS    :     63     Yes       107.349293       67.6443173      0.808537183
EGADS    :     64     Yes       94.7284993       41.7493571                0
EGADS    :     65     Yes       79.4370049       29.3018771                0
EGADS    :     66     Yes        70.524066       29.3018771                0
EGADS    :     67     Yes       139.227902                0       7.07099122
EGADS    :     68     Yes        165.02399                0       13.6055284
EGADS    :     69     Yes       173.282633                0       13.6055284
EGADS    :     70     Yes       172.805054                0       13.3315303
EGADS    :     71     Yes       168.687412                0        13.033327
EGADS    :     72     Yes       153.156875                0       6.71984855
EGADS    :     73     Yes       162.492237                0        7.4148274
EGADS    :     74     Yes       153.156875                0       8.10980625
EGADS    :     75     Yes       168.687412                0       13.6297335
EGADS    :     76     Yes       118.391317                0       3.99272703
EGADS    :     77     Yes       123.552357                0        4.7180639
EGADS    :     78     Yes       122.843146                0       4.52165604
EGADS    :     79     Yes       121.153699                0       4.20550678
EGADS    :     80     Yes       107.581644                0      0.865881946
EGADS    :     81     Yes       111.248847                0       1.31074802
EGADS    :     82     Yes       111.050367                0       1.25578139
EGADS    :     83     Yes       107.349293                0      0.808537183
EGADS    :     84     Yes       94.7284993                0                0
EGADS    :     85     Yes       100.269362                0                0
EGADS    :     86     Yes        70.524066                0                0
EGADS    :     87     Yes       79.4370049                0                0
EGADS    :     88     Yes       94.7284993                0                0
EGADS    :     89     Yes       107.349293                0       1.84589548
EGADS    :     90     Yes       107.581644                0       1.89111513
EGADS    :     91     Yes       121.153699                0       4.50848923
EGADS    :     92     Yes       160.542569                0       11.9206428
EGADS    :     93     Yes       151.486032      0.673415422       11.9206428
EGADS    :     94     Yes       165.862466      0.235428105       34.9229244
EGADS    :     95     Yes       169.168425                0       34.9229244
EGADS    :     96     Yes        169.38016                0        35.487551
EGADS    :     97     Yes       162.942213                0        35.487551
EGADS    :     98     Yes       90.5173952       29.3018771                0
EGADS    :     99     Yes       60.5173952       29.3018771                0
EGADS    :    100     Yes       60.5173952       29.3018771                0
EGADS    :    101     Yes       90.5173952       29.3018771                0
EGADS    :    102     Yes       165.862466                0       34.9229244
EGADS    :    103     Yes       151.486032                0       11.9206428
EGADS    :    104     Yes       90.5173952                0                0
EGADS    :    105     Yes       60.5173952                0                0
EGADS    :    106     Yes       60.5173952                0                0
EGADS    :    107     Yes       90.5173952                0                0
EGADS    :    108     Yes       111.321903                0       1.86654259
EGADS    :    109     Yes       108.055298                0       0.93793256
EGADS    :    110     Yes        121.33061                0       4.22828065
EGADS    :    111     Yes       122.700876                0       4.71377572
EGADS    :    112     Yes       107.907885                0       1.87632098
EGADS    :    113     Yes       121.289329                0       4.49106118
EGADS    :    114     Yes       100.394138                0                0
EGADS    :    115     Yes       95.1284577                0                0
EGADS    :    116     Yes       107.505559                0      0.813039939
EGADS    :    117     Yes       110.968457                0      0.689237814
EGADS    :    118     Yes       95.3800953                0                0
EGADS    :    119     Yes       107.657908                0       1.77558767
EGADS    :    120     Yes       97.2857328                0                0
EGADS    :    121     Yes       93.6847537                0                0
EGADS    :    122     Yes       94.0587466                0                0
EGADS    :    123     Yes       97.7824572                0                0
EGADS    :    124     Yes       93.9345512                0                0
EGADS    :    125     Yes       94.3601422                0                0
EGADS    :    126     Yes       97.2857328       13.7821489                0
EGADS    :    127     Yes       97.7824572       32.3393376                0
EGADS    :    128     Yes       94.3601422       32.2302343                0
EGADS    :    129     Yes       93.9345512       13.6726922                0
EGADS    :    130     Yes       93.6847537       13.6742093                0
EGADS    :    131     Yes       94.0587466       32.2320648                0
EGADS    :    132     Yes       100.394138       42.0879216                0
EGADS    :    133     Yes       110.968457       67.4483237      0.689237814
EGADS    :    134     Yes       107.657908       67.3218336       1.77558767
EGADS    :    135     Yes       95.3800953       41.8796344                0
EGADS    :    136     Yes       95.1284577       41.9993571                0
EGADS    :    137     Yes       107.505559       67.3943173      0.813039939
EGADS    :    138     Yes       121.330781       95.7095395       4.49106118
EGADS    :    139     Yes       122.742253       95.7419985       4.26970731
EGADS    :    140     Yes       108.055908       68.3356022       1.87632098
EGADS    :    141     Yes       111.300912       68.4526045      0.818951249
EGADS    :    142     Yes       121.289158       95.7293907       4.22828065
EGADS    :    143     Yes       107.907275       68.4064908       0.93793256
EGADS    :    144     Yes       162.652062                0       6.87525931
EGADS    :    145     Yes       172.609142                0       12.9541609
EGADS    :    146     Yes       153.959016                0       6.86654493
EGADS    :    147     Yes       168.960275                0        12.950503
EGADS    :    148     Yes       169.001731                0        13.500001
EGADS    :    149     Yes        154.05778                0       8.17566644
EGADS    :    150     Yes       162.652062       7.30770007       6.87525931
EGADS    :    151     Yes       172.609142       34.0557129       12.9541609
EGADS    :    152     Yes       169.001731        33.980789        13.500001
EGADS    :    153     Yes        154.05778       7.12920153       8.17566644
EGADS    :    154     Yes       153.959016       7.18327767       6.86654493
EGADS    :    155     Yes       168.960275       34.0034872        12.950503
EGADS    :    156     Yes       160.730069                0       12.4206428
EGADS    :    157     Yes       168.980925                0       34.4229244
EGADS    :    158     Yes       166.139589      0.215327731       34.4229244
EGADS    :    159     Yes       152.388156      0.632183325       12.4206428
EGADS    :    160     Yes       152.388156                0       12.4206428
EGADS    :    161     Yes       166.139589                0       34.4229244
EGADS    :    162     Yes                0                0       1962.43554
EGADS    :    163     Yes                0                0                0
EGADS    :    164     Yes                0       1953.45847       1962.43554
EGADS    :    165     Yes                0       1953.45847                0
EGADS    :    166     Yes       2040.09979                0       1962.43554
EGADS    :    167     Yes       2040.09979                0                0
EGADS    :    168     Yes       2040.09979       1953.45847       1962.43554
EGADS    :    169     Yes       2040.09979       1953.45847                0

EGADS    : Face and Edge Match Information

EGADS    : No Face Matches Found

AFLR4    : Surface Mesh Spacing Setup

AFLR4    : Max Bounding Box Length     = 3906.92
AFLR4    : Min Bounding Box Length     = 3906.92
AFLR4    : Max Ref Bounding Box Length = 195.346
AFLR4    : Min Ref Bounding Box Length = 53.021
AFLR4    : Reference Length            = 53.021
AFLR4    : BL Thickness                = 0
AFLR4    : FarField Spacing            = 428.462
AFLR4    : Abs Min Surf Spacing        = 0.132552
AFLR4    : Min Surf Spacing            = 0.265105
AFLR4    : Max Surf Spacing            = 5.3021
AFLR4    : Global Scale Factor         = 1

AFLR4    : Geometry Definition Information

AFLR4    : Definition              Definition   Composite             Grid BC
AFLR4    :         ID                    Type          ID                Type
AFLR4    :          0     glue-only composite           -                   -
AFLR4    :          1            CAD geometry           0            STD w/BL
AFLR4    :          2            CAD geometry           0            STD w/BL
AFLR4    :          3            CAD geometry           0            STD w/BL
AFLR4    :          4            CAD geometry           0            STD w/BL
AFLR4    :          5            CAD geometry           0            STD w/BL
AFLR4    :          6            CAD geometry           0            STD w/BL
AFLR4    :          7            CAD geometry           0            STD w/BL
AFLR4    :          8            CAD geometry           0            STD w/BL
AFLR4    :          9            CAD geometry           0            STD w/BL
AFLR4    :         10            CAD geometry           0            STD w/BL
AFLR4    :         11            CAD geometry           0            STD w/BL
AFLR4    :         12            CAD geometry           0            STD w/BL
AFLR4    :         13            CAD geometry           0            STD w/BL
AFLR4    :         14            CAD geometry           0            STD w/BL
AFLR4    :         15            CAD geometry           0            STD w/BL
AFLR4    :         16            CAD geometry           0            STD w/BL
AFLR4    :         17            CAD geometry           0            STD w/BL
AFLR4    :         18            CAD geometry           0            STD w/BL
AFLR4    :         19            CAD geometry           0            STD w/BL
AFLR4    :         20            CAD geometry           0            STD w/BL
AFLR4    :         21            CAD geometry           0            STD w/BL
AFLR4    :         22            CAD geometry           0            STD w/BL
AFLR4    :         23            CAD geometry           0            STD w/BL
AFLR4    :         24            CAD geometry           0            STD w/BL
AFLR4    :         25            CAD geometry           0            STD w/BL
AFLR4    :         26            CAD geometry           0            STD w/BL
AFLR4    :         27            CAD geometry           0            STD w/BL
AFLR4    :         28            CAD geometry           0            STD w/BL
AFLR4    :         29            CAD geometry           0            STD w/BL
AFLR4    :         30            CAD geometry           0            STD w/BL
AFLR4    :         31            CAD geometry           0            STD w/BL
AFLR4    :         32            CAD geometry           0            STD w/BL
AFLR4    :         33            CAD geometry           0            STD w/BL
AFLR4    :         34            CAD geometry           0            STD w/BL
AFLR4    :         35            CAD geometry           0            STD w/BL
AFLR4    :         36            CAD geometry           0            STD w/BL
AFLR4    :         37            CAD geometry           0            STD w/BL
AFLR4    :         38            CAD geometry           0            STD w/BL
AFLR4    :         39            CAD geometry           0            STD w/BL
AFLR4    :         40            CAD geometry           0            STD w/BL
AFLR4    :         41            CAD geometry           0            STD w/BL
AFLR4    :         42            CAD geometry           0            STD w/BL
AFLR4    :         43            CAD geometry           0            STD w/BL
AFLR4    :         44            CAD geometry           0            STD w/BL
AFLR4    :         45            CAD geometry           0            STD w/BL
AFLR4    :         46            CAD geometry           0            STD w/BL
AFLR4    :         47            CAD geometry           0            STD w/BL
AFLR4    :         48            CAD geometry           0            STD w/BL
AFLR4    :         49            CAD geometry           0            STD w/BL
AFLR4    :         50            CAD geometry           0            STD w/BL
AFLR4    :         51            CAD geometry           0            STD w/BL
AFLR4    :         52            CAD geometry           0            STD w/BL
AFLR4    :         53            CAD geometry           0            STD w/BL
AFLR4    :         54            CAD geometry           0            STD w/BL
AFLR4    :         55            CAD geometry           0            STD w/BL
AFLR4    :         56            CAD geometry           0            STD w/BL
AFLR4    :         57            CAD geometry           0            STD w/BL
AFLR4    :         58            CAD geometry           0            STD w/BL
AFLR4    :         59            CAD geometry           0            STD w/BL
AFLR4    :         60            CAD geometry           0            STD w/BL
AFLR4    :         61            CAD geometry           0            STD w/BL
AFLR4    :         62            CAD geometry           0            STD w/BL
AFLR4    :         63            CAD geometry           0            STD w/BL
AFLR4    :         64            CAD geometry           0            STD w/BL
AFLR4    :         65            CAD geometry           0            STD w/BL
AFLR4    :         66            CAD geometry           0            STD w/BL
AFLR4    :         67            CAD geometry           0            STD w/BL
AFLR4    :         68            CAD geometry           0            STD w/BL
AFLR4    :         69            CAD geometry           0            STD w/BL
AFLR4    :         70            CAD geometry           0            STD w/BL
AFLR4    :         71            CAD geometry           0            STD w/BL
AFLR4    :         72            CAD geometry           0            STD w/BL
AFLR4    :         73            CAD geometry           0            STD w/BL
AFLR4    :         74            CAD geometry           0            STD w/BL
AFLR4    :         75            CAD geometry           0            STD w/BL
AFLR4    :         76            CAD geometry           0            STD w/BL
AFLR4    :         77            CAD geometry           0            STD w/BL
AFLR4    :         78            CAD geometry           0            STD w/BL
AFLR4    :         79            CAD geometry           0            STD w/BL
AFLR4    :         80            CAD geometry           0            STD w/BL
AFLR4    :         81            CAD geometry           0            STD w/BL
AFLR4    :         82            CAD geometry           0            STD w/BL
AFLR4    :         83            CAD geometry           0            STD w/BL
AFLR4    :         84            CAD geometry           0            STD w/BL
AFLR4    :         85            CAD geometry           0            STD w/BL
AFLR4    :         86            CAD geometry           0            STD w/BL
AFLR4    :         87            CAD geometry           0            STD w/BL
AFLR4    :         88            CAD geometry           0            STD w/BL
AFLR4    :         89            CAD geometry           0            STD w/BL
AFLR4    :         90            CAD geometry           0            STD w/BL
AFLR4    :         91            CAD geometry           0            STD w/BL
AFLR4    :         92            CAD geometry           0            STD w/BL
AFLR4    :         93            CAD geometry           0            STD w/BL
AFLR4    :         94            CAD geometry           0            STD w/BL
AFLR4    :         95            CAD geometry           0            STD w/BL
AFLR4    :         96            CAD geometry           0            STD w/BL
AFLR4    :         97            CAD geometry           0            STD w/BL
AFLR4    :         98            CAD geometry           0            STD w/BL
AFLR4    :         99            CAD geometry           0            STD w/BL
AFLR4    :        100            CAD geometry           0            STD w/BL
AFLR4    :        101            CAD geometry           0            STD w/BL
AFLR4    :        102            CAD geometry           0            STD w/BL
AFLR4    :        103            CAD geometry           0            STD w/BL
AFLR4    :        104            CAD geometry           0            STD w/BL
AFLR4    :        105            CAD geometry           0            STD w/BL
AFLR4    :        106            CAD geometry           0            STD w/BL
AFLR4    :        107            CAD geometry           0            STD w/BL
AFLR4    :        108            CAD geometry           0            STD w/BL
AFLR4    :        109            CAD geometry           0            STD w/BL
AFLR4    :        110            CAD geometry           0            STD w/BL
AFLR4    :        111            CAD geometry           0            STD w/BL
AFLR4    :        112            CAD geometry           0            STD w/BL
AFLR4    :        113            CAD geometry           0            FARFIELD
AFLR4    :        114            CAD geometry           0            FARFIELD
AFLR4    :        115            CAD geometry           0            FARFIELD
AFLR4    :        116            CAD geometry           0            FARFIELD
AFLR4    :        117            CAD geometry           0            FARFIELD
AFLR4    :        118            CAD geometry           0            FARFIELD

AFLR4    : Case has 10 Proximity Checking Components

AFLR4    : Component 1 includes Definitions 1 2 3 4 7 8 11 12 22
AFLR4    : Component 2 includes Definitions 5 6 9 10 15 16 17 18 19 25 26 27 28
AFLR4    :                                  31 37 38 39 40 41 42 43 51 52 53 54
AFLR4    :                                  55 56 57 68 69 70 71 72 73 77 78 82
AFLR4    :                                  83 84 88 89 93 97
AFLR4    : Component 3 includes Definitions 13 14 23 24 33 34 35 36 47 48 49 50
AFLR4    :                                  74 75 76 98 99 103 104
AFLR4    : Component 4 includes Definitions 32 46 60 61 62 63 79 80 81 108 109
AFLR4    : Component 5 includes Definitions 44 45 58 59 64 65 66 67 85 86 87
AFLR4    : Component 6 includes Definitions 20 21 29 30 90 91 92
AFLR4    : Component 7 includes Definitions 94 95 96
AFLR4    : Component 8 includes Definitions 100 101 102
AFLR4    : Component 9 includes Definitions 105 106 107
AFLR4    : Component 10 includes Definitions 110 111 112

AFLR4    : Define CAD surface definition 1
AFLR4    : Define CAD surface definition 2
AFLR4    : Define CAD surface definition 3
AFLR4    : Define CAD surface definition 4
AFLR4    : Define CAD surface definition 5
AFLR4    : Define CAD surface definition 6
AFLR4    : Define CAD surface definition 7
AFLR4    : Define CAD surface definition 8
AFLR4    : Define CAD surface definition 9
AFLR4    : Define CAD surface definition 10
AFLR4    : Define CAD surface definition 11
AFLR4    : Define CAD surface definition 12
AFLR4    : Define CAD surface definition 13
AFLR4    : Define CAD surface definition 14
AFLR4    : Define CAD surface definition 15
AFLR4    : Define CAD surface definition 16
AFLR4    : Define CAD surface definition 17
AFLR4    : Define CAD surface definition 18
AFLR4    : Define CAD surface definition 19
AFLR4    : Define CAD surface definition 20
AFLR4    : Define CAD surface definition 21
AFLR4    : Define CAD surface definition 22
AFLR4    : Define CAD surface definition 23
AFLR4    : Define CAD surface definition 24
AFLR4    : Define CAD surface definition 25
AFLR4    : Define CAD surface definition 26
AFLR4    : Define CAD surface definition 27
AFLR4    : Define CAD surface definition 28
AFLR4    : Define CAD surface definition 29
AFLR4    : Define CAD surface definition 30
AFLR4    : Define CAD surface definition 31
AFLR4    : Define CAD surface definition 32
AFLR4    : Define CAD surface definition 33
AFLR4    : Define CAD surface definition 34
AFLR4    : Define CAD surface definition 35
AFLR4    : Define CAD surface definition 36
AFLR4    : Define CAD surface definition 37
AFLR4    : Define CAD surface definition 38
AFLR4    : Define CAD surface definition 39
AFLR4    : Define CAD surface definition 40
AFLR4    : Define CAD surface definition 41
AFLR4    : Define CAD surface definition 42
AFLR4    : Define CAD surface definition 43
AFLR4    : Define CAD surface definition 44
AFLR4    : Define CAD surface definition 45
AFLR4    : Define CAD surface definition 46
AFLR4    : Define CAD surface definition 47
AFLR4    : Define CAD surface definition 48
AFLR4    : Define CAD surface definition 49
AFLR4    : Define CAD surface definition 50
AFLR4    : Define CAD surface definition 51
AFLR4    : Define CAD surface definition 52
AFLR4    : Define CAD surface definition 53
AFLR4    : Define CAD surface definition 54
AFLR4    : Define CAD surface definition 55
AFLR4    : Define CAD surface definition 56
AFLR4    : Define CAD surface definition 57
AFLR4    : Define CAD surface definition 58
AFLR4    : Define CAD surface definition 59
AFLR4    : Define CAD surface definition 60
AFLR4    : Define CAD surface definition 61
AFLR4    : Define CAD surface definition 62
AFLR4    : Define CAD surface definition 63
AFLR4    : Define CAD surface definition 64
AFLR4    : Define CAD surface definition 65
AFLR4    : Define CAD surface definition 66
AFLR4    : Define CAD surface definition 67
AFLR4    : Define CAD surface definition 68
AFLR4    : Define CAD surface definition 69
AFLR4    : Define CAD surface definition 70
AFLR4    : Define CAD surface definition 71
AFLR4    : Define CAD surface definition 72
AFLR4    : Define CAD surface definition 73
AFLR4    : Define CAD surface definition 74
AFLR4    : Define CAD surface definition 75
AFLR4    : Define CAD surface definition 76
AFLR4    : Define CAD surface definition 77
AFLR4    : Define CAD surface definition 78
AFLR4    : Define CAD surface definition 79
AFLR4    : Define CAD surface definition 80
AFLR4    : Define CAD surface definition 81
AFLR4    : Define CAD surface definition 82
AFLR4    : Define CAD surface definition 83
AFLR4    : Define CAD surface definition 84
AFLR4    : Define CAD surface definition 85
AFLR4    : Define CAD surface definition 86
AFLR4    : Define CAD surface definition 87
AFLR4    : Define CAD surface definition 88
AFLR4    : Define CAD surface definition 89
AFLR4    : Define CAD surface definition 90
AFLR4    : Define CAD surface definition 91
AFLR4    : Define CAD surface definition 92
AFLR4    : Define CAD surface definition 93
AFLR4    : Define CAD surface definition 94
AFLR4    : Define CAD surface definition 95
AFLR4    : Define CAD surface definition 96
AFLR4    : Define CAD surface definition 97
AFLR4    : Define CAD surface definition 98
AFLR4    : Define CAD surface definition 99
AFLR4    : Define CAD surface definition 100
AFLR4    : Define CAD surface definition 101
AFLR4    : Define CAD surface definition 102
AFLR4    : Define CAD surface definition 103
AFLR4    : Define CAD surface definition 104
AFLR4    : Define CAD surface definition 105
AFLR4    : Define CAD surface definition 106
AFLR4    : Define CAD surface definition 107
AFLR4    : Define CAD surface definition 108
AFLR4    : Define CAD surface definition 109
AFLR4    : Define CAD surface definition 110
AFLR4    : Define CAD surface definition 111
AFLR4    : Define CAD surface definition 112
AFLR4    : Define CAD surface definition 113
AFLR4    : Define CAD surface definition 114
AFLR4    : Define CAD surface definition 115
AFLR4    : Define CAD surface definition 116
AFLR4    : Define CAD surface definition 117
AFLR4    : Define CAD surface definition 118
 
AFLR43   : INPUT SURFACE MESH FROM TESS
 
AFLR43   : Quad Surface Faces=         0
AFLR43   : Tria Surface Faces=    103698
AFLR43   : Nodes             =     51867
 
 
UG PARAM : SETTING INPUT PARAMETERS FROM ARGUMENT VECTOR
 
UG PARAM : mbl                         = 1         
UG PARAM : nbl                         = 5         
UG PARAM : mblelc                      = 2         
UG PARAM : mrecm                       = 3         
UG PARAM : mrecqm                      = 3         
UG PARAM : mbl                         = 1         
UG PARAM : mrecm                       = 3         
UG PARAM : mrecqm                      = 3         
UG PARAM : mblelc                      = 1         
UG PARAM : BC_IDs                  [ 0]= 1         
UG PARAM : BC_IDs                  [ 1]= 2         
UG PARAM : BC_IDs                  [ 2]= 3         
UG PARAM : BC_IDs                  [ 3]= 4         
UG PARAM : BC_IDs                  [ 4]= 5         
UG PARAM : BC_IDs                  [ 5]= 6         
UG PARAM : BC_IDs                  [ 6]= 7         
UG PARAM : BC_IDs                  [ 7]= 8         
UG PARAM : BC_IDs                  [ 8]= 9         
UG PARAM : BC_IDs                  [ 9]= 10        
UG PARAM : BC_IDs                  [10]= 11        
UG PARAM : BC_IDs                  [11]= 12        
UG PARAM : BC_IDs                  [12]= 13        
UG PARAM : BC_IDs                  [13]= 14        
UG PARAM : BC_IDs                  [14]= 15        
UG PARAM : BC_IDs                  [15]= 16        
UG PARAM : BC_IDs                  [16]= 17        
UG PARAM : BC_IDs                  [17]= 18        
UG PARAM : BC_IDs                  [18]= 19        
UG PARAM : BC_IDs                  [19]= 20        
UG PARAM : BC_IDs                  [20]= 21        
UG PARAM : BC_IDs                  [21]= 22        
UG PARAM : BC_IDs                  [22]= 23        
UG PARAM : BC_IDs                  [23]= 24        
UG PARAM : BC_IDs                  [24]= 25        
UG PARAM : BC_IDs                  [25]= 26        
UG PARAM : BC_IDs                  [26]= 27        
UG PARAM : BC_IDs                  [27]= 28        
UG PARAM : BC_IDs                  [28]= 29        
UG PARAM : BC_IDs                  [29]= 30        
UG PARAM : BC_IDs                  [30]= 31        
UG PARAM : BC_IDs                  [31]= 32        
UG PARAM : BC_IDs                  [32]= 33        
UG PARAM : BC_IDs                  [33]= 34        
UG PARAM : BC_IDs                  [34]= 35        
UG PARAM : BC_IDs                  [35]= 36        
UG PARAM : BC_IDs                  [36]= 37        
UG PARAM : BC_IDs                  [37]= 38        
UG PARAM : BC_IDs                  [38]= 39        
UG PARAM : BC_IDs                  [39]= 40        
UG PARAM : BC_IDs                  [40]= 41        
UG PARAM : BC_IDs                  [41]= 42        
UG PARAM : BC_IDs                  [42]= 43        
UG PARAM : BC_IDs                  [43]= 44        
UG PARAM : BC_IDs                  [44]= 45        
UG PARAM : BC_IDs                  [45]= 46        
UG PARAM : BC_IDs                  [46]= 47        
UG PARAM : BC_IDs                  [47]= 48        
UG PARAM : BC_IDs                  [48]= 49        
UG PARAM : BC_IDs                  [49]= 50        
UG PARAM : BC_IDs                  [50]= 51        
UG PARAM : BC_IDs                  [51]= 52        
UG PARAM : BC_IDs                  [52]= 53        
UG PARAM : BC_IDs                  [53]= 54        
UG PARAM : BC_IDs                  [54]= 55        
UG PARAM : BC_IDs                  [55]= 56        
UG PARAM : BC_IDs                  [56]= 57        
UG PARAM : BC_IDs                  [57]= 58        
UG PARAM : BC_IDs                  [58]= 59        
UG PARAM : BC_IDs                  [59]= 60        
UG PARAM : BC_IDs                  [60]= 61        
UG PARAM : BC_IDs                  [61]= 62        
UG PARAM : BC_IDs                  [62]= 63        
UG PARAM : BC_IDs                  [63]= 64        
UG PARAM : BC_IDs                  [64]= 65        
UG PARAM : BC_IDs                  [65]= 66        
UG PARAM : BC_IDs                  [66]= 67        
UG PARAM : BC_IDs                  [67]= 68        
UG PARAM : BC_IDs                  [68]= 69        
UG PARAM : BC_IDs                  [69]= 70        
UG PARAM : BC_IDs                  [70]= 71        
UG PARAM : BC_IDs                  [71]= 72        
UG PARAM : BC_IDs                  [72]= 73        
UG PARAM : BC_IDs                  [73]= 74        
UG PARAM : BC_IDs                  [74]= 75        
UG PARAM : BC_IDs                  [75]= 76        
UG PARAM : BC_IDs                  [76]= 77        
UG PARAM : BC_IDs                  [77]= 78        
UG PARAM : BC_IDs                  [78]= 79        
UG PARAM : BC_IDs                  [79]= 80        
UG PARAM : BC_IDs                  [80]= 81        
UG PARAM : BC_IDs                  [81]= 82        
UG PARAM : BC_IDs                  [82]= 83        
UG PARAM : BC_IDs                  [83]= 84        
UG PARAM : BC_IDs                  [84]= 85        
UG PARAM : BC_IDs                  [85]= 86        
UG PARAM : BC_IDs                  [86]= 87        
UG PARAM : BC_IDs                  [87]= 88        
UG PARAM : BC_IDs                  [88]= 89        
UG PARAM : BC_IDs                  [89]= 90        
UG PARAM : BC_IDs                  [90]= 91        
UG PARAM : BC_IDs                  [91]= 92        
UG PARAM : BC_IDs                  [92]= 93        
UG PARAM : BC_IDs                  [93]= 94        
UG PARAM : BC_IDs                  [94]= 95        
UG PARAM : BC_IDs                  [95]= 96        
UG PARAM : BC_IDs                  [96]= 97        
UG PARAM : BC_IDs                  [97]= 98        
UG PARAM : BC_IDs                  [98]= 99        
UG PARAM : BC_IDs                  [99]= 100       
UG PARAM : BC_IDs                  [117]= 118       
UG PARAM : BL_DS                   [ 0]= 0.434102  
UG PARAM : BL_DS                   [ 1]= 0.434102  
UG PARAM : BL_DS                   [ 2]= 0.434102  
UG PARAM : BL_DS                   [ 3]= 0.434102  
UG PARAM : BL_DS                   [ 4]= 0.434102  
UG PARAM : BL_DS                   [ 5]= 0.434102  
UG PARAM : BL_DS                   [ 6]= 0.434102  
UG PARAM : BL_DS                   [ 7]= 0.434102  
UG PARAM : BL_DS                   [ 8]= 0.434102  
UG PARAM : BL_DS                   [ 9]= 0.434102  
UG PARAM : BL_DS                   [10]= 0.434102  
UG PARAM : BL_DS                   [11]= 0.434102  
UG PARAM : BL_DS                   [12]= 0.434102  
UG PARAM : BL_DS                   [13]= 0.434102  
UG PARAM : BL_DS                   [14]= 0.434102  
UG PARAM : BL_DS                   [15]= 0.434102  
UG PARAM : BL_DS                   [16]= 0.434102  
UG PARAM : BL_DS                   [17]= 0.434102  
UG PARAM : BL_DS                   [18]= 0.434102  
UG PARAM : BL_DS                   [19]= 0.434102  
UG PARAM : BL_DS                   [20]= 0.434102  
UG PARAM : BL_DS                   [21]= 0.434102  
UG PARAM : BL_DS                   [22]= 0.434102  
UG PARAM : BL_DS                   [23]= 0.434102  
UG PARAM : BL_DS                   [24]= 0.434102  
UG PARAM : BL_DS                   [25]= 0.434102  
UG PARAM : BL_DS                   [26]= 0.434102  
UG PARAM : BL_DS                   [27]= 0.434102  
UG PARAM : BL_DS                   [28]= 0.434102  
UG PARAM : BL_DS                   [29]= 0.434102  
UG PARAM : BL_DS                   [30]= 0.434102  
UG PARAM : BL_DS                   [31]= 0.434102  
UG PARAM : BL_DS                   [32]= 0.434102  
UG PARAM : BL_DS                   [33]= 0.434102  
UG PARAM : BL_DS                   [34]= 0.434102  
UG PARAM : BL_DS                   [35]= 0.434102  
UG PARAM : BL_DS                   [36]= 0.434102  
UG PARAM : BL_DS                   [37]= 0.434102  
UG PARAM : BL_DS                   [38]= 0.434102  
UG PARAM : BL_DS                   [39]= 0.434102  
UG PARAM : BL_DS                   [40]= 0.434102  
UG PARAM : BL_DS                   [41]= 0.434102  
UG PARAM : BL_DS                   [42]= 0.434102  
UG PARAM : BL_DS                   [43]= 0.434102  
UG PARAM : BL_DS                   [44]= 0.434102  
UG PARAM : BL_DS                   [45]= 0.434102  
UG PARAM : BL_DS                   [46]= 0.434102  
UG PARAM : BL_DS                   [47]= 0.434102  
UG PARAM : BL_DS                   [48]= 0.434102  
UG PARAM : BL_DS                   [49]= 0.434102  
UG PARAM : BL_DS                   [50]= 0.434102  
UG PARAM : BL_DS                   [51]= 0.434102  
UG PARAM : BL_DS                   [52]= 0.434102  
UG PARAM : BL_DS                   [53]= 0.434102  
UG PARAM : BL_DS                   [54]= 0.434102  
UG PARAM : BL_DS                   [55]= 0.434102  
UG PARAM : BL_DS                   [56]= 0.434102  
UG PARAM : BL_DS                   [57]= 0.434102  
UG PARAM : BL_DS                   [58]= 0.434102  
UG PARAM : BL_DS                   [59]= 0.434102  
UG PARAM : BL_DS                   [60]= 0.434102  
UG PARAM : BL_DS                   [61]= 0.434102  
UG PARAM : BL_DS                   [62]= 0.434102  
UG PARAM : BL_DS                   [63]= 0.434102  
UG PARAM : BL_DS                   [64]= 0.434102  
UG PARAM : BL_DS                   [65]= 0.434102  
UG PARAM : BL_DS                   [66]= 0.434102  
UG PARAM : BL_DS                   [67]= 0.434102  
UG PARAM : BL_DS                   [68]= 0.217051  
UG PARAM : BL_DS                   [69]= 0.217051  
UG PARAM : BL_DS                   [70]= 0.217051  
UG PARAM : BL_DS                   [71]= 0.434102  
UG PARAM : BL_DS                   [72]= 0.434102  
UG PARAM : BL_DS                   [73]= 0.217051  
UG PARAM : BL_DS                   [74]= 0.217051  
UG PARAM : BL_DS                   [75]= 0.217051  
UG PARAM : BL_DS                   [76]= 0.434102  
UG PARAM : BL_DS                   [77]= 0.434102  
UG PARAM : BL_DS                   [78]= 0.217051  
UG PARAM : BL_DS                   [79]= 0.217051  
UG PARAM : BL_DS                   [80]= 0.217051  
UG PARAM : BL_DS                   [81]= 0.434102  
UG PARAM : BL_DS                   [82]= 0.434102  
UG PARAM : BL_DS                   [83]= 0.434102  
UG PARAM : BL_DS                   [84]= 0.217051  
UG PARAM : BL_DS                   [85]= 0.217051  
UG PARAM : BL_DS                   [86]= 0.217051  
UG PARAM : BL_DS                   [87]= 0.434102  
UG PARAM : BL_DS                   [88]= 0.434102  
UG PARAM : BL_DS                   [89]= 0.217051  
UG PARAM : BL_DS                   [90]= 0.217051  
UG PARAM : BL_DS                   [91]= 0.217051  
UG PARAM : BL_DS                   [92]= 0.434102  
UG PARAM : BL_DS                   [93]= 0.217051  
UG PARAM : BL_DS                   [94]= 0.217051  
UG PARAM : BL_DS                   [95]= 0.217051  
UG PARAM : BL_DS                   [96]= 0.434102  
UG PARAM : BL_DS                   [97]= 0.434102  
UG PARAM : BL_DS                   [98]= 0.434102  
UG PARAM : BL_DS                   [99]= 0.217051  
UG PARAM : BL_DS                   [117]= 0         
UG PARAM : BL_DEL                  [ 0]= 2.17051   
UG PARAM : BL_DEL                  [ 1]= 2.17051   
UG PARAM : BL_DEL                  [ 2]= 2.17051   
UG PARAM : BL_DEL                  [ 3]= 2.17051   
UG PARAM : BL_DEL                  [ 4]= 2.17051   
UG PARAM : BL_DEL                  [ 5]= 2.17051   
UG PARAM : BL_DEL                  [ 6]= 2.17051   
UG PARAM : BL_DEL                  [ 7]= 2.17051   
UG PARAM : BL_DEL                  [ 8]= 2.17051   
UG PARAM : BL_DEL                  [ 9]= 2.17051   
UG PARAM : BL_DEL                  [10]= 2.17051   
UG PARAM : BL_DEL                  [11]= 2.17051   
UG PARAM : BL_DEL                  [12]= 2.17051   
UG PARAM : BL_DEL                  [13]= 2.17051   
UG PARAM : BL_DEL                  [14]= 2.17051   
UG PARAM : BL_DEL                  [15]= 2.17051   
UG PARAM : BL_DEL                  [16]= 2.17051   
UG PARAM : BL_DEL                  [17]= 2.17051   
UG PARAM : BL_DEL                  [18]= 2.17051   
UG PARAM : BL_DEL                  [19]= 2.17051   
UG PARAM : BL_DEL                  [20]= 2.17051   
UG PARAM : BL_DEL                  [21]= 2.17051   
UG PARAM : BL_DEL                  [22]= 2.17051   
UG PARAM : BL_DEL                  [23]= 2.17051   
UG PARAM : BL_DEL                  [24]= 2.17051   
UG PARAM : BL_DEL                  [25]= 2.17051   
UG PARAM : BL_DEL                  [26]= 2.17051   
UG PARAM : BL_DEL                  [27]= 2.17051   
UG PARAM : BL_DEL                  [28]= 2.17051   
UG PARAM : BL_DEL                  [29]= 2.17051   
UG PARAM : BL_DEL                  [30]= 2.17051   
UG PARAM : BL_DEL                  [31]= 2.17051   
UG PARAM : BL_DEL                  [32]= 2.17051   
UG PARAM : BL_DEL                  [33]= 2.17051   
UG PARAM : BL_DEL                  [34]= 2.17051   
UG PARAM : BL_DEL                  [35]= 2.17051   
UG PARAM : BL_DEL                  [36]= 2.17051   
UG PARAM : BL_DEL                  [37]= 2.17051   
UG PARAM : BL_DEL                  [38]= 2.17051   
UG PARAM : BL_DEL                  [39]= 2.17051   
UG PARAM : BL_DEL                  [40]= 2.17051   
UG PARAM : BL_DEL                  [41]= 2.17051   
UG PARAM : BL_DEL                  [42]= 2.17051   
UG PARAM : BL_DEL                  [43]= 2.17051   
UG PARAM : BL_DEL                  [44]= 2.17051   
UG PARAM : BL_DEL                  [45]= 2.17051   
UG PARAM : BL_DEL                  [46]= 2.17051   
UG PARAM : BL_DEL                  [47]= 2.17051   
UG PARAM : BL_DEL                  [48]= 2.17051   
UG PARAM : BL_DEL                  [49]= 2.17051   
UG PARAM : BL_DEL                  [50]= 2.17051   
UG PARAM : BL_DEL                  [51]= 2.17051   
UG PARAM : BL_DEL                  [52]= 2.17051   
UG PARAM : BL_DEL                  [53]= 2.17051   
UG PARAM : BL_DEL                  [54]= 2.17051   
UG PARAM : BL_DEL                  [55]= 2.17051   
UG PARAM : BL_DEL                  [56]= 2.17051   
UG PARAM : BL_DEL                  [57]= 2.17051   
UG PARAM : BL_DEL                  [58]= 2.17051   
UG PARAM : BL_DEL                  [59]= 2.17051   
UG PARAM : BL_DEL                  [60]= 2.17051   
UG PARAM : BL_DEL                  [61]= 2.17051   
UG PARAM : BL_DEL                  [62]= 2.17051   
UG PARAM : BL_DEL                  [63]= 2.17051   
UG PARAM : BL_DEL                  [64]= 2.17051   
UG PARAM : BL_DEL                  [65]= 2.17051   
UG PARAM : BL_DEL                  [66]= 2.17051   
UG PARAM : BL_DEL                  [67]= 2.17051   
UG PARAM : BL_DEL                  [68]= 2.17051   
UG PARAM : BL_DEL                  [69]= 2.17051   
UG PARAM : BL_DEL                  [70]= 2.17051   
UG PARAM : BL_DEL                  [71]= 2.17051   
UG PARAM : BL_DEL                  [72]= 2.17051   
UG PARAM : BL_DEL                  [73]= 2.17051   
UG PARAM : BL_DEL                  [74]= 2.17051   
UG PARAM : BL_DEL                  [75]= 2.17051   
UG PARAM : BL_DEL                  [76]= 2.17051   
UG PARAM : BL_DEL                  [77]= 2.17051   
UG PARAM : BL_DEL                  [78]= 2.17051   
UG PARAM : BL_DEL                  [79]= 2.17051   
UG PARAM : BL_DEL                  [80]= 2.17051   
UG PARAM : BL_DEL                  [81]= 2.17051   
UG PARAM : BL_DEL                  [82]= 2.17051   
UG PARAM : BL_DEL                  [83]= 2.17051   
UG PARAM : BL_DEL                  [84]= 2.17051   
UG PARAM : BL_DEL                  [85]= 2.17051   
UG PARAM : BL_DEL                  [86]= 2.17051   
UG PARAM : BL_DEL                  [87]= 2.17051   
UG PARAM : BL_DEL                  [88]= 2.17051   
UG PARAM : BL_DEL                  [89]= 2.17051   
UG PARAM : BL_DEL                  [90]= 2.17051   
UG PARAM : BL_DEL                  [91]= 2.17051   
UG PARAM : BL_DEL                  [92]= 2.17051   
UG PARAM : BL_DEL                  [93]= 2.17051   
UG PARAM : BL_DEL                  [94]= 2.17051   
UG PARAM : BL_DEL                  [95]= 2.17051   
UG PARAM : BL_DEL                  [96]= 2.17051   
UG PARAM : BL_DEL                  [97]= 2.17051   
UG PARAM : BL_DEL                  [98]= 2.17051   
UG PARAM : BL_DEL                  [99]= 2.17051   
UG PARAM : BL_DEL                  [117]= 0         
UG PARAM : mpfrmt                      = 0         
 
AFLR3    : ---------------------------------------
AFLR3    : AFLR3 LIBRARY
AFLR3    : ADVANCING-FRONT/LOCAL-RECONNECTION
AFLR3    : TETRAHEDRAL GRID GENERATOR
AFLR3    : Version Number 16.32.50
AFLR3    : Version Date   10/31/23 @ 06:31PM
AFLR3    : Compile OS     Darwin 23.3.0 arm64
AFLR3    : Compile Date   02/08/24 @ 04:22PM
AFLR3    : Copyright 1994-2021, D.L. Marcum
AFLR3    : ---------------------------------------
 
AFLR3 IC : INPUT SURFACE GRID CHECK
 
AFLR3 IC : Nodes, Elements   =     51867         0

UG3      : Boundary Conditions

UG3      :  B-Face ID            Boundary Condition
UG3      :          1                    Solid w/BL
UG3      :          2                    Solid w/BL
UG3      :          3                    Solid w/BL
UG3      :          4                    Solid w/BL
UG3      :          5                    Solid w/BL
UG3      :          6                    Solid w/BL
UG3      :          7                    Solid w/BL
UG3      :          8                    Solid w/BL
UG3      :          9                    Solid w/BL
UG3      :         10                    Solid w/BL
UG3      :         11                    Solid w/BL
UG3      :         12                    Solid w/BL
UG3      :         13                    Solid w/BL
UG3      :         14                    Solid w/BL
UG3      :         15                    Solid w/BL
UG3      :         16                    Solid w/BL
UG3      :         17                    Solid w/BL
UG3      :         18                    Solid w/BL
UG3      :         19                    Solid w/BL
UG3      :         20                    Solid w/BL
UG3      :         21                    Solid w/BL
UG3      :         22                    Solid w/BL
UG3      :         23                    Solid w/BL
UG3      :         24                    Solid w/BL
UG3      :         25                    Solid w/BL
UG3      :         26                    Solid w/BL
UG3      :         27                    Solid w/BL
UG3      :         28                    Solid w/BL
UG3      :         29                    Solid w/BL
UG3      :         30                    Solid w/BL
UG3      :         31                    Solid w/BL
UG3      :         32                    Solid w/BL
UG3      :         33                    Solid w/BL
UG3      :         34                    Solid w/BL
UG3      :         35                    Solid w/BL
UG3      :         36                    Solid w/BL
UG3      :         37                    Solid w/BL
UG3      :         38                    Solid w/BL
UG3      :         39                    Solid w/BL
UG3      :         40                    Solid w/BL
UG3      :         41                    Solid w/BL
UG3      :         42                    Solid w/BL
UG3      :         43                    Solid w/BL
UG3      :         44                    Solid w/BL
UG3      :         45                    Solid w/BL
UG3      :         46                    Solid w/BL
UG3      :         47                    Solid w/BL
UG3      :         48                    Solid w/BL
UG3      :         49                    Solid w/BL
UG3      :         50                    Solid w/BL
UG3      :         51                    Solid w/BL
UG3      :         52                    Solid w/BL
UG3      :         53                    Solid w/BL
UG3      :         54                    Solid w/BL
UG3      :         55                    Solid w/BL
UG3      :         56                    Solid w/BL
UG3      :         57                    Solid w/BL
UG3      :         58                    Solid w/BL
UG3      :         59                    Solid w/BL
UG3      :         60                    Solid w/BL
UG3      :         61                    Solid w/BL
UG3      :         62                    Solid w/BL
UG3      :         63                    Solid w/BL
UG3      :         64                    Solid w/BL
UG3      :         65                    Solid w/BL
UG3      :         66                    Solid w/BL
UG3      :         67                    Solid w/BL
UG3      :         68                    Solid w/BL
UG3      :         69                    Solid w/BL
UG3      :         70                    Solid w/BL
UG3      :         71                    Solid w/BL
UG3      :         72                    Solid w/BL
UG3      :         73                    Solid w/BL
UG3      :         74                    Solid w/BL
UG3      :         75                    Solid w/BL
UG3      :         76                    Solid w/BL
UG3      :         77                    Solid w/BL
UG3      :         78                    Solid w/BL
UG3      :         79                    Solid w/BL
UG3      :         80                    Solid w/BL
UG3      :         81                    Solid w/BL
UG3      :         82                    Solid w/BL
UG3      :         83                    Solid w/BL
UG3      :         84                    Solid w/BL
UG3      :         85                    Solid w/BL
UG3      :         86                    Solid w/BL
UG3      :         87                    Solid w/BL
UG3      :         88                    Solid w/BL
UG3      :         89                    Solid w/BL
UG3      :         90                    Solid w/BL
UG3      :         91                    Solid w/BL
UG3      :         92                    Solid w/BL
UG3      :         93                    Solid w/BL
UG3      :         94                    Solid w/BL
UG3      :         95                    Solid w/BL
UG3      :         96                    Solid w/BL
UG3      :         97                    Solid w/BL
UG3      :         98                    Solid w/BL
UG3      :         99                    Solid w/BL
UG3      :        100                    Solid w/BL
UG3      :        101                    Solid w/BL
UG3      :        102                    Solid w/BL
UG3      :        103                    Solid w/BL
UG3      :        104                    Solid w/BL
UG3      :        105                    Solid w/BL
UG3      :        106                    Solid w/BL
UG3      :        107                    Solid w/BL
UG3      :        108                    Solid w/BL
UG3      :        109                    Solid w/BL
UG3      :        110                    Solid w/BL
UG3      :        111                    Solid w/BL
UG3      :        112                    Solid w/BL
UG3      :        113                      FarField
UG3      :        114                      FarField
UG3      :        115                      FarField
UG3      :        116                      FarField
UG3      :        117                      FarField
UG3      :        118                      FarField
 
AFLR3    : CPU Time          =     0.062   seconds
 
AFLR3    : DONE
 
ANBL3    : ---------------------------------------
ANBL3    : ANBL3 LIBRARY
ANBL3    : ADVANCING-NORMAL
ANBL3    : BOUNDARY-LAYER (BL)
ANBL3    : STRUCTURED-LAYER (SL)
ANBL3    : SPECIFIED NORMAL SPACING (SNS)
ANBL3    : TETRAHEDRAL/PENTAHEDRAL GRID GENERATOR
ANBL3    : Version Number 9.34.2
ANBL3    : Version Date   03/10/23 @ 04:32PM
ANBL3    : Compile OS     Darwin 23.3.0 arm64
ANBL3    : Compile Date   02/08/24 @ 04:22PM
ANBL3    : Copyright 1994-2021, D.L. Marcum
ANBL3    : ---------------------------------------
 
ANBL3 BLC: BL BOUNDARY CONDITIONS CHECK
 
ANBL3 BLC: Nodes, Elements   =     51867         0
 
ANBL3    : CPU Time          =     0.051   seconds
 
ANBL3    : DONE
 
ANBL3 BLG: BL NODE GENERATION
 
ANBL3 BLG: Nodes, Layer      =         0         0
ANBL3 BLG: Nodes, Layer      =    101707         2
ANBL3 BLG: Nodes, Layer      =    148358         3
ANBL3 BLG: Nodes, Layer      =    189573         4
ANBL3 BLG: Nodes, Layer      =    225956         5
ANBL3 BLG: Nodes, Layer      =    257468         6
 
ANBL3    : CPU Time          =    19.932   seconds
 
ANBL3    : DONE
 
AFLR3 IC : INPUT SURFACE GRID CHECK
 
AFLR3 IC : Nodes, Elements   =     51867         0
 
AFLR3    : CPU Time          =     0.033   seconds
 
AFLR3 IG : INITIAL VOLUME GRID GENERATION
 
AFLR3 IG : Nodes, Elements   =     51867         0
AFLR3 IG : Nodes, Elements   =         8        10
AFLR3 IG : Nodes, Elements   =     10374     68606
AFLR3 IG : Nodes, Elements   =     20748    137036
AFLR3 IG : Nodes, Elements   =     31122    202936
AFLR3 IG : Nodes, Elements   =     41496    265778
AFLR3 IG : Nodes, Elements   =     51870    338482
AFLR3 IG : Nodes, Elements   =     51874    338515
AFLR3 IG : Nodes, Elements   =     51874    337441
AFLR3 IG : Nodes, Elements   =     51874    340152
AFLR3 IG : Nodes, Elements   =     51874    335996
AFLR3 IG : Nodes, Elements   =     51874    335947
AFLR3 IG : Nodes, Elements   =     51874    337016
AFLR3 IG : Nodes, Elements   =     51874    336965
AFLR3 IG : Nodes, Elements   =     51874    333692
AFLR3 IG : Nodes, Elements   =     51874    333694
AFLR3 IG : Nodes, Elements   =     51874    333692
AFLR3 IG : Nodes, Elements   =     51874    334677
AFLR3 IG : Nodes, Elements   =     51874    333721
AFLR3 IG : Nodes, Elements   =     51874    333723
AFLR3 IG : Nodes, Elements   =     51874    333721
AFLR3 IG : Nodes, Elements   =     51874    334472
AFLR3 IG : Nodes, Elements   =     51874    334436
AFLR3 IG : Nodes, Elements   =     51874    332919
AFLR3 IG : Nodes, Elements   =     51874    332916
AFLR3 IG : Nodes, Elements   =     51874    333740
AFLR3 IG : Nodes, Elements   =     51874    332969
AFLR3 IG : Nodes, Elements   =     51874    332968
AFLR3 IG : Nodes, Elements   =     51874    333584
AFLR3 IG : Nodes, Elements   =     51874    333550
AFLR3 IG : Nodes, Elements   =     51874    332766
AFLR3 IG : Nodes, Elements   =     51874    333470
AFLR3 IG : Nodes, Elements   =     51874    332807
AFLR3 IG : Nodes, Elements   =     51874    333365
AFLR3 IG : Nodes, Elements   =     51874    333337
AFLR3 IG : Nodes, Elements   =     51874    332668
AFLR3 IG : Nodes, Elements   =     51874    332669
AFLR3 IG : Nodes, Elements   =     51874    333348
AFLR3 IG : Nodes, Elements   =     51874    332734
AFLR3 IG : Nodes, Elements   =     51874    333261
AFLR3 IG : Nodes, Elements   =     51874    333232
AFLR3 IG : Nodes, Elements   =     51874    332662
AFLR3 IG : Nodes, Elements   =     51874    333278
AFLR3 IG : Nodes, Elements   =     51874    332721
AFLR3 IG : Nodes, Elements   =     51874    333220
AFLR3 IG : Nodes, Elements   =     51874    333191
AFLR3 IG : Nodes, Elements   =     51874    332661
AFLR3 IG : Nodes, Elements   =     51874    333258
AFLR3 IG : Nodes, Elements   =     51874    332708
AFLR3 IG : Nodes, Elements   =     51874    333183
AFLR3 IG : Nodes, Elements   =     51874    333154
AFLR3 IG : Nodes, Elements   =     51874    332643
AFLR3 IG : Nodes, Elements   =     51874    332644
AFLR3 IG : Nodes, Elements   =     51874    332643
AFLR3 IG : Nodes, Elements   =     51874    333329
AFLR3 IG : Nodes, Elements   =     51874    332676
AFLR3 IG : Nodes, Elements   =     51874    332678
AFLR3 IG : Nodes, Elements   =     51874    332677
AFLR3 IG : Nodes, Elements   =     51874    332876
AFLR3 IG : Nodes, Elements   =     51874    332868
AFLR3 IG : Nodes, Elements   =     51874    332597
AFLR3 IG : Nodes, Elements   =     51874    332598
AFLR3 IG : Nodes, Elements   =     51874    332826
AFLR3 IG : Nodes, Elements   =     51874    332614
AFLR3 IG : Nodes, Elements   =     51874    332615
AFLR3 IG : Nodes, Elements   =     51874    332614
AFLR3 IG : Nodes, Elements   =     51874    332790
AFLR3 IG : Nodes, Elements   =     51874    332784
AFLR3 IG : Nodes, Elements   =     51874    332604
AFLR3 IG : Nodes, Elements   =     51874    332603
AFLR3 IG : Nodes, Elements   =     51874    332767
AFLR3 IG : Nodes, Elements   =     51874    332615
AFLR3 IG : Nodes, Elements   =     51874    332771
AFLR3 IG : Nodes, Elements   =     51874    332761
AFLR3 IG : Nodes, Elements   =     51874    332599
AFLR3 IG : Nodes, Elements   =     51874    332945
AFLR3 IG : Nodes, Elements   =     51874    332645
AFLR3 IG : Nodes, Elements   =     51874    332726
AFLR3 IG : Nodes, Elements   =     51874    332723
AFLR3 IG : Nodes, Elements   =     51874    332620
AFLR3 IG : Nodes, Elements   =     51874    332745
AFLR3 IG : Nodes, Elements   =     51874    332644
AFLR3 IG : Nodes, Elements   =     51874    332740
AFLR3 IG : Nodes, Elements   =     51874    332737
AFLR3 IG : Nodes, Elements   =     51874    332630
AFLR3 IG : Nodes, Elements   =     51867    178633
AFLR3 IG : Nodes, Elements   =     51867    182441
AFLR3 IG : Nodes, Elements   =     51867    165529
AFLR3 IG : Nodes, Elements   =     51867    162407
 
AFLR3    : CPU Time          =     5.242   seconds
 
AFLR3 GG : ISOTROPIC VOLUME GRID GENERATION
 
AFLR3 GG : Nodes, Elements   =     51867    162407
AFLR3 GGi: Nodes, Elements   =     51871    162419
AFLR3 GGi: Nodes, Elements   =     51871    162494
AFLR3 GGi: Nodes, Elements   =     51871    162339
AFLR3 GGi: Nodes, Elements   =     51871    162292
AFLR3 GGi: Nodes, Elements   =     51873    162298
AFLR3 GGi: Nodes, Elements   =     51873    162328
AFLR3 GGi: Nodes, Elements   =     51873    162265
AFLR3 GGi: Nodes, Elements   =     51873    162247
AFLR3 GGi: Nodes, Elements   =     51875    162253
AFLR3 GGi: Nodes, Elements   =     51875    162280
AFLR3 GGi: Nodes, Elements   =     51875    162200
AFLR3 GGi: Nodes, Elements   =     51875    162164
AFLR3 GGi: Nodes, Elements   =     51876    162167
AFLR3 GGi: Nodes, Elements   =     51876    162242
AFLR3 GGi: Nodes, Elements   =     51876    162183
AFLR3 GGi: Nodes, Elements   =     51876    162169
AFLR3 GG : Nodes, Elements   =     64933    201458
AFLR3 GG : Nodes, Elements   =     64933    248399
AFLR3 GG : Nodes, Elements   =     64933    233752
AFLR3 GG : Nodes, Elements   =     64933    231496
AFLR3 GG : Nodes, Elements   =     76647    266789
AFLR3 GG : Nodes, Elements   =     76647    317908
AFLR3 GG : Nodes, Elements   =     76647    303156
AFLR3 GG : Nodes, Elements   =     76647    301137
AFLR3 GG : Nodes, Elements   =     88416    336606
AFLR3 GG : Nodes, Elements   =     88416    387427
AFLR3 GG : Nodes, Elements   =     88416    374184
AFLR3 GG : Nodes, Elements   =     88416    372071
AFLR3 GG : Nodes, Elements   =     99519    405523
AFLR3 GG : Nodes, Elements   =     99519    452972
AFLR3 GG : Nodes, Elements   =     99519    440500
AFLR3 GG : Nodes, Elements   =     99519    438473
AFLR3 GG : Nodes, Elements   =    109943    469883
AFLR3 GG : Nodes, Elements   =    109943    514143
AFLR3 GG : Nodes, Elements   =    109943    502448
AFLR3 GG : Nodes, Elements   =    109943    500453
AFLR3 GG : Nodes, Elements   =    119766    530016
AFLR3 GG : Nodes, Elements   =    119766    571724
AFLR3 GG : Nodes, Elements   =    119766    561057
AFLR3 GG : Nodes, Elements   =    119766    559363
AFLR3 GG : Nodes, Elements   =    128922    586936
AFLR3 GG : Nodes, Elements   =    128922    625858
AFLR3 GG : Nodes, Elements   =    128922    615706
AFLR3 GG : Nodes, Elements   =    128922    614036
AFLR3 GG : Nodes, Elements   =    137522    639933
AFLR3 GG : Nodes, Elements   =    137522    676057
AFLR3 GG : Nodes, Elements   =    137522    666758
AFLR3 GG : Nodes, Elements   =    137522    665273
AFLR3 GG : Nodes, Elements   =    145622    689682
AFLR3 GG : Nodes, Elements   =    145622    723723
AFLR3 GG : Nodes, Elements   =    145622    714945
AFLR3 GG : Nodes, Elements   =    145622    713516
AFLR3 GG : Nodes, Elements   =    153327    736719
AFLR3 GG : Nodes, Elements   =    153327    769583
AFLR3 GG : Nodes, Elements   =    153327    760946
AFLR3 GG : Nodes, Elements   =    153327    759517
AFLR3 GG : Nodes, Elements   =    160529    781203
AFLR3 GG : Nodes, Elements   =    160529    811630
AFLR3 GG : Nodes, Elements   =    160529    803739
AFLR3 GG : Nodes, Elements   =    160529    802379
AFLR3 GG : Nodes, Elements   =    167386    823028
AFLR3 GG : Nodes, Elements   =    167386    852013
AFLR3 GG : Nodes, Elements   =    167386    844440
AFLR3 GG : Nodes, Elements   =    167386    843151
AFLR3 GG : Nodes, Elements   =    173897    862762
AFLR3 GG : Nodes, Elements   =    173897    890329
AFLR3 GG : Nodes, Elements   =    173897    883219
AFLR3 GG : Nodes, Elements   =    173897    882011
AFLR3 GG : Nodes, Elements   =    180221    901078
AFLR3 GG : Nodes, Elements   =    180221    927570
AFLR3 GG : Nodes, Elements   =    180221    920737
AFLR3 GG : Nodes, Elements   =    180221    919628
AFLR3 GG : Nodes, Elements   =    186176    937548
AFLR3 GG : Nodes, Elements   =    186176    962834
AFLR3 GG : Nodes, Elements   =    186176    956280
AFLR3 GG : Nodes, Elements   =    186176    955184
AFLR3 GG : Nodes, Elements   =    191911    972448
AFLR3 GG : Nodes, Elements   =    191911    996696
AFLR3 GG : Nodes, Elements   =    191911    990431
AFLR3 GG : Nodes, Elements   =    191911    989340
AFLR3 GG : Nodes, Elements   =    197410   1005887
AFLR3 GG : Nodes, Elements   =    197410   1029009
AFLR3 GG : Nodes, Elements   =    197410   1023149
AFLR3 GG : Nodes, Elements   =    197410   1022123
AFLR3 GG : Nodes, Elements   =    202696   1038035
AFLR3 GG : Nodes, Elements   =    202696   1060252
AFLR3 GG : Nodes, Elements   =    202696   1054630
AFLR3 GG : Nodes, Elements   =    202696   1053670
AFLR3 GG : Nodes, Elements   =    207773   1068947
AFLR3 GG : Nodes, Elements   =    207773   1090317
AFLR3 GG : Nodes, Elements   =    207773   1084888
AFLR3 GG : Nodes, Elements   =    207773   1083937
AFLR3 GG : Nodes, Elements   =    212719   1098813
AFLR3 GG : Nodes, Elements   =    212719   1119613
AFLR3 GG : Nodes, Elements   =    212719   1114328
AFLR3 GG : Nodes, Elements   =    212719   1113481
AFLR3 GG : Nodes, Elements   =    217443   1127697
AFLR3 GG : Nodes, Elements   =    217443   1147712
AFLR3 GG : Nodes, Elements   =    217443   1142490
AFLR3 GG : Nodes, Elements   =    217443   1141618
AFLR3 GG : Nodes, Elements   =    221919   1155082
AFLR3 GG : Nodes, Elements   =    221919   1174247
AFLR3 GG : Nodes, Elements   =    221919   1169266
AFLR3 GG : Nodes, Elements   =    221919   1168450
AFLR3 GG : Nodes, Elements   =    226226   1181405
AFLR3 GG : Nodes, Elements   =    226226   1199437
AFLR3 GG : Nodes, Elements   =    226226   1194892
AFLR3 GG : Nodes, Elements   =    226226   1194140
AFLR3 GG : Nodes, Elements   =    230276   1206311
AFLR3 GG : Nodes, Elements   =    230276   1223527
AFLR3 GG : Nodes, Elements   =    230276   1219098
AFLR3 GG : Nodes, Elements   =    230276   1218341
AFLR3 GG : Nodes, Elements   =    234179   1230076
AFLR3 GG : Nodes, Elements   =    234179   1246369
AFLR3 GG : Nodes, Elements   =    234179   1242304
AFLR3 GG : Nodes, Elements   =    234179   1241633
AFLR3 GG : Nodes, Elements   =    237883   1252771
AFLR3 GG : Nodes, Elements   =    237883   1268485
AFLR3 GG : Nodes, Elements   =    237883   1264428
AFLR3 GG : Nodes, Elements   =    237883   1263788
AFLR3 GG : Nodes, Elements   =    241323   1274120
AFLR3 GG : Nodes, Elements   =    241323   1288541
AFLR3 GG : Nodes, Elements   =    241323   1284890
AFLR3 GG : Nodes, Elements   =    241323   1284351
AFLR3 GG : Nodes, Elements   =    244594   1294181
AFLR3 GG : Nodes, Elements   =    244594   1307909
AFLR3 GG : Nodes, Elements   =    244594   1304529
AFLR3 GG : Nodes, Elements   =    244594   1303991
AFLR3 GG : Nodes, Elements   =    247653   1313179
AFLR3 GG : Nodes, Elements   =    247653   1326023
AFLR3 GG : Nodes, Elements   =    247653   1322762
AFLR3 GG : Nodes, Elements   =    247653   1322235
AFLR3 GG : Nodes, Elements   =    250573   1331006
AFLR3 GG : Nodes, Elements   =    250573   1343063
AFLR3 GG : Nodes, Elements   =    250573   1340117
AFLR3 GG : Nodes, Elements   =    250573   1339650
AFLR3 GG : Nodes, Elements   =    253250   1347691
AFLR3 GG : Nodes, Elements   =    253250   1358890
AFLR3 GG : Nodes, Elements   =    253250   1356104
AFLR3 GG : Nodes, Elements   =    253250   1355655
AFLR3 GG : Nodes, Elements   =    255720   1363076
AFLR3 GG : Nodes, Elements   =    255720   1373406
AFLR3 GG : Nodes, Elements   =    255720   1370780
AFLR3 GG : Nodes, Elements   =    255720   1370395
AFLR3 GG : Nodes, Elements   =    258030   1377337
AFLR3 GG : Nodes, Elements   =    258030   1386970
AFLR3 GG : Nodes, Elements   =    258030   1384475
AFLR3 GG : Nodes, Elements   =    258030   1384129
AFLR3 GG : Nodes, Elements   =    260140   1390468
AFLR3 GG : Nodes, Elements   =    260140   1399380
AFLR3 GG : Nodes, Elements   =    260140   1397088
AFLR3 GG : Nodes, Elements   =    260140   1396756
AFLR3 GG : Nodes, Elements   =    262101   1402652
AFLR3 GG : Nodes, Elements   =    262101   1410823
AFLR3 GG : Nodes, Elements   =    262101   1408750
AFLR3 GG : Nodes, Elements   =    262101   1408449
AFLR3 GG : Nodes, Elements   =    263874   1413772
AFLR3 GG : Nodes, Elements   =    263874   1421265
AFLR3 GG : Nodes, Elements   =    263874   1419328
AFLR3 GG : Nodes, Elements   =    263874   1419031
AFLR3 GG : Nodes, Elements   =    265502   1423922
AFLR3 GG : Nodes, Elements   =    265502   1430708
AFLR3 GG : Nodes, Elements   =    265502   1428992
AFLR3 GG : Nodes, Elements   =    265502   1428760
AFLR3 GG : Nodes, Elements   =    266959   1433132
AFLR3 GG : Nodes, Elements   =    266959   1439256
AFLR3 GG : Nodes, Elements   =    266959   1437692
AFLR3 GG : Nodes, Elements   =    266959   1437468
AFLR3 GG : Nodes, Elements   =    268346   1441631
AFLR3 GG : Nodes, Elements   =    268346   1447387
AFLR3 GG : Nodes, Elements   =    268346   1445961
AFLR3 GG : Nodes, Elements   =    268346   1445777
AFLR3 GG : Nodes, Elements   =    269498   1449233
AFLR3 GG : Nodes, Elements   =    269498   1454050
AFLR3 GG : Nodes, Elements   =    269498   1452772
AFLR3 GG : Nodes, Elements   =    269498   1452606
AFLR3 GG : Nodes, Elements   =    270525   1455695
AFLR3 GG : Nodes, Elements   =    270525   1460017
AFLR3 GG : Nodes, Elements   =    270525   1458918
AFLR3 GG : Nodes, Elements   =    270525   1458751
AFLR3 GG : Nodes, Elements   =    271337   1461192
AFLR3 GG : Nodes, Elements   =    271337   1464613
AFLR3 GG : Nodes, Elements   =    271337   1463713
AFLR3 GG : Nodes, Elements   =    271337   1463597
AFLR3 GG : Nodes, Elements   =    272005   1465606
AFLR3 GG : Nodes, Elements   =    272005   1468389
AFLR3 GG : Nodes, Elements   =    272005   1467643
AFLR3 GG : Nodes, Elements   =    272005   1467527
AFLR3 GG : Nodes, Elements   =    272522   1469078
AFLR3 GG : Nodes, Elements   =    272522   1471251
AFLR3 GG : Nodes, Elements   =    272522   1470671
AFLR3 GG : Nodes, Elements   =    272522   1470578
AFLR3 GG : Nodes, Elements   =    272900   1471713
AFLR3 GG : Nodes, Elements   =    272900   1473446
AFLR3 GG : Nodes, Elements   =    272900   1472908
AFLR3 GG : Nodes, Elements   =    272900   1472822
AFLR3 GG : Nodes, Elements   =    273212   1473760
AFLR3 GG : Nodes, Elements   =    273212   1475130
AFLR3 GG : Nodes, Elements   =    273212   1474740
AFLR3 GG : Nodes, Elements   =    273212   1474662
AFLR3 GG : Nodes, Elements   =    273460   1475407
AFLR3 GG : Nodes, Elements   =    273460   1476525
AFLR3 GG : Nodes, Elements   =    273460   1476174
AFLR3 GG : Nodes, Elements   =    273460   1476113
AFLR3 GG : Nodes, Elements   =    273642   1476659
AFLR3 GG : Nodes, Elements   =    273642   1477507
AFLR3 GG : Nodes, Elements   =    273642   1477240
AFLR3 GG : Nodes, Elements   =    273642   1477168
AFLR3 GG : Nodes, Elements   =    273768   1477546
AFLR3 GG : Nodes, Elements   =    273768   1478211
AFLR3 GG : Nodes, Elements   =    273768   1477960
AFLR3 GG : Nodes, Elements   =    273768   1477911
AFLR3 GG : Nodes, Elements   =    273846   1478146
AFLR3 GG : Nodes, Elements   =    273846   1478569
AFLR3 GG : Nodes, Elements   =    273846   1478416
AFLR3 GG : Nodes, Elements   =    273846   1478361
AFLR3 GG : Nodes, Elements   =    273916   1478572
AFLR3 GG : Nodes, Elements   =    273916   1478978
AFLR3 GG : Nodes, Elements   =    273916   1478829
AFLR3 GG : Nodes, Elements   =    273916   1478792
AFLR3 GG : Nodes, Elements   =    273965   1478939
AFLR3 GG : Nodes, Elements   =    273965   1479226
AFLR3 GG : Nodes, Elements   =    273965   1479106
AFLR3 GG : Nodes, Elements   =    273965   1479072
AFLR3 GG : Nodes, Elements   =    273995   1479162
AFLR3 GG : Nodes, Elements   =    273995   1479324
AFLR3 GG : Nodes, Elements   =    273995   1479246
AFLR3 GG : Nodes, Elements   =    273995   1479229
AFLR3 GG : Nodes, Elements   =    274008   1479268
AFLR3 GG : Nodes, Elements   =    274008   1479350
AFLR3 GG : Nodes, Elements   =    274008   1479303
AFLR3 GG : Nodes, Elements   =    274008   1479299
AFLR3 GG : Nodes, Elements   =    274012   1479311
AFLR3 GG : Nodes, Elements   =    274012   1479332
AFLR3 GG : Nodes, Elements   =    274012   1479324
AFLR3 GG : Nodes, Elements   =    274012   1479320
AFLR3 GG : Nodes, Elements   =    274016   1479332
AFLR3 GG : Nodes, Elements   =    274016   1479370
AFLR3 GG : Nodes, Elements   =    274016   1479347
AFLR3 GG : Nodes, Elements   =    274016   1479345
AFLR3 GG : Nodes, Elements   =    274021   1479360
AFLR3 GG : Nodes, Elements   =    274021   1479413
AFLR3 GG : Nodes, Elements   =    274021   1479388
AFLR3 GG : Nodes, Elements   =    274021   1479378
AFLR3 GG : Nodes, Elements   =    274023   1479384
AFLR3 GG : Nodes, Elements   =    274023   1479402
AFLR3 GG : Nodes, Elements   =    274023   1479391
AFLR3 GG : Nodes, Elements   =    274023   1479389
AFLR3 GG : Nodes, Elements   =    274024   1479392
AFLR3 GG : Nodes, Elements   =    274024   1479397
AFLR3 GG : Nodes, Elements   =    274024   1479394
AFLR3 GG : Nodes, Elements   =    274079   1479560
AFLR3 GG : Nodes, Elements   =    274079   1479755
AFLR3 GG : Nodes, Elements   =    274079   1479704
AFLR3 GG : Nodes, Elements   =    274079   1479700
AFLR3 GG : Nodes, Elements   =    274095   1479748
AFLR3 GG : Nodes, Elements   =    274095   1479820
AFLR3 GG : Nodes, Elements   =    274095   1479790
AFLR3 GG : Nodes, Elements   =    274095   1479786
AFLR3 GG : Nodes, Elements   =    274099   1479798
AFLR3 GG : Nodes, Elements   =    274099   1479811
AFLR3 GG : Nodes, Elements   =    274099   1479810
AFLR3 GG : Nodes, Elements   =    274099   1479811
AFLR3 GG : Nodes, Elements   =    274100   1479814
AFLR3 GG : Nodes, Elements   =    274100   1479822
AFLR3 GG : Nodes, Elements   =    274100   1479817
AFLR3 GG : Nodes, Elements   =    274100   1479816
 
AFLR3    : CPU Time          =    11.171   seconds
 
AFLR3 QI : QUALITY IMPROVEMENT
 
AFLR3 QI : Nodes, Elements   =    274100   1479816
AFLR3 QI : Nodes, Elements   =    270658   1460360
AFLR3 QI : Nodes, Elements   =    270212   1457844
AFLR3 QI : Nodes, Elements   =    270191   1457719
AFLR3 QI : Nodes, Elements   =    270190   1457713
AFLR3 QI : Nodes, Elements   =    270190   1471003
AFLR3 QI : Nodes, Elements   =    270190   1457159
AFLR3 QI : Nodes, Elements   =    270190   1455643
AFLR3 QI : Nodes, Elements   =    270190   1465645
AFLR3 QI : Nodes, Elements   =    270190   1456025
AFLR3 QI : Nodes, Elements   =    270190   1455542
AFLR3 QI : Nodes, Elements   =    270190   1459176
AFLR3 QI : Nodes, Elements   =    270190   1455122
AFLR3 QI : Nodes, Elements   =    270190   1454503
AFLR3 QI : Nodes, Elements   =    270190   1457304
AFLR3 QI : Nodes, Elements   =    270190   1454487
AFLR3 QI : Nodes, Elements   =    270190   1454110
AFLR3 QI : Nodes, Elements   =    270190   1456624
AFLR3 QI : Nodes, Elements   =    270190   1454198
AFLR3 QI : Nodes, Elements   =    270190   1453902
AFLR3 QI : Nodes, Elements   =    270190   1453852
AFLR3 QI : Nodes, Elements   =    270204   1453915
AFLR3 QI : Nodes, Elements   =    270204   1456382
AFLR3 QI : Nodes, Elements   =    270204   1454046
AFLR3 QI : Nodes, Elements   =    270204   1453918
AFLR3 QI : Nodes, Elements   =    270204   1456247
AFLR3 QI : Nodes, Elements   =    270204   1454017
AFLR3 QI : Nodes, Elements   =    270204   1453797
 
AFLR3    : CPU Time          =     3.449   seconds
 
AFLR3 QRG: QUALITY GRID RE-GENERATION
 
AFLR3 QRG: Nodes, Elements   =    270204   1453797
AFLR3 QRG: Nodes, Elements   =    270207   1453812
AFLR3 QRG: Nodes, Elements   =    270209   1453823
AFLR3 QRG: Nodes, Elements   =    270211   1453835
AFLR3 QRG: Nodes, Elements   =    270217   1453865
AFLR3 QRG: Nodes, Elements   =    270218   1453869
AFLR3 QRG: Nodes, Elements   =    270221   1453885
AFLR3 QRG: Nodes, Elements   =    270222   1453888
AFLR3 QRG: Nodes, Elements   =    270228   1453918
AFLR3 QRG: Nodes, Elements   =    270229   1453924
AFLR3 QRG: Nodes, Elements   =    270240   1453980
AFLR3 QRG: Nodes, Elements   =    270244   1453997
AFLR3 QRG: Nodes, Elements   =    270257   1454068
AFLR3 QRG: Nodes, Elements   =    270280   1454194
AFLR3 QRG: Nodes, Elements   =    270296   1454273
 
AFLR3    : CPU Time          =     0.122   seconds
 
AFLR3    : DONE
 
ANBL3 BLM: BL VOLUME GRID MERGE
 
ANBL3 BLM: Nodes, Elements   =    270296   1454273
 
UG3      : OUTPUT GRID
 
UG3      : Grid File Name    = .tmp.b8.ugrid
UG3      : Quad Surface Faces=         0
UG3      : Tria Surface Faces=    103698
UG3      : Nodes             =    475917
UG3      : Total Elements    =   1885010
UG3      : Hex Elements      =         0
UG3      : Pent_5 Elements   =     20687
UG3      : Pent_6 Elements   =    390947
UG3      : Tet Elements      =   1473376
 
ANBL3 BLM: Nodes, Elements   =    475917   2687591
ANBL3 BLM: Nodes, Elements   =    475917     19103
 
ANBL3    : CPU Time          =     0.284   seconds
 
ANBL3    : DONE

OVERALL  : CPU Time          =    40.852   seconds

UG3      : DIHEDRAL ANGLE CHECK

UG3      : No. Tet Elems     =   1473376
UG3      : Min, Max Ang      =     1.294     174.3
UG3      : Average Angle     =      70.1
UG3      : No. Angle&gt;160.0   =       338
UG3      : No. Angle&gt;179.9   =         0

UG3      : No. Pyramid Elems =     20687
UG3      : Min, Max Ang      =      7.23     174.4
UG3      : Average Angle     =      82.6
UG3      : No. Angle&gt;160.0   =       129
UG3      : No. Angle&gt;179.9   =         0

UG3      : No. Prism Elems   =    390947
UG3      : Min, Max Ang      =     6.851     174.6
UG3      : Average Angle     =      80.1
UG3      : No. Angle&gt;160.0   =       732
UG3      : No. Angle&gt;179.9   =         0

UG3      : VOL CHECK

UG3      : Total-Volume      =  5.96e+10

UG3      : No. Tet Elems     =   1473376
UG3      : Min Vol           =   5.2e-06
UG3      : Average Vol       =  4.05e+04
UG3      : Total-Tet-Vol     =  5.96e+10
UG3      : No. Vol&lt;TOL       =         0

UG3      : No. Pyramid Elems =     20687
UG3      : Min Vol           =  2.25e-05
UG3      : Average Vol       =    0.0432
UG3      : Total-Pyramid-Vol =       894
UG3      : No. Vol&lt;TOL       =         0

UG3      : No. Prism Elems   =    390947
UG3      : Min Vol           =   2.9e-05
UG3      : Average Vol       =     0.112
UG3      : Total-Prism-Vol   =  4.38e+04
UG3      : No. Vol&lt;TOL       =         0

UG3      : Q VOL-LENGTH-RATIO CHECK
                      2/3        2
UG3      : Q = c * Vol   / sum( L  )
UG3      : 0 &lt;= Q &lt;= 1
UG3      : Note that L includes scaling for BL-aspect=ratio

UG3      : No. Tet Elems     =   1473376
UG3      : Min, Max Q        =    0.0972         1
UG3      : Average Q         =     0.852
UG3      : No. Q&lt;       0.1  =         1
UG3      : No. Q&lt;      0.01  =         0

UG3      : No. Pyramid Elems =     20687
UG3      : Min, Max Q        =     0.212         1
UG3      : Average Q         =     0.781
UG3      : No. Q&lt;       0.1  =         0
UG3      : No. Q&lt;      0.01  =         0

UG3      : No. Prism Elems   =    390947
UG3      : Min, Max Q        =     0.254         1
UG3      : Average Q         =     0.909
UG3      : No. Q&lt;       0.1  =         0
UG3      : No. Q&lt;      0.01  =         0

UG3      : CPU Time          =     0.000   seconds

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.8.1
EGADS    : ---------------------------------------

EGADS    : CREATE EGADS TESS FROM AFLR3 DATA

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EGADS    : CREATING TESSELLATION FOR BODY 0 EDGE 176

EGADS    : CREATING TESSELLATION FOR BODY 0 FACE 1
EGADS    : CREATING TESSELLATION FOR BODY 0 FACE 2
EGADS    : CREATING TESSELLATION FOR BODY 0 FACE 3
EGADS    : CREATING TESSELLATION FOR BODY 0 FACE 4
EGADS    : CREATING TESSELLATION FOR BODY 0 FACE 5
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EGADS    : CREATING TESSELLATION FOR BODY 0 FACE 7
EGADS    : CREATING TESSELLATION FOR BODY 0 FACE 8
EGADS    : CREATING TESSELLATION FOR BODY 0 FACE 9
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EGADS    : CREATING TESSELLATION FOR BODY 0 FACE 11
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EGADS    : CREATING TESSELLATION FOR BODY 0 FACE 13
EGADS    : CREATING TESSELLATION FOR BODY 0 FACE 14
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EGADS    : CREATING TESSELLATION FOR BODY 0 FACE 16
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EGADS    : CREATING TESSELLATION FOR BODY 0 FACE 18
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EGADS    : CREATING TESSELLATION FOR BODY 0 FACE 21
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EGADS    : CREATING TESSELLATION FOR BODY 0 FACE 25
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EGADS    : CREATING TESSELLATION FOR BODY 0 FACE 27
EGADS    : CREATING TESSELLATION FOR BODY 0 FACE 28
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EGADS    : CREATING TESSELLATION FOR BODY 0 FACE 34
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EGADS    : CREATING TESSELLATION FOR BODY 0 FACE 46
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EGADS    : CREATING TESSELLATION FOR BODY 0 FACE 67

EGADS    : CREATING TESSELLATION FOR BODY 1 EDGE 177
EGADS    : CREATING TESSELLATION FOR BODY 1 EDGE 178
EGADS    : CREATING TESSELLATION FOR BODY 1 EDGE 179
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EGADS    : CREATING TESSELLATION FOR BODY 1 EDGE 184
EGADS    : CREATING TESSELLATION FOR BODY 1 EDGE 185

EGADS    : CREATING TESSELLATION FOR BODY 1 FACE 68
EGADS    : CREATING TESSELLATION FOR BODY 1 FACE 69
EGADS    : CREATING TESSELLATION FOR BODY 1 FACE 70
EGADS    : CREATING TESSELLATION FOR BODY 1 FACE 71
EGADS    : CREATING TESSELLATION FOR BODY 1 FACE 72

EGADS    : CREATING TESSELLATION FOR BODY 2 EDGE 186
EGADS    : CREATING TESSELLATION FOR BODY 2 EDGE 187
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EGADS    : CREATING TESSELLATION FOR BODY 2 EDGE 193
EGADS    : CREATING TESSELLATION FOR BODY 2 EDGE 194

EGADS    : CREATING TESSELLATION FOR BODY 2 FACE 73
EGADS    : CREATING TESSELLATION FOR BODY 2 FACE 74
EGADS    : CREATING TESSELLATION FOR BODY 2 FACE 75
EGADS    : CREATING TESSELLATION FOR BODY 2 FACE 76
EGADS    : CREATING TESSELLATION FOR BODY 2 FACE 77

EGADS    : CREATING TESSELLATION FOR BODY 3 EDGE 195
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EGADS    : CREATING TESSELLATION FOR BODY 3 EDGE 203

EGADS    : CREATING TESSELLATION FOR BODY 3 FACE 78
EGADS    : CREATING TESSELLATION FOR BODY 3 FACE 79
EGADS    : CREATING TESSELLATION FOR BODY 3 FACE 80
EGADS    : CREATING TESSELLATION FOR BODY 3 FACE 81
EGADS    : CREATING TESSELLATION FOR BODY 3 FACE 82

EGADS    : CREATING TESSELLATION FOR BODY 4 EDGE 204
EGADS    : CREATING TESSELLATION FOR BODY 4 EDGE 205
EGADS    : CREATING TESSELLATION FOR BODY 4 EDGE 206
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EGADS    : CREATING TESSELLATION FOR BODY 4 EDGE 210
EGADS    : CREATING TESSELLATION FOR BODY 4 EDGE 211
EGADS    : CREATING TESSELLATION FOR BODY 4 EDGE 212

EGADS    : CREATING TESSELLATION FOR BODY 4 FACE 83
EGADS    : CREATING TESSELLATION FOR BODY 4 FACE 84
EGADS    : CREATING TESSELLATION FOR BODY 4 FACE 85
EGADS    : CREATING TESSELLATION FOR BODY 4 FACE 86
EGADS    : CREATING TESSELLATION FOR BODY 4 FACE 87

EGADS    : CREATING TESSELLATION FOR BODY 5 EDGE 213
EGADS    : CREATING TESSELLATION FOR BODY 5 EDGE 214
EGADS    : CREATING TESSELLATION FOR BODY 5 EDGE 215
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EGADS    : CREATING TESSELLATION FOR BODY 5 EDGE 219
EGADS    : CREATING TESSELLATION FOR BODY 5 EDGE 220
EGADS    : CREATING TESSELLATION FOR BODY 5 EDGE 221

EGADS    : CREATING TESSELLATION FOR BODY 5 FACE 88
EGADS    : CREATING TESSELLATION FOR BODY 5 FACE 89
EGADS    : CREATING TESSELLATION FOR BODY 5 FACE 90
EGADS    : CREATING TESSELLATION FOR BODY 5 FACE 91
EGADS    : CREATING TESSELLATION FOR BODY 5 FACE 92

EGADS    : CREATING TESSELLATION FOR BODY 6 EDGE 222
EGADS    : CREATING TESSELLATION FOR BODY 6 EDGE 223
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EGADS    : CREATING TESSELLATION FOR BODY 6 EDGE 229
EGADS    : CREATING TESSELLATION FOR BODY 6 EDGE 230

EGADS    : CREATING TESSELLATION FOR BODY 6 FACE 93
EGADS    : CREATING TESSELLATION FOR BODY 6 FACE 94
EGADS    : CREATING TESSELLATION FOR BODY 6 FACE 95
EGADS    : CREATING TESSELLATION FOR BODY 6 FACE 96
EGADS    : CREATING TESSELLATION FOR BODY 6 FACE 97

EGADS    : CREATING TESSELLATION FOR BODY 7 EDGE 231
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EGADS    : CREATING TESSELLATION FOR BODY 7 EDGE 238
EGADS    : CREATING TESSELLATION FOR BODY 7 EDGE 239

EGADS    : CREATING TESSELLATION FOR BODY 7 FACE 98
EGADS    : CREATING TESSELLATION FOR BODY 7 FACE 99
EGADS    : CREATING TESSELLATION FOR BODY 7 FACE 100
EGADS    : CREATING TESSELLATION FOR BODY 7 FACE 101
EGADS    : CREATING TESSELLATION FOR BODY 7 FACE 102

EGADS    : CREATING TESSELLATION FOR BODY 8 EDGE 240
EGADS    : CREATING TESSELLATION FOR BODY 8 EDGE 241
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EGADS    : CREATING TESSELLATION FOR BODY 8 EDGE 247
EGADS    : CREATING TESSELLATION FOR BODY 8 EDGE 248

EGADS    : CREATING TESSELLATION FOR BODY 8 FACE 103
EGADS    : CREATING TESSELLATION FOR BODY 8 FACE 104
EGADS    : CREATING TESSELLATION FOR BODY 8 FACE 105
EGADS    : CREATING TESSELLATION FOR BODY 8 FACE 106
EGADS    : CREATING TESSELLATION FOR BODY 8 FACE 107

EGADS    : CREATING TESSELLATION FOR BODY 9 EDGE 249
EGADS    : CREATING TESSELLATION FOR BODY 9 EDGE 250
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EGADS    : CREATING TESSELLATION FOR BODY 9 EDGE 257

EGADS    : CREATING TESSELLATION FOR BODY 9 FACE 108
EGADS    : CREATING TESSELLATION FOR BODY 9 FACE 109
EGADS    : CREATING TESSELLATION FOR BODY 9 FACE 110
EGADS    : CREATING TESSELLATION FOR BODY 9 FACE 111
EGADS    : CREATING TESSELLATION FOR BODY 9 FACE 112

EGADS    : CREATING TESSELLATION FOR BODY 10 EDGE 258
EGADS    : CREATING TESSELLATION FOR BODY 10 EDGE 259
EGADS    : CREATING TESSELLATION FOR BODY 10 EDGE 260
EGADS    : CREATING TESSELLATION FOR BODY 10 EDGE 261
EGADS    : CREATING TESSELLATION FOR BODY 10 EDGE 262
EGADS    : CREATING TESSELLATION FOR BODY 10 EDGE 263
EGADS    : CREATING TESSELLATION FOR BODY 10 EDGE 264
EGADS    : CREATING TESSELLATION FOR BODY 10 EDGE 265
EGADS    : CREATING TESSELLATION FOR BODY 10 EDGE 266
EGADS    : CREATING TESSELLATION FOR BODY 10 EDGE 267
EGADS    : CREATING TESSELLATION FOR BODY 10 EDGE 268
EGADS    : CREATING TESSELLATION FOR BODY 10 EDGE 269

EGADS    : CREATING TESSELLATION FOR BODY 10 FACE 113
EGADS    : CREATING TESSELLATION FOR BODY 10 FACE 114
EGADS    : CREATING TESSELLATION FOR BODY 10 FACE 115
EGADS    : CREATING TESSELLATION FOR BODY 10 FACE 116
EGADS    : CREATING TESSELLATION FOR BODY 10 FACE 117
EGADS    : CREATING TESSELLATION FOR BODY 10 FACE 118

EGADS    : EGADS TESS CREATED

EGADS    : CHECK TESS FACE NODE MAP

EGADS    : CHECKING NODE MAP FOR BODY 0 FACE 1
EGADS    : CHECKING NODE MAP FOR BODY 0 FACE 2
EGADS    : CHECKING NODE MAP FOR BODY 0 FACE 3
EGADS    : CHECKING NODE MAP FOR BODY 0 FACE 4
EGADS    : CHECKING NODE MAP FOR BODY 0 FACE 5
EGADS    : CHECKING NODE MAP FOR BODY 0 FACE 6
EGADS    : CHECKING NODE MAP FOR BODY 0 FACE 7
EGADS    : CHECKING NODE MAP FOR BODY 0 FACE 8
EGADS    : CHECKING NODE MAP FOR BODY 0 FACE 9
EGADS    : CHECKING NODE MAP FOR BODY 0 FACE 10
EGADS    : CHECKING NODE MAP FOR BODY 0 FACE 11
EGADS    : CHECKING NODE MAP FOR BODY 0 FACE 12
EGADS    : CHECKING NODE MAP FOR BODY 0 FACE 13
EGADS    : CHECKING NODE MAP FOR BODY 0 FACE 14
EGADS    : CHECKING NODE MAP FOR BODY 0 FACE 15
EGADS    : CHECKING NODE MAP FOR BODY 0 FACE 16
EGADS    : CHECKING NODE MAP FOR BODY 0 FACE 17
EGADS    : CHECKING NODE MAP FOR BODY 0 FACE 18
EGADS    : CHECKING NODE MAP FOR BODY 0 FACE 19
EGADS    : CHECKING NODE MAP FOR BODY 0 FACE 20
EGADS    : CHECKING NODE MAP FOR BODY 0 FACE 21
EGADS    : CHECKING NODE MAP FOR BODY 0 FACE 22
EGADS    : CHECKING NODE MAP FOR BODY 0 FACE 23
EGADS    : CHECKING NODE MAP FOR BODY 0 FACE 24
EGADS    : CHECKING NODE MAP FOR BODY 0 FACE 25
EGADS    : CHECKING NODE MAP FOR BODY 0 FACE 26
EGADS    : CHECKING NODE MAP FOR BODY 0 FACE 27
EGADS    : CHECKING NODE MAP FOR BODY 0 FACE 28
EGADS    : CHECKING NODE MAP FOR BODY 0 FACE 29
EGADS    : CHECKING NODE MAP FOR BODY 0 FACE 30
EGADS    : CHECKING NODE MAP FOR BODY 0 FACE 31
EGADS    : CHECKING NODE MAP FOR BODY 0 FACE 32
EGADS    : CHECKING NODE MAP FOR BODY 0 FACE 33
EGADS    : CHECKING NODE MAP FOR BODY 0 FACE 34
EGADS    : CHECKING NODE MAP FOR BODY 0 FACE 35
EGADS    : CHECKING NODE MAP FOR BODY 0 FACE 36
EGADS    : CHECKING NODE MAP FOR BODY 0 FACE 37
EGADS    : CHECKING NODE MAP FOR BODY 0 FACE 38
EGADS    : CHECKING NODE MAP FOR BODY 0 FACE 39
EGADS    : CHECKING NODE MAP FOR BODY 0 FACE 40
EGADS    : CHECKING NODE MAP FOR BODY 0 FACE 41
EGADS    : CHECKING NODE MAP FOR BODY 0 FACE 42
EGADS    : CHECKING NODE MAP FOR BODY 0 FACE 43
EGADS    : CHECKING NODE MAP FOR BODY 0 FACE 44
EGADS    : CHECKING NODE MAP FOR BODY 0 FACE 45
EGADS    : CHECKING NODE MAP FOR BODY 0 FACE 46
EGADS    : CHECKING NODE MAP FOR BODY 0 FACE 47
EGADS    : CHECKING NODE MAP FOR BODY 0 FACE 48
EGADS    : CHECKING NODE MAP FOR BODY 0 FACE 49
EGADS    : CHECKING NODE MAP FOR BODY 0 FACE 50
EGADS    : CHECKING NODE MAP FOR BODY 0 FACE 51
EGADS    : CHECKING NODE MAP FOR BODY 0 FACE 52
EGADS    : CHECKING NODE MAP FOR BODY 0 FACE 53
EGADS    : CHECKING NODE MAP FOR BODY 0 FACE 54
EGADS    : CHECKING NODE MAP FOR BODY 0 FACE 55
EGADS    : CHECKING NODE MAP FOR BODY 0 FACE 56
EGADS    : CHECKING NODE MAP FOR BODY 0 FACE 57
EGADS    : CHECKING NODE MAP FOR BODY 0 FACE 58
EGADS    : CHECKING NODE MAP FOR BODY 0 FACE 59
EGADS    : CHECKING NODE MAP FOR BODY 0 FACE 60
EGADS    : CHECKING NODE MAP FOR BODY 0 FACE 61
EGADS    : CHECKING NODE MAP FOR BODY 0 FACE 62
EGADS    : CHECKING NODE MAP FOR BODY 0 FACE 63
EGADS    : CHECKING NODE MAP FOR BODY 0 FACE 64
EGADS    : CHECKING NODE MAP FOR BODY 0 FACE 65
EGADS    : CHECKING NODE MAP FOR BODY 0 FACE 66
EGADS    : CHECKING NODE MAP FOR BODY 0 FACE 67
EGADS    : CHECKING NODE MAP FOR BODY 1 FACE 68
EGADS    : CHECKING NODE MAP FOR BODY 1 FACE 69
EGADS    : CHECKING NODE MAP FOR BODY 1 FACE 70
EGADS    : CHECKING NODE MAP FOR BODY 1 FACE 71
EGADS    : CHECKING NODE MAP FOR BODY 1 FACE 72
EGADS    : CHECKING NODE MAP FOR BODY 2 FACE 73
EGADS    : CHECKING NODE MAP FOR BODY 2 FACE 74
EGADS    : CHECKING NODE MAP FOR BODY 2 FACE 75
EGADS    : CHECKING NODE MAP FOR BODY 2 FACE 76
EGADS    : CHECKING NODE MAP FOR BODY 2 FACE 77
EGADS    : CHECKING NODE MAP FOR BODY 3 FACE 78
EGADS    : CHECKING NODE MAP FOR BODY 3 FACE 79
EGADS    : CHECKING NODE MAP FOR BODY 3 FACE 80
EGADS    : CHECKING NODE MAP FOR BODY 3 FACE 81
EGADS    : CHECKING NODE MAP FOR BODY 3 FACE 82
EGADS    : CHECKING NODE MAP FOR BODY 4 FACE 83
EGADS    : CHECKING NODE MAP FOR BODY 4 FACE 84
EGADS    : CHECKING NODE MAP FOR BODY 4 FACE 85
EGADS    : CHECKING NODE MAP FOR BODY 4 FACE 86
EGADS    : CHECKING NODE MAP FOR BODY 4 FACE 87
EGADS    : CHECKING NODE MAP FOR BODY 5 FACE 88
EGADS    : CHECKING NODE MAP FOR BODY 5 FACE 89
EGADS    : CHECKING NODE MAP FOR BODY 5 FACE 90
EGADS    : CHECKING NODE MAP FOR BODY 5 FACE 91
EGADS    : CHECKING NODE MAP FOR BODY 5 FACE 92
EGADS    : CHECKING NODE MAP FOR BODY 6 FACE 93
EGADS    : CHECKING NODE MAP FOR BODY 6 FACE 94
EGADS    : CHECKING NODE MAP FOR BODY 6 FACE 95
EGADS    : CHECKING NODE MAP FOR BODY 6 FACE 96
EGADS    : CHECKING NODE MAP FOR BODY 6 FACE 97
EGADS    : CHECKING NODE MAP FOR BODY 7 FACE 98
EGADS    : CHECKING NODE MAP FOR BODY 7 FACE 99
EGADS    : CHECKING NODE MAP FOR BODY 7 FACE 100
EGADS    : CHECKING NODE MAP FOR BODY 7 FACE 101
EGADS    : CHECKING NODE MAP FOR BODY 7 FACE 102
EGADS    : CHECKING NODE MAP FOR BODY 8 FACE 103
EGADS    : CHECKING NODE MAP FOR BODY 8 FACE 104
EGADS    : CHECKING NODE MAP FOR BODY 8 FACE 105
EGADS    : CHECKING NODE MAP FOR BODY 8 FACE 106
EGADS    : CHECKING NODE MAP FOR BODY 8 FACE 107
EGADS    : CHECKING NODE MAP FOR BODY 9 FACE 108
EGADS    : CHECKING NODE MAP FOR BODY 9 FACE 109
EGADS    : CHECKING NODE MAP FOR BODY 9 FACE 110
EGADS    : CHECKING NODE MAP FOR BODY 9 FACE 111
EGADS    : CHECKING NODE MAP FOR BODY 9 FACE 112
EGADS    : CHECKING NODE MAP FOR BODY 10 FACE 113
EGADS    : CHECKING NODE MAP FOR BODY 10 FACE 114
EGADS    : CHECKING NODE MAP FOR BODY 10 FACE 115
EGADS    : CHECKING NODE MAP FOR BODY 10 FACE 116
EGADS    : CHECKING NODE MAP FOR BODY 10 FACE 117
EGADS    : CHECKING NODE MAP FOR BODY 10 FACE 118
Volume mesh:
	Number of nodes          = 475917
	Number of elements       = 1988708
	Number of triangles      = 103698
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 1473376
	Number of pyramids       = 20687
	Number of prisms         = 390947
	Number of hexahedrals    = 0

Writing vtk file ....

Writing vtk general file ....
Finished writing vtk file


real	1m5.516s
user	1m9.230s
sys	0m11.061s
+ status=0
+ set +x

=================================================
data/session07/12_aflr4_aflr3_ViscousTransport.py passed (as expected)
=================================================


=================================================
aflr4_curv_factor.py test;
+ python aflr4_curv_factor.py
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/CAPS/training/2023/training.log

MESSAGE:: Building wingOml

Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 2
	Name = Wing, index = 1
	Name = Farfield, index = 2
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 3
	Name = leftWing, index = 1
	Name = riteWing, index = 2
	Name = Farfield, index = 3

Getting mesh sizing parameters
	Mesh sizing name - Farfield
	Mesh sizing name - leftWing
	Mesh sizing name - riteWing
	Done getting mesh sizing parameters
 
AFLR2    : ---------------------------------------
AFLR2    : AFLR2 LIBRARY
AFLR2    : ADVANCING-FRONT/LOCAL-RECONNECTION
AFLR2    : TRIA/QUAD GRID GENERATOR
AFLR2    : Version Number 9.18.1
AFLR2    : Version Date   06/11/24 @ 05:52PM
AFLR2    : Compile OS     Darwin 23.5.0 arm64
AFLR2    : Compile Date   06/11/24 @ 05:52PM
AFLR2    : Copyright 1994-2021, D.L. Marcum
AFLR2    : ---------------------------------------
 
AFLR4    : ---------------------------------------
AFLR4    : AFLR4 LIBRARY
AFLR4    : ADVANCING-FRONT/LOCAL-RECONNECTION
AFLR4    : TRIA/QUAD SURFACE GRID GENERATOR
AFLR4    : Version Number 11.5.15
AFLR4    : Version Date   07/19/24 @ 07:04PM
AFLR4    : Compile OS     Darwin 23.5.0 arm64
AFLR4    : Compile Date   07/19/24 @ 07:06PM
AFLR4    : Copyright 1994-2021, D.L. Marcum
AFLR4    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.8.1
EGADS    : ---------------------------------------

EGADS    : EGADS CAD Geometry Setup

EGADS    : Model has 2 Active Bodies

EGADS    : Body 0 is a SolidBody
EGADS    : Body 0 has 1 Shells
EGADS    : Body 0 has 10 Faces
EGADS    : Body 0 has 18 Edges
EGADS    : Body 0 has 10 Loops
EGADS    : Body 0 has 10 Nodes
EGADS    : Body 1 is a SolidBody
EGADS    : Body 1 has 1 Shells
EGADS    : Body 1 has 6 Faces
EGADS    : Body 1 has 12 Edges
EGADS    : Body 1 has 6 Loops
EGADS    : Body 1 has 8 Nodes

EGADS    : Check Grid BCs

EGADS    : Grid BCs are OK

EGADS    : Face Neighbor-Faces Information

EGADS    : QC  = Face Quad Combination Flag
EGADS    : IER = Face Isolated Edge Refinement Flag
EGADS    : ER  = Face Edge Refinement Factor
EGADS    :       Not applicable for Faces with a FarField Grid BC.
EGADS    : SF  = Face Scale Factor
EGADS    :       Not applicable for Faces with a FarField Grid BC.

EGADS    :   Face          Body    QC   IER       ER    Scale   Neighbor
EGADS    :     ID  Active    ID  Flag  Flag   Weight   Factor   Faces
EGADS    :      1     Yes     0     0     1        1        1   2 3 6
EGADS    :      2     Yes     0     0     1        1        1   1 4 5
EGADS    :      3     Yes     0     0     1        1        1   1 4 8
EGADS    :      4     Yes     0     0     1        1        1   2 3 5
EGADS    :      5     Yes     0     0     1        1        1   2 4
EGADS    :      6     Yes     0     0     1        1        1   1 7 8
EGADS    :      7     Yes     0     0     1        1        1   6 9 10
EGADS    :      8     Yes     0     0     1        1        1   3 6 9
EGADS    :      9     Yes     0     0     1        1        1   7 8 10
EGADS    :     10     Yes     0     0     1        1        1   7 9
EGADS    :     11     Yes     1     0     1       NA       NA   13 14 15 16
EGADS    :     12     Yes     1     0     1       NA       NA   13 14 15 16
EGADS    :     13     Yes     1     0     1       NA       NA   11 12 15 16
EGADS    :     14     Yes     1     0     1       NA       NA   11 12 15 16
EGADS    :     15     Yes     1     0     1       NA       NA   11 12 13 14
EGADS    :     16     Yes     1     0     1       NA       NA   11 12 13 14

EGADS    : Face Edges Information

EGADS    :   Face   Edges
EGADS    :      1   -1 2 3 -4
EGADS    :      2   -5 4 6 -7
EGADS    :      3   -3 8 1 -9
EGADS    :      4   -6 9 5 -10
EGADS    :      5   7 10
EGADS    :      6   11 13 -12 -2
EGADS    :      7   14 16 -15 -13
EGADS    :      8   12 17 -11 -8
EGADS    :      9   15 18 -14 -17
EGADS    :     10   -16 -18
EGADS    :     11   19 20 -21 -22
EGADS    :     12   -23 26 25 -24
EGADS    :     13   27 23 -28 -19
EGADS    :     14   -29 21 30 -25
EGADS    :     15   22 29 -26 -27
EGADS    :     16   -20 28 24 -30

EGADS    : Face Loops Information

EGADS    :   Face   Loops
EGADS    :      1   1
EGADS    :      2   2
EGADS    :      3   3
EGADS    :      4   4
EGADS    :      5   5
EGADS    :      6   6
EGADS    :      7   7
EGADS    :      8   8
EGADS    :      9   9
EGADS    :     10   10
EGADS    :     11   11
EGADS    :     12   12
EGADS    :     13   13
EGADS    :     14   14
EGADS    :     15   15
EGADS    :     16   16

EGADS    : Loop Edges Information

EGADS    :   Loop  Active   Edges
EGADS    :      1     Yes   -1 2 3 -4
EGADS    :      2     Yes   -5 4 6 -7
EGADS    :      3     Yes   -3 8 1 -9
EGADS    :      4     Yes   -6 9 5 -10
EGADS    :      5     Yes   7 10
EGADS    :      6     Yes   11 13 -12 -2
EGADS    :      7     Yes   14 16 -15 -13
EGADS    :      8     Yes   12 17 -11 -8
EGADS    :      9     Yes   15 18 -14 -17
EGADS    :     10     Yes   -16 -18
EGADS    :     11     Yes   19 20 -21 -22
EGADS    :     12     Yes   -23 26 25 -24
EGADS    :     13     Yes   27 23 -28 -19
EGADS    :     14     Yes   -29 21 30 -25
EGADS    :     15     Yes   22 29 -26 -27
EGADS    :     16     Yes   -20 28 24 -30

EGADS    : Edge Node, Scale Factor, and Neighbor-Faces Information

EGADS    : ESF = Edge Scale Factor
EGADS    :       Not applicable for DEGENERATE Edges or Edges with a FarField
EGADS    :       Grid BC Neighbor Face.

EGADS    :                                             Neighbor
EGADS    :   Edge  Body  Active Node1 Node2      ESF   Faces
EGADS    :      1     0     Yes     1     2        1   1 3
EGADS    :      2     0     Yes     1     3        1   1 6
EGADS    :      3     0     Yes     3     4        1   1 3
EGADS    :      4     0     Yes     2     4        1   1 2
EGADS    :      5     0     Yes     2     5        1   2 4
EGADS    :      6     0     Yes     4     6        1   2 4
EGADS    :      7     0     Yes     5     6        1   2 5
EGADS    :      8     0     Yes     3     1        1   3 8
EGADS    :      9     0     Yes     4     2        1   3 4
EGADS    :     10     0     Yes     6     5        1   4 5
EGADS    :     11     0     Yes     1     7        1   6 8
EGADS    :     12     0     Yes     3     8        1   6 8
EGADS    :     13     0     Yes     7     8        1   6 7
EGADS    :     14     0     Yes     7     9        1   7 9
EGADS    :     15     0     Yes     8    10        1   7 9
EGADS    :     16     0     Yes     9    10        1   7 10
EGADS    :     17     0     Yes     8     7        1   8 9
EGADS    :     18     0     Yes    10     9        1   9 10
EGADS    :     19     1     Yes    12    11       NA   11 13
EGADS    :     20     1     Yes    11    13       NA   11 16
EGADS    :     21     1     Yes    14    13       NA   11 14
EGADS    :     22     1     Yes    12    14       NA   11 15
EGADS    :     23     1     Yes    16    15       NA   12 13
EGADS    :     24     1     Yes    15    17       NA   12 16
EGADS    :     25     1     Yes    18    17       NA   12 14
EGADS    :     26     1     Yes    16    18       NA   12 15
EGADS    :     27     1     Yes    12    16       NA   13 15
EGADS    :     28     1     Yes    11    15       NA   13 16
EGADS    :     29     1     Yes    14    18       NA   14 15
EGADS    :     30     1     Yes    13    17       NA   14 16

EGADS    : Node Information

EGADS    :   Node  Active      Coordinates
EGADS    :      1     Yes       97.2007855                0                0
EGADS    :      2     Yes       97.9335611                0                0
EGADS    :      3     Yes               50                0                0
EGADS    :      4     Yes       75.3047874                0                0
EGADS    :      5     Yes       123.552357                0        4.7180639
EGADS    :      6     Yes       118.391317                0       3.99272703
EGADS    :      7     Yes       97.9335611       36.1389817                0
EGADS    :      8     Yes       75.3047874       36.1389817                0
EGADS    :      9     Yes       123.552357       97.6729236        4.7180639
EGADS    :     10     Yes       118.391317       97.6729236       3.99272703
EGADS    :     11     Yes                0                0       1951.57774
EGADS    :     12     Yes                0                0                0
EGADS    :     13     Yes                0       1953.45847       1951.57774
EGADS    :     14     Yes                0       1953.45847                0
EGADS    :     15     Yes       2040.21562                0       1951.57774
EGADS    :     16     Yes       2040.21562                0                0
EGADS    :     17     Yes       2040.21562       1953.45847       1951.57774
EGADS    :     18     Yes       2040.21562       1953.45847                0

EGADS    : Face and Edge Match Information

EGADS    : No Face Matches Found

AFLR4    : Surface Mesh Spacing Setup

AFLR4    : Max Bounding Box Length     = 3906.92
AFLR4    : Min Bounding Box Length     = 3906.92
AFLR4    : Max Ref Bounding Box Length = 195.346
AFLR4    : Min Ref Bounding Box Length = 13.1976
AFLR4    : Reference Length            = 21.7051
AFLR4    : BL Thickness                = 0
AFLR4    : FarField Spacing            = 530.302
AFLR4    : Abs Min Surf Spacing        = 0.0542627
AFLR4    : Min Surf Spacing            = 0.108525
AFLR4    : Max Surf Spacing            = 2.17051
AFLR4    : Global Scale Factor         = 1

AFLR4    : Geometry Definition Information

AFLR4    : Definition              Definition   Composite             Grid BC
AFLR4    :         ID                    Type          ID                Type
AFLR4    :          0     glue-only composite           -                   -
AFLR4    :          1            CAD geometry           0            STD w/BL
AFLR4    :          2            CAD geometry           0            STD w/BL
AFLR4    :          3            CAD geometry           0            STD w/BL
AFLR4    :          4            CAD geometry           0            STD w/BL
AFLR4    :          5            CAD geometry           0            STD w/BL
AFLR4    :          6            CAD geometry           0            STD w/BL
AFLR4    :          7            CAD geometry           0            STD w/BL
AFLR4    :          8            CAD geometry           0            STD w/BL
AFLR4    :          9            CAD geometry           0            STD w/BL
AFLR4    :         10            CAD geometry           0            STD w/BL
AFLR4    :         11            CAD geometry           0            FARFIELD
AFLR4    :         12            CAD geometry           0            FARFIELD
AFLR4    :         13            CAD geometry           0            FARFIELD
AFLR4    :         14            CAD geometry           0            FARFIELD
AFLR4    :         15            CAD geometry           0            FARFIELD
AFLR4    :         16            CAD geometry           0            FARFIELD

AFLR4    : Define CAD surface definition 1
AFLR4    : Define CAD surface definition 2
AFLR4    : Define CAD surface definition 3
AFLR4    : Define CAD surface definition 4
AFLR4    : Define CAD surface definition 5
AFLR4    : Define CAD surface definition 6
AFLR4    : Define CAD surface definition 7
AFLR4    : Define CAD surface definition 8
AFLR4    : Define CAD surface definition 9
AFLR4    : Define CAD surface definition 10
AFLR4    : Define CAD surface definition 11
AFLR4    : Define CAD surface definition 12
AFLR4    : Define CAD surface definition 13
AFLR4    : Define CAD surface definition 14
AFLR4    : Define CAD surface definition 15
AFLR4    : Define CAD surface definition 16

AFLR4    : Surface Grid Generation

AFLR4    : Generate optimal mesh on surface definition 1
AFLR2    : Nodes, Trias,Quads=     24884     49047         0
AFLR4    : Nodes, Trias,Quads=     19518     38315         0

AFLR4    : Generate optimal mesh on surface definition 2
AFLR2    : Nodes, Trias,Quads=     51312    101531         0
AFLR4    : Nodes, Trias,Quads=     29743     58393         0

AFLR4    : Generate optimal mesh on surface definition 3
AFLR2    : Nodes, Trias,Quads=     12428     24250         0
AFLR4    : Nodes, Trias,Quads=      9098     17590         0

AFLR4    : Generate optimal mesh on surface definition 4
AFLR2    : Nodes, Trias,Quads=     42374     83719         0
AFLR4    : Nodes, Trias,Quads=     25099     49169         0

AFLR4    : Generate optimal mesh on surface definition 5
AFLR2    : Nodes, Trias,Quads=       121       175         0
AFLR4    : Nodes, Trias,Quads=       101       135         0

AFLR4    : Generate optimal mesh on surface definition 6
AFLR2    : Nodes, Trias,Quads=     24944     49167         0
AFLR4    : Nodes, Trias,Quads=     20103     39485         0

AFLR4    : Generate optimal mesh on surface definition 7
AFLR2    : Nodes, Trias,Quads=     50494     99895         0
AFLR4    : Nodes, Trias,Quads=     29637     58181         0

AFLR4    : Generate optimal mesh on surface definition 8
AFLR2    : Nodes, Trias,Quads=     11747     22888         0
AFLR4    : Nodes, Trias,Quads=      9180     17754         0

AFLR4    : Generate optimal mesh on surface definition 9
AFLR2    : Nodes, Trias,Quads=     43574     86119         0
AFLR4    : Nodes, Trias,Quads=     25109     49189         0

AFLR4    : Generate optimal mesh on surface definition 10
AFLR2    : Nodes, Trias,Quads=       121       175         0
AFLR4    : Nodes, Trias,Quads=       101       135         0

AFLR4    : Generate optimal mesh on surface definition 11
AFLR2    : Nodes, Trias,Quads=        73       116         0
AFLR4    : Nodes, Trias,Quads=        68       106         0

AFLR4    : Generate optimal mesh on surface definition 12
AFLR2    : Nodes, Trias,Quads=        73       116         0
AFLR4    : Nodes, Trias,Quads=        68       106         0

AFLR4    : Generate optimal mesh on surface definition 13
AFLR2    : Nodes, Trias,Quads=        73       116         0
AFLR4    : Nodes, Trias,Quads=        68       106         0

AFLR4    : Generate optimal mesh on surface definition 14
AFLR2    : Nodes, Trias,Quads=        73       116         0
AFLR4    : Nodes, Trias,Quads=        68       106         0

AFLR4    : Generate optimal mesh on surface definition 15
AFLR2    : Nodes, Trias,Quads=        73       116         0
AFLR4    : Nodes, Trias,Quads=        68       106         0

AFLR4    : Generate optimal mesh on surface definition 16
AFLR2    : Nodes, Trias,Quads=        73       116         0
AFLR4    : Nodes, Trias,Quads=        68       106         0

DGEOM    : Add surface definitions to composite definition 0
DGEOM    : Glue composite surface definition 0
DGEOM    : Nodes,Faces,BEdges=    164495    328982      7180

AFLR4    : Curvature BG Surface Grid Generation

AFLR4    : Nodes, Faces      =    164495    328982

AFLR4    : Surface Grid Generation

AFLR4    : Generate optimal mesh on surface definition 1
AFLR2    : Nodes, Trias,Quads=     17390     33750         0
AFLR4    : Nodes, Trias,Quads=     32853     64676         0

AFLR4    : Generate optimal mesh on surface definition 2
AFLR2    : Nodes, Trias,Quads=     31290     61090         0
AFLR4    : Nodes, Trias,Quads=     45229     88968         0

AFLR4    : Generate optimal mesh on surface definition 3
AFLR2    : Nodes, Trias,Quads=     13604     26291         0
AFLR4    : Nodes, Trias,Quads=     18530     36143         0

AFLR4    : Generate optimal mesh on surface definition 4
AFLR2    : Nodes, Trias,Quads=     29109     56772         0
AFLR4    : Nodes, Trias,Quads=     31797     62148         0

AFLR4    : Generate optimal mesh on surface definition 5
AFLR2    : Nodes, Trias,Quads=       199       298         0
AFLR4    : Nodes, Trias,Quads=       185       270         0

AFLR4    : Generate optimal mesh on surface definition 6
AFLR2    : Nodes, Trias,Quads=     17365     33700         0
AFLR4    : Nodes, Trias,Quads=     32928     64826         0

AFLR4    : Generate optimal mesh on surface definition 7
AFLR2    : Nodes, Trias,Quads=     31485     61480         0
AFLR4    : Nodes, Trias,Quads=     45207     88924         0

AFLR4    : Generate optimal mesh on surface definition 8
AFLR2    : Nodes, Trias,Quads=     13973     27029         0
AFLR4    : Nodes, Trias,Quads=     18547     36177         0

AFLR4    : Generate optimal mesh on surface definition 9
AFLR2    : Nodes, Trias,Quads=     29417     57388         0
AFLR4    : Nodes, Trias,Quads=     31852     62258         0

AFLR4    : Generate optimal mesh on surface definition 10
AFLR2    : Nodes, Trias,Quads=       199       298         0
AFLR4    : Nodes, Trias,Quads=       185       270         0

AFLR4    : Generate optimal mesh on surface definition 11
AFLR2    : Nodes, Trias,Quads=        73       116         0
AFLR4    : Nodes, Trias,Quads=        68       106         0

AFLR4    : Generate optimal mesh on surface definition 12
AFLR2    : Nodes, Trias,Quads=        73       116         0
AFLR4    : Nodes, Trias,Quads=        68       106         0

AFLR4    : Generate optimal mesh on surface definition 13
AFLR2    : Nodes, Trias,Quads=        73       116         0
AFLR4    : Nodes, Trias,Quads=        68       106         0

AFLR4    : Generate optimal mesh on surface definition 14
AFLR2    : Nodes, Trias,Quads=        73       116         0
AFLR4    : Nodes, Trias,Quads=        68       106         0

AFLR4    : Generate optimal mesh on surface definition 15
AFLR2    : Nodes, Trias,Quads=        73       116         0
AFLR4    : Nodes, Trias,Quads=        68       106         0

AFLR4    : Generate optimal mesh on surface definition 16
AFLR2    : Nodes, Trias,Quads=        73       116         0
AFLR4    : Nodes, Trias,Quads=        68       106         0

DGEOM    : Add surface definitions to composite definition 0
DGEOM    : Glue composite surface definition 0
DGEOM    : Nodes,Faces,BEdges=    252652    505296     10114

OVERALL  : CPU Time          =     4.185   seconds
Body 1 (of 2)
Number of nodes    = 252332
Number of elements = 504660
Number of triangle elements      = 504660
Number of quadrilateral elements = 0
Body 2 (of 2)
Number of nodes    = 320
Number of elements = 636
Number of triangle elements      = 636
Number of quadrilateral elements = 0
----------------------------
Total number of nodes    = 252652
Total number of elements = 505296
Total number of triangle elements      = 505296
Total number of quadrilateral elements = 0

Getting mesh sizing parameters
	Mesh sizing name - Farfield
	Mesh sizing name - leftWing
	Mesh sizing name - riteWing
	Done getting mesh sizing parameters

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.8.1
EGADS    : ---------------------------------------

EGADS    : EGADS CAD Geometry Setup

EGADS    : Model has 2 Active Bodies

EGADS    : Body 0 is a SolidBody
EGADS    : Body 0 has 1 Shells
EGADS    : Body 0 has 10 Faces
EGADS    : Body 0 has 18 Edges
EGADS    : Body 0 has 10 Loops
EGADS    : Body 0 has 10 Nodes
EGADS    : Body 1 is a SolidBody
EGADS    : Body 1 has 1 Shells
EGADS    : Body 1 has 6 Faces
EGADS    : Body 1 has 12 Edges
EGADS    : Body 1 has 6 Loops
EGADS    : Body 1 has 8 Nodes

EGADS    : Check Grid BCs

EGADS    : Grid BCs are OK

EGADS    : Face Neighbor-Faces Information

EGADS    : QC  = Face Quad Combination Flag
EGADS    : IER = Face Isolated Edge Refinement Flag
EGADS    : ER  = Face Edge Refinement Factor
EGADS    :       Not applicable for Faces with a FarField Grid BC.
EGADS    : SF  = Face Scale Factor
EGADS    :       Not applicable for Faces with a FarField Grid BC.

EGADS    :   Face          Body    QC   IER       ER    Scale   Neighbor
EGADS    :     ID  Active    ID  Flag  Flag   Weight   Factor   Faces
EGADS    :      1     Yes     0     0     1        1        1   2 3 6
EGADS    :      2     Yes     0     0     1        1        1   1 4 5
EGADS    :      3     Yes     0     0     1        1        1   1 4 8
EGADS    :      4     Yes     0     0     1        1        1   2 3 5
EGADS    :      5     Yes     0     0     1        1        1   2 4
EGADS    :      6     Yes     0     0     1        1        1   1 7 8
EGADS    :      7     Yes     0     0     1        1        1   6 9 10
EGADS    :      8     Yes     0     0     1        1        1   3 6 9
EGADS    :      9     Yes     0     0     1        1        1   7 8 10
EGADS    :     10     Yes     0     0     1        1        1   7 9
EGADS    :     11     Yes     1     0     1       NA       NA   13 14 15 16
EGADS    :     12     Yes     1     0     1       NA       NA   13 14 15 16
EGADS    :     13     Yes     1     0     1       NA       NA   11 12 15 16
EGADS    :     14     Yes     1     0     1       NA       NA   11 12 15 16
EGADS    :     15     Yes     1     0     1       NA       NA   11 12 13 14
EGADS    :     16     Yes     1     0     1       NA       NA   11 12 13 14

EGADS    : Face Edges Information

EGADS    :   Face   Edges
EGADS    :      1   -1 2 3 -4
EGADS    :      2   -5 4 6 -7
EGADS    :      3   -3 8 1 -9
EGADS    :      4   -6 9 5 -10
EGADS    :      5   7 10
EGADS    :      6   11 13 -12 -2
EGADS    :      7   14 16 -15 -13
EGADS    :      8   12 17 -11 -8
EGADS    :      9   15 18 -14 -17
EGADS    :     10   -16 -18
EGADS    :     11   19 20 -21 -22
EGADS    :     12   -23 26 25 -24
EGADS    :     13   27 23 -28 -19
EGADS    :     14   -29 21 30 -25
EGADS    :     15   22 29 -26 -27
EGADS    :     16   -20 28 24 -30

EGADS    : Face Loops Information

EGADS    :   Face   Loops
EGADS    :      1   1
EGADS    :      2   2
EGADS    :      3   3
EGADS    :      4   4
EGADS    :      5   5
EGADS    :      6   6
EGADS    :      7   7
EGADS    :      8   8
EGADS    :      9   9
EGADS    :     10   10
EGADS    :     11   11
EGADS    :     12   12
EGADS    :     13   13
EGADS    :     14   14
EGADS    :     15   15
EGADS    :     16   16

EGADS    : Loop Edges Information

EGADS    :   Loop  Active   Edges
EGADS    :      1     Yes   -1 2 3 -4
EGADS    :      2     Yes   -5 4 6 -7
EGADS    :      3     Yes   -3 8 1 -9
EGADS    :      4     Yes   -6 9 5 -10
EGADS    :      5     Yes   7 10
EGADS    :      6     Yes   11 13 -12 -2
EGADS    :      7     Yes   14 16 -15 -13
EGADS    :      8     Yes   12 17 -11 -8
EGADS    :      9     Yes   15 18 -14 -17
EGADS    :     10     Yes   -16 -18
EGADS    :     11     Yes   19 20 -21 -22
EGADS    :     12     Yes   -23 26 25 -24
EGADS    :     13     Yes   27 23 -28 -19
EGADS    :     14     Yes   -29 21 30 -25
EGADS    :     15     Yes   22 29 -26 -27
EGADS    :     16     Yes   -20 28 24 -30

EGADS    : Edge Node, Scale Factor, and Neighbor-Faces Information

EGADS    : ESF = Edge Scale Factor
EGADS    :       Not applicable for DEGENERATE Edges or Edges with a FarField
EGADS    :       Grid BC Neighbor Face.

EGADS    :                                             Neighbor
EGADS    :   Edge  Body  Active Node1 Node2      ESF   Faces
EGADS    :      1     0     Yes     1     2        1   1 3
EGADS    :      2     0     Yes     1     3        1   1 6
EGADS    :      3     0     Yes     3     4        1   1 3
EGADS    :      4     0     Yes     2     4        1   1 2
EGADS    :      5     0     Yes     2     5        1   2 4
EGADS    :      6     0     Yes     4     6        1   2 4
EGADS    :      7     0     Yes     5     6        1   2 5
EGADS    :      8     0     Yes     3     1        1   3 8
EGADS    :      9     0     Yes     4     2        1   3 4
EGADS    :     10     0     Yes     6     5        1   4 5
EGADS    :     11     0     Yes     1     7        1   6 8
EGADS    :     12     0     Yes     3     8        1   6 8
EGADS    :     13     0     Yes     7     8        1   6 7
EGADS    :     14     0     Yes     7     9        1   7 9
EGADS    :     15     0     Yes     8    10        1   7 9
EGADS    :     16     0     Yes     9    10        1   7 10
EGADS    :     17     0     Yes     8     7        1   8 9
EGADS    :     18     0     Yes    10     9        1   9 10
EGADS    :     19     1     Yes    12    11       NA   11 13
EGADS    :     20     1     Yes    11    13       NA   11 16
EGADS    :     21     1     Yes    14    13       NA   11 14
EGADS    :     22     1     Yes    12    14       NA   11 15
EGADS    :     23     1     Yes    16    15       NA   12 13
EGADS    :     24     1     Yes    15    17       NA   12 16
EGADS    :     25     1     Yes    18    17       NA   12 14
EGADS    :     26     1     Yes    16    18       NA   12 15
EGADS    :     27     1     Yes    12    16       NA   13 15
EGADS    :     28     1     Yes    11    15       NA   13 16
EGADS    :     29     1     Yes    14    18       NA   14 15
EGADS    :     30     1     Yes    13    17       NA   14 16

EGADS    : Node Information

EGADS    :   Node  Active      Coordinates
EGADS    :      1     Yes       97.2007855                0                0
EGADS    :      2     Yes       97.9335611                0                0
EGADS    :      3     Yes               50                0                0
EGADS    :      4     Yes       75.3047874                0                0
EGADS    :      5     Yes       123.552357                0        4.7180639
EGADS    :      6     Yes       118.391317                0       3.99272703
EGADS    :      7     Yes       97.9335611       36.1389817                0
EGADS    :      8     Yes       75.3047874       36.1389817                0
EGADS    :      9     Yes       123.552357       97.6729236        4.7180639
EGADS    :     10     Yes       118.391317       97.6729236       3.99272703
EGADS    :     11     Yes                0                0       1951.57774
EGADS    :     12     Yes                0                0                0
EGADS    :     13     Yes                0       1953.45847       1951.57774
EGADS    :     14     Yes                0       1953.45847                0
EGADS    :     15     Yes       2040.21562                0       1951.57774
EGADS    :     16     Yes       2040.21562                0                0
EGADS    :     17     Yes       2040.21562       1953.45847       1951.57774
EGADS    :     18     Yes       2040.21562       1953.45847                0

EGADS    : Face and Edge Match Information

EGADS    : No Face Matches Found

AFLR4    : Surface Mesh Spacing Setup

AFLR4    : Max Bounding Box Length     = 3906.92
AFLR4    : Min Bounding Box Length     = 3906.92
AFLR4    : Max Ref Bounding Box Length = 195.346
AFLR4    : Min Ref Bounding Box Length = 13.1976
AFLR4    : Reference Length            = 21.7051
AFLR4    : BL Thickness                = 0
AFLR4    : FarField Spacing            = 530.302
AFLR4    : Abs Min Surf Spacing        = 0.0542627
AFLR4    : Min Surf Spacing            = 0.108525
AFLR4    : Max Surf Spacing            = 2.17051
AFLR4    : Global Scale Factor         = 1

AFLR4    : Geometry Definition Information

AFLR4    : Definition              Definition   Composite             Grid BC
AFLR4    :         ID                    Type          ID                Type
AFLR4    :          0     glue-only composite           -                   -
AFLR4    :          1            CAD geometry           0            STD w/BL
AFLR4    :          2            CAD geometry           0            STD w/BL
AFLR4    :          3            CAD geometry           0            STD w/BL
AFLR4    :          4            CAD geometry           0            STD w/BL
AFLR4    :          5            CAD geometry           0            STD w/BL
AFLR4    :          6            CAD geometry           0            STD w/BL
AFLR4    :          7            CAD geometry           0            STD w/BL
AFLR4    :          8            CAD geometry           0            STD w/BL
AFLR4    :          9            CAD geometry           0            STD w/BL
AFLR4    :         10            CAD geometry           0            STD w/BL
AFLR4    :         11            CAD geometry           0            FARFIELD
AFLR4    :         12            CAD geometry           0            FARFIELD
AFLR4    :         13            CAD geometry           0            FARFIELD
AFLR4    :         14            CAD geometry           0            FARFIELD
AFLR4    :         15            CAD geometry           0            FARFIELD
AFLR4    :         16            CAD geometry           0            FARFIELD

AFLR4    : Define CAD surface definition 1
AFLR4    : Define CAD surface definition 2
AFLR4    : Define CAD surface definition 3
AFLR4    : Define CAD surface definition 4
AFLR4    : Define CAD surface definition 5
AFLR4    : Define CAD surface definition 6
AFLR4    : Define CAD surface definition 7
AFLR4    : Define CAD surface definition 8
AFLR4    : Define CAD surface definition 9
AFLR4    : Define CAD surface definition 10
AFLR4    : Define CAD surface definition 11
AFLR4    : Define CAD surface definition 12
AFLR4    : Define CAD surface definition 13
AFLR4    : Define CAD surface definition 14
AFLR4    : Define CAD surface definition 15
AFLR4    : Define CAD surface definition 16

AFLR4    : Surface Grid Generation

AFLR4    : Generate optimal mesh on surface definition 1
AFLR2    : Nodes, Trias,Quads=      9007     17500         0
AFLR4    : Nodes, Trias,Quads=      5492     10470         0

AFLR4    : Generate optimal mesh on surface definition 2
AFLR2    : Nodes, Trias,Quads=     19258     37712         0
AFLR4    : Nodes, Trias,Quads=      6995     13186         0

AFLR4    : Generate optimal mesh on surface definition 3
AFLR2    : Nodes, Trias,Quads=     10154     19797         0
AFLR4    : Nodes, Trias,Quads=      5055      9599         0

AFLR4    : Generate optimal mesh on surface definition 4
AFLR2    : Nodes, Trias,Quads=     16967     33133         0
AFLR4    : Nodes, Trias,Quads=      6575     12349         0

AFLR4    : Generate optimal mesh on surface definition 5
AFLR2    : Nodes, Trias,Quads=        55        71         0
AFLR4    : Nodes, Trias,Quads=        46        53         0

AFLR4    : Generate optimal mesh on surface definition 6
AFLR2    : Nodes, Trias,Quads=      8983     17452         0
AFLR4    : Nodes, Trias,Quads=      5519     10524         0

AFLR4    : Generate optimal mesh on surface definition 7
AFLR2    : Nodes, Trias,Quads=     17854     34904         0
AFLR4    : Nodes, Trias,Quads=      7001     13198         0

AFLR4    : Generate optimal mesh on surface definition 8
AFLR2    : Nodes, Trias,Quads=      8865     17219         0
AFLR4    : Nodes, Trias,Quads=      5045      9579         0

AFLR4    : Generate optimal mesh on surface definition 9
AFLR2    : Nodes, Trias,Quads=     16322     31843         0
AFLR4    : Nodes, Trias,Quads=      6569     12337         0

AFLR4    : Generate optimal mesh on surface definition 10
AFLR2    : Nodes, Trias,Quads=        55        71         0
AFLR4    : Nodes, Trias,Quads=        46        53         0

AFLR4    : Generate optimal mesh on surface definition 11
AFLR2    : Nodes, Trias,Quads=        73       116         0
AFLR4    : Nodes, Trias,Quads=        68       106         0

AFLR4    : Generate optimal mesh on surface definition 12
AFLR2    : Nodes, Trias,Quads=        73       116         0
AFLR4    : Nodes, Trias,Quads=        68       106         0

AFLR4    : Generate optimal mesh on surface definition 13
AFLR2    : Nodes, Trias,Quads=        73       116         0
AFLR4    : Nodes, Trias,Quads=        68       106         0

AFLR4    : Generate optimal mesh on surface definition 14
AFLR2    : Nodes, Trias,Quads=        73       116         0
AFLR4    : Nodes, Trias,Quads=        68       106         0

AFLR4    : Generate optimal mesh on surface definition 15
AFLR2    : Nodes, Trias,Quads=        73       116         0
AFLR4    : Nodes, Trias,Quads=        68       106         0

AFLR4    : Generate optimal mesh on surface definition 16
AFLR2    : Nodes, Trias,Quads=        73       116         0
AFLR4    : Nodes, Trias,Quads=        68       106         0

DGEOM    : Add surface definitions to composite definition 0
DGEOM    : Glue composite surface definition 0
DGEOM    : Nodes,Faces,BEdges=     45996     91984      5486

AFLR4    : Curvature BG Surface Grid Generation

AFLR4    : Nodes, Faces      =     45996     91984

AFLR4    : Surface Grid Generation

AFLR4    : Generate optimal mesh on surface definition 1
AFLR2    : Nodes, Trias,Quads=     13047     25194         0
AFLR4    : Nodes, Trias,Quads=     11649     22398         0

AFLR4    : Generate optimal mesh on surface definition 2
AFLR2    : Nodes, Trias,Quads=     27646     53873         0
AFLR4    : Nodes, Trias,Quads=     17620     33821         0

AFLR4    : Generate optimal mesh on surface definition 3
AFLR2    : Nodes, Trias,Quads=     12513     24157         0
AFLR4    : Nodes, Trias,Quads=     11328     21787         0

AFLR4    : Generate optimal mesh on surface definition 4
AFLR2    : Nodes, Trias,Quads=     27612     53806         0
AFLR4    : Nodes, Trias,Quads=     17068     32718         0

AFLR4    : Generate optimal mesh on surface definition 5
AFLR2    : Nodes, Trias,Quads=       200       300         0
AFLR4    : Nodes, Trias,Quads=       186       272         0

AFLR4    : Generate optimal mesh on surface definition 6
AFLR2    : Nodes, Trias,Quads=     13070     25240         0
AFLR4    : Nodes, Trias,Quads=     11568     22236         0

AFLR4    : Generate optimal mesh on surface definition 7
AFLR2    : Nodes, Trias,Quads=     27812     54205         0
AFLR4    : Nodes, Trias,Quads=     17650     33881         0

AFLR4    : Generate optimal mesh on surface definition 8
AFLR2    : Nodes, Trias,Quads=     12528     24187         0
AFLR4    : Nodes, Trias,Quads=     11340     21811         0

AFLR4    : Generate optimal mesh on surface definition 9
AFLR2    : Nodes, Trias,Quads=     27858     54298         0
AFLR4    : Nodes, Trias,Quads=     17112     32806         0

AFLR4    : Generate optimal mesh on surface definition 10
AFLR2    : Nodes, Trias,Quads=       200       300         0
AFLR4    : Nodes, Trias,Quads=       186       272         0

AFLR4    : Generate optimal mesh on surface definition 11
AFLR2    : Nodes, Trias,Quads=        73       116         0
AFLR4    : Nodes, Trias,Quads=        68       106         0

AFLR4    : Generate optimal mesh on surface definition 12
AFLR2    : Nodes, Trias,Quads=        73       116         0
AFLR4    : Nodes, Trias,Quads=        68       106         0

AFLR4    : Generate optimal mesh on surface definition 13
AFLR2    : Nodes, Trias,Quads=        73       116         0
AFLR4    : Nodes, Trias,Quads=        68       106         0

AFLR4    : Generate optimal mesh on surface definition 14
AFLR2    : Nodes, Trias,Quads=        73       116         0
AFLR4    : Nodes, Trias,Quads=        68       106         0

AFLR4    : Generate optimal mesh on surface definition 15
AFLR2    : Nodes, Trias,Quads=        73       116         0
AFLR4    : Nodes, Trias,Quads=        68       106         0

AFLR4    : Generate optimal mesh on surface definition 16
AFLR2    : Nodes, Trias,Quads=        73       116         0
AFLR4    : Nodes, Trias,Quads=        68       106         0

DGEOM    : Add surface definitions to composite definition 0
DGEOM    : Glue composite surface definition 0
DGEOM    : Nodes,Faces,BEdges=    111323    222638      9560

OVERALL  : CPU Time          =     1.725   seconds
Body 1 (of 2)
Number of nodes    = 111003
Number of elements = 222002
Number of triangle elements      = 222002
Number of quadrilateral elements = 0
Body 2 (of 2)
Number of nodes    = 320
Number of elements = 636
Number of triangle elements      = 636
Number of quadrilateral elements = 0
----------------------------
Total number of nodes    = 111323
Total number of elements = 222638
Total number of triangle elements      = 222638
Total number of quadrilateral elements = 0

Getting mesh sizing parameters
	Mesh sizing name - Farfield
	Mesh sizing name - leftWing
	Mesh sizing name - riteWing
	Done getting mesh sizing parameters

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.8.1
EGADS    : ---------------------------------------

EGADS    : EGADS CAD Geometry Setup

EGADS    : Model has 2 Active Bodies

EGADS    : Body 0 is a SolidBody
EGADS    : Body 0 has 1 Shells
EGADS    : Body 0 has 10 Faces
EGADS    : Body 0 has 18 Edges
EGADS    : Body 0 has 10 Loops
EGADS    : Body 0 has 10 Nodes
EGADS    : Body 1 is a SolidBody
EGADS    : Body 1 has 1 Shells
EGADS    : Body 1 has 6 Faces
EGADS    : Body 1 has 12 Edges
EGADS    : Body 1 has 6 Loops
EGADS    : Body 1 has 8 Nodes

EGADS    : Check Grid BCs

EGADS    : Grid BCs are OK

EGADS    : Face Neighbor-Faces Information

EGADS    : QC  = Face Quad Combination Flag
EGADS    : IER = Face Isolated Edge Refinement Flag
EGADS    : ER  = Face Edge Refinement Factor
EGADS    :       Not applicable for Faces with a FarField Grid BC.
EGADS    : SF  = Face Scale Factor
EGADS    :       Not applicable for Faces with a FarField Grid BC.

EGADS    :   Face          Body    QC   IER       ER    Scale   Neighbor
EGADS    :     ID  Active    ID  Flag  Flag   Weight   Factor   Faces
EGADS    :      1     Yes     0     0     1        1        1   2 3 6
EGADS    :      2     Yes     0     0     1        1        1   1 4 5
EGADS    :      3     Yes     0     0     1        1        1   1 4 8
EGADS    :      4     Yes     0     0     1        1        1   2 3 5
EGADS    :      5     Yes     0     0     1        1        1   2 4
EGADS    :      6     Yes     0     0     1        1        1   1 7 8
EGADS    :      7     Yes     0     0     1        1        1   6 9 10
EGADS    :      8     Yes     0     0     1        1        1   3 6 9
EGADS    :      9     Yes     0     0     1        1        1   7 8 10
EGADS    :     10     Yes     0     0     1        1        1   7 9
EGADS    :     11     Yes     1     0     1       NA       NA   13 14 15 16
EGADS    :     12     Yes     1     0     1       NA       NA   13 14 15 16
EGADS    :     13     Yes     1     0     1       NA       NA   11 12 15 16
EGADS    :     14     Yes     1     0     1       NA       NA   11 12 15 16
EGADS    :     15     Yes     1     0     1       NA       NA   11 12 13 14
EGADS    :     16     Yes     1     0     1       NA       NA   11 12 13 14

EGADS    : Face Edges Information

EGADS    :   Face   Edges
EGADS    :      1   -1 2 3 -4
EGADS    :      2   -5 4 6 -7
EGADS    :      3   -3 8 1 -9
EGADS    :      4   -6 9 5 -10
EGADS    :      5   7 10
EGADS    :      6   11 13 -12 -2
EGADS    :      7   14 16 -15 -13
EGADS    :      8   12 17 -11 -8
EGADS    :      9   15 18 -14 -17
EGADS    :     10   -16 -18
EGADS    :     11   19 20 -21 -22
EGADS    :     12   -23 26 25 -24
EGADS    :     13   27 23 -28 -19
EGADS    :     14   -29 21 30 -25
EGADS    :     15   22 29 -26 -27
EGADS    :     16   -20 28 24 -30

EGADS    : Face Loops Information

EGADS    :   Face   Loops
EGADS    :      1   1
EGADS    :      2   2
EGADS    :      3   3
EGADS    :      4   4
EGADS    :      5   5
EGADS    :      6   6
EGADS    :      7   7
EGADS    :      8   8
EGADS    :      9   9
EGADS    :     10   10
EGADS    :     11   11
EGADS    :     12   12
EGADS    :     13   13
EGADS    :     14   14
EGADS    :     15   15
EGADS    :     16   16

EGADS    : Loop Edges Information

EGADS    :   Loop  Active   Edges
EGADS    :      1     Yes   -1 2 3 -4
EGADS    :      2     Yes   -5 4 6 -7
EGADS    :      3     Yes   -3 8 1 -9
EGADS    :      4     Yes   -6 9 5 -10
EGADS    :      5     Yes   7 10
EGADS    :      6     Yes   11 13 -12 -2
EGADS    :      7     Yes   14 16 -15 -13
EGADS    :      8     Yes   12 17 -11 -8
EGADS    :      9     Yes   15 18 -14 -17
EGADS    :     10     Yes   -16 -18
EGADS    :     11     Yes   19 20 -21 -22
EGADS    :     12     Yes   -23 26 25 -24
EGADS    :     13     Yes   27 23 -28 -19
EGADS    :     14     Yes   -29 21 30 -25
EGADS    :     15     Yes   22 29 -26 -27
EGADS    :     16     Yes   -20 28 24 -30

EGADS    : Edge Node, Scale Factor, and Neighbor-Faces Information

EGADS    : ESF = Edge Scale Factor
EGADS    :       Not applicable for DEGENERATE Edges or Edges with a FarField
EGADS    :       Grid BC Neighbor Face.

EGADS    :                                             Neighbor
EGADS    :   Edge  Body  Active Node1 Node2      ESF   Faces
EGADS    :      1     0     Yes     1     2        1   1 3
EGADS    :      2     0     Yes     1     3        1   1 6
EGADS    :      3     0     Yes     3     4        1   1 3
EGADS    :      4     0     Yes     2     4        1   1 2
EGADS    :      5     0     Yes     2     5        1   2 4
EGADS    :      6     0     Yes     4     6        1   2 4
EGADS    :      7     0     Yes     5     6        1   2 5
EGADS    :      8     0     Yes     3     1        1   3 8
EGADS    :      9     0     Yes     4     2        1   3 4
EGADS    :     10     0     Yes     6     5        1   4 5
EGADS    :     11     0     Yes     1     7        1   6 8
EGADS    :     12     0     Yes     3     8        1   6 8
EGADS    :     13     0     Yes     7     8        1   6 7
EGADS    :     14     0     Yes     7     9        1   7 9
EGADS    :     15     0     Yes     8    10        1   7 9
EGADS    :     16     0     Yes     9    10        1   7 10
EGADS    :     17     0     Yes     8     7        1   8 9
EGADS    :     18     0     Yes    10     9        1   9 10
EGADS    :     19     1     Yes    12    11       NA   11 13
EGADS    :     20     1     Yes    11    13       NA   11 16
EGADS    :     21     1     Yes    14    13       NA   11 14
EGADS    :     22     1     Yes    12    14       NA   11 15
EGADS    :     23     1     Yes    16    15       NA   12 13
EGADS    :     24     1     Yes    15    17       NA   12 16
EGADS    :     25     1     Yes    18    17       NA   12 14
EGADS    :     26     1     Yes    16    18       NA   12 15
EGADS    :     27     1     Yes    12    16       NA   13 15
EGADS    :     28     1     Yes    11    15       NA   13 16
EGADS    :     29     1     Yes    14    18       NA   14 15
EGADS    :     30     1     Yes    13    17       NA   14 16

EGADS    : Node Information

EGADS    :   Node  Active      Coordinates
EGADS    :      1     Yes       97.2007855                0                0
EGADS    :      2     Yes       97.9335611                0                0
EGADS    :      3     Yes               50                0                0
EGADS    :      4     Yes       75.3047874                0                0
EGADS    :      5     Yes       123.552357                0        4.7180639
EGADS    :      6     Yes       118.391317                0       3.99272703
EGADS    :      7     Yes       97.9335611       36.1389817                0
EGADS    :      8     Yes       75.3047874       36.1389817                0
EGADS    :      9     Yes       123.552357       97.6729236        4.7180639
EGADS    :     10     Yes       118.391317       97.6729236       3.99272703
EGADS    :     11     Yes                0                0       1951.57774
EGADS    :     12     Yes                0                0                0
EGADS    :     13     Yes                0       1953.45847       1951.57774
EGADS    :     14     Yes                0       1953.45847                0
EGADS    :     15     Yes       2040.21562                0       1951.57774
EGADS    :     16     Yes       2040.21562                0                0
EGADS    :     17     Yes       2040.21562       1953.45847       1951.57774
EGADS    :     18     Yes       2040.21562       1953.45847                0

EGADS    : Face and Edge Match Information

EGADS    : No Face Matches Found

AFLR4    : Surface Mesh Spacing Setup

AFLR4    : Max Bounding Box Length     = 3906.92
AFLR4    : Min Bounding Box Length     = 3906.92
AFLR4    : Max Ref Bounding Box Length = 195.346
AFLR4    : Min Ref Bounding Box Length = 13.1976
AFLR4    : Reference Length            = 21.7051
AFLR4    : BL Thickness                = 0
AFLR4    : FarField Spacing            = 530.302
AFLR4    : Abs Min Surf Spacing        = 0.0542627
AFLR4    : Min Surf Spacing            = 0.108525
AFLR4    : Max Surf Spacing            = 2.17051
AFLR4    : Global Scale Factor         = 1

AFLR4    : Geometry Definition Information

AFLR4    : Definition              Definition   Composite             Grid BC
AFLR4    :         ID                    Type          ID                Type
AFLR4    :          0     glue-only composite           -                   -
AFLR4    :          1            CAD geometry           0            STD w/BL
AFLR4    :          2            CAD geometry           0            STD w/BL
AFLR4    :          3            CAD geometry           0            STD w/BL
AFLR4    :          4            CAD geometry           0            STD w/BL
AFLR4    :          5            CAD geometry           0            STD w/BL
AFLR4    :          6            CAD geometry           0            STD w/BL
AFLR4    :          7            CAD geometry           0            STD w/BL
AFLR4    :          8            CAD geometry           0            STD w/BL
AFLR4    :          9            CAD geometry           0            STD w/BL
AFLR4    :         10            CAD geometry           0            STD w/BL
AFLR4    :         11            CAD geometry           0            FARFIELD
AFLR4    :         12            CAD geometry           0            FARFIELD
AFLR4    :         13            CAD geometry           0            FARFIELD
AFLR4    :         14            CAD geometry           0            FARFIELD
AFLR4    :         15            CAD geometry           0            FARFIELD
AFLR4    :         16            CAD geometry           0            FARFIELD

AFLR4    : Define CAD surface definition 1
AFLR4    : Define CAD surface definition 2
AFLR4    : Define CAD surface definition 3
AFLR4    : Define CAD surface definition 4
AFLR4    : Define CAD surface definition 5
AFLR4    : Define CAD surface definition 6
AFLR4    : Define CAD surface definition 7
AFLR4    : Define CAD surface definition 8
AFLR4    : Define CAD surface definition 9
AFLR4    : Define CAD surface definition 10
AFLR4    : Define CAD surface definition 11
AFLR4    : Define CAD surface definition 12
AFLR4    : Define CAD surface definition 13
AFLR4    : Define CAD surface definition 14
AFLR4    : Define CAD surface definition 15
AFLR4    : Define CAD surface definition 16

AFLR4    : Surface Grid Generation

AFLR4    : Generate optimal mesh on surface definition 1
AFLR2    : Nodes, Trias,Quads=      8732     16959         0
AFLR4    : Nodes, Trias,Quads=      5233      9961         0

AFLR4    : Generate optimal mesh on surface definition 2
AFLR2    : Nodes, Trias,Quads=     18087     35388         0
AFLR4    : Nodes, Trias,Quads=      5569     10352         0

AFLR4    : Generate optimal mesh on surface definition 3
AFLR2    : Nodes, Trias,Quads=     10182     19859         0
AFLR4    : Nodes, Trias,Quads=      4951      9397         0

AFLR4    : Generate optimal mesh on surface definition 4
AFLR2    : Nodes, Trias,Quads=     16336     31887         0
AFLR4    : Nodes, Trias,Quads=      5435     10085         0

AFLR4    : Generate optimal mesh on surface definition 5
AFLR2    : Nodes, Trias,Quads=        55        71         0
AFLR4    : Nodes, Trias,Quads=        45        51         0

AFLR4    : Generate optimal mesh on surface definition 6
AFLR2    : Nodes, Trias,Quads=      8705     16905         0
AFLR4    : Nodes, Trias,Quads=      5312     10119         0

AFLR4    : Generate optimal mesh on surface definition 7
AFLR2    : Nodes, Trias,Quads=     17908     35030         0
AFLR4    : Nodes, Trias,Quads=      5567     10348         0

AFLR4    : Generate optimal mesh on surface definition 8
AFLR2    : Nodes, Trias,Quads=      8823     17141         0
AFLR4    : Nodes, Trias,Quads=      4980      9455         0

AFLR4    : Generate optimal mesh on surface definition 9
AFLR2    : Nodes, Trias,Quads=     16876     32967         0
AFLR4    : Nodes, Trias,Quads=      5357      9929         0

AFLR4    : Generate optimal mesh on surface definition 10
AFLR2    : Nodes, Trias,Quads=        55        71         0
AFLR4    : Nodes, Trias,Quads=        46        53         0

AFLR4    : Generate optimal mesh on surface definition 11
AFLR2    : Nodes, Trias,Quads=        73       116         0
AFLR4    : Nodes, Trias,Quads=        68       106         0

AFLR4    : Generate optimal mesh on surface definition 12
AFLR2    : Nodes, Trias,Quads=        73       116         0
AFLR4    : Nodes, Trias,Quads=        68       106         0

AFLR4    : Generate optimal mesh on surface definition 13
AFLR2    : Nodes, Trias,Quads=        73       116         0
AFLR4    : Nodes, Trias,Quads=        68       106         0

AFLR4    : Generate optimal mesh on surface definition 14
AFLR2    : Nodes, Trias,Quads=        73       116         0
AFLR4    : Nodes, Trias,Quads=        68       106         0

AFLR4    : Generate optimal mesh on surface definition 15
AFLR2    : Nodes, Trias,Quads=        73       116         0
AFLR4    : Nodes, Trias,Quads=        68       106         0

AFLR4    : Generate optimal mesh on surface definition 16
AFLR2    : Nodes, Trias,Quads=        73       116         0
AFLR4    : Nodes, Trias,Quads=        68       106         0

DGEOM    : Add surface definitions to composite definition 0
DGEOM    : Glue composite surface definition 0
DGEOM    : Nodes,Faces,BEdges=     40197     80386      5388

AFLR4    : Curvature BG Surface Grid Generation

AFLR4    : Nodes, Faces      =     40197     80386

AFLR4    : Surface Grid Generation

AFLR4    : Generate optimal mesh on surface definition 1
AFLR2    : Nodes, Trias,Quads=     13069     25242         0
AFLR4    : Nodes, Trias,Quads=      9852     18808         0

AFLR4    : Generate optimal mesh on surface definition 2
AFLR2    : Nodes, Trias,Quads=     26888     52364         0
AFLR4    : Nodes, Trias,Quads=     15212     29012         0

AFLR4    : Generate optimal mesh on surface definition 3
AFLR2    : Nodes, Trias,Quads=     12381     23898         0
AFLR4    : Nodes, Trias,Quads=      9776     18688         0

AFLR4    : Generate optimal mesh on surface definition 4
AFLR2    : Nodes, Trias,Quads=     27058     52705         0
AFLR4    : Nodes, Trias,Quads=     15006     28601         0

AFLR4    : Generate optimal mesh on surface definition 5
AFLR2    : Nodes, Trias,Quads=       200       300         0
AFLR4    : Nodes, Trias,Quads=       186       272         0

AFLR4    : Generate optimal mesh on surface definition 6
AFLR2    : Nodes, Trias,Quads=     12940     24984         0
AFLR4    : Nodes, Trias,Quads=      9917     18938         0

AFLR4    : Generate optimal mesh on surface definition 7
AFLR2    : Nodes, Trias,Quads=     27325     53238         0
AFLR4    : Nodes, Trias,Quads=     15148     28884         0

AFLR4    : Generate optimal mesh on surface definition 8
AFLR2    : Nodes, Trias,Quads=     12423     23982         0
AFLR4    : Nodes, Trias,Quads=      9812     18760         0

AFLR4    : Generate optimal mesh on surface definition 9
AFLR2    : Nodes, Trias,Quads=     27246     53081         0
AFLR4    : Nodes, Trias,Quads=     15188     28965         0

AFLR4    : Generate optimal mesh on surface definition 10
AFLR2    : Nodes, Trias,Quads=       200       300         0
AFLR4    : Nodes, Trias,Quads=       186       272         0

AFLR4    : Generate optimal mesh on surface definition 11
AFLR2    : Nodes, Trias,Quads=        73       116         0
AFLR4    : Nodes, Trias,Quads=        68       106         0

AFLR4    : Generate optimal mesh on surface definition 12
AFLR2    : Nodes, Trias,Quads=        73       116         0
AFLR4    : Nodes, Trias,Quads=        68       106         0

AFLR4    : Generate optimal mesh on surface definition 13
AFLR2    : Nodes, Trias,Quads=        73       116         0
AFLR4    : Nodes, Trias,Quads=        68       106         0

AFLR4    : Generate optimal mesh on surface definition 14
AFLR2    : Nodes, Trias,Quads=        73       116         0
AFLR4    : Nodes, Trias,Quads=        68       106         0

AFLR4    : Generate optimal mesh on surface definition 15
AFLR2    : Nodes, Trias,Quads=        73       116         0
AFLR4    : Nodes, Trias,Quads=        68       106         0

AFLR4    : Generate optimal mesh on surface definition 16
AFLR2    : Nodes, Trias,Quads=        73       116         0
AFLR4    : Nodes, Trias,Quads=        68       106         0

DGEOM    : Add surface definitions to composite definition 0
DGEOM    : Glue composite surface definition 0
DGEOM    : Nodes,Faces,BEdges=     95922    191836      9514

OVERALL  : CPU Time          =     1.569   seconds
Body 1 (of 2)
Number of nodes    = 95602
Number of elements = 191200
Number of triangle elements      = 191200
Number of quadrilateral elements = 0
Body 2 (of 2)
Number of nodes    = 320
Number of elements = 636
Number of triangle elements      = 636
Number of quadrilateral elements = 0
----------------------------
Total number of nodes    = 95922
Total number of elements = 191836
Total number of triangle elements      = 191836
Total number of quadrilateral elements = 0

real	0m21.746s
user	0m21.294s
sys	0m0.678s
+ status=0
+ set +x

=================================================
solutions/session07/aflr4_curv_factor.py passed (as expected)
=================================================


=================================================
aflr4_InviscidTransport.py test;
+ python aflr4_InviscidTransport.py
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/CAPS/training/2023/training.log

MESSAGE:: Building wingOml


MESSAGE:: Building pylonOml


MESSAGE:: Building nacelleOml


MESSAGE:: Building htailOml


MESSAGE:: Building vtailOml


MESSAGE:: Building fuseOml

Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 7
	Name = Fuselage, index = 1
	Name = Wing, index = 2
	Name = Htail, index = 3
	Name = Pylon, index = 4
	Name = Vtail, index = 5
	Name = Nacelle, index = 6
	Name = Farfield, index = 7
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 8
	Name = Fuselage, index = 1
	Name = riteWing, index = 2
	Name = leftWing, index = 3
	Name = Htail, index = 4
	Name = Pylon, index = 5
	Name = Vtail, index = 6
	Name = Nacelle, index = 7
	Name = Farfield, index = 8

Getting mesh sizing parameters
	Mesh sizing name - Farfield
	Mesh sizing name - Fuselage
	Mesh sizing name - Htail
	Mesh sizing name - Pylon
	Mesh sizing name - Vtail
	Mesh sizing name - leftWing
	Mesh sizing name - riteWing
	Done getting mesh sizing parameters
 
AFLR2    : ---------------------------------------
AFLR2    : AFLR2 LIBRARY
AFLR2    : ADVANCING-FRONT/LOCAL-RECONNECTION
AFLR2    : TRIA/QUAD GRID GENERATOR
AFLR2    : Version Number 9.18.1
AFLR2    : Version Date   06/11/24 @ 05:52PM
AFLR2    : Compile OS     Darwin 23.5.0 arm64
AFLR2    : Compile Date   06/11/24 @ 05:52PM
AFLR2    : Copyright 1994-2021, D.L. Marcum
AFLR2    : ---------------------------------------
 
AFLR4    : ---------------------------------------
AFLR4    : AFLR4 LIBRARY
AFLR4    : ADVANCING-FRONT/LOCAL-RECONNECTION
AFLR4    : TRIA/QUAD SURFACE GRID GENERATOR
AFLR4    : Version Number 11.5.15
AFLR4    : Version Date   07/19/24 @ 07:04PM
AFLR4    : Compile OS     Darwin 23.5.0 arm64
AFLR4    : Compile Date   07/19/24 @ 07:06PM
AFLR4    : Copyright 1994-2021, D.L. Marcum
AFLR4    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.8.1
EGADS    : ---------------------------------------

EGADS    : EGADS CAD Geometry Setup

EGADS    : Model has 2 Active Bodies

EGADS    : Body 0 is a SolidBody
EGADS    : Body 0 has 1 Shells
EGADS    : Body 0 has 40 Faces
EGADS    : Body 0 has 95 Edges
EGADS    : Body 0 has 44 Loops
EGADS    : Body 0 has 53 Nodes
EGADS    : Body 1 is a SolidBody
EGADS    : Body 1 has 1 Shells
EGADS    : Body 1 has 6 Faces
EGADS    : Body 1 has 12 Edges
EGADS    : Body 1 has 6 Loops
EGADS    : Body 1 has 8 Nodes

EGADS    : Check Grid BCs

EGADS    : Grid BCs are OK

EGADS    : Face Neighbor-Faces Information

EGADS    : QC  = Face Quad Combination Flag
EGADS    : IER = Face Isolated Edge Refinement Flag
EGADS    : ER  = Face Edge Refinement Factor
EGADS    :       Not applicable for Faces with a FarField Grid BC.
EGADS    : SF  = Face Scale Factor
EGADS    :       Not applicable for Faces with a FarField Grid BC.

EGADS    :   Face          Body    QC   IER       ER    Scale   Neighbor
EGADS    :     ID  Active    ID  Flag  Flag   Weight   Factor   Faces
EGADS    :      1     Yes     0     0     1        0        4   2 3 4 5 6
EGADS    :      2     Yes     0     0     1        0        4   1 7 8 9 10
EGADS    :      3     Yes     0     0     1        0        4   1 8 11 12 13 14
EGADS    :      4     Yes     0     0     1        0        4   1 7 12
EGADS    :      5     Yes     0     0     1        0        4   1 6 15
EGADS    :      6     Yes     0     0     1        0        4   1 5 16 17 18
EGADS    :      7     Yes     0     0     1        0        4   2 4 19
EGADS    :      8     Yes     0     0     1        0        4   2 3 11 19 20 21
EGADS    :      9     Yes     0     0     1        0        4   2 10 22 23 24
EGADS    :     10     Yes     0     0     1        0        4   2 9 25
EGADS    :     11     Yes     0     0     1        0        4   3 8 12 19
EGADS    :     12     Yes     0     0     1        0        4   3 4 11 13 14 19
EGADS    :                                                      26
EGADS    :     13     Yes     0     0     1        0        4   3 12 14 27
EGADS    :     14     Yes     0     0     1        0        4   3 12 13 27
EGADS    :     15     Yes     0     0     1        0        4   5 16 28
EGADS    :     16     Yes     0     0     1        0        4   6 15 28
EGADS    :     17     Yes     0     0     1        0        1   6 18 29
EGADS    :     18     Yes     0     0     1        0        1   6 17 30
EGADS    :     19     Yes     0     0     1        0        4   7 8 11 12 20 21
EGADS    :                                                      31
EGADS    :     20     Yes     0     0     1        0        4   8 19 21 32
EGADS    :     21     Yes     0     0     1        0        4   8 19 20 32
EGADS    :     22     Yes     0     0     1        0        4   9 25 33
EGADS    :     23     Yes     0     0     1        0        1   9 24 34
EGADS    :     24     Yes     0     0     1        0        1   9 23 35
EGADS    :     25     Yes     0     0     1        0        4   10 22 33
EGADS    :     26     Yes     0     0     1        0        4   12 31 36
EGADS    :     27     Yes     0     0     1        0        4   13 14
EGADS    :     28     Yes     0     0     1        0        4   15 16
EGADS    :     29     Yes     0     0     1        0        1   17 30 37
EGADS    :     30     Yes     0     0     1        0        1   18 29 38
EGADS    :     31     Yes     0     0     1        0        4   19 26 36
EGADS    :     32     Yes     0     0     1        0        4   20 21
EGADS    :     33     Yes     0     0     1        0        4   22 25
EGADS    :     34     Yes     0     0     1        0        1   23 35 39
EGADS    :     35     Yes     0     0     1        0        1   24 34 40
EGADS    :     36     Yes     0     0     1        0        4   26 31
EGADS    :     37     Yes     0     0     1        0        1   29 38
EGADS    :     38     Yes     0     0     1        0        1   30 37
EGADS    :     39     Yes     0     0     1        0        1   34 40
EGADS    :     40     Yes     0     0     1        0        1   35 39
EGADS    :     41     Yes     1     0     1       NA       NA   43 44 45 46
EGADS    :     42     Yes     1     0     1       NA       NA   43 44 45 46
EGADS    :     43     Yes     1     0     1       NA       NA   41 42 45 46
EGADS    :     44     Yes     1     0     1       NA       NA   41 42 45 46
EGADS    :     45     Yes     1     0     1       NA       NA   41 42 43 44
EGADS    :     46     Yes     1     0     1       NA       NA   41 42 43 44

EGADS    : Face Edges Information

EGADS    :   Face   Edges
EGADS    :      1   -1 4 3 -2 -5 -6
EGADS    :      2   -7 9 1 -8 10 11
EGADS    :      3   -12 2 17 -16 -15 14 -13
EGADS    :      4   -3 18 19 -20
EGADS    :      5   21 22 -23 5
EGADS    :      6   23 24 -21 6 25 26
EGADS    :      7   -19 27 7 -28
EGADS    :      8   -29 8 12 -33 -32 31 30
EGADS    :      9   -34 -10 36 -35 37 38
EGADS    :     10   -36 -11 34 -39
EGADS    :     11   13 40 41 33
EGADS    :     12   -17 20 46 45 44 -40 -14 -43 -42
EGADS    :     13   47 48 -49 43 15
EGADS    :     14   49 50 -47 16 42
EGADS    :     15   51 53 -52 -22
EGADS    :     16   52 54 -51 -24
EGADS    :     17   -55 57 -25 -56
EGADS    :     18   -57 58 56 -26
EGADS    :     19   -46 28 29 61 60 32 -41 -44 59
EGADS    :     20   -62 -61 -30 64 -63
EGADS    :     21   -64 -31 -60 62 -65
EGADS    :     22   -66 35 67 -68
EGADS    :     23   69 70 -37 -71
EGADS    :     24   71 -38 -70 -72
EGADS    :     25   -67 39 66 -73
EGADS    :     26   -74 -45 76 -75
EGADS    :     27   -48 -50
EGADS    :     28   -53 -54
EGADS    :     29   77 55 78 79 -80 -81
EGADS    :     30   -77 83 80 -82 -78 -58
EGADS    :     31   -76 -59 74 -84
EGADS    :     32   65 63
EGADS    :     33   73 68
EGADS    :     34   85 -69 86 87 -88 -89
EGADS    :     35   -85 91 88 -90 -86 72
EGADS    :     36   75 84
EGADS    :     37   -79 92 81 -93
EGADS    :     38   82 93 -83 -92
EGADS    :     39   -87 94 89 -95
EGADS    :     40   90 95 -91 -94
EGADS    :     41   96 97 -98 -99
EGADS    :     42   -100 103 102 -101
EGADS    :     43   104 100 -105 -96
EGADS    :     44   -106 98 107 -102
EGADS    :     45   99 106 -103 -104
EGADS    :     46   -97 105 101 -107

EGADS    : Face Loops Information

EGADS    :   Face   Loops
EGADS    :      1   1 2
EGADS    :      2   3 4
EGADS    :      3   5
EGADS    :      4   6
EGADS    :      5   7
EGADS    :      6   8 9
EGADS    :      7   10
EGADS    :      8   11
EGADS    :      9   12 13
EGADS    :     10   14
EGADS    :     11   15
EGADS    :     12   16
EGADS    :     13   17
EGADS    :     14   18
EGADS    :     15   19
EGADS    :     16   20
EGADS    :     17   21
EGADS    :     18   22
EGADS    :     19   23
EGADS    :     20   24
EGADS    :     21   25
EGADS    :     22   26
EGADS    :     23   27
EGADS    :     24   28
EGADS    :     25   29
EGADS    :     26   30
EGADS    :     27   31
EGADS    :     28   32
EGADS    :     29   33
EGADS    :     30   34
EGADS    :     31   35
EGADS    :     32   36
EGADS    :     33   37
EGADS    :     34   38
EGADS    :     35   39
EGADS    :     36   40
EGADS    :     37   41
EGADS    :     38   42
EGADS    :     39   43
EGADS    :     40   44
EGADS    :     41   45
EGADS    :     42   46
EGADS    :     43   47
EGADS    :     44   48
EGADS    :     45   49
EGADS    :     46   50

EGADS    : Loop Edges Information

EGADS    :   Loop  Active   Edges
EGADS    :      1     Yes   -1 4 3 -2
EGADS    :      2     Yes   -5 -6
EGADS    :      3     Yes   -7 9 1 -8
EGADS    :      4     Yes   10 11
EGADS    :      5     Yes   -12 2 17 -16 -15 14 -13
EGADS    :      6     Yes   -3 18 19 -20
EGADS    :      7     Yes   21 22 -23 5
EGADS    :      8     Yes   23 24 -21 6
EGADS    :      9     Yes   25 26
EGADS    :     10     Yes   -19 27 7 -28
EGADS    :     11     Yes   -29 8 12 -33 -32 31 30
EGADS    :     12     Yes   -34 -10 36 -35
EGADS    :     13     Yes   37 38
EGADS    :     14     Yes   -36 -11 34 -39
EGADS    :     15     Yes   13 40 41 33
EGADS    :     16     Yes   -17 20 46 45 44 -40 -14 -43 -42
EGADS    :     17     Yes   47 48 -49 43 15
EGADS    :     18     Yes   49 50 -47 16 42
EGADS    :     19     Yes   51 53 -52 -22
EGADS    :     20     Yes   52 54 -51 -24
EGADS    :     21     Yes   -55 57 -25 -56
EGADS    :     22     Yes   -57 58 56 -26
EGADS    :     23     Yes   -46 28 29 61 60 32 -41 -44 59
EGADS    :     24     Yes   -62 -61 -30 64 -63
EGADS    :     25     Yes   -64 -31 -60 62 -65
EGADS    :     26     Yes   -66 35 67 -68
EGADS    :     27     Yes   69 70 -37 -71
EGADS    :     28     Yes   71 -38 -70 -72
EGADS    :     29     Yes   -67 39 66 -73
EGADS    :     30     Yes   -74 -45 76 -75
EGADS    :     31     Yes   -48 -50
EGADS    :     32     Yes   -53 -54
EGADS    :     33     Yes   77 55 78 79 -80 -81
EGADS    :     34     Yes   -77 83 80 -82 -78 -58
EGADS    :     35     Yes   -76 -59 74 -84
EGADS    :     36     Yes   65 63
EGADS    :     37     Yes   73 68
EGADS    :     38     Yes   85 -69 86 87 -88 -89
EGADS    :     39     Yes   -85 91 88 -90 -86 72
EGADS    :     40     Yes   75 84
EGADS    :     41     Yes   -79 92 81 -93
EGADS    :     42     Yes   82 93 -83 -92
EGADS    :     43     Yes   -87 94 89 -95
EGADS    :     44     Yes   90 95 -91 -94
EGADS    :     45     Yes   96 97 -98 -99
EGADS    :     46     Yes   -100 103 102 -101
EGADS    :     47     Yes   104 100 -105 -96
EGADS    :     48     Yes   -106 98 107 -102
EGADS    :     49     Yes   99 106 -103 -104
EGADS    :     50     Yes   -97 105 101 -107

EGADS    : Edge Node, Scale Factor, and Neighbor-Faces Information

EGADS    : ESF = Edge Scale Factor
EGADS    :       Not applicable for DEGENERATE Edges or Edges with a FarField
EGADS    :       Grid BC Neighbor Face.

EGADS    :                                             Neighbor
EGADS    :   Edge  Body  Active Node1 Node2      ESF   Faces
EGADS    :      1     0     Yes     1     2        1   1 2
EGADS    :      2     0     Yes     2     3        1   1 3
EGADS    :      3     0     Yes     1     3        1   1 4
EGADS    :      4     0   DEGEN     1     1        -   1
EGADS    :      5     0     Yes     4     5        1   1 5
EGADS    :      6     0     Yes     5     4        1   1 6
EGADS    :      7     0     Yes     1     6        1   2 7
EGADS    :      8     0     Yes     6     2        1   2 8
EGADS    :      9     0   DEGEN     1     1        -   2
EGADS    :     10     0     Yes     7     8        1   2 9
EGADS    :     11     0     Yes     8     7        1   2 10
EGADS    :     12     0     Yes     2     9        1   3 8
EGADS    :     13     0     Yes     9    10        1   3 11
EGADS    :     14     0     Yes    11    10        1   3 12
EGADS    :     15     0     Yes    11    12        1   3 13
EGADS    :     16     0     Yes    12    13        1   3 14
EGADS    :     17     0     Yes     3    13        1   3 12
EGADS    :     18     0   DEGEN     1     1        -   4
EGADS    :     19     0     Yes     1    14        1   4 7
EGADS    :     20     0     Yes     3    14        1   4 12
EGADS    :     21     0     Yes     5    15        1   5 6
EGADS    :     22     0     Yes    15    16        1   5 15
EGADS    :     23     0     Yes     4    16        1   5 6
EGADS    :     24     0     Yes    16    15        1   6 16
EGADS    :     25     0     Yes    17    18        1   6 17
EGADS    :     26     0     Yes    18    17        1   6 18
EGADS    :     27     0   DEGEN     1     1        -   7
EGADS    :     28     0     Yes    14     6        1   7 19
EGADS    :     29     0     Yes     6    19        1   8 19
EGADS    :     30     0     Yes    20    19        1   8 20
EGADS    :     31     0     Yes    21    20        1   8 21
EGADS    :     32     0     Yes    21    22        1   8 19
EGADS    :     33     0     Yes    22     9        1   8 11
EGADS    :     34     0     Yes     8    23        1   9 10
EGADS    :     35     0     Yes    23    24        1   9 22
EGADS    :     36     0     Yes     7    24        1   9 10
EGADS    :     37     0     Yes    25    26        1   9 23
EGADS    :     38     0     Yes    26    25        1   9 24
EGADS    :     39     0     Yes    24    23        1   10 25
EGADS    :     40     0     Yes    10    27        1   11 12
EGADS    :     41     0     Yes    27    22        1   11 19
EGADS    :     42     0     Yes    13    28        1   12 14
EGADS    :     43     0     Yes    28    11        1   12 13
EGADS    :     44     0     Yes    29    27        1   12 19
EGADS    :     45     0     Yes    30    29        1   12 26
EGADS    :     46     0     Yes    14    30        1   12 19
EGADS    :     47     0     Yes    12    31        1   13 14
EGADS    :     48     0     Yes    31    32        1   13 27
EGADS    :     49     0     Yes    28    32        1   13 14
EGADS    :     50     0     Yes    32    31        1   14 27
EGADS    :     51     0     Yes    15    33        1   15 16
EGADS    :     52     0     Yes    16    34        1   15 16
EGADS    :     53     0     Yes    33    34        1   15 28
EGADS    :     54     0     Yes    34    33        1   16 28
EGADS    :     55     0     Yes    35    36        1   17 29
EGADS    :     56     0     Yes    36    17        1   17 18
EGADS    :     57     0     Yes    35    18        1   17 18
EGADS    :     58     0     Yes    35    36        1   18 30
EGADS    :     59     0     Yes    29    30        1   19 31
EGADS    :     60     0     Yes    37    21        1   19 21
EGADS    :     61     0     Yes    19    37        1   19 20
EGADS    :     62     0     Yes    37    38        1   20 21
EGADS    :     63     0     Yes    38    39        1   20 32
EGADS    :     64     0     Yes    20    39        1   20 21
EGADS    :     65     0     Yes    39    38        1   21 32
EGADS    :     66     0     Yes    23    40        1   22 25
EGADS    :     67     0     Yes    24    41        1   22 25
EGADS    :     68     0     Yes    40    41        1   22 33
EGADS    :     69     0     Yes    42    43        1   23 34
EGADS    :     70     0     Yes    43    26        1   23 24
EGADS    :     71     0     Yes    42    25        1   23 24
EGADS    :     72     0     Yes    42    43        1   24 35
EGADS    :     73     0     Yes    41    40        1   25 33
EGADS    :     74     0     Yes    29    44        1   26 31
EGADS    :     75     0     Yes    44    45        1   26 36
EGADS    :     76     0     Yes    30    45        1   26 31
EGADS    :     77     0     Yes    46    35        1   29 30
EGADS    :     78     0     Yes    36    47        1   29 30
EGADS    :     79     0     Yes    47    48        1   29 37
EGADS    :     80     0     Yes    49    48        1   29 30
EGADS    :     81     0     Yes    46    49        1   29 37
EGADS    :     82     0     Yes    47    48        1   30 38
EGADS    :     83     0     Yes    46    49        1   30 38
EGADS    :     84     0     Yes    45    44        1   31 36
EGADS    :     85     0     Yes    50    43        1   34 35
EGADS    :     86     0     Yes    42    51        1   34 35
EGADS    :     87     0     Yes    51    52        1   34 39
EGADS    :     88     0     Yes    53    52        1   34 35
EGADS    :     89     0     Yes    50    53        1   34 39
EGADS    :     90     0     Yes    51    52        1   35 40
EGADS    :     91     0     Yes    50    53        1   35 40
EGADS    :     92     0     Yes    47    46        1   37 38
EGADS    :     93     0     Yes    48    49        1   37 38
EGADS    :     94     0     Yes    51    50        1   39 40
EGADS    :     95     0     Yes    52    53        1   39 40
EGADS    :     96     1     Yes    55    54       NA   41 43
EGADS    :     97     1     Yes    54    56       NA   41 46
EGADS    :     98     1     Yes    57    56       NA   41 44
EGADS    :     99     1     Yes    55    57       NA   41 45
EGADS    :    100     1     Yes    59    58       NA   42 43
EGADS    :    101     1     Yes    58    60       NA   42 46
EGADS    :    102     1     Yes    61    60       NA   42 44
EGADS    :    103     1     Yes    59    61       NA   42 45
EGADS    :    104     1     Yes    55    59       NA   43 45
EGADS    :    105     1     Yes    54    58       NA   43 46
EGADS    :    106     1     Yes    57    61       NA   44 45
EGADS    :    107     1     Yes    56    60       NA   44 46

EGADS    : Node Information

EGADS    :   Node  Active      Coordinates
EGADS    :      1     Yes                0                0                0
EGADS    :      2     Yes       121.026192                0                0
EGADS    :      3     Yes       121.026192               10                0
EGADS    :      4     Yes       54.9020417       7.00084115                0
EGADS    :      5     Yes        97.361045       7.90366896                0
EGADS    :      6     Yes       121.026192                0                0
EGADS    :      7     Yes        97.361045                0                0
EGADS    :      8     Yes       54.9020417                0                0
EGADS    :      9     Yes       165.026192                0                7
EGADS    :     10     Yes       165.026192              0.5              8.5
EGADS    :     11     Yes       156.577382       2.32417494       6.86784347
EGADS    :     12     Yes       160.457816       1.16501909       6.24763245
EGADS    :     13     Yes       152.092394       3.29252447       6.00142548
EGADS    :     14     Yes       121.026192                0               10
EGADS    :     15     Yes       97.9335611       36.1389817                0
EGADS    :     16     Yes       75.3047874       36.1389817                0
EGADS    :     17     Yes       72.4759225       29.3018771                0
EGADS    :     18     Yes       83.5054156       29.3018771                0
EGADS    :     19     Yes       152.092394                0       6.00142548
EGADS    :     20     Yes       160.457816                0       6.24763245
EGADS    :     21     Yes       156.577382                0       6.86784347
EGADS    :     22     Yes       165.026192                0              8.5
EGADS    :     23     Yes       75.3047874                0                0
EGADS    :     24     Yes       97.9335611                0                0
EGADS    :     25     Yes       72.4759225                0                0
EGADS    :     26     Yes       83.5054156                0                0
EGADS    :     27     Yes       165.026192                0               10
EGADS    :     28     Yes       139.227902       5.03861756       7.07099122
EGADS    :     29     Yes       159.822328                0               10
EGADS    :     30     Yes       137.454662                0               10
EGADS    :     31     Yes       173.282633        35.781198       13.6055284
EGADS    :     32     Yes        165.02399        35.781198       13.6055284
EGADS    :     33     Yes       123.552357       97.6729236        4.7180639
EGADS    :     34     Yes       118.391317       97.6729236       3.99272703
EGADS    :     35     Yes       79.4370049       29.3018771                0
EGADS    :     36     Yes        70.524066       29.3018771                0
EGADS    :     37     Yes       139.227902                0       7.07099122
EGADS    :     38     Yes        165.02399                0       13.6055284
EGADS    :     39     Yes       173.282633                0       13.6055284
EGADS    :     40     Yes       118.391317                0       3.99272703
EGADS    :     41     Yes       123.552357                0        4.7180639
EGADS    :     42     Yes        70.524066                0                0
EGADS    :     43     Yes       79.4370049                0                0
EGADS    :     44     Yes        169.38016                0        35.487551
EGADS    :     45     Yes       162.942213                0        35.487551
EGADS    :     46     Yes       90.5173952       29.3018771                0
EGADS    :     47     Yes       60.5173952       29.3018771                0
EGADS    :     48     Yes       60.5173952       29.3018771                0
EGADS    :     49     Yes       90.5173952       29.3018771                0
EGADS    :     50     Yes       90.5173952                0                0
EGADS    :     51     Yes       60.5173952                0                0
EGADS    :     52     Yes       60.5173952                0                0
EGADS    :     53     Yes       90.5173952                0                0
EGADS    :     54     Yes                0                0       1962.43554
EGADS    :     55     Yes                0                0                0
EGADS    :     56     Yes                0       1953.45847       1962.43554
EGADS    :     57     Yes                0       1953.45847                0
EGADS    :     58     Yes       2040.09979                0       1962.43554
EGADS    :     59     Yes       2040.09979                0                0
EGADS    :     60     Yes       2040.09979       1953.45847       1962.43554
EGADS    :     61     Yes       2040.09979       1953.45847                0

EGADS    : Face and Edge Match Information

EGADS    : No Face Matches Found

AFLR4    : Surface Mesh Spacing Setup

AFLR4    : Max Bounding Box Length     = 3906.92
AFLR4    : Min Bounding Box Length     = 3906.92
AFLR4    : Max Ref Bounding Box Length = 195.346
AFLR4    : Min Ref Bounding Box Length = 53.021
AFLR4    : Reference Length            = 21.7051
AFLR4    : BL Thickness                = 0
AFLR4    : FarField Spacing            = 530.302
AFLR4    : Abs Min Surf Spacing        = 0.0542627
AFLR4    : Min Surf Spacing            = 0.108525
AFLR4    : Max Surf Spacing            = 2.17051
AFLR4    : Global Scale Factor         = 1

AFLR4    : Geometry Definition Information

AFLR4    : Definition              Definition   Composite             Grid BC
AFLR4    :         ID                    Type          ID                Type
AFLR4    :          0     glue-only composite           -                   -
AFLR4    :          1            CAD geometry           0            STD w/BL
AFLR4    :          2            CAD geometry           0            STD w/BL
AFLR4    :          3            CAD geometry           0            STD w/BL
AFLR4    :          4            CAD geometry           0            STD w/BL
AFLR4    :          5            CAD geometry           0            STD w/BL
AFLR4    :          6            CAD geometry           0            STD w/BL
AFLR4    :          7            CAD geometry           0            STD w/BL
AFLR4    :          8            CAD geometry           0            STD w/BL
AFLR4    :          9            CAD geometry           0            STD w/BL
AFLR4    :         10            CAD geometry           0            STD w/BL
AFLR4    :         11            CAD geometry           0            STD w/BL
AFLR4    :         12            CAD geometry           0            STD w/BL
AFLR4    :         13            CAD geometry           0            STD w/BL
AFLR4    :         14            CAD geometry           0            STD w/BL
AFLR4    :         15            CAD geometry           0            STD w/BL
AFLR4    :         16            CAD geometry           0            STD w/BL
AFLR4    :         17            CAD geometry           0            STD w/BL
AFLR4    :         18            CAD geometry           0            STD w/BL
AFLR4    :         19            CAD geometry           0            STD w/BL
AFLR4    :         20            CAD geometry           0            STD w/BL
AFLR4    :         21            CAD geometry           0            STD w/BL
AFLR4    :         22            CAD geometry           0            STD w/BL
AFLR4    :         23            CAD geometry           0            STD w/BL
AFLR4    :         24            CAD geometry           0            STD w/BL
AFLR4    :         25            CAD geometry           0            STD w/BL
AFLR4    :         26            CAD geometry           0            STD w/BL
AFLR4    :         27            CAD geometry           0            STD w/BL
AFLR4    :         28            CAD geometry           0            STD w/BL
AFLR4    :         29            CAD geometry           0            STD w/BL
AFLR4    :         30            CAD geometry           0            STD w/BL
AFLR4    :         31            CAD geometry           0            STD w/BL
AFLR4    :         32            CAD geometry           0            STD w/BL
AFLR4    :         33            CAD geometry           0            STD w/BL
AFLR4    :         34            CAD geometry           0            STD w/BL
AFLR4    :         35            CAD geometry           0            STD w/BL
AFLR4    :         36            CAD geometry           0            STD w/BL
AFLR4    :         37            CAD geometry           0            STD w/BL
AFLR4    :         38            CAD geometry           0            STD w/BL
AFLR4    :         39            CAD geometry           0            STD w/BL
AFLR4    :         40            CAD geometry           0            STD w/BL
AFLR4    :         41            CAD geometry           0            FARFIELD
AFLR4    :         42            CAD geometry           0            FARFIELD
AFLR4    :         43            CAD geometry           0            FARFIELD
AFLR4    :         44            CAD geometry           0            FARFIELD
AFLR4    :         45            CAD geometry           0            FARFIELD
AFLR4    :         46            CAD geometry           0            FARFIELD

AFLR4    : Case has 6 Proximity Checking Components

AFLR4    : Component 1 includes Definitions 1 2 3 4 7 8 11 12 19
AFLR4    : Component 2 includes Definitions 5 6 9 10 15 16 22 25 28 33
AFLR4    : Component 3 includes Definitions 13 14 20 21 27 32
AFLR4    : Component 4 includes Definitions 26 31 36
AFLR4    : Component 5 includes Definitions 29 30 34 35 37 38 39 40
AFLR4    : Component 6 includes Definitions 17 18 23 24

AFLR4    : Define CAD surface definition 1
AFLR4    : Define CAD surface definition 2
AFLR4    : Define CAD surface definition 3
AFLR4    : Define CAD surface definition 4
AFLR4    : Define CAD surface definition 5
AFLR4    : Define CAD surface definition 6
AFLR4    : Define CAD surface definition 7
AFLR4    : Define CAD surface definition 8
AFLR4    : Define CAD surface definition 9
AFLR4    : Define CAD surface definition 10
AFLR4    : Define CAD surface definition 11
AFLR4    : Define CAD surface definition 12
AFLR4    : Define CAD surface definition 13
AFLR4    : Define CAD surface definition 14
AFLR4    : Define CAD surface definition 15
AFLR4    : Define CAD surface definition 16
AFLR4    : Define CAD surface definition 17
AFLR4    : Define CAD surface definition 18
AFLR4    : Define CAD surface definition 19
AFLR4    : Define CAD surface definition 20
AFLR4    : Define CAD surface definition 21
AFLR4    : Define CAD surface definition 22
AFLR4    : Define CAD surface definition 23
AFLR4    : Define CAD surface definition 24
AFLR4    : Define CAD surface definition 25
AFLR4    : Define CAD surface definition 26
AFLR4    : Define CAD surface definition 27
AFLR4    : Define CAD surface definition 28
AFLR4    : Define CAD surface definition 29
AFLR4    : Define CAD surface definition 30
AFLR4    : Define CAD surface definition 31
AFLR4    : Define CAD surface definition 32
AFLR4    : Define CAD surface definition 33
AFLR4    : Define CAD surface definition 34
AFLR4    : Define CAD surface definition 35
AFLR4    : Define CAD surface definition 36
AFLR4    : Define CAD surface definition 37
AFLR4    : Define CAD surface definition 38
AFLR4    : Define CAD surface definition 39
AFLR4    : Define CAD surface definition 40
AFLR4    : Define CAD surface definition 41
AFLR4    : Define CAD surface definition 42
AFLR4    : Define CAD surface definition 43
AFLR4    : Define CAD surface definition 44
AFLR4    : Define CAD surface definition 45
AFLR4    : Define CAD surface definition 46

AFLR4    : Surface Grid Generation

AFLR4    : Generate optimal mesh on surface definition 1
AFLR2    : Nodes, Trias,Quads=       246       377         0
AFLR4    : Nodes, Trias,Quads=       228       341         0

AFLR4    : Generate optimal mesh on surface definition 2
AFLR2    : Nodes, Trias,Quads=       245       375         0
AFLR4    : Nodes, Trias,Quads=       231       347         0

AFLR4    : Generate optimal mesh on surface definition 3
AFLR2    : Nodes, Trias,Quads=       193       322         0
AFLR4    : Nodes, Trias,Quads=       123       182         0

AFLR4    : Generate optimal mesh on surface definition 4
AFLR2    : Nodes, Trias,Quads=       151       227         0
AFLR4    : Nodes, Trias,Quads=       168       261         0

AFLR4    : Generate optimal mesh on surface definition 5
AFLR2    : Nodes, Trias,Quads=      1008      1880         0
AFLR4    : Nodes, Trias,Quads=       667      1198         0

AFLR4    : Generate optimal mesh on surface definition 6
AFLR2    : Nodes, Trias,Quads=      1591      2995         0
AFLR4    : Nodes, Trias,Quads=      1102      2017         0

AFLR4    : Generate optimal mesh on surface definition 7
AFLR2    : Nodes, Trias,Quads=       151       227         0
AFLR4    : Nodes, Trias,Quads=       169       263         0

AFLR4    : Generate optimal mesh on surface definition 8
AFLR2    : Nodes, Trias,Quads=       193       322         0
AFLR4    : Nodes, Trias,Quads=       125       186         0

AFLR4    : Generate optimal mesh on surface definition 9
AFLR2    : Nodes, Trias,Quads=      1596      3005         0
AFLR4    : Nodes, Trias,Quads=      1074      1961         0

AFLR4    : Generate optimal mesh on surface definition 10
AFLR2    : Nodes, Trias,Quads=      1006      1876         0
AFLR4    : Nodes, Trias,Quads=       664      1192         0

AFLR4    : Generate optimal mesh on surface definition 11
AFLR2    : Nodes, Trias,Quads=        22        26         0
AFLR4    : Nodes, Trias,Quads=        22        26         0

AFLR4    : Generate optimal mesh on surface definition 12
AFLR2    : Nodes, Trias,Quads=       506       895         0
AFLR4    : Nodes, Trias,Quads=       318       519         0

AFLR4    : Generate optimal mesh on surface definition 13
AFLR2    : Nodes, Trias,Quads=      1283      2419         0
AFLR4    : Nodes, Trias,Quads=       743      1339         0

AFLR4    : Generate optimal mesh on surface definition 14
AFLR2    : Nodes, Trias,Quads=      1282      2418         0
AFLR4    : Nodes, Trias,Quads=       752      1358         0

AFLR4    : Generate optimal mesh on surface definition 15
AFLR2    : Nodes, Trias,Quads=      2043      3860         0
AFLR4    : Nodes, Trias,Quads=       939      1652         0

AFLR4    : Generate optimal mesh on surface definition 16
AFLR2    : Nodes, Trias,Quads=      1981      3736         0
AFLR4    : Nodes, Trias,Quads=       917      1608         0

AFLR4    : Generate optimal mesh on surface definition 17
AFLR2    : Nodes, Trias,Quads=       360       636         0
AFLR4    : Nodes, Trias,Quads=       217       350         0

AFLR4    : Generate optimal mesh on surface definition 18
AFLR2    : Nodes, Trias,Quads=       364       644         0
AFLR4    : Nodes, Trias,Quads=       222       360         0

AFLR4    : Generate optimal mesh on surface definition 19
AFLR2    : Nodes, Trias,Quads=       554       991         0
AFLR4    : Nodes, Trias,Quads=       313       509         0

AFLR4    : Generate optimal mesh on surface definition 20
AFLR2    : Nodes, Trias,Quads=      1279      2412         0
AFLR4    : Nodes, Trias,Quads=       752      1358         0

AFLR4    : Generate optimal mesh on surface definition 21
AFLR2    : Nodes, Trias,Quads=      1280      2413         0
AFLR4    : Nodes, Trias,Quads=       746      1345         0

AFLR4    : Generate optimal mesh on surface definition 22
AFLR2    : Nodes, Trias,Quads=      1992      3758         0
AFLR4    : Nodes, Trias,Quads=       930      1634         0

AFLR4    : Generate optimal mesh on surface definition 23
AFLR2    : Nodes, Trias,Quads=       361       638         0
AFLR4    : Nodes, Trias,Quads=       220       356         0

AFLR4    : Generate optimal mesh on surface definition 24
AFLR2    : Nodes, Trias,Quads=       359       634         0
AFLR4    : Nodes, Trias,Quads=       217       350         0

AFLR4    : Generate optimal mesh on surface definition 25
AFLR2    : Nodes, Trias,Quads=      1995      3764         0
AFLR4    : Nodes, Trias,Quads=       928      1630         0

AFLR4    : Generate optimal mesh on surface definition 26
AFLR2    : Nodes, Trias,Quads=      1185      2231         0
AFLR4    : Nodes, Trias,Quads=       777      1415         0

AFLR4    : Generate optimal mesh on surface definition 27
AFLR2    : Nodes, Trias,Quads=        32        40         0
AFLR4    : Nodes, Trias,Quads=        22        20         0

AFLR4    : Generate optimal mesh on surface definition 28
AFLR2    : Nodes, Trias,Quads=        23        28         0
AFLR4    : Nodes, Trias,Quads=        16        14         0

AFLR4    : Generate optimal mesh on surface definition 29
AFLR2    : Nodes, Trias,Quads=      4557      8810         0
AFLR4    : Nodes, Trias,Quads=      4493      8682         0

AFLR4    : Generate optimal mesh on surface definition 30
AFLR2    : Nodes, Trias,Quads=      4584      8864         0
AFLR4    : Nodes, Trias,Quads=      4397      8490         0

AFLR4    : Generate optimal mesh on surface definition 31
AFLR2    : Nodes, Trias,Quads=      1154      2169         0
AFLR4    : Nodes, Trias,Quads=       790      1441         0

AFLR4    : Generate optimal mesh on surface definition 32
AFLR2    : Nodes, Trias,Quads=        32        40         0
AFLR4    : Nodes, Trias,Quads=        22        20         0

AFLR4    : Generate optimal mesh on surface definition 33
AFLR2    : Nodes, Trias,Quads=        23        28         0
AFLR4    : Nodes, Trias,Quads=        16        14         0

AFLR4    : Generate optimal mesh on surface definition 34
AFLR2    : Nodes, Trias,Quads=      4604      8904         0
AFLR4    : Nodes, Trias,Quads=      4409      8514         0

AFLR4    : Generate optimal mesh on surface definition 35
AFLR2    : Nodes, Trias,Quads=      4566      8828         0
AFLR4    : Nodes, Trias,Quads=      4389      8474         0

AFLR4    : Generate optimal mesh on surface definition 36
AFLR2    : Nodes, Trias,Quads=        26        32         0
AFLR4    : Nodes, Trias,Quads=        18        16         0

AFLR4    : Generate optimal mesh on surface definition 37
AFLR2    : Nodes, Trias,Quads=      4908      9492         0
AFLR4    : Nodes, Trias,Quads=      4321      8318         0

AFLR4    : Generate optimal mesh on surface definition 38
AFLR2    : Nodes, Trias,Quads=      4956      9588         0
AFLR4    : Nodes, Trias,Quads=      4337      8350         0

AFLR4    : Generate optimal mesh on surface definition 39
AFLR2    : Nodes, Trias,Quads=      4908      9492         0
AFLR4    : Nodes, Trias,Quads=      4321      8318         0

AFLR4    : Generate optimal mesh on surface definition 40
AFLR2    : Nodes, Trias,Quads=      4956      9588         0
AFLR4    : Nodes, Trias,Quads=      4337      8350         0

AFLR4    : Generate optimal mesh on surface definition 41
AFLR2    : Nodes, Trias,Quads=        73       116         0
AFLR4    : Nodes, Trias,Quads=        68       106         0

AFLR4    : Generate optimal mesh on surface definition 42
AFLR2    : Nodes, Trias,Quads=        73       116         0
AFLR4    : Nodes, Trias,Quads=        68       106         0

AFLR4    : Generate optimal mesh on surface definition 43
AFLR2    : Nodes, Trias,Quads=        73       116         0
AFLR4    : Nodes, Trias,Quads=        68       106         0

AFLR4    : Generate optimal mesh on surface definition 44
AFLR2    : Nodes, Trias,Quads=        73       116         0
AFLR4    : Nodes, Trias,Quads=        68       106         0

AFLR4    : Generate optimal mesh on surface definition 45
AFLR2    : Nodes, Trias,Quads=        73       116         0
AFLR4    : Nodes, Trias,Quads=        68       106         0

AFLR4    : Generate optimal mesh on surface definition 46
AFLR2    : Nodes, Trias,Quads=        73       116         0
AFLR4    : Nodes, Trias,Quads=        68       106         0

DGEOM    : Add surface definitions to composite definition 0
DGEOM    : Glue composite surface definition 0
DGEOM    : Nodes,Faces,BEdges=     46707     93414      6222

AFLR4    : Curvature BG Surface Grid Generation

AFLR4    : Nodes, Faces      =     46707     93414

AFLR4    : Surface Grid Generation

AFLR4    : Generate optimal mesh on surface definition 1
AFLR2    : Nodes, Trias,Quads=       273       422         0
AFLR4    : Nodes, Trias,Quads=       408       692         0

AFLR4    : Generate optimal mesh on surface definition 2
AFLR2    : Nodes, Trias,Quads=       270       416         0
AFLR4    : Nodes, Trias,Quads=       418       712         0

AFLR4    : Generate optimal mesh on surface definition 3
AFLR2    : Nodes, Trias,Quads=       242       410         0
AFLR4    : Nodes, Trias,Quads=       156       238         0

AFLR4    : Generate optimal mesh on surface definition 4
AFLR2    : Nodes, Trias,Quads=       166       252         0
AFLR4    : Nodes, Trias,Quads=       208       336         0

AFLR4    : Generate optimal mesh on surface definition 5
AFLR2    : Nodes, Trias,Quads=      1032      1928         0
AFLR4    : Nodes, Trias,Quads=       926      1716         0

AFLR4    : Generate optimal mesh on surface definition 6
AFLR2    : Nodes, Trias,Quads=      1629      3071         0
AFLR4    : Nodes, Trias,Quads=      1448      2709         0

AFLR4    : Generate optimal mesh on surface definition 7
AFLR2    : Nodes, Trias,Quads=       166       252         0
AFLR4    : Nodes, Trias,Quads=       209       338         0

AFLR4    : Generate optimal mesh on surface definition 8
AFLR2    : Nodes, Trias,Quads=       242       410         0
AFLR4    : Nodes, Trias,Quads=       158       242         0

AFLR4    : Generate optimal mesh on surface definition 9
AFLR2    : Nodes, Trias,Quads=      1619      3052         0
AFLR4    : Nodes, Trias,Quads=      1459      2732         0

AFLR4    : Generate optimal mesh on surface definition 10
AFLR2    : Nodes, Trias,Quads=      1061      1985         0
AFLR4    : Nodes, Trias,Quads=       914      1691         0

AFLR4    : Generate optimal mesh on surface definition 11
AFLR2    : Nodes, Trias,Quads=        22        26         0
AFLR4    : Nodes, Trias,Quads=        22        26         0

AFLR4    : Generate optimal mesh on surface definition 12
AFLR2    : Nodes, Trias,Quads=       566      1006         0
AFLR4    : Nodes, Trias,Quads=       447       768         0

AFLR4    : Generate optimal mesh on surface definition 13
AFLR2    : Nodes, Trias,Quads=      1270      2391         0
AFLR4    : Nodes, Trias,Quads=       995      1841         0

AFLR4    : Generate optimal mesh on surface definition 14
AFLR2    : Nodes, Trias,Quads=      1288      2429         0
AFLR4    : Nodes, Trias,Quads=       990      1833         0

AFLR4    : Generate optimal mesh on surface definition 15
AFLR2    : Nodes, Trias,Quads=      1935      3648         0
AFLR4    : Nodes, Trias,Quads=      1624      3026         0

AFLR4    : Generate optimal mesh on surface definition 16
AFLR2    : Nodes, Trias,Quads=      1955      3687         0
AFLR4    : Nodes, Trias,Quads=      1594      2965         0

AFLR4    : Generate optimal mesh on surface definition 17
AFLR2    : Nodes, Trias,Quads=       356       628         0
AFLR4    : Nodes, Trias,Quads=       275       466         0

AFLR4    : Generate optimal mesh on surface definition 18
AFLR2    : Nodes, Trias,Quads=       369       653         0
AFLR4    : Nodes, Trias,Quads=       291       497         0

AFLR4    : Generate optimal mesh on surface definition 19
AFLR2    : Nodes, Trias,Quads=       592      1060         0
AFLR4    : Nodes, Trias,Quads=       435       746         0

AFLR4    : Generate optimal mesh on surface definition 20
AFLR2    : Nodes, Trias,Quads=      1250      2354         0
AFLR4    : Nodes, Trias,Quads=       997      1848         0

AFLR4    : Generate optimal mesh on surface definition 21
AFLR2    : Nodes, Trias,Quads=      1228      2308         0
AFLR4    : Nodes, Trias,Quads=       997      1846         0

AFLR4    : Generate optimal mesh on surface definition 22
AFLR2    : Nodes, Trias,Quads=      1999      3775         0
AFLR4    : Nodes, Trias,Quads=      1610      2997         0

AFLR4    : Generate optimal mesh on surface definition 23
AFLR2    : Nodes, Trias,Quads=       367       649         0
AFLR4    : Nodes, Trias,Quads=       286       487         0

AFLR4    : Generate optimal mesh on surface definition 24
AFLR2    : Nodes, Trias,Quads=       357       630         0
AFLR4    : Nodes, Trias,Quads=       280       476         0

AFLR4    : Generate optimal mesh on surface definition 25
AFLR2    : Nodes, Trias,Quads=      1997      3772         0
AFLR4    : Nodes, Trias,Quads=      1598      2974         0

AFLR4    : Generate optimal mesh on surface definition 26
AFLR2    : Nodes, Trias,Quads=      1194      2247         0
AFLR4    : Nodes, Trias,Quads=       942      1743         0

AFLR4    : Generate optimal mesh on surface definition 27
AFLR2    : Nodes, Trias,Quads=        32        40         0
AFLR4    : Nodes, Trias,Quads=        22        20         0

AFLR4    : Generate optimal mesh on surface definition 28
AFLR2    : Nodes, Trias,Quads=        30        40         0
AFLR4    : Nodes, Trias,Quads=        18        16         0

AFLR4    : Generate optimal mesh on surface definition 29
AFLR2    : Nodes, Trias,Quads=      4710      9112         0
AFLR4    : Nodes, Trias,Quads=      4567      8826         0

AFLR4    : Generate optimal mesh on surface definition 30
AFLR2    : Nodes, Trias,Quads=      4722      9136         0
AFLR4    : Nodes, Trias,Quads=      4491      8674         0

AFLR4    : Generate optimal mesh on surface definition 31
AFLR2    : Nodes, Trias,Quads=      1221      2301         0
AFLR4    : Nodes, Trias,Quads=       955      1769         0

AFLR4    : Generate optimal mesh on surface definition 32
AFLR2    : Nodes, Trias,Quads=        33        42         0
AFLR4    : Nodes, Trias,Quads=        22        20         0

AFLR4    : Generate optimal mesh on surface definition 33
AFLR2    : Nodes, Trias,Quads=        30        40         0
AFLR4    : Nodes, Trias,Quads=        18        16         0

AFLR4    : Generate optimal mesh on surface definition 34
AFLR2    : Nodes, Trias,Quads=      4711      9114         0
AFLR4    : Nodes, Trias,Quads=      4490      8672         0

AFLR4    : Generate optimal mesh on surface definition 35
AFLR2    : Nodes, Trias,Quads=      4729      9150         0
AFLR4    : Nodes, Trias,Quads=      4472      8636         0

AFLR4    : Generate optimal mesh on surface definition 36
AFLR2    : Nodes, Trias,Quads=        26        32         0
AFLR4    : Nodes, Trias,Quads=        18        16         0

AFLR4    : Generate optimal mesh on surface definition 37
AFLR2    : Nodes, Trias,Quads=      4980      9633         0
AFLR4    : Nodes, Trias,Quads=      4420      8513         0

AFLR4    : Generate optimal mesh on surface definition 38
AFLR2    : Nodes, Trias,Quads=      5016      9705         0
AFLR4    : Nodes, Trias,Quads=      4436      8545         0

AFLR4    : Generate optimal mesh on surface definition 39
AFLR2    : Nodes, Trias,Quads=      4980      9633         0
AFLR4    : Nodes, Trias,Quads=      4420      8513         0

AFLR4    : Generate optimal mesh on surface definition 40
AFLR2    : Nodes, Trias,Quads=      5016      9705         0
AFLR4    : Nodes, Trias,Quads=      4436      8545         0

AFLR4    : Generate optimal mesh on surface definition 41
AFLR2    : Nodes, Trias,Quads=        73       116         0
AFLR4    : Nodes, Trias,Quads=        68       106         0

AFLR4    : Generate optimal mesh on surface definition 42
AFLR2    : Nodes, Trias,Quads=        73       116         0
AFLR4    : Nodes, Trias,Quads=        68       106         0

AFLR4    : Generate optimal mesh on surface definition 43
AFLR2    : Nodes, Trias,Quads=        73       116         0
AFLR4    : Nodes, Trias,Quads=        68       106         0

AFLR4    : Generate optimal mesh on surface definition 44
AFLR2    : Nodes, Trias,Quads=        73       116         0
AFLR4    : Nodes, Trias,Quads=        68       106         0

AFLR4    : Generate optimal mesh on surface definition 45
AFLR2    : Nodes, Trias,Quads=        73       116         0
AFLR4    : Nodes, Trias,Quads=        68       106         0

AFLR4    : Generate optimal mesh on surface definition 46
AFLR2    : Nodes, Trias,Quads=        73       116         0
AFLR4    : Nodes, Trias,Quads=        68       106         0

DGEOM    : Add surface definitions to composite definition 0
DGEOM    : Glue composite surface definition 0
DGEOM    : Nodes,Faces,BEdges=     53681    107362      6314

AFLR4    : Proximity BG Surface Grid Generation

AFLR4    : Nodes, Trias      =     55586    111172
AFLR4    : Nodes, Trias      =     56019    112038

AFLR4    : Surface Grid Generation

AFLR4    : Generate optimal mesh on surface definition 1
AFLR2    : Nodes, Trias,Quads=       812      1370         0
AFLR4    : Nodes, Trias,Quads=      1176      2098         0

AFLR4    : Generate optimal mesh on surface definition 2
AFLR2    : Nodes, Trias,Quads=       874      1486         0
AFLR4    : Nodes, Trias,Quads=      1195      2128         0

AFLR4    : Generate optimal mesh on surface definition 3
AFLR2    : Nodes, Trias,Quads=       500       889         0
AFLR4    : Nodes, Trias,Quads=       338       565         0

AFLR4    : Generate optimal mesh on surface definition 4
AFLR2    : Nodes, Trias,Quads=       436       751         0
AFLR4    : Nodes, Trias,Quads=       532       943         0

AFLR4    : Generate optimal mesh on surface definition 5
AFLR2    : Nodes, Trias,Quads=      2548      4881         0
AFLR4    : Nodes, Trias,Quads=      1628      3041         0

AFLR4    : Generate optimal mesh on surface definition 6
AFLR2    : Nodes, Trias,Quads=      3802      7298         0
AFLR4    : Nodes, Trias,Quads=      3195      6084         0

AFLR4    : Generate optimal mesh on surface definition 7
AFLR2    : Nodes, Trias,Quads=       511       892         0
AFLR4    : Nodes, Trias,Quads=       620      1110         0

AFLR4    : Generate optimal mesh on surface definition 8
AFLR2    : Nodes, Trias,Quads=       502       892         0
AFLR4    : Nodes, Trias,Quads=       351       590         0

AFLR4    : Generate optimal mesh on surface definition 9
AFLR2    : Nodes, Trias,Quads=      3816      7325         0
AFLR4    : Nodes, Trias,Quads=      3204      6101         0

AFLR4    : Generate optimal mesh on surface definition 10
AFLR2    : Nodes, Trias,Quads=      2644      5074         0
AFLR4    : Nodes, Trias,Quads=      1637      3060         0

AFLR4    : Generate optimal mesh on surface definition 11
AFLR2    : Nodes, Trias,Quads=        22        26         0
AFLR4    : Nodes, Trias,Quads=        22        26         0

AFLR4    : Generate optimal mesh on surface definition 12
AFLR2    : Nodes, Trias,Quads=       897      1624         0
AFLR4    : Nodes, Trias,Quads=       699      1228         0

AFLR4    : Generate optimal mesh on surface definition 13
AFLR2    : Nodes, Trias,Quads=      1666      3146         0
AFLR4    : Nodes, Trias,Quads=      1327      2468         0

AFLR4    : Generate optimal mesh on surface definition 14
AFLR2    : Nodes, Trias,Quads=      1654      3125         0
AFLR4    : Nodes, Trias,Quads=      1272      2361         0

AFLR4    : Generate optimal mesh on surface definition 15
AFLR2    : Nodes, Trias,Quads=      2402      4570         0
AFLR4    : Nodes, Trias,Quads=      1835      3436         0

AFLR4    : Generate optimal mesh on surface definition 16
AFLR2    : Nodes, Trias,Quads=      2397      4559         0
AFLR4    : Nodes, Trias,Quads=      1799      3363         0

AFLR4    : Generate optimal mesh on surface definition 17
AFLR2    : Nodes, Trias,Quads=      1558      2936         0
AFLR4    : Nodes, Trias,Quads=       935      1690         0

AFLR4    : Generate optimal mesh on surface definition 18
AFLR2    : Nodes, Trias,Quads=      1504      2833         0
AFLR4    : Nodes, Trias,Quads=       899      1623         0

AFLR4    : Generate optimal mesh on surface definition 19
AFLR2    : Nodes, Trias,Quads=      1056      1933         0
AFLR4    : Nodes, Trias,Quads=       835      1491         0

AFLR4    : Generate optimal mesh on surface definition 20
AFLR2    : Nodes, Trias,Quads=      1750      3308         0
AFLR4    : Nodes, Trias,Quads=      1338      2484         0

AFLR4    : Generate optimal mesh on surface definition 21
AFLR2    : Nodes, Trias,Quads=      1647      3107         0
AFLR4    : Nodes, Trias,Quads=      1344      2501         0

AFLR4    : Generate optimal mesh on surface definition 22
AFLR2    : Nodes, Trias,Quads=      2438      4642         0
AFLR4    : Nodes, Trias,Quads=      1804      3374         0

AFLR4    : Generate optimal mesh on surface definition 23
AFLR2    : Nodes, Trias,Quads=      1488      2801         0
AFLR4    : Nodes, Trias,Quads=       896      1617         0

AFLR4    : Generate optimal mesh on surface definition 24
AFLR2    : Nodes, Trias,Quads=      1636      3088         0
AFLR4    : Nodes, Trias,Quads=       972      1760         0

AFLR4    : Generate optimal mesh on surface definition 25
AFLR2    : Nodes, Trias,Quads=      2484      4735         0
AFLR4    : Nodes, Trias,Quads=      1793      3353         0

AFLR4    : Generate optimal mesh on surface definition 26
AFLR2    : Nodes, Trias,Quads=      1469      2777         0
AFLR4    : Nodes, Trias,Quads=      1074      1987         0

AFLR4    : Generate optimal mesh on surface definition 27
AFLR2    : Nodes, Trias,Quads=        32        40         0
AFLR4    : Nodes, Trias,Quads=        22        20         0

AFLR4    : Generate optimal mesh on surface definition 28
AFLR2    : Nodes, Trias,Quads=        30        39         0
AFLR4    : Nodes, Trias,Quads=        19        17         0

AFLR4    : Generate optimal mesh on surface definition 29
AFLR2    : Nodes, Trias,Quads=      6621     12889         0
AFLR4    : Nodes, Trias,Quads=      4948      9543         0

AFLR4    : Generate optimal mesh on surface definition 30
AFLR2    : Nodes, Trias,Quads=      6934     13515         0
AFLR4    : Nodes, Trias,Quads=      4856      9359         0

AFLR4    : Generate optimal mesh on surface definition 31
AFLR2    : Nodes, Trias,Quads=      1460      2759         0
AFLR4    : Nodes, Trias,Quads=      1102      2043         0

AFLR4    : Generate optimal mesh on surface definition 32
AFLR2    : Nodes, Trias,Quads=        33        42         0
AFLR4    : Nodes, Trias,Quads=        22        20         0

AFLR4    : Generate optimal mesh on surface definition 33
AFLR2    : Nodes, Trias,Quads=        30        39         0
AFLR4    : Nodes, Trias,Quads=        19        17         0

AFLR4    : Generate optimal mesh on surface definition 34
AFLR2    : Nodes, Trias,Quads=      6810     13267         0
AFLR4    : Nodes, Trias,Quads=      4903      9453         0

AFLR4    : Generate optimal mesh on surface definition 35
AFLR2    : Nodes, Trias,Quads=      7228     14100         0
AFLR4    : Nodes, Trias,Quads=      4901      9446         0

AFLR4    : Generate optimal mesh on surface definition 36
AFLR2    : Nodes, Trias,Quads=        30        38         0
AFLR4    : Nodes, Trias,Quads=        20        18         0

AFLR4    : Generate optimal mesh on surface definition 37
AFLR2    : Nodes, Trias,Quads=      5067      9804         0
AFLR4    : Nodes, Trias,Quads=      4466      8602         0

AFLR4    : Generate optimal mesh on surface definition 38
AFLR2    : Nodes, Trias,Quads=      5098      9866         0
AFLR4    : Nodes, Trias,Quads=      4493      8656         0

AFLR4    : Generate optimal mesh on surface definition 39
AFLR2    : Nodes, Trias,Quads=      5066      9802         0
AFLR4    : Nodes, Trias,Quads=      4466      8602         0

AFLR4    : Generate optimal mesh on surface definition 40
AFLR2    : Nodes, Trias,Quads=      5098      9866         0
AFLR4    : Nodes, Trias,Quads=      4493      8656         0

AFLR4    : Generate optimal mesh on surface definition 41
AFLR2    : Nodes, Trias,Quads=        73       116         0
AFLR4    : Nodes, Trias,Quads=        68       106         0

AFLR4    : Generate optimal mesh on surface definition 42
AFLR2    : Nodes, Trias,Quads=        73       116         0
AFLR4    : Nodes, Trias,Quads=        68       106         0

AFLR4    : Generate optimal mesh on surface definition 43
AFLR2    : Nodes, Trias,Quads=        73       116         0
AFLR4    : Nodes, Trias,Quads=        68       106         0

AFLR4    : Generate optimal mesh on surface definition 44
AFLR2    : Nodes, Trias,Quads=        73       116         0
AFLR4    : Nodes, Trias,Quads=        68       106         0

AFLR4    : Generate optimal mesh on surface definition 45
AFLR2    : Nodes, Trias,Quads=        73       116         0
AFLR4    : Nodes, Trias,Quads=        68       106         0

AFLR4    : Generate optimal mesh on surface definition 46
AFLR2    : Nodes, Trias,Quads=        73       116         0
AFLR4    : Nodes, Trias,Quads=        68       106         0

DGEOM    : Add surface definitions to composite definition 0
DGEOM    : Glue composite surface definition 0
DGEOM    : Nodes,Faces,BEdges=     67785    135570      8062

OVERALL  : CPU Time          =     3.113   seconds
Body 1 (of 2)
Number of nodes    = 67465
Number of elements = 134934
Number of triangle elements      = 134934
Number of quadrilateral elements = 0
Body 2 (of 2)
Number of nodes    = 320
Number of elements = 636
Number of triangle elements      = 636
Number of quadrilateral elements = 0
----------------------------
Total number of nodes    = 67785
Total number of elements = 135570
Total number of triangle elements      = 135570
Total number of quadrilateral elements = 0

real	0m10.616s
user	0m14.047s
sys	0m2.379s
+ status=0
+ set +x

=================================================
solutions/session07/aflr4_InviscidTransport.py passed (as expected)
=================================================


=================================================
aflr4_InviscidTransport_150k.py test;
+ python aflr4_InviscidTransport_150k.py
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/CAPS/training/2023/training.log

MESSAGE:: Building wingOml


MESSAGE:: Building pylonOml


MESSAGE:: Building nacelleOml


MESSAGE:: Building htailOml


MESSAGE:: Building vtailOml


MESSAGE:: Building fuseOml

Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 7
	Name = Fuselage, index = 1
	Name = Wing, index = 2
	Name = Htail, index = 3
	Name = Pylon, index = 4
	Name = Vtail, index = 5
	Name = Nacelle, index = 6
	Name = Farfield, index = 7
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 8
	Name = Fuselage, index = 1
	Name = riteWing, index = 2
	Name = leftWing, index = 3
	Name = Htail, index = 4
	Name = Pylon, index = 5
	Name = Vtail, index = 6
	Name = Nacelle, index = 7
	Name = Farfield, index = 8

Getting mesh sizing parameters
	Mesh sizing name - Farfield
	Mesh sizing name - Fuselage
	Mesh sizing name - Htail
	Mesh sizing name - Pylon
	Mesh sizing name - Vtail
	Mesh sizing name - leftWing
	Mesh sizing name - riteWing
	Done getting mesh sizing parameters
 
AFLR2    : ---------------------------------------
AFLR2    : AFLR2 LIBRARY
AFLR2    : ADVANCING-FRONT/LOCAL-RECONNECTION
AFLR2    : TRIA/QUAD GRID GENERATOR
AFLR2    : Version Number 9.18.1
AFLR2    : Version Date   06/11/24 @ 05:52PM
AFLR2    : Compile OS     Darwin 23.5.0 arm64
AFLR2    : Compile Date   06/11/24 @ 05:52PM
AFLR2    : Copyright 1994-2021, D.L. Marcum
AFLR2    : ---------------------------------------
 
AFLR4    : ---------------------------------------
AFLR4    : AFLR4 LIBRARY
AFLR4    : ADVANCING-FRONT/LOCAL-RECONNECTION
AFLR4    : TRIA/QUAD SURFACE GRID GENERATOR
AFLR4    : Version Number 11.5.15
AFLR4    : Version Date   07/19/24 @ 07:04PM
AFLR4    : Compile OS     Darwin 23.5.0 arm64
AFLR4    : Compile Date   07/19/24 @ 07:06PM
AFLR4    : Copyright 1994-2021, D.L. Marcum
AFLR4    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.8.1
EGADS    : ---------------------------------------

EGADS    : EGADS CAD Geometry Setup

EGADS    : Model has 2 Active Bodies

EGADS    : Body 0 is a SolidBody
EGADS    : Body 0 has 1 Shells
EGADS    : Body 0 has 40 Faces
EGADS    : Body 0 has 95 Edges
EGADS    : Body 0 has 44 Loops
EGADS    : Body 0 has 53 Nodes
EGADS    : Body 1 is a SolidBody
EGADS    : Body 1 has 1 Shells
EGADS    : Body 1 has 6 Faces
EGADS    : Body 1 has 12 Edges
EGADS    : Body 1 has 6 Loops
EGADS    : Body 1 has 8 Nodes

EGADS    : Check Grid BCs

EGADS    : Grid BCs are OK

EGADS    : Face Neighbor-Faces Information

EGADS    : QC  = Face Quad Combination Flag
EGADS    : IER = Face Isolated Edge Refinement Flag
EGADS    : ER  = Face Edge Refinement Factor
EGADS    :       Not applicable for Faces with a FarField Grid BC.
EGADS    : SF  = Face Scale Factor
EGADS    :       Not applicable for Faces with a FarField Grid BC.

EGADS    :   Face          Body    QC   IER       ER    Scale   Neighbor
EGADS    :     ID  Active    ID  Flag  Flag   Weight   Factor   Faces
EGADS    :      1     Yes     0     0     1        0        1   2 3 4 5 6
EGADS    :      2     Yes     0     0     1        0        1   1 7 8 9 10
EGADS    :      3     Yes     0     0     1        0        1   1 8 11 12 13 14
EGADS    :      4     Yes     0     0     1        0        1   1 7 12
EGADS    :      5     Yes     0     0     1        0        2   1 6 15
EGADS    :      6     Yes     0     0     1        0        2   1 5 16 17 18
EGADS    :      7     Yes     0     0     1        0        1   2 4 19
EGADS    :      8     Yes     0     0     1        0        1   2 3 11 19 20 21
EGADS    :      9     Yes     0     0     1        0        2   2 10 22 23 24
EGADS    :     10     Yes     0     0     1        0        2   2 9 25
EGADS    :     11     Yes     0     0     1        0        1   3 8 12 19
EGADS    :     12     Yes     0     0     1        0        1   3 4 11 13 14 19
EGADS    :                                                      26
EGADS    :     13     Yes     0     0     1        0        2   3 12 14 27
EGADS    :     14     Yes     0     0     1        0        2   3 12 13 27
EGADS    :     15     Yes     0     0     1        0        2   5 16 28
EGADS    :     16     Yes     0     0     1        0        2   6 15 28
EGADS    :     17     Yes     0     0     1        0        1   6 18 29
EGADS    :     18     Yes     0     0     1        0        1   6 17 30
EGADS    :     19     Yes     0     0     1        0        1   7 8 11 12 20 21
EGADS    :                                                      31
EGADS    :     20     Yes     0     0     1        0        2   8 19 21 32
EGADS    :     21     Yes     0     0     1        0        2   8 19 20 32
EGADS    :     22     Yes     0     0     1        0        2   9 25 33
EGADS    :     23     Yes     0     0     1        0        1   9 24 34
EGADS    :     24     Yes     0     0     1        0        1   9 23 35
EGADS    :     25     Yes     0     0     1        0        2   10 22 33
EGADS    :     26     Yes     0     0     1        0        2   12 31 36
EGADS    :     27     Yes     0     0     1        0        2   13 14
EGADS    :     28     Yes     0     0     1        0        2   15 16
EGADS    :     29     Yes     0     0     1        0        1   17 30 37
EGADS    :     30     Yes     0     0     1        0        1   18 29 38
EGADS    :     31     Yes     0     0     1        0        2   19 26 36
EGADS    :     32     Yes     0     0     1        0        2   20 21
EGADS    :     33     Yes     0     0     1        0        2   22 25
EGADS    :     34     Yes     0     0     1        0        1   23 35 39
EGADS    :     35     Yes     0     0     1        0        1   24 34 40
EGADS    :     36     Yes     0     0     1        0        2   26 31
EGADS    :     37     Yes     0     0     1        0        1   29 38
EGADS    :     38     Yes     0     0     1        0        1   30 37
EGADS    :     39     Yes     0     0     1        0        1   34 40
EGADS    :     40     Yes     0     0     1        0        1   35 39
EGADS    :     41     Yes     1     0     1       NA       NA   43 44 45 46
EGADS    :     42     Yes     1     0     1       NA       NA   43 44 45 46
EGADS    :     43     Yes     1     0     1       NA       NA   41 42 45 46
EGADS    :     44     Yes     1     0     1       NA       NA   41 42 45 46
EGADS    :     45     Yes     1     0     1       NA       NA   41 42 43 44
EGADS    :     46     Yes     1     0     1       NA       NA   41 42 43 44

EGADS    : Face Edges Information

EGADS    :   Face   Edges
EGADS    :      1   -1 4 3 -2 -5 -6
EGADS    :      2   -7 9 1 -8 10 11
EGADS    :      3   -12 2 17 -16 -15 14 -13
EGADS    :      4   -3 18 19 -20
EGADS    :      5   21 22 -23 5
EGADS    :      6   23 24 -21 6 25 26
EGADS    :      7   -19 27 7 -28
EGADS    :      8   -29 8 12 -33 -32 31 30
EGADS    :      9   -34 -10 36 -35 37 38
EGADS    :     10   -36 -11 34 -39
EGADS    :     11   13 40 41 33
EGADS    :     12   -17 20 46 45 44 -40 -14 -43 -42
EGADS    :     13   47 48 -49 43 15
EGADS    :     14   49 50 -47 16 42
EGADS    :     15   51 53 -52 -22
EGADS    :     16   52 54 -51 -24
EGADS    :     17   -55 57 -25 -56
EGADS    :     18   -57 58 56 -26
EGADS    :     19   -46 28 29 61 60 32 -41 -44 59
EGADS    :     20   -62 -61 -30 64 -63
EGADS    :     21   -64 -31 -60 62 -65
EGADS    :     22   -66 35 67 -68
EGADS    :     23   69 70 -37 -71
EGADS    :     24   71 -38 -70 -72
EGADS    :     25   -67 39 66 -73
EGADS    :     26   -74 -45 76 -75
EGADS    :     27   -48 -50
EGADS    :     28   -53 -54
EGADS    :     29   77 55 78 79 -80 -81
EGADS    :     30   -77 83 80 -82 -78 -58
EGADS    :     31   -76 -59 74 -84
EGADS    :     32   65 63
EGADS    :     33   73 68
EGADS    :     34   85 -69 86 87 -88 -89
EGADS    :     35   -85 91 88 -90 -86 72
EGADS    :     36   75 84
EGADS    :     37   -79 92 81 -93
EGADS    :     38   82 93 -83 -92
EGADS    :     39   -87 94 89 -95
EGADS    :     40   90 95 -91 -94
EGADS    :     41   96 97 -98 -99
EGADS    :     42   -100 103 102 -101
EGADS    :     43   104 100 -105 -96
EGADS    :     44   -106 98 107 -102
EGADS    :     45   99 106 -103 -104
EGADS    :     46   -97 105 101 -107

EGADS    : Face Loops Information

EGADS    :   Face   Loops
EGADS    :      1   1 2
EGADS    :      2   3 4
EGADS    :      3   5
EGADS    :      4   6
EGADS    :      5   7
EGADS    :      6   8 9
EGADS    :      7   10
EGADS    :      8   11
EGADS    :      9   12 13
EGADS    :     10   14
EGADS    :     11   15
EGADS    :     12   16
EGADS    :     13   17
EGADS    :     14   18
EGADS    :     15   19
EGADS    :     16   20
EGADS    :     17   21
EGADS    :     18   22
EGADS    :     19   23
EGADS    :     20   24
EGADS    :     21   25
EGADS    :     22   26
EGADS    :     23   27
EGADS    :     24   28
EGADS    :     25   29
EGADS    :     26   30
EGADS    :     27   31
EGADS    :     28   32
EGADS    :     29   33
EGADS    :     30   34
EGADS    :     31   35
EGADS    :     32   36
EGADS    :     33   37
EGADS    :     34   38
EGADS    :     35   39
EGADS    :     36   40
EGADS    :     37   41
EGADS    :     38   42
EGADS    :     39   43
EGADS    :     40   44
EGADS    :     41   45
EGADS    :     42   46
EGADS    :     43   47
EGADS    :     44   48
EGADS    :     45   49
EGADS    :     46   50

EGADS    : Loop Edges Information

EGADS    :   Loop  Active   Edges
EGADS    :      1     Yes   -1 4 3 -2
EGADS    :      2     Yes   -5 -6
EGADS    :      3     Yes   -7 9 1 -8
EGADS    :      4     Yes   10 11
EGADS    :      5     Yes   -12 2 17 -16 -15 14 -13
EGADS    :      6     Yes   -3 18 19 -20
EGADS    :      7     Yes   21 22 -23 5
EGADS    :      8     Yes   23 24 -21 6
EGADS    :      9     Yes   25 26
EGADS    :     10     Yes   -19 27 7 -28
EGADS    :     11     Yes   -29 8 12 -33 -32 31 30
EGADS    :     12     Yes   -34 -10 36 -35
EGADS    :     13     Yes   37 38
EGADS    :     14     Yes   -36 -11 34 -39
EGADS    :     15     Yes   13 40 41 33
EGADS    :     16     Yes   -17 20 46 45 44 -40 -14 -43 -42
EGADS    :     17     Yes   47 48 -49 43 15
EGADS    :     18     Yes   49 50 -47 16 42
EGADS    :     19     Yes   51 53 -52 -22
EGADS    :     20     Yes   52 54 -51 -24
EGADS    :     21     Yes   -55 57 -25 -56
EGADS    :     22     Yes   -57 58 56 -26
EGADS    :     23     Yes   -46 28 29 61 60 32 -41 -44 59
EGADS    :     24     Yes   -62 -61 -30 64 -63
EGADS    :     25     Yes   -64 -31 -60 62 -65
EGADS    :     26     Yes   -66 35 67 -68
EGADS    :     27     Yes   69 70 -37 -71
EGADS    :     28     Yes   71 -38 -70 -72
EGADS    :     29     Yes   -67 39 66 -73
EGADS    :     30     Yes   -74 -45 76 -75
EGADS    :     31     Yes   -48 -50
EGADS    :     32     Yes   -53 -54
EGADS    :     33     Yes   77 55 78 79 -80 -81
EGADS    :     34     Yes   -77 83 80 -82 -78 -58
EGADS    :     35     Yes   -76 -59 74 -84
EGADS    :     36     Yes   65 63
EGADS    :     37     Yes   73 68
EGADS    :     38     Yes   85 -69 86 87 -88 -89
EGADS    :     39     Yes   -85 91 88 -90 -86 72
EGADS    :     40     Yes   75 84
EGADS    :     41     Yes   -79 92 81 -93
EGADS    :     42     Yes   82 93 -83 -92
EGADS    :     43     Yes   -87 94 89 -95
EGADS    :     44     Yes   90 95 -91 -94
EGADS    :     45     Yes   96 97 -98 -99
EGADS    :     46     Yes   -100 103 102 -101
EGADS    :     47     Yes   104 100 -105 -96
EGADS    :     48     Yes   -106 98 107 -102
EGADS    :     49     Yes   99 106 -103 -104
EGADS    :     50     Yes   -97 105 101 -107

EGADS    : Edge Node, Scale Factor, and Neighbor-Faces Information

EGADS    : ESF = Edge Scale Factor
EGADS    :       Not applicable for DEGENERATE Edges or Edges with a FarField
EGADS    :       Grid BC Neighbor Face.

EGADS    :                                             Neighbor
EGADS    :   Edge  Body  Active Node1 Node2      ESF   Faces
EGADS    :      1     0     Yes     1     2        1   1 2
EGADS    :      2     0     Yes     2     3        1   1 3
EGADS    :      3     0     Yes     1     3        1   1 4
EGADS    :      4     0   DEGEN     1     1        -   1
EGADS    :      5     0     Yes     4     5        1   1 5
EGADS    :      6     0     Yes     5     4        1   1 6
EGADS    :      7     0     Yes     1     6        1   2 7
EGADS    :      8     0     Yes     6     2        1   2 8
EGADS    :      9     0   DEGEN     1     1        -   2
EGADS    :     10     0     Yes     7     8        1   2 9
EGADS    :     11     0     Yes     8     7        1   2 10
EGADS    :     12     0     Yes     2     9        1   3 8
EGADS    :     13     0     Yes     9    10        1   3 11
EGADS    :     14     0     Yes    11    10        1   3 12
EGADS    :     15     0     Yes    11    12        1   3 13
EGADS    :     16     0     Yes    12    13        1   3 14
EGADS    :     17     0     Yes     3    13        1   3 12
EGADS    :     18     0   DEGEN     1     1        -   4
EGADS    :     19     0     Yes     1    14        1   4 7
EGADS    :     20     0     Yes     3    14        1   4 12
EGADS    :     21     0     Yes     5    15        1   5 6
EGADS    :     22     0     Yes    15    16        1   5 15
EGADS    :     23     0     Yes     4    16        1   5 6
EGADS    :     24     0     Yes    16    15        1   6 16
EGADS    :     25     0     Yes    17    18        1   6 17
EGADS    :     26     0     Yes    18    17        1   6 18
EGADS    :     27     0   DEGEN     1     1        -   7
EGADS    :     28     0     Yes    14     6        1   7 19
EGADS    :     29     0     Yes     6    19        1   8 19
EGADS    :     30     0     Yes    20    19        1   8 20
EGADS    :     31     0     Yes    21    20        1   8 21
EGADS    :     32     0     Yes    21    22        1   8 19
EGADS    :     33     0     Yes    22     9        1   8 11
EGADS    :     34     0     Yes     8    23        1   9 10
EGADS    :     35     0     Yes    23    24        1   9 22
EGADS    :     36     0     Yes     7    24        1   9 10
EGADS    :     37     0     Yes    25    26        1   9 23
EGADS    :     38     0     Yes    26    25        1   9 24
EGADS    :     39     0     Yes    24    23        1   10 25
EGADS    :     40     0     Yes    10    27        1   11 12
EGADS    :     41     0     Yes    27    22        1   11 19
EGADS    :     42     0     Yes    13    28        1   12 14
EGADS    :     43     0     Yes    28    11        1   12 13
EGADS    :     44     0     Yes    29    27        1   12 19
EGADS    :     45     0     Yes    30    29        1   12 26
EGADS    :     46     0     Yes    14    30        1   12 19
EGADS    :     47     0     Yes    12    31        1   13 14
EGADS    :     48     0     Yes    31    32        1   13 27
EGADS    :     49     0     Yes    28    32        1   13 14
EGADS    :     50     0     Yes    32    31        1   14 27
EGADS    :     51     0     Yes    15    33        1   15 16
EGADS    :     52     0     Yes    16    34        1   15 16
EGADS    :     53     0     Yes    33    34        1   15 28
EGADS    :     54     0     Yes    34    33        1   16 28
EGADS    :     55     0     Yes    35    36        1   17 29
EGADS    :     56     0     Yes    36    17        1   17 18
EGADS    :     57     0     Yes    35    18        1   17 18
EGADS    :     58     0     Yes    35    36        1   18 30
EGADS    :     59     0     Yes    29    30        1   19 31
EGADS    :     60     0     Yes    37    21        1   19 21
EGADS    :     61     0     Yes    19    37        1   19 20
EGADS    :     62     0     Yes    37    38        1   20 21
EGADS    :     63     0     Yes    38    39        1   20 32
EGADS    :     64     0     Yes    20    39        1   20 21
EGADS    :     65     0     Yes    39    38        1   21 32
EGADS    :     66     0     Yes    23    40        1   22 25
EGADS    :     67     0     Yes    24    41        1   22 25
EGADS    :     68     0     Yes    40    41        1   22 33
EGADS    :     69     0     Yes    42    43        1   23 34
EGADS    :     70     0     Yes    43    26        1   23 24
EGADS    :     71     0     Yes    42    25        1   23 24
EGADS    :     72     0     Yes    42    43        1   24 35
EGADS    :     73     0     Yes    41    40        1   25 33
EGADS    :     74     0     Yes    29    44        1   26 31
EGADS    :     75     0     Yes    44    45        1   26 36
EGADS    :     76     0     Yes    30    45        1   26 31
EGADS    :     77     0     Yes    46    35        1   29 30
EGADS    :     78     0     Yes    36    47        1   29 30
EGADS    :     79     0     Yes    47    48        1   29 37
EGADS    :     80     0     Yes    49    48        1   29 30
EGADS    :     81     0     Yes    46    49        1   29 37
EGADS    :     82     0     Yes    47    48        1   30 38
EGADS    :     83     0     Yes    46    49        1   30 38
EGADS    :     84     0     Yes    45    44        1   31 36
EGADS    :     85     0     Yes    50    43        1   34 35
EGADS    :     86     0     Yes    42    51        1   34 35
EGADS    :     87     0     Yes    51    52        1   34 39
EGADS    :     88     0     Yes    53    52        1   34 35
EGADS    :     89     0     Yes    50    53        1   34 39
EGADS    :     90     0     Yes    51    52        1   35 40
EGADS    :     91     0     Yes    50    53        1   35 40
EGADS    :     92     0     Yes    47    46        1   37 38
EGADS    :     93     0     Yes    48    49        1   37 38
EGADS    :     94     0     Yes    51    50        1   39 40
EGADS    :     95     0     Yes    52    53        1   39 40
EGADS    :     96     1     Yes    55    54       NA   41 43
EGADS    :     97     1     Yes    54    56       NA   41 46
EGADS    :     98     1     Yes    57    56       NA   41 44
EGADS    :     99     1     Yes    55    57       NA   41 45
EGADS    :    100     1     Yes    59    58       NA   42 43
EGADS    :    101     1     Yes    58    60       NA   42 46
EGADS    :    102     1     Yes    61    60       NA   42 44
EGADS    :    103     1     Yes    59    61       NA   42 45
EGADS    :    104     1     Yes    55    59       NA   43 45
EGADS    :    105     1     Yes    54    58       NA   43 46
EGADS    :    106     1     Yes    57    61       NA   44 45
EGADS    :    107     1     Yes    56    60       NA   44 46

EGADS    : Node Information

EGADS    :   Node  Active      Coordinates
EGADS    :      1     Yes                0                0                0
EGADS    :      2     Yes       121.026192                0                0
EGADS    :      3     Yes       121.026192               10                0
EGADS    :      4     Yes       54.9020417       7.00084115                0
EGADS    :      5     Yes        97.361045       7.90366896                0
EGADS    :      6     Yes       121.026192                0                0
EGADS    :      7     Yes        97.361045                0                0
EGADS    :      8     Yes       54.9020417                0                0
EGADS    :      9     Yes       165.026192                0                7
EGADS    :     10     Yes       165.026192              0.5              8.5
EGADS    :     11     Yes       156.577382       2.32417494       6.86784347
EGADS    :     12     Yes       160.457816       1.16501909       6.24763245
EGADS    :     13     Yes       152.092394       3.29252447       6.00142548
EGADS    :     14     Yes       121.026192                0               10
EGADS    :     15     Yes       97.9335611       36.1389817                0
EGADS    :     16     Yes       75.3047874       36.1389817                0
EGADS    :     17     Yes       72.4759225       29.3018771                0
EGADS    :     18     Yes       83.5054156       29.3018771                0
EGADS    :     19     Yes       152.092394                0       6.00142548
EGADS    :     20     Yes       160.457816                0       6.24763245
EGADS    :     21     Yes       156.577382                0       6.86784347
EGADS    :     22     Yes       165.026192                0              8.5
EGADS    :     23     Yes       75.3047874                0                0
EGADS    :     24     Yes       97.9335611                0                0
EGADS    :     25     Yes       72.4759225                0                0
EGADS    :     26     Yes       83.5054156                0                0
EGADS    :     27     Yes       165.026192                0               10
EGADS    :     28     Yes       139.227902       5.03861756       7.07099122
EGADS    :     29     Yes       159.822328                0               10
EGADS    :     30     Yes       137.454662                0               10
EGADS    :     31     Yes       173.282633        35.781198       13.6055284
EGADS    :     32     Yes        165.02399        35.781198       13.6055284
EGADS    :     33     Yes       123.552357       97.6729236        4.7180639
EGADS    :     34     Yes       118.391317       97.6729236       3.99272703
EGADS    :     35     Yes       79.4370049       29.3018771                0
EGADS    :     36     Yes        70.524066       29.3018771                0
EGADS    :     37     Yes       139.227902                0       7.07099122
EGADS    :     38     Yes        165.02399                0       13.6055284
EGADS    :     39     Yes       173.282633                0       13.6055284
EGADS    :     40     Yes       118.391317                0       3.99272703
EGADS    :     41     Yes       123.552357                0        4.7180639
EGADS    :     42     Yes        70.524066                0                0
EGADS    :     43     Yes       79.4370049                0                0
EGADS    :     44     Yes        169.38016                0        35.487551
EGADS    :     45     Yes       162.942213                0        35.487551
EGADS    :     46     Yes       90.5173952       29.3018771                0
EGADS    :     47     Yes       60.5173952       29.3018771                0
EGADS    :     48     Yes       60.5173952       29.3018771                0
EGADS    :     49     Yes       90.5173952       29.3018771                0
EGADS    :     50     Yes       90.5173952                0                0
EGADS    :     51     Yes       60.5173952                0                0
EGADS    :     52     Yes       60.5173952                0                0
EGADS    :     53     Yes       90.5173952                0                0
EGADS    :     54     Yes                0                0       1962.43554
EGADS    :     55     Yes                0                0                0
EGADS    :     56     Yes                0       1953.45847       1962.43554
EGADS    :     57     Yes                0       1953.45847                0
EGADS    :     58     Yes       2040.09979                0       1962.43554
EGADS    :     59     Yes       2040.09979                0                0
EGADS    :     60     Yes       2040.09979       1953.45847       1962.43554
EGADS    :     61     Yes       2040.09979       1953.45847                0

EGADS    : Face and Edge Match Information

EGADS    : No Face Matches Found

AFLR4    : Surface Mesh Spacing Setup

AFLR4    : Max Bounding Box Length     = 3906.92
AFLR4    : Min Bounding Box Length     = 3906.92
AFLR4    : Max Ref Bounding Box Length = 195.346
AFLR4    : Min Ref Bounding Box Length = 53.021
AFLR4    : Reference Length            = 21.7051
AFLR4    : BL Thickness                = 0
AFLR4    : FarField Spacing            = 1060.6
AFLR4    : Abs Min Surf Spacing        = 0.0542627
AFLR4    : Min Surf Spacing            = 0.108525
AFLR4    : Max Surf Spacing            = 2.17051
AFLR4    : Global Scale Factor         = 2

AFLR4    : Geometry Definition Information

AFLR4    : Definition              Definition   Composite             Grid BC
AFLR4    :         ID                    Type          ID                Type
AFLR4    :          0     glue-only composite           -                   -
AFLR4    :          1            CAD geometry           0            STD w/BL
AFLR4    :          2            CAD geometry           0            STD w/BL
AFLR4    :          3            CAD geometry           0            STD w/BL
AFLR4    :          4            CAD geometry           0            STD w/BL
AFLR4    :          5            CAD geometry           0            STD w/BL
AFLR4    :          6            CAD geometry           0            STD w/BL
AFLR4    :          7            CAD geometry           0            STD w/BL
AFLR4    :          8            CAD geometry           0            STD w/BL
AFLR4    :          9            CAD geometry           0            STD w/BL
AFLR4    :         10            CAD geometry           0            STD w/BL
AFLR4    :         11            CAD geometry           0            STD w/BL
AFLR4    :         12            CAD geometry           0            STD w/BL
AFLR4    :         13            CAD geometry           0            STD w/BL
AFLR4    :         14            CAD geometry           0            STD w/BL
AFLR4    :         15            CAD geometry           0            STD w/BL
AFLR4    :         16            CAD geometry           0            STD w/BL
AFLR4    :         17            CAD geometry           0            STD w/BL
AFLR4    :         18            CAD geometry           0            STD w/BL
AFLR4    :         19            CAD geometry           0            STD w/BL
AFLR4    :         20            CAD geometry           0            STD w/BL
AFLR4    :         21            CAD geometry           0            STD w/BL
AFLR4    :         22            CAD geometry           0            STD w/BL
AFLR4    :         23            CAD geometry           0            STD w/BL
AFLR4    :         24            CAD geometry           0            STD w/BL
AFLR4    :         25            CAD geometry           0            STD w/BL
AFLR4    :         26            CAD geometry           0            STD w/BL
AFLR4    :         27            CAD geometry           0            STD w/BL
AFLR4    :         28            CAD geometry           0            STD w/BL
AFLR4    :         29            CAD geometry           0            STD w/BL
AFLR4    :         30            CAD geometry           0            STD w/BL
AFLR4    :         31            CAD geometry           0            STD w/BL
AFLR4    :         32            CAD geometry           0            STD w/BL
AFLR4    :         33            CAD geometry           0            STD w/BL
AFLR4    :         34            CAD geometry           0            STD w/BL
AFLR4    :         35            CAD geometry           0            STD w/BL
AFLR4    :         36            CAD geometry           0            STD w/BL
AFLR4    :         37            CAD geometry           0            STD w/BL
AFLR4    :         38            CAD geometry           0            STD w/BL
AFLR4    :         39            CAD geometry           0            STD w/BL
AFLR4    :         40            CAD geometry           0            STD w/BL
AFLR4    :         41            CAD geometry           0            FARFIELD
AFLR4    :         42            CAD geometry           0            FARFIELD
AFLR4    :         43            CAD geometry           0            FARFIELD
AFLR4    :         44            CAD geometry           0            FARFIELD
AFLR4    :         45            CAD geometry           0            FARFIELD
AFLR4    :         46            CAD geometry           0            FARFIELD

AFLR4    : Case has 6 Proximity Checking Components

AFLR4    : Component 1 includes Definitions 1 2 3 4 7 8 11 12 19
AFLR4    : Component 2 includes Definitions 5 6 9 10 15 16 22 25 28 33
AFLR4    : Component 3 includes Definitions 13 14 20 21 27 32
AFLR4    : Component 4 includes Definitions 26 31 36
AFLR4    : Component 5 includes Definitions 29 30 34 35 37 38 39 40
AFLR4    : Component 6 includes Definitions 17 18 23 24

AFLR4    : Define CAD surface definition 1
AFLR4    : Define CAD surface definition 2
AFLR4    : Define CAD surface definition 3
AFLR4    : Define CAD surface definition 4
AFLR4    : Define CAD surface definition 5
AFLR4    : Define CAD surface definition 6
AFLR4    : Define CAD surface definition 7
AFLR4    : Define CAD surface definition 8
AFLR4    : Define CAD surface definition 9
AFLR4    : Define CAD surface definition 10
AFLR4    : Define CAD surface definition 11
AFLR4    : Define CAD surface definition 12
AFLR4    : Define CAD surface definition 13
AFLR4    : Define CAD surface definition 14
AFLR4    : Define CAD surface definition 15
AFLR4    : Define CAD surface definition 16
AFLR4    : Define CAD surface definition 17
AFLR4    : Define CAD surface definition 18
AFLR4    : Define CAD surface definition 19
AFLR4    : Define CAD surface definition 20
AFLR4    : Define CAD surface definition 21
AFLR4    : Define CAD surface definition 22
AFLR4    : Define CAD surface definition 23
AFLR4    : Define CAD surface definition 24
AFLR4    : Define CAD surface definition 25
AFLR4    : Define CAD surface definition 26
AFLR4    : Define CAD surface definition 27
AFLR4    : Define CAD surface definition 28
AFLR4    : Define CAD surface definition 29
AFLR4    : Define CAD surface definition 30
AFLR4    : Define CAD surface definition 31
AFLR4    : Define CAD surface definition 32
AFLR4    : Define CAD surface definition 33
AFLR4    : Define CAD surface definition 34
AFLR4    : Define CAD surface definition 35
AFLR4    : Define CAD surface definition 36
AFLR4    : Define CAD surface definition 37
AFLR4    : Define CAD surface definition 38
AFLR4    : Define CAD surface definition 39
AFLR4    : Define CAD surface definition 40
AFLR4    : Define CAD surface definition 41
AFLR4    : Define CAD surface definition 42
AFLR4    : Define CAD surface definition 43
AFLR4    : Define CAD surface definition 44
AFLR4    : Define CAD surface definition 45
AFLR4    : Define CAD surface definition 46

AFLR4    : Surface Grid Generation

AFLR4    : Generate optimal mesh on surface definition 1
AFLR2    : Nodes, Trias,Quads=       327       522         0
AFLR4    : Nodes, Trias,Quads=       305       478         0

AFLR4    : Generate optimal mesh on surface definition 2
AFLR2    : Nodes, Trias,Quads=       329       526         0
AFLR4    : Nodes, Trias,Quads=       303       474         0

AFLR4    : Generate optimal mesh on surface definition 3
AFLR2    : Nodes, Trias,Quads=       207       346         0
AFLR4    : Nodes, Trias,Quads=       137       206         0

AFLR4    : Generate optimal mesh on surface definition 4
AFLR2    : Nodes, Trias,Quads=       192       299         0
AFLR4    : Nodes, Trias,Quads=       210       335         0

AFLR4    : Generate optimal mesh on surface definition 5
AFLR2    : Nodes, Trias,Quads=       720      1326         0
AFLR4    : Nodes, Trias,Quads=       529       944         0

AFLR4    : Generate optimal mesh on surface definition 6
AFLR2    : Nodes, Trias,Quads=       997      1847         0
AFLR4    : Nodes, Trias,Quads=       752      1357         0

AFLR4    : Generate optimal mesh on surface definition 7
AFLR2    : Nodes, Trias,Quads=       192       299         0
AFLR4    : Nodes, Trias,Quads=       209       333         0

AFLR4    : Generate optimal mesh on surface definition 8
AFLR2    : Nodes, Trias,Quads=       206       344         0
AFLR4    : Nodes, Trias,Quads=       136       204         0

AFLR4    : Generate optimal mesh on surface definition 9
AFLR2    : Nodes, Trias,Quads=       997      1847         0
AFLR4    : Nodes, Trias,Quads=       746      1345         0

AFLR4    : Generate optimal mesh on surface definition 10
AFLR2    : Nodes, Trias,Quads=       714      1314         0
AFLR4    : Nodes, Trias,Quads=       521       928         0

AFLR4    : Generate optimal mesh on surface definition 11
AFLR2    : Nodes, Trias,Quads=        34        46         0
AFLR4    : Nodes, Trias,Quads=        32        42         0

AFLR4    : Generate optimal mesh on surface definition 12
AFLR2    : Nodes, Trias,Quads=       731      1320         0
AFLR4    : Nodes, Trias,Quads=       492       842         0

AFLR4    : Generate optimal mesh on surface definition 13
AFLR2    : Nodes, Trias,Quads=      1370      2586         0
AFLR4    : Nodes, Trias,Quads=       805      1456         0

AFLR4    : Generate optimal mesh on surface definition 14
AFLR2    : Nodes, Trias,Quads=      1357      2560         0
AFLR4    : Nodes, Trias,Quads=       802      1450         0

AFLR4    : Generate optimal mesh on surface definition 15
AFLR2    : Nodes, Trias,Quads=      1943      3668         0
AFLR4    : Nodes, Trias,Quads=       877      1536         0

AFLR4    : Generate optimal mesh on surface definition 16
AFLR2    : Nodes, Trias,Quads=      1868      3519         0
AFLR4    : Nodes, Trias,Quads=       849      1481         0

AFLR4    : Generate optimal mesh on surface definition 17
AFLR2    : Nodes, Trias,Quads=       150       248         0
AFLR4    : Nodes, Trias,Quads=        96       140         0

AFLR4    : Generate optimal mesh on surface definition 18
AFLR2    : Nodes, Trias,Quads=       158       264         0
AFLR4    : Nodes, Trias,Quads=        98       144         0

AFLR4    : Generate optimal mesh on surface definition 19
AFLR2    : Nodes, Trias,Quads=       850      1558         0
AFLR4    : Nodes, Trias,Quads=       456       770         0

AFLR4    : Generate optimal mesh on surface definition 20
AFLR2    : Nodes, Trias,Quads=      1363      2572         0
AFLR4    : Nodes, Trias,Quads=       809      1464         0

AFLR4    : Generate optimal mesh on surface definition 21
AFLR2    : Nodes, Trias,Quads=      1368      2582         0
AFLR4    : Nodes, Trias,Quads=       808      1462         0

AFLR4    : Generate optimal mesh on surface definition 22
AFLR2    : Nodes, Trias,Quads=      1874      3531         0
AFLR4    : Nodes, Trias,Quads=       851      1485         0

AFLR4    : Generate optimal mesh on surface definition 23
AFLR2    : Nodes, Trias,Quads=       157       262         0
AFLR4    : Nodes, Trias,Quads=        98       144         0

AFLR4    : Generate optimal mesh on surface definition 24
AFLR2    : Nodes, Trias,Quads=       152       252         0
AFLR4    : Nodes, Trias,Quads=        95       138         0

AFLR4    : Generate optimal mesh on surface definition 25
AFLR2    : Nodes, Trias,Quads=      1914      3610         0
AFLR4    : Nodes, Trias,Quads=       872      1526         0

AFLR4    : Generate optimal mesh on surface definition 26
AFLR2    : Nodes, Trias,Quads=      1258      2369         0
AFLR4    : Nodes, Trias,Quads=       856      1565         0

AFLR4    : Generate optimal mesh on surface definition 27
AFLR2    : Nodes, Trias,Quads=        32        40         0
AFLR4    : Nodes, Trias,Quads=        22        20         0

AFLR4    : Generate optimal mesh on surface definition 28
AFLR2    : Nodes, Trias,Quads=        23        28         0
AFLR4    : Nodes, Trias,Quads=        16        14         0

AFLR4    : Generate optimal mesh on surface definition 29
AFLR2    : Nodes, Trias,Quads=      1026      1934         0
AFLR4    : Nodes, Trias,Quads=       996      1874         0

AFLR4    : Generate optimal mesh on surface definition 30
AFLR2    : Nodes, Trias,Quads=      1024      1930         0
AFLR4    : Nodes, Trias,Quads=      1031      1944         0

AFLR4    : Generate optimal mesh on surface definition 31
AFLR2    : Nodes, Trias,Quads=      1283      2419         0
AFLR4    : Nodes, Trias,Quads=       848      1549         0

AFLR4    : Generate optimal mesh on surface definition 32
AFLR2    : Nodes, Trias,Quads=        32        40         0
AFLR4    : Nodes, Trias,Quads=        22        20         0

AFLR4    : Generate optimal mesh on surface definition 33
AFLR2    : Nodes, Trias,Quads=        23        28         0
AFLR4    : Nodes, Trias,Quads=        16        14         0

AFLR4    : Generate optimal mesh on surface definition 34
AFLR2    : Nodes, Trias,Quads=      1022      1926         0
AFLR4    : Nodes, Trias,Quads=      1023      1928         0

AFLR4    : Generate optimal mesh on surface definition 35
AFLR2    : Nodes, Trias,Quads=      1026      1934         0
AFLR4    : Nodes, Trias,Quads=      1023      1928         0

AFLR4    : Generate optimal mesh on surface definition 36
AFLR2    : Nodes, Trias,Quads=        26        32         0
AFLR4    : Nodes, Trias,Quads=        18        16         0

AFLR4    : Generate optimal mesh on surface definition 37
AFLR2    : Nodes, Trias,Quads=       549       997         0
AFLR4    : Nodes, Trias,Quads=       465       829         0

AFLR4    : Generate optimal mesh on surface definition 38
AFLR2    : Nodes, Trias,Quads=       539       977         0
AFLR4    : Nodes, Trias,Quads=       461       821         0

AFLR4    : Generate optimal mesh on surface definition 39
AFLR2    : Nodes, Trias,Quads=       549       997         0
AFLR4    : Nodes, Trias,Quads=       465       829         0

AFLR4    : Generate optimal mesh on surface definition 40
AFLR2    : Nodes, Trias,Quads=       539       977         0
AFLR4    : Nodes, Trias,Quads=       461       821         0

AFLR4    : Generate optimal mesh on surface definition 41
AFLR2    : Nodes, Trias,Quads=        20        26         0
AFLR4    : Nodes, Trias,Quads=        16        18         0

AFLR4    : Generate optimal mesh on surface definition 42
AFLR2    : Nodes, Trias,Quads=        20        26         0
AFLR4    : Nodes, Trias,Quads=        16        18         0

AFLR4    : Generate optimal mesh on surface definition 43
AFLR2    : Nodes, Trias,Quads=        20        26         0
AFLR4    : Nodes, Trias,Quads=        16        18         0

AFLR4    : Generate optimal mesh on surface definition 44
AFLR2    : Nodes, Trias,Quads=        20        26         0
AFLR4    : Nodes, Trias,Quads=        16        18         0

AFLR4    : Generate optimal mesh on surface definition 45
AFLR2    : Nodes, Trias,Quads=        20        26         0
AFLR4    : Nodes, Trias,Quads=        16        18         0

AFLR4    : Generate optimal mesh on surface definition 46
AFLR2    : Nodes, Trias,Quads=        20        26         0
AFLR4    : Nodes, Trias,Quads=        16        18         0

DGEOM    : Add surface definitions to composite definition 0
DGEOM    : Glue composite surface definition 0
DGEOM    : Nodes,Faces,BEdges=     17482     34964      4366

AFLR4    : Curvature BG Surface Grid Generation

AFLR4    : Nodes, Faces      =     17482     34964

AFLR4    : Surface Grid Generation

AFLR4    : Generate optimal mesh on surface definition 1
AFLR2    : Nodes, Trias,Quads=       345       551         0
AFLR4    : Nodes, Trias,Quads=       528       917         0

AFLR4    : Generate optimal mesh on surface definition 2
AFLR2    : Nodes, Trias,Quads=       347       555         0
AFLR4    : Nodes, Trias,Quads=       516       893         0

AFLR4    : Generate optimal mesh on surface definition 3
AFLR2    : Nodes, Trias,Quads=       263       449         0
AFLR4    : Nodes, Trias,Quads=       182       287         0

AFLR4    : Generate optimal mesh on surface definition 4
AFLR2    : Nodes, Trias,Quads=       224       358         0
AFLR4    : Nodes, Trias,Quads=       237       384         0

AFLR4    : Generate optimal mesh on surface definition 5
AFLR2    : Nodes, Trias,Quads=       782      1447         0
AFLR4    : Nodes, Trias,Quads=       663      1209         0

AFLR4    : Generate optimal mesh on surface definition 6
AFLR2    : Nodes, Trias,Quads=      1016      1884         0
AFLR4    : Nodes, Trias,Quads=       903      1658         0

AFLR4    : Generate optimal mesh on surface definition 7
AFLR2    : Nodes, Trias,Quads=       222       354         0
AFLR4    : Nodes, Trias,Quads=       239       388         0

AFLR4    : Generate optimal mesh on surface definition 8
AFLR2    : Nodes, Trias,Quads=       252       427         0
AFLR4    : Nodes, Trias,Quads=       183       289         0

AFLR4    : Generate optimal mesh on surface definition 9
AFLR2    : Nodes, Trias,Quads=      1017      1886         0
AFLR4    : Nodes, Trias,Quads=       895      1642         0

AFLR4    : Generate optimal mesh on surface definition 10
AFLR2    : Nodes, Trias,Quads=       784      1451         0
AFLR4    : Nodes, Trias,Quads=       654      1191         0

AFLR4    : Generate optimal mesh on surface definition 11
AFLR2    : Nodes, Trias,Quads=        34        46         0
AFLR4    : Nodes, Trias,Quads=        32        42         0

AFLR4    : Generate optimal mesh on surface definition 12
AFLR2    : Nodes, Trias,Quads=       797      1447         0
AFLR4    : Nodes, Trias,Quads=       657      1167         0

AFLR4    : Generate optimal mesh on surface definition 13
AFLR2    : Nodes, Trias,Quads=      1388      2619         0
AFLR4    : Nodes, Trias,Quads=      1053      1949         0

AFLR4    : Generate optimal mesh on surface definition 14
AFLR2    : Nodes, Trias,Quads=      1387      2619         0
AFLR4    : Nodes, Trias,Quads=      1033      1911         0

AFLR4    : Generate optimal mesh on surface definition 15
AFLR2    : Nodes, Trias,Quads=      1858      3501         0
AFLR4    : Nodes, Trias,Quads=      1509      2803         0

AFLR4    : Generate optimal mesh on surface definition 16
AFLR2    : Nodes, Trias,Quads=      1856      3497         0
AFLR4    : Nodes, Trias,Quads=      1483      2751         0

AFLR4    : Generate optimal mesh on surface definition 17
AFLR2    : Nodes, Trias,Quads=       151       250         0
AFLR4    : Nodes, Trias,Quads=       104       156         0

AFLR4    : Generate optimal mesh on surface definition 18
AFLR2    : Nodes, Trias,Quads=       153       254         0
AFLR4    : Nodes, Trias,Quads=       106       160         0

AFLR4    : Generate optimal mesh on surface definition 19
AFLR2    : Nodes, Trias,Quads=       864      1581         0
AFLR4    : Nodes, Trias,Quads=       654      1161         0

AFLR4    : Generate optimal mesh on surface definition 20
AFLR2    : Nodes, Trias,Quads=      1408      2661         0
AFLR4    : Nodes, Trias,Quads=      1029      1903         0

AFLR4    : Generate optimal mesh on surface definition 21
AFLR2    : Nodes, Trias,Quads=      1379      2601         0
AFLR4    : Nodes, Trias,Quads=      1055      1953         0

AFLR4    : Generate optimal mesh on surface definition 22
AFLR2    : Nodes, Trias,Quads=      1878      3542         0
AFLR4    : Nodes, Trias,Quads=      1505      2796         0

AFLR4    : Generate optimal mesh on surface definition 23
AFLR2    : Nodes, Trias,Quads=       152       252         0
AFLR4    : Nodes, Trias,Quads=       107       162         0

AFLR4    : Generate optimal mesh on surface definition 24
AFLR2    : Nodes, Trias,Quads=       148       244         0
AFLR4    : Nodes, Trias,Quads=       107       162         0

AFLR4    : Generate optimal mesh on surface definition 25
AFLR2    : Nodes, Trias,Quads=      1877      3540         0
AFLR4    : Nodes, Trias,Quads=      1464      2714         0

AFLR4    : Generate optimal mesh on surface definition 26
AFLR2    : Nodes, Trias,Quads=      1251      2354         0
AFLR4    : Nodes, Trias,Quads=      1009      1870         0

AFLR4    : Generate optimal mesh on surface definition 27
AFLR2    : Nodes, Trias,Quads=        33        42         0
AFLR4    : Nodes, Trias,Quads=        22        20         0

AFLR4    : Generate optimal mesh on surface definition 28
AFLR2    : Nodes, Trias,Quads=        30        40         0
AFLR4    : Nodes, Trias,Quads=        18        16         0

AFLR4    : Generate optimal mesh on surface definition 29
AFLR2    : Nodes, Trias,Quads=      1050      1977         0
AFLR4    : Nodes, Trias,Quads=      1007      1891         0

AFLR4    : Generate optimal mesh on surface definition 30
AFLR2    : Nodes, Trias,Quads=      1063      2003         0
AFLR4    : Nodes, Trias,Quads=      1050      1977         0

AFLR4    : Generate optimal mesh on surface definition 31
AFLR2    : Nodes, Trias,Quads=      1283      2418         0
AFLR4    : Nodes, Trias,Quads=       993      1838         0

AFLR4    : Generate optimal mesh on surface definition 32
AFLR2    : Nodes, Trias,Quads=        33        42         0
AFLR4    : Nodes, Trias,Quads=        22        20         0

AFLR4    : Generate optimal mesh on surface definition 33
AFLR2    : Nodes, Trias,Quads=        30        40         0
AFLR4    : Nodes, Trias,Quads=        18        16         0

AFLR4    : Generate optimal mesh on surface definition 34
AFLR2    : Nodes, Trias,Quads=      1068      2013         0
AFLR4    : Nodes, Trias,Quads=      1038      1953         0

AFLR4    : Generate optimal mesh on surface definition 35
AFLR2    : Nodes, Trias,Quads=      1051      1979         0
AFLR4    : Nodes, Trias,Quads=      1060      1997         0

AFLR4    : Generate optimal mesh on surface definition 36
AFLR2    : Nodes, Trias,Quads=        26        32         0
AFLR4    : Nodes, Trias,Quads=        18        16         0

AFLR4    : Generate optimal mesh on surface definition 37
AFLR2    : Nodes, Trias,Quads=       614      1122         0
AFLR4    : Nodes, Trias,Quads=       538       970         0

AFLR4    : Generate optimal mesh on surface definition 38
AFLR2    : Nodes, Trias,Quads=       613      1120         0
AFLR4    : Nodes, Trias,Quads=       536       966         0

AFLR4    : Generate optimal mesh on surface definition 39
AFLR2    : Nodes, Trias,Quads=       614      1122         0
AFLR4    : Nodes, Trias,Quads=       538       970         0

AFLR4    : Generate optimal mesh on surface definition 40
AFLR2    : Nodes, Trias,Quads=       613      1120         0
AFLR4    : Nodes, Trias,Quads=       536       966         0

AFLR4    : Generate optimal mesh on surface definition 41
AFLR2    : Nodes, Trias,Quads=        20        26         0
AFLR4    : Nodes, Trias,Quads=        16        18         0

AFLR4    : Generate optimal mesh on surface definition 42
AFLR2    : Nodes, Trias,Quads=        20        26         0
AFLR4    : Nodes, Trias,Quads=        16        18         0

AFLR4    : Generate optimal mesh on surface definition 43
AFLR2    : Nodes, Trias,Quads=        20        26         0
AFLR4    : Nodes, Trias,Quads=        16        18         0

AFLR4    : Generate optimal mesh on surface definition 44
AFLR2    : Nodes, Trias,Quads=        20        26         0
AFLR4    : Nodes, Trias,Quads=        16        18         0

AFLR4    : Generate optimal mesh on surface definition 45
AFLR2    : Nodes, Trias,Quads=        20        26         0
AFLR4    : Nodes, Trias,Quads=        16        18         0

AFLR4    : Generate optimal mesh on surface definition 46
AFLR2    : Nodes, Trias,Quads=        20        26         0
AFLR4    : Nodes, Trias,Quads=        16        18         0

DGEOM    : Add surface definitions to composite definition 0
DGEOM    : Glue composite surface definition 0
DGEOM    : Nodes,Faces,BEdges=     23121     46242      4468

AFLR4    : Proximity BG Surface Grid Generation

AFLR4    : Nodes, Trias      =     24916     49832
AFLR4    : Nodes, Trias      =     25214     50428
AFLR4    : Nodes, Trias      =     25244     50488

AFLR4    : Surface Grid Generation

AFLR4    : Generate optimal mesh on surface definition 1
AFLR2    : Nodes, Trias,Quads=       846      1435         0
AFLR4    : Nodes, Trias,Quads=      1260      2263         0

AFLR4    : Generate optimal mesh on surface definition 2
AFLR2    : Nodes, Trias,Quads=       839      1423         0
AFLR4    : Nodes, Trias,Quads=      1223      2191         0

AFLR4    : Generate optimal mesh on surface definition 3
AFLR2    : Nodes, Trias,Quads=       542       968         0
AFLR4    : Nodes, Trias,Quads=       382       648         0

AFLR4    : Generate optimal mesh on surface definition 4
AFLR2    : Nodes, Trias,Quads=       488       851         0
AFLR4    : Nodes, Trias,Quads=       550       975         0

AFLR4    : Generate optimal mesh on surface definition 5
AFLR2    : Nodes, Trias,Quads=      2089      3983         0
AFLR4    : Nodes, Trias,Quads=      1392      2589         0

AFLR4    : Generate optimal mesh on surface definition 6
AFLR2    : Nodes, Trias,Quads=      2244      4252         0
AFLR4    : Nodes, Trias,Quads=      2188      4140         0

AFLR4    : Generate optimal mesh on surface definition 7
AFLR2    : Nodes, Trias,Quads=       525       921         0
AFLR4    : Nodes, Trias,Quads=       580      1031         0

AFLR4    : Generate optimal mesh on surface definition 8
AFLR2    : Nodes, Trias,Quads=       556       996         0
AFLR4    : Nodes, Trias,Quads=       378       640         0

AFLR4    : Generate optimal mesh on surface definition 9
AFLR2    : Nodes, Trias,Quads=      2230      4228         0
AFLR4    : Nodes, Trias,Quads=      2157      4082         0

AFLR4    : Generate optimal mesh on surface definition 10
AFLR2    : Nodes, Trias,Quads=      1987      3785         0
AFLR4    : Nodes, Trias,Quads=      1340      2491         0

AFLR4    : Generate optimal mesh on surface definition 11
AFLR2    : Nodes, Trias,Quads=        34        46         0
AFLR4    : Nodes, Trias,Quads=        32        42         0

AFLR4    : Generate optimal mesh on surface definition 12
AFLR2    : Nodes, Trias,Quads=      1255      2302         0
AFLR4    : Nodes, Trias,Quads=      1212      2216         0

AFLR4    : Generate optimal mesh on surface definition 13
AFLR2    : Nodes, Trias,Quads=      1787      3375         0
AFLR4    : Nodes, Trias,Quads=      1433      2667         0

AFLR4    : Generate optimal mesh on surface definition 14
AFLR2    : Nodes, Trias,Quads=      1950      3690         0
AFLR4    : Nodes, Trias,Quads=      1464      2718         0

AFLR4    : Generate optimal mesh on surface definition 15
AFLR2    : Nodes, Trias,Quads=      2205      4188         0
AFLR4    : Nodes, Trias,Quads=      1705      3188         0

AFLR4    : Generate optimal mesh on surface definition 16
AFLR2    : Nodes, Trias,Quads=      2214      4206         0
AFLR4    : Nodes, Trias,Quads=      1671      3120         0

AFLR4    : Generate optimal mesh on surface definition 17
AFLR2    : Nodes, Trias,Quads=       867      1604         0
AFLR4    : Nodes, Trias,Quads=       540       950         0

AFLR4    : Generate optimal mesh on surface definition 18
AFLR2    : Nodes, Trias,Quads=       781      1440         0
AFLR4    : Nodes, Trias,Quads=       488       854         0

AFLR4    : Generate optimal mesh on surface definition 19
AFLR2    : Nodes, Trias,Quads=      1504      2802         0
AFLR4    : Nodes, Trias,Quads=      1199      2192         0

AFLR4    : Generate optimal mesh on surface definition 20
AFLR2    : Nodes, Trias,Quads=      1929      3652         0
AFLR4    : Nodes, Trias,Quads=      1446      2686         0

AFLR4    : Generate optimal mesh on surface definition 21
AFLR2    : Nodes, Trias,Quads=      1717      3238         0
AFLR4    : Nodes, Trias,Quads=      1404      2612         0

AFLR4    : Generate optimal mesh on surface definition 22
AFLR2    : Nodes, Trias,Quads=      2202      4184         0
AFLR4    : Nodes, Trias,Quads=      1664      3108         0

AFLR4    : Generate optimal mesh on surface definition 23
AFLR2    : Nodes, Trias,Quads=       740      1361         0
AFLR4    : Nodes, Trias,Quads=       455       791         0

AFLR4    : Generate optimal mesh on surface definition 24
AFLR2    : Nodes, Trias,Quads=       829      1531         0
AFLR4    : Nodes, Trias,Quads=       516       905         0

AFLR4    : Generate optimal mesh on surface definition 25
AFLR2    : Nodes, Trias,Quads=      2226      4231         0
AFLR4    : Nodes, Trias,Quads=      1646      3071         0

AFLR4    : Generate optimal mesh on surface definition 26
AFLR2    : Nodes, Trias,Quads=      1507      2846         0
AFLR4    : Nodes, Trias,Quads=      1151      2134         0

AFLR4    : Generate optimal mesh on surface definition 27
AFLR2    : Nodes, Trias,Quads=        35        45         0
AFLR4    : Nodes, Trias,Quads=        23        21         0

AFLR4    : Generate optimal mesh on surface definition 28
AFLR2    : Nodes, Trias,Quads=        27        34         0
AFLR4    : Nodes, Trias,Quads=        18        16         0

AFLR4    : Generate optimal mesh on surface definition 29
AFLR2    : Nodes, Trias,Quads=      1742      3319         0
AFLR4    : Nodes, Trias,Quads=      1421      2677         0

AFLR4    : Generate optimal mesh on surface definition 30
AFLR2    : Nodes, Trias,Quads=      1706      3250         0
AFLR4    : Nodes, Trias,Quads=      1419      2676         0

AFLR4    : Generate optimal mesh on surface definition 31
AFLR2    : Nodes, Trias,Quads=      1521      2874         0
AFLR4    : Nodes, Trias,Quads=      1145      2122         0

AFLR4    : Generate optimal mesh on surface definition 32
AFLR2    : Nodes, Trias,Quads=        33        42         0
AFLR4    : Nodes, Trias,Quads=        22        20         0

AFLR4    : Generate optimal mesh on surface definition 33
AFLR2    : Nodes, Trias,Quads=        30        39         0
AFLR4    : Nodes, Trias,Quads=        19        17         0

AFLR4    : Generate optimal mesh on surface definition 34
AFLR2    : Nodes, Trias,Quads=      1700      3238         0
AFLR4    : Nodes, Trias,Quads=      1405      2648         0

AFLR4    : Generate optimal mesh on surface definition 35
AFLR2    : Nodes, Trias,Quads=      1792      3419         0
AFLR4    : Nodes, Trias,Quads=      1444      2723         0

AFLR4    : Generate optimal mesh on surface definition 36
AFLR2    : Nodes, Trias,Quads=        30        38         0
AFLR4    : Nodes, Trias,Quads=        20        18         0

AFLR4    : Generate optimal mesh on surface definition 37
AFLR2    : Nodes, Trias,Quads=       617      1127         0
AFLR4    : Nodes, Trias,Quads=       563      1019         0

AFLR4    : Generate optimal mesh on surface definition 38
AFLR2    : Nodes, Trias,Quads=       618      1129         0
AFLR4    : Nodes, Trias,Quads=       558      1009         0

AFLR4    : Generate optimal mesh on surface definition 39
AFLR2    : Nodes, Trias,Quads=       617      1127         0
AFLR4    : Nodes, Trias,Quads=       563      1019         0

AFLR4    : Generate optimal mesh on surface definition 40
AFLR2    : Nodes, Trias,Quads=       618      1129         0
AFLR4    : Nodes, Trias,Quads=       558      1009         0

AFLR4    : Generate optimal mesh on surface definition 41
AFLR2    : Nodes, Trias,Quads=        20        26         0
AFLR4    : Nodes, Trias,Quads=        16        18         0

AFLR4    : Generate optimal mesh on surface definition 42
AFLR2    : Nodes, Trias,Quads=        20        26         0
AFLR4    : Nodes, Trias,Quads=        16        18         0

AFLR4    : Generate optimal mesh on surface definition 43
AFLR2    : Nodes, Trias,Quads=        20        26         0
AFLR4    : Nodes, Trias,Quads=        16        18         0

AFLR4    : Generate optimal mesh on surface definition 44
AFLR2    : Nodes, Trias,Quads=        20        26         0
AFLR4    : Nodes, Trias,Quads=        16        18         0

AFLR4    : Generate optimal mesh on surface definition 45
AFLR2    : Nodes, Trias,Quads=        20        26         0
AFLR4    : Nodes, Trias,Quads=        16        18         0

AFLR4    : Generate optimal mesh on surface definition 46
AFLR2    : Nodes, Trias,Quads=        20        26         0
AFLR4    : Nodes, Trias,Quads=        16        18         0

DGEOM    : Add surface definitions to composite definition 0
DGEOM    : Glue composite surface definition 0
DGEOM    : Nodes,Faces,BEdges=     35703     71406      6010

OVERALL  : CPU Time          =     1.966   seconds
Body 1 (of 2)
Number of nodes    = 35647
Number of elements = 71298
Number of triangle elements      = 71298
Number of quadrilateral elements = 0
Body 2 (of 2)
Number of nodes    = 56
Number of elements = 108
Number of triangle elements      = 108
Number of quadrilateral elements = 0
----------------------------
Total number of nodes    = 35703
Total number of elements = 71406
Total number of triangle elements      = 71406
Total number of quadrilateral elements = 0
--&gt; Toal Elements 71406

real	0m9.082s
user	0m12.525s
sys	0m2.295s
+ status=0
+ set +x

=================================================
solutions/session07/aflr4_InviscidTransport_150k.py passed (as expected)
=================================================

execute_Training.sh: line 293: ulimit: stack size: cannot modify limit: Operation not permitted
flowCart: /Users/jenkins/util/cart3d/cart3d_v1.5.9_OSX64_ICC--22.11.16/bin/OSX64_ICC//flowCart

=================================================
1_cart3d_InviscidWing.py test;
+ python 1_cart3d_InviscidWing.py
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/CAPS/training/2023/training.log

MESSAGE:: Building wingOml

Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = Wing, index = 1
 Body size = 209.164356
 Tessellating body 1 with  MaxEdge = 5.229109  Sag = 0.209164  Angle = 15.000000
 Executing: autoInputs -r 8.000000 -nDiv 6 -maxR 9  &gt; autoInputs.out
 Executing: ./aero.csh &gt; aero.out
C_A    0.086485028
C_Y    -2.1874522e-05
C_N    0.55362646
C_D    0.10094764
C_S    -2.1874522e-05
C_L    0.55117283
C_l    -6.33338e-05
C_m    0.893921
C_n    -0.000182003
C_M_x  -6.80764e-05
C_M_y  0.893921
C_M_z  -0.000180283

real	0m22.440s
user	0m41.190s
sys	0m0.717s
+ status=0
+ set +x

=================================================
data/session08/1_cart3d_InviscidWing.py passed (as expected)
=================================================


=================================================
4_cart3d_OpenMDAO_alpha.py test;
+ python 4_cart3d_OpenMDAO_alpha.py
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/CAPS/training/2023/training.log
[VIGGEN.MIT.EDU:54259] shmem: mmap: an error occurred while determining whether or not /var/folders/l7/7s0m18td3fxg_w_dxpkj1d600000gp/T//ompi.VIGGEN.502/jf.0/4138926080/sm_segment.VIGGEN.502.f6b30000.0 could be created.

MESSAGE:: Building wingOml

Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = Wing, index = 1

Getting CFD design variables.......
	Number of design variables - 1
	Design Variable name - alpha
	Done getting CFD design variables
Getting CFD functional.......
	Number of design variables - 1
	Objective name - CL2
	Done getting CFD functional
 Body size = 196.565248
 Tessellating body 1 with  MaxEdge = 4.914131  Sag = 0.196565  Angle = 15.000000
 Executing: autoInputs -r 5.000000 -nDiv 7 -maxR 9  &gt; autoInputs.out
 o Evaluating Cart3D functionals and/or gradients
   ATTENTION: using static geometry ../inputs/Components.i.tri
   (19:29:01) Running aero.csh on 2 core(s) in M0.4A1.5B0_DP1
   (19:29:49) aero.csh done
 o case M0.4A1.5B0_DP1, averaging data over 1 cycle(s)
 o Evaluating Cart3D functionals and/or gradients
   ATTENTION: using static geometry ../inputs/Components.i.tri
   (19:29:49) Running aero.csh on 2 core(s) in M0.4A1.5B0_DP1
   (19:30:59) aero.csh done
              Max memory allowed:       32 GB
              Flow hexes:               264563
              Estimated cutter memory:  0.026456 GB / DV
              Estimated xsensit memory: 0.502670 GB / DV
              Available threads:        2
              # DVs:                    1
   o Number of simultaneous cutter jobs:   1
   (19:30:59) Linearizing cut-cells
   (19:30:59) ... done
   o Number of simultaneous xsensit jobs:  1
   (19:30:59) Computing gradients
   (19:31:03) ... done
 o case M0.4A1.5B0_DP1, averaging data over 1 cycle(s)
RUNNING THE L-BFGS-B CODE

           * * *

Machine precision = 2.220D-16
 N =            1     M =           10

At X0         0 variables are exactly at the bounds

At iterate    0    f=  1.88225D-02    |proj g|=  2.44220D-02
 o Evaluating Cart3D functionals and/or gradients
   ATTENTION: using static geometry ../inputs/Components.i.tri
   (19:31:04) Running aero.csh on 2 core(s) in M0.4A1.47558B0_DP1
   (19:31:51) aero.csh done
 o case M0.4A1.47558B0_DP1, averaging data over 1 cycle(s)
 o Evaluating Cart3D functionals and/or gradients
   ATTENTION: using static geometry ../inputs/Components.i.tri
   (19:31:52) Running aero.csh on 2 core(s) in M0.4A1.47558B0_DP1
   (19:33:01) aero.csh done
              Max memory allowed:       32 GB
              Flow hexes:               264563
              Estimated cutter memory:  0.026456 GB / DV
              Estimated xsensit memory: 0.502670 GB / DV
              Available threads:        2
              # DVs:                    1
   o Number of simultaneous cutter jobs:   1
   (19:33:01) Linearizing cut-cells
   (19:33:01) ... done
   o Number of simultaneous xsensit jobs:  1
   (19:33:01) Computing gradients
   (19:33:05) ... done
 o case M0.4A1.47558B0_DP1, averaging data over 1 cycle(s)

At iterate    1    f=  1.82188D-02    |proj g|=  2.40420D-02
 o Evaluating Cart3D functionals and/or gradients
   ATTENTION: using static geometry ../inputs/Components.i.tri
   (19:33:06) Running aero.csh on 2 core(s) in M0.4A-0.0697692B0_DP1
   (19:34:30) aero.csh done
 o case M0.4A-0.0697692B0_DP1, averaging data over 1 cycle(s)
 o Evaluating Cart3D functionals and/or gradients
   ATTENTION: using static geometry ../inputs/Components.i.tri
   (19:34:32) Running aero.csh on 2 core(s) in M0.4A-0.0697692B0_DP1
   (19:38:07) aero.csh done
              Max memory allowed:       32 GB
              Flow hexes:               264563
              Estimated cutter memory:  0.026456 GB / DV
              Estimated xsensit memory: 0.502670 GB / DV
              Available threads:        2
              # DVs:                    1
   o Number of simultaneous cutter jobs:   1
   (19:38:07) Linearizing cut-cells
   (19:38:07) ... done
   o Number of simultaneous xsensit jobs:  1
   (19:38:07) Computing gradients
   (19:38:11) ... done
 o case M0.4A-0.0697692B0_DP1, averaging data over 1 cycle(s)

At iterate    2    f=  4.18871D-05    |proj g|=  1.18308D-03
 o Evaluating Cart3D functionals and/or gradients
   ATTENTION: using static geometry ../inputs/Components.i.tri
   (19:38:11) Running aero.csh on 2 core(s) in M0.4A0.00270895B0_DP1
   (19:39:00) aero.csh done
 o case M0.4A0.00270895B0_DP1, averaging data over 1 cycle(s)
 o Evaluating Cart3D functionals and/or gradients
   ATTENTION: using static geometry ../inputs/Components.i.tri
   (19:39:00) Running aero.csh on 2 core(s) in M0.4A0.00270895B0_DP1
   (19:40:09) aero.csh done
              Max memory allowed:       32 GB
              Flow hexes:               264563
              Estimated cutter memory:  0.026456 GB / DV
              Estimated xsensit memory: 0.502670 GB / DV
              Available threads:        2
              # DVs:                    1
   o Number of simultaneous cutter jobs:   1
   (19:40:09) Linearizing cut-cells
   (19:40:09) ... done
   o Number of simultaneous xsensit jobs:  1
   (19:40:09) Computing gradients
   (19:40:13) ... done
 o case M0.4A0.00270895B0_DP1, averaging data over 1 cycle(s)

At iterate    3    f=  8.61443D-08    |proj g|=  5.38279D-05
 o Evaluating Cart3D functionals and/or gradients
   ATTENTION: using static geometry ../inputs/Components.i.tri
   (19:40:14) Running aero.csh on 2 core(s) in M0.4A-0.000445161B0_DP1
   (19:41:02) aero.csh done
 o case M0.4A-0.000445161B0_DP1, averaging data over 1 cycle(s)
 o Evaluating Cart3D functionals and/or gradients
   ATTENTION: using static geometry ../inputs/Components.i.tri
   (19:41:03) Running aero.csh on 2 core(s) in M0.4A-0.000445161B0_DP1
   (19:42:12) aero.csh done
              Max memory allowed:       32 GB
              Flow hexes:               264563
              Estimated cutter memory:  0.026456 GB / DV
              Estimated xsensit memory: 0.502670 GB / DV
              Available threads:        2
              # DVs:                    1
   o Number of simultaneous cutter jobs:   1
   (19:42:12) Linearizing cut-cells
   (19:42:12) ... done
   o Number of simultaneous xsensit jobs:  1
   (19:42:12) Computing gradients
   (19:42:16) ... done
 o case M0.4A-0.000445161B0_DP1, averaging data over 1 cycle(s)

At iterate    4    f=  1.38980D-11    |proj g|=  6.83851D-07

           * * *

Tit   = total number of iterations
Tnf   = total number of function evaluations
Tnint = total number of segments explored during Cauchy searches
Skip  = number of BFGS updates skipped
Nact  = number of active bounds at final generalized Cauchy point
Projg = norm of the final projected gradient
F     = final function value

           * * *

   N    Tit     Tnf  Tnint  Skip  Nact     Projg        F
    1      4      5      4     0     0   6.839D-07   1.390D-11
  F =   1.3897976632999999E-011

CONVERGENCE: NORM_OF_PROJECTED_GRADIENT_&lt;=_PGTOL            
Optimization Complete
-----------------------------------
Optimized alpha: [-0.00044516]

real	13m17.745s
user	20m49.811s
sys	0m9.685s
+ status=0
+ set +x

=================================================
data/session08/4_cart3d_OpenMDAO_alpha.py passed (as expected)
=================================================


=================================================
5_cart3d_OpenMDAO_twist.py test;
+ python 5_cart3d_OpenMDAO_twist.py
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/CAPS/training/2023/training.log
[VIGGEN.MIT.EDU:79574] shmem: mmap: an error occurred while determining whether or not /var/folders/l7/7s0m18td3fxg_w_dxpkj1d600000gp/T//ompi.VIGGEN.502/jf.0/453574656/sm_segment.VIGGEN.502.1b090000.0 could be created.

MESSAGE:: Building wingOml

Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = Wing, index = 1

Getting CFD design variables.......
	Number of design variables - 1
	Design Variable name - wing:alphab
	Done getting CFD design variables
Getting CFD functional.......
	Number of design variables - 1
	Objective name - CL2
	Done getting CFD functional
 Body size = 196.567836
 Tessellating body 1 with  MaxEdge = 4.914196  Sag = 0.196568  Angle = 15.000000
 Executing: autoInputs -r 5.000000 -nDiv 7 -maxR 9  &gt; autoInputs.out
 o Evaluating Cart3D functionals and/or gradients
   ATTENTION: using static geometry ../inputs/Components.i.tri
   (19:42:19) Running aero.csh on 2 core(s) in M0.4A0B0_DP1
   (19:43:06) aero.csh done
 o case M0.4A0B0_DP1, averaging data over 1 cycle(s)

MESSAGE:: Building wingOml

 o Evaluating Cart3D functionals and/or gradients
   ATTENTION: using static geometry ../inputs/Components.i.tri
   (19:43:07) Running aero.csh on 2 core(s) in M0.4A0B0_DP1
   (19:44:16) aero.csh done
              Max memory allowed:       32 GB
              Flow hexes:               260350
              Estimated cutter memory:  0.026035 GB / DV
              Estimated xsensit memory: 0.494665 GB / DV
              Available threads:        2
              # DVs:                    1
   o Number of simultaneous cutter jobs:   1
   (19:44:16) Linearizing cut-cells
   (19:44:18) ... done
   o Number of simultaneous xsensit jobs:  1
   (19:44:18) Computing gradients
   (19:44:22) ... done
 o case M0.4A0B0_DP1, averaging data over 1 cycle(s)
RUNNING THE L-BFGS-B CODE

           * * *

Machine precision = 2.220D-16
 N =            1     M =           10

At X0         0 variables are exactly at the bounds

At iterate    0    f=  5.30094D-03    |proj g|=  7.31928D-03

MESSAGE:: Building wingOml

Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = Wing, index = 1
 Body size = 196.567822
 Tessellating body 1 with  MaxEdge = 4.914196  Sag = 0.196568  Angle = 15.000000
 Executing: autoInputs -r 5.000000 -nDiv 7 -maxR 9  &gt; autoInputs.out
 o Evaluating Cart3D functionals and/or gradients
   ATTENTION: using static geometry ../inputs/Components.i.tri
   (19:44:23) Running aero.csh on 2 core(s) in M0.4A0B0_DP1
   (19:45:11) aero.csh done
 o case M0.4A0B0_DP1, averaging data over 1 cycle(s)

MESSAGE:: Building wingOml

 o Evaluating Cart3D functionals and/or gradients
   ATTENTION: using static geometry ../inputs/Components.i.tri
   (19:45:12) Running aero.csh on 2 core(s) in M0.4A0B0_DP1
   (19:46:20) aero.csh done
              Max memory allowed:       32 GB
              Flow hexes:               260454
              Estimated cutter memory:  0.026045 GB / DV
              Estimated xsensit memory: 0.494863 GB / DV
              Available threads:        2
              # DVs:                    1
   o Number of simultaneous cutter jobs:   1
   (19:46:21) Linearizing cut-cells
   (19:46:23) ... done
   o Number of simultaneous xsensit jobs:  1
   (19:46:23) Computing gradients
   (19:46:27) ... done
 o case M0.4A0B0_DP1, averaging data over 1 cycle(s)

At iterate    1    f=  5.25523D-03    |proj g|=  7.29015D-03

MESSAGE:: Building wingOml

Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = Wing, index = 1
 Body size = 196.565774
 Tessellating body 1 with  MaxEdge = 4.914144  Sag = 0.196566  Angle = 15.000000
 Executing: autoInputs -r 5.000000 -nDiv 7 -maxR 9  &gt; autoInputs.out
 o Evaluating Cart3D functionals and/or gradients
   ATTENTION: using static geometry ../inputs/Components.i.tri
   (19:46:28) Running aero.csh on 2 core(s) in M0.4A0B0_DP1
   (19:47:15) aero.csh done
 o case M0.4A0B0_DP1, averaging data over 1 cycle(s)

MESSAGE:: Building wingOml

 o Evaluating Cart3D functionals and/or gradients
   ATTENTION: using static geometry ../inputs/Components.i.tri
   (19:47:16) Running aero.csh on 2 core(s) in M0.4A0B0_DP1
   (19:48:25) aero.csh done
              Max memory allowed:       32 GB
              Flow hexes:               261758
              Estimated cutter memory:  0.026176 GB / DV
              Estimated xsensit memory: 0.497340 GB / DV
              Available threads:        2
              # DVs:                    1
   o Number of simultaneous cutter jobs:   1
   (19:48:25) Linearizing cut-cells
   (19:48:27) ... done
   o Number of simultaneous xsensit jobs:  1
   (19:48:27) Computing gradients
   (19:48:31) ... done
 o case M0.4A0B0_DP1, averaging data over 1 cycle(s)

At iterate    2    f=  2.98455D-04    |proj g|=  1.85742D-03

MESSAGE:: Building wingOml

Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = Wing, index = 1
 Body size = 196.565298
 Tessellating body 1 with  MaxEdge = 4.914132  Sag = 0.196565  Angle = 15.000000
 Executing: autoInputs -r 5.000000 -nDiv 7 -maxR 9  &gt; autoInputs.out
 o Evaluating Cart3D functionals and/or gradients
   ATTENTION: using static geometry ../inputs/Components.i.tri
   (19:48:32) Running aero.csh on 2 core(s) in M0.4A0B0_DP1
   (19:49:21) aero.csh done
 o case M0.4A0B0_DP1, averaging data over 1 cycle(s)

MESSAGE:: Building wingOml

 o Evaluating Cart3D functionals and/or gradients
   ATTENTION: using static geometry ../inputs/Components.i.tri
   (19:49:21) Running aero.csh on 2 core(s) in M0.4A0B0_DP1
   (19:50:31) aero.csh done
              Max memory allowed:       32 GB
              Flow hexes:               264228
              Estimated cutter memory:  0.026423 GB / DV
              Estimated xsensit memory: 0.502033 GB / DV
              Available threads:        2
              # DVs:                    1
   o Number of simultaneous cutter jobs:   1
   (19:50:31) Linearizing cut-cells
   (19:50:33) ... done
   o Number of simultaneous xsensit jobs:  1
   (19:50:33) Computing gradients
   (19:50:37) ... done
 o case M0.4A0B0_DP1, averaging data over 1 cycle(s)

At iterate    3    f=  3.84355D-06    |proj g|=  2.40011D-04

MESSAGE:: Building wingOml

Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = Wing, index = 1
 Body size = 196.565263
 Tessellating body 1 with  MaxEdge = 4.914132  Sag = 0.196565  Angle = 15.000000
 Executing: autoInputs -r 5.000000 -nDiv 7 -maxR 9  &gt; autoInputs.out
 o Evaluating Cart3D functionals and/or gradients
   ATTENTION: using static geometry ../inputs/Components.i.tri
   (19:50:38) Running aero.csh on 2 core(s) in M0.4A0B0_DP1
   (19:51:26) aero.csh done
 o case M0.4A0B0_DP1, averaging data over 1 cycle(s)

MESSAGE:: Building wingOml

 o Evaluating Cart3D functionals and/or gradients
   ATTENTION: using static geometry ../inputs/Components.i.tri
   (19:51:27) Running aero.csh on 2 core(s) in M0.4A0B0_DP1
   (19:52:36) aero.csh done
              Max memory allowed:       32 GB
              Flow hexes:               264265
              Estimated cutter memory:  0.026426 GB / DV
              Estimated xsensit memory: 0.502104 GB / DV
              Available threads:        2
              # DVs:                    1
   o Number of simultaneous cutter jobs:   1
   (19:52:36) Linearizing cut-cells
   (19:52:38) ... done
   o Number of simultaneous xsensit jobs:  1
   (19:52:38) Computing gradients
   (19:52:42) ... done
 o case M0.4A0B0_DP1, averaging data over 1 cycle(s)

At iterate    4    f=  3.66987D-07    |proj g|=  7.23152D-05

MESSAGE:: Building wingOml

Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = Wing, index = 1
 Body size = 196.565248
 Tessellating body 1 with  MaxEdge = 4.914131  Sag = 0.196565  Angle = 15.000000
 Executing: autoInputs -r 5.000000 -nDiv 7 -maxR 9  &gt; autoInputs.out
 o Evaluating Cart3D functionals and/or gradients
   ATTENTION: using static geometry ../inputs/Components.i.tri
   (19:52:44) Running aero.csh on 2 core(s) in M0.4A0B0_DP1
   (19:53:32) aero.csh done
 o case M0.4A0B0_DP1, averaging data over 1 cycle(s)

MESSAGE:: Building wingOml

 o Evaluating Cart3D functionals and/or gradients
   ATTENTION: using static geometry ../inputs/Components.i.tri
   (19:53:32) Running aero.csh on 2 core(s) in M0.4A0B0_DP1
   (19:54:41) aero.csh done
              Max memory allowed:       32 GB
              Flow hexes:               264535
              Estimated cutter memory:  0.026454 GB / DV
              Estimated xsensit memory: 0.502617 GB / DV
              Available threads:        2
              # DVs:                    1
   o Number of simultaneous cutter jobs:   1
   (19:54:42) Linearizing cut-cells
   (19:54:44) ... done
   o Number of simultaneous xsensit jobs:  1
   (19:54:44) Computing gradients
   (19:54:48) ... done
 o case M0.4A0B0_DP1, averaging data over 1 cycle(s)

At iterate    5    f=  2.00842D-09    |proj g|=  5.37815D-06

           * * *

Tit   = total number of iterations
Tnf   = total number of function evaluations
Tnint = total number of segments explored during Cauchy searches
Skip  = number of BFGS updates skipped
Nact  = number of active bounds at final generalized Cauchy point
Projg = norm of the final projected gradient
F     = final function value

           * * *

   N    Tit     Tnf  Tnint  Skip  Nact     Projg        F
    1      5      6      5     0     0   5.378D-06   2.008D-09
  F =   2.0084224803000001E-009

CONVERGENCE: REL_REDUCTION_OF_F_&lt;=_FACTR*EPSMCH             
Optimization Complete
-----------------------------------
Optimized wing:alphab: [0.00011371]

real	12m31.767s
user	23m13.022s
sys	0m8.303s
+ status=0
+ set +x

=================================================
data/session08/5_cart3d_OpenMDAO_twist.py passed (as expected)
=================================================


=================================================
2_su2_InviscidWing.py test;
+ python 2_su2_InviscidWing.py
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/CAPS/training/2023/training.log

MESSAGE:: Building wingOml

Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 2
	Name = Wing, index = 1
	Name = Farfield, index = 2
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 3
	Name = leftWing, index = 1
	Name = riteWing, index = 2
	Name = Farfield, index = 3

Getting mesh sizing parameters
	Mesh sizing name - Farfield
	Mesh sizing name - leftWing
	Mesh sizing name - riteWing
	Done getting mesh sizing parameters
 
AFLR2    : ---------------------------------------
AFLR2    : AFLR2 LIBRARY
AFLR2    : ADVANCING-FRONT/LOCAL-RECONNECTION
AFLR2    : TRIA/QUAD GRID GENERATOR
AFLR2    : Version Number 9.18.1
AFLR2    : Version Date   06/11/24 @ 05:52PM
AFLR2    : Compile OS     Darwin 23.5.0 arm64
AFLR2    : Compile Date   06/11/24 @ 05:52PM
AFLR2    : Copyright 1994-2021, D.L. Marcum
AFLR2    : ---------------------------------------
 
AFLR4    : ---------------------------------------
AFLR4    : AFLR4 LIBRARY
AFLR4    : ADVANCING-FRONT/LOCAL-RECONNECTION
AFLR4    : TRIA/QUAD SURFACE GRID GENERATOR
AFLR4    : Version Number 11.5.15
AFLR4    : Version Date   07/19/24 @ 07:04PM
AFLR4    : Compile OS     Darwin 23.5.0 arm64
AFLR4    : Compile Date   07/19/24 @ 07:06PM
AFLR4    : Copyright 1994-2021, D.L. Marcum
AFLR4    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.8.1
EGADS    : ---------------------------------------

EGADS    : EGADS CAD Geometry Setup

EGADS    : Model has 2 Active Bodies

EGADS    : Body 0 is a SolidBody
EGADS    : Body 0 has 1 Shells
EGADS    : Body 0 has 10 Faces
EGADS    : Body 0 has 18 Edges
EGADS    : Body 0 has 10 Loops
EGADS    : Body 0 has 10 Nodes
EGADS    : Body 1 is a SolidBody
EGADS    : Body 1 has 1 Shells
EGADS    : Body 1 has 6 Faces
EGADS    : Body 1 has 12 Edges
EGADS    : Body 1 has 6 Loops
EGADS    : Body 1 has 8 Nodes

EGADS    : Check Grid BCs

EGADS    : Grid BCs are OK

EGADS    : Face Neighbor-Faces Information

EGADS    : QC  = Face Quad Combination Flag
EGADS    : IER = Face Isolated Edge Refinement Flag
EGADS    : ER  = Face Edge Refinement Factor
EGADS    :       Not applicable for Faces with a FarField Grid BC.
EGADS    : SF  = Face Scale Factor
EGADS    :       Not applicable for Faces with a FarField Grid BC.

EGADS    :   Face          Body    QC   IER       ER    Scale   Neighbor
EGADS    :     ID  Active    ID  Flag  Flag   Weight   Factor   Faces
EGADS    :      1     Yes     0     0     1        1        1   2 3 6
EGADS    :      2     Yes     0     0     1        1        1   1 4 5
EGADS    :      3     Yes     0     0     1        1        1   1 4 8
EGADS    :      4     Yes     0     0     1        1        1   2 3 5
EGADS    :      5     Yes     0     0     1        1        1   2 4
EGADS    :      6     Yes     0     0     1        1        1   1 7 8
EGADS    :      7     Yes     0     0     1        1        1   6 9 10
EGADS    :      8     Yes     0     0     1        1        1   3 6 9
EGADS    :      9     Yes     0     0     1        1        1   7 8 10
EGADS    :     10     Yes     0     0     1        1        1   7 9
EGADS    :     11     Yes     1     0     1       NA       NA   13 14 15 16
EGADS    :     12     Yes     1     0     1       NA       NA   13 14 15 16
EGADS    :     13     Yes     1     0     1       NA       NA   11 12 15 16
EGADS    :     14     Yes     1     0     1       NA       NA   11 12 15 16
EGADS    :     15     Yes     1     0     1       NA       NA   11 12 13 14
EGADS    :     16     Yes     1     0     1       NA       NA   11 12 13 14

EGADS    : Face Edges Information

EGADS    :   Face   Edges
EGADS    :      1   -1 2 3 -4
EGADS    :      2   -5 4 6 -7
EGADS    :      3   -3 8 1 -9
EGADS    :      4   -6 9 5 -10
EGADS    :      5   7 10
EGADS    :      6   11 13 -12 -2
EGADS    :      7   14 16 -15 -13
EGADS    :      8   12 17 -11 -8
EGADS    :      9   15 18 -14 -17
EGADS    :     10   -16 -18
EGADS    :     11   19 20 -21 -22
EGADS    :     12   -23 26 25 -24
EGADS    :     13   27 23 -28 -19
EGADS    :     14   -29 21 30 -25
EGADS    :     15   22 29 -26 -27
EGADS    :     16   -20 28 24 -30

EGADS    : Face Loops Information

EGADS    :   Face   Loops
EGADS    :      1   1
EGADS    :      2   2
EGADS    :      3   3
EGADS    :      4   4
EGADS    :      5   5
EGADS    :      6   6
EGADS    :      7   7
EGADS    :      8   8
EGADS    :      9   9
EGADS    :     10   10
EGADS    :     11   11
EGADS    :     12   12
EGADS    :     13   13
EGADS    :     14   14
EGADS    :     15   15
EGADS    :     16   16

EGADS    : Loop Edges Information

EGADS    :   Loop  Active   Edges
EGADS    :      1     Yes   -1 2 3 -4
EGADS    :      2     Yes   -5 4 6 -7
EGADS    :      3     Yes   -3 8 1 -9
EGADS    :      4     Yes   -6 9 5 -10
EGADS    :      5     Yes   7 10
EGADS    :      6     Yes   11 13 -12 -2
EGADS    :      7     Yes   14 16 -15 -13
EGADS    :      8     Yes   12 17 -11 -8
EGADS    :      9     Yes   15 18 -14 -17
EGADS    :     10     Yes   -16 -18
EGADS    :     11     Yes   19 20 -21 -22
EGADS    :     12     Yes   -23 26 25 -24
EGADS    :     13     Yes   27 23 -28 -19
EGADS    :     14     Yes   -29 21 30 -25
EGADS    :     15     Yes   22 29 -26 -27
EGADS    :     16     Yes   -20 28 24 -30

EGADS    : Edge Node, Scale Factor, and Neighbor-Faces Information

EGADS    : ESF = Edge Scale Factor
EGADS    :       Not applicable for DEGENERATE Edges or Edges with a FarField
EGADS    :       Grid BC Neighbor Face.

EGADS    :                                             Neighbor
EGADS    :   Edge  Body  Active Node1 Node2      ESF   Faces
EGADS    :      1     0     Yes     1     2        1   1 3
EGADS    :      2     0     Yes     1     3        1   1 6
EGADS    :      3     0     Yes     3     4        1   1 3
EGADS    :      4     0     Yes     2     4        1   1 2
EGADS    :      5     0     Yes     2     5        1   2 4
EGADS    :      6     0     Yes     4     6        1   2 4
EGADS    :      7     0     Yes     5     6        1   2 5
EGADS    :      8     0     Yes     3     1        1   3 8
EGADS    :      9     0     Yes     4     2        1   3 4
EGADS    :     10     0     Yes     6     5        1   4 5
EGADS    :     11     0     Yes     1     7        1   6 8
EGADS    :     12     0     Yes     3     8        1   6 8
EGADS    :     13     0     Yes     7     8        1   6 7
EGADS    :     14     0     Yes     7     9        1   7 9
EGADS    :     15     0     Yes     8    10        1   7 9
EGADS    :     16     0     Yes     9    10        1   7 10
EGADS    :     17     0     Yes     8     7        1   8 9
EGADS    :     18     0     Yes    10     9        1   9 10
EGADS    :     19     1     Yes    12    11       NA   11 13
EGADS    :     20     1     Yes    11    13       NA   11 16
EGADS    :     21     1     Yes    14    13       NA   11 14
EGADS    :     22     1     Yes    12    14       NA   11 15
EGADS    :     23     1     Yes    16    15       NA   12 13
EGADS    :     24     1     Yes    15    17       NA   12 16
EGADS    :     25     1     Yes    18    17       NA   12 14
EGADS    :     26     1     Yes    16    18       NA   12 15
EGADS    :     27     1     Yes    12    16       NA   13 15
EGADS    :     28     1     Yes    11    15       NA   13 16
EGADS    :     29     1     Yes    14    18       NA   14 15
EGADS    :     30     1     Yes    13    17       NA   14 16

EGADS    : Node Information

EGADS    :   Node  Active      Coordinates
EGADS    :      1     Yes       97.2007855                0                0
EGADS    :      2     Yes       97.9335611                0                0
EGADS    :      3     Yes               50                0                0
EGADS    :      4     Yes       75.3047874                0                0
EGADS    :      5     Yes       123.552357                0        4.7180639
EGADS    :      6     Yes       118.391317                0       3.99272703
EGADS    :      7     Yes       97.9335611       36.1389817                0
EGADS    :      8     Yes       75.3047874       36.1389817                0
EGADS    :      9     Yes       123.552357       97.6729236        4.7180639
EGADS    :     10     Yes       118.391317       97.6729236       3.99272703
EGADS    :     11     Yes                0                0       1951.57774
EGADS    :     12     Yes                0                0                0
EGADS    :     13     Yes                0       1953.45847       1951.57774
EGADS    :     14     Yes                0       1953.45847                0
EGADS    :     15     Yes       2040.21562                0       1951.57774
EGADS    :     16     Yes       2040.21562                0                0
EGADS    :     17     Yes       2040.21562       1953.45847       1951.57774
EGADS    :     18     Yes       2040.21562       1953.45847                0

EGADS    : Face and Edge Match Information

EGADS    : No Face Matches Found

AFLR4    : Surface Mesh Spacing Setup

AFLR4    : Max Bounding Box Length     = 3906.92
AFLR4    : Min Bounding Box Length     = 3906.92
AFLR4    : Max Ref Bounding Box Length = 195.346
AFLR4    : Min Ref Bounding Box Length = 13.1976
AFLR4    : Reference Length            = 21.7051
AFLR4    : BL Thickness                = 0
AFLR4    : FarField Spacing            = 2651.51
AFLR4    : Abs Min Surf Spacing        = 0.0542627
AFLR4    : Min Surf Spacing            = 0.108525
AFLR4    : Max Surf Spacing            = 2.17051
AFLR4    : Global Scale Factor         = 5

AFLR4    : Geometry Definition Information

AFLR4    : Definition              Definition   Composite             Grid BC
AFLR4    :         ID                    Type          ID                Type
AFLR4    :          0     glue-only composite           -                   -
AFLR4    :          1            CAD geometry           0            STD w/BL
AFLR4    :          2            CAD geometry           0            STD w/BL
AFLR4    :          3            CAD geometry           0            STD w/BL
AFLR4    :          4            CAD geometry           0            STD w/BL
AFLR4    :          5            CAD geometry           0            STD w/BL
AFLR4    :          6            CAD geometry           0            STD w/BL
AFLR4    :          7            CAD geometry           0            STD w/BL
AFLR4    :          8            CAD geometry           0            STD w/BL
AFLR4    :          9            CAD geometry           0            STD w/BL
AFLR4    :         10            CAD geometry           0            STD w/BL
AFLR4    :         11            CAD geometry           0            FARFIELD
AFLR4    :         12            CAD geometry           0            FARFIELD
AFLR4    :         13            CAD geometry           0            FARFIELD
AFLR4    :         14            CAD geometry           0            FARFIELD
AFLR4    :         15            CAD geometry           0            FARFIELD
AFLR4    :         16            CAD geometry           0            FARFIELD

AFLR4    : Define CAD surface definition 1
AFLR4    : Define CAD surface definition 2
AFLR4    : Define CAD surface definition 3
AFLR4    : Define CAD surface definition 4
AFLR4    : Define CAD surface definition 5
AFLR4    : Define CAD surface definition 6
AFLR4    : Define CAD surface definition 7
AFLR4    : Define CAD surface definition 8
AFLR4    : Define CAD surface definition 9
AFLR4    : Define CAD surface definition 10
AFLR4    : Define CAD surface definition 11
AFLR4    : Define CAD surface definition 12
AFLR4    : Define CAD surface definition 13
AFLR4    : Define CAD surface definition 14
AFLR4    : Define CAD surface definition 15
AFLR4    : Define CAD surface definition 16

AFLR4    : Surface Grid Generation

AFLR4    : Generate optimal mesh on surface definition 1
AFLR2    : Nodes, Trias,Quads=      1107      2082         0
AFLR4    : Nodes, Trias,Quads=       685      1238         0

AFLR4    : Generate optimal mesh on surface definition 2
AFLR2    : Nodes, Trias,Quads=      1473      2759         0
AFLR4    : Nodes, Trias,Quads=       721      1255         0

AFLR4    : Generate optimal mesh on surface definition 3
AFLR2    : Nodes, Trias,Quads=      1116      2100         0
AFLR4    : Nodes, Trias,Quads=       671      1210         0

AFLR4    : Generate optimal mesh on surface definition 4
AFLR2    : Nodes, Trias,Quads=      1458      2729         0
AFLR4    : Nodes, Trias,Quads=       714      1241         0

AFLR4    : Generate optimal mesh on surface definition 5
AFLR2    : Nodes, Trias,Quads=        20        24         0
AFLR4    : Nodes, Trias,Quads=        14        12         0

AFLR4    : Generate optimal mesh on surface definition 6
AFLR2    : Nodes, Trias,Quads=      1108      2084         0
AFLR4    : Nodes, Trias,Quads=       683      1234         0

AFLR4    : Generate optimal mesh on surface definition 7
AFLR2    : Nodes, Trias,Quads=      1488      2789         0
AFLR4    : Nodes, Trias,Quads=       714      1241         0

AFLR4    : Generate optimal mesh on surface definition 8
AFLR2    : Nodes, Trias,Quads=      1112      2092         0
AFLR4    : Nodes, Trias,Quads=       653      1174         0

AFLR4    : Generate optimal mesh on surface definition 9
AFLR2    : Nodes, Trias,Quads=      1456      2725         0
AFLR4    : Nodes, Trias,Quads=       708      1229         0

AFLR4    : Generate optimal mesh on surface definition 10
AFLR2    : Nodes, Trias,Quads=        20        24         0
AFLR4    : Nodes, Trias,Quads=        14        12         0

AFLR4    : Generate optimal mesh on surface definition 11
AFLR2    : Nodes, Trias,Quads=         5         4         0
AFLR4    : Nodes, Trias,Quads=         4         2         0

AFLR4    : Generate optimal mesh on surface definition 12
AFLR2    : Nodes, Trias,Quads=         5         4         0
AFLR4    : Nodes, Trias,Quads=         4         2         0

AFLR4    : Generate optimal mesh on surface definition 13
AFLR2    : Nodes, Trias,Quads=         5         4         0
AFLR4    : Nodes, Trias,Quads=         4         2         0

AFLR4    : Generate optimal mesh on surface definition 14
AFLR2    : Nodes, Trias,Quads=         5         4         0
AFLR4    : Nodes, Trias,Quads=         4         2         0

AFLR4    : Generate optimal mesh on surface definition 15
AFLR2    : Nodes, Trias,Quads=         5         4         0
AFLR4    : Nodes, Trias,Quads=         4         2         0

AFLR4    : Generate optimal mesh on surface definition 16
AFLR2    : Nodes, Trias,Quads=         5         4         0
AFLR4    : Nodes, Trias,Quads=         4         2         0

DGEOM    : Add surface definitions to composite definition 0
DGEOM    : Glue composite surface definition 0
DGEOM    : Nodes,Faces,BEdges=      4933      9858      1312

AFLR4    : Curvature BG Surface Grid Generation

AFLR4    : Nodes, Faces      =      4933      9858

AFLR4    : Surface Grid Generation

AFLR4    : Generate optimal mesh on surface definition 1
AFLR2    : Nodes, Trias,Quads=     12796     24695         0
AFLR4    : Nodes, Trias,Quads=      7764     14631         0

AFLR4    : Generate optimal mesh on surface definition 2
AFLR2    : Nodes, Trias,Quads=     29251     57087         0
AFLR4    : Nodes, Trias,Quads=     12448     23481         0

AFLR4    : Generate optimal mesh on surface definition 3
AFLR2    : Nodes, Trias,Quads=     12136     23411         0
AFLR4    : Nodes, Trias,Quads=      7447     14033         0

AFLR4    : Generate optimal mesh on surface definition 4
AFLR2    : Nodes, Trias,Quads=     29424     57435         0
AFLR4    : Nodes, Trias,Quads=     12399     23385         0

AFLR4    : Generate optimal mesh on surface definition 5
AFLR2    : Nodes, Trias,Quads=       196       293         0
AFLR4    : Nodes, Trias,Quads=       188       277         0

AFLR4    : Generate optimal mesh on surface definition 6
AFLR2    : Nodes, Trias,Quads=     12819     24741         0
AFLR4    : Nodes, Trias,Quads=      7725     14553         0

AFLR4    : Generate optimal mesh on surface definition 7
AFLR2    : Nodes, Trias,Quads=     29437     57459         0
AFLR4    : Nodes, Trias,Quads=     12412     23409         0

AFLR4    : Generate optimal mesh on surface definition 8
AFLR2    : Nodes, Trias,Quads=     12144     23427         0
AFLR4    : Nodes, Trias,Quads=      7471     14081         0

AFLR4    : Generate optimal mesh on surface definition 9
AFLR2    : Nodes, Trias,Quads=     29445     57477         0
AFLR4    : Nodes, Trias,Quads=     12478     23543         0

AFLR4    : Generate optimal mesh on surface definition 10
AFLR2    : Nodes, Trias,Quads=       196       293         0
AFLR4    : Nodes, Trias,Quads=       188       277         0

AFLR4    : Generate optimal mesh on surface definition 11
AFLR2    : Nodes, Trias,Quads=        12        14         0
AFLR4    : Nodes, Trias,Quads=         8         6         0

AFLR4    : Generate optimal mesh on surface definition 12
AFLR2    : Nodes, Trias,Quads=        12        14         0
AFLR4    : Nodes, Trias,Quads=         8         6         0

AFLR4    : Generate optimal mesh on surface definition 13
AFLR2    : Nodes, Trias,Quads=        12        14         0
AFLR4    : Nodes, Trias,Quads=         8         6         0

AFLR4    : Generate optimal mesh on surface definition 14
AFLR2    : Nodes, Trias,Quads=        12        14         0
AFLR4    : Nodes, Trias,Quads=         8         6         0

AFLR4    : Generate optimal mesh on surface definition 15
AFLR2    : Nodes, Trias,Quads=        12        14         0
AFLR4    : Nodes, Trias,Quads=         8         6         0

AFLR4    : Generate optimal mesh on surface definition 16
AFLR2    : Nodes, Trias,Quads=        12        14         0
AFLR4    : Nodes, Trias,Quads=         8         6         0

DGEOM    : Add surface definitions to composite definition 0
DGEOM    : Glue composite surface definition 0
DGEOM    : Nodes,Faces,BEdges=     75857    151706      9398

OVERALL  : CPU Time          =     0.979   seconds
Body 1 (of 2)
Number of nodes    = 75837
Number of elements = 151670
Number of triangle elements      = 151670
Number of quadrilateral elements = 0
Body 2 (of 2)
Number of nodes    = 20
Number of elements = 36
Number of triangle elements      = 36
Number of quadrilateral elements = 0
----------------------------
Total number of nodes    = 75857
Total number of elements = 151706
Total number of triangle elements      = 151706
Total number of quadrilateral elements = 0
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 3
	Name = leftWing, index = 1
	Name = riteWing, index = 2
	Name = Farfield, index = 3
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 2
	Name = Wing, index = 1
	Name = Farfield, index = 2
Getting volume mesh
 
UG PARAM : SETTING INPUT PARAMETERS FROM ARGUMENT VECTOR
 
UG PARAM : mrecm                       = 3         
UG PARAM : mrecqm                      = 3         
UG PARAM : mpfrmt                      = 0         
 
AFLR2    : ---------------------------------------
AFLR2    : AFLR2 LIBRARY
AFLR2    : ADVANCING-FRONT/LOCAL-RECONNECTION
AFLR2    : TRIA/QUAD GRID GENERATOR
AFLR2    : Version Number 9.18.1
AFLR2    : Version Date   06/11/24 @ 05:52PM
AFLR2    : Compile OS     Darwin 23.5.0 arm64
AFLR2    : Compile Date   06/11/24 @ 05:52PM
AFLR2    : Copyright 1994-2021, D.L. Marcum
AFLR2    : ---------------------------------------
 
AFLR4    : ---------------------------------------
AFLR4    : AFLR4 LIBRARY
AFLR4    : ADVANCING-FRONT/LOCAL-RECONNECTION
AFLR4    : TRIA/QUAD SURFACE GRID GENERATOR
AFLR4    : Version Number 11.5.15
AFLR4    : Version Date   07/19/24 @ 07:04PM
AFLR4    : Compile OS     Darwin 23.5.0 arm64
AFLR4    : Compile Date   07/19/24 @ 07:06PM
AFLR4    : Copyright 1994-2021, D.L. Marcum
AFLR4    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.8.1
EGADS    : ---------------------------------------

EGADS    : EGADS CAD Geometry Setup

EGADS    : Model has 2 Active Bodies

EGADS    : Body 0 is a SolidBody
EGADS    : Body 0 has 1 Shells
EGADS    : Body 0 has 10 Faces
EGADS    : Body 0 has 18 Edges
EGADS    : Body 0 has 10 Loops
EGADS    : Body 0 has 10 Nodes
EGADS    : Body 1 is a SolidBody
EGADS    : Body 1 has 1 Shells
EGADS    : Body 1 has 6 Faces
EGADS    : Body 1 has 12 Edges
EGADS    : Body 1 has 6 Loops
EGADS    : Body 1 has 8 Nodes

EGADS    : Check Grid BCs

EGADS    : Grid BCs are OK

EGADS    : Face Neighbor-Faces Information

EGADS    : QC  = Face Quad Combination Flag
EGADS    : IER = Face Isolated Edge Refinement Flag
EGADS    : ER  = Face Edge Refinement Factor
EGADS    :       Not applicable for Faces with a FarField Grid BC.
EGADS    : SF  = Face Scale Factor
EGADS    :       Not applicable for Faces with a FarField Grid BC.

EGADS    :   Face          Body    QC   IER       ER    Scale   Neighbor
EGADS    :     ID  Active    ID  Flag  Flag   Weight   Factor   Faces
EGADS    :      1     Yes     0     0     1        1        1   2 3 6
EGADS    :      2     Yes     0     0     1        1        1   1 4 5
EGADS    :      3     Yes     0     0     1        1        1   1 4 8
EGADS    :      4     Yes     0     0     1        1        1   2 3 5
EGADS    :      5     Yes     0     0     1        1        1   2 4
EGADS    :      6     Yes     0     0     1        1        1   1 7 8
EGADS    :      7     Yes     0     0     1        1        1   6 9 10
EGADS    :      8     Yes     0     0     1        1        1   3 6 9
EGADS    :      9     Yes     0     0     1        1        1   7 8 10
EGADS    :     10     Yes     0     0     1        1        1   7 9
EGADS    :     11     Yes     1     0     1       NA       NA   13 14 15 16
EGADS    :     12     Yes     1     0     1       NA       NA   13 14 15 16
EGADS    :     13     Yes     1     0     1       NA       NA   11 12 15 16
EGADS    :     14     Yes     1     0     1       NA       NA   11 12 15 16
EGADS    :     15     Yes     1     0     1       NA       NA   11 12 13 14
EGADS    :     16     Yes     1     0     1       NA       NA   11 12 13 14

EGADS    : Face Edges Information

EGADS    :   Face   Edges
EGADS    :      1   -1 2 3 -4
EGADS    :      2   -5 4 6 -7
EGADS    :      3   -3 8 1 -9
EGADS    :      4   -6 9 5 -10
EGADS    :      5   7 10
EGADS    :      6   11 13 -12 -2
EGADS    :      7   14 16 -15 -13
EGADS    :      8   12 17 -11 -8
EGADS    :      9   15 18 -14 -17
EGADS    :     10   -16 -18
EGADS    :     11   19 20 -21 -22
EGADS    :     12   -23 26 25 -24
EGADS    :     13   27 23 -28 -19
EGADS    :     14   -29 21 30 -25
EGADS    :     15   22 29 -26 -27
EGADS    :     16   -20 28 24 -30

EGADS    : Face Loops Information

EGADS    :   Face   Loops
EGADS    :      1   1
EGADS    :      2   2
EGADS    :      3   3
EGADS    :      4   4
EGADS    :      5   5
EGADS    :      6   6
EGADS    :      7   7
EGADS    :      8   8
EGADS    :      9   9
EGADS    :     10   10
EGADS    :     11   11
EGADS    :     12   12
EGADS    :     13   13
EGADS    :     14   14
EGADS    :     15   15
EGADS    :     16   16

EGADS    : Loop Edges Information

EGADS    :   Loop  Active   Edges
EGADS    :      1     Yes   -1 2 3 -4
EGADS    :      2     Yes   -5 4 6 -7
EGADS    :      3     Yes   -3 8 1 -9
EGADS    :      4     Yes   -6 9 5 -10
EGADS    :      5     Yes   7 10
EGADS    :      6     Yes   11 13 -12 -2
EGADS    :      7     Yes   14 16 -15 -13
EGADS    :      8     Yes   12 17 -11 -8
EGADS    :      9     Yes   15 18 -14 -17
EGADS    :     10     Yes   -16 -18
EGADS    :     11     Yes   19 20 -21 -22
EGADS    :     12     Yes   -23 26 25 -24
EGADS    :     13     Yes   27 23 -28 -19
EGADS    :     14     Yes   -29 21 30 -25
EGADS    :     15     Yes   22 29 -26 -27
EGADS    :     16     Yes   -20 28 24 -30

EGADS    : Edge Node, Scale Factor, and Neighbor-Faces Information

EGADS    : ESF = Edge Scale Factor
EGADS    :       Not applicable for DEGENERATE Edges or Edges with a FarField
EGADS    :       Grid BC Neighbor Face.

EGADS    :                                             Neighbor
EGADS    :   Edge  Body  Active Node1 Node2      ESF   Faces
EGADS    :      1     0     Yes     1     2        1   1 3
EGADS    :      2     0     Yes     1     3        1   1 6
EGADS    :      3     0     Yes     3     4        1   1 3
EGADS    :      4     0     Yes     2     4        1   1 2
EGADS    :      5     0     Yes     2     5        1   2 4
EGADS    :      6     0     Yes     4     6        1   2 4
EGADS    :      7     0     Yes     5     6        1   2 5
EGADS    :      8     0     Yes     3     1        1   3 8
EGADS    :      9     0     Yes     4     2        1   3 4
EGADS    :     10     0     Yes     6     5        1   4 5
EGADS    :     11     0     Yes     1     7        1   6 8
EGADS    :     12     0     Yes     3     8        1   6 8
EGADS    :     13     0     Yes     7     8        1   6 7
EGADS    :     14     0     Yes     7     9        1   7 9
EGADS    :     15     0     Yes     8    10        1   7 9
EGADS    :     16     0     Yes     9    10        1   7 10
EGADS    :     17     0     Yes     8     7        1   8 9
EGADS    :     18     0     Yes    10     9        1   9 10
EGADS    :     19     1     Yes    12    11       NA   11 13
EGADS    :     20     1     Yes    11    13       NA   11 16
EGADS    :     21     1     Yes    14    13       NA   11 14
EGADS    :     22     1     Yes    12    14       NA   11 15
EGADS    :     23     1     Yes    16    15       NA   12 13
EGADS    :     24     1     Yes    15    17       NA   12 16
EGADS    :     25     1     Yes    18    17       NA   12 14
EGADS    :     26     1     Yes    16    18       NA   12 15
EGADS    :     27     1     Yes    12    16       NA   13 15
EGADS    :     28     1     Yes    11    15       NA   13 16
EGADS    :     29     1     Yes    14    18       NA   14 15
EGADS    :     30     1     Yes    13    17       NA   14 16

EGADS    : Node Information

EGADS    :   Node  Active      Coordinates
EGADS    :      1     Yes       97.2007855                0                0
EGADS    :      2     Yes       97.9335611                0                0
EGADS    :      3     Yes               50                0                0
EGADS    :      4     Yes       75.3047874                0                0
EGADS    :      5     Yes       123.552357                0        4.7180639
EGADS    :      6     Yes       118.391317                0       3.99272703
EGADS    :      7     Yes       97.9335611       36.1389817                0
EGADS    :      8     Yes       75.3047874       36.1389817                0
EGADS    :      9     Yes       123.552357       97.6729236        4.7180639
EGADS    :     10     Yes       118.391317       97.6729236       3.99272703
EGADS    :     11     Yes                0                0       1951.57774
EGADS    :     12     Yes                0                0                0
EGADS    :     13     Yes                0       1953.45847       1951.57774
EGADS    :     14     Yes                0       1953.45847                0
EGADS    :     15     Yes       2040.21562                0       1951.57774
EGADS    :     16     Yes       2040.21562                0                0
EGADS    :     17     Yes       2040.21562       1953.45847       1951.57774
EGADS    :     18     Yes       2040.21562       1953.45847                0

EGADS    : Face and Edge Match Information

EGADS    : No Face Matches Found

AFLR4    : Surface Mesh Spacing Setup

AFLR4    : Max Bounding Box Length     = 3906.92
AFLR4    : Min Bounding Box Length     = 3906.92
AFLR4    : Max Ref Bounding Box Length = 195.346
AFLR4    : Min Ref Bounding Box Length = 13.1976
AFLR4    : Reference Length            = 13.1976
AFLR4    : BL Thickness                = 0
AFLR4    : FarField Spacing            = 428.309
AFLR4    : Abs Min Surf Spacing        = 0.032994
AFLR4    : Min Surf Spacing            = 0.065988
AFLR4    : Max Surf Spacing            = 1.31976
AFLR4    : Global Scale Factor         = 1

AFLR4    : Geometry Definition Information

AFLR4    : Definition              Definition   Composite             Grid BC
AFLR4    :         ID                    Type          ID                Type
AFLR4    :          0     glue-only composite           -                   -
AFLR4    :          1            CAD geometry           0                 STD
AFLR4    :          2            CAD geometry           0                 STD
AFLR4    :          3            CAD geometry           0                 STD
AFLR4    :          4            CAD geometry           0                 STD
AFLR4    :          5            CAD geometry           0                 STD
AFLR4    :          6            CAD geometry           0                 STD
AFLR4    :          7            CAD geometry           0                 STD
AFLR4    :          8            CAD geometry           0                 STD
AFLR4    :          9            CAD geometry           0                 STD
AFLR4    :         10            CAD geometry           0                 STD
AFLR4    :         11            CAD geometry           0            FARFIELD
AFLR4    :         12            CAD geometry           0            FARFIELD
AFLR4    :         13            CAD geometry           0            FARFIELD
AFLR4    :         14            CAD geometry           0            FARFIELD
AFLR4    :         15            CAD geometry           0            FARFIELD
AFLR4    :         16            CAD geometry           0            FARFIELD

AFLR4    : Define CAD surface definition 1
AFLR4    : Define CAD surface definition 2
AFLR4    : Define CAD surface definition 3
AFLR4    : Define CAD surface definition 4
AFLR4    : Define CAD surface definition 5
AFLR4    : Define CAD surface definition 6
AFLR4    : Define CAD surface definition 7
AFLR4    : Define CAD surface definition 8
AFLR4    : Define CAD surface definition 9
AFLR4    : Define CAD surface definition 10
AFLR4    : Define CAD surface definition 11
AFLR4    : Define CAD surface definition 12
AFLR4    : Define CAD surface definition 13
AFLR4    : Define CAD surface definition 14
AFLR4    : Define CAD surface definition 15
AFLR4    : Define CAD surface definition 16
 
AFLR43   : INPUT SURFACE MESH FROM TESS
 
AFLR43   : Quad Surface Faces=         0
AFLR43   : Tria Surface Faces=    151706
AFLR43   : Nodes             =     75857
 
 
UG PARAM : SETTING INPUT PARAMETERS FROM ARGUMENT VECTOR
 
UG PARAM : mrecm                       = 3         
UG PARAM : mrecqm                      = 3         
UG PARAM : mpfrmt                      = 0         
 
AFLR3    : ---------------------------------------
AFLR3    : AFLR3 LIBRARY
AFLR3    : ADVANCING-FRONT/LOCAL-RECONNECTION
AFLR3    : TETRAHEDRAL GRID GENERATOR
AFLR3    : Version Number 16.32.50
AFLR3    : Version Date   10/31/23 @ 06:31PM
AFLR3    : Compile OS     Darwin 23.3.0 arm64
AFLR3    : Compile Date   02/08/24 @ 04:22PM
AFLR3    : Copyright 1994-2021, D.L. Marcum
AFLR3    : ---------------------------------------
 
AFLR3 IC : INPUT SURFACE GRID CHECK
 
AFLR3 IC : Nodes, Elements   =     75857         0

UG3      : Boundary Conditions

UG3      :  B-Face ID            Boundary Condition
UG3      :          1                         Solid
UG3      :          2                         Solid
UG3      :          3                         Solid
UG3      :          4                         Solid
UG3      :          5                         Solid
UG3      :          6                         Solid
UG3      :          7                         Solid
UG3      :          8                         Solid
UG3      :          9                         Solid
UG3      :         10                         Solid
UG3      :         11                      FarField
UG3      :         12                      FarField
UG3      :         13                      FarField
UG3      :         14                      FarField
UG3      :         15                      FarField
UG3      :         16                      FarField
 
AFLR3    : CPU Time          =     0.090   seconds
 
AFLR3 IG : INITIAL VOLUME GRID GENERATION
 
AFLR3 IG : Nodes, Elements   =     75857         0
AFLR3 IG : Nodes, Elements   =         8        10
AFLR3 IG : Nodes, Elements   =     15172    111199
AFLR3 IG : Nodes, Elements   =     30344    239871
AFLR3 IG : Nodes, Elements   =     45516    364757
AFLR3 IG : Nodes, Elements   =     60688    488029
AFLR3 IG : Nodes, Elements   =     75860    649416
AFLR3 IG : Nodes, Elements   =     75864    649502
AFLR3 IG : Nodes, Elements   =     75864    648282
AFLR3 IG : Nodes, Elements   =     75864    648415
AFLR3 IG : Nodes, Elements   =     75864    647563
AFLR3 IG : Nodes, Elements   =     75857    416423
AFLR3 IG : Nodes, Elements   =     75857    417606
AFLR3 IG : Nodes, Elements   =     75857    261925
AFLR3 IG : Nodes, Elements   =     75857    238679
 
AFLR3    : CPU Time          =     2.505   seconds
 
AFLR3 GG : ISOTROPIC VOLUME GRID GENERATION
 
AFLR3 GG : Nodes, Elements   =     75857    238679
AFLR3 GG : Nodes, Elements   =     97036    302794
AFLR3 GG : Nodes, Elements   =     97036    381323
AFLR3 GG : Nodes, Elements   =     97036    348553
AFLR3 GG : Nodes, Elements   =    114433    404125
AFLR3 GG : Nodes, Elements   =    114433    479502
AFLR3 GG : Nodes, Elements   =    114433    449390
AFLR3 GG : Nodes, Elements   =    137578    521259
AFLR3 GG : Nodes, Elements   =    137578    620175
AFLR3 GG : Nodes, Elements   =    137578    582534
AFLR3 GG : Nodes, Elements   =    137578    570299
AFLR3 GG : Nodes, Elements   =    162763    647836
AFLR3 GG : Nodes, Elements   =    162763    770341
AFLR3 GG : Nodes, Elements   =    162763    731548
AFLR3 GG : Nodes, Elements   =    190585    816203
AFLR3 GG : Nodes, Elements   =    190585    935984
AFLR3 GG : Nodes, Elements   =    190585    899107
AFLR3 GG : Nodes, Elements   =    219816    987499
AFLR3 GG : Nodes, Elements   =    219816   1108410
AFLR3 GG : Nodes, Elements   =    219816   1073232
AFLR3 GG : Nodes, Elements   =    250105   1164614
AFLR3 GG : Nodes, Elements   =    250105   1287642
AFLR3 GG : Nodes, Elements   =    250105   1252761
AFLR3 GG : Nodes, Elements   =    279892   1342494
AFLR3 GG : Nodes, Elements   =    279892   1462443
AFLR3 GG : Nodes, Elements   =    279892   1429923
AFLR3 GG : Nodes, Elements   =    309074   1517784
AFLR3 GG : Nodes, Elements   =    309074   1634324
AFLR3 GG : Nodes, Elements   =    309074   1603191
AFLR3 GG : Nodes, Elements   =    337155   1687725
AFLR3 GG : Nodes, Elements   =    337155   1799086
AFLR3 GG : Nodes, Elements   =    337155   1770201
AFLR3 GG : Nodes, Elements   =    364031   1851037
AFLR3 GG : Nodes, Elements   =    364031   1958040
AFLR3 GG : Nodes, Elements   =    364031   1929929
AFLR3 GG : Nodes, Elements   =    389893   2007694
AFLR3 GG : Nodes, Elements   =    389893   2110445
AFLR3 GG : Nodes, Elements   =    389893   2083831
AFLR3 GG : Nodes, Elements   =    414588   2158046
AFLR3 GG : Nodes, Elements   =    414588   2256223
AFLR3 GG : Nodes, Elements   =    414588   2230399
AFLR3 GG : Nodes, Elements   =    437949   2300612
AFLR3 GG : Nodes, Elements   =    437949   2392665
AFLR3 GG : Nodes, Elements   =    437949   2369220
AFLR3 GG : Nodes, Elements   =    460028   2435556
AFLR3 GG : Nodes, Elements   =    460028   2523443
AFLR3 GG : Nodes, Elements   =    460028   2500481
AFLR3 GG : Nodes, Elements   =    481028   2563562
AFLR3 GG : Nodes, Elements   =    481028   2645943
AFLR3 GG : Nodes, Elements   =    481028   2625418
AFLR3 GG : Nodes, Elements   =    500564   2684111
AFLR3 GG : Nodes, Elements   =    500564   2760869
AFLR3 GG : Nodes, Elements   =    500564   2741486
AFLR3 GG : Nodes, Elements   =    519023   2796921
AFLR3 GG : Nodes, Elements   =    519023   2869294
AFLR3 GG : Nodes, Elements   =    519023   2851235
AFLR3 GG : Nodes, Elements   =    536227   2902907
AFLR3 GG : Nodes, Elements   =    536227   2970978
AFLR3 GG : Nodes, Elements   =    536227   2953488
AFLR3 GG : Nodes, Elements   =    552417   3002099
AFLR3 GG : Nodes, Elements   =    552417   3066275
AFLR3 GG : Nodes, Elements   =    552417   3049807
AFLR3 GG : Nodes, Elements   =    567559   3095278
AFLR3 GG : Nodes, Elements   =    567559   3155304
AFLR3 GG : Nodes, Elements   =    567559   3139713
AFLR3 GG : Nodes, Elements   =    581855   3182642
AFLR3 GG : Nodes, Elements   =    581855   3239064
AFLR3 GG : Nodes, Elements   =    581855   3224765
AFLR3 GG : Nodes, Elements   =    595142   3264660
AFLR3 GG : Nodes, Elements   =    595142   3317200
AFLR3 GG : Nodes, Elements   =    595142   3303799
AFLR3 GG : Nodes, Elements   =    607536   3341007
AFLR3 GG : Nodes, Elements   =    607536   3389453
AFLR3 GG : Nodes, Elements   =    607536   3377251
AFLR3 GG : Nodes, Elements   =    619010   3411685
AFLR3 GG : Nodes, Elements   =    619010   3457021
AFLR3 GG : Nodes, Elements   =    619010   3445397
AFLR3 GG : Nodes, Elements   =    629458   3476760
AFLR3 GG : Nodes, Elements   =    629458   3517836
AFLR3 GG : Nodes, Elements   =    629458   3507282
AFLR3 GG : Nodes, Elements   =    638979   3535863
AFLR3 GG : Nodes, Elements   =    638979   3573549
AFLR3 GG : Nodes, Elements   =    638979   3563786
AFLR3 GG : Nodes, Elements   =    647722   3590028
AFLR3 GG : Nodes, Elements   =    647722   3624053
AFLR3 GG : Nodes, Elements   =    647722   3615570
AFLR3 GG : Nodes, Elements   =    655612   3639251
AFLR3 GG : Nodes, Elements   =    655612   3670585
AFLR3 GG : Nodes, Elements   =    655612   3662351
AFLR3 GG : Nodes, Elements   =    662779   3683858
AFLR3 GG : Nodes, Elements   =    662779   3712160
AFLR3 GG : Nodes, Elements   =    662779   3704757
AFLR3 GG : Nodes, Elements   =    669454   3724790
AFLR3 GG : Nodes, Elements   =    669454   3750712
AFLR3 GG : Nodes, Elements   =    669454   3744123
AFLR3 GG : Nodes, Elements   =    675397   3761956
AFLR3 GG : Nodes, Elements   =    675397   3785252
AFLR3 GG : Nodes, Elements   =    675397   3779313
AFLR3 GG : Nodes, Elements   =    680809   3795555
AFLR3 GG : Nodes, Elements   =    680809   3817005
AFLR3 GG : Nodes, Elements   =    680809   3811333
AFLR3 GG : Nodes, Elements   =    685665   3825906
AFLR3 GG : Nodes, Elements   =    685665   3844891
AFLR3 GG : Nodes, Elements   =    685665   3840070
AFLR3 GG : Nodes, Elements   =    690086   3853337
AFLR3 GG : Nodes, Elements   =    690086   3871017
AFLR3 GG : Nodes, Elements   =    690086   3866262
AFLR3 GG : Nodes, Elements   =    694035   3878112
AFLR3 GG : Nodes, Elements   =    694035   3893779
AFLR3 GG : Nodes, Elements   =    694035   3889637
AFLR3 GG : Nodes, Elements   =    697620   3900399
AFLR3 GG : Nodes, Elements   =    697620   3914441
AFLR3 GG : Nodes, Elements   =    697620   3910923
AFLR3 GG : Nodes, Elements   =    700718   3920220
AFLR3 GG : Nodes, Elements   =    700718   3932327
AFLR3 GG : Nodes, Elements   =    700718   3929172
AFLR3 GG : Nodes, Elements   =    703391   3937194
AFLR3 GG : Nodes, Elements   =    703391   3947746
AFLR3 GG : Nodes, Elements   =    703391   3944953
AFLR3 GG : Nodes, Elements   =    705696   3951869
AFLR3 GG : Nodes, Elements   =    705696   3960843
AFLR3 GG : Nodes, Elements   =    705696   3958600
AFLR3 GG : Nodes, Elements   =    707556   3964183
AFLR3 GG : Nodes, Elements   =    707556   3971425
AFLR3 GG : Nodes, Elements   =    707556   3969536
AFLR3 GG : Nodes, Elements   =    709105   3974184
AFLR3 GG : Nodes, Elements   =    709105   3980363
AFLR3 GG : Nodes, Elements   =    709105   3978685
AFLR3 GG : Nodes, Elements   =    710382   3982517
AFLR3 GG : Nodes, Elements   =    710382   3987670
AFLR3 GG : Nodes, Elements   =    710382   3986193
AFLR3 GG : Nodes, Elements   =    711500   3989547
AFLR3 GG : Nodes, Elements   =    711500   3993879
AFLR3 GG : Nodes, Elements   =    711500   3992791
AFLR3 GG : Nodes, Elements   =    712386   3995449
AFLR3 GG : Nodes, Elements   =    712386   3998928
AFLR3 GG : Nodes, Elements   =    712386   3997984
AFLR3 GG : Nodes, Elements   =    713092   4000102
AFLR3 GG : Nodes, Elements   =    713092   4002840
AFLR3 GG : Nodes, Elements   =    713092   4002110
AFLR3 GG : Nodes, Elements   =    713683   4003883
AFLR3 GG : Nodes, Elements   =    713683   4006165
AFLR3 GG : Nodes, Elements   =    713683   4005545
AFLR3 GG : Nodes, Elements   =    714102   4006803
AFLR3 GG : Nodes, Elements   =    714102   4008493
AFLR3 GG : Nodes, Elements   =    714102   4007992
AFLR3 GG : Nodes, Elements   =    714383   4008836
AFLR3 GG : Nodes, Elements   =    714383   4009992
AFLR3 GG : Nodes, Elements   =    714383   4009630
AFLR3 GG : Nodes, Elements   =    714565   4010176
AFLR3 GG : Nodes, Elements   =    714565   4010905
AFLR3 GG : Nodes, Elements   =    714565   4010667
AFLR3 GG : Nodes, Elements   =    714710   4011102
AFLR3 GG : Nodes, Elements   =    714710   4011707
AFLR3 GG : Nodes, Elements   =    714710   4011510
AFLR3 GG : Nodes, Elements   =    714817   4011832
AFLR3 GG : Nodes, Elements   =    714817   4012263
AFLR3 GG : Nodes, Elements   =    714817   4012113
AFLR3 GG : Nodes, Elements   =    714886   4012320
AFLR3 GG : Nodes, Elements   =    714886   4012623
AFLR3 GG : Nodes, Elements   =    714886   4012501
AFLR3 GG : Nodes, Elements   =    714931   4012636
AFLR3 GG : Nodes, Elements   =    714931   4012830
AFLR3 GG : Nodes, Elements   =    714931   4012764
AFLR3 GG : Nodes, Elements   =    714965   4012866
AFLR3 GG : Nodes, Elements   =    714965   4013013
AFLR3 GG : Nodes, Elements   =    714965   4012950
AFLR3 GG : Nodes, Elements   =    714994   4013037
AFLR3 GG : Nodes, Elements   =    714994   4013157
AFLR3 GG : Nodes, Elements   =    714994   4013121
AFLR3 GG : Nodes, Elements   =    715020   4013199
AFLR3 GG : Nodes, Elements   =    715020   4013311
AFLR3 GG : Nodes, Elements   =    715020   4013266
AFLR3 GG : Nodes, Elements   =    715040   4013326
AFLR3 GG : Nodes, Elements   =    715040   4013398
AFLR3 GG : Nodes, Elements   =    715040   4013378
AFLR3 GG : Nodes, Elements   =    715056   4013426
AFLR3 GG : Nodes, Elements   =    715056   4013497
AFLR3 GG : Nodes, Elements   =    715056   4013477
AFLR3 GG : Nodes, Elements   =    715069   4013516
AFLR3 GG : Nodes, Elements   =    715069   4013568
AFLR3 GG : Nodes, Elements   =    715069   4013551
AFLR3 GG : Nodes, Elements   =    715076   4013572
AFLR3 GG : Nodes, Elements   =    715076   4013609
AFLR3 GG : Nodes, Elements   =    715076   4013590
AFLR3 GG : Nodes, Elements   =    715080   4013602
AFLR3 GG : Nodes, Elements   =    715080   4013619
AFLR3 GG : Nodes, Elements   =    715080   4013611
AFLR3 GG : Nodes, Elements   =    715221   4014034
AFLR3 GG : Nodes, Elements   =    715221   4014794
AFLR3 GG : Nodes, Elements   =    715221   4014418
AFLR3 GG : Nodes, Elements   =    715295   4014640
AFLR3 GG : Nodes, Elements   =    715295   4014974
AFLR3 GG : Nodes, Elements   =    715295   4014832
AFLR3 GG : Nodes, Elements   =    715340   4014967
AFLR3 GG : Nodes, Elements   =    715340   4015216
AFLR3 GG : Nodes, Elements   =    715340   4015085
AFLR3 GG : Nodes, Elements   =    715398   4015259
AFLR3 GG : Nodes, Elements   =    715398   4015521
AFLR3 GG : Nodes, Elements   =    715398   4015431
AFLR3 GG : Nodes, Elements   =    715428   4015521
AFLR3 GG : Nodes, Elements   =    715428   4015681
AFLR3 GG : Nodes, Elements   =    715428   4015602
AFLR3 GG : Nodes, Elements   =    715441   4015641
AFLR3 GG : Nodes, Elements   =    715441   4015712
AFLR3 GG : Nodes, Elements   =    715441   4015681
AFLR3 GG : Nodes, Elements   =    715446   4015696
AFLR3 GG : Nodes, Elements   =    715446   4015717
AFLR3 GG : Nodes, Elements   =    715446   4015706
AFLR3 GG : Nodes, Elements   =    715447   4015709
AFLR3 GG : Nodes, Elements   =    715447   4015712
AFLR3 GG : Nodes, Elements   =    715447   4015710
 
AFLR3    : CPU Time          =    48.991   seconds
 
AFLR3 QI : QUALITY IMPROVEMENT
 
AFLR3 QI : Nodes, Elements   =    715447   4015710
AFLR3 QI : Nodes, Elements   =    708655   3977757
AFLR3 QI : Nodes, Elements   =    706642   3966512
AFLR3 QI : Nodes, Elements   =    706080   3963343
AFLR3 QI : Nodes, Elements   =    705965   3962681
AFLR3 QI : Nodes, Elements   =    705940   3962544
AFLR3 QI : Nodes, Elements   =    705936   3962520
AFLR3 QI : Nodes, Elements   =    705936   3980235
AFLR3 QI : Nodes, Elements   =    705936   3958971
AFLR3 QI : Nodes, Elements   =    705936   3950968
AFLR3 QI : Nodes, Elements   =    705936   3964620
AFLR3 QI : Nodes, Elements   =    705936   3950929
AFLR3 QI : Nodes, Elements   =    705936   3950401
AFLR3 QI : Nodes, Elements   =    705936   3963184
AFLR3 QI : Nodes, Elements   =    705936   3950747
AFLR3 QI : Nodes, Elements   =    705936   3950348
AFLR3 QI : Nodes, Elements   =    705936   3962853
AFLR3 QI : Nodes, Elements   =    705936   3950630
AFLR3 QI : Nodes, Elements   =    705936   3950330
AFLR3 QI : Nodes, Elements   =    705936   3962713
AFLR3 QI : Nodes, Elements   =    705936   3950584
AFLR3 QI : Nodes, Elements   =    705936   3950299
AFLR3 QI : Nodes, Elements   =    705936   3950298
AFLR3 QI : Nodes, Elements   =    705962   3950412
AFLR3 QI : Nodes, Elements   =    705962   3962907
AFLR3 QI : Nodes, Elements   =    705962   3950755
AFLR3 QI : Nodes, Elements   =    705962   3950478
AFLR3 QI : Nodes, Elements   =    705962   3962751
AFLR3 QI : Nodes, Elements   =    705962   3950718
AFLR3 QI : Nodes, Elements   =    705962   3950478
 
AFLR3    : CPU Time          =    14.916   seconds
 
AFLR3 QRG: QUALITY GRID RE-GENERATION
 
AFLR3 QRG: Nodes, Elements   =    705962   3950478
AFLR3 QRG: Nodes, Elements   =    705956   3950446
AFLR3 QRG: Nodes, Elements   =    705950   3950421
AFLR3 QRG: Nodes, Elements   =    705949   3950418
AFLR3 QRG: Nodes, Elements   =    705947   3950409
AFLR3 QRG: Nodes, Elements   =    705945   3950399
AFLR3 QRG: Nodes, Elements   =    705963   3950505
AFLR3 QRG: Nodes, Elements   =    705960   3950492
AFLR3 QRG: Nodes, Elements   =    705958   3950483
AFLR3 QRG: Nodes, Elements   =    705955   3950470
AFLR3 QRG: Nodes, Elements   =    705954   3950465
AFLR3 QRG: Nodes, Elements   =    705954   3950467
AFLR3 QRG: Nodes, Elements   =    705953   3950463
AFLR3 QRG: Nodes, Elements   =    705952   3950459
AFLR3 QRG: Nodes, Elements   =    705951   3950455
AFLR3 QRG: Nodes, Elements   =    705950   3950452
AFLR3 QRG: Nodes, Elements   =    705949   3950449
AFLR3 QRG: Nodes, Elements   =    705948   3950445
AFLR3 QRG: Nodes, Elements   =    705947   3950439
AFLR3 QRG: Nodes, Elements   =    705948   3950443
AFLR3 QRG: Nodes, Elements   =    705947   3950439
AFLR3 QRG: Nodes, Elements   =    705946   3950435
AFLR3 QRG: Nodes, Elements   =    705971   3950587
AFLR3 QRG: Nodes, Elements   =    705970   3950583
AFLR3 QRG: Nodes, Elements   =    705969   3950579
AFLR3 QRG: Nodes, Elements   =    705976   3950614
AFLR3 QRG: Nodes, Elements   =    705977   3950623
AFLR3 QRG: Nodes, Elements   =    706039   3950970
 
AFLR3    : CPU Time          =     0.354   seconds
 
AFLR3    : DONE

UG3      : DIHEDRAL ANGLE CHECK

UG3      : No. Tet Elems     =   3950970
UG3      : Min, Max Ang      =   0.00123       180
UG3      : Average Angle     =      70.2
UG3      : No. Angle&gt;160.0   =       182
UG3      : No. Angle&gt;179.9   =         8

UG3      : VOL CHECK

UG3      : Total-Volume      =  5.96e+10

UG3      : No. Tet Elems     =   3950970
UG3      : Min Vol           =   6.4e-09
UG3      : Average Vol       =  1.51e+04
UG3      : Total-Tet-Vol     =  5.96e+10
UG3      : No. Vol&lt;TOL       =         0

UG3      : Q VOL-LENGTH-RATIO CHECK
                      2/3        2
UG3      : Q = c * Vol   / sum( L  )
UG3      : 0 &lt;= Q &lt;= 1

UG3      : No. Tet Elems     =   3950970
UG3      : Min, Max Q        =  9.19e-05         1
UG3      : Average Q         =      0.86
UG3      : No. Q&lt;       0.1  =       430
UG3      : No. Q&lt;      0.01  =        10

OVERALL  : CPU Time          =     1.160   minutes

UG3      : DIHEDRAL ANGLE CHECK

UG3      : No. Tet Elems     =   3950970
UG3      : Min, Max Ang      =   0.00123       180
UG3      : Average Angle     =      70.2
UG3      : No. Angle&gt;160.0   =       182
UG3      : No. Angle&gt;179.9   =         8

UG3      : VOL CHECK

UG3      : Total-Volume      =  5.96e+10

UG3      : No. Tet Elems     =   3950970
UG3      : Min Vol           =   6.4e-09
UG3      : Average Vol       =  1.51e+04
UG3      : Total-Tet-Vol     =  5.96e+10
UG3      : No. Vol&lt;TOL       =         0

UG3      : Q VOL-LENGTH-RATIO CHECK
                      2/3        2
UG3      : Q = c * Vol   / sum( L  )
UG3      : 0 &lt;= Q &lt;= 1
UG3      : Note that L includes scaling for BL-aspect=ratio

UG3      : No. Tet Elems     =   3950970
UG3      : Min, Max Q        =  0.000257         1
UG3      : Average Q         =     0.839
UG3      : No. Q&lt;       0.1  =        25
UG3      : No. Q&lt;      0.01  =         8

UG3      : CPU Time          =     0.000   seconds

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.8.1
EGADS    : ---------------------------------------

EGADS    : CREATE EGADS TESS FROM AFLR3 DATA

EGADS    : CREATING TESSELLATION FOR BODY 0 EDGE 1
EGADS    : CREATING TESSELLATION FOR BODY 0 EDGE 2
EGADS    : CREATING TESSELLATION FOR BODY 0 EDGE 3
EGADS    : CREATING TESSELLATION FOR BODY 0 EDGE 4
EGADS    : CREATING TESSELLATION FOR BODY 0 EDGE 5
EGADS    : CREATING TESSELLATION FOR BODY 0 EDGE 6
EGADS    : CREATING TESSELLATION FOR BODY 0 EDGE 7
EGADS    : CREATING TESSELLATION FOR BODY 0 EDGE 8
EGADS    : CREATING TESSELLATION FOR BODY 0 EDGE 9
EGADS    : CREATING TESSELLATION FOR BODY 0 EDGE 10
EGADS    : CREATING TESSELLATION FOR BODY 0 EDGE 11
EGADS    : CREATING TESSELLATION FOR BODY 0 EDGE 12
EGADS    : CREATING TESSELLATION FOR BODY 0 EDGE 13
EGADS    : CREATING TESSELLATION FOR BODY 0 EDGE 14
EGADS    : CREATING TESSELLATION FOR BODY 0 EDGE 15
EGADS    : CREATING TESSELLATION FOR BODY 0 EDGE 16
EGADS    : CREATING TESSELLATION FOR BODY 0 EDGE 17
EGADS    : CREATING TESSELLATION FOR BODY 0 EDGE 18

EGADS    : CREATING TESSELLATION FOR BODY 0 FACE 1
EGADS    : CREATING TESSELLATION FOR BODY 0 FACE 2
EGADS    : CREATING TESSELLATION FOR BODY 0 FACE 3
EGADS    : CREATING TESSELLATION FOR BODY 0 FACE 4
EGADS    : CREATING TESSELLATION FOR BODY 0 FACE 5
EGADS    : CREATING TESSELLATION FOR BODY 0 FACE 6
EGADS    : CREATING TESSELLATION FOR BODY 0 FACE 7
EGADS    : CREATING TESSELLATION FOR BODY 0 FACE 8
EGADS    : CREATING TESSELLATION FOR BODY 0 FACE 9
EGADS    : CREATING TESSELLATION FOR BODY 0 FACE 10

EGADS    : CREATING TESSELLATION FOR BODY 1 EDGE 19
EGADS    : CREATING TESSELLATION FOR BODY 1 EDGE 20
EGADS    : CREATING TESSELLATION FOR BODY 1 EDGE 21
EGADS    : CREATING TESSELLATION FOR BODY 1 EDGE 22
EGADS    : CREATING TESSELLATION FOR BODY 1 EDGE 23
EGADS    : CREATING TESSELLATION FOR BODY 1 EDGE 24
EGADS    : CREATING TESSELLATION FOR BODY 1 EDGE 25
EGADS    : CREATING TESSELLATION FOR BODY 1 EDGE 26
EGADS    : CREATING TESSELLATION FOR BODY 1 EDGE 27
EGADS    : CREATING TESSELLATION FOR BODY 1 EDGE 28
EGADS    : CREATING TESSELLATION FOR BODY 1 EDGE 29
EGADS    : CREATING TESSELLATION FOR BODY 1 EDGE 30

EGADS    : CREATING TESSELLATION FOR BODY 1 FACE 11
EGADS    : CREATING TESSELLATION FOR BODY 1 FACE 12
EGADS    : CREATING TESSELLATION FOR BODY 1 FACE 13
EGADS    : CREATING TESSELLATION FOR BODY 1 FACE 14
EGADS    : CREATING TESSELLATION FOR BODY 1 FACE 15
EGADS    : CREATING TESSELLATION FOR BODY 1 FACE 16

EGADS    : EGADS TESS CREATED

EGADS    : CHECK TESS FACE NODE MAP

EGADS    : CHECKING NODE MAP FOR BODY 0 FACE 1
EGADS    : CHECKING NODE MAP FOR BODY 0 FACE 2
EGADS    : CHECKING NODE MAP FOR BODY 0 FACE 3
EGADS    : CHECKING NODE MAP FOR BODY 0 FACE 4
EGADS    : CHECKING NODE MAP FOR BODY 0 FACE 5
EGADS    : CHECKING NODE MAP FOR BODY 0 FACE 6
EGADS    : CHECKING NODE MAP FOR BODY 0 FACE 7
EGADS    : CHECKING NODE MAP FOR BODY 0 FACE 8
EGADS    : CHECKING NODE MAP FOR BODY 0 FACE 9
EGADS    : CHECKING NODE MAP FOR BODY 0 FACE 10
EGADS    : CHECKING NODE MAP FOR BODY 1 FACE 11
EGADS    : CHECKING NODE MAP FOR BODY 1 FACE 12
EGADS    : CHECKING NODE MAP FOR BODY 1 FACE 13
EGADS    : CHECKING NODE MAP FOR BODY 1 FACE 14
EGADS    : CHECKING NODE MAP FOR BODY 1 FACE 15
EGADS    : CHECKING NODE MAP FOR BODY 1 FACE 16
Volume mesh:
	Number of nodes          = 706039
	Number of elements       = 4102676
	Number of triangles      = 151706
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 3950970
	Number of pyramids       = 0
	Number of prisms         = 0
	Number of hexahedrals    = 0

Writing SU2 file ....
Finished writing SU2 file

Getting CFD boundary conditions
	Boundary condition name - Farfield
	Boundary condition name - Wing
	Done getting CFD boundary conditions
Warning: The su2 cfg file will be overwritten!
Write SU2 configuration file for version "BlackBird (7.5.1) "


Running SU2......

-------------------------------------------------------------------------
|    ___ _   _ ___                                                      |
|   / __| | | |_  )   Release 8.0.0 "Harrier"                           |
|   \__ \ |_| |/ /                                                      |
|   |___/\___//___|   Suite (Computational Fluid Dynamics Code)         |
|                                                                       |
-------------------------------------------------------------------------
| SU2 Project Website: <a href='https://su2code.github.io'>https://su2code.github.io</a>                        |
|                                                                       |
| The SU2 Project is maintained by the SU2 Foundation                   |
| (<a href='http://su2foundation.org'>http://su2foundation.org</a>)                                            |
-------------------------------------------------------------------------
| Copyright 2012-2023, SU2 Contributors                                 |
|                                                                       |
| SU2 is free software; you can redistribute it and/or                  |
| modify it under the terms of the GNU Lesser General Public            |
| License as published by the Free Software Foundation; either          |
| version 2.1 of the License, or (at your option) any later version.    |
|                                                                       |
| SU2 is distributed in the hope that it will be useful,                |
| but WITHOUT ANY WARRANTY; without even the implied warranty of        |
| MERCHANTABILITY or FITNESS FOR A PARTICULAR PURPOSE. See the GNU      |
| Lesser General Public License for more details.                       |
|                                                                       |
| You should have received a copy of the GNU Lesser General Public      |
| License along with SU2. If not, see &lt;<a href='http://www.gnu.org/licenses/'>http://www.gnu.org/licenses/</a>&gt;.   |
-------------------------------------------------------------------------

Parsing config file for zone 0

----------------- Physical Case Definition ( Zone 0 ) -------------------
Compressible Euler equations.
Mach number: 0.5.
Angle of attack (AoA): 1 deg, and angle of sideslip (AoS): 0 deg.
No restart solution, use the values at infinity (freestream).
Dimensional simulation.
The reference area is 4240 m^2.
The semi-span will be computed using the max y(3D) value.
The reference length is 195.346 m.
Reference origin for moment evaluation is (55.4263, 0, 0).
Surface(s) where the force coefficients are evaluated: BC_1.

Surface(s) plotted in the output file: BC_1.
Input mesh file name: ../aflr3/aflr3_CAPS.su2

--------------- Space Numerical Integration ( Zone 0 ) ------------------
Roe (with entropy fix = 0.001) solver for the flow inviscid terms.
Standard Roe without low-dissipation function.
Second order integration in space, with slope limiter.
Venkatakrishnan slope-limiting method, with constant: 0.05.
The reference element size is: 1. 
Gradient for upwind reconstruction: inverse-distance weighted Least-Squares.
Gradient for viscous and source terms: inverse-distance weighted Least-Squares.

--------------- Time Numerical Integration  ( Zone 0 ) ------------------
Local time stepping (steady state simulation).
Euler implicit method for the flow equations.
FGMRES is used for solving the linear system.
Using a ILU(0) preconditioning.
Convergence criteria of the linear solver: 1e-06.
Max number of linear iterations: 10.
V Multigrid Cycle, with 2 multigrid levels.
Damping factor for the residual restriction: 0.75.
Damping factor for the correction prolongation: 0.75.
No CFL adaptation.
+-------------------------------------------+
|  MG Level| Presmooth|PostSmooth|CorrectSmo|
+-------------------------------------------+
|         0|         1|         0|         0|
|         1|         2|         0|         0|
|         2|         3|         0|         0|
+-------------------------------------------+
Courant-Friedrichs-Lewy number:       10

------------------ Convergence Criteria  ( Zone 0 ) ---------------------
Maximum number of solver subiterations: 10.
Begin convergence monitoring at iteration 5.
Residual minimum value: 1e-8.
Cauchy series min. value: 1e-10.
Number of Cauchy elements: 100.
Begin windowed time average at iteration 0.

-------------------- Output Information ( Zone 0 ) ----------------------
File writing frequency: 
+------------------------------------+
|                     File| Frequency|
+------------------------------------+
|                  RESTART|       250|
|              SURFACE_CSV|       250|
|                 PARAVIEW|       250|
|         SURFACE_PARAVIEW|       250|
+------------------------------------+
Writing the convergence history file every 1 inner iterations.
Writing the screen convergence history every 1 inner iterations.
The tabular file format is CSV (.csv).
Convergence history file name: history.
Forces breakdown file name: forces_breakdown_inviscidWing.dat.
Surface file name: surface_flow_inviscidWing.
Volume file name: flow_inviscidWing.
Restart file name: restart_flow_inviscidWing.dat.

------------- Config File Boundary Information ( Zone 0 ) ---------------
+-----------------------------------------------------------------------+
|                        Marker Type|                        Marker Name|
+-----------------------------------------------------------------------+
|                         Euler wall|                               BC_1|
+-----------------------------------------------------------------------+
|                          Far-field|                               BC_2|
+-----------------------------------------------------------------------+

-------------------- Output Preprocessing ( Zone 0 ) --------------------

WARNING: SURFACE_PRESSURE_DROP can only be computed for at least 2 surfaces (outlet, inlet, ...)

Screen output fields: TIME_ITER, OUTER_ITER, INNER_ITER, CUR_TIME, TIME_STEP, WALL_TIME, RMS_DENSITY, RMS_MOMENTUM-X, RMS_MOMENTUM-Y, RMS_ENERGY, EFFICIENCY
History output group(s): ITER, TIME_DOMAIN, WALL_TIME, RMS_RES, AERO_COEFF
Convergence field(s): RMS_DENSITY
Warning: No (valid) fields chosen for time convergence monitoring. Time convergence monitoring inactive.
Volume output fields: COORDINATES, SOLUTION, PRIMITIVE

------------------- Geometry Preprocessing ( Zone 0 ) -------------------
Three dimensional problem.
706039 grid points.
3950970 volume elements.
2 surface markers.
151670 boundary elements in index 0 (Marker = BC_1).
36 boundary elements in index 1 (Marker = BC_2).
3950970 tetrahedra.
Setting point connectivity.
Renumbering points (Reverse Cuthill McKee Ordering).
Recomputing point connectivity.
Setting element connectivity.
Checking the numerical grid orientation.
All volume elements are correctly orientend.
All surface elements are correctly orientend.
Identifying edges and vertices.
Setting the control volume structure.
Volume of the computational grid: 5.96352e+10.
Searching for the closest normal neighbors to the surfaces.
Storing a mapping from global to local point index.
Compute the surface curvature.
Max K: 122.726. Mean K: 4.02932. Standard deviation K: 11.9593.
Checking for periodicity.
Computing mesh quality statistics for the dual control volumes.
+--------------------------------------------------------------+
|           Mesh Quality Metric|        Minimum|        Maximum|
+--------------------------------------------------------------+
|    Orthogonality Angle (deg.)|        12.0095|        87.3048|
|     CV Face Area Aspect Ratio|        1.03091|        15816.5|
|           CV Sub-Volume Ratio|        1.00173|         567326|
+--------------------------------------------------------------+
Setting the multigrid structure.
+-------------------------------------------+
|  MG Level|       CVs|Aggl. Rate|       CFL|
+-------------------------------------------+
|         0|    706039|    1/1.00|        10|
|         1|    116093|    1/6.08|    8.2177|
|         2|     17733|    1/6.55|   6.58922|
+-------------------------------------------+
Finding max control volume width.
Semi-span length = 97.6729 m.
Wetted area = 8795.17 m^2.
Area projection in the x-plane = 681.45 m^2, y-plane = 449.381 m^2, z-plane = 4224.13 m^2.
Max. coordinate in the x-direction = 123.552 m, y-direction = 97.6729 m, z-direction = 4.71806 m.
Min. coordinate in the x-direction = 49.9621 m, y-direction = -97.6729 m, z-direction = -8.47903 m.
Checking if Euler &amp; Symmetry markers are straight/plane:
Boundary marker BC_1 is NOT a single plane.
Computing wall distances.

-------------------- Solver Preprocessing ( Zone 0 ) --------------------
Inviscid flow: Computing density based on free-stream
temperature and pressure using the ideal gas law.
Force coefficients computed using free-stream values.

-- Models:
+------------------------------------------------------------------------------+
|          Viscosity Model|        Conductivity Model|              Fluid Model|
+------------------------------------------------------------------------------+
|                        -|                         -|             STANDARD_AIR|
+------------------------------------------------------------------------------+
-- Fluid properties:
+------------------------------------------------------------------------------+
|                  Name|    Dim. value|    Ref. value|      Unit|Non-dim. value|
+------------------------------------------------------------------------------+
|          Gas Constant|       287.058|             1|  N.m/kg.K|       287.058|
|      Spec. Heat Ratio|             -|             -|         -|           1.4|
+------------------------------------------------------------------------------+
-- Initial and free-stream conditions:
+------------------------------------------------------------------------------+
|                  Name|    Dim. value|    Ref. value|      Unit|Non-dim. value|
+------------------------------------------------------------------------------+
|       Static Pressure|        101325|             1|        Pa|        101325|
|               Density|       1.22498|             1|    kg/m^3|       1.22498|
|           Temperature|        288.15|             1|         K|        288.15|
|          Total Energy|        221265|             1|   m^2/s^2|        221265|
|            Velocity-X|       170.123|             1|       m/s|       170.123|
|            Velocity-Y|             0|             1|       m/s|             0|
|            Velocity-Z|        2.9695|             1|       m/s|        2.9695|
|    Velocity Magnitude|       170.149|             1|       m/s|       170.149|
+------------------------------------------------------------------------------+
|           Mach Number|             -|             -|         -|           0.5|
+------------------------------------------------------------------------------+
Initialize Jacobian structure (Euler). MG level: 0.
Initialize Jacobian structure (Euler). MG level: 1.
Initialize Jacobian structure (Euler). MG level: 2.

------------------- Numerics Preprocessing ( Zone 0 ) -------------------

----------------- Integration Preprocessing ( Zone 0 ) ------------------

------------------- Iteration Preprocessing ( Zone 0 ) ------------------
Euler/Navier-Stokes/RANS fluid iteration.

------------------------------ Begin Solver -----------------------------

Simulation Run using the Single-zone Driver
WARNING: SU2 was not compiled for an AVX-capable architecture. Performance could be better,
         see <a href='https://su2code.github.io/docs_v7/Build-SU2-Linux-MacOS/#compiler-optimizations'>https://su2code.github.io/docs_v7/Build-SU2-Linux-MacOS/#compiler-optimizations</a>
WARNING: SU2 was not compiled for an AVX-capable architecture. Performance could be better,
         see <a href='https://su2code.github.io/docs_v7/Build-SU2-Linux-MacOS/#compiler-optimizations'>https://su2code.github.io/docs_v7/Build-SU2-Linux-MacOS/#compiler-optimizations</a>
WARNING: SU2 was not compiled for an AVX-capable architecture. Performance could be better,
         see <a href='https://su2code.github.io/docs_v7/Build-SU2-Linux-MacOS/#compiler-optimizations'>https://su2code.github.io/docs_v7/Build-SU2-Linux-MacOS/#compiler-optimizations</a>
+----------------------------------------------------------------------------------------------------------------------------------------------+
|   Time_Iter|  Outer_Iter|  Inner_Iter|    Cur_Time|   Time_Step|   Time(sec)|    rms[Rho]|   rms[RhoU]|   rms[RhoV]|   rms[RhoE]|        CEff|
+----------------------------------------------------------------------------------------------------------------------------------------------+
|           0|           0|           0|  0.0000e+00|  0.0000e+00|  1.3237e+01|    0.413477|    2.693384|    2.166473|    5.896322|   -0.410143|
|           0|           0|           1|  0.0000e+00|  0.0000e+00|  1.1878e+01|    3.050554|    5.559574|    5.273010|    8.536816|   -0.135737|
|           0|           0|           2|  0.0000e+00|  0.0000e+00|  1.1167e+01|    4.801359|    7.342376|    6.970135|   10.293693|   14.702205|
|           0|           0|           3|  0.0000e+00|  0.0000e+00|  1.0824e+01|    6.706527|    9.081364|    9.135145|   12.120102|  -66.410775|
|           0|           0|           4|  0.0000e+00|  0.0000e+00|  1.0588e+01|    6.306706|    8.650493|    8.379244|   11.723915|  -15.500630|
|           0|           0|           5|  0.0000e+00|  0.0000e+00|  1.0456e+01|    5.992382|    8.154250|    8.212880|   11.438780|   95.651198|
|           0|           0|           6|  0.0000e+00|  0.0000e+00|  1.0366e+01|    6.230651|    8.555249|    8.572561|   11.716780|   18.259965|
|           0|           0|           7|  0.0000e+00|  0.0000e+00|  1.0226e+01|    6.372540|    8.839403|    8.672407|   11.840955|   27.521211|
|           0|           0|           8|  0.0000e+00|  0.0000e+00|  1.0160e+01|    6.462239|    8.690028|    8.766410|   11.848066|    7.259007|
|           0|           0|           9|  0.0000e+00|  0.0000e+00|  1.0115e+01|    6.377436|    8.657118|    8.783328|   11.816921|   11.546451|

----------------------------- Solver Exit -------------------------------

Maximum number of iterations reached (ITER = 10) before convergence.
+-----------------------------------------------------------------------+
|      Convergence Field     |     Value    |   Criterion  |  Converged |
+-----------------------------------------------------------------------+
|                    rms[Rho]|       6.37744|          &lt; -8|          No|
+-----------------------------------------------------------------------+
-------------------------------------------------------------------------
+-----------------------------------------------------------------------+
|        File Writing Summary       |              Filename             |
+-----------------------------------------------------------------------+
|SU2 binary restart                 |restart_flow_inviscidWing.dat      |

Writing the forces breakdown file (forces_breakdown_inviscidWing.dat).
|CSV file                           |surface_flow_inviscidWing.csv      |

Writing the forces breakdown file (forces_breakdown_inviscidWing.dat).
|Paraview                           |flow_inviscidWing.vtu              |

Writing the forces breakdown file (forces_breakdown_inviscidWing.dat).
|Paraview surface                   |surface_flow_inviscidWing.vtu      |

Writing the forces breakdown file (forces_breakdown_inviscidWing.dat).
+-----------------------------------------------------------------------+
Warning: there are 774 non-physical points in the solution.
Warning: 21 reconstructed states for upwinding are non-physical.

--------------------------- Finalizing Solver ---------------------------
Deleted CNumerics container.
Deleted CIntegration container.
Deleted CSolver container.
Deleted CIteration container.
Deleted CInterface container.
Deleted CGeometry container.
Deleted CFreeFormDefBox class.
Deleted CSurfaceMovement class.
Deleted CVolumetricMovement class.
Deleted CConfig container.
Deleted nInst container.
Deleted COutput class.
-------------------------------------------------------------------------

------------------------- Exit Success (SU2_CFD) ------------------------


==&gt; Total Forces and Moments
--&gt; Cl =  -3.418779 Cd =  -0.296089
--&gt; Cmx =  0.005741 Cmy =  0.587705 Cmz =  0.008331
--&gt; Cx =  -0.236378 Cy =  0.038895 Cz =  -3.423426

real	4m31.039s
user	4m24.777s
sys	0m4.935s
+ status=0
+ set +x

=================================================
data/session08/2_su2_InviscidWing.py passed (as expected)
=================================================


=================================================
1_astros_ModalCantilever.py test;
+ python 1_astros_ModalCantilever.py
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/CAPS/training/2023/training.log

==&gt; Loading geometry from file "../ESP/transport.csm"...

==&gt; Running mASTROS pre-analysis...

MESSAGE:: Building wingOml


MESSAGE:: Building wingWaffle

Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 5
	Name = leftWingSkin, index = 1
	Name = wingRib, index = 2
	Name = riteWingSkin, index = 3
	Name = wingSpar1, index = 4
	Name = wingSpar2, index = 5
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 2
	Name = wingSpar1, index = 1
	Name = wingSpar2, index = 2
Getting surface mesh for body 1 (of 1)
Body 1 (of 1)
Number of nodes    = 425
Number of elements = 482
Number of triangle elements      = 0
Number of quadrilateral elements = 482
----------------------------
Total number of nodes    = 425
Total number of elements = 482
Mapping Csys attributes ................
	Number of unique Csys attributes = 2
	Name = leftWingSkin, index = 1
	Name = riteWingSkin, index = 2

Getting FEA coordinate systems.......
	Number of coordinate systems - 2
	Coordinate system name - leftWingSkin
	Coordinate system name - riteWingSkin
Mapping capsConstraint attributes ................
	Number of unique capsConstraint attributes = 1
	Name = rootConstraint, index = 1
Mapping capsLoad attributes ................
	Number of unique capsLoad attributes = 4
	Name = leftWingSkin, index = 1
	Name = riteWingSkin, index = 2
	Name = leftPointLoad, index = 3
	Name = ritePointLoad, index = 4
Mapping capsBound attributes ................
	Number of unique capsBound attributes = 4
	Name = upperWing, index = 1
	Name = lowerWing, index = 2
	Name = leftTip, index = 3
	Name = riteTip, index = 4
Mapping capsConnect attributes ................
	Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
	Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
	Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 5
	Name = leftWingSkin, index = 1
	Name = wingRib, index = 2
	Name = riteWingSkin, index = 3
	Name = wingSpar1, index = 4
	Name = wingSpar2, index = 5
Setting FEA Data
	Mesh for body = 0
	Number of nodal coordinates = 425
	Number of elements = 482
	Elemental Nodes = 0
	Elemental Rods  = 0
	Elemental Tria3 = 0
	Elemental Quad4 = 482
Aero_Reference value is NULL - No aero reference parameters set

Getting FEA materials.......
	Number of materials - 2
	Material name - Madeupium
	Material name - Unobtainium
	No "materialType" specified for Material tuple Unobtainium, defaulting to "Isotropic"
	Done getting FEA materials

Getting FEA properties.......
	Number of properties - 5
	Property name - leftWingSkin
	Property name - riteWingSkin
	Property name - wingRib
	Property name - wingSpar1
	Property name - wingSpar2
	Done getting FEA properties
Updating mesh element types based on properties input

Getting FEA constraints.......
	Number of constraints - 1
	Constraint name - rootConstraint
	No "constraintType" specified for Constraint tuple rootConstraint, defaulting to "ZeroDisplacement"
	No "groupName" specified for Constraint tuple rootConstraint, going to use constraint name
	Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults
Load tuple is NULL - No loads applied
Optimization Control tuple is NULL - Default optimization control is used

Getting FEA optimization control.......
Done getting FEA Optimization Control
Design_Variable tuple is NULL - No design variables applied
Design_Constraint tuple is NULL - No design constraints applied

Getting FEA analyses.......
	Number of analyses - 1
	Analysis name - EigenAnalysis
	Done getting FEA analyses

Writing Astros grid and connectivity file (in large field format) ....
Finished writing Astros grid file

Writing subElement types (if any) - appending mesh file

Writing Astros instruction file....
	Warning: No constraints specified for case EigenAnalysis, assuming all constraints are applied!!!!
	Writing analysis cards
	Writing constraint cards--all constraints for each subcase
	Writing material cards
	Writing property cards
	Writing coordinate system cards

==&gt; Running mASTROS...

==&gt; Running mASTROS post-analysis...
Reading Astros OUT file - extracting Eigen-Values!
	Number of Eigen-Values = 10
	Loading Eigen-Value = 1
	Loading Eigen-Value = 2
	Loading Eigen-Value = 3
	Loading Eigen-Value = 4
	Loading Eigen-Value = 5
	Loading Eigen-Value = 6
	Loading Eigen-Value = 7
	Loading Eigen-Value = 8
	Loading Eigen-Value = 9
	Loading Eigen-Value = 10

--&gt; Eigen-frequencies:
    1 : 0.00145606
    2 : 0.0014575
    3 : 0.00332859
    4 : 0.00333096
    5 : 0.00445176
    6 : 0.00445507
    7 : 0.00894917
    8 : 0.0089521
    9 : 0.0110353
    10: 0.0110413

real	0m49.053s
user	0m37.339s
sys	0m31.613s
+ status=0
+ set +x

=================================================
data/session09/1_astros_ModalCantilever.py passed (as expected)
=================================================


=================================================
2_astros_ModalSupport.py test;
+ python 2_astros_ModalSupport.py
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/CAPS/training/2023/training.log

==&gt; Loading geometry from file "../ESP/transport.csm"...

==&gt; Running mASTROS pre-analysis...

MESSAGE:: Building wingOml


MESSAGE:: Building wingWaffle

Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 6
	Name = leftWingSkin, index = 1
	Name = wingRib, index = 2
	Name = riteWingSkin, index = 3
	Name = wingSpar1, index = 4
	Name = wingSpar2, index = 5
	Name = ribSupport, index = 6
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 2
	Name = wingSpar1, index = 1
	Name = wingSpar2, index = 2
Getting surface mesh for body 1 (of 2)
Getting surface mesh for body 2 (of 2)
Body 1 (of 2)
Number of nodes    = 831
Number of elements = 962
Number of triangle elements      = 0
Number of quadrilateral elements = 962
Body 2 (of 2)
Number of nodes    = 1
Number of elements = 0
Number of triangle elements      = 0
Number of quadrilateral elements = 0
----------------------------
Total number of nodes    = 832
Total number of elements = 962
Mapping Csys attributes ................
	Number of unique Csys attributes = 2
	Name = leftWingSkin, index = 1
	Name = riteWingSkin, index = 2

Getting FEA coordinate systems.......
	Number of coordinate systems - 2
	Coordinate system name - leftWingSkin
	Coordinate system name - riteWingSkin
Mapping capsConstraint attributes ................
	Number of unique capsConstraint attributes = 1
	Name = ribRootPoint, index = 1
Mapping capsLoad attributes ................
	Number of unique capsLoad attributes = 2
	Name = leftPointLoad, index = 1
	Name = ritePointLoad, index = 2
Mapping capsBound attributes ................
	Number of unique capsBound attributes = 4
	Name = upperWing, index = 1
	Name = lowerWing, index = 2
	Name = leftTip, index = 3
	Name = riteTip, index = 4
Mapping capsConnect attributes ................
	Number of unique capsConnect attributes = 1
	Name = ribRoot, index = 1
Mapping capsResponse attributes ................
	Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
	Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 6
	Name = leftWingSkin, index = 1
	Name = wingRib, index = 2
	Name = riteWingSkin, index = 3
	Name = wingSpar1, index = 4
	Name = wingSpar2, index = 5
	Name = ribSupport, index = 6
Setting FEA Data
	Mesh for body = 0
	Number of nodal coordinates = 831
	Number of elements = 962
	Elemental Nodes = 0
	Elemental Rods  = 0
	Elemental Tria3 = 0
	Elemental Quad4 = 962
Setting FEA Data
	Mesh for body = 1
	Number of nodal coordinates = 1
	Number of elements = 1
	Elemental Nodes = 1
	Elemental Rods  = 0
	Elemental Tria3 = 0
	Elemental Quad4 = 0
Combining multiple FEA meshes!
	Combined Number of nodal coordinates = 832
	Combined Number of elements = 963
	Combined Elemental Nodes = 1
	Combined Elemental Rods  = 0
	Combined Elemental Tria3 = 0
	Combined Elemental Quad4 = 962
Aero_Reference value is NULL - No aero reference parameters set

Getting FEA materials.......
	Number of materials - 2
	Material name - Madeupium
	Material name - Unobtainium
	No "materialType" specified for Material tuple Unobtainium, defaulting to "Isotropic"
	Done getting FEA materials

Getting FEA properties.......
	Number of properties - 6
	Property name - leftWingSkin
	Property name - ribSupport
	Property name - riteWingSkin
	Property name - wingRib
	Property name - wingSpar1
	Property name - wingSpar2
	Done getting FEA properties
Updating mesh element types based on properties input

Getting FEA constraints.......
	Number of constraints - 1
	Constraint name - ribRootPoint
	No "constraintType" specified for Constraint tuple ribRootPoint, defaulting to "ZeroDisplacement"
	No "groupName" specified for Constraint tuple ribRootPoint, going to use constraint name
	Done getting FEA constraints

Getting FEA supports.......
	Number of supports - 1
	Support name - ribRootPoint
	No "groupName" specified for Support tuple ribRootPoint, going to use support name
	Done getting FEA supports

Getting FEA connections.......
	Number of connection tuples - 1
	Connection name - ribRoot
	No "groupName" specified for Connection tuple ribRoot!
	Looking for automatic connections from the use of capsConnectLink for ribRoot
	9 automatic connections were made for capsConnect ribRoot (node id 832)
	Done getting FEA connections
Load tuple is NULL - No loads applied
Optimization Control tuple is NULL - Default optimization control is used

Getting FEA optimization control.......
Done getting FEA Optimization Control
Design_Variable tuple is NULL - No design variables applied
Design_Constraint tuple is NULL - No design constraints applied

Getting FEA analyses.......
	Number of analyses - 1
	Analysis name - EigenAnalysis
	Done getting FEA analyses

Writing Astros grid and connectivity file (in large field format) ....
Finished writing Astros grid file

Writing subElement types (if any) - appending mesh file
Writing connection cards - appending mesh file

Writing Astros instruction file....
	Warning: No constraints specified for case EigenAnalysis, assuming all constraints are applied!!!!
	Writing analysis cards
	Writing constraint cards--all constraints for each subcase
	Writing support cards
	Writing material cards
	Writing property cards
	Writing coordinate system cards

==&gt; Running mASTROS...

==&gt; Running mASTROS post-analysis...
Reading Astros OUT file - extracting Eigen-Values!
	Number of Eigen-Values = 10
	Loading Eigen-Value = 1
	Loading Eigen-Value = 2
	Loading Eigen-Value = 3
	Loading Eigen-Value = 4
	Loading Eigen-Value = 5
	Loading Eigen-Value = 6
	Loading Eigen-Value = 7
	Loading Eigen-Value = 8
	Loading Eigen-Value = 9
	Loading Eigen-Value = 10

--&gt; Eigen-frequencies:
    1 : 1.54136e-08
    2 : 0.00142051
    3 : 0.0017451
    4 : 0.00323704
    5 : 0.00324885
    6 : 0.00432995
    7 : 0.00512483
    8 : 0.0087361
    9 : 0.010063
    10: 0.0107025

real	2m45.157s
user	2m24.277s
sys	0m56.538s
+ status=0
+ set +x

=================================================
data/session09/2_astros_ModalSupport.py passed (as expected)
=================================================


=================================================
3_astros_StaticCantilever.py test;
+ python 3_astros_StaticCantilever.py
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/CAPS/training/2023/training.log

==&gt; Loading geometry from file "../ESP/transport.csm"...

==&gt; Running mASTROS pre-analysis...

MESSAGE:: Building wingOml


MESSAGE:: Building wingWaffle

Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 5
	Name = leftWingSkin, index = 1
	Name = wingRib, index = 2
	Name = riteWingSkin, index = 3
	Name = wingSpar1, index = 4
	Name = wingSpar2, index = 5
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 2
	Name = wingSpar1, index = 1
	Name = wingSpar2, index = 2
Getting surface mesh for body 1 (of 1)
Body 1 (of 1)
Number of nodes    = 425
Number of elements = 482
Number of triangle elements      = 0
Number of quadrilateral elements = 482
----------------------------
Total number of nodes    = 425
Total number of elements = 482
Mapping Csys attributes ................
	Number of unique Csys attributes = 2
	Name = leftWingSkin, index = 1
	Name = riteWingSkin, index = 2

Getting FEA coordinate systems.......
	Number of coordinate systems - 2
	Coordinate system name - leftWingSkin
	Coordinate system name - riteWingSkin
Mapping capsConstraint attributes ................
	Number of unique capsConstraint attributes = 1
	Name = rootConstraint, index = 1
Mapping capsLoad attributes ................
	Number of unique capsLoad attributes = 4
	Name = leftWingSkin, index = 1
	Name = riteWingSkin, index = 2
	Name = leftPointLoad, index = 3
	Name = ritePointLoad, index = 4
Mapping capsBound attributes ................
	Number of unique capsBound attributes = 4
	Name = upperWing, index = 1
	Name = lowerWing, index = 2
	Name = leftTip, index = 3
	Name = riteTip, index = 4
Mapping capsConnect attributes ................
	Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
	Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
	Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 5
	Name = leftWingSkin, index = 1
	Name = wingRib, index = 2
	Name = riteWingSkin, index = 3
	Name = wingSpar1, index = 4
	Name = wingSpar2, index = 5
Setting FEA Data
	Mesh for body = 0
	Number of nodal coordinates = 425
	Number of elements = 482
	Elemental Nodes = 0
	Elemental Rods  = 0
	Elemental Tria3 = 0
	Elemental Quad4 = 482
Aero_Reference value is NULL - No aero reference parameters set

Getting FEA materials.......
	Number of materials - 2
	Material name - Madeupium
	Material name - Unobtainium
	No "materialType" specified for Material tuple Unobtainium, defaulting to "Isotropic"
	Done getting FEA materials

Getting FEA properties.......
	Number of properties - 5
	Property name - leftWingSkin
	Property name - riteWingSkin
	Property name - wingRib
	Property name - wingSpar1
	Property name - wingSpar2
	Done getting FEA properties
Updating mesh element types based on properties input

Getting FEA constraints.......
	Number of constraints - 1
	Constraint name - rootConstraint
	No "constraintType" specified for Constraint tuple rootConstraint, defaulting to "ZeroDisplacement"
	No "groupName" specified for Constraint tuple rootConstraint, going to use constraint name
	Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults

Getting FEA loads.......
	Number of loads - 2
	Load name - leftPointLoad
	No "groupName" specified for Load tuple leftPointLoad, going to use load name
	Load name - ritePointLoad
	No "groupName" specified for Load tuple ritePointLoad, going to use load name
	Done getting FEA loads
Optimization Control tuple is NULL - Default optimization control is used

Getting FEA optimization control.......
Done getting FEA Optimization Control
Design_Variable tuple is NULL - No design variables applied
Design_Constraint tuple is NULL - No design constraints applied
Analysis tuple is NULL

Getting FEA analyses.......
	Number of analyses - 1
	Analysis name - Default
	Done getting FEA analyses

Writing Astros grid and connectivity file (in large field format) ....
Finished writing Astros grid file

Writing subElement types (if any) - appending mesh file

Writing Astros instruction file....
	Writing analysis cards
	Writing load ADD cards
	Writing constraint cards--each subcase individually
	Writing load cards
	Writing material cards
	Writing property cards
	Writing coordinate system cards

==&gt; Running mASTROS...
Note: The following floating-point exceptions are signalling: IEEE_UNDERFLOW_FLAG

==&gt; Running mASTROS post-analysis...

--&gt; Maximum displacements:
--&gt; Tmax 238433.3403112283
--&gt; T1max 16861.9
--&gt; T2max 16414.9
--&gt; T3max 237286.0

real	0m13.545s
user	0m17.432s
sys	0m16.850s
+ status=0
+ set +x

=================================================
data/session09/3_astros_StaticCantilever.py passed (as expected)
=================================================


=================================================
4_astros_Composite.py test;
+ python 4_astros_Composite.py
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/CAPS/training/2023/training.log

==&gt; Loading geometry from file "../ESP/transport.csm"...

MESSAGE:: Building wingOml


MESSAGE:: Building wingWaffle


==&gt; Running mASTROS pre-analysis...
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 5
	Name = leftWingSkin, index = 1
	Name = wingRib, index = 2
	Name = riteWingSkin, index = 3
	Name = wingSpar1, index = 4
	Name = wingSpar2, index = 5
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 2
	Name = wingSpar1, index = 1
	Name = wingSpar2, index = 2
Getting surface mesh for body 1 (of 1)
Body 1 (of 1)
Number of nodes    = 425
Number of elements = 482
Number of triangle elements      = 0
Number of quadrilateral elements = 482
----------------------------
Total number of nodes    = 425
Total number of elements = 482
Mapping Csys attributes ................
	Number of unique Csys attributes = 2
	Name = leftWingSkin, index = 1
	Name = riteWingSkin, index = 2

Getting FEA coordinate systems.......
	Number of coordinate systems - 2
	Coordinate system name - leftWingSkin
	Coordinate system name - riteWingSkin
Mapping capsConstraint attributes ................
	Number of unique capsConstraint attributes = 1
	Name = rootConstraint, index = 1
Mapping capsLoad attributes ................
	Number of unique capsLoad attributes = 4
	Name = leftWingSkin, index = 1
	Name = riteWingSkin, index = 2
	Name = leftPointLoad, index = 3
	Name = ritePointLoad, index = 4
Mapping capsBound attributes ................
	Number of unique capsBound attributes = 4
	Name = upperWing, index = 1
	Name = lowerWing, index = 2
	Name = leftTip, index = 3
	Name = riteTip, index = 4
Mapping capsConnect attributes ................
	Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
	Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
	Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 5
	Name = leftWingSkin, index = 1
	Name = wingRib, index = 2
	Name = riteWingSkin, index = 3
	Name = wingSpar1, index = 4
	Name = wingSpar2, index = 5
Setting FEA Data
	Mesh for body = 0
	Number of nodal coordinates = 425
	Number of elements = 482
	Elemental Nodes = 0
	Elemental Rods  = 0
	Elemental Tria3 = 0
	Elemental Quad4 = 482
Aero_Reference value is NULL - No aero reference parameters set

Getting FEA materials.......
	Number of materials - 2
	Material name - Aluminum
	No "materialType" specified for Material tuple Aluminum, defaulting to "Isotropic"
	Material name - Graphite_epoxy
	Done getting FEA materials

Getting FEA properties.......
	Number of properties - 5
	Property name - leftWingSkin
	Property name - riteWingSkin
	Property name - wingRib
	Property name - wingSpar1
	Property name - wingSpar2
	Done getting FEA properties
Updating mesh element types based on properties input

Getting FEA constraints.......
	Number of constraints - 1
	Constraint name - rootConstraint
	No "constraintType" specified for Constraint tuple rootConstraint, defaulting to "ZeroDisplacement"
	No "groupName" specified for Constraint tuple rootConstraint, going to use constraint name
	Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults

Getting FEA loads.......
	Number of loads - 2
	Load name - leftPointLoad
	No "groupName" specified for Load tuple leftPointLoad, going to use load name
	Load name - ritePointLoad
	No "groupName" specified for Load tuple ritePointLoad, going to use load name
	Done getting FEA loads
Optimization Control tuple is NULL - Default optimization control is used

Getting FEA optimization control.......
Done getting FEA Optimization Control
Design_Variable tuple is NULL - No design variables applied
Design_Constraint tuple is NULL - No design constraints applied
Analysis tuple is NULL

Getting FEA analyses.......
	Number of analyses - 1
	Analysis name - Default
	Done getting FEA analyses

Writing Astros grid and connectivity file (in large field format) ....
Finished writing Astros grid file

Writing subElement types (if any) - appending mesh file

Writing Astros instruction file....
	Writing analysis cards
	Writing load ADD cards
	Writing constraint cards--each subcase individually
	Writing load cards
	Writing material cards
	Writing property cards
	Writing coordinate system cards

==&gt; Running mASTROS...
Note: The following floating-point exceptions are signalling: IEEE_UNDERFLOW_FLAG

==&gt; Running mASTROS post-analysis...

--&gt; Maximum displacements:
--&gt; Tmax 52594.60117638786
--&gt; T1max 4359.68
--&gt; T2max 3216.5
--&gt; T3max 52322.2

real	0m13.683s
user	0m17.664s
sys	0m16.518s
+ status=0
+ set +x

=================================================
data/session09/4_astros_Composite.py passed (as expected)
=================================================

[VIGGEN.MIT.EDU:83962] shmem: mmap: an error occurred while determining whether or not /var/folders/l7/7s0m18td3fxg_w_dxpkj1d600000gp/T//ompi.VIGGEN.502/jf.0/2263351296/sm_segment.VIGGEN.502.86e80000.0 could be created.

=================================================
6_tacs_StaticCantilever.py test;
+ python 6_tacs_StaticCantilever.py
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/CAPS/training/2023/training.log
[VIGGEN.MIT.EDU:83972] shmem: mmap: an error occurred while determining whether or not /var/folders/l7/7s0m18td3fxg_w_dxpkj1d600000gp/T//ompi.VIGGEN.502/jf.0/3262054400/sm_segment.VIGGEN.502.c26f0000.0 could be created.

==&gt; Loading geometry from file "../ESP/transport.csm"...

==&gt; Running TACS pre-analysis...

MESSAGE:: Building wingOml


MESSAGE:: Building wingWaffle

Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 5
	Name = leftWingSkin, index = 1
	Name = wingRib, index = 2
	Name = riteWingSkin, index = 3
	Name = wingSpar1, index = 4
	Name = wingSpar2, index = 5
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 2
	Name = wingSpar1, index = 1
	Name = wingSpar2, index = 2
Getting surface mesh for body 1 (of 1)
Body 1 (of 1)
Number of nodes    = 425
Number of elements = 482
Number of triangle elements      = 0
Number of quadrilateral elements = 482
----------------------------
Total number of nodes    = 425
Total number of elements = 482
Mapping Csys attributes ................
	Number of unique Csys attributes = 2
	Name = leftWingSkin, index = 1
	Name = riteWingSkin, index = 2

Getting FEA coordinate systems.......
	Number of coordinate systems - 2
	Coordinate system name - leftWingSkin
	Coordinate system name - riteWingSkin
Mapping capsConstraint attributes ................
	Number of unique capsConstraint attributes = 1
	Name = rootConstraint, index = 1
Mapping capsLoad attributes ................
	Number of unique capsLoad attributes = 4
	Name = leftWingSkin, index = 1
	Name = riteWingSkin, index = 2
	Name = leftPointLoad, index = 3
	Name = ritePointLoad, index = 4
Mapping capsBound attributes ................
	Number of unique capsBound attributes = 4
	Name = upperWing, index = 1
	Name = lowerWing, index = 2
	Name = leftTip, index = 3
	Name = riteTip, index = 4
Mapping capsConnect attributes ................
	Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
	Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
	Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 5
	Name = leftWingSkin, index = 1
	Name = wingRib, index = 2
	Name = riteWingSkin, index = 3
	Name = wingSpar1, index = 4
	Name = wingSpar2, index = 5
Setting FEA Data
	Mesh for body = 0
	Number of nodal coordinates = 425
	Number of elements = 482
	Elemental Nodes = 0
	Elemental Rods  = 0
	Elemental Tria3 = 0
	Elemental Quad4 = 482

Getting FEA materials.......
	Number of materials - 1
	Material name - aluminum
	Done getting FEA materials

Getting FEA properties.......
	Number of properties - 5
	Property name - leftWingSkin
	Property name - riteWingSkin
	Property name - wingRib
	Property name - wingSpar1
	Property name - wingSpar2
	Done getting FEA properties
Updating mesh element types based on properties input

Getting FEA constraints.......
	Number of constraints - 1
	Constraint name - rootConstraint
	No "groupName" specified for Constraint tuple rootConstraint, going to use constraint name
	Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults

Getting FEA loads.......
	Number of loads - 2
	Load name - leftWingSkin
	No "groupName" specified for Load tuple leftWingSkin, going to use load name
	Load name - riteWingSkin
	No "groupName" specified for Load tuple riteWingSkin, going to use load name
	Done getting FEA loads
Design_Variable tuple is NULL - No design variables applied
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL

Getting FEA analyses.......
	Number of analyses - 1
	Analysis name - Default
	Done getting FEA analyses

Writing Nastran grid and connectivity file (in large field format) ....
Finished writing Nastran grid file

Writing subElement types (if any) - appending mesh file

Writing TACS instruction file....
	Writing analysis cards
	Writing load ADD cards
	Writing constraint ADD cards
	Writing load cards
	Writing constraint cards
	Writing material cards
	Writing property cards
	Writing coordinate system cards
[0] Creating TACSAssembler with numOwnedNodes = 425 numElements = 482
[0] BCSRMat: ILU(1000) Input fill ratio 20.00, actual fill ratio: 2.84, nnz(ILU) = 11729

==&gt; Running TACS...

==&gt; Running TACS post-analysis...
Tacs Analysis Outputs...
	functional mass = 511406.7093694836
	functional ks_vmfailure = 0.01913505172742016

real	0m14.614s
user	0m17.314s
sys	0m15.986s
+ status=0
+ set +x

=================================================
data/session09/6_tacs_StaticCantilever.py passed (as expected)
=================================================


=================================================
7_tacs_sizing.py test;
+ python 7_tacs_sizing.py
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/CAPS/training/2023/training.log
[VIGGEN.MIT.EDU:84000] shmem: mmap: an error occurred while determining whether or not /var/folders/l7/7s0m18td3fxg_w_dxpkj1d600000gp/T//ompi.VIGGEN.502/jf.0/1314258944/sm_segment.VIGGEN.502.4e560000.0 could be created.

==&gt; Loading geometry from file "../ESP/transport.csm"...

==&gt; Starting optimization...

MESSAGE:: Building wingOml


MESSAGE:: Building wingWaffle

Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 5
	Name = leftWingSkin, index = 1
	Name = wingRib, index = 2
	Name = riteWingSkin, index = 3
	Name = wingSpar1, index = 4
	Name = wingSpar2, index = 5
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 2
	Name = wingSpar1, index = 1
	Name = wingSpar2, index = 2
Getting surface mesh for body 1 (of 1)
Body 1 (of 1)
Number of nodes    = 3852
Number of elements = 4061
Number of triangle elements      = 0
Number of quadrilateral elements = 4061
----------------------------
Total number of nodes    = 3852
Total number of elements = 4061
Mapping Csys attributes ................
	Number of unique Csys attributes = 2
	Name = leftWingSkin, index = 1
	Name = riteWingSkin, index = 2

Getting FEA coordinate systems.......
	Number of coordinate systems - 2
	Coordinate system name - leftWingSkin
	Coordinate system name - riteWingSkin
Mapping capsConstraint attributes ................
	Number of unique capsConstraint attributes = 1
	Name = rootConstraint, index = 1
Mapping capsLoad attributes ................
	Number of unique capsLoad attributes = 4
	Name = leftWingSkin, index = 1
	Name = riteWingSkin, index = 2
	Name = leftPointLoad, index = 3
	Name = ritePointLoad, index = 4
Mapping capsBound attributes ................
	Number of unique capsBound attributes = 4
	Name = upperWing, index = 1
	Name = lowerWing, index = 2
	Name = leftTip, index = 3
	Name = riteTip, index = 4
Mapping capsConnect attributes ................
	Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
	Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
	Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 5
	Name = leftWingSkin, index = 1
	Name = wingRib, index = 2
	Name = riteWingSkin, index = 3
	Name = wingSpar1, index = 4
	Name = wingSpar2, index = 5
Setting FEA Data
	Mesh for body = 0
	Number of nodal coordinates = 3852
	Number of elements = 4061
	Elemental Nodes = 0
	Elemental Rods  = 0
	Elemental Tria3 = 0
	Elemental Quad4 = 4061

Getting FEA materials.......
	Number of materials - 1
	Material name - aluminum
	Done getting FEA materials

Getting FEA properties.......
	Number of properties - 5
	Property name - leftWingSkin
	Property name - riteWingSkin
	Property name - wingRib
	Property name - wingSpar1
	Property name - wingSpar2
	Done getting FEA properties
Updating mesh element types based on properties input

Getting FEA constraints.......
	Number of constraints - 1
	Constraint name - rootConstraint
	No "groupName" specified for Constraint tuple rootConstraint, going to use constraint name
	Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults

Getting FEA loads.......
	Number of loads - 2
	Load name - leftWingSkin
	No "groupName" specified for Load tuple leftWingSkin, going to use load name
	Load name - riteWingSkin
	No "groupName" specified for Load tuple riteWingSkin, going to use load name
	Done getting FEA loads

Getting FEA design variables.......
	Number of design variables          - 3
	Design_Variable name - ribThk
	Design_Variable name - skinThk
	Design_Variable name - sparThk
	Design_Variable_Relation name - relLeftSkin
	Design_Variable_Relation name - relRib
	Design_Variable_Relation name - relRiteSkin
	Design_Variable_Relation name - relSpar
	Number of design variable relations - 4
	Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL

Getting FEA analyses.......
	Number of analyses - 1
	Analysis name - Default
	Done getting FEA analyses

Writing Nastran grid and connectivity file (in large field format) ....
Finished writing Nastran grid file

Writing subElement types (if any) - appending mesh file

Writing TACS instruction file....
	Writing analysis cards
	Writing load ADD cards
	Writing constraint ADD cards
	Writing load cards
	Writing constraint cards
	Writing material cards
	Writing property cards
	Writing coordinate system cards
	Writing design variable cards
	Writing design variable relation cards
[0] Creating TACSAssembler with numOwnedNodes = 3852 numElements = 4061
[0] BCSRMat: ILU(1000) Input fill ratio 20.00, actual fill ratio: 5.81, nnz(ILU) = 208414
[0] BCSRMat: ILU(1000) Input fill ratio 20.00, actual fill ratio: 5.81, nnz(ILU) = 208414
/Users/jenkins/workspace/ESP_bPreBuilt/CAPS/training/2023/data/session09/7_tacs_sizing.py:144: DeprecationWarning: Conversion of an array with ndim &gt; 0 to a scalar is deprecated, and will error in future. Ensure you extract a single element from your array before performing this operation. (Deprecated NumPy 1.25.)
  xarray[ithick] = float(inputs[thick_dv])
--&gt; ribThk [0.05]
--&gt; skinThk [0.003]
--&gt; sparThk [0.1]
--&gt; mass [351348.85842654]
--&gt; ks_vmfailure [0.1846542]
--&gt; mass [351348.85842654]
--&gt; ks_vmfailure [0.1846542]
--&gt; mass ribThk [[2050883.76790736]]
--&gt; mass skinThk [[10032748.65482082]]
--&gt; mass sparThk [[1314431.32692686]]
--&gt; ks_vmfailure ribThk [[-0.00701648]]
--&gt; ks_vmfailure skinThk [[-0.77735853]]
--&gt; ks_vmfailure sparThk [[-0.0041996]]
[0] BCSRMat: ILU(1000) Input fill ratio 20.00, actual fill ratio: 5.81, nnz(ILU) = 208414
--&gt; ribThk [0.001]
--&gt; skinThk [0.0073915]
--&gt; sparThk [0.001]
--&gt; mass [164785.66958227]
--&gt; ks_vmfailure [0.18458243]
--&gt; mass ribThk [[2050883.76790736]]
--&gt; mass skinThk [[10032748.65482082]]
--&gt; mass sparThk [[1314431.32692686]]
--&gt; ks_vmfailure ribThk [[-0.27196737]]
--&gt; ks_vmfailure skinThk [[-0.30937548]]
--&gt; ks_vmfailure sparThk [[-0.20964257]]
[0] BCSRMat: ILU(1000) Input fill ratio 20.00, actual fill ratio: 5.81, nnz(ILU) = 208414
--&gt; ribThk [0.001]
--&gt; skinThk [0.001]
--&gt; sparThk [0.02275036]
--&gt; mass [129250.70931662]
--&gt; ks_vmfailure [0.202395]
[0] BCSRMat: ILU(1000) Input fill ratio 20.00, actual fill ratio: 5.81, nnz(ILU) = 208414
--&gt; ribThk [0.001]
--&gt; skinThk [0.00647724]
--&gt; sparThk [0.00411124]
--&gt; mass [159702.63601836]
--&gt; ks_vmfailure [0.1846874]
--&gt; mass ribThk [[2050883.76790736]]
--&gt; mass skinThk [[10032748.65482082]]
--&gt; mass sparThk [[1314431.32692686]]
--&gt; ks_vmfailure ribThk [[-0.28436096]]
--&gt; ks_vmfailure skinThk [[-0.36624822]]
--&gt; ks_vmfailure sparThk [[-0.04559206]]
[0] BCSRMat: ILU(1000) Input fill ratio 20.00, actual fill ratio: 5.81, nnz(ILU) = 208414
--&gt; ribThk [0.01796767]
--&gt; skinThk [0.001]
--&gt; sparThk [0.0012266]
--&gt; mass [135757.93266609]
--&gt; ks_vmfailure [0.20100422]
[0] BCSRMat: ILU(1000) Input fill ratio 20.00, actual fill ratio: 5.81, nnz(ILU) = 208414
--&gt; ribThk [0.00335945]
--&gt; skinThk [0.0057156]
--&gt; sparThk [0.00371011]
--&gt; mass [156372.98610093]
--&gt; ks_vmfailure [0.184766]
--&gt; mass ribThk [[2050883.76790736]]
--&gt; mass skinThk [[10032748.65482082]]
--&gt; mass sparThk [[1314431.32692686]]
--&gt; ks_vmfailure ribThk [[-0.04729604]]
--&gt; ks_vmfailure skinThk [[-0.42959551]]
--&gt; ks_vmfailure sparThk [[-0.0555554]]
[0] BCSRMat: ILU(1000) Input fill ratio 20.00, actual fill ratio: 5.81, nnz(ILU) = 208414
--&gt; ribThk [0.00375231]
--&gt; skinThk [0.01186673]
--&gt; sparThk [0.00559871]
--&gt; mass [221373.85547163]
--&gt; ks_vmfailure [0.18335011]
[0] BCSRMat: ILU(1000) Input fill ratio 20.00, actual fill ratio: 5.81, nnz(ILU) = 208414
--&gt; ribThk [0.00339874]
--&gt; skinThk [0.00633071]
--&gt; sparThk [0.00389897]
--&gt; mass [162873.073038]
--&gt; ks_vmfailure [0.18451376]
[0] BCSRMat: ILU(1000) Input fill ratio 20.00, actual fill ratio: 5.81, nnz(ILU) = 208414
--&gt; ribThk [0.00336363]
--&gt; skinThk [0.00578104]
--&gt; sparThk [0.00373021]
--&gt; mass [157064.50395361]
--&gt; ks_vmfailure [0.18473687]
--&gt; mass ribThk [[2050883.76790736]]
--&gt; mass skinThk [[10032748.65482082]]
--&gt; mass sparThk [[1314431.32692686]]
--&gt; ks_vmfailure ribThk [[-0.04666555]]
--&gt; ks_vmfailure skinThk [[-0.42080693]]
--&gt; ks_vmfailure sparThk [[-0.05455913]]
[0] BCSRMat: ILU(1000) Input fill ratio 20.00, actual fill ratio: 5.81, nnz(ILU) = 208414
--&gt; ribThk [0.001]
--&gt; skinThk [0.01144045]
--&gt; sparThk [0.01226502]
--&gt; mass [220214.90621319]
--&gt; ks_vmfailure [0.18348938]
--&gt; mass ribThk [[2050883.76790736]]
--&gt; mass skinThk [[10032748.65482082]]
--&gt; mass sparThk [[1314431.32692686]]
--&gt; ks_vmfailure ribThk [[-0.22365806]]
--&gt; ks_vmfailure skinThk [[-0.11520218]]
--&gt; ks_vmfailure sparThk [[-0.00935336]]
[0] BCSRMat: ILU(1000) Input fill ratio 20.00, actual fill ratio: 5.81, nnz(ILU) = 208414
--&gt; ribThk [0.0072684]
--&gt; skinThk [0.01192856]
--&gt; sparThk [0.01559744]
--&gt; mass [242347.90075183]
--&gt; ks_vmfailure [0.18318684]
[0] BCSRMat: ILU(1000) Input fill ratio 20.00, actual fill ratio: 5.81, nnz(ILU) = 208414
--&gt; ribThk [0.00374641]
--&gt; skinThk [0.01165431]
--&gt; sparThk [0.01372508]
--&gt; mass [229912.18133305]
--&gt; ks_vmfailure [0.18327621]
[0] BCSRMat: ILU(1000) Input fill ratio 20.00, actual fill ratio: 5.81, nnz(ILU) = 208414
--&gt; ribThk [0.00242408]
--&gt; skinThk [0.01155134]
--&gt; sparThk [0.01302209]
--&gt; mass [225243.1650107]
--&gt; ks_vmfailure [0.1833334]
--&gt; mass ribThk [[2050883.76790736]]
--&gt; mass skinThk [[10032748.65482082]]
--&gt; mass sparThk [[1314431.32692686]]
--&gt; ks_vmfailure ribThk [[-0.0434139]]
--&gt; ks_vmfailure skinThk [[-0.10912079]]
--&gt; ks_vmfailure sparThk [[-0.00870169]]
[0] BCSRMat: ILU(1000) Input fill ratio 20.00, actual fill ratio: 5.81, nnz(ILU) = 208414
--&gt; ribThk [0.00273287]
--&gt; skinThk [0.02302448]
--&gt; sparThk [0.0208413]
--&gt; mass [351261.40661445]
--&gt; ks_vmfailure [0.18265034]
[0] BCSRMat: ILU(1000) Input fill ratio 20.00, actual fill ratio: 5.81, nnz(ILU) = 208414
--&gt; ribThk [0.0024606]
--&gt; skinThk [0.01290839]
--&gt; sparThk [0.01394695]
--&gt; mass [240148.65608909]
--&gt; ks_vmfailure [0.18319167]
--&gt; mass ribThk [[2050883.76790736]]
--&gt; mass skinThk [[10032748.65482082]]
--&gt; mass sparThk [[1314431.32692686]]
--&gt; ks_vmfailure ribThk [[-0.04034006]]
--&gt; ks_vmfailure skinThk [[-0.08778047]]
--&gt; ks_vmfailure sparThk [[-0.00731659]]
[0] BCSRMat: ILU(1000) Input fill ratio 20.00, actual fill ratio: 5.81, nnz(ILU) = 208414
--&gt; ribThk [0.006155]
--&gt; skinThk [0.0257837]
--&gt; sparThk [0.00197909]
--&gt; mass [361169.22513746]
--&gt; ks_vmfailure [0.18264483]
--&gt; mass ribThk [[2050883.76790736]]
--&gt; mass skinThk [[10032748.65482082]]
--&gt; mass sparThk [[1314431.32692686]]
--&gt; ks_vmfailure ribThk [[-0.00640593]]
--&gt; ks_vmfailure skinThk [[-0.02501034]]
--&gt; ks_vmfailure sparThk [[-0.04889085]]
[0] BCSRMat: ILU(1000) Input fill ratio 20.00, actual fill ratio: 5.81, nnz(ILU) = 208414
--&gt; ribThk [0.00712924]
--&gt; skinThk [0.0266472]
--&gt; sparThk [0.01459881]
--&gt; mass [388418.28899787]
--&gt; ks_vmfailure [0.18252538]
[0] BCSRMat: ILU(1000) Input fill ratio 20.00, actual fill ratio: 5.81, nnz(ILU) = 208414
--&gt; ribThk [0.00664408]
--&gt; skinThk [0.02621719]
--&gt; sparThk [0.00831441]
--&gt; mass [374848.72598794]
--&gt; ks_vmfailure [0.18255641]
--&gt; mass ribThk [[2050883.76790736]]
--&gt; mass skinThk [[10032748.65482082]]
--&gt; mass sparThk [[1314431.32692686]]
--&gt; ks_vmfailure ribThk [[-0.00573855]]
--&gt; ks_vmfailure skinThk [[-0.02377713]]
--&gt; ks_vmfailure sparThk [[-0.00357553]]
[0] BCSRMat: ILU(1000) Input fill ratio 20.00, actual fill ratio: 5.81, nnz(ILU) = 208414
--&gt; ribThk [0.01009093]
--&gt; skinThk [0.04871646]
--&gt; sparThk [0.00877853]
--&gt; mass [608257.37495975]
--&gt; ks_vmfailure [0.18224988]
[0] BCSRMat: ILU(1000) Input fill ratio 20.00, actual fill ratio: 5.81, nnz(ILU) = 208414
--&gt; ribThk [0.00758534]
--&gt; skinThk [0.03236121]
--&gt; sparThk [0.00844115]
--&gt; mass [438587.11278419]
--&gt; ks_vmfailure [0.18243234]
--&gt; mass ribThk [[2050883.76790736]]
--&gt; mass skinThk [[10032748.65482082]]
--&gt; mass sparThk [[1314431.32692686]]
--&gt; ks_vmfailure ribThk [[-0.00425207]]
--&gt; ks_vmfailure skinThk [[-0.01579314]]
--&gt; ks_vmfailure sparThk [[-0.00300188]]
[0] BCSRMat: ILU(1000) Input fill ratio 20.00, actual fill ratio: 5.81, nnz(ILU) = 208414
--&gt; ribThk [0.0124328]
--&gt; skinThk [0.05769986]
--&gt; sparThk [0.01228772]
--&gt; mass [707801.04480008]
--&gt; ks_vmfailure [0.1821848]
--&gt; mass ribThk [[2050883.76790736]]
--&gt; mass skinThk [[10032748.65482082]]
--&gt; mass sparThk [[1314431.32692686]]
--&gt; ks_vmfailure ribThk [[-0.00154459]]
--&gt; ks_vmfailure skinThk [[-0.00512032]]
--&gt; ks_vmfailure sparThk [[-0.00130412]]
[0] BCSRMat: ILU(1000) Input fill ratio 20.00, actual fill ratio: 5.81, nnz(ILU) = 208414
--&gt; ribThk [0.01950989]
--&gt; skinThk [0.08934871]
--&gt; sparThk [0.0213468]
--&gt; mass [1051747.85053898]
--&gt; ks_vmfailure [0.1820658]
--&gt; mass ribThk [[2050883.76790736]]
--&gt; mass skinThk [[10032748.65482082]]
--&gt; mass sparThk [[1314431.32692686]]
--&gt; ks_vmfailure ribThk [[-0.00063906]]
--&gt; ks_vmfailure skinThk [[-0.00214823]]
--&gt; ks_vmfailure sparThk [[-0.00044876]]
[0] BCSRMat: ILU(1000) Input fill ratio 20.00, actual fill ratio: 5.81, nnz(ILU) = 208414
--&gt; ribThk [0.02583689]
--&gt; skinThk [0.11659568]
--&gt; sparThk [0.02854152]
--&gt; mass [1347542.82109991]
--&gt; ks_vmfailure [0.18201544]
--&gt; mass ribThk [[2050883.76790736]]
--&gt; mass skinThk [[10032748.65482082]]
--&gt; mass sparThk [[1314431.32692686]]
--&gt; ks_vmfailure ribThk [[-0.00036949]]
--&gt; ks_vmfailure skinThk [[-0.001262]]
--&gt; ks_vmfailure sparThk [[-0.00025396]]
[0] BCSRMat: ILU(1000) Input fill ratio 20.00, actual fill ratio: 5.81, nnz(ILU) = 208414
--&gt; ribThk [0.02866513]
--&gt; skinThk [0.12727245]
--&gt; sparThk [0.03216313]
--&gt; mass [1465220.87471137]
--&gt; ks_vmfailure [0.18200133]
--&gt; mass ribThk [[2050883.76790736]]
--&gt; mass skinThk [[10032748.65482082]]
--&gt; mass sparThk [[1314431.32692686]]
--&gt; ks_vmfailure ribThk [[-0.00030315]]
--&gt; ks_vmfailure skinThk [[-0.0010584]]
--&gt; ks_vmfailure sparThk [[-0.00020293]]
[0] BCSRMat: ILU(1000) Input fill ratio 20.00, actual fill ratio: 5.81, nnz(ILU) = 208414
--&gt; ribThk [0.02925022]
--&gt; skinThk [0.12815145]
--&gt; sparThk [0.03326292]
--&gt; mass [1476685.21150207]
--&gt; ks_vmfailure [0.18200002]
--&gt; mass ribThk [[2050883.76790736]]
--&gt; mass skinThk [[10032748.65482082]]
--&gt; mass sparThk [[1314431.32692686]]
--&gt; ks_vmfailure ribThk [[-0.00029294]]
--&gt; ks_vmfailure skinThk [[-0.00104297]]
--&gt; ks_vmfailure sparThk [[-0.00019215]]
[0] BCSRMat: ILU(1000) Input fill ratio 20.00, actual fill ratio: 5.81, nnz(ILU) = 208414
--&gt; ribThk [0.03009621]
--&gt; skinThk [0.1275515]
--&gt; sparThk [0.03531214]
--&gt; mass [1475094.60332159]
--&gt; ks_vmfailure [0.18200002]
--&gt; mass ribThk [[2050883.76790736]]
--&gt; mass skinThk [[10032748.65482082]]
--&gt; mass sparThk [[1314431.32692686]]
--&gt; ks_vmfailure ribThk [[-0.00028081]]
--&gt; ks_vmfailure skinThk [[-0.00105015]]
--&gt; ks_vmfailure sparThk [[-0.00017649]]
[0] BCSRMat: ILU(1000) Input fill ratio 20.00, actual fill ratio: 5.81, nnz(ILU) = 208414
--&gt; ribThk [0.0328392]
--&gt; skinThk [0.12577741]
--&gt; sparThk [0.04163974]
--&gt; mass [1471238.3581688]
--&gt; ks_vmfailure [0.18200018]
--&gt; mass ribThk [[2050883.76790736]]
--&gt; mass skinThk [[10032748.65482082]]
--&gt; mass sparThk [[1314431.32692686]]
--&gt; ks_vmfailure ribThk [[-0.00024714]]
--&gt; ks_vmfailure skinThk [[-0.00107055]]
--&gt; ks_vmfailure sparThk [[-0.00014459]]
[0] BCSRMat: ILU(1000) Input fill ratio 20.00, actual fill ratio: 5.81, nnz(ILU) = 208414
--&gt; ribThk [0.03383625]
--&gt; skinThk [0.12543563]
--&gt; sparThk [0.04369691]
--&gt; mass [1472558.27241667]
--&gt; ks_vmfailure [0.18200001]
--&gt; mass ribThk [[2050883.76790736]]
--&gt; mass skinThk [[10032748.65482082]]
--&gt; mass sparThk [[1314431.32692686]]
--&gt; ks_vmfailure ribThk [[-0.00023649]]
--&gt; ks_vmfailure skinThk [[-0.00107307]]
--&gt; ks_vmfailure sparThk [[-0.00013766]]
[0] BCSRMat: ILU(1000) Input fill ratio 20.00, actual fill ratio: 5.81, nnz(ILU) = 208414
--&gt; ribThk [0.03427623]
--&gt; skinThk [0.12525038]
--&gt; sparThk [0.04448082]
--&gt; mass [1472632.44194227]
--&gt; ks_vmfailure [0.182]
--&gt; mass ribThk [[2050883.76790736]]
--&gt; mass skinThk [[10032748.65482082]]
--&gt; mass sparThk [[1314431.32692686]]
--&gt; ks_vmfailure ribThk [[-0.00023207]]
--&gt; ks_vmfailure skinThk [[-0.00107486]]
--&gt; ks_vmfailure sparThk [[-0.00013542]]
[0] BCSRMat: ILU(1000) Input fill ratio 20.00, actual fill ratio: 5.81, nnz(ILU) = 208414
--&gt; ribThk [0.03444291]
--&gt; skinThk [0.12519626]
--&gt; sparThk [0.04463972]
--&gt; mass [1472640.20078909]
--&gt; ks_vmfailure [0.182]
--&gt; mass ribThk [[2050883.76790736]]
--&gt; mass skinThk [[10032748.65482082]]
--&gt; mass sparThk [[1314431.32692686]]
--&gt; ks_vmfailure ribThk [[-0.0002304]]
--&gt; ks_vmfailure skinThk [[-0.00107543]]
--&gt; ks_vmfailure sparThk [[-0.00013502]]
[0] BCSRMat: ILU(1000) Input fill ratio 20.00, actual fill ratio: 5.81, nnz(ILU) = 208414
--&gt; ribThk [0.0348802]
--&gt; skinThk [0.12509099]
--&gt; sparThk [0.04473341]
--&gt; mass [1472603.98217904]
--&gt; ks_vmfailure [0.182]
--&gt; mass ribThk [[2050883.76790736]]
--&gt; mass skinThk [[10032748.65482082]]
--&gt; mass sparThk [[1314431.32692686]]
--&gt; ks_vmfailure ribThk [[-0.00022607]]
--&gt; ks_vmfailure skinThk [[-0.0010767]]
--&gt; ks_vmfailure sparThk [[-0.00013492]]
[0] BCSRMat: ILU(1000) Input fill ratio 20.00, actual fill ratio: 5.81, nnz(ILU) = 208414
--&gt; ribThk [0.03534323]
--&gt; skinThk [0.12504137]
--&gt; sparThk [0.04436116]
--&gt; mass [1472566.46844939]
--&gt; ks_vmfailure [0.182]
--&gt; mass ribThk [[2050883.76790736]]
--&gt; mass skinThk [[10032748.65482082]]
--&gt; mass sparThk [[1314431.32692686]]
--&gt; ks_vmfailure ribThk [[-0.00022152]]
--&gt; ks_vmfailure skinThk [[-0.00107758]]
--&gt; ks_vmfailure sparThk [[-0.00013618]]
[0] BCSRMat: ILU(1000) Input fill ratio 20.00, actual fill ratio: 5.81, nnz(ILU) = 208414
--&gt; ribThk [0.0356444]
--&gt; skinThk [0.125092]
--&gt; sparThk [0.04348019]
--&gt; mass [1472534.17646355]
--&gt; ks_vmfailure [0.182]
--&gt; mass ribThk [[2050883.76790736]]
--&gt; mass skinThk [[10032748.65482082]]
--&gt; mass sparThk [[1314431.32692686]]
--&gt; ks_vmfailure ribThk [[-0.00021851]]
--&gt; ks_vmfailure skinThk [[-0.00107752]]
--&gt; ks_vmfailure sparThk [[-0.00013901]]
[0] BCSRMat: ILU(1000) Input fill ratio 20.00, actual fill ratio: 5.81, nnz(ILU) = 208414
--&gt; ribThk [0.03558665]
--&gt; skinThk [0.12517522]
--&gt; sparThk [0.04293808]
--&gt; mass [1472538.0779954]
--&gt; ks_vmfailure [0.182]
--&gt; mass ribThk [[2050883.76790736]]
--&gt; mass skinThk [[10032748.65482082]]
--&gt; mass sparThk [[1314431.32692686]]
--&gt; ks_vmfailure ribThk [[-0.00021892]]
--&gt; ks_vmfailure skinThk [[-0.0010768]]
--&gt; ks_vmfailure sparThk [[-0.00014078]]
[0] BCSRMat: ILU(1000) Input fill ratio 20.00, actual fill ratio: 5.81, nnz(ILU) = 208414
--&gt; ribThk [0.03548923]
--&gt; skinThk [0.12520791]
--&gt; sparThk [0.0428432]
--&gt; mass [1472541.53467339]
--&gt; ks_vmfailure [0.182]
--&gt; mass ribThk [[2050883.76790736]]
--&gt; mass skinThk [[10032748.65482082]]
--&gt; mass sparThk [[1314431.32692686]]
--&gt; ks_vmfailure ribThk [[-0.0002198]]
--&gt; ks_vmfailure skinThk [[-0.00107644]]
--&gt; ks_vmfailure sparThk [[-0.00014107]]
[0] BCSRMat: ILU(1000) Input fill ratio 20.00, actual fill ratio: 5.81, nnz(ILU) = 208414
--&gt; ribThk [0.03546489]
--&gt; skinThk [0.12521187]
--&gt; sparThk [0.04285139]
--&gt; mass [1472542.05815828]
--&gt; ks_vmfailure [0.182]
--&gt; mass ribThk [[2050883.76790736]]
--&gt; mass skinThk [[10032748.65482082]]
--&gt; mass sparThk [[1314431.32692686]]
--&gt; ks_vmfailure ribThk [[-0.00022003]]
--&gt; ks_vmfailure skinThk [[-0.00107639]]
--&gt; ks_vmfailure sparThk [[-0.00014103]]
[0] BCSRMat: ILU(1000) Input fill ratio 20.00, actual fill ratio: 5.81, nnz(ILU) = 208414
--&gt; ribThk [0.03546431]
--&gt; skinThk [0.12521175]
--&gt; sparThk [0.04285324]
--&gt; mass [1472542.08686109]
--&gt; ks_vmfailure [0.182]
--&gt; mass ribThk [[2050883.76790736]]
--&gt; mass skinThk [[10032748.65482082]]
--&gt; mass sparThk [[1314431.32692686]]
--&gt; ks_vmfailure ribThk [[-0.00022003]]
--&gt; ks_vmfailure skinThk [[-0.00107639]]
--&gt; ks_vmfailure sparThk [[-0.00014102]]
Optimization terminated successfully    (Exit mode 0)
            Current function value: 4.207263105317389
            Iterations: 28
            Function evaluations: 37
            Gradient evaluations: 28
Optimization Complete
-----------------------------------
==&gt; Optimized value:
--&gt;  ribThk [0.03546431]
--&gt;  skinThk [0.12521175]
--&gt;  sparThk [0.04285324]

real	0m40.141s
user	0m44.817s
sys	0m16.445s
+ status=0
+ set +x

=================================================
data/session09/7_tacs_sizing.py passed (as expected)
=================================================


=================================================
2_aeroelastic_Iterative_SU2_Astros.py test;
+ python 2_aeroelastic_Iterative_SU2_Astros.py
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/CAPS/training/2023/training.log

MESSAGE:: Building wingOml


MESSAGE:: Building wingWaffle


==&gt; Running SU2 pre-analysis...
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 2
	Name = Wing, index = 1
	Name = Farfield, index = 2
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 3
	Name = leftWing, index = 1
	Name = riteWing, index = 2
	Name = Farfield, index = 3

Getting mesh sizing parameters
	Mesh sizing name - Farfield
	Mesh sizing name - leftWing
	Mesh sizing name - riteWing
	Done getting mesh sizing parameters
 
AFLR2    : ---------------------------------------
AFLR2    : AFLR2 LIBRARY
AFLR2    : ADVANCING-FRONT/LOCAL-RECONNECTION
AFLR2    : TRIA/QUAD GRID GENERATOR
AFLR2    : Version Number 9.18.1
AFLR2    : Version Date   06/11/24 @ 05:52PM
AFLR2    : Compile OS     Darwin 23.5.0 arm64
AFLR2    : Compile Date   06/11/24 @ 05:52PM
AFLR2    : Copyright 1994-2021, D.L. Marcum
AFLR2    : ---------------------------------------
 
AFLR4    : ---------------------------------------
AFLR4    : AFLR4 LIBRARY
AFLR4    : ADVANCING-FRONT/LOCAL-RECONNECTION
AFLR4    : TRIA/QUAD SURFACE GRID GENERATOR
AFLR4    : Version Number 11.5.15
AFLR4    : Version Date   07/19/24 @ 07:04PM
AFLR4    : Compile OS     Darwin 23.5.0 arm64
AFLR4    : Compile Date   07/19/24 @ 07:06PM
AFLR4    : Copyright 1994-2021, D.L. Marcum
AFLR4    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.8.1
EGADS    : ---------------------------------------

EGADS    : EGADS CAD Geometry Setup

EGADS    : Model has 2 Active Bodies

EGADS    : Body 0 is a SolidBody
EGADS    : Body 0 has 1 Shells
EGADS    : Body 0 has 10 Faces
EGADS    : Body 0 has 18 Edges
EGADS    : Body 0 has 10 Loops
EGADS    : Body 0 has 10 Nodes
EGADS    : Body 1 is a SolidBody
EGADS    : Body 1 has 1 Shells
EGADS    : Body 1 has 6 Faces
EGADS    : Body 1 has 12 Edges
EGADS    : Body 1 has 6 Loops
EGADS    : Body 1 has 8 Nodes

EGADS    : Check Grid BCs

EGADS    : Grid BCs are OK

EGADS    : Face Neighbor-Faces Information

EGADS    : QC  = Face Quad Combination Flag
EGADS    : IER = Face Isolated Edge Refinement Flag
EGADS    : ER  = Face Edge Refinement Factor
EGADS    :       Not applicable for Faces with a FarField Grid BC.
EGADS    : SF  = Face Scale Factor
EGADS    :       Not applicable for Faces with a FarField Grid BC.

EGADS    :   Face          Body    QC   IER       ER    Scale   Neighbor
EGADS    :     ID  Active    ID  Flag  Flag   Weight   Factor   Faces
EGADS    :      1     Yes     0     0     1        1        1   2 3 6
EGADS    :      2     Yes     0     0     1        1        1   1 4 5
EGADS    :      3     Yes     0     0     1        1        1   1 4 8
EGADS    :      4     Yes     0     0     1        1        1   2 3 5
EGADS    :      5     Yes     0     0     1        1        1   2 4
EGADS    :      6     Yes     0     0     1        1        1   1 7 8
EGADS    :      7     Yes     0     0     1        1        1   6 9 10
EGADS    :      8     Yes     0     0     1        1        1   3 6 9
EGADS    :      9     Yes     0     0     1        1        1   7 8 10
EGADS    :     10     Yes     0     0     1        1        1   7 9
EGADS    :     11     Yes     1     0     1       NA       NA   13 14 15 16
EGADS    :     12     Yes     1     0     1       NA       NA   13 14 15 16
EGADS    :     13     Yes     1     0     1       NA       NA   11 12 15 16
EGADS    :     14     Yes     1     0     1       NA       NA   11 12 15 16
EGADS    :     15     Yes     1     0     1       NA       NA   11 12 13 14
EGADS    :     16     Yes     1     0     1       NA       NA   11 12 13 14

EGADS    : Face Edges Information

EGADS    :   Face   Edges
EGADS    :      1   -1 2 3 -4
EGADS    :      2   -5 4 6 -7
EGADS    :      3   -3 8 1 -9
EGADS    :      4   -6 9 5 -10
EGADS    :      5   7 10
EGADS    :      6   11 13 -12 -2
EGADS    :      7   14 16 -15 -13
EGADS    :      8   12 17 -11 -8
EGADS    :      9   15 18 -14 -17
EGADS    :     10   -16 -18
EGADS    :     11   19 20 -21 -22
EGADS    :     12   -23 26 25 -24
EGADS    :     13   27 23 -28 -19
EGADS    :     14   -29 21 30 -25
EGADS    :     15   22 29 -26 -27
EGADS    :     16   -20 28 24 -30

EGADS    : Face Loops Information

EGADS    :   Face   Loops
EGADS    :      1   1
EGADS    :      2   2
EGADS    :      3   3
EGADS    :      4   4
EGADS    :      5   5
EGADS    :      6   6
EGADS    :      7   7
EGADS    :      8   8
EGADS    :      9   9
EGADS    :     10   10
EGADS    :     11   11
EGADS    :     12   12
EGADS    :     13   13
EGADS    :     14   14
EGADS    :     15   15
EGADS    :     16   16

EGADS    : Loop Edges Information

EGADS    :   Loop  Active   Edges
EGADS    :      1     Yes   -1 2 3 -4
EGADS    :      2     Yes   -5 4 6 -7
EGADS    :      3     Yes   -3 8 1 -9
EGADS    :      4     Yes   -6 9 5 -10
EGADS    :      5     Yes   7 10
EGADS    :      6     Yes   11 13 -12 -2
EGADS    :      7     Yes   14 16 -15 -13
EGADS    :      8     Yes   12 17 -11 -8
EGADS    :      9     Yes   15 18 -14 -17
EGADS    :     10     Yes   -16 -18
EGADS    :     11     Yes   19 20 -21 -22
EGADS    :     12     Yes   -23 26 25 -24
EGADS    :     13     Yes   27 23 -28 -19
EGADS    :     14     Yes   -29 21 30 -25
EGADS    :     15     Yes   22 29 -26 -27
EGADS    :     16     Yes   -20 28 24 -30

EGADS    : Edge Node, Scale Factor, and Neighbor-Faces Information

EGADS    : ESF = Edge Scale Factor
EGADS    :       Not applicable for DEGENERATE Edges or Edges with a FarField
EGADS    :       Grid BC Neighbor Face.

EGADS    :                                             Neighbor
EGADS    :   Edge  Body  Active Node1 Node2      ESF   Faces
EGADS    :      1     0     Yes     1     2        1   1 3
EGADS    :      2     0     Yes     1     3        1   1 6
EGADS    :      3     0     Yes     3     4        1   1 3
EGADS    :      4     0     Yes     2     4        1   1 2
EGADS    :      5     0     Yes     2     5        1   2 4
EGADS    :      6     0     Yes     4     6        1   2 4
EGADS    :      7     0     Yes     5     6        1   2 5
EGADS    :      8     0     Yes     3     1        1   3 8
EGADS    :      9     0     Yes     4     2        1   3 4
EGADS    :     10     0     Yes     6     5        1   4 5
EGADS    :     11     0     Yes     1     7        1   6 8
EGADS    :     12     0     Yes     3     8        1   6 8
EGADS    :     13     0     Yes     7     8        1   6 7
EGADS    :     14     0     Yes     7     9        1   7 9
EGADS    :     15     0     Yes     8    10        1   7 9
EGADS    :     16     0     Yes     9    10        1   7 10
EGADS    :     17     0     Yes     8     7        1   8 9
EGADS    :     18     0     Yes    10     9        1   9 10
EGADS    :     19     1     Yes    12    11       NA   11 13
EGADS    :     20     1     Yes    11    13       NA   11 16
EGADS    :     21     1     Yes    14    13       NA   11 14
EGADS    :     22     1     Yes    12    14       NA   11 15
EGADS    :     23     1     Yes    16    15       NA   12 13
EGADS    :     24     1     Yes    15    17       NA   12 16
EGADS    :     25     1     Yes    18    17       NA   12 14
EGADS    :     26     1     Yes    16    18       NA   12 15
EGADS    :     27     1     Yes    12    16       NA   13 15
EGADS    :     28     1     Yes    11    15       NA   13 16
EGADS    :     29     1     Yes    14    18       NA   14 15
EGADS    :     30     1     Yes    13    17       NA   14 16

EGADS    : Node Information

EGADS    :   Node  Active      Coordinates
EGADS    :      1     Yes       97.2007855                0                0
EGADS    :      2     Yes       97.9335611                0                0
EGADS    :      3     Yes               50                0                0
EGADS    :      4     Yes       75.3047874                0                0
EGADS    :      5     Yes       123.552357                0        4.7180639
EGADS    :      6     Yes       118.391317                0       3.99272703
EGADS    :      7     Yes       97.9335611       36.1389817                0
EGADS    :      8     Yes       75.3047874       36.1389817                0
EGADS    :      9     Yes       123.552357       97.6729236        4.7180639
EGADS    :     10     Yes       118.391317       97.6729236       3.99272703
EGADS    :     11     Yes                0                0       1951.57774
EGADS    :     12     Yes                0                0                0
EGADS    :     13     Yes                0       1953.45847       1951.57774
EGADS    :     14     Yes                0       1953.45847                0
EGADS    :     15     Yes       2040.21562                0       1951.57774
EGADS    :     16     Yes       2040.21562                0                0
EGADS    :     17     Yes       2040.21562       1953.45847       1951.57774
EGADS    :     18     Yes       2040.21562       1953.45847                0

EGADS    : Face and Edge Match Information

EGADS    : No Face Matches Found

AFLR4    : Surface Mesh Spacing Setup

AFLR4    : Max Bounding Box Length     = 3906.92
AFLR4    : Min Bounding Box Length     = 3906.92
AFLR4    : Max Ref Bounding Box Length = 195.346
AFLR4    : Min Ref Bounding Box Length = 13.1976
AFLR4    : Reference Length            = 21.7051
AFLR4    : BL Thickness                = 0
AFLR4    : FarField Spacing            = 2651.51
AFLR4    : Abs Min Surf Spacing        = 0.0542627
AFLR4    : Min Surf Spacing            = 0.108525
AFLR4    : Max Surf Spacing            = 2.17051
AFLR4    : Global Scale Factor         = 5

AFLR4    : Geometry Definition Information

AFLR4    : Definition              Definition   Composite             Grid BC
AFLR4    :         ID                    Type          ID                Type
AFLR4    :          0     glue-only composite           -                   -
AFLR4    :          1            CAD geometry           0            STD w/BL
AFLR4    :          2            CAD geometry           0            STD w/BL
AFLR4    :          3            CAD geometry           0            STD w/BL
AFLR4    :          4            CAD geometry           0            STD w/BL
AFLR4    :          5            CAD geometry           0            STD w/BL
AFLR4    :          6            CAD geometry           0            STD w/BL
AFLR4    :          7            CAD geometry           0            STD w/BL
AFLR4    :          8            CAD geometry           0            STD w/BL
AFLR4    :          9            CAD geometry           0            STD w/BL
AFLR4    :         10            CAD geometry           0            STD w/BL
AFLR4    :         11            CAD geometry           0            FARFIELD
AFLR4    :         12            CAD geometry           0            FARFIELD
AFLR4    :         13            CAD geometry           0            FARFIELD
AFLR4    :         14            CAD geometry           0            FARFIELD
AFLR4    :         15            CAD geometry           0            FARFIELD
AFLR4    :         16            CAD geometry           0            FARFIELD

AFLR4    : Define CAD surface definition 1
AFLR4    : Define CAD surface definition 2
AFLR4    : Define CAD surface definition 3
AFLR4    : Define CAD surface definition 4
AFLR4    : Define CAD surface definition 5
AFLR4    : Define CAD surface definition 6
AFLR4    : Define CAD surface definition 7
AFLR4    : Define CAD surface definition 8
AFLR4    : Define CAD surface definition 9
AFLR4    : Define CAD surface definition 10
AFLR4    : Define CAD surface definition 11
AFLR4    : Define CAD surface definition 12
AFLR4    : Define CAD surface definition 13
AFLR4    : Define CAD surface definition 14
AFLR4    : Define CAD surface definition 15
AFLR4    : Define CAD surface definition 16

AFLR4    : Surface Grid Generation

AFLR4    : Generate optimal mesh on surface definition 1
AFLR2    : Nodes, Trias,Quads=      1107      2082         0
AFLR4    : Nodes, Trias,Quads=       685      1238         0

AFLR4    : Generate optimal mesh on surface definition 2
AFLR2    : Nodes, Trias,Quads=      1473      2759         0
AFLR4    : Nodes, Trias,Quads=       721      1255         0

AFLR4    : Generate optimal mesh on surface definition 3
AFLR2    : Nodes, Trias,Quads=      1116      2100         0
AFLR4    : Nodes, Trias,Quads=       671      1210         0

AFLR4    : Generate optimal mesh on surface definition 4
AFLR2    : Nodes, Trias,Quads=      1458      2729         0
AFLR4    : Nodes, Trias,Quads=       714      1241         0

AFLR4    : Generate optimal mesh on surface definition 5
AFLR2    : Nodes, Trias,Quads=        20        24         0
AFLR4    : Nodes, Trias,Quads=        14        12         0

AFLR4    : Generate optimal mesh on surface definition 6
AFLR2    : Nodes, Trias,Quads=      1108      2084         0
AFLR4    : Nodes, Trias,Quads=       683      1234         0

AFLR4    : Generate optimal mesh on surface definition 7
AFLR2    : Nodes, Trias,Quads=      1488      2789         0
AFLR4    : Nodes, Trias,Quads=       714      1241         0

AFLR4    : Generate optimal mesh on surface definition 8
AFLR2    : Nodes, Trias,Quads=      1112      2092         0
AFLR4    : Nodes, Trias,Quads=       653      1174         0

AFLR4    : Generate optimal mesh on surface definition 9
AFLR2    : Nodes, Trias,Quads=      1456      2725         0
AFLR4    : Nodes, Trias,Quads=       708      1229         0

AFLR4    : Generate optimal mesh on surface definition 10
AFLR2    : Nodes, Trias,Quads=        20        24         0
AFLR4    : Nodes, Trias,Quads=        14        12         0

AFLR4    : Generate optimal mesh on surface definition 11
AFLR2    : Nodes, Trias,Quads=         5         4         0
AFLR4    : Nodes, Trias,Quads=         4         2         0

AFLR4    : Generate optimal mesh on surface definition 12
AFLR2    : Nodes, Trias,Quads=         5         4         0
AFLR4    : Nodes, Trias,Quads=         4         2         0

AFLR4    : Generate optimal mesh on surface definition 13
AFLR2    : Nodes, Trias,Quads=         5         4         0
AFLR4    : Nodes, Trias,Quads=         4         2         0

AFLR4    : Generate optimal mesh on surface definition 14
AFLR2    : Nodes, Trias,Quads=         5         4         0
AFLR4    : Nodes, Trias,Quads=         4         2         0

AFLR4    : Generate optimal mesh on surface definition 15
AFLR2    : Nodes, Trias,Quads=         5         4         0
AFLR4    : Nodes, Trias,Quads=         4         2         0

AFLR4    : Generate optimal mesh on surface definition 16
AFLR2    : Nodes, Trias,Quads=         5         4         0
AFLR4    : Nodes, Trias,Quads=         4         2         0

DGEOM    : Add surface definitions to composite definition 0
DGEOM    : Glue composite surface definition 0
DGEOM    : Nodes,Faces,BEdges=      4933      9858      1312

AFLR4    : Curvature BG Surface Grid Generation

AFLR4    : Nodes, Faces      =      4933      9858

AFLR4    : Surface Grid Generation

AFLR4    : Generate optimal mesh on surface definition 1
AFLR2    : Nodes, Trias,Quads=     12796     24695         0
AFLR4    : Nodes, Trias,Quads=      7764     14631         0

AFLR4    : Generate optimal mesh on surface definition 2
AFLR2    : Nodes, Trias,Quads=     29251     57087         0
AFLR4    : Nodes, Trias,Quads=     12448     23481         0

AFLR4    : Generate optimal mesh on surface definition 3
AFLR2    : Nodes, Trias,Quads=     12136     23411         0
AFLR4    : Nodes, Trias,Quads=      7447     14033         0

AFLR4    : Generate optimal mesh on surface definition 4
AFLR2    : Nodes, Trias,Quads=     29424     57435         0
AFLR4    : Nodes, Trias,Quads=     12399     23385         0

AFLR4    : Generate optimal mesh on surface definition 5
AFLR2    : Nodes, Trias,Quads=       196       293         0
AFLR4    : Nodes, Trias,Quads=       188       277         0

AFLR4    : Generate optimal mesh on surface definition 6
AFLR2    : Nodes, Trias,Quads=     12819     24741         0
AFLR4    : Nodes, Trias,Quads=      7725     14553         0

AFLR4    : Generate optimal mesh on surface definition 7
AFLR2    : Nodes, Trias,Quads=     29437     57459         0
AFLR4    : Nodes, Trias,Quads=     12412     23409         0

AFLR4    : Generate optimal mesh on surface definition 8
AFLR2    : Nodes, Trias,Quads=     12144     23427         0
AFLR4    : Nodes, Trias,Quads=      7471     14081         0

AFLR4    : Generate optimal mesh on surface definition 9
AFLR2    : Nodes, Trias,Quads=     29445     57477         0
AFLR4    : Nodes, Trias,Quads=     12478     23543         0

AFLR4    : Generate optimal mesh on surface definition 10
AFLR2    : Nodes, Trias,Quads=       196       293         0
AFLR4    : Nodes, Trias,Quads=       188       277         0

AFLR4    : Generate optimal mesh on surface definition 11
AFLR2    : Nodes, Trias,Quads=        12        14         0
AFLR4    : Nodes, Trias,Quads=         8         6         0

AFLR4    : Generate optimal mesh on surface definition 12
AFLR2    : Nodes, Trias,Quads=        12        14         0
AFLR4    : Nodes, Trias,Quads=         8         6         0

AFLR4    : Generate optimal mesh on surface definition 13
AFLR2    : Nodes, Trias,Quads=        12        14         0
AFLR4    : Nodes, Trias,Quads=         8         6         0

AFLR4    : Generate optimal mesh on surface definition 14
AFLR2    : Nodes, Trias,Quads=        12        14         0
AFLR4    : Nodes, Trias,Quads=         8         6         0

AFLR4    : Generate optimal mesh on surface definition 15
AFLR2    : Nodes, Trias,Quads=        12        14         0
AFLR4    : Nodes, Trias,Quads=         8         6         0

AFLR4    : Generate optimal mesh on surface definition 16
AFLR2    : Nodes, Trias,Quads=        12        14         0
AFLR4    : Nodes, Trias,Quads=         8         6         0

DGEOM    : Add surface definitions to composite definition 0
DGEOM    : Glue composite surface definition 0
DGEOM    : Nodes,Faces,BEdges=     75857    151706      9398

OVERALL  : CPU Time          =     0.981   seconds
Body 1 (of 2)
Number of nodes    = 75837
Number of elements = 151670
Number of triangle elements      = 151670
Number of quadrilateral elements = 0
Body 2 (of 2)
Number of nodes    = 20
Number of elements = 36
Number of triangle elements      = 36
Number of quadrilateral elements = 0
----------------------------
Total number of nodes    = 75857
Total number of elements = 151706
Total number of triangle elements      = 151706
Total number of quadrilateral elements = 0
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 3
	Name = leftWing, index = 1
	Name = riteWing, index = 2
	Name = Farfield, index = 3
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 2
	Name = Wing, index = 1
	Name = Farfield, index = 2
Getting volume mesh
 
UG PARAM : SETTING INPUT PARAMETERS FROM ARGUMENT VECTOR
 
UG PARAM : mrecm                       = 3         
UG PARAM : mrecqm                      = 3         
UG PARAM : mpfrmt                      = 0         
 
AFLR2    : ---------------------------------------
AFLR2    : AFLR2 LIBRARY
AFLR2    : ADVANCING-FRONT/LOCAL-RECONNECTION
AFLR2    : TRIA/QUAD GRID GENERATOR
AFLR2    : Version Number 9.18.1
AFLR2    : Version Date   06/11/24 @ 05:52PM
AFLR2    : Compile OS     Darwin 23.5.0 arm64
AFLR2    : Compile Date   06/11/24 @ 05:52PM
AFLR2    : Copyright 1994-2021, D.L. Marcum
AFLR2    : ---------------------------------------
 
AFLR4    : ---------------------------------------
AFLR4    : AFLR4 LIBRARY
AFLR4    : ADVANCING-FRONT/LOCAL-RECONNECTION
AFLR4    : TRIA/QUAD SURFACE GRID GENERATOR
AFLR4    : Version Number 11.5.15
AFLR4    : Version Date   07/19/24 @ 07:04PM
AFLR4    : Compile OS     Darwin 23.5.0 arm64
AFLR4    : Compile Date   07/19/24 @ 07:06PM
AFLR4    : Copyright 1994-2021, D.L. Marcum
AFLR4    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.8.1
EGADS    : ---------------------------------------

EGADS    : EGADS CAD Geometry Setup

EGADS    : Model has 2 Active Bodies

EGADS    : Body 0 is a SolidBody
EGADS    : Body 0 has 1 Shells
EGADS    : Body 0 has 10 Faces
EGADS    : Body 0 has 18 Edges
EGADS    : Body 0 has 10 Loops
EGADS    : Body 0 has 10 Nodes
EGADS    : Body 1 is a SolidBody
EGADS    : Body 1 has 1 Shells
EGADS    : Body 1 has 6 Faces
EGADS    : Body 1 has 12 Edges
EGADS    : Body 1 has 6 Loops
EGADS    : Body 1 has 8 Nodes

EGADS    : Check Grid BCs

EGADS    : Grid BCs are OK

EGADS    : Face Neighbor-Faces Information

EGADS    : QC  = Face Quad Combination Flag
EGADS    : IER = Face Isolated Edge Refinement Flag
EGADS    : ER  = Face Edge Refinement Factor
EGADS    :       Not applicable for Faces with a FarField Grid BC.
EGADS    : SF  = Face Scale Factor
EGADS    :       Not applicable for Faces with a FarField Grid BC.

EGADS    :   Face          Body    QC   IER       ER    Scale   Neighbor
EGADS    :     ID  Active    ID  Flag  Flag   Weight   Factor   Faces
EGADS    :      1     Yes     0     0     1        1        1   2 3 6
EGADS    :      2     Yes     0     0     1        1        1   1 4 5
EGADS    :      3     Yes     0     0     1        1        1   1 4 8
EGADS    :      4     Yes     0     0     1        1        1   2 3 5
EGADS    :      5     Yes     0     0     1        1        1   2 4
EGADS    :      6     Yes     0     0     1        1        1   1 7 8
EGADS    :      7     Yes     0     0     1        1        1   6 9 10
EGADS    :      8     Yes     0     0     1        1        1   3 6 9
EGADS    :      9     Yes     0     0     1        1        1   7 8 10
EGADS    :     10     Yes     0     0     1        1        1   7 9
EGADS    :     11     Yes     1     0     1       NA       NA   13 14 15 16
EGADS    :     12     Yes     1     0     1       NA       NA   13 14 15 16
EGADS    :     13     Yes     1     0     1       NA       NA   11 12 15 16
EGADS    :     14     Yes     1     0     1       NA       NA   11 12 15 16
EGADS    :     15     Yes     1     0     1       NA       NA   11 12 13 14
EGADS    :     16     Yes     1     0     1       NA       NA   11 12 13 14

EGADS    : Face Edges Information

EGADS    :   Face   Edges
EGADS    :      1   -1 2 3 -4
EGADS    :      2   -5 4 6 -7
EGADS    :      3   -3 8 1 -9
EGADS    :      4   -6 9 5 -10
EGADS    :      5   7 10
EGADS    :      6   11 13 -12 -2
EGADS    :      7   14 16 -15 -13
EGADS    :      8   12 17 -11 -8
EGADS    :      9   15 18 -14 -17
EGADS    :     10   -16 -18
EGADS    :     11   19 20 -21 -22
EGADS    :     12   -23 26 25 -24
EGADS    :     13   27 23 -28 -19
EGADS    :     14   -29 21 30 -25
EGADS    :     15   22 29 -26 -27
EGADS    :     16   -20 28 24 -30

EGADS    : Face Loops Information

EGADS    :   Face   Loops
EGADS    :      1   1
EGADS    :      2   2
EGADS    :      3   3
EGADS    :      4   4
EGADS    :      5   5
EGADS    :      6   6
EGADS    :      7   7
EGADS    :      8   8
EGADS    :      9   9
EGADS    :     10   10
EGADS    :     11   11
EGADS    :     12   12
EGADS    :     13   13
EGADS    :     14   14
EGADS    :     15   15
EGADS    :     16   16

EGADS    : Loop Edges Information

EGADS    :   Loop  Active   Edges
EGADS    :      1     Yes   -1 2 3 -4
EGADS    :      2     Yes   -5 4 6 -7
EGADS    :      3     Yes   -3 8 1 -9
EGADS    :      4     Yes   -6 9 5 -10
EGADS    :      5     Yes   7 10
EGADS    :      6     Yes   11 13 -12 -2
EGADS    :      7     Yes   14 16 -15 -13
EGADS    :      8     Yes   12 17 -11 -8
EGADS    :      9     Yes   15 18 -14 -17
EGADS    :     10     Yes   -16 -18
EGADS    :     11     Yes   19 20 -21 -22
EGADS    :     12     Yes   -23 26 25 -24
EGADS    :     13     Yes   27 23 -28 -19
EGADS    :     14     Yes   -29 21 30 -25
EGADS    :     15     Yes   22 29 -26 -27
EGADS    :     16     Yes   -20 28 24 -30

EGADS    : Edge Node, Scale Factor, and Neighbor-Faces Information

EGADS    : ESF = Edge Scale Factor
EGADS    :       Not applicable for DEGENERATE Edges or Edges with a FarField
EGADS    :       Grid BC Neighbor Face.

EGADS    :                                             Neighbor
EGADS    :   Edge  Body  Active Node1 Node2      ESF   Faces
EGADS    :      1     0     Yes     1     2        1   1 3
EGADS    :      2     0     Yes     1     3        1   1 6
EGADS    :      3     0     Yes     3     4        1   1 3
EGADS    :      4     0     Yes     2     4        1   1 2
EGADS    :      5     0     Yes     2     5        1   2 4
EGADS    :      6     0     Yes     4     6        1   2 4
EGADS    :      7     0     Yes     5     6        1   2 5
EGADS    :      8     0     Yes     3     1        1   3 8
EGADS    :      9     0     Yes     4     2        1   3 4
EGADS    :     10     0     Yes     6     5        1   4 5
EGADS    :     11     0     Yes     1     7        1   6 8
EGADS    :     12     0     Yes     3     8        1   6 8
EGADS    :     13     0     Yes     7     8        1   6 7
EGADS    :     14     0     Yes     7     9        1   7 9
EGADS    :     15     0     Yes     8    10        1   7 9
EGADS    :     16     0     Yes     9    10        1   7 10
EGADS    :     17     0     Yes     8     7        1   8 9
EGADS    :     18     0     Yes    10     9        1   9 10
EGADS    :     19     1     Yes    12    11       NA   11 13
EGADS    :     20     1     Yes    11    13       NA   11 16
EGADS    :     21     1     Yes    14    13       NA   11 14
EGADS    :     22     1     Yes    12    14       NA   11 15
EGADS    :     23     1     Yes    16    15       NA   12 13
EGADS    :     24     1     Yes    15    17       NA   12 16
EGADS    :     25     1     Yes    18    17       NA   12 14
EGADS    :     26     1     Yes    16    18       NA   12 15
EGADS    :     27     1     Yes    12    16       NA   13 15
EGADS    :     28     1     Yes    11    15       NA   13 16
EGADS    :     29     1     Yes    14    18       NA   14 15
EGADS    :     30     1     Yes    13    17       NA   14 16

EGADS    : Node Information

EGADS    :   Node  Active      Coordinates
EGADS    :      1     Yes       97.2007855                0                0
EGADS    :      2     Yes       97.9335611                0                0
EGADS    :      3     Yes               50                0                0
EGADS    :      4     Yes       75.3047874                0                0
EGADS    :      5     Yes       123.552357                0        4.7180639
EGADS    :      6     Yes       118.391317                0       3.99272703
EGADS    :      7     Yes       97.9335611       36.1389817                0
EGADS    :      8     Yes       75.3047874       36.1389817                0
EGADS    :      9     Yes       123.552357       97.6729236        4.7180639
EGADS    :     10     Yes       118.391317       97.6729236       3.99272703
EGADS    :     11     Yes                0                0       1951.57774
EGADS    :     12     Yes                0                0                0
EGADS    :     13     Yes                0       1953.45847       1951.57774
EGADS    :     14     Yes                0       1953.45847                0
EGADS    :     15     Yes       2040.21562                0       1951.57774
EGADS    :     16     Yes       2040.21562                0                0
EGADS    :     17     Yes       2040.21562       1953.45847       1951.57774
EGADS    :     18     Yes       2040.21562       1953.45847                0

EGADS    : Face and Edge Match Information

EGADS    : No Face Matches Found

AFLR4    : Surface Mesh Spacing Setup

AFLR4    : Max Bounding Box Length     = 3906.92
AFLR4    : Min Bounding Box Length     = 3906.92
AFLR4    : Max Ref Bounding Box Length = 195.346
AFLR4    : Min Ref Bounding Box Length = 13.1976
AFLR4    : Reference Length            = 13.1976
AFLR4    : BL Thickness                = 0
AFLR4    : FarField Spacing            = 428.309
AFLR4    : Abs Min Surf Spacing        = 0.032994
AFLR4    : Min Surf Spacing            = 0.065988
AFLR4    : Max Surf Spacing            = 1.31976
AFLR4    : Global Scale Factor         = 1

AFLR4    : Geometry Definition Information

AFLR4    : Definition              Definition   Composite             Grid BC
AFLR4    :         ID                    Type          ID                Type
AFLR4    :          0     glue-only composite           -                   -
AFLR4    :          1            CAD geometry           0                 STD
AFLR4    :          2            CAD geometry           0                 STD
AFLR4    :          3            CAD geometry           0                 STD
AFLR4    :          4            CAD geometry           0                 STD
AFLR4    :          5            CAD geometry           0                 STD
AFLR4    :          6            CAD geometry           0                 STD
AFLR4    :          7            CAD geometry           0                 STD
AFLR4    :          8            CAD geometry           0                 STD
AFLR4    :          9            CAD geometry           0                 STD
AFLR4    :         10            CAD geometry           0                 STD
AFLR4    :         11            CAD geometry           0            FARFIELD
AFLR4    :         12            CAD geometry           0            FARFIELD
AFLR4    :         13            CAD geometry           0            FARFIELD
AFLR4    :         14            CAD geometry           0            FARFIELD
AFLR4    :         15            CAD geometry           0            FARFIELD
AFLR4    :         16            CAD geometry           0            FARFIELD

AFLR4    : Define CAD surface definition 1
AFLR4    : Define CAD surface definition 2
AFLR4    : Define CAD surface definition 3
AFLR4    : Define CAD surface definition 4
AFLR4    : Define CAD surface definition 5
AFLR4    : Define CAD surface definition 6
AFLR4    : Define CAD surface definition 7
AFLR4    : Define CAD surface definition 8
AFLR4    : Define CAD surface definition 9
AFLR4    : Define CAD surface definition 10
AFLR4    : Define CAD surface definition 11
AFLR4    : Define CAD surface definition 12
AFLR4    : Define CAD surface definition 13
AFLR4    : Define CAD surface definition 14
AFLR4    : Define CAD surface definition 15
AFLR4    : Define CAD surface definition 16
 
AFLR43   : INPUT SURFACE MESH FROM TESS
 
AFLR43   : Quad Surface Faces=         0
AFLR43   : Tria Surface Faces=    151706
AFLR43   : Nodes             =     75857
 
 
UG PARAM : SETTING INPUT PARAMETERS FROM ARGUMENT VECTOR
 
UG PARAM : mrecm                       = 3         
UG PARAM : mrecqm                      = 3         
UG PARAM : mpfrmt                      = 0         
 
AFLR3    : ---------------------------------------
AFLR3    : AFLR3 LIBRARY
AFLR3    : ADVANCING-FRONT/LOCAL-RECONNECTION
AFLR3    : TETRAHEDRAL GRID GENERATOR
AFLR3    : Version Number 16.32.50
AFLR3    : Version Date   10/31/23 @ 06:31PM
AFLR3    : Compile OS     Darwin 23.3.0 arm64
AFLR3    : Compile Date   02/08/24 @ 04:22PM
AFLR3    : Copyright 1994-2021, D.L. Marcum
AFLR3    : ---------------------------------------
 
AFLR3 IC : INPUT SURFACE GRID CHECK
 
AFLR3 IC : Nodes, Elements   =     75857         0

UG3      : Boundary Conditions

UG3      :  B-Face ID            Boundary Condition
UG3      :          1                         Solid
UG3      :          2                         Solid
UG3      :          3                         Solid
UG3      :          4                         Solid
UG3      :          5                         Solid
UG3      :          6                         Solid
UG3      :          7                         Solid
UG3      :          8                         Solid
UG3      :          9                         Solid
UG3      :         10                         Solid
UG3      :         11                      FarField
UG3      :         12                      FarField
UG3      :         13                      FarField
UG3      :         14                      FarField
UG3      :         15                      FarField
UG3      :         16                      FarField
 
AFLR3    : CPU Time          =     0.086   seconds
 
AFLR3 IG : INITIAL VOLUME GRID GENERATION
 
AFLR3 IG : Nodes, Elements   =     75857         0
AFLR3 IG : Nodes, Elements   =         8        10
AFLR3 IG : Nodes, Elements   =     15172    111199
AFLR3 IG : Nodes, Elements   =     30344    239871
AFLR3 IG : Nodes, Elements   =     45516    364757
AFLR3 IG : Nodes, Elements   =     60688    488029
AFLR3 IG : Nodes, Elements   =     75860    649416
AFLR3 IG : Nodes, Elements   =     75864    649502
AFLR3 IG : Nodes, Elements   =     75864    648282
AFLR3 IG : Nodes, Elements   =     75864    648415
AFLR3 IG : Nodes, Elements   =     75864    647563
AFLR3 IG : Nodes, Elements   =     75857    416423
AFLR3 IG : Nodes, Elements   =     75857    417606
AFLR3 IG : Nodes, Elements   =     75857    261925
AFLR3 IG : Nodes, Elements   =     75857    238679
 
AFLR3    : CPU Time          =     2.392   seconds
 
AFLR3 GG : ISOTROPIC VOLUME GRID GENERATION
 
AFLR3 GG : Nodes, Elements   =     75857    238679
AFLR3 GG : Nodes, Elements   =     97036    302794
AFLR3 GG : Nodes, Elements   =     97036    381323
AFLR3 GG : Nodes, Elements   =     97036    348553
AFLR3 GG : Nodes, Elements   =    114433    404125
AFLR3 GG : Nodes, Elements   =    114433    479502
AFLR3 GG : Nodes, Elements   =    114433    449390
AFLR3 GG : Nodes, Elements   =    137578    521259
AFLR3 GG : Nodes, Elements   =    137578    620175
AFLR3 GG : Nodes, Elements   =    137578    582534
AFLR3 GG : Nodes, Elements   =    137578    570299
AFLR3 GG : Nodes, Elements   =    162763    647836
AFLR3 GG : Nodes, Elements   =    162763    770341
AFLR3 GG : Nodes, Elements   =    162763    731548
AFLR3 GG : Nodes, Elements   =    190585    816203
AFLR3 GG : Nodes, Elements   =    190585    935984
AFLR3 GG : Nodes, Elements   =    190585    899107
AFLR3 GG : Nodes, Elements   =    219816    987499
AFLR3 GG : Nodes, Elements   =    219816   1108410
AFLR3 GG : Nodes, Elements   =    219816   1073232
AFLR3 GG : Nodes, Elements   =    250105   1164614
AFLR3 GG : Nodes, Elements   =    250105   1287642
AFLR3 GG : Nodes, Elements   =    250105   1252761
AFLR3 GG : Nodes, Elements   =    279892   1342494
AFLR3 GG : Nodes, Elements   =    279892   1462443
AFLR3 GG : Nodes, Elements   =    279892   1429923
AFLR3 GG : Nodes, Elements   =    309074   1517784
AFLR3 GG : Nodes, Elements   =    309074   1634324
AFLR3 GG : Nodes, Elements   =    309074   1603191
AFLR3 GG : Nodes, Elements   =    337155   1687725
AFLR3 GG : Nodes, Elements   =    337155   1799086
AFLR3 GG : Nodes, Elements   =    337155   1770201
AFLR3 GG : Nodes, Elements   =    364031   1851037
AFLR3 GG : Nodes, Elements   =    364031   1958040
AFLR3 GG : Nodes, Elements   =    364031   1929929
AFLR3 GG : Nodes, Elements   =    389893   2007694
AFLR3 GG : Nodes, Elements   =    389893   2110445
AFLR3 GG : Nodes, Elements   =    389893   2083831
AFLR3 GG : Nodes, Elements   =    414588   2158046
AFLR3 GG : Nodes, Elements   =    414588   2256223
AFLR3 GG : Nodes, Elements   =    414588   2230399
AFLR3 GG : Nodes, Elements   =    437949   2300612
AFLR3 GG : Nodes, Elements   =    437949   2392665
AFLR3 GG : Nodes, Elements   =    437949   2369220
AFLR3 GG : Nodes, Elements   =    460028   2435556
AFLR3 GG : Nodes, Elements   =    460028   2523443
AFLR3 GG : Nodes, Elements   =    460028   2500481
AFLR3 GG : Nodes, Elements   =    481028   2563562
AFLR3 GG : Nodes, Elements   =    481028   2645943
AFLR3 GG : Nodes, Elements   =    481028   2625418
AFLR3 GG : Nodes, Elements   =    500564   2684111
AFLR3 GG : Nodes, Elements   =    500564   2760869
AFLR3 GG : Nodes, Elements   =    500564   2741486
AFLR3 GG : Nodes, Elements   =    519023   2796921
AFLR3 GG : Nodes, Elements   =    519023   2869294
AFLR3 GG : Nodes, Elements   =    519023   2851235
AFLR3 GG : Nodes, Elements   =    536227   2902907
AFLR3 GG : Nodes, Elements   =    536227   2970978
AFLR3 GG : Nodes, Elements   =    536227   2953488
AFLR3 GG : Nodes, Elements   =    552417   3002099
AFLR3 GG : Nodes, Elements   =    552417   3066275
AFLR3 GG : Nodes, Elements   =    552417   3049807
AFLR3 GG : Nodes, Elements   =    567559   3095278
AFLR3 GG : Nodes, Elements   =    567559   3155304
AFLR3 GG : Nodes, Elements   =    567559   3139713
AFLR3 GG : Nodes, Elements   =    581855   3182642
AFLR3 GG : Nodes, Elements   =    581855   3239064
AFLR3 GG : Nodes, Elements   =    581855   3224765
AFLR3 GG : Nodes, Elements   =    595142   3264660
AFLR3 GG : Nodes, Elements   =    595142   3317200
AFLR3 GG : Nodes, Elements   =    595142   3303799
AFLR3 GG : Nodes, Elements   =    607536   3341007
AFLR3 GG : Nodes, Elements   =    607536   3389453
AFLR3 GG : Nodes, Elements   =    607536   3377251
AFLR3 GG : Nodes, Elements   =    619010   3411685
AFLR3 GG : Nodes, Elements   =    619010   3457021
AFLR3 GG : Nodes, Elements   =    619010   3445397
AFLR3 GG : Nodes, Elements   =    629458   3476760
AFLR3 GG : Nodes, Elements   =    629458   3517836
AFLR3 GG : Nodes, Elements   =    629458   3507282
AFLR3 GG : Nodes, Elements   =    638979   3535863
AFLR3 GG : Nodes, Elements   =    638979   3573549
AFLR3 GG : Nodes, Elements   =    638979   3563786
AFLR3 GG : Nodes, Elements   =    647722   3590028
AFLR3 GG : Nodes, Elements   =    647722   3624053
AFLR3 GG : Nodes, Elements   =    647722   3615570
AFLR3 GG : Nodes, Elements   =    655612   3639251
AFLR3 GG : Nodes, Elements   =    655612   3670585
AFLR3 GG : Nodes, Elements   =    655612   3662351
AFLR3 GG : Nodes, Elements   =    662779   3683858
AFLR3 GG : Nodes, Elements   =    662779   3712160
AFLR3 GG : Nodes, Elements   =    662779   3704757
AFLR3 GG : Nodes, Elements   =    669454   3724790
AFLR3 GG : Nodes, Elements   =    669454   3750712
AFLR3 GG : Nodes, Elements   =    669454   3744123
AFLR3 GG : Nodes, Elements   =    675397   3761956
AFLR3 GG : Nodes, Elements   =    675397   3785252
AFLR3 GG : Nodes, Elements   =    675397   3779313
AFLR3 GG : Nodes, Elements   =    680809   3795555
AFLR3 GG : Nodes, Elements   =    680809   3817005
AFLR3 GG : Nodes, Elements   =    680809   3811333
AFLR3 GG : Nodes, Elements   =    685665   3825906
AFLR3 GG : Nodes, Elements   =    685665   3844891
AFLR3 GG : Nodes, Elements   =    685665   3840070
AFLR3 GG : Nodes, Elements   =    690086   3853337
AFLR3 GG : Nodes, Elements   =    690086   3871017
AFLR3 GG : Nodes, Elements   =    690086   3866262
AFLR3 GG : Nodes, Elements   =    694035   3878112
AFLR3 GG : Nodes, Elements   =    694035   3893779
AFLR3 GG : Nodes, Elements   =    694035   3889637
AFLR3 GG : Nodes, Elements   =    697620   3900399
AFLR3 GG : Nodes, Elements   =    697620   3914441
AFLR3 GG : Nodes, Elements   =    697620   3910923
AFLR3 GG : Nodes, Elements   =    700718   3920220
AFLR3 GG : Nodes, Elements   =    700718   3932327
AFLR3 GG : Nodes, Elements   =    700718   3929172
AFLR3 GG : Nodes, Elements   =    703391   3937194
AFLR3 GG : Nodes, Elements   =    703391   3947746
AFLR3 GG : Nodes, Elements   =    703391   3944953
AFLR3 GG : Nodes, Elements   =    705696   3951869
AFLR3 GG : Nodes, Elements   =    705696   3960843
AFLR3 GG : Nodes, Elements   =    705696   3958600
AFLR3 GG : Nodes, Elements   =    707556   3964183
AFLR3 GG : Nodes, Elements   =    707556   3971425
AFLR3 GG : Nodes, Elements   =    707556   3969536
AFLR3 GG : Nodes, Elements   =    709105   3974184
AFLR3 GG : Nodes, Elements   =    709105   3980363
AFLR3 GG : Nodes, Elements   =    709105   3978685
AFLR3 GG : Nodes, Elements   =    710382   3982517
AFLR3 GG : Nodes, Elements   =    710382   3987670
AFLR3 GG : Nodes, Elements   =    710382   3986193
AFLR3 GG : Nodes, Elements   =    711500   3989547
AFLR3 GG : Nodes, Elements   =    711500   3993879
AFLR3 GG : Nodes, Elements   =    711500   3992791
AFLR3 GG : Nodes, Elements   =    712386   3995449
AFLR3 GG : Nodes, Elements   =    712386   3998928
AFLR3 GG : Nodes, Elements   =    712386   3997984
AFLR3 GG : Nodes, Elements   =    713092   4000102
AFLR3 GG : Nodes, Elements   =    713092   4002840
AFLR3 GG : Nodes, Elements   =    713092   4002110
AFLR3 GG : Nodes, Elements   =    713683   4003883
AFLR3 GG : Nodes, Elements   =    713683   4006165
AFLR3 GG : Nodes, Elements   =    713683   4005545
AFLR3 GG : Nodes, Elements   =    714102   4006803
AFLR3 GG : Nodes, Elements   =    714102   4008493
AFLR3 GG : Nodes, Elements   =    714102   4007992
AFLR3 GG : Nodes, Elements   =    714383   4008836
AFLR3 GG : Nodes, Elements   =    714383   4009992
AFLR3 GG : Nodes, Elements   =    714383   4009630
AFLR3 GG : Nodes, Elements   =    714565   4010176
AFLR3 GG : Nodes, Elements   =    714565   4010905
AFLR3 GG : Nodes, Elements   =    714565   4010667
AFLR3 GG : Nodes, Elements   =    714710   4011102
AFLR3 GG : Nodes, Elements   =    714710   4011707
AFLR3 GG : Nodes, Elements   =    714710   4011510
AFLR3 GG : Nodes, Elements   =    714817   4011832
AFLR3 GG : Nodes, Elements   =    714817   4012263
AFLR3 GG : Nodes, Elements   =    714817   4012113
AFLR3 GG : Nodes, Elements   =    714886   4012320
AFLR3 GG : Nodes, Elements   =    714886   4012623
AFLR3 GG : Nodes, Elements   =    714886   4012501
AFLR3 GG : Nodes, Elements   =    714931   4012636
AFLR3 GG : Nodes, Elements   =    714931   4012830
AFLR3 GG : Nodes, Elements   =    714931   4012764
AFLR3 GG : Nodes, Elements   =    714965   4012866
AFLR3 GG : Nodes, Elements   =    714965   4013013
AFLR3 GG : Nodes, Elements   =    714965   4012950
AFLR3 GG : Nodes, Elements   =    714994   4013037
AFLR3 GG : Nodes, Elements   =    714994   4013157
AFLR3 GG : Nodes, Elements   =    714994   4013121
AFLR3 GG : Nodes, Elements   =    715020   4013199
AFLR3 GG : Nodes, Elements   =    715020   4013311
AFLR3 GG : Nodes, Elements   =    715020   4013266
AFLR3 GG : Nodes, Elements   =    715040   4013326
AFLR3 GG : Nodes, Elements   =    715040   4013398
AFLR3 GG : Nodes, Elements   =    715040   4013378
AFLR3 GG : Nodes, Elements   =    715056   4013426
AFLR3 GG : Nodes, Elements   =    715056   4013497
AFLR3 GG : Nodes, Elements   =    715056   4013477
AFLR3 GG : Nodes, Elements   =    715069   4013516
AFLR3 GG : Nodes, Elements   =    715069   4013568
AFLR3 GG : Nodes, Elements   =    715069   4013551
AFLR3 GG : Nodes, Elements   =    715076   4013572
AFLR3 GG : Nodes, Elements   =    715076   4013609
AFLR3 GG : Nodes, Elements   =    715076   4013590
AFLR3 GG : Nodes, Elements   =    715080   4013602
AFLR3 GG : Nodes, Elements   =    715080   4013619
AFLR3 GG : Nodes, Elements   =    715080   4013611
AFLR3 GG : Nodes, Elements   =    715221   4014034
AFLR3 GG : Nodes, Elements   =    715221   4014794
AFLR3 GG : Nodes, Elements   =    715221   4014418
AFLR3 GG : Nodes, Elements   =    715295   4014640
AFLR3 GG : Nodes, Elements   =    715295   4014974
AFLR3 GG : Nodes, Elements   =    715295   4014832
AFLR3 GG : Nodes, Elements   =    715340   4014967
AFLR3 GG : Nodes, Elements   =    715340   4015216
AFLR3 GG : Nodes, Elements   =    715340   4015085
AFLR3 GG : Nodes, Elements   =    715398   4015259
AFLR3 GG : Nodes, Elements   =    715398   4015521
AFLR3 GG : Nodes, Elements   =    715398   4015431
AFLR3 GG : Nodes, Elements   =    715428   4015521
AFLR3 GG : Nodes, Elements   =    715428   4015681
AFLR3 GG : Nodes, Elements   =    715428   4015602
AFLR3 GG : Nodes, Elements   =    715441   4015641
AFLR3 GG : Nodes, Elements   =    715441   4015712
AFLR3 GG : Nodes, Elements   =    715441   4015681
AFLR3 GG : Nodes, Elements   =    715446   4015696
AFLR3 GG : Nodes, Elements   =    715446   4015717
AFLR3 GG : Nodes, Elements   =    715446   4015706
AFLR3 GG : Nodes, Elements   =    715447   4015709
AFLR3 GG : Nodes, Elements   =    715447   4015712
AFLR3 GG : Nodes, Elements   =    715447   4015710
 
AFLR3    : CPU Time          =    48.498   seconds
 
AFLR3 QI : QUALITY IMPROVEMENT
 
AFLR3 QI : Nodes, Elements   =    715447   4015710
AFLR3 QI : Nodes, Elements   =    708655   3977757
AFLR3 QI : Nodes, Elements   =    706642   3966512
AFLR3 QI : Nodes, Elements   =    706080   3963343
AFLR3 QI : Nodes, Elements   =    705965   3962681
AFLR3 QI : Nodes, Elements   =    705940   3962544
AFLR3 QI : Nodes, Elements   =    705936   3962520
AFLR3 QI : Nodes, Elements   =    705936   3980235
AFLR3 QI : Nodes, Elements   =    705936   3958971
AFLR3 QI : Nodes, Elements   =    705936   3950968
AFLR3 QI : Nodes, Elements   =    705936   3964620
AFLR3 QI : Nodes, Elements   =    705936   3950929
AFLR3 QI : Nodes, Elements   =    705936   3950401
AFLR3 QI : Nodes, Elements   =    705936   3963184
AFLR3 QI : Nodes, Elements   =    705936   3950747
AFLR3 QI : Nodes, Elements   =    705936   3950348
AFLR3 QI : Nodes, Elements   =    705936   3962853
AFLR3 QI : Nodes, Elements   =    705936   3950630
AFLR3 QI : Nodes, Elements   =    705936   3950330
AFLR3 QI : Nodes, Elements   =    705936   3962713
AFLR3 QI : Nodes, Elements   =    705936   3950584
AFLR3 QI : Nodes, Elements   =    705936   3950299
AFLR3 QI : Nodes, Elements   =    705936   3950298
AFLR3 QI : Nodes, Elements   =    705962   3950412
AFLR3 QI : Nodes, Elements   =    705962   3962907
AFLR3 QI : Nodes, Elements   =    705962   3950755
AFLR3 QI : Nodes, Elements   =    705962   3950478
AFLR3 QI : Nodes, Elements   =    705962   3962751
AFLR3 QI : Nodes, Elements   =    705962   3950718
AFLR3 QI : Nodes, Elements   =    705962   3950478
 
AFLR3    : CPU Time          =    14.906   seconds
 
AFLR3 QRG: QUALITY GRID RE-GENERATION
 
AFLR3 QRG: Nodes, Elements   =    705962   3950478
AFLR3 QRG: Nodes, Elements   =    705956   3950446
AFLR3 QRG: Nodes, Elements   =    705950   3950421
AFLR3 QRG: Nodes, Elements   =    705949   3950418
AFLR3 QRG: Nodes, Elements   =    705947   3950409
AFLR3 QRG: Nodes, Elements   =    705945   3950399
AFLR3 QRG: Nodes, Elements   =    705963   3950505
AFLR3 QRG: Nodes, Elements   =    705960   3950492
AFLR3 QRG: Nodes, Elements   =    705958   3950483
AFLR3 QRG: Nodes, Elements   =    705955   3950470
AFLR3 QRG: Nodes, Elements   =    705954   3950465
AFLR3 QRG: Nodes, Elements   =    705954   3950467
AFLR3 QRG: Nodes, Elements   =    705953   3950463
AFLR3 QRG: Nodes, Elements   =    705952   3950459
AFLR3 QRG: Nodes, Elements   =    705951   3950455
AFLR3 QRG: Nodes, Elements   =    705950   3950452
AFLR3 QRG: Nodes, Elements   =    705949   3950449
AFLR3 QRG: Nodes, Elements   =    705948   3950445
AFLR3 QRG: Nodes, Elements   =    705947   3950439
AFLR3 QRG: Nodes, Elements   =    705948   3950443
AFLR3 QRG: Nodes, Elements   =    705947   3950439
AFLR3 QRG: Nodes, Elements   =    705946   3950435
AFLR3 QRG: Nodes, Elements   =    705971   3950587
AFLR3 QRG: Nodes, Elements   =    705970   3950583
AFLR3 QRG: Nodes, Elements   =    705969   3950579
AFLR3 QRG: Nodes, Elements   =    705976   3950614
AFLR3 QRG: Nodes, Elements   =    705977   3950623
AFLR3 QRG: Nodes, Elements   =    706039   3950970
 
AFLR3    : CPU Time          =     0.354   seconds
 
AFLR3    : DONE

UG3      : DIHEDRAL ANGLE CHECK

UG3      : No. Tet Elems     =   3950970
UG3      : Min, Max Ang      =   0.00123       180
UG3      : Average Angle     =      70.2
UG3      : No. Angle&gt;160.0   =       182
UG3      : No. Angle&gt;179.9   =         8

UG3      : VOL CHECK

UG3      : Total-Volume      =  5.96e+10

UG3      : No. Tet Elems     =   3950970
UG3      : Min Vol           =   6.4e-09
UG3      : Average Vol       =  1.51e+04
UG3      : Total-Tet-Vol     =  5.96e+10
UG3      : No. Vol&lt;TOL       =         0

UG3      : Q VOL-LENGTH-RATIO CHECK
                      2/3        2
UG3      : Q = c * Vol   / sum( L  )
UG3      : 0 &lt;= Q &lt;= 1

UG3      : No. Tet Elems     =   3950970
UG3      : Min, Max Q        =  9.19e-05         1
UG3      : Average Q         =      0.86
UG3      : No. Q&lt;       0.1  =       430
UG3      : No. Q&lt;      0.01  =        10

OVERALL  : CPU Time          =     1.149   minutes

UG3      : DIHEDRAL ANGLE CHECK

UG3      : No. Tet Elems     =   3950970
UG3      : Min, Max Ang      =   0.00123       180
UG3      : Average Angle     =      70.2
UG3      : No. Angle&gt;160.0   =       182
UG3      : No. Angle&gt;179.9   =         8

UG3      : VOL CHECK

UG3      : Total-Volume      =  5.96e+10

UG3      : No. Tet Elems     =   3950970
UG3      : Min Vol           =   6.4e-09
UG3      : Average Vol       =  1.51e+04
UG3      : Total-Tet-Vol     =  5.96e+10
UG3      : No. Vol&lt;TOL       =         0

UG3      : Q VOL-LENGTH-RATIO CHECK
                      2/3        2
UG3      : Q = c * Vol   / sum( L  )
UG3      : 0 &lt;= Q &lt;= 1
UG3      : Note that L includes scaling for BL-aspect=ratio

UG3      : No. Tet Elems     =   3950970
UG3      : Min, Max Q        =  0.000257         1
UG3      : Average Q         =     0.839
UG3      : No. Q&lt;       0.1  =        25
UG3      : No. Q&lt;      0.01  =         8

UG3      : CPU Time          =     0.000   seconds

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.8.1
EGADS    : ---------------------------------------

EGADS    : CREATE EGADS TESS FROM AFLR3 DATA

EGADS    : CREATING TESSELLATION FOR BODY 0 EDGE 1
EGADS    : CREATING TESSELLATION FOR BODY 0 EDGE 2
EGADS    : CREATING TESSELLATION FOR BODY 0 EDGE 3
EGADS    : CREATING TESSELLATION FOR BODY 0 EDGE 4
EGADS    : CREATING TESSELLATION FOR BODY 0 EDGE 5
EGADS    : CREATING TESSELLATION FOR BODY 0 EDGE 6
EGADS    : CREATING TESSELLATION FOR BODY 0 EDGE 7
EGADS    : CREATING TESSELLATION FOR BODY 0 EDGE 8
EGADS    : CREATING TESSELLATION FOR BODY 0 EDGE 9
EGADS    : CREATING TESSELLATION FOR BODY 0 EDGE 10
EGADS    : CREATING TESSELLATION FOR BODY 0 EDGE 11
EGADS    : CREATING TESSELLATION FOR BODY 0 EDGE 12
EGADS    : CREATING TESSELLATION FOR BODY 0 EDGE 13
EGADS    : CREATING TESSELLATION FOR BODY 0 EDGE 14
EGADS    : CREATING TESSELLATION FOR BODY 0 EDGE 15
EGADS    : CREATING TESSELLATION FOR BODY 0 EDGE 16
EGADS    : CREATING TESSELLATION FOR BODY 0 EDGE 17
EGADS    : CREATING TESSELLATION FOR BODY 0 EDGE 18

EGADS    : CREATING TESSELLATION FOR BODY 0 FACE 1
EGADS    : CREATING TESSELLATION FOR BODY 0 FACE 2
EGADS    : CREATING TESSELLATION FOR BODY 0 FACE 3
EGADS    : CREATING TESSELLATION FOR BODY 0 FACE 4
EGADS    : CREATING TESSELLATION FOR BODY 0 FACE 5
EGADS    : CREATING TESSELLATION FOR BODY 0 FACE 6
EGADS    : CREATING TESSELLATION FOR BODY 0 FACE 7
EGADS    : CREATING TESSELLATION FOR BODY 0 FACE 8
EGADS    : CREATING TESSELLATION FOR BODY 0 FACE 9
EGADS    : CREATING TESSELLATION FOR BODY 0 FACE 10

EGADS    : CREATING TESSELLATION FOR BODY 1 EDGE 19
EGADS    : CREATING TESSELLATION FOR BODY 1 EDGE 20
EGADS    : CREATING TESSELLATION FOR BODY 1 EDGE 21
EGADS    : CREATING TESSELLATION FOR BODY 1 EDGE 22
EGADS    : CREATING TESSELLATION FOR BODY 1 EDGE 23
EGADS    : CREATING TESSELLATION FOR BODY 1 EDGE 24
EGADS    : CREATING TESSELLATION FOR BODY 1 EDGE 25
EGADS    : CREATING TESSELLATION FOR BODY 1 EDGE 26
EGADS    : CREATING TESSELLATION FOR BODY 1 EDGE 27
EGADS    : CREATING TESSELLATION FOR BODY 1 EDGE 28
EGADS    : CREATING TESSELLATION FOR BODY 1 EDGE 29
EGADS    : CREATING TESSELLATION FOR BODY 1 EDGE 30

EGADS    : CREATING TESSELLATION FOR BODY 1 FACE 11
EGADS    : CREATING TESSELLATION FOR BODY 1 FACE 12
EGADS    : CREATING TESSELLATION FOR BODY 1 FACE 13
EGADS    : CREATING TESSELLATION FOR BODY 1 FACE 14
EGADS    : CREATING TESSELLATION FOR BODY 1 FACE 15
EGADS    : CREATING TESSELLATION FOR BODY 1 FACE 16

EGADS    : EGADS TESS CREATED

EGADS    : CHECK TESS FACE NODE MAP

EGADS    : CHECKING NODE MAP FOR BODY 0 FACE 1
EGADS    : CHECKING NODE MAP FOR BODY 0 FACE 2
EGADS    : CHECKING NODE MAP FOR BODY 0 FACE 3
EGADS    : CHECKING NODE MAP FOR BODY 0 FACE 4
EGADS    : CHECKING NODE MAP FOR BODY 0 FACE 5
EGADS    : CHECKING NODE MAP FOR BODY 0 FACE 6
EGADS    : CHECKING NODE MAP FOR BODY 0 FACE 7
EGADS    : CHECKING NODE MAP FOR BODY 0 FACE 8
EGADS    : CHECKING NODE MAP FOR BODY 0 FACE 9
EGADS    : CHECKING NODE MAP FOR BODY 0 FACE 10
EGADS    : CHECKING NODE MAP FOR BODY 1 FACE 11
EGADS    : CHECKING NODE MAP FOR BODY 1 FACE 12
EGADS    : CHECKING NODE MAP FOR BODY 1 FACE 13
EGADS    : CHECKING NODE MAP FOR BODY 1 FACE 14
EGADS    : CHECKING NODE MAP FOR BODY 1 FACE 15
EGADS    : CHECKING NODE MAP FOR BODY 1 FACE 16
Volume mesh:
	Number of nodes          = 706039
	Number of elements       = 4102676
	Number of triangles      = 151706
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 3950970
	Number of pyramids       = 0
	Number of prisms         = 0
	Number of hexahedrals    = 0

Writing SU2 file ....
Finished writing SU2 file

Getting CFD boundary conditions
	Boundary condition name - Farfield
	Boundary condition name - Wing
	Done getting CFD boundary conditions
Writing SU2 data transfer files
Writing SU2 Motion File - aeroelasticIterative_motion.dat
Warning: The su2 cfg file will be overwritten!
Write SU2 configuration file for version "Harrier (8.0.1)"

==&gt; Running SU2......

-------------------------------------------------------------------------
|    ___ _   _ ___                                                      |
|   / __| | | |_  )   Release 8.0.0 "Harrier"                           |
|   \__ \ |_| |/ /                                                      |
|   |___/\___//___|   Suite (Computational Fluid Dynamics Code)         |
|                                                                       |
-------------------------------------------------------------------------
| SU2 Project Website: <a href='https://su2code.github.io'>https://su2code.github.io</a>                        |
|                                                                       |
| The SU2 Project is maintained by the SU2 Foundation                   |
| (<a href='http://su2foundation.org'>http://su2foundation.org</a>)                                            |
-------------------------------------------------------------------------
| Copyright 2012-2023, SU2 Contributors                                 |
|                                                                       |
| SU2 is free software; you can redistribute it and/or                  |
| modify it under the terms of the GNU Lesser General Public            |
| License as published by the Free Software Foundation; either          |
| version 2.1 of the License, or (at your option) any later version.    |
|                                                                       |
| SU2 is distributed in the hope that it will be useful,                |
| but WITHOUT ANY WARRANTY; without even the implied warranty of        |
| MERCHANTABILITY or FITNESS FOR A PARTICULAR PURPOSE. See the GNU      |
| Lesser General Public License for more details.                       |
|                                                                       |
| You should have received a copy of the GNU Lesser General Public      |
| License along with SU2. If not, see &lt;<a href='http://www.gnu.org/licenses/'>http://www.gnu.org/licenses/</a>&gt;.   |
-------------------------------------------------------------------------

Parsing config file for zone 0

----------------- Physical Case Definition ( Zone 0 ) -------------------
Compressible Euler equations.
Mach number: 0.294118.
Angle of attack (AoA): 0 deg, and angle of sideslip (AoS): 0 deg.
No restart solution, use the values at infinity (freestream).
Dimensional simulation.
The reference area is 4240 m^2.
The semi-span will be computed using the max y(3D) value.
The reference length is 195.346 m.
Reference origin for moment evaluation is (55.4263, 0, 0).
Surface(s) where the force coefficients are evaluated: BC_1.

Surface(s) plotted in the output file: BC_1.
Surface(s) affected by the design variables: BC_1.
Input mesh file name: ../aflr3/aflr3_CAPS.su2

--------------- Space Numerical Integration ( Zone 0 ) ------------------
Roe (with entropy fix = 0.001) solver for the flow inviscid terms.
Standard Roe without low-dissipation function.
Second order integration in space, with slope limiter.
Venkatakrishnan slope-limiting method, with constant: 0.05.
The reference element size is: 1. 
Gradient for upwind reconstruction: inverse-distance weighted Least-Squares.
Gradient for viscous and source terms: inverse-distance weighted Least-Squares.

--------------- Time Numerical Integration  ( Zone 0 ) ------------------
Local time stepping (steady state simulation).
Euler implicit method for the flow equations.
FGMRES is used for solving the linear system.
Using a ILU(0) preconditioning.
Convergence criteria of the linear solver: 1e-06.
Max number of linear iterations: 10.
V Multigrid Cycle, with 2 multigrid levels.
Damping factor for the residual restriction: 0.75.
Damping factor for the correction prolongation: 0.75.
No CFL adaptation.
+-------------------------------------------+
|  MG Level| Presmooth|PostSmooth|CorrectSmo|
+-------------------------------------------+
|         0|         1|         0|         0|
|         1|         2|         0|         0|
|         2|         3|         0|         0|
+-------------------------------------------+
Courant-Friedrichs-Lewy number:       10

------------------ Convergence Criteria  ( Zone 0 ) ---------------------
Maximum number of solver subiterations: 5.
Begin convergence monitoring at iteration 5.
Residual minimum value: 1e-14.
Cauchy series min. value: 1e-10.
Number of Cauchy elements: 100.
Begin windowed time average at iteration 0.

-------------------- Output Information ( Zone 0 ) ----------------------
File writing frequency: 
+------------------------------------+
|                     File| Frequency|
+------------------------------------+
|                  RESTART|       250|
|              SURFACE_CSV|       250|
|                  TECPLOT|       250|
|          SURFACE_TECPLOT|       250|
+------------------------------------+
Writing the convergence history file every 1 inner iterations.
Writing the screen convergence history every 1 inner iterations.
The tabular file format is CSV (.csv).
Convergence history file name: history.
Forces breakdown file name: forces_breakdown_aeroelasticIterative.dat.
Surface file name: surface_flow_aeroelasticIterative.
Volume file name: flow_aeroelasticIterative.
Restart file name: restart_flow_aeroelasticIterative.dat.

------------- Config File Boundary Information ( Zone 0 ) ---------------
+-----------------------------------------------------------------------+
|                        Marker Type|                        Marker Name|
+-----------------------------------------------------------------------+
|                         Euler wall|                               BC_1|
+-----------------------------------------------------------------------+
|                          Far-field|                               BC_2|
+-----------------------------------------------------------------------+

-------------------- Output Preprocessing ( Zone 0 ) --------------------

WARNING: SURFACE_PRESSURE_DROP can only be computed for at least 2 surfaces (outlet, inlet, ...)

Screen output fields: TIME_ITER, OUTER_ITER, INNER_ITER, CUR_TIME, TIME_STEP, WALL_TIME, RMS_DENSITY, RMS_MOMENTUM-X, RMS_MOMENTUM-Y, RMS_ENERGY, EFFICIENCY
History output group(s): ITER, TIME_DOMAIN, WALL_TIME, RMS_RES, AERO_COEFF
Convergence field(s): RMS_DENSITY
Warning: No (valid) fields chosen for time convergence monitoring. Time convergence monitoring inactive.
Volume output fields: COORDINATES, SOLUTION, PRIMITIVE

------------------- Geometry Preprocessing ( Zone 0 ) -------------------
Three dimensional problem.
706039 grid points.
3950970 volume elements.
2 surface markers.
151670 boundary elements in index 0 (Marker = BC_1).
36 boundary elements in index 1 (Marker = BC_2).
3950970 tetrahedra.
Setting point connectivity.
Renumbering points (Reverse Cuthill McKee Ordering).
Recomputing point connectivity.
Setting element connectivity.
Checking the numerical grid orientation.
All volume elements are correctly orientend.
All surface elements are correctly orientend.
Identifying edges and vertices.
Setting the control volume structure.
Volume of the computational grid: 5.96352e+10.
Searching for the closest normal neighbors to the surfaces.
Storing a mapping from global to local point index.
Compute the surface curvature.
Max K: 122.726. Mean K: 4.02932. Standard deviation K: 11.9593.
Checking for periodicity.
Computing mesh quality statistics for the dual control volumes.
+--------------------------------------------------------------+
|           Mesh Quality Metric|        Minimum|        Maximum|
+--------------------------------------------------------------+
|    Orthogonality Angle (deg.)|        12.0095|        87.3048|
|     CV Face Area Aspect Ratio|        1.03091|        15816.5|
|           CV Sub-Volume Ratio|        1.00173|         567326|
+--------------------------------------------------------------+
Setting the multigrid structure.
+-------------------------------------------+
|  MG Level|       CVs|Aggl. Rate|       CFL|
+-------------------------------------------+
|         0|    706039|    1/1.00|        10|
|         1|    116093|    1/6.08|    8.2177|
|         2|     17733|    1/6.55|   6.58922|
+-------------------------------------------+
Finding max control volume width.
Semi-span length = 97.6729 m.
Wetted area = 8795.17 m^2.
Area projection in the x-plane = 681.45 m^2, y-plane = 449.381 m^2, z-plane = 4224.13 m^2.
Max. coordinate in the x-direction = 123.552 m, y-direction = 97.6729 m, z-direction = 4.71806 m.
Min. coordinate in the x-direction = 49.9621 m, y-direction = -97.6729 m, z-direction = -8.47903 m.
Checking if Euler &amp; Symmetry markers are straight/plane:
Boundary marker BC_1 is NOT a single plane.
Computing wall distances.

-------------------- Solver Preprocessing ( Zone 0 ) --------------------
Inviscid flow: Computing density based on free-stream
temperature and pressure using the ideal gas law.
Force coefficients computed using free-stream values.

-- Models:
+------------------------------------------------------------------------------+
|          Viscosity Model|        Conductivity Model|              Fluid Model|
+------------------------------------------------------------------------------+
|                        -|                         -|             STANDARD_AIR|
+------------------------------------------------------------------------------+
-- Fluid properties:
+------------------------------------------------------------------------------+
|                  Name|    Dim. value|    Ref. value|      Unit|Non-dim. value|
+------------------------------------------------------------------------------+
|          Gas Constant|       287.058|             1|  N.m/kg.K|       287.058|
|      Spec. Heat Ratio|             -|             -|         -|           1.4|
+------------------------------------------------------------------------------+
-- Initial and free-stream conditions:
+------------------------------------------------------------------------------+
|                  Name|    Dim. value|    Ref. value|      Unit|Non-dim. value|
+------------------------------------------------------------------------------+
|       Static Pressure|        101325|             1|        Pa|        101325|
|               Density|       1.22498|             1|    kg/m^3|       1.22498|
|           Temperature|        288.15|             1|         K|        288.15|
|          Total Energy|        211798|             1|   m^2/s^2|        211798|
|            Velocity-X|       100.087|             1|       m/s|       100.087|
|            Velocity-Y|             0|             1|       m/s|             0|
|            Velocity-Z|             0|             1|       m/s|             0|
|    Velocity Magnitude|       100.087|             1|       m/s|       100.087|
+------------------------------------------------------------------------------+
|           Mach Number|             -|             -|         -|      0.294118|
+------------------------------------------------------------------------------+
Initialize Jacobian structure (Euler). MG level: 0.
Initialize Jacobian structure (Euler). MG level: 1.
Initialize Jacobian structure (Euler). MG level: 2.

------------------- Numerics Preprocessing ( Zone 0 ) -------------------

----------------- Integration Preprocessing ( Zone 0 ) ------------------

------------------- Iteration Preprocessing ( Zone 0 ) ------------------
Euler/Navier-Stokes/RANS fluid iteration.

------------------------------ Begin Solver -----------------------------

Simulation Run using the Single-zone Driver
WARNING: SU2 was not compiled for an AVX-capable architecture. Performance could be better,
         see <a href='https://su2code.github.io/docs_v7/Build-SU2-Linux-MacOS/#compiler-optimizations'>https://su2code.github.io/docs_v7/Build-SU2-Linux-MacOS/#compiler-optimizations</a>
WARNING: SU2 was not compiled for an AVX-capable architecture. Performance could be better,
         see <a href='https://su2code.github.io/docs_v7/Build-SU2-Linux-MacOS/#compiler-optimizations'>https://su2code.github.io/docs_v7/Build-SU2-Linux-MacOS/#compiler-optimizations</a>
WARNING: SU2 was not compiled for an AVX-capable architecture. Performance could be better,
         see <a href='https://su2code.github.io/docs_v7/Build-SU2-Linux-MacOS/#compiler-optimizations'>https://su2code.github.io/docs_v7/Build-SU2-Linux-MacOS/#compiler-optimizations</a>
+----------------------------------------------------------------------------------------------------------------------------------------------+
|   Time_Iter|  Outer_Iter|  Inner_Iter|    Cur_Time|   Time_Step|   Time(sec)|    rms[Rho]|   rms[RhoU]|   rms[RhoV]|   rms[RhoE]|        CEff|
+----------------------------------------------------------------------------------------------------------------------------------------------+
|           0|           0|           0|  0.0000e+00|  0.0000e+00|  1.3932e+01|    0.178549|    2.299579|    1.905942|    5.647655|   -0.745851|
|           0|           0|           1|  0.0000e+00|  0.0000e+00|  1.2556e+01|    3.053474|    5.365496|    5.299353|    8.509028|   -0.693630|
|           0|           0|           2|  0.0000e+00|  0.0000e+00|  1.1640e+01|    4.808955|    7.211019|    7.019322|   10.275785|  -30.434626|
|           0|           0|           3|  0.0000e+00|  0.0000e+00|  1.1185e+01|    6.401588|    8.954608|    8.670879|   11.829152|  -20.481769|
|           0|           0|           4|  0.0000e+00|  0.0000e+00|  1.0814e+01|    7.021661|    9.357758|    9.356548|   12.379885|    0.913660|

----------------------------- Solver Exit -------------------------------

Maximum number of iterations reached (ITER = 5) before convergence.
+-----------------------------------------------------------------------+
|      Convergence Field     |     Value    |   Criterion  |  Converged |
+-----------------------------------------------------------------------+
|                    rms[Rho]|       7.02166|         &lt; -14|          No|
+-----------------------------------------------------------------------+
-------------------------------------------------------------------------
+-----------------------------------------------------------------------+
|        File Writing Summary       |              Filename             |
+-----------------------------------------------------------------------+
|SU2 binary restart                 |restart_flow_aeroelasticIterative.dat|

Writing the forces breakdown file (forces_breakdown_aeroelasticIterative.dat).
|CSV file                           |surface_flow_aeroelasticIterative.csv|

Writing the forces breakdown file (forces_breakdown_aeroelasticIterative.dat).
|Tecplot binary                     |flow_aeroelasticIterative.szplt    |

Writing the forces breakdown file (forces_breakdown_aeroelasticIterative.dat).
|Tecplot binary surface             |surface_flow_aeroelasticIterative.szplt|

Writing the forces breakdown file (forces_breakdown_aeroelasticIterative.dat).
+-----------------------------------------------------------------------+
Warning: there are 1 non-physical points in the solution.
Warning: 9 reconstructed states for upwinding are non-physical.

--------------------------- Finalizing Solver ---------------------------
Deleted CNumerics container.
Deleted CIntegration container.
Deleted CSolver container.
Deleted CIteration container.
Deleted CInterface container.
Deleted CGeometry container.
Deleted CFreeFormDefBox class.
Deleted CSurfaceMovement class.
Deleted CVolumetricMovement class.
Deleted CConfig container.
Deleted nInst container.
Deleted COutput class.
-------------------------------------------------------------------------

------------------------- Exit Success (SU2_CFD) ------------------------


==&gt; Running SU2 post-analysis...

==&gt; Running ASTROS pre-analysis...
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 5
	Name = leftWingSkin, index = 1
	Name = wingRib, index = 2
	Name = riteWingSkin, index = 3
	Name = wingSpar1, index = 4
	Name = wingSpar2, index = 5
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 2
	Name = wingSpar1, index = 1
	Name = wingSpar2, index = 2
Getting surface mesh for body 1 (of 1)
Body 1 (of 1)
Number of nodes    = 425
Number of elements = 482
Number of triangle elements      = 0
Number of quadrilateral elements = 482
----------------------------
Total number of nodes    = 425
Total number of elements = 482
Mapping Csys attributes ................
	Number of unique Csys attributes = 2
	Name = leftWingSkin, index = 1
	Name = riteWingSkin, index = 2

Getting FEA coordinate systems.......
	Number of coordinate systems - 2
	Coordinate system name - leftWingSkin
	Coordinate system name - riteWingSkin
Mapping capsConstraint attributes ................
	Number of unique capsConstraint attributes = 1
	Name = rootConstraint, index = 1
Mapping capsLoad attributes ................
	Number of unique capsLoad attributes = 4
	Name = leftWingSkin, index = 1
	Name = riteWingSkin, index = 2
	Name = leftPointLoad, index = 3
	Name = ritePointLoad, index = 4
Mapping capsBound attributes ................
	Number of unique capsBound attributes = 4
	Name = upperWing, index = 1
	Name = lowerWing, index = 2
	Name = leftTip, index = 3
	Name = riteTip, index = 4
Mapping capsConnect attributes ................
	Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
	Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
	Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 5
	Name = leftWingSkin, index = 1
	Name = wingRib, index = 2
	Name = riteWingSkin, index = 3
	Name = wingSpar1, index = 4
	Name = wingSpar2, index = 5
Setting FEA Data
	Mesh for body = 0
	Number of nodal coordinates = 425
	Number of elements = 482
	Elemental Nodes = 0
	Elemental Rods  = 0
	Elemental Tria3 = 0
	Elemental Quad4 = 482
Aero_Reference value is NULL - No aero reference parameters set

Getting FEA materials.......
	Number of materials - 2
	Material name - Madeupium
	Material name - Unobtainium
	No "materialType" specified for Material tuple Unobtainium, defaulting to "Isotropic"
	Done getting FEA materials

Getting FEA properties.......
	Number of properties - 5
	Property name - leftWingSkin
	Property name - riteWingSkin
	Property name - wingRib
	Property name - wingSpar1
	Property name - wingSpar2
	Done getting FEA properties
Updating mesh element types based on properties input

Getting FEA constraints.......
	Number of constraints - 1
	Constraint name - rootConstraint
	No "constraintType" specified for Constraint tuple rootConstraint, defaulting to "ZeroDisplacement"
	Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults

Getting FEA loads.......
	Number of loads - 1
	Load name - pressureAero
	No "groupName" specified for Load tuple pressureAero, going to use load name
	Done getting FEA loads
Optimization Control tuple is NULL - Default optimization control is used

Getting FEA optimization control.......
Done getting FEA Optimization Control
Design_Variable tuple is NULL - No design variables applied
Design_Constraint tuple is NULL - No design constraints applied
Analysis tuple is NULL

Getting FEA analyses.......
	Number of analyses - 1
	Analysis name - Default
	Done getting FEA analyses
Reading SU2 AeroLoad File - surface_flow_aeroelasticIterative.csv
	Number of variables = 16
	Number of data points = 75837
 CAPS Info: Bound 'upperWing' Normalized Integrated 'Pressure'
            Rank 0: src = 4.015957e+12, tgt = 4.015957e+12, diff = 1.850023e+03
Reading SU2 AeroLoad File - surface_flow_aeroelasticIterative.csv
	Number of variables = 16
	Number of data points = 75837
 CAPS Info: Bound 'lowerWing' Normalized Integrated 'Pressure'
            Rank 0: src = 3.830651e+12, tgt = 3.830651e+12, diff = 1.595186e+02
Reading SU2 AeroLoad File - surface_flow_aeroelasticIterative.csv
	Number of variables = 16
	Number of data points = 75837
 CAPS Info: Bound 'leftTip' Normalized Integrated 'Pressure'
            Rank 0: src = 2.182362e+09, tgt = 2.182389e+09, diff = 2.701834e+04
Reading SU2 AeroLoad File - surface_flow_aeroelasticIterative.csv
	Number of variables = 16
	Number of data points = 75837
 CAPS Info: Bound 'riteTip' Normalized Integrated 'Pressure'
            Rank 0: src = 1.185248e+09, tgt = 1.185248e+09, diff = 1.541585e+02
Extracting external pressure loads from data transfer....
	TransferName = upperWing
	Number of Elements = 98 (total = 98)
Extracting external pressure loads from data transfer....
	TransferName = lowerWing
	Number of Elements = 98 (total = 196)
Extracting external pressure loads from data transfer....
	TransferName = leftTip
	Number of Elements = 17 (total = 213)
Extracting external pressure loads from data transfer....
	TransferName = riteTip
	Number of Elements = 17 (total = 230)

Writing Astros grid and connectivity file (in free field format) ....
Finished writing Astros grid file

Writing subElement types (if any) - appending mesh file

Writing Astros instruction file....
	Writing analysis cards
	Writing load ADD cards
	Writing constraint cards--each subcase individually
	Writing load cards
	Writing material cards
	Writing property cards
	Writing coordinate system cards

==&gt; Running mASTROS......
Note: The following floating-point exceptions are signalling: IEEE_UNDERFLOW_FLAG

==&gt; Running ASTROS post-analysis...

==&gt; Running SU2 pre-analysis...
Writing boundary flags
 - bcProps.surfaceProp[0].surfaceType = 3
 - bcProps.surfaceProp[1].surfaceType = 1
Done boundary flags
Writing SU2 data transfer files
Writing SU2 Motion File - aeroelasticIterative_motion.dat
Warning: The su2 cfg file will be overwritten!
Write SU2 configuration file for version "Harrier (8.0.1)"

==&gt; Running SU2......

-------------------------------------------------------------------------
|    ___ _   _ ___                                                      |
|   / __| | | |_  )   Release 8.0.0 "Harrier"                           |
|   \__ \ |_| |/ /                                                      |
|   |___/\___//___|   Suite (Mesh Deformation Code)                     |
|                                                                       |
-------------------------------------------------------------------------
| SU2 Project Website: <a href='https://su2code.github.io'>https://su2code.github.io</a>                        |
|                                                                       |
| The SU2 Project is maintained by the SU2 Foundation                   |
| (<a href='http://su2foundation.org'>http://su2foundation.org</a>)                                            |
-------------------------------------------------------------------------
| Copyright 2012-2023, SU2 Contributors                                 |
|                                                                       |
| SU2 is free software; you can redistribute it and/or                  |
| modify it under the terms of the GNU Lesser General Public            |
| License as published by the Free Software Foundation; either          |
| version 2.1 of the License, or (at your option) any later version.    |
|                                                                       |
| SU2 is distributed in the hope that it will be useful,                |
| but WITHOUT ANY WARRANTY; without even the implied warranty of        |
| MERCHANTABILITY or FITNESS FOR A PARTICULAR PURPOSE. See the GNU      |
| Lesser General Public License for more details.                       |
|                                                                       |
| You should have received a copy of the GNU Lesser General Public      |
| License along with SU2. If not, see &lt;<a href='http://www.gnu.org/licenses/'>http://www.gnu.org/licenses/</a>&gt;.   |
-------------------------------------------------------------------------

----------------- Physical Case Definition ( Zone 0 ) -------------------
Input mesh file name: ../aflr3/aflr3_CAPS.su2

---------------- Grid deformation parameters ( Zone 0 )  ----------------
Grid deformation using a linear elasticity method.


-------------------- Output Information ( Zone 0 ) ----------------------
Output mesh file name: ../aflr3/aflr3_CAPS.su2. 
Cell stiffness scaled by distance to nearest solid surface.

------------- Config File Boundary Information ( Zone 0 ) ---------------
+-----------------------------------------------------------------------+
|                        Marker Type|                        Marker Name|
+-----------------------------------------------------------------------+
|                         Euler wall|                               BC_1|
+-----------------------------------------------------------------------+
|                          Far-field|                               BC_2|
+-----------------------------------------------------------------------+
Three dimensional problem.
706039 grid points.
3950970 volume elements.
2 surface markers.
151670 boundary elements in index 0 (Marker = BC_1).
36 boundary elements in index 1 (Marker = BC_2).
3950970 tetrahedra.

----------------------- Preprocessing computations ----------------------
Setting local point connectivity.
Checking the numerical grid orientation of the interior elements.
All volume elements are correctly orientend.
All surface elements are correctly orientend.
Identify edges and vertices.
Setting the bound control volume structure.
Volume of the computational grid: 5.96352e+10.
  Info: Ignoring the following volume output fields/groups:
  SOLUTION
Volume output fields: COORDINATES
  Info: Ignoring the following screen output fields:
  RMS_DENSITY, RMS_MOMENTUM-X, RMS_MOMENTUM-Y, RMS_ENERGY, EFFICIENCY
Screen output fields: TIME_ITER, OUTER_ITER, INNER_ITER, CUR_TIME, TIME_STEP, WALL_TIME
  Info: Ignoring the following history output groups:
  RMS_RES, AERO_COEFF
History output group(s): ITER, TIME_DOMAIN, WALL_TIME
Warning: No (valid) fields chosen for convergence monitoring. Convergence monitoring inactive.
Warning: No (valid) fields chosen for time convergence monitoring. Time convergence monitoring inactive.

--------------------- Surface grid deformation (ZONE 0) -----------------
Performing the deformation of the surface grid.
Updating the surface coordinates from the input file.

------------------- Volumetric grid deformation (ZONE 0) ----------------
Performing the deformation of the volumetric grid.
Build timed out (after 120 minutes). Marking the build as failed.
Build was aborted
[GNU C Compiler (gcc)Clang] Skipping execution of recorder since overall result is 'FAILURE'
execute_Training.sh: line 45: 84036 Terminated: 15          $VALGRIND_COMMAND python $1
     84037                       | tee -a $LOGFILE
[WS-CLEANUP] Deleting project workspace...
[WS-CLEANUP] Skipped based on build state FAILURE
Finished: FAILURE