Started by upstream project "ESP_bPreBuilt" build number 69
originally caused by:
 Started by user galbramc
Running as galbramc
[EnvInject] - Loading node environment variables.
Building remotely on viggen 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 '2024-04-28T12:59:25.118 -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 2481

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 '2024-04-28T12:59:25.118 -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 858

No changes for svn+ssh://acdl.mit.edu/home/svnroot/OpenCSM/trunk/Jenkins since the previous build
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’
[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/jenkins16178747823331257502.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=7.6
++ OCCTREF=7.6
++ AFLR_VERSION=11.5.14
++ SU2_VERSION=8.0.0
++ TETGEN_VERSION=1.6.0
++ VSP_VERSION=3.34.0
++ export PYTHON_VERSION=3.11.9
++ PYTHON_VERSION=3.11.9
++ 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
++ [[ '' == \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
++ [[ 7.6 != '' ]]
++ [[ '' != '' ]]
++ [[ 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}";
export MANPATH="/opt/homebrew/share/man${MANPATH+:$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
++++ export MANPATH=/opt/homebrew/share/man:
++++ MANPATH=/opt/homebrew/share/man:
++++ 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_11.5.14
++ AFLR=/Users/jenkins/util/AFLR/aflr_lib_11.5.14
++ [[ 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-3.34.0-MacOS
++ VSP3_ROOT=/Users/jenkins/util/OpenVSP/OpenVSP-3.34.0-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 https://acdl.mit.edu/ESP/archive/ESPbeta-macos-arm64.tgz
--2024-04-28 12:59:33--  https://acdl.mit.edu/ESP/archive/ESPbeta-macos-arm64.tgz
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: 492152537 (469M) [application/x-gzip]
Saving to: ‘ESPbeta-macos-arm64.tgz’

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  8600K .......... .......... .......... .......... ..........  1% 17.2M 30s
  8650K .......... .......... .......... .......... ..........  1% 27.3M 30s
  8700K .......... .......... .......... .......... ..........  1% 17.1M 30s
  8750K .......... .......... .......... .......... ..........  1% 29.1M 30s
  8800K .......... .......... .......... .......... ..........  1% 27.6M 30s
  8850K .......... .......... .......... .......... ..........  1% 17.6M 30s
  8900K .......... .......... .......... .......... ..........  1% 34.1M 30s
  8950K .......... .......... .......... .......... ..........  1% 18.1M 30s
  9000K .......... .......... .......... .......... ..........  1% 29.2M 30s
  9050K .......... .......... .......... .......... ..........  1% 17.8M 30s
  9100K .......... .......... .......... .......... ..........  1% 15.2M 30s
  9150K .......... .......... .......... .......... ..........  1% 19.5M 30s
  9200K .......... .......... .......... .......... ..........  1% 31.1M 30s
  9250K .......... .......... .......... .......... ..........  1% 17.2M 30s
  9300K .......... .......... .......... .......... ..........  1% 23.7M 30s
  9350K .......... .......... .......... .......... ..........  1% 13.9M 30s
  9400K .......... .......... .......... .......... ..........  1% 19.1M 30s
  9450K .......... .......... .......... .......... ..........  1% 12.3M 30s
  9500K .......... .......... .......... .......... ..........  1% 15.7M 30s
  9550K .......... .......... .......... .......... ..........  1% 14.2M 30s
  9600K .......... .......... .......... .......... ..........  2% 11.9M 30s
  9650K .......... .......... .......... .......... ..........  2% 16.5M 30s
  9700K .......... .......... .......... .......... ..........  2% 11.3M 30s
  9750K .......... .......... .......... .......... ..........  2% 9.78M 30s
  9800K .......... .......... .......... .......... ..........  2% 11.8M 30s
  9850K .......... .......... .......... .......... ..........  2% 9.69M 30s
  9900K .......... .......... .......... .......... ..........  2% 9.07M 30s
  9950K .......... .......... .......... .......... ..........  2% 9.24M 30s
 10000K .......... .......... .......... .......... ..........  2% 10.9M 30s
 10050K .......... .......... .......... .......... ..........  2% 9.37M 30s
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 22450K .......... .......... .......... .......... ..........  4% 8.65M 36s
 22500K .......... .......... .......... .......... ..........  4% 12.6M 36s
 22550K .......... .......... .......... .......... ..........  4% 8.25M 36s
 22600K .......... .......... .......... .......... ..........  4% 7.92M 36s
 22650K .......... .......... .......... .......... ..........  4% 7.44M 36s
 22700K .......... .......... .......... .......... ..........  4% 4.33M 36s
 22750K .......... .......... .......... .......... ..........  4% 7.52M 36s
 22800K .......... .......... .......... .......... ..........  4% 6.86M 36s
 22850K .......... .......... .......... .......... ..........  4% 10.0M 36s
 22900K .......... .......... .......... .......... ..........  4% 8.45M 36s
 22950K .......... .......... .......... .......... ..........  4% 9.71M 36s
 23000K .......... .......... .......... .......... ..........  4% 11.9M 36s
 23050K .......... .......... .......... .......... ..........  4% 10.2M 36s
 23100K .......... .......... .......... .......... ..........  4% 7.35M 36s
 23150K .......... .......... .......... .......... ..........  4% 8.84M 36s
 23200K .......... .......... .......... .......... ..........  4% 6.89M 36s
 23250K .......... .......... .......... .......... ..........  4% 9.51M 36s
 23300K .......... .......... .......... .......... ..........  4% 14.1M 36s
 23350K .......... .......... .......... .......... ..........  4% 10.1M 36s
 23400K .......... .......... .......... .......... ..........  4% 12.2M 36s
 23450K .......... .......... .......... .......... ..........  4% 9.49M 36s
 23500K .......... .......... .......... .......... ..........  4% 13.1M 36s
 23550K .......... .......... .......... .......... ..........  4% 12.7M 36s
 23600K .......... .......... .......... .......... ..........  4% 9.25M 36s
 23650K .......... .......... .......... .......... ..........  4% 18.7M 36s
 23700K .......... .......... .......... .......... ..........  4% 29.4M 36s
 23750K .......... .......... .......... .......... ..........  4% 31.4M 36s
 23800K .......... .......... .......... .......... ..........  4% 23.2M 36s
 23850K .......... .......... .......... .......... ..........  4% 14.6M 36s
 23900K .......... .......... .......... .......... ..........  4% 90.3M 36s
 23950K .......... .......... .......... .......... ..........  4% 25.7M 36s
 24000K .......... .......... .......... .......... ..........  5% 33.1M 36s
 24050K .......... .......... .......... .......... ..........  5% 24.0M 36s
 24100K .......... .......... .......... .......... ..........  5% 19.0M 36s
 24150K .......... .......... .......... .......... ..........  5% 19.2M 36s
 24200K .......... .......... .......... .......... ..........  5% 14.2M 36s
 24250K .......... .......... .......... .......... ..........  5% 13.7M 36s
 24300K .......... .......... .......... .......... ..........  5% 13.7M 36s
 24350K .......... .......... .......... .......... ..........  5% 17.0M 36s
 24400K .......... .......... .......... .......... ..........  5% 13.6M 36s
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 24500K .......... .......... .......... .......... ..........  5% 14.8M 36s
 24550K .......... .......... .......... .......... ..........  5% 9.98M 36s
 24600K .......... .......... .......... .......... ..........  5% 8.52M 36s
 24650K .......... .......... .......... .......... ..........  5% 13.0M 36s
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 24750K .......... .......... .......... .......... ..........  5% 13.3M 36s
 24800K .......... .......... .......... .......... ..........  5% 8.82M 36s
 24850K .......... .......... .......... .......... ..........  5% 6.15M 36s
 24900K .......... .......... .......... .......... ..........  5% 11.8M 36s
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 25150K .......... .......... .......... .......... ..........  5% 7.23M 36s
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 25250K .......... .......... .......... .......... ..........  5% 6.23M 36s
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 25350K .......... .......... .......... .......... ..........  5% 7.59M 36s
 25400K .......... .......... .......... .......... ..........  5% 12.6M 36s
 25450K .......... .......... .......... .......... ..........  5% 34.4M 36s
 25500K .......... .......... .......... .......... ..........  5% 31.5M 36s
 25550K .......... .......... .......... .......... ..........  5% 19.0M 36s
 25600K .......... .......... .......... .......... ..........  5% 15.0M 36s
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 25700K .......... .......... .......... .......... ..........  5% 9.71M 36s
 25750K .......... .......... .......... .......... ..........  5% 13.1M 36s
 25800K .......... .......... .......... .......... ..........  5% 13.7M 36s
 25850K .......... .......... .......... .......... ..........  5% 9.06M 36s
 25900K .......... .......... .......... .......... ..........  5% 12.8M 36s
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 26050K .......... .......... .......... .......... ..........  5% 9.59M 36s
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 26150K .......... .......... .......... .......... ..........  5% 6.12M 36s
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 26700K .......... .......... .......... .......... ..........  5% 11.6M 36s
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 26800K .......... .......... .......... .......... ..........  5% 11.1M 36s
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 26900K .......... .......... .......... .......... ..........  5% 22.5M 36s
 26950K .......... .......... .......... .......... ..........  5% 11.8M 36s
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 27150K .......... .......... .......... .......... ..........  5% 11.5M 36s
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 27300K .......... .......... .......... .......... ..........  5% 8.84M 36s
 27350K .......... .......... .......... .......... ..........  5% 8.64M 36s
 27400K .......... .......... .......... .......... ..........  5% 8.60M 36s
 27450K .......... .......... .......... .......... ..........  5% 8.92M 36s
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 27550K .......... .......... .......... .......... ..........  5% 28.7M 36s
 27600K .......... .......... .......... .......... ..........  5% 16.9M 36s
 27650K .......... .......... .......... .......... ..........  5% 27.2M 36s
 27700K .......... .......... .......... .......... ..........  5% 19.1M 36s
 27750K .......... .......... .......... .......... ..........  5% 28.9M 36s
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 27900K .......... .......... .......... .......... ..........  5% 16.5M 36s
 27950K .......... .......... .......... .......... ..........  5% 27.3M 36s
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 28050K .......... .......... .......... .......... ..........  5% 18.8M 36s
 28100K .......... .......... .......... .......... ..........  5% 11.2M 36s
 28150K .......... .......... .......... .......... ..........  5% 17.9M 36s
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 28800K .......... .......... .......... .......... ..........  6% 8.83M 37s
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 29050K .......... .......... .......... .......... ..........  6% 29.2M 36s
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 29150K .......... .......... .......... .......... ..........  6% 51.4M 36s
 29200K .......... .......... .......... .......... ..........  6% 17.0M 36s
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 29300K .......... .......... .......... .......... ..........  6% 25.3M 36s
 29350K .......... .......... .......... .......... ..........  6% 17.3M 36s
 29400K .......... .......... .......... .......... ..........  6% 30.3M 36s
 29450K .......... .......... .......... .......... ..........  6% 17.5M 36s
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 29550K .......... .......... .......... .......... ..........  6% 14.6M 36s
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 29650K .......... .......... .......... .......... ..........  6% 15.8M 36s
 29700K .......... .......... .......... .......... ..........  6% 10.8M 36s
 29750K .......... .......... .......... .......... ..........  6% 17.0M 36s
 29800K .......... .......... .......... .......... ..........  6% 14.5M 36s
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 30000K .......... .......... .......... .......... ..........  6% 8.93M 36s
 30050K .......... .......... .......... .......... ..........  6% 15.1M 36s
 30100K .......... .......... .......... .......... ..........  6% 11.1M 36s
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 30300K .......... .......... .......... .......... ..........  6% 13.1M 36s
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 30400K .......... .......... .......... .......... ..........  6% 9.29M 36s
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 30600K .......... .......... .......... .......... ..........  6% 9.46M 36s
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 30700K .......... .......... .......... .......... ..........  6% 7.75M 36s
 30750K .......... .......... .......... .......... ..........  6% 8.84M 36s
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 30900K .......... .......... .......... .......... ..........  6% 24.5M 36s
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 32150K .......... .......... .......... .......... ..........  6% 13.5M 36s
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 32250K .......... .......... .......... .......... ..........  6% 16.4M 36s
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 35150K .......... .......... .......... .......... ..........  7% 11.8M 36s
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 36450K .......... .......... .......... .......... ..........  7% 7.20M 37s
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 50550K .......... .......... .......... .......... .......... 10% 10.8M 36s
 50600K .......... .......... .......... .......... .......... 10% 7.41M 37s
 50650K .......... .......... .......... .......... .......... 10% 9.24M 37s
 50700K .......... .......... .......... .......... .......... 10% 6.41M 37s
 50750K .......... .......... .......... .......... .......... 10% 8.30M 37s
 50800K .......... .......... .......... .......... .......... 10% 9.05M 37s
 50850K .......... .......... .......... .......... .......... 10% 15.8M 37s
 50900K .......... .......... .......... .......... .......... 10% 23.4M 37s
 50950K .......... .......... .......... .......... .......... 10% 10.3M 37s
 51000K .......... .......... .......... .......... .......... 10% 15.7M 37s
 51050K .......... .......... .......... .......... .......... 10% 16.0M 36s
 51100K .......... .......... .......... .......... .......... 10% 11.1M 36s
 51150K .......... .......... .......... .......... .......... 10% 13.5M 36s
 51200K .......... .......... .......... .......... .......... 10% 10.2M 36s
 51250K .......... .......... .......... .......... .......... 10% 9.54M 36s
 51300K .......... .......... .......... .......... .......... 10% 11.2M 36s
 51350K .......... .......... .......... .......... .......... 10% 11.6M 36s
 51400K .......... .......... .......... .......... .......... 10% 12.2M 36s
 51450K .......... .......... .......... .......... .......... 10% 8.81M 36s
 51500K .......... .......... .......... .......... .......... 10% 11.5M 36s
 51550K .......... .......... .......... .......... .......... 10% 11.4M 36s
 51600K .......... .......... .......... .......... .......... 10% 6.65M 36s
 51650K .......... .......... .......... .......... .......... 10% 7.16M 37s
 51700K .......... .......... .......... .......... .......... 10% 5.02M 37s
 51750K .......... .......... .......... .......... .......... 10% 10.3M 37s
 51800K .......... .......... .......... .......... .......... 10% 9.94M 37s
 51850K .......... .......... .......... .......... .......... 10% 7.43M 37s
 51900K .......... .......... .......... .......... .......... 10% 9.23M 37s
 51950K .......... .......... .......... .......... .......... 10% 7.57M 37s
 52000K .......... .......... .......... .......... .......... 10% 8.67M 37s
 52050K .......... .......... .......... .......... .......... 10% 11.5M 37s
 52100K .......... .......... .......... .......... .......... 10% 9.35M 37s
 52150K .......... .......... .......... .......... .......... 10% 12.2M 37s
 52200K .......... .......... .......... .......... .......... 10% 9.34M 37s
 52250K .......... .......... .......... .......... .......... 10% 14.0M 37s
 52300K .......... .......... .......... .......... .......... 10% 10.1M 37s
 52350K .......... .......... .......... .......... .......... 10% 5.34M 37s
 52400K .......... .......... .......... .......... .......... 10% 9.44M 37s
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 52500K .......... .......... .......... .......... .......... 10% 14.5M 37s
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 52600K .......... .......... .......... .......... .......... 10% 9.38M 37s
 52650K .......... .......... .......... .......... .......... 10% 12.1M 37s
 52700K .......... .......... .......... .......... .......... 10% 7.48M 37s
 52750K .......... .......... .......... .......... .......... 10% 6.68M 37s
 52800K .......... .......... .......... .......... .......... 10% 6.56M 37s
 52850K .......... .......... .......... .......... .......... 11% 5.52M 37s
 52900K .......... .......... .......... .......... .......... 11% 5.99M 37s
 52950K .......... .......... .......... .......... .......... 11% 9.31M 37s
 53000K .......... .......... .......... .......... .......... 11% 19.4M 37s
 53050K .......... .......... .......... .......... .......... 11% 25.2M 37s
 53100K .......... .......... .......... .......... .......... 11% 12.4M 37s
 53150K .......... .......... .......... .......... .......... 11% 13.1M 37s
 53200K .......... .......... .......... .......... .......... 11% 12.4M 37s
 53250K .......... .......... .......... .......... .......... 11% 12.4M 37s
 53300K .......... .......... .......... .......... .......... 11% 14.6M 37s
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 53400K .......... .......... .......... .......... .......... 11% 13.9M 37s
 53450K .......... .......... .......... .......... .......... 11% 11.9M 37s
 53500K .......... .......... .......... .......... .......... 11% 15.2M 37s
 53550K .......... .......... .......... .......... .......... 11% 12.7M 37s
 53600K .......... .......... .......... .......... .......... 11% 14.6M 37s
 53650K .......... .......... .......... .......... .......... 11% 35.0M 37s
 53700K .......... .......... .......... .......... .......... 11% 37.0M 37s
 53750K .......... .......... .......... .......... .......... 11% 24.9M 36s
 53800K .......... .......... .......... .......... .......... 11% 33.4M 36s
 53850K .......... .......... .......... .......... .......... 11% 34.2M 36s
 53900K .......... .......... .......... .......... .......... 11% 29.5M 36s
 53950K .......... .......... .......... .......... .......... 11% 13.7M 36s
 54000K .......... .......... .......... .......... .......... 11% 26.9M 36s
 54050K .......... .......... .......... .......... .......... 11% 21.9M 36s
 54100K .......... .......... .......... .......... .......... 11% 15.7M 36s
 54150K .......... .......... .......... .......... .......... 11% 14.2M 36s
 54200K .......... .......... .......... .......... .......... 11% 11.3M 36s
 54250K .......... .......... .......... .......... .......... 11% 13.6M 36s
 54300K .......... .......... .......... .......... .......... 11% 13.8M 36s
 54350K .......... .......... .......... .......... .......... 11% 10.2M 36s
 54400K .......... .......... .......... .......... .......... 11% 15.7M 36s
 54450K .......... .......... .......... .......... .......... 11% 10.6M 36s
 54500K .......... .......... .......... .......... .......... 11% 13.2M 36s
 54550K .......... .......... .......... .......... .......... 11% 17.0M 36s
 54600K .......... .......... .......... .......... .......... 11% 19.7M 36s
 54650K .......... .......... .......... .......... .......... 11% 24.2M 36s
 54700K .......... .......... .......... .......... .......... 11% 19.3M 36s
 54750K .......... .......... .......... .......... .......... 11% 10.8M 36s
 54800K .......... .......... .......... .......... .......... 11% 24.0M 36s
 54850K .......... .......... .......... .......... .......... 11% 13.9M 36s
 54900K .......... .......... .......... .......... .......... 11% 15.0M 36s
 54950K .......... .......... .......... .......... .......... 11% 13.1M 36s
 55000K .......... .......... .......... .......... .......... 11% 12.2M 36s
 55050K .......... .......... .......... .......... .......... 11% 14.1M 36s
 55100K .......... .......... .......... .......... .......... 11% 11.8M 36s
 55150K .......... .......... .......... .......... .......... 11% 11.1M 36s
 55200K .......... .......... .......... .......... .......... 11% 11.7M 36s
 55250K .......... .......... .......... .......... .......... 11% 17.4M 36s
 55300K .......... .......... .......... .......... .......... 11% 14.7M 36s
 55350K .......... .......... .......... .......... .......... 11% 10.6M 36s
 55400K .......... .......... .......... .......... .......... 11% 12.7M 36s
 55450K .......... .......... .......... .......... .......... 11% 12.8M 36s
 55500K .......... .......... .......... .......... .......... 11% 12.1M 36s
 55550K .......... .......... .......... .......... .......... 11% 10.2M 36s
 55600K .......... .......... .......... .......... .......... 11% 15.1M 36s
 55650K .......... .......... .......... .......... .......... 11% 15.1M 36s
 55700K .......... .......... .......... .......... .......... 11% 18.9M 36s
 55750K .......... .......... .......... .......... .......... 11% 85.7M 36s
 55800K .......... .......... .......... .......... .......... 11% 41.5M 36s
 55850K .......... .......... .......... .......... .......... 11% 37.5M 36s
 55900K .......... .......... .......... .......... .......... 11% 23.0M 36s
 55950K .......... .......... .......... .......... .......... 11% 54.3M 36s
 56000K .......... .......... .......... .......... .......... 11% 31.4M 36s
 56050K .......... .......... .......... .......... .......... 11% 29.5M 36s
 56100K .......... .......... .......... .......... .......... 11% 19.4M 36s
 56150K .......... .......... .......... .......... .......... 11% 20.5M 36s
 56200K .......... .......... .......... .......... .......... 11% 14.4M 36s
 56250K .......... .......... .......... .......... .......... 11% 16.6M 36s
 56300K .......... .......... .......... .......... .......... 11% 14.4M 36s
 56350K .......... .......... .......... .......... .......... 11% 13.6M 36s
 56400K .......... .......... .......... .......... .......... 11% 15.2M 36s
 56450K .......... .......... .......... .......... .......... 11% 11.5M 36s
 56500K .......... .......... .......... .......... .......... 11% 6.99M 36s
 56550K .......... .......... .......... .......... .......... 11% 8.41M 36s
 56600K .......... .......... .......... .......... .......... 11% 6.09M 36s
 56650K .......... .......... .......... .......... .......... 11% 9.21M 36s
 56700K .......... .......... .......... .......... .......... 11% 6.48M 36s
 56750K .......... .......... .......... .......... .......... 11% 9.89M 36s
 56800K .......... .......... .......... .......... .......... 11% 8.23M 36s
 56850K .......... .......... .......... .......... .......... 11% 7.02M 36s
 56900K .......... .......... .......... .......... .......... 11% 7.75M 36s
 56950K .......... .......... .......... .......... .......... 11% 6.44M 36s
 57000K .......... .......... .......... .......... .......... 11% 12.3M 36s
 57050K .......... .......... .......... .......... .......... 11% 10.7M 36s
 57100K .......... .......... .......... .......... .......... 11% 9.69M 36s
 57150K .......... .......... .......... .......... .......... 11% 8.64M 36s
 57200K .......... .......... .......... .......... .......... 11% 7.89M 36s
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 57300K .......... .......... .......... .......... .......... 11% 8.46M 36s
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 57400K .......... .......... .......... .......... .......... 11% 8.17M 36s
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 57500K .......... .......... .......... .......... .......... 11% 18.1M 36s
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 57900K .......... .......... .......... .......... .......... 12% 15.1M 36s
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 58050K .......... .......... .......... .......... .......... 12% 10.8M 36s
 58100K .......... .......... .......... .......... .......... 12% 8.64M 36s
 58150K .......... .......... .......... .......... .......... 12% 11.4M 36s
 58200K .......... .......... .......... .......... .......... 12% 9.21M 36s
 58250K .......... .......... .......... .......... .......... 12% 10.0M 36s
 58300K .......... .......... .......... .......... .......... 12% 9.46M 36s
 58350K .......... .......... .......... .......... .......... 12% 7.32M 36s
 58400K .......... .......... .......... .......... .......... 12% 6.93M 36s
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 58750K .......... .......... .......... .......... .......... 12% 10.4M 36s
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 59250K .......... .......... .......... .......... .......... 12% 11.3M 36s
 59300K .......... .......... .......... .......... .......... 12% 10.1M 36s
 59350K .......... .......... .......... .......... .......... 12% 9.75M 36s
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 59600K .......... .......... .......... .......... .......... 12% 9.89M 36s
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 59700K .......... .......... .......... .......... .......... 12% 10.3M 36s
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 59800K .......... .......... .......... .......... .......... 12% 8.04M 36s
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 61050K .......... .......... .......... .......... .......... 12% 58.1M 36s
 61100K .......... .......... .......... .......... .......... 12% 33.6M 36s
 61150K .......... .......... .......... .......... .......... 12% 46.2M 36s
 61200K .......... .......... .......... .......... .......... 12% 27.3M 36s
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 61500K .......... .......... .......... .......... .......... 12% 23.9M 36s
 61550K .......... .......... .......... .......... .......... 12% 60.9M 36s
 61600K .......... .......... .......... .......... .......... 12% 19.8M 36s
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 61800K .......... .......... .......... .......... .......... 12% 17.1M 36s
 61850K .......... .......... .......... .......... .......... 12% 12.6M 36s
 61900K .......... .......... .......... .......... .......... 12% 14.6M 36s
 61950K .......... .......... .......... .......... .......... 12% 13.1M 36s
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 62100K .......... .......... .......... .......... .......... 12% 9.96M 36s
 62150K .......... .......... .......... .......... .......... 12% 12.3M 36s
 62200K .......... .......... .......... .......... .......... 12% 15.0M 36s
 62250K .......... .......... .......... .......... .......... 12% 28.0M 35s
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 62550K .......... .......... .......... .......... .......... 13% 85.5M 35s
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 62800K .......... .......... .......... .......... .......... 13% 21.3M 35s
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 63100K .......... .......... .......... .......... .......... 13% 8.41M 35s
 63150K .......... .......... .......... .......... .......... 13% 16.0M 35s
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 64100K .......... .......... .......... .......... .......... 13% 18.6M 35s
 64150K .......... .......... .......... .......... .......... 13% 38.3M 35s
 64200K .......... .......... .......... .......... .......... 13% 22.3M 35s
 64250K .......... .......... .......... .......... .......... 13% 29.1M 35s
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 92250K .......... .......... .......... .......... .......... 19% 6.63M 34s
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 93300K .......... .......... .......... .......... .......... 19% 9.97M 34s
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100000K .......... .......... .......... .......... .......... 20% 11.9M 34s
100050K .......... .......... .......... .......... .......... 20% 5.78M 34s
100100K .......... .......... .......... .......... .......... 20% 8.48M 34s
100150K .......... .......... .......... .......... .......... 20% 9.25M 34s
100200K .......... .......... .......... .......... .......... 20% 9.05M 34s
100250K .......... .......... .......... .......... .......... 20% 9.30M 34s
100300K .......... .......... .......... .......... .......... 20% 8.32M 34s
100350K .......... .......... .......... .......... .......... 20% 8.85M 34s
100400K .......... .......... .......... .......... .......... 20% 16.3M 34s
100450K .......... .......... .......... .......... .......... 20% 21.2M 34s
100500K .......... .......... .......... .......... .......... 20% 28.9M 34s
100550K .......... .......... .......... .......... .......... 20% 14.6M 34s
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100650K .......... .......... .......... .......... .......... 20% 19.5M 33s
100700K .......... .......... .......... .......... .......... 20% 18.9M 33s
100750K .......... .......... .......... .......... .......... 20% 23.1M 33s
100800K .......... .......... .......... .......... .......... 20% 17.7M 33s
100850K .......... .......... .......... .......... .......... 20% 10.6M 33s
100900K .......... .......... .......... .......... .......... 21% 19.7M 33s
100950K .......... .......... .......... .......... .......... 21% 15.2M 33s
101000K .......... .......... .......... .......... .......... 21% 12.5M 33s
101050K .......... .......... .......... .......... .......... 21% 10.1M 33s
101100K .......... .......... .......... .......... .......... 21% 13.9M 33s
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101200K .......... .......... .......... .......... .......... 21% 10.8M 33s
101250K .......... .......... .......... .......... .......... 21% 14.8M 33s
101300K .......... .......... .......... .......... .......... 21% 15.7M 33s
101350K .......... .......... .......... .......... .......... 21% 10.5M 33s
101400K .......... .......... .......... .......... .......... 21% 14.1M 33s
101450K .......... .......... .......... .......... .......... 21% 12.8M 33s
101500K .......... .......... .......... .......... .......... 21% 14.4M 33s
101550K .......... .......... .......... .......... .......... 21% 14.6M 33s
101600K .......... .......... .......... .......... .......... 21% 12.4M 33s
101650K .......... .......... .......... .......... .......... 21% 7.69M 33s
101700K .......... .......... .......... .......... .......... 21% 4.88M 33s
101750K .......... .......... .......... .......... .......... 21% 7.58M 33s
101800K .......... .......... .......... .......... .......... 21% 9.48M 33s
101850K .......... .......... .......... .......... .......... 21% 7.03M 33s
101900K .......... .......... .......... .......... .......... 21% 11.3M 33s
101950K .......... .......... .......... .......... .......... 21% 8.65M 33s
102000K .......... .......... .......... .......... .......... 21% 6.88M 33s
102050K .......... .......... .......... .......... .......... 21% 15.5M 33s
102100K .......... .......... .......... .......... .......... 21% 11.7M 33s
102150K .......... .......... .......... .......... .......... 21% 15.2M 33s
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102250K .......... .......... .......... .......... .......... 21% 11.5M 33s
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102400K .......... .......... .......... .......... .......... 21% 10.8M 33s
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102500K .......... .......... .......... .......... .......... 21% 8.79M 33s
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102800K .......... .......... .......... .......... .......... 21% 8.41M 33s
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103100K .......... .......... .......... .......... .......... 21% 17.7M 33s
103150K .......... .......... .......... .......... .......... 21% 14.7M 33s
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103700K .......... .......... .......... .......... .......... 21% 7.17M 33s
103750K .......... .......... .......... .......... .......... 21% 11.7M 33s
103800K .......... .......... .......... .......... .......... 21% 8.41M 33s
103850K .......... .......... .......... .......... .......... 21% 6.81M 33s
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104000K .......... .......... .......... .......... .......... 21% 9.70M 33s
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104100K .......... .......... .......... .......... .......... 21% 23.6M 33s
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105000K .......... .......... .......... .......... .......... 21% 8.10M 33s
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105100K .......... .......... .......... .......... .......... 21% 4.70M 33s
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105200K .......... .......... .......... .......... .......... 21% 22.5M 33s
105250K .......... .......... .......... .......... .......... 21% 14.6M 33s
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105350K .......... .......... .......... .......... .......... 21% 8.49M 33s
105400K .......... .......... .......... .......... .......... 21% 16.4M 33s
105450K .......... .......... .......... .......... .......... 21% 13.2M 33s
105500K .......... .......... .......... .......... .......... 21% 14.4M 33s
105550K .......... .......... .......... .......... .......... 21% 11.0M 33s
105600K .......... .......... .......... .......... .......... 21% 14.0M 33s
105650K .......... .......... .......... .......... .......... 21% 12.7M 33s
105700K .......... .......... .......... .......... .......... 22% 11.8M 33s
105750K .......... .......... .......... .......... .......... 22% 12.9M 33s
105800K .......... .......... .......... .......... .......... 22% 12.6M 33s
105850K .......... .......... .......... .......... .......... 22% 13.4M 33s
105900K .......... .......... .......... .......... .......... 22% 21.5M 33s
105950K .......... .......... .......... .......... .......... 22% 18.2M 33s
106000K .......... .......... .......... .......... .......... 22% 7.31M 33s
106050K .......... .......... .......... .......... .......... 22% 6.32M 33s
106100K .......... .......... .......... .......... .......... 22% 5.48M 33s
106150K .......... .......... .......... .......... .......... 22% 5.78M 33s
106200K .......... .......... .......... .......... .......... 22% 5.17M 33s
106250K .......... .......... .......... .......... .......... 22% 11.5M 33s
106300K .......... .......... .......... .......... .......... 22% 12.8M 33s
106350K .......... .......... .......... .......... .......... 22% 9.68M 33s
106400K .......... .......... .......... .......... .......... 22% 11.1M 33s
106450K .......... .......... .......... .......... .......... 22% 6.42M 33s
106500K .......... .......... .......... .......... .......... 22% 8.99M 33s
106550K .......... .......... .......... .......... .......... 22% 9.25M 33s
106600K .......... .......... .......... .......... .......... 22% 5.88M 33s
106650K .......... .......... .......... .......... .......... 22% 7.54M 33s
106700K .......... .......... .......... .......... .......... 22% 10.2M 33s
106750K .......... .......... .......... .......... .......... 22% 8.82M 33s
106800K .......... .......... .......... .......... .......... 22% 7.32M 33s
106850K .......... .......... .......... .......... .......... 22% 6.06M 33s
106900K .......... .......... .......... .......... .......... 22% 6.41M 33s
106950K .......... .......... .......... .......... .......... 22% 5.69M 33s
107000K .......... .......... .......... .......... .......... 22% 7.80M 33s
107050K .......... .......... .......... .......... .......... 22% 9.63M 33s
107100K .......... .......... .......... .......... .......... 22% 9.46M 33s
107150K .......... .......... .......... .......... .......... 22% 6.10M 33s
107200K .......... .......... .......... .......... .......... 22% 8.42M 33s
107250K .......... .......... .......... .......... .......... 22% 9.52M 33s
107300K .......... .......... .......... .......... .......... 22% 11.1M 33s
107350K .......... .......... .......... .......... .......... 22% 6.96M 33s
107400K .......... .......... .......... .......... .......... 22% 8.70M 33s
107450K .......... .......... .......... .......... .......... 22% 6.95M 33s
107500K .......... .......... .......... .......... .......... 22% 12.3M 33s
107550K .......... .......... .......... .......... .......... 22% 59.7M 33s
107600K .......... .......... .......... .......... .......... 22% 18.0M 33s
107650K .......... .......... .......... .......... .......... 22% 15.0M 33s
107700K .......... .......... .......... .......... .......... 22% 11.8M 33s
107750K .......... .......... .......... .......... .......... 22% 12.6M 33s
107800K .......... .......... .......... .......... .......... 22% 15.1M 33s
107850K .......... .......... .......... .......... .......... 22% 11.5M 33s
107900K .......... .......... .......... .......... .......... 22% 9.93M 33s
107950K .......... .......... .......... .......... .......... 22% 12.8M 33s
108000K .......... .......... .......... .......... .......... 22% 9.43M 33s
108050K .......... .......... .......... .......... .......... 22% 9.14M 33s
108100K .......... .......... .......... .......... .......... 22% 10.9M 33s
108150K .......... .......... .......... .......... .......... 22% 18.5M 33s
108200K .......... .......... .......... .......... .......... 22% 7.74M 33s
108250K .......... .......... .......... .......... .......... 22% 9.15M 33s
108300K .......... .......... .......... .......... .......... 22% 7.75M 33s
108350K .......... .......... .......... .......... .......... 22% 7.20M 33s
108400K .......... .......... .......... .......... .......... 22% 7.62M 33s
108450K .......... .......... .......... .......... .......... 22% 6.94M 33s
108500K .......... .......... .......... .......... .......... 22% 11.4M 33s
108550K .......... .......... .......... .......... .......... 22% 31.6M 33s
108600K .......... .......... .......... .......... .......... 22% 19.4M 33s
108650K .......... .......... .......... .......... .......... 22% 17.7M 33s
108700K .......... .......... .......... .......... .......... 22% 28.1M 33s
108750K .......... .......... .......... .......... .......... 22% 18.5M 33s
108800K .......... .......... .......... .......... .......... 22% 26.8M 33s
108850K .......... .......... .......... .......... .......... 22% 17.3M 33s
108900K .......... .......... .......... .......... .......... 22% 13.5M 33s
108950K .......... .......... .......... .......... .......... 22% 41.3M 33s
109000K .......... .......... .......... .......... .......... 22% 15.8M 33s
109050K .......... .......... .......... .......... .......... 22% 16.3M 33s
109100K .......... .......... .......... .......... .......... 22% 13.0M 33s
109150K .......... .......... .......... .......... .......... 22% 16.4M 33s
109200K .......... .......... .......... .......... .......... 22% 11.2M 33s
109250K .......... .......... .......... .......... .......... 22% 14.5M 33s
109300K .......... .......... .......... .......... .......... 22% 12.3M 33s
109350K .......... .......... .......... .......... .......... 22% 10.8M 33s
109400K .......... .......... .......... .......... .......... 22% 12.4M 33s
109450K .......... .......... .......... .......... .......... 22% 10.0M 33s
109500K .......... .......... .......... .......... .......... 22% 11.7M 33s
109550K .......... .......... .......... .......... .......... 22% 14.9M 33s
109600K .......... .......... .......... .......... .......... 22% 12.1M 33s
109650K .......... .......... .......... .......... .......... 22% 12.8M 33s
109700K .......... .......... .......... .......... .......... 22% 10.6M 33s
109750K .......... .......... .......... .......... .......... 22% 12.3M 33s
109800K .......... .......... .......... .......... .......... 22% 12.1M 33s
109850K .......... .......... .......... .......... .......... 22% 7.77M 33s
109900K .......... .......... .......... .......... .......... 22% 6.33M 33s
109950K .......... .......... .......... .......... .......... 22% 5.86M 33s
110000K .......... .......... .......... .......... .......... 22% 9.92M 33s
110050K .......... .......... .......... .......... .......... 22% 11.7M 33s
110100K .......... .......... .......... .......... .......... 22% 7.89M 33s
110150K .......... .......... .......... .......... .......... 22% 16.3M 33s
110200K .......... .......... .......... .......... .......... 22% 11.4M 33s
110250K .......... .......... .......... .......... .......... 22% 14.4M 33s
110300K .......... .......... .......... .......... .......... 22% 13.2M 33s
110350K .......... .......... .......... .......... .......... 22% 10.5M 33s
110400K .......... .......... .......... .......... .......... 22% 12.7M 33s
110450K .......... .......... .......... .......... .......... 22% 13.7M 33s
110500K .......... .......... .......... .......... .......... 23% 12.3M 33s
110550K .......... .......... .......... .......... .......... 23% 10.1M 33s
110600K .......... .......... .......... .......... .......... 23% 11.7M 33s
110650K .......... .......... .......... .......... .......... 23% 15.9M 33s
110700K .......... .......... .......... .......... .......... 23% 14.8M 33s
110750K .......... .......... .......... .......... .......... 23% 15.2M 33s
110800K .......... .......... .......... .......... .......... 23% 13.6M 33s
110850K .......... .......... .......... .......... .......... 23% 15.2M 33s
110900K .......... .......... .......... .......... .......... 23% 14.4M 33s
110950K .......... .......... .......... .......... .......... 23% 12.7M 33s
111000K .......... .......... .......... .......... .......... 23% 11.9M 33s
111050K .......... .......... .......... .......... .......... 23% 12.0M 33s
111100K .......... .......... .......... .......... .......... 23% 12.5M 33s
111150K .......... .......... .......... .......... .......... 23% 23.6M 33s
111200K .......... .......... .......... .......... .......... 23% 29.2M 33s
111250K .......... .......... .......... .......... .......... 23% 23.1M 33s
111300K .......... .......... .......... .......... .......... 23% 81.4M 33s
111350K .......... .......... .......... .......... .......... 23% 30.4M 33s
111400K .......... .......... .......... .......... .......... 23% 53.7M 33s
111450K .......... .......... .......... .......... .......... 23% 33.3M 33s
111500K .......... .......... .......... .......... .......... 23% 24.7M 33s
111550K .......... .......... .......... .......... .......... 23% 18.1M 33s
111600K .......... .......... .......... .......... .......... 23% 14.6M 33s
111650K .......... .......... .......... .......... .......... 23% 26.4M 33s
111700K .......... .......... .......... .......... .......... 23% 16.8M 33s
111750K .......... .......... .......... .......... .......... 23% 18.1M 33s
111800K .......... .......... .......... .......... .......... 23% 16.2M 33s
111850K .......... .......... .......... .......... .......... 23% 18.3M 33s
111900K .......... .......... .......... .......... .......... 23% 17.5M 33s
111950K .......... .......... .......... .......... .......... 23% 17.5M 33s
112000K .......... .......... .......... .......... .......... 23% 25.6M 33s
112050K .......... .......... .......... .......... .......... 23% 18.3M 33s
112100K .......... .......... .......... .......... .......... 23% 14.3M 33s
112150K .......... .......... .......... .......... .......... 23% 16.0M 33s
112200K .......... .......... .......... .......... .......... 23% 12.6M 33s
112250K .......... .......... .......... .......... .......... 23% 11.4M 33s
112300K .......... .......... .......... .......... .......... 23% 8.10M 33s
112350K .......... .......... .......... .......... .......... 23% 7.06M 33s
112400K .......... .......... .......... .......... .......... 23% 7.47M 33s
112450K .......... .......... .......... .......... .......... 23% 6.93M 33s
112500K .......... .......... .......... .......... .......... 23% 5.99M 33s
112550K .......... .......... .......... .......... .......... 23% 5.70M 33s
112600K .......... .......... .......... .......... .......... 23% 4.91M 33s
112650K .......... .......... .......... .......... .......... 23% 5.23M 33s
112700K .......... .......... .......... .......... .......... 23% 8.29M 33s
112750K .......... .......... .......... .......... .......... 23% 8.12M 33s
112800K .......... .......... .......... .......... .......... 23% 7.51M 33s
112850K .......... .......... .......... .......... .......... 23% 7.07M 33s
112900K .......... .......... .......... .......... .......... 23% 7.49M 33s
112950K .......... .......... .......... .......... .......... 23% 5.79M 33s
113000K .......... .......... .......... .......... .......... 23% 8.07M 33s
113050K .......... .......... .......... .......... .......... 23% 8.80M 33s
113100K .......... .......... .......... .......... .......... 23% 7.96M 33s
113150K .......... .......... .......... .......... .......... 23% 9.99M 33s
113200K .......... .......... .......... .......... .......... 23% 7.24M 33s
113250K .......... .......... .......... .......... .......... 23% 7.14M 33s
113300K .......... .......... .......... .......... .......... 23% 9.61M 33s
113350K .......... .......... .......... .......... .......... 23% 6.11M 33s
113400K .......... .......... .......... .......... .......... 23% 4.88M 33s
113450K .......... .......... .......... .......... .......... 23% 5.49M 33s
113500K .......... .......... .......... .......... .......... 23% 4.08M 33s
113550K .......... .......... .......... .......... .......... 23% 5.84M 33s
113600K .......... .......... .......... .......... .......... 23% 6.23M 33s
113650K .......... .......... .......... .......... .......... 23% 6.36M 33s
113700K .......... .......... .......... .......... .......... 23% 7.55M 33s
113750K .......... .......... .......... .......... .......... 23% 9.89M 33s
113800K .......... .......... .......... .......... .......... 23% 13.5M 33s
113850K .......... .......... .......... .......... .......... 23% 9.54M 33s
113900K .......... .......... .......... .......... .......... 23% 11.8M 33s
113950K .......... .......... .......... .......... .......... 23% 6.71M 33s
114000K .......... .......... .......... .......... .......... 23% 8.20M 33s
114050K .......... .......... .......... .......... .......... 23% 7.93M 33s
114100K .......... .......... .......... .......... .......... 23% 7.47M 33s
114150K .......... .......... .......... .......... .......... 23% 8.49M 33s
114200K .......... .......... .......... .......... .......... 23% 8.82M 33s
114250K .......... .......... .......... .......... .......... 23% 8.12M 33s
114300K .......... .......... .......... .......... .......... 23% 9.77M 33s
114350K .......... .......... .......... .......... .......... 23% 9.73M 33s
114400K .......... .......... .......... .......... .......... 23% 11.0M 33s
114450K .......... .......... .......... .......... .......... 23% 8.23M 33s
114500K .......... .......... .......... .......... .......... 23% 14.5M 33s
114550K .......... .......... .......... .......... .......... 23% 11.9M 33s
114600K .......... .......... .......... .......... .......... 23% 8.82M 33s
114650K .......... .......... .......... .......... .......... 23% 7.54M 33s
114700K .......... .......... .......... .......... .......... 23% 8.37M 33s
114750K .......... .......... .......... .......... .......... 23% 7.04M 33s
114800K .......... .......... .......... .......... .......... 23% 12.2M 33s
114850K .......... .......... .......... .......... .......... 23% 10.6M 33s
114900K .......... .......... .......... .......... .......... 23% 11.1M 33s
114950K .......... .......... .......... .......... .......... 23% 9.50M 33s
115000K .......... .......... .......... .......... .......... 23% 11.9M 33s
115050K .......... .......... .......... .......... .......... 23% 12.8M 33s
115100K .......... .......... .......... .......... .......... 23% 10.0M 33s
115150K .......... .......... .......... .......... .......... 23% 11.7M 33s
115200K .......... .......... .......... .......... .......... 23% 18.3M 33s
115250K .......... .......... .......... .......... .......... 23% 36.2M 33s
115300K .......... .......... .......... .......... .......... 24% 18.0M 33s
115350K .......... .......... .......... .......... .......... 24% 64.8M 33s
115400K .......... .......... .......... .......... .......... 24% 18.1M 33s
115450K .......... .......... .......... .......... .......... 24% 14.4M 33s
115500K .......... .......... .......... .......... .......... 24% 12.7M 33s
115550K .......... .......... .......... .......... .......... 24% 12.3M 33s
115600K .......... .......... .......... .......... .......... 24% 10.4M 33s
115650K .......... .......... .......... .......... .......... 24% 15.1M 33s
115700K .......... .......... .......... .......... .......... 24% 8.21M 33s
115750K .......... .......... .......... .......... .......... 24% 10.9M 33s
115800K .......... .......... .......... .......... .......... 24% 13.9M 33s
115850K .......... .......... .......... .......... .......... 24% 10.5M 33s
115900K .......... .......... .......... .......... .......... 24% 12.0M 33s
115950K .......... .......... .......... .......... .......... 24% 12.0M 32s
116000K .......... .......... .......... .......... .......... 24% 12.8M 32s
116050K .......... .......... .......... .......... .......... 24% 16.3M 32s
116100K .......... .......... .......... .......... .......... 24% 23.3M 32s
116150K .......... .......... .......... .......... .......... 24% 23.2M 32s
116200K .......... .......... .......... .......... .......... 24% 23.5M 32s
116250K .......... .......... .......... .......... .......... 24% 15.4M 32s
116300K .......... .......... .......... .......... .......... 24% 16.4M 32s
116350K .......... .......... .......... .......... .......... 24% 9.78M 32s
116400K .......... .......... .......... .......... .......... 24% 19.7M 32s
116450K .......... .......... .......... .......... .......... 24% 11.6M 32s
116500K .......... .......... .......... .......... .......... 24% 11.5M 32s
116550K .......... .......... .......... .......... .......... 24% 12.5M 32s
116600K .......... .......... .......... .......... .......... 24% 10.4M 32s
116650K .......... .......... .......... .......... .......... 24% 11.2M 32s
116700K .......... .......... .......... .......... .......... 24% 9.08M 32s
116750K .......... .......... .......... .......... .......... 24% 13.6M 32s
116800K .......... .......... .......... .......... .......... 24% 11.2M 32s
116850K .......... .......... .......... .......... .......... 24% 8.62M 32s
116900K .......... .......... .......... .......... .......... 24% 10.6M 32s
116950K .......... .......... .......... .......... .......... 24% 8.90M 32s
117000K .......... .......... .......... .......... .......... 24% 7.43M 32s
117050K .......... .......... .......... .......... .......... 24% 15.3M 32s
117100K .......... .......... .......... .......... .......... 24% 18.1M 32s
117150K .......... .......... .......... .......... .......... 24% 31.4M 32s
117200K .......... .......... .......... .......... .......... 24% 12.5M 32s
117250K .......... .......... .......... .......... .......... 24% 14.7M 32s
117300K .......... .......... .......... .......... .......... 24% 13.4M 32s
117350K .......... .......... .......... .......... .......... 24% 7.67M 32s
117400K .......... .......... .......... .......... .......... 24% 8.36M 32s
117450K .......... .......... .......... .......... .......... 24% 7.39M 32s
117500K .......... .......... .......... .......... .......... 24% 8.62M 32s
117550K .......... .......... .......... .......... .......... 24% 9.24M 32s
117600K .......... .......... .......... .......... .......... 24% 5.84M 32s
117650K .......... .......... .......... .......... .......... 24% 7.27M 32s
117700K .......... .......... .......... .......... .......... 24% 14.1M 32s
117750K .......... .......... .......... .......... .......... 24% 14.3M 32s
117800K .......... .......... .......... .......... .......... 24% 19.2M 32s
117850K .......... .......... .......... .......... .......... 24% 15.2M 32s
117900K .......... .......... .......... .......... .......... 24% 14.6M 32s
117950K .......... .......... .......... .......... .......... 24% 6.30M 32s
118000K .......... .......... .......... .......... .......... 24% 9.67M 32s
118050K .......... .......... .......... .......... .......... 24% 6.01M 32s
118100K .......... .......... .......... .......... .......... 24% 5.56M 32s
118150K .......... .......... .......... .......... .......... 24% 14.5M 32s
118200K .......... .......... .......... .......... .......... 24% 7.77M 32s
118250K .......... .......... .......... .......... .......... 24% 9.25M 32s
118300K .......... .......... .......... .......... .......... 24% 9.46M 32s
118350K .......... .......... .......... .......... .......... 24% 7.73M 32s
118400K .......... .......... .......... .......... .......... 24% 7.72M 32s
118450K .......... .......... .......... .......... .......... 24% 6.20M 32s
118500K .......... .......... .......... .......... .......... 24% 6.01M 32s
118550K .......... .......... .......... .......... .......... 24% 5.03M 32s
118600K .......... .......... .......... .......... .......... 24% 4.37M 32s
118650K .......... .......... .......... .......... .......... 24% 5.17M 32s
118700K .......... .......... .......... .......... .......... 24% 10.5M 32s
118750K .......... .......... .......... .......... .......... 24% 16.1M 32s
118800K .......... .......... .......... .......... .......... 24% 14.6M 32s
118850K .......... .......... .......... .......... .......... 24% 16.5M 32s
118900K .......... .......... .......... .......... .......... 24% 20.9M 32s
118950K .......... .......... .......... .......... .......... 24% 13.2M 32s
119000K .......... .......... .......... .......... .......... 24% 17.5M 32s
119050K .......... .......... .......... .......... .......... 24% 13.3M 32s
119100K .......... .......... .......... .......... .......... 24% 13.0M 32s
119150K .......... .......... .......... .......... .......... 24% 11.9M 32s
119200K .......... .......... .......... .......... .......... 24% 11.7M 32s
119250K .......... .......... .......... .......... .......... 24% 9.51M 32s
119300K .......... .......... .......... .......... .......... 24% 10.8M 32s
119350K .......... .......... .......... .......... .......... 24% 11.8M 32s
119400K .......... .......... .......... .......... .......... 24% 11.8M 32s
119450K .......... .......... .......... .......... .......... 24% 9.49M 32s
119500K .......... .......... .......... .......... .......... 24% 12.6M 32s
119550K .......... .......... .......... .......... .......... 24% 12.6M 32s
119600K .......... .......... .......... .......... .......... 24% 11.7M 32s
119650K .......... .......... .......... .......... .......... 24% 11.9M 32s
119700K .......... .......... .......... .......... .......... 24% 11.1M 32s
119750K .......... .......... .......... .......... .......... 24% 9.93M 32s
119800K .......... .......... .......... .......... .......... 24% 7.97M 32s
119850K .......... .......... .......... .......... .......... 24% 6.51M 32s
119900K .......... .......... .......... .......... .......... 24% 6.83M 32s
119950K .......... .......... .......... .......... .......... 24% 6.42M 32s
120000K .......... .......... .......... .......... .......... 24% 8.65M 32s
120050K .......... .......... .......... .......... .......... 24% 5.99M 32s
120100K .......... .......... .......... .......... .......... 24% 5.52M 32s
120150K .......... .......... .......... .......... .......... 25% 5.62M 32s
120200K .......... .......... .......... .......... .......... 25% 6.13M 32s
120250K .......... .......... .......... .......... .......... 25% 9.67M 32s
120300K .......... .......... .......... .......... .......... 25% 11.6M 32s
120350K .......... .......... .......... .......... .......... 25% 5.62M 32s
120400K .......... .......... .......... .......... .......... 25% 4.87M 32s
120450K .......... .......... .......... .......... .......... 25% 3.34M 32s
120500K .......... .......... .......... .......... .......... 25% 3.74M 32s
120550K .......... .......... .......... .......... .......... 25% 3.90M 32s
120600K .......... .......... .......... .......... .......... 25% 13.2M 32s
120650K .......... .......... .......... .......... .......... 25% 9.73M 32s
120700K .......... .......... .......... .......... .......... 25% 9.40M 32s
120750K .......... .......... .......... .......... .......... 25% 9.48M 32s
120800K .......... .......... .......... .......... .......... 25% 8.07M 32s
120850K .......... .......... .......... .......... .......... 25% 6.08M 32s
120900K .......... .......... .......... .......... .......... 25% 7.60M 32s
120950K .......... .......... .......... .......... .......... 25% 4.43M 32s
121000K .......... .......... .......... .......... .......... 25% 8.28M 32s
121050K .......... .......... .......... .......... .......... 25% 7.30M 32s
121100K .......... .......... .......... .......... .......... 25% 4.05M 32s
121150K .......... .......... .......... .......... .......... 25% 6.14M 32s
121200K .......... .......... .......... .......... .......... 25% 9.74M 32s
121250K .......... .......... .......... .......... .......... 25% 18.0M 32s
121300K .......... .......... .......... .......... .......... 25% 19.5M 32s
121350K .......... .......... .......... .......... .......... 25% 13.2M 32s
121400K .......... .......... .......... .......... .......... 25% 34.1M 32s
121450K .......... .......... .......... .......... .......... 25% 9.50M 32s
121500K .......... .......... .......... .......... .......... 25% 10.3M 32s
121550K .......... .......... .......... .......... .......... 25% 8.38M 32s
121600K .......... .......... .......... .......... .......... 25% 7.55M 32s
121650K .......... .......... .......... .......... .......... 25% 7.61M 32s
121700K .......... .......... .......... .......... .......... 25% 7.21M 32s
121750K .......... .......... .......... .......... .......... 25% 7.61M 32s
121800K .......... .......... .......... .......... .......... 25% 7.44M 32s
121850K .......... .......... .......... .......... .......... 25% 7.61M 32s
121900K .......... .......... .......... .......... .......... 25% 9.67M 32s
121950K .......... .......... .......... .......... .......... 25% 6.75M 32s
122000K .......... .......... .......... .......... .......... 25% 6.41M 32s
122050K .......... .......... .......... .......... .......... 25% 8.10M 32s
122100K .......... .......... .......... .......... .......... 25% 6.25M 32s
122150K .......... .......... .......... .......... .......... 25% 5.76M 32s
122200K .......... .......... .......... .......... .......... 25% 6.87M 32s
122250K .......... .......... .......... .......... .......... 25% 6.32M 32s
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122350K .......... .......... .......... .......... .......... 25% 5.11M 32s
122400K .......... .......... .......... .......... .......... 25% 6.17M 32s
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122500K .......... .......... .......... .......... .......... 25% 5.60M 32s
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122600K .......... .......... .......... .......... .......... 25% 19.1M 32s
122650K .......... .......... .......... .......... .......... 25% 42.8M 32s
122700K .......... .......... .......... .......... .......... 25% 44.5M 32s
122750K .......... .......... .......... .......... .......... 25% 18.8M 32s
122800K .......... .......... .......... .......... .......... 25% 81.2M 32s
122850K .......... .......... .......... .......... .......... 25% 24.9M 32s
122900K .......... .......... .......... .......... .......... 25% 66.3M 32s
122950K .......... .......... .......... .......... .......... 25% 15.4M 32s
123000K .......... .......... .......... .......... .......... 25% 22.1M 32s
123050K .......... .......... .......... .......... .......... 25% 14.7M 32s
123100K .......... .......... .......... .......... .......... 25% 10.5M 32s
123150K .......... .......... .......... .......... .......... 25% 11.1M 32s
123200K .......... .......... .......... .......... .......... 25% 10.8M 32s
123250K .......... .......... .......... .......... .......... 25% 9.22M 32s
123300K .......... .......... .......... .......... .......... 25% 6.81M 32s
123350K .......... .......... .......... .......... .......... 25% 5.95M 32s
123400K .......... .......... .......... .......... .......... 25% 5.47M 32s
123450K .......... .......... .......... .......... .......... 25% 4.05M 32s
123500K .......... .......... .......... .......... .......... 25% 6.92M 32s
123550K .......... .......... .......... .......... .......... 25% 6.36M 32s
123600K .......... .......... .......... .......... .......... 25% 5.22M 32s
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123700K .......... .......... .......... .......... .......... 25% 4.98M 32s
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123800K .......... .......... .......... .......... .......... 25% 6.94M 32s
123850K .......... .......... .......... .......... .......... 25% 5.15M 32s
123900K .......... .......... .......... .......... .......... 25% 5.22M 32s
123950K .......... .......... .......... .......... .......... 25% 6.26M 32s
124000K .......... .......... .......... .......... .......... 25% 28.6M 32s
124050K .......... .......... .......... .......... .......... 25% 17.9M 32s
124100K .......... .......... .......... .......... .......... 25% 10.4M 32s
124150K .......... .......... .......... .......... .......... 25% 28.5M 32s
124200K .......... .......... .......... .......... .......... 25% 17.6M 32s
124250K .......... .......... .......... .......... .......... 25% 14.6M 32s
124300K .......... .......... .......... .......... .......... 25% 14.7M 32s
124350K .......... .......... .......... .......... .......... 25% 11.8M 32s
124400K .......... .......... .......... .......... .......... 25% 8.42M 32s
124450K .......... .......... .......... .......... .......... 25% 6.88M 32s
124500K .......... .......... .......... .......... .......... 25% 6.77M 32s
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124700K .......... .......... .......... .......... .......... 25% 6.42M 32s
124750K .......... .......... .......... .......... .......... 25% 18.0M 32s
124800K .......... .......... .......... .......... .......... 25% 28.1M 32s
124850K .......... .......... .......... .......... .......... 25% 15.0M 32s
124900K .......... .......... .......... .......... .......... 25% 11.1M 32s
124950K .......... .......... .......... .......... .......... 26% 10.1M 32s
125000K .......... .......... .......... .......... .......... 26% 1.55M 32s
125050K .......... .......... .......... .......... .......... 26% 9.23M 32s
125100K .......... .......... .......... .......... .......... 26% 67.6M 32s
125150K .......... .......... .......... .......... .......... 26% 76.3M 32s
125200K .......... .......... .......... .......... .......... 26% 67.0M 32s
125250K .......... .......... .......... .......... .......... 26% 7.83M 32s
125300K .......... .......... .......... .......... .......... 26% 16.0M 32s
125350K .......... .......... .......... .......... .......... 26% 26.6M 32s
125400K .......... .......... .......... .......... .......... 26% 13.1M 32s
125450K .......... .......... .......... .......... .......... 26% 39.7M 32s
125500K .......... .......... .......... .......... .......... 26% 22.6M 32s
125550K .......... .......... .......... .......... .......... 26% 25.1M 32s
125600K .......... .......... .......... .......... .......... 26% 9.90M 32s
125650K .......... .......... .......... .......... .......... 26% 9.56M 32s
125700K .......... .......... .......... .......... .......... 26% 10.4M 32s
125750K .......... .......... .......... .......... .......... 26% 7.44M 32s
125800K .......... .......... .......... .......... .......... 26% 11.1M 32s
125850K .......... .......... .......... .......... .......... 26% 6.99M 32s
125900K .......... .......... .......... .......... .......... 26% 7.61M 32s
125950K .......... .......... .......... .......... .......... 26% 5.82M 32s
126000K .......... .......... .......... .......... .......... 26% 8.90M 32s
126050K .......... .......... .......... .......... .......... 26% 9.53M 32s
126100K .......... .......... .......... .......... .......... 26% 14.6M 32s
126150K .......... .......... .......... .......... .......... 26% 20.4M 32s
126200K .......... .......... .......... .......... .......... 26% 16.4M 32s
126250K .......... .......... .......... .......... .......... 26% 14.4M 32s
126300K .......... .......... .......... .......... .......... 26% 15.5M 32s
126350K .......... .......... .......... .......... .......... 26% 10.5M 32s
126400K .......... .......... .......... .......... .......... 26% 13.1M 32s
126450K .......... .......... .......... .......... .......... 26% 9.45M 32s
126500K .......... .......... .......... .......... .......... 26% 9.39M 32s
126550K .......... .......... .......... .......... .......... 26% 10.2M 32s
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126650K .......... .......... .......... .......... .......... 26% 10.1M 32s
126700K .......... .......... .......... .......... .......... 26% 9.13M 32s
126750K .......... .......... .......... .......... .......... 26% 5.99M 32s
126800K .......... .......... .......... .......... .......... 26% 9.03M 32s
126850K .......... .......... .......... .......... .......... 26% 8.21M 32s
126900K .......... .......... .......... .......... .......... 26% 8.09M 32s
126950K .......... .......... .......... .......... .......... 26% 7.45M 32s
127000K .......... .......... .......... .......... .......... 26% 8.45M 32s
127050K .......... .......... .......... .......... .......... 26% 7.15M 32s
127100K .......... .......... .......... .......... .......... 26% 9.42M 32s
127150K .......... .......... .......... .......... .......... 26% 16.5M 32s
127200K .......... .......... .......... .......... .......... 26% 10.4M 32s
127250K .......... .......... .......... .......... .......... 26% 14.7M 32s
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127350K .......... .......... .......... .......... .......... 26% 10.0M 32s
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127450K .......... .......... .......... .......... .......... 26% 10.1M 32s
127500K .......... .......... .......... .......... .......... 26% 12.7M 32s
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127650K .......... .......... .......... .......... .......... 26% 14.9M 32s
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127800K .......... .......... .......... .......... .......... 26% 8.47M 32s
127850K .......... .......... .......... .......... .......... 26% 8.07M 32s
127900K .......... .......... .......... .......... .......... 26% 8.86M 32s
127950K .......... .......... .......... .......... .......... 26% 7.04M 32s
128000K .......... .......... .......... .......... .......... 26% 8.23M 32s
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128100K .......... .......... .......... .......... .......... 26% 7.68M 32s
128150K .......... .......... .......... .......... .......... 26% 7.89M 32s
128200K .......... .......... .......... .......... .......... 26% 7.34M 32s
128250K .......... .......... .......... .......... .......... 26% 7.72M 32s
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128400K .......... .......... .......... .......... .......... 26% 20.1M 32s
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128500K .......... .......... .......... .......... .......... 26% 31.7M 32s
128550K .......... .......... .......... .......... .......... 26% 21.1M 32s
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128650K .......... .......... .......... .......... .......... 26% 18.9M 32s
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128750K .......... .......... .......... .......... .......... 26% 14.1M 32s
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128850K .......... .......... .......... .......... .......... 26% 12.6M 32s
128900K .......... .......... .......... .......... .......... 26% 11.4M 32s
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129000K .......... .......... .......... .......... .......... 26% 13.5M 32s
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129100K .......... .......... .......... .......... .......... 26% 8.52M 32s
129150K .......... .......... .......... .......... .......... 26% 10.8M 32s
129200K .......... .......... .......... .......... .......... 26% 6.27M 32s
129250K .......... .......... .......... .......... .......... 26% 5.52M 32s
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129450K .......... .......... .......... .......... .......... 26% 15.8M 32s
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129650K .......... .......... .......... .......... .......... 26% 11.9M 32s
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130000K .......... .......... .......... .......... .......... 27% 8.92M 32s
130050K .......... .......... .......... .......... .......... 27% 7.74M 32s
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130150K .......... .......... .......... .......... .......... 27% 6.66M 32s
130200K .......... .......... .......... .......... .......... 27% 3.70M 32s
130250K .......... .......... .......... .......... .......... 27% 3.98M 32s
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130750K .......... .......... .......... .......... .......... 27% 16.8M 32s
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130900K .......... .......... .......... .......... .......... 27% 15.1M 32s
130950K .......... .......... .......... .......... .......... 27% 11.8M 32s
131000K .......... .......... .......... .......... .......... 27% 14.4M 32s
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131100K .......... .......... .......... .......... .......... 27% 8.78M 32s
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131200K .......... .......... .......... .......... .......... 27% 5.34M 32s
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131300K .......... .......... .......... .......... .......... 27% 4.67M 32s
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131400K .......... .......... .......... .......... .......... 27% 10.6M 32s
131450K .......... .......... .......... .......... .......... 27% 15.6M 32s
131500K .......... .......... .......... .......... .......... 27% 22.6M 32s
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131600K .......... .......... .......... .......... .......... 27% 13.5M 32s
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131700K .......... .......... .......... .......... .......... 27% 14.8M 32s
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131800K .......... .......... .......... .......... .......... 27% 8.19M 32s
131850K .......... .......... .......... .......... .......... 27% 5.78M 32s
131900K .......... .......... .......... .......... .......... 27% 7.76M 32s
131950K .......... .......... .......... .......... .......... 27% 4.68M 32s
132000K .......... .......... .......... .......... .......... 27% 3.94M 32s
132050K .......... .......... .......... .......... .......... 27% 3.66M 32s
132100K .......... .......... .......... .......... .......... 27% 3.58M 32s
132150K .......... .......... .......... .......... .......... 27% 6.53M 32s
132200K .......... .......... .......... .......... .......... 27% 5.58M 32s
132250K .......... .......... .......... .......... .......... 27% 6.04M 32s
132300K .......... .......... .......... .......... .......... 27% 6.66M 32s
132350K .......... .......... .......... .......... .......... 27% 10.1M 32s
132400K .......... .......... .......... .......... .......... 27% 23.6M 32s
132450K .......... .......... .......... .......... .......... 27% 23.4M 32s
132500K .......... .......... .......... .......... .......... 27% 27.0M 32s
132550K .......... .......... .......... .......... .......... 27% 29.3M 32s
132600K .......... .......... .......... .......... .......... 27% 25.4M 32s
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132700K .......... .......... .......... .......... .......... 27% 17.2M 32s
132750K .......... .......... .......... .......... .......... 27% 16.7M 32s
132800K .......... .......... .......... .......... .......... 27% 18.0M 32s
132850K .......... .......... .......... .......... .......... 27% 17.5M 32s
132900K .......... .......... .......... .......... .......... 27% 12.2M 32s
132950K .......... .......... .......... .......... .......... 27% 13.0M 32s
133000K .......... .......... .......... .......... .......... 27% 11.9M 32s
133050K .......... .......... .......... .......... .......... 27% 11.9M 32s
133100K .......... .......... .......... .......... .......... 27% 9.38M 32s
133150K .......... .......... .......... .......... .......... 27% 11.4M 32s
133200K .......... .......... .......... .......... .......... 27% 7.95M 32s
133250K .......... .......... .......... .......... .......... 27% 8.61M 32s
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133350K .......... .......... .......... .......... .......... 27% 7.40M 32s
133400K .......... .......... .......... .......... .......... 27% 8.71M 32s
133450K .......... .......... .......... .......... .......... 27% 6.02M 32s
133500K .......... .......... .......... .......... .......... 27% 6.24M 32s
133550K .......... .......... .......... .......... .......... 27% 6.75M 32s
133600K .......... .......... .......... .......... .......... 27% 5.58M 32s
133650K .......... .......... .......... .......... .......... 27% 8.93M 32s
133700K .......... .......... .......... .......... .......... 27% 6.46M 32s
133750K .......... .......... .......... .......... .......... 27% 7.53M 32s
133800K .......... .......... .......... .......... .......... 27% 8.40M 32s
133850K .......... .......... .......... .......... .......... 27% 6.38M 32s
133900K .......... .......... .......... .......... .......... 27% 7.46M 32s
133950K .......... .......... .......... .......... .......... 27% 6.58M 32s
134000K .......... .......... .......... .......... .......... 27% 7.18M 32s
134050K .......... .......... .......... .......... .......... 27% 14.2M 32s
134100K .......... .......... .......... .......... .......... 27% 11.5M 32s
134150K .......... .......... .......... .......... .......... 27% 21.5M 32s
134200K .......... .......... .......... .......... .......... 27% 8.87M 32s
134250K .......... .......... .......... .......... .......... 27% 8.14M 32s
134300K .......... .......... .......... .......... .......... 27% 11.5M 32s
134350K .......... .......... .......... .......... .......... 27% 9.23M 32s
134400K .......... .......... .......... .......... .......... 27% 7.31M 32s
134450K .......... .......... .......... .......... .......... 27% 14.0M 32s
134500K .......... .......... .......... .......... .......... 27% 13.5M 32s
134550K .......... .......... .......... .......... .......... 28% 11.4M 32s
134600K .......... .......... .......... .......... .......... 28% 8.47M 32s
134650K .......... .......... .......... .......... .......... 28% 10.7M 32s
134700K .......... .......... .......... .......... .......... 28% 8.62M 32s
134750K .......... .......... .......... .......... .......... 28% 9.79M 32s
134800K .......... .......... .......... .......... .......... 28% 8.67M 32s
134850K .......... .......... .......... .......... .......... 28% 16.5M 32s
134900K .......... .......... .......... .......... .......... 28% 24.8M 32s
134950K .......... .......... .......... .......... .......... 28% 13.4M 32s
135000K .......... .......... .......... .......... .......... 28% 7.89M 32s
135050K .......... .......... .......... .......... .......... 28% 11.8M 32s
135100K .......... .......... .......... .......... .......... 28% 10.2M 32s
135150K .......... .......... .......... .......... .......... 28% 5.78M 32s
135200K .......... .......... .......... .......... .......... 28% 7.90M 32s
135250K .......... .......... .......... .......... .......... 28% 6.78M 32s
135300K .......... .......... .......... .......... .......... 28% 5.47M 32s
135350K .......... .......... .......... .......... .......... 28% 8.56M 32s
135400K .......... .......... .......... .......... .......... 28% 7.44M 32s
135450K .......... .......... .......... .......... .......... 28% 6.81M 32s
135500K .......... .......... .......... .......... .......... 28% 7.02M 32s
135550K .......... .......... .......... .......... .......... 28% 7.31M 32s
135600K .......... .......... .......... .......... .......... 28% 6.76M 32s
135650K .......... .......... .......... .......... .......... 28% 5.15M 32s
135700K .......... .......... .......... .......... .......... 28% 4.69M 32s
135750K .......... .......... .......... .......... .......... 28% 4.60M 32s
135800K .......... .......... .......... .......... .......... 28% 5.79M 32s
135850K .......... .......... .......... .......... .......... 28% 12.5M 32s
135900K .......... .......... .......... .......... .......... 28% 18.3M 32s
135950K .......... .......... .......... .......... .......... 28% 14.3M 32s
136000K .......... .......... .......... .......... .......... 28% 20.3M 32s
136050K .......... .......... .......... .......... .......... 28% 17.0M 32s
136100K .......... .......... .......... .......... .......... 28% 11.8M 32s
136150K .......... .......... .......... .......... .......... 28% 13.1M 32s
136200K .......... .......... .......... .......... .......... 28% 15.5M 32s
136250K .......... .......... .......... .......... .......... 28% 12.4M 32s
136300K .......... .......... .......... .......... .......... 28% 12.6M 32s
136350K .......... .......... .......... .......... .......... 28% 10.3M 32s
136400K .......... .......... .......... .......... .......... 28% 13.1M 32s
136450K .......... .......... .......... .......... .......... 28% 11.2M 32s
136500K .......... .......... .......... .......... .......... 28% 9.51M 32s
136550K .......... .......... .......... .......... .......... 28% 9.59M 32s
136600K .......... .......... .......... .......... .......... 28% 7.30M 32s
136650K .......... .......... .......... .......... .......... 28% 12.7M 32s
136700K .......... .......... .......... .......... .......... 28% 16.3M 32s
136750K .......... .......... .......... .......... .......... 28% 29.8M 32s
136800K .......... .......... .......... .......... .......... 28% 17.0M 32s
136850K .......... .......... .......... .......... .......... 28% 65.9M 32s
136900K .......... .......... .......... .......... .......... 28% 37.2M 32s
136950K .......... .......... .......... .......... .......... 28% 14.9M 32s
137000K .......... .......... .......... .......... .......... 28% 18.0M 32s
137050K .......... .......... .......... .......... .......... 28% 54.7M 32s
137100K .......... .......... .......... .......... .......... 28% 13.0M 32s
137150K .......... .......... .......... .......... .......... 28% 17.5M 31s
137200K .......... .......... .......... .......... .......... 28% 12.6M 31s
137250K .......... .......... .......... .......... .......... 28% 14.7M 31s
137300K .......... .......... .......... .......... .......... 28% 8.28M 31s
137350K .......... .......... .......... .......... .......... 28% 9.55M 31s
137400K .......... .......... .......... .......... .......... 28% 11.9M 31s
137450K .......... .......... .......... .......... .......... 28% 9.98M 31s
137500K .......... .......... .......... .......... .......... 28% 12.2M 31s
137550K .......... .......... .......... .......... .......... 28% 9.72M 31s
137600K .......... .......... .......... .......... .......... 28% 11.0M 31s
137650K .......... .......... .......... .......... .......... 28% 10.3M 31s
137700K .......... .......... .......... .......... .......... 28% 6.69M 31s
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137800K .......... .......... .......... .......... .......... 28% 6.76M 31s
137850K .......... .......... .......... .......... .......... 28% 5.61M 31s
137900K .......... .......... .......... .......... .......... 28% 6.44M 31s
137950K .......... .......... .......... .......... .......... 28% 8.15M 31s
138000K .......... .......... .......... .......... .......... 28% 21.0M 31s
138050K .......... .......... .......... .......... .......... 28% 23.9M 31s
138100K .......... .......... .......... .......... .......... 28% 29.1M 31s
138150K .......... .......... .......... .......... .......... 28% 26.9M 31s
138200K .......... .......... .......... .......... .......... 28% 17.9M 31s
138250K .......... .......... .......... .......... .......... 28% 31.7M 31s
138300K .......... .......... .......... .......... .......... 28% 46.2M 31s
138350K .......... .......... .......... .......... .......... 28% 16.5M 31s
138400K .......... .......... .......... .......... .......... 28% 34.1M 31s
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138500K .......... .......... .......... .......... .......... 28% 19.0M 31s
138550K .......... .......... .......... .......... .......... 28% 19.5M 31s
138600K .......... .......... .......... .......... .......... 28% 15.6M 31s
138650K .......... .......... .......... .......... .......... 28% 17.9M 31s
138700K .......... .......... .......... .......... .......... 28% 9.95M 31s
138750K .......... .......... .......... .......... .......... 28% 25.7M 31s
138800K .......... .......... .......... .......... .......... 28% 14.6M 31s
138850K .......... .......... .......... .......... .......... 28% 11.5M 31s
138900K .......... .......... .......... .......... .......... 28% 17.4M 31s
138950K .......... .......... .......... .......... .......... 28% 9.98M 31s
139000K .......... .......... .......... .......... .......... 28% 14.5M 31s
139050K .......... .......... .......... .......... .......... 28% 11.9M 31s
139100K .......... .......... .......... .......... .......... 28% 12.7M 31s
139150K .......... .......... .......... .......... .......... 28% 13.5M 31s
139200K .......... .......... .......... .......... .......... 28% 11.5M 31s
139250K .......... .......... .......... .......... .......... 28% 13.1M 31s
139300K .......... .......... .......... .......... .......... 28% 9.40M 31s
139350K .......... .......... .......... .......... .......... 29% 10.5M 31s
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139450K .......... .......... .......... .......... .......... 29% 9.12M 31s
139500K .......... .......... .......... .......... .......... 29% 12.3M 31s
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139600K .......... .......... .......... .......... .......... 29% 8.56M 31s
139650K .......... .......... .......... .......... .......... 29% 11.2M 31s
139700K .......... .......... .......... .......... .......... 29% 5.67M 31s
139750K .......... .......... .......... .......... .......... 29% 7.04M 31s
139800K .......... .......... .......... .......... .......... 29% 5.22M 31s
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139900K .......... .......... .......... .......... .......... 29% 4.43M 31s
139950K .......... .......... .......... .......... .......... 29% 3.10M 31s
140000K .......... .......... .......... .......... .......... 29% 5.07M 31s
140050K .......... .......... .......... .......... .......... 29% 8.28M 31s
140100K .......... .......... .......... .......... .......... 29% 11.1M 31s
140150K .......... .......... .......... .......... .......... 29% 11.0M 31s
140200K .......... .......... .......... .......... .......... 29% 8.65M 31s
140250K .......... .......... .......... .......... .......... 29% 12.3M 31s
140300K .......... .......... .......... .......... .......... 29% 7.16M 31s
140350K .......... .......... .......... .......... .......... 29% 10.8M 31s
140400K .......... .......... .......... .......... .......... 29% 7.07M 31s
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140500K .......... .......... .......... .......... .......... 29% 7.15M 31s
140550K .......... .......... .......... .......... .......... 29% 7.32M 31s
140600K .......... .......... .......... .......... .......... 29% 5.59M 31s
140650K .......... .......... .......... .......... .......... 29% 9.66M 31s
140700K .......... .......... .......... .......... .......... 29% 6.38M 31s
140750K .......... .......... .......... .......... .......... 29% 7.59M 31s
140800K .......... .......... .......... .......... .......... 29% 9.40M 31s
140850K .......... .......... .......... .......... .......... 29% 7.29M 31s
140900K .......... .......... .......... .......... .......... 29% 10.1M 31s
140950K .......... .......... .......... .......... .......... 29% 11.0M 31s
141000K .......... .......... .......... .......... .......... 29% 11.4M 31s
141050K .......... .......... .......... .......... .......... 29% 10.5M 31s
141100K .......... .......... .......... .......... .......... 29% 9.26M 31s
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141200K .......... .......... .......... .......... .......... 29% 9.45M 31s
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141300K .......... .......... .......... .......... .......... 29% 8.42M 31s
141350K .......... .......... .......... .......... .......... 29% 6.56M 31s
141400K .......... .......... .......... .......... .......... 29% 6.08M 31s
141450K .......... .......... .......... .......... .......... 29% 6.69M 31s
141500K .......... .......... .......... .......... .......... 29% 9.21M 31s
141550K .......... .......... .......... .......... .......... 29% 7.45M 31s
141600K .......... .......... .......... .......... .......... 29% 7.51M 31s
141650K .......... .......... .......... .......... .......... 29% 7.57M 31s
141700K .......... .......... .......... .......... .......... 29% 7.35M 31s
141750K .......... .......... .......... .......... .......... 29% 16.4M 31s
141800K .......... .......... .......... .......... .......... 29% 18.5M 31s
141850K .......... .......... .......... .......... .......... 29% 15.2M 31s
141900K .......... .......... .......... .......... .......... 29% 17.3M 31s
141950K .......... .......... .......... .......... .......... 29% 11.7M 31s
142000K .......... .......... .......... .......... .......... 29% 12.1M 31s
142050K .......... .......... .......... .......... .......... 29% 14.5M 31s
142100K .......... .......... .......... .......... .......... 29% 8.18M 31s
142150K .......... .......... .......... .......... .......... 29% 16.7M 31s
142200K .......... .......... .......... .......... .......... 29% 12.6M 31s
142250K .......... .......... .......... .......... .......... 29% 16.7M 31s
142300K .......... .......... .......... .......... .......... 29% 13.3M 31s
142350K .......... .......... .......... .......... .......... 29% 10.3M 31s
142400K .......... .......... .......... .......... .......... 29% 14.6M 31s
142450K .......... .......... .......... .......... .......... 29% 7.28M 31s
142500K .......... .......... .......... .......... .......... 29% 8.91M 31s
142550K .......... .......... .......... .......... .......... 29% 12.6M 31s
142600K .......... .......... .......... .......... .......... 29% 15.0M 31s
142650K .......... .......... .......... .......... .......... 29% 22.1M 31s
142700K .......... .......... .......... .......... .......... 29% 16.6M 31s
142750K .......... .......... .......... .......... .......... 29% 27.0M 31s
142800K .......... .......... .......... .......... .......... 29% 17.1M 31s
142850K .......... .......... .......... .......... .......... 29% 13.5M 31s
142900K .......... .......... .......... .......... .......... 29% 17.1M 31s
142950K .......... .......... .......... .......... .......... 29% 15.6M 31s
143000K .......... .......... .......... .......... .......... 29% 8.30M 31s
143050K .......... .......... .......... .......... .......... 29% 8.56M 31s
143100K .......... .......... .......... .......... .......... 29% 9.45M 31s
143150K .......... .......... .......... .......... .......... 29% 11.3M 31s
143200K .......... .......... .......... .......... .......... 29% 9.01M 31s
143250K .......... .......... .......... .......... .......... 29% 8.50M 31s
143300K .......... .......... .......... .......... .......... 29% 8.43M 31s
143350K .......... .......... .......... .......... .......... 29% 7.95M 31s
143400K .......... .......... .......... .......... .......... 29% 7.28M 31s
143450K .......... .......... .......... .......... .......... 29% 6.42M 31s
143500K .......... .......... .......... .......... .......... 29% 6.94M 31s
143550K .......... .......... .......... .......... .......... 29% 6.92M 31s
143600K .......... .......... .......... .......... .......... 29% 5.30M 31s
143650K .......... .......... .......... .......... .......... 29% 5.84M 31s
143700K .......... .......... .......... .......... .......... 29% 8.48M 31s
143750K .......... .......... .......... .......... .......... 29% 10.6M 31s
143800K .......... .......... .......... .......... .......... 29% 13.9M 31s
143850K .......... .......... .......... .......... .......... 29% 9.97M 31s
143900K .......... .......... .......... .......... .......... 29% 12.5M 31s
143950K .......... .......... .......... .......... .......... 29% 9.00M 31s
144000K .......... .......... .......... .......... .......... 29% 9.73M 31s
144050K .......... .......... .......... .......... .......... 29% 10.0M 31s
144100K .......... .......... .......... .......... .......... 29% 8.67M 31s
144150K .......... .......... .......... .......... .......... 30% 10.6M 31s
144200K .......... .......... .......... .......... .......... 30% 10.1M 31s
144250K .......... .......... .......... .......... .......... 30% 16.2M 31s
144300K .......... .......... .......... .......... .......... 30% 27.3M 31s
144350K .......... .......... .......... .......... .......... 30% 26.2M 31s
144400K .......... .......... .......... .......... .......... 30% 19.5M 31s
144450K .......... .......... .......... .......... .......... 30% 28.8M 31s
144500K .......... .......... .......... .......... .......... 30% 34.5M 31s
144550K .......... .......... .......... .......... .......... 30% 34.1M 31s
144600K .......... .......... .......... .......... .......... 30% 29.9M 31s
144650K .......... .......... .......... .......... .......... 30% 30.9M 31s
144700K .......... .......... .......... .......... .......... 30% 19.7M 31s
144750K .......... .......... .......... .......... .......... 30% 37.6M 31s
144800K .......... .......... .......... .......... .......... 30% 25.1M 31s
144850K .......... .......... .......... .......... .......... 30% 20.7M 31s
144900K .......... .......... .......... .......... .......... 30% 19.9M 31s
144950K .......... .......... .......... .......... .......... 30% 11.2M 31s
145000K .......... .......... .......... .......... .......... 30% 10.1M 31s
145050K .......... .......... .......... .......... .......... 30% 11.0M 31s
145100K .......... .......... .......... .......... .......... 30% 7.45M 31s
145150K .......... .......... .......... .......... .......... 30% 8.41M 31s
145200K .......... .......... .......... .......... .......... 30% 7.50M 31s
145250K .......... .......... .......... .......... .......... 30% 10.3M 31s
145300K .......... .......... .......... .......... .......... 30% 9.54M 31s
145350K .......... .......... .......... .......... .......... 30% 8.80M 31s
145400K .......... .......... .......... .......... .......... 30% 8.85M 31s
145450K .......... .......... .......... .......... .......... 30% 8.03M 31s
145500K .......... .......... .......... .......... .......... 30% 7.71M 31s
145550K .......... .......... .......... .......... .......... 30% 28.5M 31s
145600K .......... .......... .......... .......... .......... 30% 17.1M 31s
145650K .......... .......... .......... .......... .......... 30% 17.6M 31s
145700K .......... .......... .......... .......... .......... 30% 11.8M 31s
145750K .......... .......... .......... .......... .......... 30% 15.8M 31s
145800K .......... .......... .......... .......... .......... 30% 14.6M 31s
145850K .......... .......... .......... .......... .......... 30% 12.7M 31s
145900K .......... .......... .......... .......... .......... 30% 15.3M 31s
145950K .......... .......... .......... .......... .......... 30% 9.68M 31s
146000K .......... .......... .......... .......... .......... 30% 13.0M 31s
146050K .......... .......... .......... .......... .......... 30% 13.3M 31s
146100K .......... .......... .......... .......... .......... 30% 11.4M 31s
146150K .......... .......... .......... .......... .......... 30% 10.4M 31s
146200K .......... .......... .......... .......... .......... 30% 10.2M 31s
146250K .......... .......... .......... .......... .......... 30% 79.0M 31s
146300K .......... .......... .......... .......... .......... 30% 17.7M 31s
146350K .......... .......... .......... .......... .......... 30% 18.9M 31s
146400K .......... .......... .......... .......... .......... 30% 47.0M 31s
146450K .......... .......... .......... .......... .......... 30% 14.6M 31s
146500K .......... .......... .......... .......... .......... 30% 14.8M 31s
146550K .......... .......... .......... .......... .......... 30% 11.9M 31s
146600K .......... .......... .......... .......... .......... 30% 12.2M 31s
146650K .......... .......... .......... .......... .......... 30% 13.5M 31s
146700K .......... .......... .......... .......... .......... 30% 8.70M 31s
146750K .......... .......... .......... .......... .......... 30% 10.9M 31s
146800K .......... .......... .......... .......... .......... 30% 8.25M 31s
146850K .......... .......... .......... .......... .......... 30% 6.84M 31s
146900K .......... .......... .......... .......... .......... 30% 6.46M 31s
146950K .......... .......... .......... .......... .......... 30% 5.83M 31s
147000K .......... .......... .......... .......... .......... 30% 6.67M 31s
147050K .......... .......... .......... .......... .......... 30% 11.0M 31s
147100K .......... .......... .......... .......... .......... 30% 19.3M 31s
147150K .......... .......... .......... .......... .......... 30% 22.3M 31s
147200K .......... .......... .......... .......... .......... 30% 18.6M 31s
147250K .......... .......... .......... .......... .......... 30% 21.1M 31s
147300K .......... .......... .......... .......... .......... 30% 19.1M 31s
147350K .......... .......... .......... .......... .......... 30% 11.9M 31s
147400K .......... .......... .......... .......... .......... 30% 21.1M 31s
147450K .......... .......... .......... .......... .......... 30% 12.1M 31s
147500K .......... .......... .......... .......... .......... 30% 12.1M 31s
147550K .......... .......... .......... .......... .......... 30% 7.88M 31s
147600K .......... .......... .......... .......... .......... 30% 8.30M 31s
147650K .......... .......... .......... .......... .......... 30% 6.66M 31s
147700K .......... .......... .......... .......... .......... 30% 5.12M 31s
147750K .......... .......... .......... .......... .......... 30% 7.71M 31s
147800K .......... .......... .......... .......... .......... 30% 5.21M 31s
147850K .......... .......... .......... .......... .......... 30% 6.05M 31s
147900K .......... .......... .......... .......... .......... 30% 5.08M 31s
147950K .......... .......... .......... .......... .......... 30% 4.32M 31s
148000K .......... .......... .......... .......... .......... 30% 9.46M 31s
148050K .......... .......... .......... .......... .......... 30% 7.02M 31s
148100K .......... .......... .......... .......... .......... 30% 6.69M 31s
148150K .......... .......... .......... .......... .......... 30% 10.3M 31s
148200K .......... .......... .......... .......... .......... 30% 10.2M 31s
148250K .......... .......... .......... .......... .......... 30% 14.5M 31s
148300K .......... .......... .......... .......... .......... 30% 10.8M 31s
148350K .......... .......... .......... .......... .......... 30% 10.2M 31s
148400K .......... .......... .......... .......... .......... 30% 9.59M 31s
148450K .......... .......... .......... .......... .......... 30% 8.10M 31s
148500K .......... .......... .......... .......... .......... 30% 8.02M 31s
148550K .......... .......... .......... .......... .......... 30% 6.80M 31s
148600K .......... .......... .......... .......... .......... 30% 6.23M 31s
148650K .......... .......... .......... .......... .......... 30% 7.50M 31s
148700K .......... .......... .......... .......... .......... 30% 5.33M 31s
148750K .......... .......... .......... .......... .......... 30% 5.77M 31s
148800K .......... .......... .......... .......... .......... 30% 6.78M 31s
148850K .......... .......... .......... .......... .......... 30% 6.14M 31s
148900K .......... .......... .......... .......... .......... 30% 12.2M 31s
148950K .......... .......... .......... .......... .......... 31% 19.8M 31s
149000K .......... .......... .......... .......... .......... 31% 27.0M 31s
149050K .......... .......... .......... .......... .......... 31% 12.6M 31s
149100K .......... .......... .......... .......... .......... 31% 27.7M 31s
149150K .......... .......... .......... .......... .......... 31% 27.7M 31s
149200K .......... .......... .......... .......... .......... 31% 15.2M 31s
149250K .......... .......... .......... .......... .......... 31% 21.0M 31s
149300K .......... .......... .......... .......... .......... 31% 13.4M 30s
149350K .......... .......... .......... .......... .......... 31% 8.42M 30s
149400K .......... .......... .......... .......... .......... 31% 10.5M 30s
149450K .......... .......... .......... .......... .......... 31% 8.57M 30s
149500K .......... .......... .......... .......... .......... 31% 9.43M 30s
149550K .......... .......... .......... .......... .......... 31% 8.24M 30s
149600K .......... .......... .......... .......... .......... 31% 6.03M 30s
149650K .......... .......... .......... .......... .......... 31% 11.8M 30s
149700K .......... .......... .......... .......... .......... 31% 20.2M 30s
149750K .......... .......... .......... .......... .......... 31% 24.6M 30s
149800K .......... .......... .......... .......... .......... 31% 34.7M 30s
149850K .......... .......... .......... .......... .......... 31% 12.3M 30s
149900K .......... .......... .......... .......... .......... 31% 9.98M 30s
149950K .......... .......... .......... .......... .......... 31% 9.21M 30s
150000K .......... .......... .......... .......... .......... 31% 7.43M 30s
150050K .......... .......... .......... .......... .......... 31% 6.72M 30s
150100K .......... .......... .......... .......... .......... 31% 5.57M 30s
150150K .......... .......... .......... .......... .......... 31% 5.38M 30s
150200K .......... .......... .......... .......... .......... 31% 6.41M 30s
150250K .......... .......... .......... .......... .......... 31% 12.6M 30s
150300K .......... .......... .......... .......... .......... 31% 11.5M 30s
150350K .......... .......... .......... .......... .......... 31% 8.61M 30s
150400K .......... .......... .......... .......... .......... 31% 7.51M 30s
150450K .......... .......... .......... .......... .......... 31% 5.14M 30s
150500K .......... .......... .......... .......... .......... 31% 9.75M 30s
150550K .......... .......... .......... .......... .......... 31% 7.88M 30s
150600K .......... .......... .......... .......... .......... 31% 6.64M 30s
150650K .......... .......... .......... .......... .......... 31% 6.15M 30s
150700K .......... .......... .......... .......... .......... 31% 5.31M 30s
150750K .......... .......... .......... .......... .......... 31% 5.08M 30s
150800K .......... .......... .......... .......... .......... 31% 16.4M 30s
150850K .......... .......... .......... .......... .......... 31% 16.6M 30s
150900K .......... .......... .......... .......... .......... 31% 33.3M 30s
150950K .......... .......... .......... .......... .......... 31% 18.8M 30s
151000K .......... .......... .......... .......... .......... 31% 29.0M 30s
151050K .......... .......... .......... .......... .......... 31% 20.1M 30s
151100K .......... .......... .......... .......... .......... 31% 18.6M 30s
151150K .......... .......... .......... .......... .......... 31% 15.8M 30s
151200K .......... .......... .......... .......... .......... 31% 12.6M 30s
151250K .......... .......... .......... .......... .......... 31% 10.1M 30s
151300K .......... .......... .......... .......... .......... 31% 25.3M 30s
151350K .......... .......... .......... .......... .......... 31% 10.3M 30s
151400K .......... .......... .......... .......... .......... 31% 10.1M 30s
151450K .......... .......... .......... .......... .......... 31% 8.11M 30s
151500K .......... .......... .......... .......... .......... 31% 10.1M 30s
151550K .......... .......... .......... .......... .......... 31% 8.58M 30s
151600K .......... .......... .......... .......... .......... 31% 9.50M 30s
151650K .......... .......... .......... .......... .......... 31% 9.54M 30s
151700K .......... .......... .......... .......... .......... 31% 21.5M 30s
151750K .......... .......... .......... .......... .......... 31% 16.6M 30s
151800K .......... .......... .......... .......... .......... 31% 44.9M 30s
151850K .......... .......... .......... .......... .......... 31% 20.6M 30s
151900K .......... .......... .......... .......... .......... 31% 20.3M 30s
151950K .......... .......... .......... .......... .......... 31% 20.0M 30s
152000K .......... .......... .......... .......... .......... 31% 12.0M 30s
152050K .......... .......... .......... .......... .......... 31% 14.9M 30s
152100K .......... .......... .......... .......... .......... 31% 11.1M 30s
152150K .......... .......... .......... .......... .......... 31% 12.4M 30s
152200K .......... .......... .......... .......... .......... 31% 9.48M 30s
152250K .......... .......... .......... .......... .......... 31% 10.1M 30s
152300K .......... .......... .......... .......... .......... 31% 10.7M 30s
152350K .......... .......... .......... .......... .......... 31% 9.58M 30s
152400K .......... .......... .......... .......... .......... 31% 13.1M 30s
152450K .......... .......... .......... .......... .......... 31% 27.8M 30s
152500K .......... .......... .......... .......... .......... 31% 28.8M 30s
152550K .......... .......... .......... .......... .......... 31% 18.1M 30s
152600K .......... .......... .......... .......... .......... 31% 30.6M 30s
152650K .......... .......... .......... .......... .......... 31% 31.2M 30s
152700K .......... .......... .......... .......... .......... 31% 15.1M 30s
152750K .......... .......... .......... .......... .......... 31% 17.9M 30s
152800K .......... .......... .......... .......... .......... 31% 17.9M 30s
152850K .......... .......... .......... .......... .......... 31% 9.06M 30s
152900K .......... .......... .......... .......... .......... 31% 21.2M 30s
152950K .......... .......... .......... .......... .......... 31% 12.2M 30s
153000K .......... .......... .......... .......... .......... 31% 11.5M 30s
153050K .......... .......... .......... .......... .......... 31% 10.5M 30s
153100K .......... .......... .......... .......... .......... 31% 12.1M 30s
153150K .......... .......... .......... .......... .......... 31% 9.12M 30s
153200K .......... .......... .......... .......... .......... 31% 9.01M 30s
153250K .......... .......... .......... .......... .......... 31% 12.2M 30s
153300K .......... .......... .......... .......... .......... 31% 11.4M 30s
153350K .......... .......... .......... .......... .......... 31% 7.19M 30s
153400K .......... .......... .......... .......... .......... 31% 8.06M 30s
153450K .......... .......... .......... .......... .......... 31% 7.94M 30s
153500K .......... .......... .......... .......... .......... 31% 12.8M 30s
153550K .......... .......... .......... .......... .......... 31% 16.4M 30s
153600K .......... .......... .......... .......... .......... 31% 24.6M 30s
153650K .......... .......... .......... .......... .......... 31% 12.7M 30s
153700K .......... .......... .......... .......... .......... 31% 37.4M 30s
153750K .......... .......... .......... .......... .......... 32% 22.3M 30s
153800K .......... .......... .......... .......... .......... 32% 17.2M 30s
153850K .......... .......... .......... .......... .......... 32% 15.6M 30s
153900K .......... .......... .......... .......... .......... 32% 14.2M 30s
153950K .......... .......... .......... .......... .......... 32% 15.8M 30s
154000K .......... .......... .......... .......... .......... 32% 16.5M 30s
154050K .......... .......... .......... .......... .......... 32% 14.6M 30s
154100K .......... .......... .......... .......... .......... 32% 14.1M 30s
154150K .......... .......... .......... .......... .......... 32% 11.6M 30s
154200K .......... .......... .......... .......... .......... 32% 12.3M 30s
154250K .......... .......... .......... .......... .......... 32% 14.0M 30s
154300K .......... .......... .......... .......... .......... 32% 9.50M 30s
154350K .......... .......... .......... .......... .......... 32% 7.63M 30s
154400K .......... .......... .......... .......... .......... 32% 6.54M 30s
154450K .......... .......... .......... .......... .......... 32% 7.67M 30s
154500K .......... .......... .......... .......... .......... 32% 7.70M 30s
154550K .......... .......... .......... .......... .......... 32% 7.10M 30s
154600K .......... .......... .......... .......... .......... 32% 4.69M 30s
154650K .......... .......... .......... .......... .......... 32% 7.51M 30s
154700K .......... .......... .......... .......... .......... 32% 11.9M 30s
154750K .......... .......... .......... .......... .......... 32% 17.5M 30s
154800K .......... .......... .......... .......... .......... 32% 16.5M 30s
154850K .......... .......... .......... .......... .......... 32% 10.2M 30s
154900K .......... .......... .......... .......... .......... 32% 18.9M 30s
154950K .......... .......... .......... .......... .......... 32% 8.50M 30s
155000K .......... .......... .......... .......... .......... 32% 10.3M 30s
155050K .......... .......... .......... .......... .......... 32% 7.62M 30s
155100K .......... .......... .......... .......... .......... 32% 8.70M 30s
155150K .......... .......... .......... .......... .......... 32% 7.39M 30s
155200K .......... .......... .......... .......... .......... 32% 8.06M 30s
155250K .......... .......... .......... .......... .......... 32% 7.77M 30s
155300K .......... .......... .......... .......... .......... 32% 8.14M 30s
155350K .......... .......... .......... .......... .......... 32% 5.01M 30s
155400K .......... .......... .......... .......... .......... 32% 9.90M 30s
155450K .......... .......... .......... .......... .......... 32% 14.4M 30s
155500K .......... .......... .......... .......... .......... 32% 11.7M 30s
155550K .......... .......... .......... .......... .......... 32% 46.9M 30s
155600K .......... .......... .......... .......... .......... 32% 11.5M 30s
155650K .......... .......... .......... .......... .......... 32% 18.0M 30s
155700K .......... .......... .......... .......... .......... 32% 12.5M 30s
155750K .......... .......... .......... .......... .......... 32% 17.0M 30s
155800K .......... .......... .......... .......... .......... 32% 11.1M 30s
155850K .......... .......... .......... .......... .......... 32% 7.92M 30s
155900K .......... .......... .......... .......... .......... 32% 13.6M 30s
155950K .......... .......... .......... .......... .......... 32% 9.86M 30s
156000K .......... .......... .......... .......... .......... 32% 13.1M 30s
156050K .......... .......... .......... .......... .......... 32% 13.1M 30s
156100K .......... .......... .......... .......... .......... 32% 10.3M 30s
156150K .......... .......... .......... .......... .......... 32% 9.09M 30s
156200K .......... .......... .......... .......... .......... 32% 4.82M 30s
156250K .......... .......... .......... .......... .......... 32% 9.82M 30s
156300K .......... .......... .......... .......... .......... 32% 45.1M 30s
156350K .......... .......... .......... .......... .......... 32% 18.7M 30s
156400K .......... .......... .......... .......... .......... 32% 12.7M 30s
156450K .......... .......... .......... .......... .......... 32% 15.1M 30s
156500K .......... .......... .......... .......... .......... 32% 16.4M 30s
156550K .......... .......... .......... .......... .......... 32% 14.7M 30s
156600K .......... .......... .......... .......... .......... 32% 10.7M 30s
156650K .......... .......... .......... .......... .......... 32% 14.1M 30s
156700K .......... .......... .......... .......... .......... 32% 11.1M 30s
156750K .......... .......... .......... .......... .......... 32% 13.8M 30s
156800K .......... .......... .......... .......... .......... 32% 10.6M 30s
156850K .......... .......... .......... .......... .......... 32% 8.96M 30s
156900K .......... .......... .......... .......... .......... 32% 10.2M 30s
156950K .......... .......... .......... .......... .......... 32% 6.32M 30s
157000K .......... .......... .......... .......... .......... 32% 10.2M 30s
157050K .......... .......... .......... .......... .......... 32% 8.49M 30s
157100K .......... .......... .......... .......... .......... 32% 8.08M 30s
157150K .......... .......... .......... .......... .......... 32% 7.02M 30s
157200K .......... .......... .......... .......... .......... 32% 8.23M 30s
157250K .......... .......... .......... .......... .......... 32% 7.63M 30s
157300K .......... .......... .......... .......... .......... 32% 7.09M 30s
157350K .......... .......... .......... .......... .......... 32% 6.15M 30s
157400K .......... .......... .......... .......... .......... 32% 9.26M 30s
157450K .......... .......... .......... .......... .......... 32% 15.8M 30s
157500K .......... .......... .......... .......... .......... 32% 19.1M 30s
157550K .......... .......... .......... .......... .......... 32% 28.8M 30s
157600K .......... .......... .......... .......... .......... 32% 20.8M 30s
157650K .......... .......... .......... .......... .......... 32% 18.0M 30s
157700K .......... .......... .......... .......... .......... 32% 14.4M 30s
157750K .......... .......... .......... .......... .......... 32% 17.3M 30s
157800K .......... .......... .......... .......... .......... 32% 20.6M 30s
157850K .......... .......... .......... .......... .......... 32% 15.1M 30s
157900K .......... .......... .......... .......... .......... 32% 11.9M 30s
157950K .......... .......... .......... .......... .......... 32% 9.71M 30s
158000K .......... .......... .......... .......... .......... 32% 11.1M 30s
158050K .......... .......... .......... .......... .......... 32% 10.6M 30s
158100K .......... .......... .......... .......... .......... 32% 8.69M 30s
158150K .......... .......... .......... .......... .......... 32% 8.20M 30s
158200K .......... .......... .......... .......... .......... 32% 8.58M 30s
158250K .......... .......... .......... .......... .......... 32% 6.58M 30s
158300K .......... .......... .......... .......... .......... 32% 6.86M 30s
158350K .......... .......... .......... .......... .......... 32% 6.42M 30s
158400K .......... .......... .......... .......... .......... 32% 5.99M 30s
158450K .......... .......... .......... .......... .......... 32% 4.76M 30s
158500K .......... .......... .......... .......... .......... 32% 4.51M 30s
158550K .......... .......... .......... .......... .......... 32% 5.46M 30s
158600K .......... .......... .......... .......... .......... 33% 4.60M 30s
158650K .......... .......... .......... .......... .......... 33% 4.96M 30s
158700K .......... .......... .......... .......... .......... 33% 7.03M 30s
158750K .......... .......... .......... .......... .......... 33% 17.3M 30s
158800K .......... .......... .......... .......... .......... 33% 27.0M 30s
158850K .......... .......... .......... .......... .......... 33% 16.9M 30s
158900K .......... .......... .......... .......... .......... 33% 27.3M 30s
158950K .......... .......... .......... .......... .......... 33% 26.1M 30s
159000K .......... .......... .......... .......... .......... 33% 27.9M 30s
159050K .......... .......... .......... .......... .......... 33% 17.3M 30s
159100K .......... .......... .......... .......... .......... 33% 18.5M 30s
159150K .......... .......... .......... .......... .......... 33% 24.1M 30s
159200K .......... .......... .......... .......... .......... 33% 28.4M 30s
159250K .......... .......... .......... .......... .......... 33% 19.7M 30s
159300K .......... .......... .......... .......... .......... 33% 13.0M 30s
159350K .......... .......... .......... .......... .......... 33% 10.6M 30s
159400K .......... .......... .......... .......... .......... 33% 11.9M 30s
159450K .......... .......... .......... .......... .......... 33% 10.8M 30s
159500K .......... .......... .......... .......... .......... 33% 9.80M 30s
159550K .......... .......... .......... .......... .......... 33% 11.0M 30s
159600K .......... .......... .......... .......... .......... 33% 6.50M 30s
159650K .......... .......... .......... .......... .......... 33% 8.88M 30s
159700K .......... .......... .......... .......... .......... 33% 8.22M 30s
159750K .......... .......... .......... .......... .......... 33% 11.1M 30s
159800K .......... .......... .......... .......... .......... 33% 8.41M 30s
159850K .......... .......... .......... .......... .......... 33% 8.27M 30s
159900K .......... .......... .......... .......... .......... 33% 8.10M 30s
159950K .......... .......... .......... .......... .......... 33% 7.19M 30s
160000K .......... .......... .......... .......... .......... 33% 8.32M 30s
160050K .......... .......... .......... .......... .......... 33% 9.07M 30s
160100K .......... .......... .......... .......... .......... 33% 22.9M 30s
160150K .......... .......... .......... .......... .......... 33% 17.9M 30s
160200K .......... .......... .......... .......... .......... 33% 19.3M 30s
160250K .......... .......... .......... .......... .......... 33% 24.7M 29s
160300K .......... .......... .......... .......... .......... 33% 15.7M 29s
160350K .......... .......... .......... .......... .......... 33% 20.7M 29s
160400K .......... .......... .......... .......... .......... 33% 9.76M 29s
160450K .......... .......... .......... .......... .......... 33% 16.8M 29s
160500K .......... .......... .......... .......... .......... 33% 6.95M 29s
160550K .......... .......... .......... .......... .......... 33% 6.20M 29s
160600K .......... .......... .......... .......... .......... 33% 4.65M 29s
160650K .......... .......... .......... .......... .......... 33% 6.05M 29s
160700K .......... .......... .......... .......... .......... 33% 9.03M 29s
160750K .......... .......... .......... .......... .......... 33% 24.9M 29s
160800K .......... .......... .......... .......... .......... 33% 17.7M 29s
160850K .......... .......... .......... .......... .......... 33% 9.94M 29s
160900K .......... .......... .......... .......... .......... 33% 18.9M 29s
160950K .......... .......... .......... .......... .......... 33% 10.6M 29s
161000K .......... .......... .......... .......... .......... 33% 13.0M 29s
161050K .......... .......... .......... .......... .......... 33% 7.11M 29s
161100K .......... .......... .......... .......... .......... 33% 4.95M 29s
161150K .......... .......... .......... .......... .......... 33% 7.02M 29s
161200K .......... .......... .......... .......... .......... 33% 5.96M 29s
161250K .......... .......... .......... .......... .......... 33% 5.78M 29s
161300K .......... .......... .......... .......... .......... 33% 5.01M 29s
161350K .......... .......... .......... .......... .......... 33% 5.40M 29s
161400K .......... .......... .......... .......... .......... 33% 14.1M 29s
161450K .......... .......... .......... .......... .......... 33% 7.73M 29s
161500K .......... .......... .......... .......... .......... 33% 9.13M 29s
161550K .......... .......... .......... .......... .......... 33% 12.1M 29s
161600K .......... .......... .......... .......... .......... 33% 11.1M 29s
161650K .......... .......... .......... .......... .......... 33% 10.6M 29s
161700K .......... .......... .......... .......... .......... 33% 9.74M 29s
161750K .......... .......... .......... .......... .......... 33% 11.1M 29s
161800K .......... .......... .......... .......... .......... 33% 11.0M 29s
161850K .......... .......... .......... .......... .......... 33% 9.44M 29s
161900K .......... .......... .......... .......... .......... 33% 10.3M 29s
161950K .......... .......... .......... .......... .......... 33% 7.59M 29s
162000K .......... .......... .......... .......... .......... 33% 12.9M 29s
162050K .......... .......... .......... .......... .......... 33% 9.78M 29s
162100K .......... .......... .......... .......... .......... 33% 8.91M 29s
162150K .......... .......... .......... .......... .......... 33% 9.27M 29s
162200K .......... .......... .......... .......... .......... 33% 9.43M 29s
162250K .......... .......... .......... .......... .......... 33% 9.08M 29s
162300K .......... .......... .......... .......... .......... 33% 7.89M 29s
162350K .......... .......... .......... .......... .......... 33% 7.14M 29s
162400K .......... .......... .......... .......... .......... 33% 14.2M 29s
162450K .......... .......... .......... .......... .......... 33% 7.56M 29s
162500K .......... .......... .......... .......... .......... 33% 8.47M 29s
162550K .......... .......... .......... .......... .......... 33% 7.74M 29s
162600K .......... .......... .......... .......... .......... 33% 6.82M 29s
162650K .......... .......... .......... .......... .......... 33% 5.60M 29s
162700K .......... .......... .......... .......... .......... 33% 8.82M 29s
162750K .......... .......... .......... .......... .......... 33% 8.65M 29s
162800K .......... .......... .......... .......... .......... 33% 8.57M 29s
162850K .......... .......... .......... .......... .......... 33% 7.56M 29s
162900K .......... .......... .......... .......... .......... 33% 7.19M 29s
162950K .......... .......... .......... .......... .......... 33% 5.40M 29s
163000K .......... .......... .......... .......... .......... 33% 8.39M 29s
163050K .......... .......... .......... .......... .......... 33% 6.44M 29s
163100K .......... .......... .......... .......... .......... 33% 5.69M 29s
163150K .......... .......... .......... .......... .......... 33% 5.22M 29s
163200K .......... .......... .......... .......... .......... 33% 4.62M 29s
163250K .......... .......... .......... .......... .......... 33%  215K 30s
163300K .......... .......... .......... .......... .......... 33% 3.22M 30s
163350K .......... .......... .......... .......... .......... 33% 5.37M 30s
163400K .......... .......... .......... .......... .......... 34% 12.4M 30s
163450K .......... .......... .......... .......... .......... 34% 8.65M 30s
163500K .......... .......... .......... .......... .......... 34% 12.5M 30s
163550K .......... .......... .......... .......... .......... 34% 14.4M 30s
163600K .......... .......... .......... .......... .......... 34% 11.1M 30s
163650K .......... .......... .......... .......... .......... 34% 12.5M 30s
163700K .......... .......... .......... .......... .......... 34% 9.70M 30s
163750K .......... .......... .......... .......... .......... 34% 13.8M 30s
163800K .......... .......... .......... .......... .......... 34% 8.53M 30s
163850K .......... .......... .......... .......... .......... 34% 9.93M 30s
163900K .......... .......... .......... .......... .......... 34% 8.26M 30s
163950K .......... .......... .......... .......... .......... 34% 8.53M 30s
164000K .......... .......... .......... .......... .......... 34% 8.22M 30s
164050K .......... .......... .......... .......... .......... 34% 7.78M 30s
164100K .......... .......... .......... .......... .......... 34% 6.13M 30s
164150K .......... .......... .......... .......... .......... 34% 6.06M 30s
164200K .......... .......... .......... .......... .......... 34% 6.52M 30s
164250K .......... .......... .......... .......... .......... 34% 47.7M 30s
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177200K .......... .......... .......... .......... .......... 36% 18.9M 29s
177250K .......... .......... .......... .......... .......... 36% 13.3M 29s
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178000K .......... .......... .......... .......... .......... 37% 11.4M 29s
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178100K .......... .......... .......... .......... .......... 37% 7.77M 29s
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178250K .......... .......... .......... .......... .......... 37% 9.56M 29s
178300K .......... .......... .......... .......... .......... 37% 10.8M 29s
178350K .......... .......... .......... .......... .......... 37% 10.5M 29s
178400K .......... .......... .......... .......... .......... 37% 25.8M 29s
178450K .......... .......... .......... .......... .......... 37% 17.1M 29s
178500K .......... .......... .......... .......... .......... 37% 28.6M 29s
178550K .......... .......... .......... .......... .......... 37% 20.0M 29s
178600K .......... .......... .......... .......... .......... 37% 13.0M 29s
178650K .......... .......... .......... .......... .......... 37% 41.5M 29s
178700K .......... .......... .......... .......... .......... 37% 8.98M 29s
178750K .......... .......... .......... .......... .......... 37% 20.1M 29s
178800K .......... .......... .......... .......... .......... 37% 15.4M 29s
178850K .......... .......... .......... .......... .......... 37% 7.29M 29s
178900K .......... .......... .......... .......... .......... 37% 7.52M 28s
178950K .......... .......... .......... .......... .......... 37% 6.47M 28s
179000K .......... .......... .......... .......... .......... 37% 7.90M 28s
179050K .......... .......... .......... .......... .......... 37% 5.06M 29s
179100K .......... .......... .......... .......... .......... 37% 4.78M 29s
179150K .......... .......... .......... .......... .......... 37% 5.54M 29s
179200K .......... .......... .......... .......... .......... 37% 4.44M 29s
179250K .......... .......... .......... .......... .......... 37% 17.4M 29s
179300K .......... .......... .......... .......... .......... 37% 32.1M 28s
179350K .......... .......... .......... .......... .......... 37% 17.7M 28s
179400K .......... .......... .......... .......... .......... 37% 80.7M 28s
179450K .......... .......... .......... .......... .......... 37% 31.3M 28s
179500K .......... .......... .......... .......... .......... 37% 39.1M 28s
179550K .......... .......... .......... .......... .......... 37% 27.8M 28s
179600K .......... .......... .......... .......... .......... 37% 16.7M 28s
179650K .......... .......... .......... .......... .......... 37% 21.9M 28s
179700K .......... .......... .......... .......... .......... 37% 15.0M 28s
179750K .......... .......... .......... .......... .......... 37% 17.2M 28s
179800K .......... .......... .......... .......... .......... 37% 13.4M 28s
179850K .......... .......... .......... .......... .......... 37% 17.5M 28s
179900K .......... .......... .......... .......... .......... 37% 15.6M 28s
179950K .......... .......... .......... .......... .......... 37% 12.3M 28s
180000K .......... .......... .......... .......... .......... 37% 12.2M 28s
180050K .......... .......... .......... .......... .......... 37% 11.4M 28s
180100K .......... .......... .......... .......... .......... 37% 8.67M 28s
180150K .......... .......... .......... .......... .......... 37% 10.3M 28s
180200K .......... .......... .......... .......... .......... 37% 7.53M 28s
180250K .......... .......... .......... .......... .......... 37% 10.3M 28s
180300K .......... .......... .......... .......... .......... 37% 9.84M 28s
180350K .......... .......... .......... .......... .......... 37% 9.22M 28s
180400K .......... .......... .......... .......... .......... 37% 17.4M 28s
180450K .......... .......... .......... .......... .......... 37% 15.0M 28s
180500K .......... .......... .......... .......... .......... 37% 8.78M 28s
180550K .......... .......... .......... .......... .......... 37% 7.05M 28s
180600K .......... .......... .......... .......... .......... 37% 8.03M 28s
180650K .......... .......... .......... .......... .......... 37% 13.2M 28s
180700K .......... .......... .......... .......... .......... 37% 6.01M 28s
180750K .......... .......... .......... .......... .......... 37% 7.65M 28s
180800K .......... .......... .......... .......... .......... 37% 6.73M 28s
180850K .......... .......... .......... .......... .......... 37% 10.5M 28s
180900K .......... .......... .......... .......... .......... 37% 10.0M 28s
180950K .......... .......... .......... .......... .......... 37% 10.3M 28s
181000K .......... .......... .......... .......... .......... 37% 8.33M 28s
181050K .......... .......... .......... .......... .......... 37% 8.94M 28s
181100K .......... .......... .......... .......... .......... 37% 7.79M 28s
181150K .......... .......... .......... .......... .......... 37% 12.3M 28s
181200K .......... .......... .......... .......... .......... 37% 8.81M 28s
181250K .......... .......... .......... .......... .......... 37% 8.73M 28s
181300K .......... .......... .......... .......... .......... 37% 7.15M 28s
181350K .......... .......... .......... .......... .......... 37% 5.50M 28s
181400K .......... .......... .......... .......... .......... 37% 8.07M 28s
181450K .......... .......... .......... .......... .......... 37% 7.77M 28s
181500K .......... .......... .......... .......... .......... 37% 8.65M 28s
181550K .......... .......... .......... .......... .......... 37% 10.7M 28s
181600K .......... .......... .......... .......... .......... 37% 6.76M 28s
181650K .......... .......... .......... .......... .......... 37% 7.32M 28s
181700K .......... .......... .......... .......... .......... 37% 7.97M 28s
181750K .......... .......... .......... .......... .......... 37% 6.13M 28s
181800K .......... .......... .......... .......... .......... 37% 7.09M 28s
181850K .......... .......... .......... .......... .......... 37% 7.79M 28s
181900K .......... .......... .......... .......... .......... 37% 9.18M 28s
181950K .......... .......... .......... .......... .......... 37% 6.54M 28s
182000K .......... .......... .......... .......... .......... 37% 8.10M 28s
182050K .......... .......... .......... .......... .......... 37% 6.80M 28s
182100K .......... .......... .......... .......... .......... 37% 10.2M 28s
182150K .......... .......... .......... .......... .......... 37% 17.9M 28s
182200K .......... .......... .......... .......... .......... 37% 11.8M 28s
182250K .......... .......... .......... .......... .......... 37% 54.7M 28s
182300K .......... .......... .......... .......... .......... 37% 9.94M 28s
182350K .......... .......... .......... .......... .......... 37% 9.23M 28s
182400K .......... .......... .......... .......... .......... 37% 11.9M 28s
182450K .......... .......... .......... .......... .......... 37% 8.87M 28s
182500K .......... .......... .......... .......... .......... 37% 7.63M 28s
182550K .......... .......... .......... .......... .......... 37% 10.6M 28s
182600K .......... .......... .......... .......... .......... 38% 7.70M 28s
182650K .......... .......... .......... .......... .......... 38% 5.40M 28s
182700K .......... .......... .......... .......... .......... 38% 6.33M 28s
182750K .......... .......... .......... .......... .......... 38% 9.72M 28s
182800K .......... .......... .......... .......... .......... 38% 8.53M 28s
182850K .......... .......... .......... .......... .......... 38% 7.55M 28s
182900K .......... .......... .......... .......... .......... 38% 12.2M 28s
182950K .......... .......... .......... .......... .......... 38% 6.62M 28s
183000K .......... .......... .......... .......... .......... 38% 10.3M 28s
183050K .......... .......... .......... .......... .......... 38% 7.58M 28s
183100K .......... .......... .......... .......... .......... 38% 14.6M 28s
183150K .......... .......... .......... .......... .......... 38% 14.6M 28s
183200K .......... .......... .......... .......... .......... 38% 8.02M 28s
183250K .......... .......... .......... .......... .......... 38% 12.1M 28s
183300K .......... .......... .......... .......... .......... 38% 13.3M 28s
183350K .......... .......... .......... .......... .......... 38% 12.4M 28s
183400K .......... .......... .......... .......... .......... 38% 12.2M 28s
183450K .......... .......... .......... .......... .......... 38% 8.68M 28s
183500K .......... .......... .......... .......... .......... 38% 8.39M 28s
183550K .......... .......... .......... .......... .......... 38% 9.29M 28s
183600K .......... .......... .......... .......... .......... 38% 9.92M 28s
183650K .......... .......... .......... .......... .......... 38% 11.5M 28s
183700K .......... .......... .......... .......... .......... 38% 8.99M 28s
183750K .......... .......... .......... .......... .......... 38% 11.1M 28s
183800K .......... .......... .......... .......... .......... 38% 9.34M 28s
183850K .......... .......... .......... .......... .......... 38% 8.50M 28s
183900K .......... .......... .......... .......... .......... 38% 9.82M 28s
183950K .......... .......... .......... .......... .......... 38% 7.79M 28s
184000K .......... .......... .......... .......... .......... 38% 12.9M 28s
184050K .......... .......... .......... .......... .......... 38% 12.2M 28s
184100K .......... .......... .......... .......... .......... 38% 9.54M 28s
184150K .......... .......... .......... .......... .......... 38% 6.91M 28s
184200K .......... .......... .......... .......... .......... 38% 7.96M 28s
184250K .......... .......... .......... .......... .......... 38% 9.30M 28s
184300K .......... .......... .......... .......... .......... 38% 8.06M 28s
184350K .......... .......... .......... .......... .......... 38% 7.16M 28s
184400K .......... .......... .......... .......... .......... 38% 5.94M 28s
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184550K .......... .......... .......... .......... .......... 38% 6.67M 28s
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184650K .......... .......... .......... .......... .......... 38% 6.78M 28s
184700K .......... .......... .......... .......... .......... 38% 6.03M 28s
184750K .......... .......... .......... .......... .......... 38% 5.46M 28s
184800K .......... .......... .......... .......... .......... 38% 10.4M 28s
184850K .......... .......... .......... .......... .......... 38% 16.3M 28s
184900K .......... .......... .......... .......... .......... 38% 29.2M 28s
184950K .......... .......... .......... .......... .......... 38% 19.3M 28s
185000K .......... .......... .......... .......... .......... 38% 18.3M 28s
185050K .......... .......... .......... .......... .......... 38% 21.0M 28s
185100K .......... .......... .......... .......... .......... 38% 8.77M 28s
185150K .......... .......... .......... .......... .......... 38% 12.9M 28s
185200K .......... .......... .......... .......... .......... 38% 8.83M 28s
185250K .......... .......... .......... .......... .......... 38% 7.95M 28s
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185400K .......... .......... .......... .......... .......... 38% 10.2M 28s
185450K .......... .......... .......... .......... .......... 38% 7.76M 28s
185500K .......... .......... .......... .......... .......... 38% 8.38M 28s
185550K .......... .......... .......... .......... .......... 38% 6.81M 28s
185600K .......... .......... .......... .......... .......... 38% 5.78M 28s
185650K .......... .......... .......... .......... .......... 38% 7.20M 28s
185700K .......... .......... .......... .......... .......... 38% 6.74M 28s
185750K .......... .......... .......... .......... .......... 38% 13.1M 28s
185800K .......... .......... .......... .......... .......... 38% 26.5M 28s
185850K .......... .......... .......... .......... .......... 38% 16.3M 28s
185900K .......... .......... .......... .......... .......... 38% 17.3M 28s
185950K .......... .......... .......... .......... .......... 38% 26.4M 28s
186000K .......... .......... .......... .......... .......... 38% 19.3M 28s
186050K .......... .......... .......... .......... .......... 38% 23.9M 28s
186100K .......... .......... .......... .......... .......... 38% 13.7M 28s
186150K .......... .......... .......... .......... .......... 38% 15.7M 28s
186200K .......... .......... .......... .......... .......... 38% 9.46M 28s
186250K .......... .......... .......... .......... .......... 38% 9.43M 28s
186300K .......... .......... .......... .......... .......... 38% 10.9M 28s
186350K .......... .......... .......... .......... .......... 38% 6.42M 28s
186400K .......... .......... .......... .......... .......... 38% 5.77M 28s
186450K .......... .......... .......... .......... .......... 38% 3.73M 28s
186500K .......... .......... .......... .......... .......... 38% 3.61M 28s
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186600K .......... .......... .......... .......... .......... 38% 4.38M 28s
186650K .......... .......... .......... .......... .......... 38% 6.39M 28s
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186750K .......... .......... .......... .......... .......... 38% 5.63M 28s
186800K .......... .......... .......... .......... .......... 38% 10.9M 28s
186850K .......... .......... .......... .......... .......... 38% 15.6M 28s
186900K .......... .......... .......... .......... .......... 38% 79.8M 28s
186950K .......... .......... .......... .......... .......... 38% 28.9M 28s
187000K .......... .......... .......... .......... .......... 38% 41.9M 28s
187050K .......... .......... .......... .......... .......... 38% 22.8M 28s
187100K .......... .......... .......... .......... .......... 38% 8.06M 28s
187150K .......... .......... .......... .......... .......... 38% 9.22M 28s
187200K .......... .......... .......... .......... .......... 38% 10.4M 28s
187250K .......... .......... .......... .......... .......... 38% 8.41M 28s
187300K .......... .......... .......... .......... .......... 38% 12.1M 28s
187350K .......... .......... .......... .......... .......... 38% 8.48M 28s
187400K .......... .......... .......... .......... .......... 39% 9.60M 28s
187450K .......... .......... .......... .......... .......... 39% 7.39M 28s
187500K .......... .......... .......... .......... .......... 39% 14.2M 28s
187550K .......... .......... .......... .......... .......... 39% 11.7M 28s
187600K .......... .......... .......... .......... .......... 39% 15.6M 28s
187650K .......... .......... .......... .......... .......... 39% 20.4M 28s
187700K .......... .......... .......... .......... .......... 39% 7.23M 28s
187750K .......... .......... .......... .......... .......... 39% 11.1M 28s
187800K .......... .......... .......... .......... .......... 39% 8.59M 28s
187850K .......... .......... .......... .......... .......... 39% 6.68M 28s
187900K .......... .......... .......... .......... .......... 39% 8.24M 28s
187950K .......... .......... .......... .......... .......... 39% 8.17M 28s
188000K .......... .......... .......... .......... .......... 39% 9.67M 28s
188050K .......... .......... .......... .......... .......... 39% 29.3M 28s
188100K .......... .......... .......... .......... .......... 39% 17.4M 28s
188150K .......... .......... .......... .......... .......... 39% 25.7M 28s
188200K .......... .......... .......... .......... .......... 39% 15.7M 28s
188250K .......... .......... .......... .......... .......... 39% 22.1M 28s
188300K .......... .......... .......... .......... .......... 39% 10.5M 28s
188350K .......... .......... .......... .......... .......... 39% 12.4M 28s
188400K .......... .......... .......... .......... .......... 39% 11.0M 28s
188450K .......... .......... .......... .......... .......... 39% 10.6M 28s
188500K .......... .......... .......... .......... .......... 39% 10.3M 28s
188550K .......... .......... .......... .......... .......... 39% 12.1M 28s
188600K .......... .......... .......... .......... .......... 39% 12.5M 28s
188650K .......... .......... .......... .......... .......... 39% 13.5M 28s
188700K .......... .......... .......... .......... .......... 39% 9.95M 28s
188750K .......... .......... .......... .......... .......... 39% 13.6M 28s
188800K .......... .......... .......... .......... .......... 39% 12.3M 28s
188850K .......... .......... .......... .......... .......... 39% 12.4M 28s
188900K .......... .......... .......... .......... .......... 39% 11.5M 28s
188950K .......... .......... .......... .......... .......... 39% 10.8M 28s
189000K .......... .......... .......... .......... .......... 39% 16.6M 28s
189050K .......... .......... .......... .......... .......... 39% 8.57M 28s
189100K .......... .......... .......... .......... .......... 39% 10.2M 28s
189150K .......... .......... .......... .......... .......... 39% 7.70M 28s
189200K .......... .......... .......... .......... .......... 39% 5.70M 28s
189250K .......... .......... .......... .......... .......... 39% 7.32M 28s
189300K .......... .......... .......... .......... .......... 39% 7.78M 28s
189350K .......... .......... .......... .......... .......... 39% 11.8M 28s
189400K .......... .......... .......... .......... .......... 39% 38.0M 28s
189450K .......... .......... .......... .......... .......... 39% 19.2M 28s
189500K .......... .......... .......... .......... .......... 39% 31.5M 28s
189550K .......... .......... .......... .......... .......... 39% 19.8M 28s
189600K .......... .......... .......... .......... .......... 39% 27.8M 28s
189650K .......... .......... .......... .......... .......... 39% 32.2M 28s
189700K .......... .......... .......... .......... .......... 39% 19.4M 28s
189750K .......... .......... .......... .......... .......... 39% 33.4M 28s
189800K .......... .......... .......... .......... .......... 39% 17.4M 28s
189850K .......... .......... .......... .......... .......... 39% 37.1M 28s
189900K .......... .......... .......... .......... .......... 39% 19.6M 28s
189950K .......... .......... .......... .......... .......... 39% 16.5M 28s
190000K .......... .......... .......... .......... .......... 39% 19.9M 28s
190050K .......... .......... .......... .......... .......... 39% 11.1M 28s
190100K .......... .......... .......... .......... .......... 39% 13.1M 28s
190150K .......... .......... .......... .......... .......... 39% 10.8M 28s
190200K .......... .......... .......... .......... .......... 39% 9.23M 28s
190250K .......... .......... .......... .......... .......... 39% 9.91M 28s
190300K .......... .......... .......... .......... .......... 39% 9.97M 28s
190350K .......... .......... .......... .......... .......... 39% 7.90M 28s
190400K .......... .......... .......... .......... .......... 39% 7.80M 28s
190450K .......... .......... .......... .......... .......... 39% 6.91M 28s
190500K .......... .......... .......... .......... .......... 39% 8.46M 28s
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190600K .......... .......... .......... .......... .......... 39% 9.13M 28s
190650K .......... .......... .......... .......... .......... 39% 8.28M 28s
190700K .......... .......... .......... .......... .......... 39% 18.5M 28s
190750K .......... .......... .......... .......... .......... 39% 17.4M 27s
190800K .......... .......... .......... .......... .......... 39% 26.0M 27s
190850K .......... .......... .......... .......... .......... 39% 14.5M 27s
190900K .......... .......... .......... .......... .......... 39% 15.5M 27s
190950K .......... .......... .......... .......... .......... 39% 26.4M 27s
191000K .......... .......... .......... .......... .......... 39% 19.5M 27s
191050K .......... .......... .......... .......... .......... 39% 17.7M 27s
191100K .......... .......... .......... .......... .......... 39% 23.2M 27s
191150K .......... .......... .......... .......... .......... 39% 19.0M 27s
191200K .......... .......... .......... .......... .......... 39% 18.9M 27s
191250K .......... .......... .......... .......... .......... 39% 17.9M 27s
191300K .......... .......... .......... .......... .......... 39% 14.6M 27s
191350K .......... .......... .......... .......... .......... 39% 17.2M 27s
191400K .......... .......... .......... .......... .......... 39% 13.3M 27s
191450K .......... .......... .......... .......... .......... 39% 12.7M 27s
191500K .......... .......... .......... .......... .......... 39% 16.1M 27s
191550K .......... .......... .......... .......... .......... 39% 11.7M 27s
191600K .......... .......... .......... .......... .......... 39% 8.54M 27s
191650K .......... .......... .......... .......... .......... 39% 6.38M 27s
191700K .......... .......... .......... .......... .......... 39% 4.47M 27s
191750K .......... .......... .......... .......... .......... 39% 8.43M 27s
191800K .......... .......... .......... .......... .......... 39% 9.50M 27s
191850K .......... .......... .......... .......... .......... 39% 5.72M 27s
191900K .......... .......... .......... .......... .......... 39% 7.67M 27s
191950K .......... .......... .......... .......... .......... 39% 6.82M 27s
192000K .......... .......... .......... .......... .......... 39% 15.9M 27s
192050K .......... .......... .......... .......... .......... 39% 17.4M 27s
192100K .......... .......... .......... .......... .......... 39% 12.1M 27s
192150K .......... .......... .......... .......... .......... 39% 15.6M 27s
192200K .......... .......... .......... .......... .......... 40% 13.9M 27s
192250K .......... .......... .......... .......... .......... 40% 10.2M 27s
192300K .......... .......... .......... .......... .......... 40% 4.20M 27s
192350K .......... .......... .......... .......... .......... 40% 6.12M 27s
192400K .......... .......... .......... .......... .......... 40% 6.50M 27s
192450K .......... .......... .......... .......... .......... 40% 5.92M 27s
192500K .......... .......... .......... .......... .......... 40% 9.68M 27s
192550K .......... .......... .......... .......... .......... 40% 7.27M 27s
192600K .......... .......... .......... .......... .......... 40% 7.08M 27s
192650K .......... .......... .......... .......... .......... 40% 12.7M 27s
192700K .......... .......... .......... .......... .......... 40% 11.4M 27s
192750K .......... .......... .......... .......... .......... 40% 14.6M 27s
192800K .......... .......... .......... .......... .......... 40% 11.5M 27s
192850K .......... .......... .......... .......... .......... 40% 11.4M 27s
192900K .......... .......... .......... .......... .......... 40% 14.1M 27s
192950K .......... .......... .......... .......... .......... 40% 9.25M 27s
193000K .......... .......... .......... .......... .......... 40% 11.0M 27s
193050K .......... .......... .......... .......... .......... 40% 11.7M 27s
193100K .......... .......... .......... .......... .......... 40% 28.0M 27s
193150K .......... .......... .......... .......... .......... 40% 18.2M 27s
193200K .......... .......... .......... .......... .......... 40% 12.8M 27s
193250K .......... .......... .......... .......... .......... 40% 13.4M 27s
193300K .......... .......... .......... .......... .......... 40% 16.8M 27s
193350K .......... .......... .......... .......... .......... 40% 9.25M 27s
193400K .......... .......... .......... .......... .......... 40% 13.0M 27s
193450K .......... .......... .......... .......... .......... 40% 8.48M 27s
193500K .......... .......... .......... .......... .......... 40% 8.61M 27s
193550K .......... .......... .......... .......... .......... 40% 7.30M 27s
193600K .......... .......... .......... .......... .......... 40% 7.59M 27s
193650K .......... .......... .......... .......... .......... 40% 10.0M 27s
193700K .......... .......... .......... .......... .......... 40% 6.19M 27s
193750K .......... .......... .......... .......... .......... 40% 6.40M 27s
193800K .......... .......... .......... .......... .......... 40% 6.43M 27s
193850K .......... .......... .......... .......... .......... 40% 5.27M 27s
193900K .......... .......... .......... .......... .......... 40% 7.03M 27s
193950K .......... .......... .......... .......... .......... 40% 4.12M 27s
194000K .......... .......... .......... .......... .......... 40% 4.25M 27s
194050K .......... .......... .......... .......... .......... 40% 3.37M 27s
194100K .......... .......... .......... .......... .......... 40% 3.66M 27s
194150K .......... .......... .......... .......... .......... 40% 9.14M 27s
194200K .......... .......... .......... .......... .......... 40% 24.0M 27s
194250K .......... .......... .......... .......... .......... 40% 25.3M 27s
194300K .......... .......... .......... .......... .......... 40% 17.1M 27s
194350K .......... .......... .......... .......... .......... 40% 16.4M 27s
194400K .......... .......... .......... .......... .......... 40% 16.4M 27s
194450K .......... .......... .......... .......... .......... 40% 10.4M 27s
194500K .......... .......... .......... .......... .......... 40% 14.5M 27s
194550K .......... .......... .......... .......... .......... 40% 9.75M 27s
194600K .......... .......... .......... .......... .......... 40% 10.8M 27s
194650K .......... .......... .......... .......... .......... 40% 8.98M 27s
194700K .......... .......... .......... .......... .......... 40% 11.1M 27s
194750K .......... .......... .......... .......... .......... 40% 10.3M 27s
194800K .......... .......... .......... .......... .......... 40% 11.2M 27s
194850K .......... .......... .......... .......... .......... 40% 6.88M 27s
194900K .......... .......... .......... .......... .......... 40% 11.2M 27s
194950K .......... .......... .......... .......... .......... 40% 9.90M 27s
195000K .......... .......... .......... .......... .......... 40% 9.54M 27s
195050K .......... .......... .......... .......... .......... 40% 9.32M 27s
195100K .......... .......... .......... .......... .......... 40% 6.69M 27s
195150K .......... .......... .......... .......... .......... 40% 10.6M 27s
195200K .......... .......... .......... .......... .......... 40% 8.07M 27s
195250K .......... .......... .......... .......... .......... 40% 9.05M 27s
195300K .......... .......... .......... .......... .......... 40% 8.27M 27s
195350K .......... .......... .......... .......... .......... 40% 6.46M 27s
195400K .......... .......... .......... .......... .......... 40% 7.97M 27s
195450K .......... .......... .......... .......... .......... 40% 5.99M 27s
195500K .......... .......... .......... .......... .......... 40% 13.9M 27s
195550K .......... .......... .......... .......... .......... 40% 48.2M 27s
195600K .......... .......... .......... .......... .......... 40% 14.0M 27s
195650K .......... .......... .......... .......... .......... 40% 31.3M 27s
195700K .......... .......... .......... .......... .......... 40% 20.2M 27s
195750K .......... .......... .......... .......... .......... 40% 17.0M 27s
195800K .......... .......... .......... .......... .......... 40% 18.8M 27s
195850K .......... .......... .......... .......... .......... 40% 13.6M 27s
195900K .......... .......... .......... .......... .......... 40% 17.5M 27s
195950K .......... .......... .......... .......... .......... 40% 11.8M 27s
196000K .......... .......... .......... .......... .......... 40% 15.8M 27s
196050K .......... .......... .......... .......... .......... 40% 11.5M 27s
196100K .......... .......... .......... .......... .......... 40% 8.21M 27s
196150K .......... .......... .......... .......... .......... 40% 8.02M 27s
196200K .......... .......... .......... .......... .......... 40% 9.72M 27s
196250K .......... .......... .......... .......... .......... 40% 10.6M 27s
196300K .......... .......... .......... .......... .......... 40% 13.0M 27s
196350K .......... .......... .......... .......... .......... 40% 7.73M 27s
196400K .......... .......... .......... .......... .......... 40% 11.7M 27s
196450K .......... .......... .......... .......... .......... 40% 7.41M 27s
196500K .......... .......... .......... .......... .......... 40% 12.2M 27s
196550K .......... .......... .......... .......... .......... 40% 10.9M 27s
196600K .......... .......... .......... .......... .......... 40% 8.21M 27s
196650K .......... .......... .......... .......... .......... 40% 9.78M 27s
196700K .......... .......... .......... .......... .......... 40% 8.48M 27s
196750K .......... .......... .......... .......... .......... 40% 9.47M 27s
196800K .......... .......... .......... .......... .......... 40% 12.6M 27s
196850K .......... .......... .......... .......... .......... 40% 25.4M 27s
196900K .......... .......... .......... .......... .......... 40% 26.9M 27s
196950K .......... .......... .......... .......... .......... 40% 24.7M 27s
197000K .......... .......... .......... .......... .......... 40% 18.3M 27s
197050K .......... .......... .......... .......... .......... 41% 28.4M 27s
197100K .......... .......... .......... .......... .......... 41% 24.0M 27s
197150K .......... .......... .......... .......... .......... 41% 20.0M 27s
197200K .......... .......... .......... .......... .......... 41% 52.6M 27s
197250K .......... .......... .......... .......... .......... 41% 27.0M 27s
197300K .......... .......... .......... .......... .......... 41% 18.4M 27s
197350K .......... .......... .......... .......... .......... 41% 17.4M 27s
197400K .......... .......... .......... .......... .......... 41% 18.9M 27s
197450K .......... .......... .......... .......... .......... 41% 11.4M 27s
197500K .......... .......... .......... .......... .......... 41% 14.5M 27s
197550K .......... .......... .......... .......... .......... 41% 11.6M 27s
197600K .......... .......... .......... .......... .......... 41% 9.16M 27s
197650K .......... .......... .......... .......... .......... 41% 8.69M 27s
197700K .......... .......... .......... .......... .......... 41% 8.82M 27s
197750K .......... .......... .......... .......... .......... 41% 5.85M 27s
197800K .......... .......... .......... .......... .......... 41% 7.67M 27s
197850K .......... .......... .......... .......... .......... 41% 6.34M 27s
197900K .......... .......... .......... .......... .......... 41% 9.03M 27s
197950K .......... .......... .......... .......... .......... 41% 6.54M 27s
198000K .......... .......... .......... .......... .......... 41% 8.42M 27s
198050K .......... .......... .......... .......... .......... 41% 10.8M 27s
198100K .......... .......... .......... .......... .......... 41% 17.4M 27s
198150K .......... .......... .......... .......... .......... 41% 26.2M 27s
198200K .......... .......... .......... .......... .......... 41% 18.5M 27s
198250K .......... .......... .......... .......... .......... 41% 22.6M 27s
198300K .......... .......... .......... .......... .......... 41% 18.1M 27s
198350K .......... .......... .......... .......... .......... 41% 14.5M 27s
198400K .......... .......... .......... .......... .......... 41% 15.2M 27s
198450K .......... .......... .......... .......... .......... 41% 12.1M 27s
198500K .......... .......... .......... .......... .......... 41% 10.5M 27s
198550K .......... .......... .......... .......... .......... 41% 12.1M 27s
198600K .......... .......... .......... .......... .......... 41% 9.95M 27s
198650K .......... .......... .......... .......... .......... 41% 12.2M 27s
198700K .......... .......... .......... .......... .......... 41% 8.53M 27s
198750K .......... .......... .......... .......... .......... 41% 10.7M 27s
198800K .......... .......... .......... .......... .......... 41% 9.95M 27s
198850K .......... .......... .......... .......... .......... 41% 6.53M 27s
198900K .......... .......... .......... .......... .......... 41% 15.0M 27s
198950K .......... .......... .......... .......... .......... 41% 7.64M 27s
199000K .......... .......... .......... .......... .......... 41% 8.71M 27s
199050K .......... .......... .......... .......... .......... 41% 6.39M 27s
199100K .......... .......... .......... .......... .......... 41% 8.27M 27s
199150K .......... .......... .......... .......... .......... 41% 8.80M 27s
199200K .......... .......... .......... .......... .......... 41% 8.53M 27s
199250K .......... .......... .......... .......... .......... 41% 12.3M 27s
199300K .......... .......... .......... .......... .......... 41% 10.9M 27s
199350K .......... .......... .......... .......... .......... 41% 10.0M 27s
199400K .......... .......... .......... .......... .......... 41% 9.85M 27s
199450K .......... .......... .......... .......... .......... 41% 8.97M 27s
199500K .......... .......... .......... .......... .......... 41% 11.2M 27s
199550K .......... .......... .......... .......... .......... 41% 11.6M 27s
199600K .......... .......... .......... .......... .......... 41% 21.1M 27s
199650K .......... .......... .......... .......... .......... 41% 25.4M 27s
199700K .......... .......... .......... .......... .......... 41% 27.7M 27s
199750K .......... .......... .......... .......... .......... 41% 27.0M 27s
199800K .......... .......... .......... .......... .......... 41% 28.6M 27s
199850K .......... .......... .......... .......... .......... 41% 25.2M 27s
199900K .......... .......... .......... .......... .......... 41% 29.7M 27s
199950K .......... .......... .......... .......... .......... 41% 27.5M 27s
200000K .......... .......... .......... .......... .......... 41% 27.4M 27s
200050K .......... .......... .......... .......... .......... 41% 28.4M 27s
200100K .......... .......... .......... .......... .......... 41% 16.1M 27s
200150K .......... .......... .......... .......... .......... 41% 69.0M 27s
200200K .......... .......... .......... .......... .......... 41% 12.8M 27s
200250K .......... .......... .......... .......... .......... 41% 13.0M 27s
200300K .......... .......... .......... .......... .......... 41% 7.47M 27s
200350K .......... .......... .......... .......... .......... 41% 8.40M 27s
200400K .......... .......... .......... .......... .......... 41% 8.06M 27s
200450K .......... .......... .......... .......... .......... 41% 7.31M 27s
200500K .......... .......... .......... .......... .......... 41% 6.78M 27s
200550K .......... .......... .......... .......... .......... 41% 6.24M 27s
200600K .......... .......... .......... .......... .......... 41% 8.19M 27s
200650K .......... .......... .......... .......... .......... 41% 12.3M 27s
200700K .......... .......... .......... .......... .......... 41% 9.53M 27s
200750K .......... .......... .......... .......... .......... 41% 11.5M 27s
200800K .......... .......... .......... .......... .......... 41% 8.41M 27s
200850K .......... .......... .......... .......... .......... 41% 10.5M 27s
200900K .......... .......... .......... .......... .......... 41% 9.97M 27s
200950K .......... .......... .......... .......... .......... 41% 6.48M 27s
201000K .......... .......... .......... .......... .......... 41% 8.38M 26s
201050K .......... .......... .......... .......... .......... 41% 7.02M 26s
201100K .......... .......... .......... .......... .......... 41% 7.24M 26s
201150K .......... .......... .......... .......... .......... 41% 6.45M 26s
201200K .......... .......... .......... .......... .......... 41% 5.20M 26s
201250K .......... .......... .......... .......... .......... 41% 5.28M 26s
201300K .......... .......... .......... .......... .......... 41% 4.88M 27s
201350K .......... .......... .......... .......... .......... 41% 6.85M 26s
201400K .......... .......... .......... .......... .......... 41% 8.34M 26s
201450K .......... .......... .......... .......... .......... 41% 6.95M 26s
201500K .......... .......... .......... .......... .......... 41% 7.14M 26s
201550K .......... .......... .......... .......... .......... 41% 9.45M 26s
201600K .......... .......... .......... .......... .......... 41% 6.81M 26s
201650K .......... .......... .......... .......... .......... 41% 8.25M 26s
201700K .......... .......... .......... .......... .......... 41% 7.28M 26s
201750K .......... .......... .......... .......... .......... 41% 7.27M 26s
201800K .......... .......... .......... .......... .......... 41% 27.5M 26s
201850K .......... .......... .......... .......... .......... 42% 9.74M 26s
201900K .......... .......... .......... .......... .......... 42% 11.1M 26s
201950K .......... .......... .......... .......... .......... 42% 8.13M 26s
202000K .......... .......... .......... .......... .......... 42% 9.84M 26s
202050K .......... .......... .......... .......... .......... 42% 9.55M 26s
202100K .......... .......... .......... .......... .......... 42% 6.63M 26s
202150K .......... .......... .......... .......... .......... 42% 9.72M 26s
202200K .......... .......... .......... .......... .......... 42% 4.93M 26s
202250K .......... .......... .......... .......... .......... 42% 4.74M 26s
202300K .......... .......... .......... .......... .......... 42% 6.09M 26s
202350K .......... .......... .......... .......... .......... 42% 3.97M 26s
202400K .......... .......... .......... .......... .......... 42% 7.27M 26s
202450K .......... .......... .......... .......... .......... 42% 6.78M 26s
202500K .......... .......... .......... .......... .......... 42% 8.59M 26s
202550K .......... .......... .......... .......... .......... 42% 12.3M 26s
202600K .......... .......... .......... .......... .......... 42% 7.61M 26s
202650K .......... .......... .......... .......... .......... 42% 7.48M 26s
202700K .......... .......... .......... .......... .......... 42% 8.13M 26s
202750K .......... .......... .......... .......... .......... 42% 8.32M 26s
202800K .......... .......... .......... .......... .......... 42% 6.85M 26s
202850K .......... .......... .......... .......... .......... 42% 6.08M 26s
202900K .......... .......... .......... .......... .......... 42% 5.50M 26s
202950K .......... .......... .......... .......... .......... 42% 5.43M 26s
203000K .......... .......... .......... .......... .......... 42% 5.67M 26s
203050K .......... .......... .......... .......... .......... 42% 6.67M 26s
203100K .......... .......... .......... .......... .......... 42% 5.57M 26s
203150K .......... .......... .......... .......... .......... 42% 6.24M 26s
203200K .......... .......... .......... .......... .......... 42% 7.86M 26s
203250K .......... .......... .......... .......... .......... 42% 7.27M 26s
203300K .......... .......... .......... .......... .......... 42% 8.43M 26s
203350K .......... .......... .......... .......... .......... 42% 5.17M 26s
203400K .......... .......... .......... .......... .......... 42% 6.16M 26s
203450K .......... .......... .......... .......... .......... 42% 6.41M 26s
203500K .......... .......... .......... .......... .......... 42% 8.47M 26s
203550K .......... .......... .......... .......... .......... 42% 7.79M 26s
203600K .......... .......... .......... .......... .......... 42% 5.00M 26s
203650K .......... .......... .......... .......... .......... 42% 10.9M 26s
203700K .......... .......... .......... .......... .......... 42% 8.92M 26s
203750K .......... .......... .......... .......... .......... 42% 10.5M 26s
203800K .......... .......... .......... .......... .......... 42% 11.3M 26s
203850K .......... .......... .......... .......... .......... 42% 7.68M 26s
203900K .......... .......... .......... .......... .......... 42% 12.1M 26s
203950K .......... .......... .......... .......... .......... 42% 9.48M 26s
204000K .......... .......... .......... .......... .......... 42% 12.6M 26s
204050K .......... .......... .......... .......... .......... 42% 17.1M 26s
204100K .......... .......... .......... .......... .......... 42% 36.1M 26s
204150K .......... .......... .......... .......... .......... 42% 20.3M 26s
204200K .......... .......... .......... .......... .......... 42% 20.6M 26s
204250K .......... .......... .......... .......... .......... 42% 16.1M 26s
204300K .......... .......... .......... .......... .......... 42% 11.1M 26s
204350K .......... .......... .......... .......... .......... 42% 6.21M 26s
204400K .......... .......... .......... .......... .......... 42% 8.43M 26s
204450K .......... .......... .......... .......... .......... 42% 5.60M 26s
204500K .......... .......... .......... .......... .......... 42% 6.28M 26s
204550K .......... .......... .......... .......... .......... 42% 3.48M 26s
204600K .......... .......... .......... .......... .......... 42% 2.33M 26s
204650K .......... .......... .......... .......... .......... 42% 8.31M 26s
204700K .......... .......... .......... .......... .......... 42% 25.0M 26s
204750K .......... .......... .......... .......... .......... 42% 13.3M 26s
204800K .......... .......... .......... .......... .......... 42% 81.1M 26s
204850K .......... .......... .......... .......... .......... 42% 11.4M 26s
204900K .......... .......... .......... .......... .......... 42% 77.9M 26s
204950K .......... .......... .......... .......... .......... 42% 13.1M 26s
205000K .......... .......... .......... .......... .......... 42% 13.3M 26s
205050K .......... .......... .......... .......... .......... 42% 10.8M 26s
205100K .......... .......... .......... .......... .......... 42% 15.7M 26s
205150K .......... .......... .......... .......... .......... 42% 18.7M 26s
205200K .......... .......... .......... .......... .......... 42% 10.2M 26s
205250K .......... .......... .......... .......... .......... 42% 9.91M 26s
205300K .......... .......... .......... .......... .......... 42% 11.9M 26s
205350K .......... .......... .......... .......... .......... 42% 7.71M 26s
205400K .......... .......... .......... .......... .......... 42% 7.93M 26s
205450K .......... .......... .......... .......... .......... 42% 8.62M 26s
205500K .......... .......... .......... .......... .......... 42% 9.97M 26s
205550K .......... .......... .......... .......... .......... 42% 10.0M 26s
205600K .......... .......... .......... .......... .......... 42% 9.25M 26s
205650K .......... .......... .......... .......... .......... 42% 11.3M 26s
205700K .......... .......... .......... .......... .......... 42% 10.5M 26s
205750K .......... .......... .......... .......... .......... 42% 8.83M 26s
205800K .......... .......... .......... .......... .......... 42% 13.0M 26s
205850K .......... .......... .......... .......... .......... 42% 10.1M 26s
205900K .......... .......... .......... .......... .......... 42% 12.2M 26s
205950K .......... .......... .......... .......... .......... 42% 10.0M 26s
206000K .......... .......... .......... .......... .......... 42% 10.2M 26s
206050K .......... .......... .......... .......... .......... 42% 9.92M 26s
206100K .......... .......... .......... .......... .......... 42% 7.76M 26s
206150K .......... .......... .......... .......... .......... 42% 11.6M 26s
206200K .......... .......... .......... .......... .......... 42% 7.58M 26s
206250K .......... .......... .......... .......... .......... 42% 12.2M 26s
206300K .......... .......... .......... .......... .......... 42% 7.95M 26s
206350K .......... .......... .......... .......... .......... 42% 6.77M 26s
206400K .......... .......... .......... .......... .......... 42% 8.33M 26s
206450K .......... .......... .......... .......... .......... 42% 7.21M 26s
206500K .......... .......... .......... .......... .......... 42% 13.3M 26s
206550K .......... .......... .......... .......... .......... 42% 18.8M 26s
206600K .......... .......... .......... .......... .......... 42% 19.3M 26s
206650K .......... .......... .......... .......... .......... 43% 14.2M 26s
206700K .......... .......... .......... .......... .......... 43% 9.90M 26s
206750K .......... .......... .......... .......... .......... 43% 10.1M 26s
206800K .......... .......... .......... .......... .......... 43% 14.6M 26s
206850K .......... .......... .......... .......... .......... 43% 11.2M 26s
206900K .......... .......... .......... .......... .......... 43% 10.7M 26s
206950K .......... .......... .......... .......... .......... 43% 5.92M 26s
207000K .......... .......... .......... .......... .......... 43% 12.7M 26s
207050K .......... .......... .......... .......... .......... 43% 7.21M 26s
207100K .......... .......... .......... .......... .......... 43% 9.72M 26s
207150K .......... .......... .......... .......... .......... 43% 9.08M 26s
207200K .......... .......... .......... .......... .......... 43% 7.21M 26s
207250K .......... .......... .......... .......... .......... 43% 9.80M 26s
207300K .......... .......... .......... .......... .......... 43% 6.24M 26s
207350K .......... .......... .......... .......... .......... 43% 7.37M 26s
207400K .......... .......... .......... .......... .......... 43% 9.40M 26s
207450K .......... .......... .......... .......... .......... 43% 9.58M 26s
207500K .......... .......... .......... .......... .......... 43% 9.17M 26s
207550K .......... .......... .......... .......... .......... 43% 12.2M 26s
207600K .......... .......... .......... .......... .......... 43% 11.4M 26s
207650K .......... .......... .......... .......... .......... 43% 9.36M 26s
207700K .......... .......... .......... .......... .......... 43% 9.24M 26s
207750K .......... .......... .......... .......... .......... 43% 12.6M 26s
207800K .......... .......... .......... .......... .......... 43% 10.1M 26s
207850K .......... .......... .......... .......... .......... 43% 7.81M 26s
207900K .......... .......... .......... .......... .......... 43% 9.16M 26s
207950K .......... .......... .......... .......... .......... 43% 7.15M 26s
208000K .......... .......... .......... .......... .......... 43% 10.3M 26s
208050K .......... .......... .......... .......... .......... 43% 13.7M 26s
208100K .......... .......... .......... .......... .......... 43% 7.25M 26s
208150K .......... .......... .......... .......... .......... 43% 10.8M 26s
208200K .......... .......... .......... .......... .......... 43% 8.50M 26s
208250K .......... .......... .......... .......... .......... 43% 4.79M 26s
208300K .......... .......... .......... .......... .......... 43% 9.99M 26s
208350K .......... .......... .......... .......... .......... 43% 5.47M 26s
208400K .......... .......... .......... .......... .......... 43% 6.88M 26s
208450K .......... .......... .......... .......... .......... 43% 4.62M 26s
208500K .......... .......... .......... .......... .......... 43% 5.44M 26s
208550K .......... .......... .......... .......... .......... 43% 7.55M 26s
208600K .......... .......... .......... .......... .......... 43% 7.88M 26s
208650K .......... .......... .......... .......... .......... 43% 6.94M 26s
208700K .......... .......... .......... .......... .......... 43% 5.66M 26s
208750K .......... .......... .......... .......... .......... 43% 6.19M 26s
208800K .......... .......... .......... .......... .......... 43% 6.17M 26s
208850K .......... .......... .......... .......... .......... 43% 5.29M 26s
208900K .......... .......... .......... .......... .......... 43% 5.83M 26s
208950K .......... .......... .......... .......... .......... 43% 5.44M 26s
209000K .......... .......... .......... .......... .......... 43% 7.32M 26s
209050K .......... .......... .......... .......... .......... 43% 5.12M 26s
209100K .......... .......... .......... .......... .......... 43% 4.67M 26s
209150K .......... .......... .......... .......... .......... 43% 8.21M 26s
209200K .......... .......... .......... .......... .......... 43% 6.85M 26s
209250K .......... .......... .......... .......... .......... 43% 11.5M 26s
209300K .......... .......... .......... .......... .......... 43% 8.83M 26s
209350K .......... .......... .......... .......... .......... 43% 8.05M 26s
209400K .......... .......... .......... .......... .......... 43% 12.2M 26s
209450K .......... .......... .......... .......... .......... 43% 10.5M 26s
209500K .......... .......... .......... .......... .......... 43% 12.7M 26s
209550K .......... .......... .......... .......... .......... 43% 8.77M 26s
209600K .......... .......... .......... .......... .......... 43% 7.44M 26s
209650K .......... .......... .......... .......... .......... 43% 13.5M 26s
209700K .......... .......... .......... .......... .......... 43% 10.2M 26s
209750K .......... .......... .......... .......... .......... 43% 10.6M 26s
209800K .......... .......... .......... .......... .......... 43% 9.54M 26s
209850K .......... .......... .......... .......... .......... 43% 6.62M 26s
209900K .......... .......... .......... .......... .......... 43% 10.8M 26s
209950K .......... .......... .......... .......... .......... 43% 7.26M 26s
210000K .......... .......... .......... .......... .......... 43% 9.01M 26s
210050K .......... .......... .......... .......... .......... 43% 12.3M 26s
210100K .......... .......... .......... .......... .......... 43% 7.79M 26s
210150K .......... .......... .......... .......... .......... 43% 8.28M 26s
210200K .......... .......... .......... .......... .......... 43% 6.97M 26s
210250K .......... .......... .......... .......... .......... 43% 10.0M 26s
210300K .......... .......... .......... .......... .......... 43% 15.8M 26s
210350K .......... .......... .......... .......... .......... 43% 20.5M 26s
210400K .......... .......... .......... .......... .......... 43% 42.0M 26s
210450K .......... .......... .......... .......... .......... 43% 15.1M 26s
210500K .......... .......... .......... .......... .......... 43% 10.8M 26s
210550K .......... .......... .......... .......... .......... 43% 12.5M 26s
210600K .......... .......... .......... .......... .......... 43% 6.88M 26s
210650K .......... .......... .......... .......... .......... 43% 9.45M 26s
210700K .......... .......... .......... .......... .......... 43% 6.63M 26s
210750K .......... .......... .......... .......... .......... 43% 7.75M 26s
210800K .......... .......... .......... .......... .......... 43% 8.11M 26s
210850K .......... .......... .......... .......... .......... 43% 8.22M 26s
210900K .......... .......... .......... .......... .......... 43% 16.7M 26s
210950K .......... .......... .......... .......... .......... 43% 27.0M 26s
211000K .......... .......... .......... .......... .......... 43% 17.3M 26s
211050K .......... .......... .......... .......... .......... 43% 30.0M 26s
211100K .......... .......... .......... .......... .......... 43% 14.0M 26s
211150K .......... .......... .......... .......... .......... 43% 22.1M 26s
211200K .......... .......... .......... .......... .......... 43% 15.1M 26s
211250K .......... .......... .......... .......... .......... 43% 11.5M 26s
211300K .......... .......... .......... .......... .......... 43% 19.8M 26s
211350K .......... .......... .......... .......... .......... 43% 11.2M 26s
211400K .......... .......... .......... .......... .......... 43% 14.4M 26s
211450K .......... .......... .......... .......... .......... 44% 9.53M 26s
211500K .......... .......... .......... .......... .......... 44% 11.9M 26s
211550K .......... .......... .......... .......... .......... 44% 11.7M 26s
211600K .......... .......... .......... .......... .......... 44% 11.7M 26s
211650K .......... .......... .......... .......... .......... 44% 12.3M 26s
211700K .......... .......... .......... .......... .......... 44% 9.83M 26s
211750K .......... .......... .......... .......... .......... 44% 22.1M 26s
211800K .......... .......... .......... .......... .......... 44% 13.4M 26s
211850K .......... .......... .......... .......... .......... 44% 12.7M 26s
211900K .......... .......... .......... .......... .......... 44% 13.0M 26s
211950K .......... .......... .......... .......... .......... 44% 11.4M 26s
212000K .......... .......... .......... .......... .......... 44% 7.66M 26s
212050K .......... .......... .......... .......... .......... 44% 10.8M 26s
212100K .......... .......... .......... .......... .......... 44% 6.86M 26s
212150K .......... .......... .......... .......... .......... 44% 11.4M 26s
212200K .......... .......... .......... .......... .......... 44% 9.01M 26s
212250K .......... .......... .......... .......... .......... 44% 8.49M 26s
212300K .......... .......... .......... .......... .......... 44% 7.05M 26s
212350K .......... .......... .......... .......... .......... 44% 5.68M 26s
212400K .......... .......... .......... .......... .......... 44% 4.11M 26s
212450K .......... .......... .......... .......... .......... 44% 4.50M 26s
212500K .......... .......... .......... .......... .......... 44% 14.3M 26s
212550K .......... .......... .......... .......... .......... 44% 13.8M 26s
212600K .......... .......... .......... .......... .......... 44% 11.2M 26s
212650K .......... .......... .......... .......... .......... 44% 20.5M 26s
212700K .......... .......... .......... .......... .......... 44% 10.2M 26s
212750K .......... .......... .......... .......... .......... 44% 15.2M 26s
212800K .......... .......... .......... .......... .......... 44% 14.6M 26s
212850K .......... .......... .......... .......... .......... 44% 10.2M 26s
212900K .......... .......... .......... .......... .......... 44% 10.5M 26s
212950K .......... .......... .......... .......... .......... 44% 9.47M 26s
213000K .......... .......... .......... .......... .......... 44% 8.41M 26s
213050K .......... .......... .......... .......... .......... 44% 11.1M 26s
213100K .......... .......... .......... .......... .......... 44% 9.08M 26s
213150K .......... .......... .......... .......... .......... 44% 8.88M 26s
213200K .......... .......... .......... .......... .......... 44% 7.03M 26s
213250K .......... .......... .......... .......... .......... 44% 7.94M 26s
213300K .......... .......... .......... .......... .......... 44% 7.58M 26s
213350K .......... .......... .......... .......... .......... 44% 7.24M 26s
213400K .......... .......... .......... .......... .......... 44% 8.38M 26s
213450K .......... .......... .......... .......... .......... 44% 12.6M 26s
213500K .......... .......... .......... .......... .......... 44% 11.3M 26s
213550K .......... .......... .......... .......... .......... 44% 16.3M 26s
213600K .......... .......... .......... .......... .......... 44% 11.6M 26s
213650K .......... .......... .......... .......... .......... 44% 9.98M 26s
213700K .......... .......... .......... .......... .......... 44% 8.34M 26s
213750K .......... .......... .......... .......... .......... 44% 10.4M 26s
213800K .......... .......... .......... .......... .......... 44% 9.92M 26s
213850K .......... .......... .......... .......... .......... 44% 9.22M 26s
213900K .......... .......... .......... .......... .......... 44% 9.48M 26s
213950K .......... .......... .......... .......... .......... 44% 5.44M 26s
214000K .......... .......... .......... .......... .......... 44% 8.80M 26s
214050K .......... .......... .......... .......... .......... 44% 16.8M 26s
214100K .......... .......... .......... .......... .......... 44% 22.2M 26s
214150K .......... .......... .......... .......... .......... 44% 21.0M 26s
214200K .......... .......... .......... .......... .......... 44% 22.9M 26s
214250K .......... .......... .......... .......... .......... 44% 13.8M 26s
214300K .......... .......... .......... .......... .......... 44% 24.3M 26s
214350K .......... .......... .......... .......... .......... 44% 9.66M 26s
214400K .......... .......... .......... .......... .......... 44% 7.69M 26s
214450K .......... .......... .......... .......... .......... 44% 9.67M 25s
214500K .......... .......... .......... .......... .......... 44% 11.9M 25s
214550K .......... .......... .......... .......... .......... 44% 9.49M 25s
214600K .......... .......... .......... .......... .......... 44% 10.9M 25s
214650K .......... .......... .......... .......... .......... 44% 11.2M 25s
214700K .......... .......... .......... .......... .......... 44% 7.45M 25s
214750K .......... .......... .......... .......... .......... 44% 7.96M 25s
214800K .......... .......... .......... .......... .......... 44% 8.68M 25s
214850K .......... .......... .......... .......... .......... 44% 4.30M 25s
214900K .......... .......... .......... .......... .......... 44% 5.92M 25s
214950K .......... .......... .......... .......... .......... 44% 4.69M 25s
215000K .......... .......... .......... .......... .......... 44% 9.08M 25s
215050K .......... .......... .......... .......... .......... 44% 9.29M 25s
215100K .......... .......... .......... .......... .......... 44% 7.32M 25s
215150K .......... .......... .......... .......... .......... 44% 8.12M 25s
215200K .......... .......... .......... .......... .......... 44% 10.9M 25s
215250K .......... .......... .......... .......... .......... 44% 10.9M 25s
215300K .......... .......... .......... .......... .......... 44% 9.79M 25s
215350K .......... .......... .......... .......... .......... 44% 8.91M 25s
215400K .......... .......... .......... .......... .......... 44% 16.9M 25s
215450K .......... .......... .......... .......... .......... 44% 10.3M 25s
215500K .......... .......... .......... .......... .......... 44% 16.4M 25s
215550K .......... .......... .......... .......... .......... 44% 15.7M 25s
215600K .......... .......... .......... .......... .......... 44% 12.7M 25s
215650K .......... .......... .......... .......... .......... 44% 13.6M 25s
215700K .......... .......... .......... .......... .......... 44% 8.83M 25s
215750K .......... .......... .......... .......... .......... 44% 9.27M 25s
215800K .......... .......... .......... .......... .......... 44% 10.7M 25s
215850K .......... .......... .......... .......... .......... 44% 8.46M 25s
215900K .......... .......... .......... .......... .......... 44% 12.0M 25s
215950K .......... .......... .......... .......... .......... 44% 44.5M 25s
216000K .......... .......... .......... .......... .......... 44% 14.4M 25s
216050K .......... .......... .......... .......... .......... 44% 14.5M 25s
216100K .......... .......... .......... .......... .......... 44% 12.6M 25s
216150K .......... .......... .......... .......... .......... 44% 14.0M 25s
216200K .......... .......... .......... .......... .......... 44% 14.1M 25s
216250K .......... .......... .......... .......... .......... 45% 11.1M 25s
216300K .......... .......... .......... .......... .......... 45% 9.56M 25s
216350K .......... .......... .......... .......... .......... 45% 11.4M 25s
216400K .......... .......... .......... .......... .......... 45% 10.9M 25s
216450K .......... .......... .......... .......... .......... 45% 8.39M 25s
216500K .......... .......... .......... .......... .......... 45% 13.3M 25s
216550K .......... .......... .......... .......... .......... 45% 9.30M 25s
216600K .......... .......... .......... .......... .......... 45% 9.10M 25s
216650K .......... .......... .......... .......... .......... 45% 12.0M 25s
216700K .......... .......... .......... .......... .......... 45% 17.4M 25s
216750K .......... .......... .......... .......... .......... 45% 31.7M 25s
216800K .......... .......... .......... .......... .......... 45% 31.8M 25s
216850K .......... .......... .......... .......... .......... 45% 25.8M 25s
216900K .......... .......... .......... .......... .......... 45% 36.2M 25s
216950K .......... .......... .......... .......... .......... 45% 18.8M 25s
217000K .......... .......... .......... .......... .......... 45% 70.6M 25s
217050K .......... .......... .......... .......... .......... 45% 21.1M 25s
217100K .......... .......... .......... .......... .......... 45% 15.5M 25s
217150K .......... .......... .......... .......... .......... 45% 37.9M 25s
217200K .......... .......... .......... .......... .......... 45% 17.1M 25s
217250K .......... .......... .......... .......... .......... 45% 17.2M 25s
217300K .......... .......... .......... .......... .......... 45% 13.3M 25s
217350K .......... .......... .......... .......... .......... 45% 13.3M 25s
217400K .......... .......... .......... .......... .......... 45% 14.0M 25s
217450K .......... .......... .......... .......... .......... 45% 12.2M 25s
217500K .......... .......... .......... .......... .......... 45% 18.2M 25s
217550K .......... .......... .......... .......... .......... 45% 13.0M 25s
217600K .......... .......... .......... .......... .......... 45% 11.5M 25s
217650K .......... .......... .......... .......... .......... 45% 11.7M 25s
217700K .......... .......... .......... .......... .......... 45% 12.0M 25s
217750K .......... .......... .......... .......... .......... 45% 11.4M 25s
217800K .......... .......... .......... .......... .......... 45% 15.1M 25s
217850K .......... .......... .......... .......... .......... 45% 7.93M 25s
217900K .......... .......... .......... .......... .......... 45% 20.0M 25s
217950K .......... .......... .......... .......... .......... 45% 11.0M 25s
218000K .......... .......... .......... .......... .......... 45% 10.3M 25s
218050K .......... .......... .......... .......... .......... 45% 9.23M 25s
218100K .......... .......... .......... .......... .......... 45% 9.33M 25s
218150K .......... .......... .......... .......... .......... 45% 7.40M 25s
218200K .......... .......... .......... .......... .......... 45% 7.46M 25s
218250K .......... .......... .......... .......... .......... 45% 6.04M 25s
218300K .......... .......... .......... .......... .......... 45% 5.92M 25s
218350K .......... .......... .......... .......... .......... 45% 4.58M 25s
218400K .......... .......... .......... .......... .......... 45% 5.04M 25s
218450K .......... .......... .......... .......... .......... 45% 5.19M 25s
218500K .......... .......... .......... .......... .......... 45% 8.63M 25s
218550K .......... .......... .......... .......... .......... 45% 7.29M 25s
218600K .......... .......... .......... .......... .......... 45% 5.10M 25s
218650K .......... .......... .......... .......... .......... 45% 6.18M 25s
218700K .......... .......... .......... .......... .......... 45% 6.50M 25s
218750K .......... .......... .......... .......... .......... 45% 9.77M 25s
218800K .......... .......... .......... .......... .......... 45% 7.89M 25s
218850K .......... .......... .......... .......... .......... 45% 7.18M 25s
218900K .......... .......... .......... .......... .......... 45% 7.87M 25s
218950K .......... .......... .......... .......... .......... 45% 7.50M 25s
219000K .......... .......... .......... .......... .......... 45% 8.09M 25s
219050K .......... .......... .......... .......... .......... 45% 10.2M 25s
219100K .......... .......... .......... .......... .......... 45% 8.90M 25s
219150K .......... .......... .......... .......... .......... 45% 8.06M 25s
219200K .......... .......... .......... .......... .......... 45% 8.76M 25s
219250K .......... .......... .......... .......... .......... 45% 12.1M 25s
219300K .......... .......... .......... .......... .......... 45% 5.91M 25s
219350K .......... .......... .......... .......... .......... 45% 6.12M 25s
219400K .......... .......... .......... .......... .......... 45% 10.3M 25s
219450K .......... .......... .......... .......... .......... 45% 6.38M 25s
219500K .......... .......... .......... .......... .......... 45% 5.24M 25s
219550K .......... .......... .......... .......... .......... 45% 4.63M 25s
219600K .......... .......... .......... .......... .......... 45% 2.28M 25s
219650K .......... .......... .......... .......... .......... 45% 4.39M 25s
219700K .......... .......... .......... .......... .......... 45% 5.31M 25s
219750K .......... .......... .......... .......... .......... 45% 19.4M 25s
219800K .......... .......... .......... .......... .......... 45% 17.3M 25s
219850K .......... .......... .......... .......... .......... 45% 12.9M 25s
219900K .......... .......... .......... .......... .......... 45% 14.1M 25s
219950K .......... .......... .......... .......... .......... 45% 11.7M 25s
220000K .......... .......... .......... .......... .......... 45% 13.1M 25s
220050K .......... .......... .......... .......... .......... 45% 9.88M 25s
220100K .......... .......... .......... .......... .......... 45% 11.4M 25s
220150K .......... .......... .......... .......... .......... 45% 10.8M 25s
220200K .......... .......... .......... .......... .......... 45% 11.5M 25s
220250K .......... .......... .......... .......... .......... 45% 14.7M 25s
220300K .......... .......... .......... .......... .......... 45% 10.8M 25s
220350K .......... .......... .......... .......... .......... 45% 10.5M 25s
220400K .......... .......... .......... .......... .......... 45% 11.5M 25s
220450K .......... .......... .......... .......... .......... 45% 9.40M 25s
220500K .......... .......... .......... .......... .......... 45% 10.6M 25s
220550K .......... .......... .......... .......... .......... 45% 10.1M 25s
220600K .......... .......... .......... .......... .......... 45% 8.99M 25s
220650K .......... .......... .......... .......... .......... 45% 8.83M 25s
220700K .......... .......... .......... .......... .......... 45% 6.32M 25s
220750K .......... .......... .......... .......... .......... 45% 10.7M 25s
220800K .......... .......... .......... .......... .......... 45% 15.0M 25s
220850K .......... .......... .......... .......... .......... 45% 10.6M 25s
220900K .......... .......... .......... .......... .......... 45% 80.7M 25s
220950K .......... .......... .......... .......... .......... 45% 13.4M 25s
221000K .......... .......... .......... .......... .......... 45% 18.6M 25s
221050K .......... .......... .......... .......... .......... 46% 15.7M 25s
221100K .......... .......... .......... .......... .......... 46% 12.7M 25s
221150K .......... .......... .......... .......... .......... 46% 14.0M 25s
221200K .......... .......... .......... .......... .......... 46% 8.37M 25s
221250K .......... .......... .......... .......... .......... 46% 10.8M 25s
221300K .......... .......... .......... .......... .......... 46% 12.6M 25s
221350K .......... .......... .......... .......... .......... 46% 10.0M 25s
221400K .......... .......... .......... .......... .......... 46% 9.29M 25s
221450K .......... .......... .......... .......... .......... 46% 8.77M 25s
221500K .......... .......... .......... .......... .......... 46% 13.2M 25s
221550K .......... .......... .......... .......... .......... 46% 12.6M 25s
221600K .......... .......... .......... .......... .......... 46% 8.80M 25s
221650K .......... .......... .......... .......... .......... 46% 7.94M 25s
221700K .......... .......... .......... .......... .......... 46% 8.20M 25s
221750K .......... .......... .......... .......... .......... 46% 5.78M 25s
221800K .......... .......... .......... .......... .......... 46% 7.62M 25s
221850K .......... .......... .......... .......... .......... 46% 6.88M 25s
221900K .......... .......... .......... .......... .......... 46% 9.19M 25s
221950K .......... .......... .......... .......... .......... 46% 13.3M 25s
222000K .......... .......... .......... .......... .......... 46% 10.8M 25s
222050K .......... .......... .......... .......... .......... 46% 11.1M 25s
222100K .......... .......... .......... .......... .......... 46% 8.72M 25s
222150K .......... .......... .......... .......... .......... 46% 10.7M 25s
222200K .......... .......... .......... .......... .......... 46% 8.48M 25s
222250K .......... .......... .......... .......... .......... 46% 8.36M 25s
222300K .......... .......... .......... .......... .......... 46% 14.8M 25s
222350K .......... .......... .......... .......... .......... 46% 15.1M 25s
222400K .......... .......... .......... .......... .......... 46% 31.2M 25s
222450K .......... .......... .......... .......... .......... 46% 27.7M 25s
222500K .......... .......... .......... .......... .......... 46% 31.9M 25s
222550K .......... .......... .......... .......... .......... 46% 35.2M 25s
222600K .......... .......... .......... .......... .......... 46% 26.1M 25s
222650K .......... .......... .......... .......... .......... 46% 34.1M 25s
222700K .......... .......... .......... .......... .......... 46% 28.3M 25s
222750K .......... .......... .......... .......... .......... 46% 32.9M 25s
222800K .......... .......... .......... .......... .......... 46% 34.8M 25s
222850K .......... .......... .......... .......... .......... 46% 21.6M 25s
222900K .......... .......... .......... .......... .......... 46% 24.2M 25s
222950K .......... .......... .......... .......... .......... 46% 25.0M 25s
223000K .......... .......... .......... .......... .......... 46% 21.4M 25s
223050K .......... .......... .......... .......... .......... 46% 20.3M 25s
223100K .......... .......... .......... .......... .......... 46% 16.6M 25s
223150K .......... .......... .......... .......... .......... 46% 19.5M 25s
223200K .......... .......... .......... .......... .......... 46% 18.5M 25s
223250K .......... .......... .......... .......... .......... 46% 18.7M 25s
223300K .......... .......... .......... .......... .......... 46% 20.7M 25s
223350K .......... .......... .......... .......... .......... 46% 17.2M 25s
223400K .......... .......... .......... .......... .......... 46% 22.9M 25s
223450K .......... .......... .......... .......... .......... 46% 22.6M 25s
223500K .......... .......... .......... .......... .......... 46% 18.6M 25s
223550K .......... .......... .......... .......... .......... 46% 19.3M 25s
223600K .......... .......... .......... .......... .......... 46% 13.0M 25s
223650K .......... .......... .......... .......... .......... 46% 11.4M 25s
223700K .......... .......... .......... .......... .......... 46% 17.1M 25s
223750K .......... .......... .......... .......... .......... 46% 8.99M 25s
223800K .......... .......... .......... .......... .......... 46% 21.3M 25s
223850K .......... .......... .......... .......... .......... 46% 13.1M 25s
223900K .......... .......... .......... .......... .......... 46% 11.8M 25s
223950K .......... .......... .......... .......... .......... 46% 9.10M 25s
224000K .......... .......... .......... .......... .......... 46% 8.28M 25s
224050K .......... .......... .......... .......... .......... 46% 12.1M 25s
224100K .......... .......... .......... .......... .......... 46% 8.07M 25s
224150K .......... .......... .......... .......... .......... 46% 13.1M 25s
224200K .......... .......... .......... .......... .......... 46% 8.39M 25s
224250K .......... .......... .......... .......... .......... 46% 17.1M 25s
224300K .......... .......... .......... .......... .......... 46% 10.7M 25s
224350K .......... .......... .......... .......... .......... 46% 6.60M 25s
224400K .......... .......... .......... .......... .......... 46% 9.43M 25s
224450K .......... .......... .......... .......... .......... 46% 7.73M 25s
224500K .......... .......... .......... .......... .......... 46% 8.09M 25s
224550K .......... .......... .......... .......... .......... 46% 7.45M 25s
224600K .......... .......... .......... .......... .......... 46% 5.69M 25s
224650K .......... .......... .......... .......... .......... 46% 11.0M 25s
224700K .......... .......... .......... .......... .......... 46% 8.52M 25s
224750K .......... .......... .......... .......... .......... 46% 11.1M 24s
224800K .......... .......... .......... .......... .......... 46% 9.06M 24s
224850K .......... .......... .......... .......... .......... 46% 9.11M 24s
224900K .......... .......... .......... .......... .......... 46% 11.6M 24s
224950K .......... .......... .......... .......... .......... 46% 8.15M 24s
225000K .......... .......... .......... .......... .......... 46% 17.0M 24s
225050K .......... .......... .......... .......... .......... 46% 30.0M 24s
225100K .......... .......... .......... .......... .......... 46% 31.9M 24s
225150K .......... .......... .......... .......... .......... 46% 23.2M 24s
225200K .......... .......... .......... .......... .......... 46% 7.79M 24s
225250K .......... .......... .......... .......... .......... 46% 8.32M 24s
225300K .......... .......... .......... .......... .......... 46% 9.12M 24s
225350K .......... .......... .......... .......... .......... 46% 8.87M 24s
225400K .......... .......... .......... .......... .......... 46% 16.5M 24s
225450K .......... .......... .......... .......... .......... 46% 9.07M 24s
225500K .......... .......... .......... .......... .......... 46% 12.4M 24s
225550K .......... .......... .......... .......... .......... 46% 8.47M 24s
225600K .......... .......... .......... .......... .......... 46% 5.45M 24s
225650K .......... .......... .......... .......... .......... 46% 6.51M 24s
225700K .......... .......... .......... .......... .......... 46% 4.34M 24s
225750K .......... .......... .......... .......... .......... 46% 6.24M 24s
225800K .......... .......... .......... .......... .......... 46% 3.86M 24s
225850K .......... .......... .......... .......... .......... 47% 3.45M 24s
225900K .......... .......... .......... .......... .......... 47% 4.21M 24s
225950K .......... .......... .......... .......... .......... 47% 8.96M 24s
226000K .......... .......... .......... .......... .......... 47% 16.1M 24s
226050K .......... .......... .......... .......... .......... 47% 10.5M 24s
226100K .......... .......... .......... .......... .......... 47% 10.6M 24s
226150K .......... .......... .......... .......... .......... 47% 9.16M 24s
226200K .......... .......... .......... .......... .......... 47% 7.81M 24s
226250K .......... .......... .......... .......... .......... 47% 5.86M 24s
226300K .......... .......... .......... .......... .......... 47% 7.16M 24s
226350K .......... .......... .......... .......... .......... 47% 6.70M 24s
226400K .......... .......... .......... .......... .......... 47% 7.40M 24s
226450K .......... .......... .......... .......... .......... 47% 5.37M 24s
226500K .......... .......... .......... .......... .......... 47% 5.57M 24s
226550K .......... .......... .......... .......... .......... 47% 6.84M 24s
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226650K .......... .......... .......... .......... .......... 47% 5.77M 24s
226700K .......... .......... .......... .......... .......... 47% 5.40M 24s
226750K .......... .......... .......... .......... .......... 47% 5.20M 24s
226800K .......... .......... .......... .......... .......... 47% 6.69M 24s
226850K .......... .......... .......... .......... .......... 47% 5.11M 24s
226900K .......... .......... .......... .......... .......... 47% 5.24M 24s
226950K .......... .......... .......... .......... .......... 47% 3.74M 24s
227000K .......... .......... .......... .......... .......... 47% 6.32M 24s
227050K .......... .......... .......... .......... .......... 47% 5.71M 24s
227100K .......... .......... .......... .......... .......... 47% 11.9M 24s
227150K .......... .......... .......... .......... .......... 47% 10.2M 24s
227200K .......... .......... .......... .......... .......... 47% 8.10M 24s
227250K .......... .......... .......... .......... .......... 47% 8.67M 24s
227300K .......... .......... .......... .......... .......... 47% 7.32M 24s
227350K .......... .......... .......... .......... .......... 47% 6.22M 24s
227400K .......... .......... .......... .......... .......... 47% 5.89M 24s
227450K .......... .......... .......... .......... .......... 47% 4.95M 24s
227500K .......... .......... .......... .......... .......... 47% 3.29M 24s
227550K .......... .......... .......... .......... .......... 47% 2.80M 24s
227600K .......... .......... .......... .......... .......... 47% 4.66M 24s
227650K .......... .......... .......... .......... .......... 47% 25.9M 24s
227700K .......... .......... .......... .......... .......... 47% 28.8M 24s
227750K .......... .......... .......... .......... .......... 47% 28.5M 24s
227800K .......... .......... .......... .......... .......... 47% 25.4M 24s
227850K .......... .......... .......... .......... .......... 47% 11.8M 24s
227900K .......... .......... .......... .......... .......... 47%  155M 24s
227950K .......... .......... .......... .......... .......... 47% 23.1M 24s
228000K .......... .......... .......... .......... .......... 47% 16.4M 24s
228050K .......... .......... .......... .......... .......... 47% 14.2M 24s
228100K .......... .......... .......... .......... .......... 47% 13.9M 24s
228150K .......... .......... .......... .......... .......... 47% 10.4M 24s
228200K .......... .......... .......... .......... .......... 47% 9.46M 24s
228250K .......... .......... .......... .......... .......... 47% 9.29M 24s
228300K .......... .......... .......... .......... .......... 47% 8.96M 24s
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228500K .......... .......... .......... .......... .......... 47% 10.6M 24s
228550K .......... .......... .......... .......... .......... 47% 6.33M 24s
228600K .......... .......... .......... .......... .......... 47% 3.59M 24s
228650K .......... .......... .......... .......... .......... 47% 4.39M 24s
228700K .......... .......... .......... .......... .......... 47% 4.01M 24s
228750K .......... .......... .......... .......... .......... 47% 6.15M 24s
228800K .......... .......... .......... .......... .......... 47% 5.22M 24s
228850K .......... .......... .......... .......... .......... 47% 4.63M 24s
228900K .......... .......... .......... .......... .......... 47% 6.89M 24s
228950K .......... .......... .......... .......... .......... 47% 11.9M 24s
229000K .......... .......... .......... .......... .......... 47% 20.5M 24s
229050K .......... .......... .......... .......... .......... 47% 11.5M 24s
229100K .......... .......... .......... .......... .......... 47% 10.2M 24s
229150K .......... .......... .......... .......... .......... 47% 9.12M 24s
229200K .......... .......... .......... .......... .......... 47% 6.37M 24s
229250K .......... .......... .......... .......... .......... 47% 5.37M 24s
229300K .......... .......... .......... .......... .......... 47% 5.04M 24s
229350K .......... .......... .......... .......... .......... 47% 6.87M 24s
229400K .......... .......... .......... .......... .......... 47% 15.8M 24s
229450K .......... .......... .......... .......... .......... 47% 18.0M 24s
229500K .......... .......... .......... .......... .......... 47% 15.7M 24s
229550K .......... .......... .......... .......... .......... 47% 15.9M 24s
229600K .......... .......... .......... .......... .......... 47% 12.2M 24s
229650K .......... .......... .......... .......... .......... 47% 13.1M 24s
229700K .......... .......... .......... .......... .......... 47% 7.05M 24s
229750K .......... .......... .......... .......... .......... 47% 5.69M 24s
229800K .......... .......... .......... .......... .......... 47% 5.97M 24s
229850K .......... .......... .......... .......... .......... 47% 5.32M 24s
229900K .......... .......... .......... .......... .......... 47% 6.66M 24s
229950K .......... .......... .......... .......... .......... 47% 5.38M 24s
230000K .......... .......... .......... .......... .......... 47% 6.28M 24s
230050K .......... .......... .......... .......... .......... 47% 5.55M 24s
230100K .......... .......... .......... .......... .......... 47% 4.26M 24s
230150K .......... .......... .......... .......... .......... 47% 5.60M 24s
230200K .......... .......... .......... .......... .......... 47% 6.77M 24s
230250K .......... .......... .......... .......... .......... 47% 10.0M 24s
230300K .......... .......... .......... .......... .......... 47% 10.3M 24s
230350K .......... .......... .......... .......... .......... 47% 7.79M 24s
230400K .......... .......... .......... .......... .......... 47% 8.69M 24s
230450K .......... .......... .......... .......... .......... 47% 6.79M 24s
230500K .......... .......... .......... .......... .......... 47% 9.59M 24s
230550K .......... .......... .......... .......... .......... 47% 9.29M 24s
230600K .......... .......... .......... .......... .......... 47% 7.57M 24s
230650K .......... .......... .......... .......... .......... 48% 8.56M 24s
230700K .......... .......... .......... .......... .......... 48% 4.97M 24s
230750K .......... .......... .......... .......... .......... 48% 4.21M 24s
230800K .......... .......... .......... .......... .......... 48% 3.47M 24s
230850K .......... .......... .......... .......... .......... 48% 3.85M 24s
230900K .......... .......... .......... .......... .......... 48% 5.44M 24s
230950K .......... .......... .......... .......... .......... 48% 4.54M 24s
231000K .......... .......... .......... .......... .......... 48% 4.46M 24s
231050K .......... .......... .......... .......... .......... 48% 3.97M 24s
231100K .......... .......... .......... .......... .......... 48% 3.47M 24s
231150K .......... .......... .......... .......... .......... 48% 11.3M 24s
231200K .......... .......... .......... .......... .......... 48% 14.6M 24s
231250K .......... .......... .......... .......... .......... 48% 15.2M 24s
231300K .......... .......... .......... .......... .......... 48% 20.7M 24s
231350K .......... .......... .......... .......... .......... 48% 23.7M 24s
231400K .......... .......... .......... .......... .......... 48% 19.4M 24s
231450K .......... .......... .......... .......... .......... 48% 9.25M 24s
231500K .......... .......... .......... .......... .......... 48% 12.1M 24s
231550K .......... .......... .......... .......... .......... 48% 13.1M 24s
231600K .......... .......... .......... .......... .......... 48% 8.25M 24s
231650K .......... .......... .......... .......... .......... 48% 8.38M 24s
231700K .......... .......... .......... .......... .......... 48% 8.80M 24s
231750K .......... .......... .......... .......... .......... 48% 11.5M 24s
231800K .......... .......... .......... .......... .......... 48% 10.3M 24s
231850K .......... .......... .......... .......... .......... 48% 7.90M 24s
231900K .......... .......... .......... .......... .......... 48% 9.05M 24s
231950K .......... .......... .......... .......... .......... 48% 6.80M 24s
232000K .......... .......... .......... .......... .......... 48% 7.14M 24s
232050K .......... .......... .......... .......... .......... 48% 7.25M 24s
232100K .......... .......... .......... .......... .......... 48% 4.37M 24s
232150K .......... .......... .......... .......... .......... 48% 11.9M 24s
232200K .......... .......... .......... .......... .......... 48% 5.64M 24s
232250K .......... .......... .......... .......... .......... 48% 5.15M 24s
232300K .......... .......... .......... .......... .......... 48% 5.76M 24s
232350K .......... .......... .......... .......... .......... 48% 6.56M 24s
232400K .......... .......... .......... .......... .......... 48% 7.33M 24s
232450K .......... .......... .......... .......... .......... 48% 5.26M 24s
232500K .......... .......... .......... .......... .......... 48% 7.41M 24s
232550K .......... .......... .......... .......... .......... 48% 5.22M 24s
232600K .......... .......... .......... .......... .......... 48% 5.19M 24s
232650K .......... .......... .......... .......... .......... 48% 5.07M 24s
232700K .......... .......... .......... .......... .......... 48% 6.19M 24s
232750K .......... .......... .......... .......... .......... 48% 6.20M 24s
232800K .......... .......... .......... .......... .......... 48% 9.51M 24s
232850K .......... .......... .......... .......... .......... 48% 5.40M 24s
232900K .......... .......... .......... .......... .......... 48% 12.4M 24s
232950K .......... .......... .......... .......... .......... 48% 6.55M 24s
233000K .......... .......... .......... .......... .......... 48% 9.69M 24s
233050K .......... .......... .......... .......... .......... 48% 8.15M 24s
233100K .......... .......... .......... .......... .......... 48% 6.89M 24s
233150K .......... .......... .......... .......... .......... 48% 9.44M 24s
233200K .......... .......... .......... .......... .......... 48% 9.08M 24s
233250K .......... .......... .......... .......... .......... 48% 9.26M 24s
233300K .......... .......... .......... .......... .......... 48% 11.2M 24s
233350K .......... .......... .......... .......... .......... 48% 6.75M 24s
233400K .......... .......... .......... .......... .......... 48% 7.93M 24s
233450K .......... .......... .......... .......... .......... 48% 6.77M 24s
233500K .......... .......... .......... .......... .......... 48% 7.10M 24s
233550K .......... .......... .......... .......... .......... 48% 8.04M 24s
233600K .......... .......... .......... .......... .......... 48% 5.92M 24s
233650K .......... .......... .......... .......... .......... 48% 9.70M 24s
233700K .......... .......... .......... .......... .......... 48% 6.53M 24s
233750K .......... .......... .......... .......... .......... 48% 7.36M 24s
233800K .......... .......... .......... .......... .......... 48% 7.52M 24s
233850K .......... .......... .......... .......... .......... 48% 5.60M 24s
233900K .......... .......... .......... .......... .......... 48% 5.15M 24s
233950K .......... .......... .......... .......... .......... 48% 8.03M 24s
234000K .......... .......... .......... .......... .......... 48% 13.6M 24s
234050K .......... .......... .......... .......... .......... 48% 10.8M 24s
234100K .......... .......... .......... .......... .......... 48% 8.95M 24s
234150K .......... .......... .......... .......... .......... 48% 10.9M 24s
234200K .......... .......... .......... .......... .......... 48% 7.39M 24s
234250K .......... .......... .......... .......... .......... 48% 12.5M 24s
234300K .......... .......... .......... .......... .......... 48% 11.3M 24s
234350K .......... .......... .......... .......... .......... 48% 10.5M 24s
234400K .......... .......... .......... .......... .......... 48% 13.9M 24s
234450K .......... .......... .......... .......... .......... 48% 11.8M 24s
234500K .......... .......... .......... .......... .......... 48% 11.9M 24s
234550K .......... .......... .......... .......... .......... 48% 9.71M 24s
234600K .......... .......... .......... .......... .......... 48% 9.74M 24s
234650K .......... .......... .......... .......... .......... 48% 7.63M 24s
234700K .......... .......... .......... .......... .......... 48% 11.9M 24s
234750K .......... .......... .......... .......... .......... 48% 11.8M 24s
234800K .......... .......... .......... .......... .......... 48% 12.7M 24s
234850K .......... .......... .......... .......... .......... 48% 9.96M 24s
234900K .......... .......... .......... .......... .......... 48% 10.9M 24s
234950K .......... .......... .......... .......... .......... 48% 8.48M 24s
235000K .......... .......... .......... .......... .......... 48% 11.3M 24s
235050K .......... .......... .......... .......... .......... 48% 10.2M 24s
235100K .......... .......... .......... .......... .......... 48% 5.54M 24s
235150K .......... .......... .......... .......... .......... 48% 9.66M 24s
235200K .......... .......... .......... .......... .......... 48% 8.09M 24s
235250K .......... .......... .......... .......... .......... 48% 10.5M 24s
235300K .......... .......... .......... .......... .......... 48% 11.7M 24s
235350K .......... .......... .......... .......... .......... 48% 11.2M 24s
235400K .......... .......... .......... .......... .......... 48% 9.09M 24s
235450K .......... .......... .......... .......... .......... 48% 12.8M 24s
235500K .......... .......... .......... .......... .......... 49% 10.6M 24s
235550K .......... .......... .......... .......... .......... 49% 10.8M 24s
235600K .......... .......... .......... .......... .......... 49% 9.50M 24s
235650K .......... .......... .......... .......... .......... 49% 9.12M 24s
235700K .......... .......... .......... .......... .......... 49% 7.22M 24s
235750K .......... .......... .......... .......... .......... 49% 7.51M 24s
235800K .......... .......... .......... .......... .......... 49% 8.07M 24s
235850K .......... .......... .......... .......... .......... 49% 6.11M 24s
235900K .......... .......... .......... .......... .......... 49% 5.16M 24s
235950K .......... .......... .......... .......... .......... 49% 4.47M 24s
236000K .......... .......... .......... .......... .......... 49% 4.82M 24s
236050K .......... .......... .......... .......... .......... 49% 8.57M 24s
236100K .......... .......... .......... .......... .......... 49% 12.1M 24s
236150K .......... .......... .......... .......... .......... 49% 13.1M 24s
236200K .......... .......... .......... .......... .......... 49% 9.07M 24s
236250K .......... .......... .......... .......... .......... 49% 10.2M 24s
236300K .......... .......... .......... .......... .......... 49% 8.15M 24s
236350K .......... .......... .......... .......... .......... 49% 5.69M 24s
236400K .......... .......... .......... .......... .......... 49% 8.00M 24s
236450K .......... .......... .......... .......... .......... 49% 5.77M 24s
236500K .......... .......... .......... .......... .......... 49% 11.2M 24s
236550K .......... .......... .......... .......... .......... 49% 11.4M 24s
236600K .......... .......... .......... .......... .......... 49% 10.9M 24s
236650K .......... .......... .......... .......... .......... 49% 10.7M 24s
236700K .......... .......... .......... .......... .......... 49% 7.89M 24s
236750K .......... .......... .......... .......... .......... 49% 13.2M 24s
236800K .......... .......... .......... .......... .......... 49% 9.80M 24s
236850K .......... .......... .......... .......... .......... 49% 12.1M 24s
236900K .......... .......... .......... .......... .......... 49% 98.6M 24s
236950K .......... .......... .......... .......... .......... 49% 24.3M 24s
237000K .......... .......... .......... .......... .......... 49% 19.9M 24s
237050K .......... .......... .......... .......... .......... 49% 33.9M 24s
237100K .......... .......... .......... .......... .......... 49% 13.0M 24s
237150K .......... .......... .......... .......... .......... 49% 19.2M 24s
237200K .......... .......... .......... .......... .......... 49% 14.4M 24s
237250K .......... .......... .......... .......... .......... 49% 19.1M 24s
237300K .......... .......... .......... .......... .......... 49% 14.6M 24s
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237400K .......... .......... .......... .......... .......... 49% 16.4M 24s
237450K .......... .......... .......... .......... .......... 49% 9.15M 24s
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237550K .......... .......... .......... .......... .......... 49% 11.2M 24s
237600K .......... .......... .......... .......... .......... 49% 6.72M 24s
237650K .......... .......... .......... .......... .......... 49% 6.22M 24s
237700K .......... .......... .......... .......... .......... 49% 6.04M 24s
237750K .......... .......... .......... .......... .......... 49% 5.38M 24s
237800K .......... .......... .......... .......... .......... 49% 6.18M 24s
237850K .......... .......... .......... .......... .......... 49% 4.99M 24s
237900K .......... .......... .......... .......... .......... 49% 4.99M 24s
237950K .......... .......... .......... .......... .......... 49% 3.97M 24s
238000K .......... .......... .......... .......... .......... 49% 4.08M 24s
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238100K .......... .......... .......... .......... .......... 49% 2.81M 24s
238150K .......... .......... .......... .......... .......... 49% 9.33M 24s
238200K .......... .......... .......... .......... .......... 49% 12.9M 24s
238250K .......... .......... .......... .......... .......... 49% 9.74M 24s
238300K .......... .......... .......... .......... .......... 49% 61.7M 24s
238350K .......... .......... .......... .......... .......... 49% 10.7M 24s
238400K .......... .......... .......... .......... .......... 49% 14.0M 24s
238450K .......... .......... .......... .......... .......... 49% 11.0M 24s
238500K .......... .......... .......... .......... .......... 49% 9.53M 24s
238550K .......... .......... .......... .......... .......... 49% 14.1M 24s
238600K .......... .......... .......... .......... .......... 49% 6.93M 24s
238650K .......... .......... .......... .......... .......... 49% 12.3M 24s
238700K .......... .......... .......... .......... .......... 49% 9.23M 24s
238750K .......... .......... .......... .......... .......... 49% 7.91M 24s
238800K .......... .......... .......... .......... .......... 49% 7.63M 24s
238850K .......... .......... .......... .......... .......... 49% 5.67M 24s
238900K .......... .......... .......... .......... .......... 49% 9.98M 24s
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239000K .......... .......... .......... .......... .......... 49% 7.91M 24s
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239100K .......... .......... .......... .......... .......... 49% 5.36M 24s
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239250K .......... .......... .......... .......... .......... 49% 6.96M 24s
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239650K .......... .......... .......... .......... .......... 49% 21.6M 24s
239700K .......... .......... .......... .......... .......... 49% 26.1M 24s
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239850K .......... .......... .......... .......... .......... 49% 14.0M 24s
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240000K .......... .......... .......... .......... .......... 49% 7.45M 24s
240050K .......... .......... .......... .......... .......... 49% 9.72M 24s
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240200K .......... .......... .......... .......... .......... 49% 3.98M 23s
240250K .......... .......... .......... .......... .......... 49% 2.59M 24s
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241000K .......... .......... .......... .......... .......... 50% 10.5M 23s
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241100K .......... .......... .......... .......... .......... 50% 6.73M 23s
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241500K .......... .......... .......... .......... .......... 50% 14.5M 23s
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242000K .......... .......... .......... .......... .......... 50% 11.9M 23s
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242150K .......... .......... .......... .......... .......... 50% 7.24M 23s
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242500K .......... .......... .......... .......... .......... 50% 9.22M 23s
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243000K .......... .......... .......... .......... .......... 50% 4.81M 23s
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243100K .......... .......... .......... .......... .......... 50% 7.46M 23s
243150K .......... .......... .......... .......... .......... 50% 17.7M 23s
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243250K .......... .......... .......... .......... .......... 50% 23.3M 23s
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243900K .......... .......... .......... .......... .......... 50% 34.6M 23s
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244000K .......... .......... .......... .......... .......... 50% 39.8M 23s
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244900K .......... .......... .......... .......... .......... 50% 8.82M 23s
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245000K .......... .......... .......... .......... .......... 50% 7.02M 23s
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245100K .......... .......... .......... .......... .......... 51% 4.83M 23s
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245200K .......... .......... .......... .......... .......... 51% 8.28M 23s
245250K .......... .......... .......... .......... .......... 51% 21.2M 23s
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245400K .......... .......... .......... .......... .......... 51% 16.1M 23s
245450K .......... .......... .......... .......... .......... 51% 14.1M 23s
245500K .......... .......... .......... .......... .......... 51% 11.1M 23s
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245650K .......... .......... .......... .......... .......... 51% 9.03M 23s
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245750K .......... .......... .......... .......... .......... 51% 13.1M 23s
245800K .......... .......... .......... .......... .......... 51% 12.1M 23s
245850K .......... .......... .......... .......... .......... 51% 9.02M 23s
245900K .......... .......... .......... .......... .......... 51% 20.9M 23s
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246000K .......... .......... .......... .......... .......... 51% 13.3M 23s
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246100K .......... .......... .......... .......... .......... 51% 8.86M 23s
246150K .......... .......... .......... .......... .......... 51% 10.7M 23s
246200K .......... .......... .......... .......... .......... 51% 7.90M 23s
246250K .......... .......... .......... .......... .......... 51% 11.1M 23s
246300K .......... .......... .......... .......... .......... 51% 9.66M 23s
246350K .......... .......... .......... .......... .......... 51% 15.8M 23s
246400K .......... .......... .......... .......... .......... 51% 11.8M 23s
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246500K .......... .......... .......... .......... .......... 51% 11.9M 23s
246550K .......... .......... .......... .......... .......... 51% 7.83M 23s
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246750K .......... .......... .......... .......... .......... 51% 10.9M 23s
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246850K .......... .......... .......... .......... .......... 51% 11.2M 23s
246900K .......... .......... .......... .......... .......... 51% 13.9M 23s
246950K .......... .......... .......... .......... .......... 51% 8.08M 23s
247000K .......... .......... .......... .......... .......... 51% 13.5M 23s
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247100K .......... .......... .......... .......... .......... 51% 7.32M 23s
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247200K .......... .......... .......... .......... .......... 51% 7.30M 23s
247250K .......... .......... .......... .......... .......... 51% 8.77M 23s
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247400K .......... .......... .......... .......... .......... 51% 9.08M 23s
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248000K .......... .......... .......... .......... .......... 51% 6.08M 23s
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248100K .......... .......... .......... .......... .......... 51% 5.60M 23s
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248250K .......... .......... .......... .......... .......... 51% 9.23M 23s
248300K .......... .......... .......... .......... .......... 51% 13.9M 23s
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248400K .......... .......... .......... .......... .......... 51% 16.8M 23s
248450K .......... .......... .......... .......... .......... 51% 12.6M 23s
248500K .......... .......... .......... .......... .......... 51% 16.7M 23s
248550K .......... .......... .......... .......... .......... 51% 12.5M 23s
248600K .......... .......... .......... .......... .......... 51% 11.7M 23s
248650K .......... .......... .......... .......... .......... 51% 12.1M 23s
248700K .......... .......... .......... .......... .......... 51% 10.7M 23s
248750K .......... .......... .......... .......... .......... 51% 11.7M 23s
248800K .......... .......... .......... .......... .......... 51% 9.29M 23s
248850K .......... .......... .......... .......... .......... 51% 14.0M 23s
248900K .......... .......... .......... .......... .......... 51% 13.9M 23s
248950K .......... .......... .......... .......... .......... 51% 8.83M 23s
249000K .......... .......... .......... .......... .......... 51% 9.73M 23s
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249100K .......... .......... .......... .......... .......... 51% 8.41M 23s
249150K .......... .......... .......... .......... .......... 51% 9.98M 23s
249200K .......... .......... .......... .......... .......... 51% 8.44M 23s
249250K .......... .......... .......... .......... .......... 51% 9.09M 23s
249300K .......... .......... .......... .......... .......... 51% 7.95M 23s
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249400K .......... .......... .......... .......... .......... 51% 8.06M 23s
249450K .......... .......... .......... .......... .......... 51% 6.89M 23s
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250000K .......... .......... .......... .......... .......... 52% 11.4M 23s
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250100K .......... .......... .......... .......... .......... 52% 10.0M 23s
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250200K .......... .......... .......... .......... .......... 52% 9.47M 23s
250250K .......... .......... .......... .......... .......... 52% 10.1M 23s
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250900K .......... .......... .......... .......... .......... 52% 9.53M 23s
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251000K .......... .......... .......... .......... .......... 52% 7.26M 23s
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251100K .......... .......... .......... .......... .......... 52% 8.65M 23s
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251500K .......... .......... .......... .......... .......... 52% 11.0M 23s
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251600K .......... .......... .......... .......... .......... 52% 10.9M 23s
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251800K .......... .......... .......... .......... .......... 52% 8.40M 23s
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251900K .......... .......... .......... .......... .......... 52% 8.41M 23s
251950K .......... .......... .......... .......... .......... 52% 6.22M 23s
252000K .......... .......... .......... .......... .......... 52% 9.34M 23s
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252150K .......... .......... .......... .......... .......... 52% 16.1M 22s
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252350K .......... .......... .......... .......... .......... 52% 9.10M 22s
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252500K .......... .......... .......... .......... .......... 52% 12.0M 22s
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252800K .......... .......... .......... .......... .......... 52% 9.85M 22s
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253000K .......... .......... .......... .......... .......... 52% 9.07M 22s
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253100K .......... .......... .......... .......... .......... 52% 67.8M 22s
253150K .......... .......... .......... .......... .......... 52% 13.8M 22s
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254250K .......... .......... .......... .......... .......... 52% 16.5M 22s
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254400K .......... .......... .......... .......... .......... 52% 77.6M 22s
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262800K .......... .......... .......... .......... .......... 54% 10.9M 21s
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263250K .......... .......... .......... .......... .......... 54% 12.2M 21s
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263550K .......... .......... .......... .......... .......... 54% 11.5M 21s
263600K .......... .......... .......... .......... .......... 54% 9.87M 21s
263650K .......... .......... .......... .......... .......... 54% 8.48M 21s
263700K .......... .......... .......... .......... .......... 54% 9.61M 21s
263750K .......... .......... .......... .......... .......... 54% 8.58M 21s
263800K .......... .......... .......... .......... .......... 54% 12.7M 21s
263850K .......... .......... .......... .......... .......... 54% 9.91M 21s
263900K .......... .......... .......... .......... .......... 54% 6.34M 21s
263950K .......... .......... .......... .......... .......... 54% 4.87M 21s
264000K .......... .......... .......... .......... .......... 54% 7.60M 21s
264050K .......... .......... .......... .......... .......... 54% 6.07M 21s
264100K .......... .......... .......... .......... .......... 54% 5.99M 21s
264150K .......... .......... .......... .......... .......... 54% 6.46M 21s
264200K .......... .......... .......... .......... .......... 54% 8.11M 21s
264250K .......... .......... .......... .......... .......... 54% 9.34M 21s
264300K .......... .......... .......... .......... .......... 55% 10.9M 21s
264350K .......... .......... .......... .......... .......... 55% 5.46M 21s
264400K .......... .......... .......... .......... .......... 55% 6.92M 21s
264450K .......... .......... .......... .......... .......... 55% 5.13M 21s
264500K .......... .......... .......... .......... .......... 55% 6.74M 21s
264550K .......... .......... .......... .......... .......... 55% 8.07M 21s
264600K .......... .......... .......... .......... .......... 55% 7.66M 21s
264650K .......... .......... .......... .......... .......... 55% 9.27M 21s
264700K .......... .......... .......... .......... .......... 55% 5.78M 21s
264750K .......... .......... .......... .......... .......... 55% 8.09M 21s
264800K .......... .......... .......... .......... .......... 55% 7.36M 21s
264850K .......... .......... .......... .......... .......... 55% 10.1M 21s
264900K .......... .......... .......... .......... .......... 55% 8.87M 21s
264950K .......... .......... .......... .......... .......... 55% 6.30M 21s
265000K .......... .......... .......... .......... .......... 55% 11.9M 21s
265050K .......... .......... .......... .......... .......... 55% 8.12M 21s
265100K .......... .......... .......... .......... .......... 55% 10.2M 21s
265150K .......... .......... .......... .......... .......... 55% 12.1M 21s
265200K .......... .......... .......... .......... .......... 55% 12.1M 21s
265250K .......... .......... .......... .......... .......... 55% 11.9M 21s
265300K .......... .......... .......... .......... .......... 55% 11.9M 21s
265350K .......... .......... .......... .......... .......... 55% 11.4M 21s
265400K .......... .......... .......... .......... .......... 55% 9.33M 21s
265450K .......... .......... .......... .......... .......... 55% 11.0M 21s
265500K .......... .......... .......... .......... .......... 55% 8.58M 21s
265550K .......... .......... .......... .......... .......... 55% 11.4M 21s
265600K .......... .......... .......... .......... .......... 55% 7.14M 21s
265650K .......... .......... .......... .......... .......... 55% 8.81M 21s
265700K .......... .......... .......... .......... .......... 55% 6.68M 21s
265750K .......... .......... .......... .......... .......... 55% 10.6M 21s
265800K .......... .......... .......... .......... .......... 55% 7.89M 21s
265850K .......... .......... .......... .......... .......... 55% 8.96M 21s
265900K .......... .......... .......... .......... .......... 55% 14.3M 21s
265950K .......... .......... .......... .......... .......... 55% 10.2M 21s
266000K .......... .......... .......... .......... .......... 55% 16.0M 21s
266050K .......... .......... .......... .......... .......... 55% 14.9M 21s
266100K .......... .......... .......... .......... .......... 55% 9.69M 21s
266150K .......... .......... .......... .......... .......... 55% 8.84M 21s
266200K .......... .......... .......... .......... .......... 55% 6.83M 21s
266250K .......... .......... .......... .......... .......... 55% 7.94M 21s
266300K .......... .......... .......... .......... .......... 55% 13.5M 21s
266350K .......... .......... .......... .......... .......... 55% 11.0M 21s
266400K .......... .......... .......... .......... .......... 55% 11.5M 21s
266450K .......... .......... .......... .......... .......... 55% 9.35M 21s
266500K .......... .......... .......... .......... .......... 55% 9.75M 21s
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266600K .......... .......... .......... .......... .......... 55% 7.17M 21s
266650K .......... .......... .......... .......... .......... 55% 7.95M 21s
266700K .......... .......... .......... .......... .......... 55% 8.05M 21s
266750K .......... .......... .......... .......... .......... 55% 8.41M 21s
266800K .......... .......... .......... .......... .......... 55% 7.89M 21s
266850K .......... .......... .......... .......... .......... 55% 9.61M 21s
266900K .......... .......... .......... .......... .......... 55% 6.52M 21s
266950K .......... .......... .......... .......... .......... 55% 8.03M 21s
267000K .......... .......... .......... .......... .......... 55% 8.80M 21s
267050K .......... .......... .......... .......... .......... 55% 9.18M 21s
267100K .......... .......... .......... .......... .......... 55% 7.21M 21s
267150K .......... .......... .......... .......... .......... 55% 8.68M 21s
267200K .......... .......... .......... .......... .......... 55% 7.03M 21s
267250K .......... .......... .......... .......... .......... 55% 7.38M 21s
267300K .......... .......... .......... .......... .......... 55% 6.70M 21s
267350K .......... .......... .......... .......... .......... 55% 4.52M 21s
267400K .......... .......... .......... .......... .......... 55% 9.30M 21s
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267500K .......... .......... .......... .......... .......... 55% 9.98M 21s
267550K .......... .......... .......... .......... .......... 55% 8.48M 21s
267600K .......... .......... .......... .......... .......... 55% 6.73M 21s
267650K .......... .......... .......... .......... .......... 55% 8.22M 21s
267700K .......... .......... .......... .......... .......... 55% 9.95M 21s
267750K .......... .......... .......... .......... .......... 55% 10.6M 21s
267800K .......... .......... .......... .......... .......... 55% 11.5M 21s
267850K .......... .......... .......... .......... .......... 55% 7.63M 21s
267900K .......... .......... .......... .......... .......... 55% 9.12M 21s
267950K .......... .......... .......... .......... .......... 55% 10.5M 21s
268000K .......... .......... .......... .......... .......... 55% 9.80M 21s
268050K .......... .......... .......... .......... .......... 55% 8.46M 21s
268100K .......... .......... .......... .......... .......... 55% 6.70M 21s
268150K .......... .......... .......... .......... .......... 55% 10.2M 21s
268200K .......... .......... .......... .......... .......... 55% 11.8M 21s
268250K .......... .......... .......... .......... .......... 55% 13.0M 21s
268300K .......... .......... .......... .......... .......... 55% 10.6M 21s
268350K .......... .......... .......... .......... .......... 55% 9.05M 21s
268400K .......... .......... .......... .......... .......... 55% 12.6M 21s
268450K .......... .......... .......... .......... .......... 55% 10.4M 21s
268500K .......... .......... .......... .......... .......... 55% 15.5M 21s
268550K .......... .......... .......... .......... .......... 55% 13.9M 21s
268600K .......... .......... .......... .......... .......... 55% 9.71M 21s
268650K .......... .......... .......... .......... .......... 55% 10.5M 21s
268700K .......... .......... .......... .......... .......... 55% 11.9M 21s
268750K .......... .......... .......... .......... .......... 55% 9.71M 21s
268800K .......... .......... .......... .......... .......... 55% 13.4M 21s
268850K .......... .......... .......... .......... .......... 55% 10.1M 21s
268900K .......... .......... .......... .......... .......... 55% 15.9M 21s
268950K .......... .......... .......... .......... .......... 55% 20.2M 21s
269000K .......... .......... .......... .......... .......... 55% 55.8M 21s
269050K .......... .......... .......... .......... .......... 55% 32.2M 21s
269100K .......... .......... .......... .......... .......... 56% 13.1M 21s
269150K .......... .......... .......... .......... .......... 56% 81.2M 21s
269200K .......... .......... .......... .......... .......... 56% 18.0M 21s
269250K .......... .......... .......... .......... .......... 56% 17.8M 21s
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269350K .......... .......... .......... .......... .......... 56% 9.06M 21s
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269450K .......... .......... .......... .......... .......... 56% 10.8M 21s
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269800K .......... .......... .......... .......... .......... 56% 13.1M 21s
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269900K .......... .......... .......... .......... .......... 56% 7.99M 21s
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270000K .......... .......... .......... .......... .......... 56% 6.80M 21s
270050K .......... .......... .......... .......... .......... 56% 4.29M 21s
270100K .......... .......... .......... .......... .......... 56% 5.80M 21s
270150K .......... .......... .......... .......... .......... 56% 8.06M 21s
270200K .......... .......... .......... .......... .......... 56% 6.71M 21s
270250K .......... .......... .......... .......... .......... 56% 6.90M 21s
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270350K .......... .......... .......... .......... .......... 56% 9.90M 21s
270400K .......... .......... .......... .......... .......... 56% 27.7M 21s
270450K .......... .......... .......... .......... .......... 56% 16.3M 21s
270500K .......... .......... .......... .......... .......... 56% 26.3M 21s
270550K .......... .......... .......... .......... .......... 56% 18.4M 21s
270600K .......... .......... .......... .......... .......... 56% 17.8M 21s
270650K .......... .......... .......... .......... .......... 56% 18.0M 21s
270700K .......... .......... .......... .......... .......... 56% 26.6M 21s
270750K .......... .......... .......... .......... .......... 56% 23.3M 21s
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270850K .......... .......... .......... .......... .......... 56% 12.2M 21s
270900K .......... .......... .......... .......... .......... 56% 13.8M 21s
270950K .......... .......... .......... .......... .......... 56% 11.7M 21s
271000K .......... .......... .......... .......... .......... 56% 12.4M 21s
271050K .......... .......... .......... .......... .......... 56% 17.9M 21s
271100K .......... .......... .......... .......... .......... 56% 13.6M 21s
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271200K .......... .......... .......... .......... .......... 56% 10.8M 21s
271250K .......... .......... .......... .......... .......... 56% 16.6M 21s
271300K .......... .......... .......... .......... .......... 56% 11.6M 21s
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271400K .......... .......... .......... .......... .......... 56% 9.06M 21s
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271500K .......... .......... .......... .......... .......... 56% 6.03M 21s
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271600K .......... .......... .......... .......... .......... 56% 6.35M 21s
271650K .......... .......... .......... .......... .......... 56% 11.1M 21s
271700K .......... .......... .......... .......... .......... 56% 16.2M 21s
271750K .......... .......... .......... .......... .......... 56% 13.1M 21s
271800K .......... .......... .......... .......... .......... 56% 11.5M 21s
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271900K .......... .......... .......... .......... .......... 56% 11.7M 21s
271950K .......... .......... .......... .......... .......... 56% 10.6M 21s
272000K .......... .......... .......... .......... .......... 56% 10.3M 21s
272050K .......... .......... .......... .......... .......... 56% 14.3M 21s
272100K .......... .......... .......... .......... .......... 56% 8.12M 21s
272150K .......... .......... .......... .......... .......... 56% 7.23M 21s
272200K .......... .......... .......... .......... .......... 56% 9.86M 21s
272250K .......... .......... .......... .......... .......... 56% 12.9M 21s
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272350K .......... .......... .......... .......... .......... 56% 10.5M 21s
272400K .......... .......... .......... .......... .......... 56% 11.6M 21s
272450K .......... .......... .......... .......... .......... 56% 8.70M 21s
272500K .......... .......... .......... .......... .......... 56% 10.8M 21s
272550K .......... .......... .......... .......... .......... 56% 12.8M 21s
272600K .......... .......... .......... .......... .......... 56% 9.94M 21s
272650K .......... .......... .......... .......... .......... 56% 13.5M 21s
272700K .......... .......... .......... .......... .......... 56% 9.36M 21s
272750K .......... .......... .......... .......... .......... 56% 19.8M 21s
272800K .......... .......... .......... .......... .......... 56% 15.2M 21s
272850K .......... .......... .......... .......... .......... 56% 65.2M 20s
272900K .......... .......... .......... .......... .......... 56% 14.3M 20s
272950K .......... .......... .......... .......... .......... 56% 23.7M 20s
273000K .......... .......... .......... .......... .......... 56% 15.5M 20s
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273100K .......... .......... .......... .......... .......... 56% 14.9M 20s
273150K .......... .......... .......... .......... .......... 56% 16.5M 20s
273200K .......... .......... .......... .......... .......... 56% 14.6M 20s
273250K .......... .......... .......... .......... .......... 56% 20.0M 20s
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273400K .......... .......... .......... .......... .......... 56% 14.7M 20s
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273500K .......... .......... .......... .......... .......... 56% 7.68M 20s
273550K .......... .......... .......... .......... .......... 56% 7.09M 20s
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273650K .......... .......... .......... .......... .......... 56% 11.6M 20s
273700K .......... .......... .......... .......... .......... 56% 11.3M 20s
273750K .......... .......... .......... .......... .......... 56% 14.3M 20s
273800K .......... .......... .......... .......... .......... 56% 35.1M 20s
273850K .......... .......... .......... .......... .......... 56% 22.2M 20s
273900K .......... .......... .......... .......... .......... 56% 17.0M 20s
273950K .......... .......... .......... .......... .......... 57% 16.7M 20s
274000K .......... .......... .......... .......... .......... 57% 13.4M 20s
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274100K .......... .......... .......... .......... .......... 57% 17.9M 20s
274150K .......... .......... .......... .......... .......... 57% 12.7M 20s
274200K .......... .......... .......... .......... .......... 57% 9.77M 20s
274250K .......... .......... .......... .......... .......... 57% 11.2M 20s
274300K .......... .......... .......... .......... .......... 57% 11.9M 20s
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274400K .......... .......... .......... .......... .......... 57% 10.0M 20s
274450K .......... .......... .......... .......... .......... 57% 9.47M 20s
274500K .......... .......... .......... .......... .......... 57% 17.4M 20s
274550K .......... .......... .......... .......... .......... 57% 31.8M 20s
274600K .......... .......... .......... .......... .......... 57% 29.1M 20s
274650K .......... .......... .......... .......... .......... 57% 31.0M 20s
274700K .......... .......... .......... .......... .......... 57% 20.4M 20s
274750K .......... .......... .......... .......... .......... 57% 24.2M 20s
274800K .......... .......... .......... .......... .......... 57% 23.3M 20s
274850K .......... .......... .......... .......... .......... 57% 23.0M 20s
274900K .......... .......... .......... .......... .......... 57% 21.0M 20s
274950K .......... .......... .......... .......... .......... 57% 18.1M 20s
275000K .......... .......... .......... .......... .......... 57% 18.9M 20s
275050K .......... .......... .......... .......... .......... 57% 20.6M 20s
275100K .......... .......... .......... .......... .......... 57% 19.0M 20s
275150K .......... .......... .......... .......... .......... 57% 16.9M 20s
275200K .......... .......... .......... .......... .......... 57% 18.1M 20s
275250K .......... .......... .......... .......... .......... 57% 23.2M 20s
275300K .......... .......... .......... .......... .......... 57% 19.1M 20s
275350K .......... .......... .......... .......... .......... 57% 16.8M 20s
275400K .......... .......... .......... .......... .......... 57% 19.7M 20s
275450K .......... .......... .......... .......... .......... 57% 34.2M 20s
275500K .......... .......... .......... .......... .......... 57% 48.7M 20s
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275600K .......... .......... .......... .......... .......... 57% 18.1M 20s
275650K .......... .......... .......... .......... .......... 57% 72.0M 20s
275700K .......... .......... .......... .......... .......... 57% 61.6M 20s
275750K .......... .......... .......... .......... .......... 57% 33.7M 20s
275800K .......... .......... .......... .......... .......... 57% 78.9M 20s
275850K .......... .......... .......... .......... .......... 57% 24.2M 20s
275900K .......... .......... .......... .......... .......... 57% 32.8M 20s
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276000K .......... .......... .......... .......... .......... 57% 22.1M 20s
276050K .......... .......... .......... .......... .......... 57% 27.9M 20s
276100K .......... .......... .......... .......... .......... 57% 23.8M 20s
276150K .......... .......... .......... .......... .......... 57% 15.2M 20s
276200K .......... .......... .......... .......... .......... 57% 18.4M 20s
276250K .......... .......... .......... .......... .......... 57% 9.62M 20s
276300K .......... .......... .......... .......... .......... 57% 31.4M 20s
276350K .......... .......... .......... .......... .......... 57% 17.2M 20s
276400K .......... .......... .......... .......... .......... 57% 15.9M 20s
276450K .......... .......... .......... .......... .......... 57% 9.58M 20s
276500K .......... .......... .......... .......... .......... 57% 13.5M 20s
276550K .......... .......... .......... .......... .......... 57% 12.6M 20s
276600K .......... .......... .......... .......... .......... 57% 11.1M 20s
276650K .......... .......... .......... .......... .......... 57% 12.1M 20s
276700K .......... .......... .......... .......... .......... 57% 9.32M 20s
276750K .......... .......... .......... .......... .......... 57% 10.3M 20s
276800K .......... .......... .......... .......... .......... 57% 9.85M 20s
276850K .......... .......... .......... .......... .......... 57% 7.09M 20s
276900K .......... .......... .......... .......... .......... 57% 10.8M 20s
276950K .......... .......... .......... .......... .......... 57% 6.56M 20s
277000K .......... .......... .......... .......... .......... 57% 8.71M 20s
277050K .......... .......... .......... .......... .......... 57% 27.1M 20s
277100K .......... .......... .......... .......... .......... 57% 24.0M 20s
277150K .......... .......... .......... .......... .......... 57% 12.0M 20s
277200K .......... .......... .......... .......... .......... 57% 62.0M 20s
277250K .......... .......... .......... .......... .......... 57% 79.5M 20s
277300K .......... .......... .......... .......... .......... 57% 34.5M 20s
277350K .......... .......... .......... .......... .......... 57% 35.0M 20s
277400K .......... .......... .......... .......... .......... 57% 21.7M 20s
277450K .......... .......... .......... .......... .......... 57% 20.1M 20s
277500K .......... .......... .......... .......... .......... 57% 27.9M 20s
277550K .......... .......... .......... .......... .......... 57% 30.0M 20s
277600K .......... .......... .......... .......... .......... 57% 19.2M 20s
277650K .......... .......... .......... .......... .......... 57% 32.1M 20s
277700K .......... .......... .......... .......... .......... 57% 18.1M 20s
277750K .......... .......... .......... .......... .......... 57% 31.9M 20s
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277900K .......... .......... .......... .......... .......... 57% 48.1M 20s
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278000K .......... .......... .......... .......... .......... 57% 20.0M 20s
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278100K .......... .......... .......... .......... .......... 57% 13.3M 20s
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278200K .......... .......... .......... .......... .......... 57% 18.9M 20s
278250K .......... .......... .......... .......... .......... 57% 12.6M 20s
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279000K .......... .......... .......... .......... .......... 58% 6.83M 20s
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291850K .......... .......... .......... .......... .......... 60% 14.5M 18s
291900K .......... .......... .......... .......... .......... 60% 17.2M 18s
291950K .......... .......... .......... .......... .......... 60% 16.8M 18s
292000K .......... .......... .......... .......... .......... 60% 12.8M 18s
292050K .......... .......... .......... .......... .......... 60% 17.8M 18s
292100K .......... .......... .......... .......... .......... 60% 15.4M 18s
292150K .......... .......... .......... .......... .......... 60% 26.4M 18s
292200K .......... .......... .......... .......... .......... 60% 28.8M 18s
292250K .......... .......... .......... .......... .......... 60% 21.4M 18s
292300K .......... .......... .......... .......... .......... 60% 66.1M 18s
292350K .......... .......... .......... .......... .......... 60% 30.9M 18s
292400K .......... .......... .......... .......... .......... 60% 42.8M 18s
292450K .......... .......... .......... .......... .......... 60% 25.6M 18s
292500K .......... .......... .......... .......... .......... 60% 33.7M 18s
292550K .......... .......... .......... .......... .......... 60% 22.0M 18s
292600K .......... .......... .......... .......... .......... 60% 22.3M 18s
292650K .......... .......... .......... .......... .......... 60% 19.8M 18s
292700K .......... .......... .......... .......... .......... 60% 17.2M 18s
292750K .......... .......... .......... .......... .......... 60% 17.5M 18s
292800K .......... .......... .......... .......... .......... 60% 35.3M 18s
292850K .......... .......... .......... .......... .......... 60% 16.2M 18s
292900K .......... .......... .......... .......... .......... 60% 15.7M 18s
292950K .......... .......... .......... .......... .......... 60% 17.1M 18s
293000K .......... .......... .......... .......... .......... 60% 18.8M 18s
293050K .......... .......... .......... .......... .......... 60% 14.6M 18s
293100K .......... .......... .......... .......... .......... 60% 14.5M 18s
293150K .......... .......... .......... .......... .......... 61% 11.5M 18s
293200K .......... .......... .......... .......... .......... 61% 9.42M 18s
293250K .......... .......... .......... .......... .......... 61% 13.5M 18s
293300K .......... .......... .......... .......... .......... 61% 13.5M 18s
293350K .......... .......... .......... .......... .......... 61% 10.6M 18s
293400K .......... .......... .......... .......... .......... 61% 9.51M 18s
293450K .......... .......... .......... .......... .......... 61% 12.2M 18s
293500K .......... .......... .......... .......... .......... 61% 8.78M 18s
293550K .......... .......... .......... .......... .......... 61% 10.3M 18s
293600K .......... .......... .......... .......... .......... 61% 11.8M 18s
293650K .......... .......... .......... .......... .......... 61% 9.76M 18s
293700K .......... .......... .......... .......... .......... 61% 7.88M 18s
293750K .......... .......... .......... .......... .......... 61% 8.63M 18s
293800K .......... .......... .......... .......... .......... 61% 15.7M 18s
293850K .......... .......... .......... .......... .......... 61% 9.92M 18s
293900K .......... .......... .......... .......... .......... 61% 12.7M 18s
293950K .......... .......... .......... .......... .......... 61% 8.45M 18s
294000K .......... .......... .......... .......... .......... 61% 12.2M 18s
294050K .......... .......... .......... .......... .......... 61% 13.0M 18s
294100K .......... .......... .......... .......... .......... 61% 10.6M 18s
294150K .......... .......... .......... .......... .......... 61% 9.96M 18s
294200K .......... .......... .......... .......... .......... 61% 12.9M 18s
294250K .......... .......... .......... .......... .......... 61% 17.9M 18s
294300K .......... .......... .......... .......... .......... 61% 30.6M 18s
294350K .......... .......... .......... .......... .......... 61% 17.6M 18s
294400K .......... .......... .......... .......... .......... 61% 23.2M 18s
294450K .......... .......... .......... .......... .......... 61% 14.6M 18s
294500K .......... .......... .......... .......... .......... 61% 13.9M 18s
294550K .......... .......... .......... .......... .......... 61% 16.4M 18s
294600K .......... .......... .......... .......... .......... 61% 12.6M 18s
294650K .......... .......... .......... .......... .......... 61% 17.2M 18s
294700K .......... .......... .......... .......... .......... 61% 12.6M 18s
294750K .......... .......... .......... .......... .......... 61% 16.5M 18s
294800K .......... .......... .......... .......... .......... 61% 11.4M 18s
294850K .......... .......... .......... .......... .......... 61% 14.5M 18s
294900K .......... .......... .......... .......... .......... 61% 15.7M 18s
294950K .......... .......... .......... .......... .......... 61% 9.43M 18s
295000K .......... .......... .......... .......... .......... 61% 12.2M 18s
295050K .......... .......... .......... .......... .......... 61% 15.3M 18s
295100K .......... .......... .......... .......... .......... 61% 9.40M 18s
295150K .......... .......... .......... .......... .......... 61% 9.32M 18s
295200K .......... .......... .......... .......... .......... 61% 9.90M 18s
295250K .......... .......... .......... .......... .......... 61% 11.1M 18s
295300K .......... .......... .......... .......... .......... 61% 8.50M 18s
295350K .......... .......... .......... .......... .......... 61% 9.50M 18s
295400K .......... .......... .......... .......... .......... 61% 11.8M 18s
295450K .......... .......... .......... .......... .......... 61% 6.44M 18s
295500K .......... .......... .......... .......... .......... 61% 10.7M 18s
295550K .......... .......... .......... .......... .......... 61% 9.05M 18s
295600K .......... .......... .......... .......... .......... 61% 7.44M 18s
295650K .......... .......... .......... .......... .......... 61% 10.8M 18s
295700K .......... .......... .......... .......... .......... 61% 12.7M 18s
295750K .......... .......... .......... .......... .......... 61% 16.4M 18s
295800K .......... .......... .......... .......... .......... 61% 14.6M 18s
295850K .......... .......... .......... .......... .......... 61% 10.6M 18s
295900K .......... .......... .......... .......... .......... 61% 12.3M 18s
295950K .......... .......... .......... .......... .......... 61% 11.3M 18s
296000K .......... .......... .......... .......... .......... 61% 12.1M 18s
296050K .......... .......... .......... .......... .......... 61% 10.9M 18s
296100K .......... .......... .......... .......... .......... 61% 9.39M 18s
296150K .......... .......... .......... .......... .......... 61% 8.22M 18s
296200K .......... .......... .......... .......... .......... 61% 7.52M 18s
296250K .......... .......... .......... .......... .......... 61% 7.79M 18s
296300K .......... .......... .......... .......... .......... 61% 8.61M 18s
296350K .......... .......... .......... .......... .......... 61% 6.80M 18s
296400K .......... .......... .......... .......... .......... 61% 6.93M 18s
296450K .......... .......... .......... .......... .......... 61% 9.91M 18s
296500K .......... .......... .......... .......... .......... 61% 9.47M 18s
296550K .......... .......... .......... .......... .......... 61% 11.7M 18s
296600K .......... .......... .......... .......... .......... 61% 7.61M 18s
296650K .......... .......... .......... .......... .......... 61% 8.69M 18s
296700K .......... .......... .......... .......... .......... 61% 7.83M 18s
296750K .......... .......... .......... .......... .......... 61% 7.65M 18s
296800K .......... .......... .......... .......... .......... 61% 7.51M 18s
296850K .......... .......... .......... .......... .......... 61% 5.70M 18s
296900K .......... .......... .......... .......... .......... 61% 12.7M 18s
296950K .......... .......... .......... .......... .......... 61% 11.3M 18s
297000K .......... .......... .......... .......... .......... 61% 21.0M 18s
297050K .......... .......... .......... .......... .......... 61% 18.7M 18s
297100K .......... .......... .......... .......... .......... 61% 17.2M 18s
297150K .......... .......... .......... .......... .......... 61% 14.0M 18s
297200K .......... .......... .......... .......... .......... 61% 13.5M 18s
297250K .......... .......... .......... .......... .......... 61% 11.6M 18s
297300K .......... .......... .......... .......... .......... 61% 17.7M 18s
297350K .......... .......... .......... .......... .......... 61% 8.23M 18s
297400K .......... .......... .......... .......... .......... 61% 10.8M 18s
297450K .......... .......... .......... .......... .......... 61% 8.51M 18s
297500K .......... .......... .......... .......... .......... 61% 5.25M 18s
297550K .......... .......... .......... .......... .......... 61% 3.86M 18s
297600K .......... .......... .......... .......... .......... 61% 5.00M 18s
297650K .......... .......... .......... .......... .......... 61% 6.53M 18s
297700K .......... .......... .......... .......... .......... 61% 8.61M 18s
297750K .......... .......... .......... .......... .......... 61% 6.30M 18s
297800K .......... .......... .......... .......... .......... 61% 7.58M 18s
297850K .......... .......... .......... .......... .......... 61% 6.51M 18s
297900K .......... .......... .......... .......... .......... 61% 6.52M 18s
297950K .......... .......... .......... .......... .......... 62% 5.22M 18s
298000K .......... .......... .......... .......... .......... 62% 7.58M 18s
298050K .......... .......... .......... .......... .......... 62% 16.6M 18s
298100K .......... .......... .......... .......... .......... 62% 15.2M 18s
298150K .......... .......... .......... .......... .......... 62% 24.0M 18s
298200K .......... .......... .......... .......... .......... 62% 17.6M 18s
298250K .......... .......... .......... .......... .......... 62% 9.92M 18s
298300K .......... .......... .......... .......... .......... 62% 14.5M 18s
298350K .......... .......... .......... .......... .......... 62% 8.99M 18s
298400K .......... .......... .......... .......... .......... 62% 10.8M 18s
298450K .......... .......... .......... .......... .......... 62% 9.74M 18s
298500K .......... .......... .......... .......... .......... 62% 10.6M 18s
298550K .......... .......... .......... .......... .......... 62% 9.35M 18s
298600K .......... .......... .......... .......... .......... 62% 6.64M 18s
298650K .......... .......... .......... .......... .......... 62% 9.96M 18s
298700K .......... .......... .......... .......... .......... 62% 11.0M 18s
298750K .......... .......... .......... .......... .......... 62% 13.0M 18s
298800K .......... .......... .......... .......... .......... 62% 10.2M 18s
298850K .......... .......... .......... .......... .......... 62% 12.1M 18s
298900K .......... .......... .......... .......... .......... 62% 9.57M 18s
298950K .......... .......... .......... .......... .......... 62% 8.89M 18s
299000K .......... .......... .......... .......... .......... 62% 9.72M 18s
299050K .......... .......... .......... .......... .......... 62% 10.0M 18s
299100K .......... .......... .......... .......... .......... 62% 8.28M 18s
299150K .......... .......... .......... .......... .......... 62% 9.34M 18s
299200K .......... .......... .......... .......... .......... 62% 7.97M 18s
299250K .......... .......... .......... .......... .......... 62% 14.5M 18s
299300K .......... .......... .......... .......... .......... 62% 16.1M 18s
299350K .......... .......... .......... .......... .......... 62% 18.4M 18s
299400K .......... .......... .......... .......... .......... 62% 14.2M 18s
299450K .......... .......... .......... .......... .......... 62% 20.4M 18s
299500K .......... .......... .......... .......... .......... 62% 17.8M 18s
299550K .......... .......... .......... .......... .......... 62% 17.9M 18s
299600K .......... .......... .......... .......... .......... 62% 12.7M 18s
299650K .......... .......... .......... .......... .......... 62% 13.6M 18s
299700K .......... .......... .......... .......... .......... 62% 11.8M 17s
299750K .......... .......... .......... .......... .......... 62% 11.3M 17s
299800K .......... .......... .......... .......... .......... 62% 17.1M 17s
299850K .......... .......... .......... .......... .......... 62% 11.5M 17s
299900K .......... .......... .......... .......... .......... 62% 12.6M 17s
299950K .......... .......... .......... .......... .......... 62% 12.7M 17s
300000K .......... .......... .......... .......... .......... 62% 8.53M 17s
300050K .......... .......... .......... .......... .......... 62% 15.5M 17s
300100K .......... .......... .......... .......... .......... 62% 7.10M 17s
300150K .......... .......... .......... .......... .......... 62% 8.57M 17s
300200K .......... .......... .......... .......... .......... 62% 7.87M 17s
300250K .......... .......... .......... .......... .......... 62% 9.87M 17s
300300K .......... .......... .......... .......... .......... 62% 11.3M 17s
300350K .......... .......... .......... .......... .......... 62% 10.7M 17s
300400K .......... .......... .......... .......... .......... 62% 10.0M 17s
300450K .......... .......... .......... .......... .......... 62% 9.47M 17s
300500K .......... .......... .......... .......... .......... 62% 10.3M 17s
300550K .......... .......... .......... .......... .......... 62% 13.6M 17s
300600K .......... .......... .......... .......... .......... 62% 7.93M 17s
300650K .......... .......... .......... .......... .......... 62% 12.6M 17s
300700K .......... .......... .......... .......... .......... 62% 34.9M 17s
300750K .......... .......... .......... .......... .......... 62% 30.1M 17s
300800K .......... .......... .......... .......... .......... 62% 31.7M 17s
300850K .......... .......... .......... .......... .......... 62% 21.5M 17s
300900K .......... .......... .......... .......... .......... 62% 26.9M 17s
300950K .......... .......... .......... .......... .......... 62% 28.1M 17s
301000K .......... .......... .......... .......... .......... 62% 27.6M 17s
301050K .......... .......... .......... .......... .......... 62% 14.7M 17s
301100K .......... .......... .......... .......... .......... 62% 22.4M 17s
301150K .......... .......... .......... .......... .......... 62% 12.7M 17s
301200K .......... .......... .......... .......... .......... 62% 13.6M 17s
301250K .......... .......... .......... .......... .......... 62% 13.8M 17s
301300K .......... .......... .......... .......... .......... 62% 15.6M 17s
301350K .......... .......... .......... .......... .......... 62% 11.5M 17s
301400K .......... .......... .......... .......... .......... 62% 10.1M 17s
301450K .......... .......... .......... .......... .......... 62% 8.19M 17s
301500K .......... .......... .......... .......... .......... 62% 10.5M 17s
301550K .......... .......... .......... .......... .......... 62% 13.7M 17s
301600K .......... .......... .......... .......... .......... 62% 8.27M 17s
301650K .......... .......... .......... .......... .......... 62% 13.8M 17s
301700K .......... .......... .......... .......... .......... 62% 31.7M 17s
301750K .......... .......... .......... .......... .......... 62% 14.9M 17s
301800K .......... .......... .......... .......... .......... 62% 53.7M 17s
301850K .......... .......... .......... .......... .......... 62% 16.7M 17s
301900K .......... .......... .......... .......... .......... 62% 18.6M 17s
301950K .......... .......... .......... .......... .......... 62% 23.6M 17s
302000K .......... .......... .......... .......... .......... 62% 17.1M 17s
302050K .......... .......... .......... .......... .......... 62% 18.7M 17s
302100K .......... .......... .......... .......... .......... 62% 14.1M 17s
302150K .......... .......... .......... .......... .......... 62% 13.2M 17s
302200K .......... .......... .......... .......... .......... 62% 9.19M 17s
302250K .......... .......... .......... .......... .......... 62% 14.3M 17s
302300K .......... .......... .......... .......... .......... 62% 11.9M 17s
302350K .......... .......... .......... .......... .......... 62% 6.95M 17s
302400K .......... .......... .......... .......... .......... 62% 6.99M 17s
302450K .......... .......... .......... .......... .......... 62% 12.7M 17s
302500K .......... .......... .......... .......... .......... 62% 8.65M 17s
302550K .......... .......... .......... .......... .......... 62% 11.3M 17s
302600K .......... .......... .......... .......... .......... 62% 8.90M 17s
302650K .......... .......... .......... .......... .......... 62% 11.4M 17s
302700K .......... .......... .......... .......... .......... 62% 8.71M 17s
302750K .......... .......... .......... .......... .......... 63% 10.8M 17s
302800K .......... .......... .......... .......... .......... 63% 10.4M 17s
302850K .......... .......... .......... .......... .......... 63% 13.7M 17s
302900K .......... .......... .......... .......... .......... 63% 18.8M 17s
302950K .......... .......... .......... .......... .......... 63% 24.9M 17s
303000K .......... .......... .......... .......... .......... 63% 32.8M 17s
303050K .......... .......... .......... .......... .......... 63% 29.2M 17s
303100K .......... .......... .......... .......... .......... 63% 12.8M 17s
303150K .......... .......... .......... .......... .......... 63% 25.2M 17s
303200K .......... .......... .......... .......... .......... 63% 12.9M 17s
303250K .......... .......... .......... .......... .......... 63% 28.5M 17s
303300K .......... .......... .......... .......... .......... 63% 19.6M 17s
303350K .......... .......... .......... .......... .......... 63% 13.9M 17s
303400K .......... .......... .......... .......... .......... 63% 14.7M 17s
303450K .......... .......... .......... .......... .......... 63% 14.0M 17s
303500K .......... .......... .......... .......... .......... 63% 16.0M 17s
303550K .......... .......... .......... .......... .......... 63% 12.9M 17s
303600K .......... .......... .......... .......... .......... 63% 9.76M 17s
303650K .......... .......... .......... .......... .......... 63% 14.6M 17s
303700K .......... .......... .......... .......... .......... 63% 13.7M 17s
303750K .......... .......... .......... .......... .......... 63% 9.42M 17s
303800K .......... .......... .......... .......... .......... 63% 16.5M 17s
303850K .......... .......... .......... .......... .......... 63% 15.3M 17s
303900K .......... .......... .......... .......... .......... 63% 50.4M 17s
303950K .......... .......... .......... .......... .......... 63% 27.7M 17s
304000K .......... .......... .......... .......... .......... 63% 31.2M 17s
304050K .......... .......... .......... .......... .......... 63% 20.6M 17s
304100K .......... .......... .......... .......... .......... 63% 40.0M 17s
304150K .......... .......... .......... .......... .......... 63% 47.3M 17s
304200K .......... .......... .......... .......... .......... 63% 23.0M 17s
304250K .......... .......... .......... .......... .......... 63% 23.0M 17s
304300K .......... .......... .......... .......... .......... 63% 16.4M 17s
304350K .......... .......... .......... .......... .......... 63% 38.5M 17s
304400K .......... .......... .......... .......... .......... 63% 18.9M 17s
304450K .......... .......... .......... .......... .......... 63% 15.6M 17s
304500K .......... .......... .......... .......... .......... 63% 31.7M 17s
304550K .......... .......... .......... .......... .......... 63% 14.7M 17s
304600K .......... .......... .......... .......... .......... 63% 18.4M 17s
304650K .......... .......... .......... .......... .......... 63% 18.0M 17s
304700K .......... .......... .......... .......... .......... 63% 16.8M 17s
304750K .......... .......... .......... .......... .......... 63% 11.1M 17s
304800K .......... .......... .......... .......... .......... 63% 29.0M 17s
304850K .......... .......... .......... .......... .......... 63% 12.1M 17s
304900K .......... .......... .......... .......... .......... 63% 14.5M 17s
304950K .......... .......... .......... .......... .......... 63% 11.4M 17s
305000K .......... .......... .......... .......... .......... 63% 14.6M 17s
305050K .......... .......... .......... .......... .......... 63% 10.8M 17s
305100K .......... .......... .......... .......... .......... 63% 9.08M 17s
305150K .......... .......... .......... .......... .......... 63% 11.2M 17s
305200K .......... .......... .......... .......... .......... 63% 9.21M 17s
305250K .......... .......... .......... .......... .......... 63% 9.75M 17s
305300K .......... .......... .......... .......... .......... 63% 9.08M 17s
305350K .......... .......... .......... .......... .......... 63% 10.8M 17s
305400K .......... .......... .......... .......... .......... 63% 22.1M 17s
305450K .......... .......... .......... .......... .......... 63% 20.0M 17s
305500K .......... .......... .......... .......... .......... 63% 25.8M 17s
305550K .......... .......... .......... .......... .......... 63% 22.7M 17s
305600K .......... .......... .......... .......... .......... 63% 22.2M 17s
305650K .......... .......... .......... .......... .......... 63% 20.0M 17s
305700K .......... .......... .......... .......... .......... 63% 17.8M 17s
305750K .......... .......... .......... .......... .......... 63% 19.6M 17s
305800K .......... .......... .......... .......... .......... 63% 19.9M 17s
305850K .......... .......... .......... .......... .......... 63% 19.2M 17s
305900K .......... .......... .......... .......... .......... 63% 18.8M 17s
305950K .......... .......... .......... .......... .......... 63% 17.7M 17s
306000K .......... .......... .......... .......... .......... 63% 18.2M 17s
306050K .......... .......... .......... .......... .......... 63% 18.6M 17s
306100K .......... .......... .......... .......... .......... 63% 19.6M 17s
306150K .......... .......... .......... .......... .......... 63% 23.6M 17s
306200K .......... .......... .......... .......... .......... 63% 20.8M 17s
306250K .......... .......... .......... .......... .......... 63% 31.3M 17s
306300K .......... .......... .......... .......... .......... 63% 15.7M 17s
306350K .......... .......... .......... .......... .......... 63% 65.9M 17s
306400K .......... .......... .......... .......... .......... 63% 78.1M 17s
306450K .......... .......... .......... .......... .......... 63% 16.0M 17s
306500K .......... .......... .......... .......... .......... 63% 37.1M 17s
306550K .......... .......... .......... .......... .......... 63% 26.7M 17s
306600K .......... .......... .......... .......... .......... 63% 23.6M 17s
306650K .......... .......... .......... .......... .......... 63% 18.9M 17s
306700K .......... .......... .......... .......... .......... 63% 12.8M 17s
306750K .......... .......... .......... .......... .......... 63% 17.5M 17s
306800K .......... .......... .......... .......... .......... 63% 11.6M 17s
306850K .......... .......... .......... .......... .......... 63% 16.6M 17s
306900K .......... .......... .......... .......... .......... 63% 12.6M 17s
306950K .......... .......... .......... .......... .......... 63% 11.9M 17s
307000K .......... .......... .......... .......... .......... 63% 18.2M 17s
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307100K .......... .......... .......... .......... .......... 63% 12.1M 17s
307150K .......... .......... .......... .......... .......... 63% 26.5M 17s
307200K .......... .......... .......... .......... .......... 63% 14.5M 17s
307250K .......... .......... .......... .......... .......... 63% 31.9M 17s
307300K .......... .......... .......... .......... .......... 63% 34.4M 17s
307350K .......... .......... .......... .......... .......... 63% 47.5M 17s
307400K .......... .......... .......... .......... .......... 63% 33.5M 17s
307450K .......... .......... .......... .......... .......... 63% 26.5M 17s
307500K .......... .......... .......... .......... .......... 63% 20.1M 17s
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307650K .......... .......... .......... .......... .......... 64% 21.6M 17s
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308000K .......... .......... .......... .......... .......... 64% 21.0M 17s
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308100K .......... .......... .......... .......... .......... 64% 19.1M 17s
308150K .......... .......... .......... .......... .......... 64% 19.9M 17s
308200K .......... .......... .......... .......... .......... 64% 30.6M 17s
308250K .......... .......... .......... .......... .......... 64% 24.5M 17s
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309100K .......... .......... .......... .......... .......... 64% 21.6M 16s
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309200K .......... .......... .......... .......... .......... 64% 36.8M 16s
309250K .......... .......... .......... .......... .......... 64% 20.7M 16s
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310000K .......... .......... .......... .......... .......... 64% 80.7M 16s
310050K .......... .......... .......... .......... .......... 64% 34.6M 16s
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310200K .......... .......... .......... .......... .......... 64% 15.8M 16s
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310300K .......... .......... .......... .......... .......... 64% 19.7M 16s
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310400K .......... .......... .......... .......... .......... 64% 20.0M 16s
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310500K .......... .......... .......... .......... .......... 64% 19.9M 16s
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310600K .......... .......... .......... .......... .......... 64% 19.6M 16s
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310800K .......... .......... .......... .......... .......... 64% 24.0M 16s
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310900K .......... .......... .......... .......... .......... 64% 79.4M 16s
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311000K .......... .......... .......... .......... .......... 64% 28.7M 16s
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311100K .......... .......... .......... .......... .......... 64% 21.5M 16s
311150K .......... .......... .......... .......... .......... 64% 23.8M 16s
311200K .......... .......... .......... .......... .......... 64% 21.0M 16s
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311400K .......... .......... .......... .......... .......... 64% 18.9M 16s
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311800K .......... .......... .......... .......... .......... 64% 9.87M 16s
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320250K .......... .......... .......... .......... .......... 66% 78.4M 15s
320300K .......... .......... .......... .......... .......... 66% 68.9M 15s
320350K .......... .......... .......... .......... .......... 66% 25.3M 15s
320400K .......... .......... .......... .......... .......... 66% 35.1M 15s
320450K .......... .......... .......... .......... .......... 66% 23.1M 15s
320500K .......... .......... .......... .......... .......... 66% 38.8M 15s
320550K .......... .......... .......... .......... .......... 66% 27.1M 15s
320600K .......... .......... .......... .......... .......... 66% 29.0M 15s
320650K .......... .......... .......... .......... .......... 66% 38.1M 15s
320700K .......... .......... .......... .......... .......... 66% 19.7M 15s
320750K .......... .......... .......... .......... .......... 66% 32.0M 15s
320800K .......... .......... .......... .......... .......... 66% 28.3M 15s
320850K .......... .......... .......... .......... .......... 66% 17.6M 15s
320900K .......... .......... .......... .......... .......... 66% 35.6M 15s
320950K .......... .......... .......... .......... .......... 66% 22.1M 15s
321000K .......... .......... .......... .......... .......... 66% 31.1M 15s
321050K .......... .......... .......... .......... .......... 66% 29.3M 15s
321100K .......... .......... .......... .......... .......... 66% 27.0M 15s
321150K .......... .......... .......... .......... .......... 66% 16.4M 15s
321200K .......... .......... .......... .......... .......... 66% 25.4M 15s
321250K .......... .......... .......... .......... .......... 66% 27.1M 15s
321300K .......... .......... .......... .......... .......... 66% 13.6M 15s
321350K .......... .......... .......... .......... .......... 66% 31.9M 15s
321400K .......... .......... .......... .......... .......... 66% 31.1M 15s
321450K .......... .......... .......... .......... .......... 66% 11.1M 15s
321500K .......... .......... .......... .......... .......... 66% 19.8M 15s
321550K .......... .......... .......... .......... .......... 66% 17.2M 15s
321600K .......... .......... .......... .......... .......... 66% 11.8M 15s
321650K .......... .......... .......... .......... .......... 66% 13.5M 15s
321700K .......... .......... .......... .......... .......... 66% 11.9M 15s
321750K .......... .......... .......... .......... .......... 66% 13.1M 15s
321800K .......... .......... .......... .......... .......... 66% 15.0M 15s
321850K .......... .......... .......... .......... .......... 66% 13.6M 15s
321900K .......... .......... .......... .......... .......... 66% 12.6M 15s
321950K .......... .......... .......... .......... .......... 66% 8.98M 15s
322000K .......... .......... .......... .......... .......... 67% 24.4M 15s
322050K .......... .......... .......... .......... .......... 67% 17.7M 15s
322100K .......... .......... .......... .......... .......... 67% 18.3M 15s
322150K .......... .......... .......... .......... .......... 67% 22.2M 15s
322200K .......... .......... .......... .......... .......... 67% 15.2M 15s
322250K .......... .......... .......... .......... .......... 67% 17.2M 15s
322300K .......... .......... .......... .......... .......... 67% 21.1M 15s
322350K .......... .......... .......... .......... .......... 67% 16.0M 15s
322400K .......... .......... .......... .......... .......... 67% 19.9M 15s
322450K .......... .......... .......... .......... .......... 67% 16.4M 15s
322500K .......... .......... .......... .......... .......... 67% 16.6M 15s
322550K .......... .......... .......... .......... .......... 67% 20.2M 15s
322600K .......... .......... .......... .......... .......... 67% 17.4M 15s
322650K .......... .......... .......... .......... .......... 67% 17.1M 15s
322700K .......... .......... .......... .......... .......... 67% 9.54M 15s
322750K .......... .......... .......... .......... .......... 67% 10.9M 15s
322800K .......... .......... .......... .......... .......... 67% 17.4M 15s
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322900K .......... .......... .......... .......... .......... 67% 16.7M 15s
322950K .......... .......... .......... .......... .......... 67% 18.5M 15s
323000K .......... .......... .......... .......... .......... 67% 19.5M 15s
323050K .......... .......... .......... .......... .......... 67% 17.6M 15s
323100K .......... .......... .......... .......... .......... 67% 17.3M 15s
323150K .......... .......... .......... .......... .......... 67% 22.1M 15s
323200K .......... .......... .......... .......... .......... 67% 18.1M 15s
323250K .......... .......... .......... .......... .......... 67% 15.7M 15s
323300K .......... .......... .......... .......... .......... 67% 18.2M 15s
323350K .......... .......... .......... .......... .......... 67% 11.8M 15s
323400K .......... .......... .......... .......... .......... 67% 19.1M 15s
323450K .......... .......... .......... .......... .......... 67% 12.7M 15s
323500K .......... .......... .......... .......... .......... 67% 25.3M 15s
323550K .......... .......... .......... .......... .......... 67% 14.2M 15s
323600K .......... .......... .......... .......... .......... 67% 16.1M 15s
323650K .......... .......... .......... .......... .......... 67% 26.4M 15s
323700K .......... .......... .......... .......... .......... 67% 18.8M 15s
323750K .......... .......... .......... .......... .......... 67% 19.6M 15s
323800K .......... .......... .......... .......... .......... 67% 15.5M 15s
323850K .......... .......... .......... .......... .......... 67% 12.6M 15s
323900K .......... .......... .......... .......... .......... 67% 20.1M 15s
323950K .......... .......... .......... .......... .......... 67% 14.4M 15s
324000K .......... .......... .......... .......... .......... 67% 13.4M 15s
324050K .......... .......... .......... .......... .......... 67% 21.6M 15s
324100K .......... .......... .......... .......... .......... 67% 14.6M 15s
324150K .......... .......... .......... .......... .......... 67% 18.0M 15s
324200K .......... .......... .......... .......... .......... 67% 15.9M 15s
324250K .......... .......... .......... .......... .......... 67% 17.5M 15s
324300K .......... .......... .......... .......... .......... 67% 23.6M 15s
324350K .......... .......... .......... .......... .......... 67% 13.3M 15s
324400K .......... .......... .......... .......... .......... 67% 74.1M 15s
324450K .......... .......... .......... .......... .......... 67% 20.1M 15s
324500K .......... .......... .......... .......... .......... 67% 22.8M 15s
324550K .......... .......... .......... .......... .......... 67% 31.6M 15s
324600K .......... .......... .......... .......... .......... 67% 17.9M 15s
324650K .......... .......... .......... .......... .......... 67% 19.9M 15s
324700K .......... .......... .......... .......... .......... 67% 18.0M 15s
324750K .......... .......... .......... .......... .......... 67% 19.1M 15s
324800K .......... .......... .......... .......... .......... 67% 20.0M 15s
324850K .......... .......... .......... .......... .......... 67% 13.3M 15s
324900K .......... .......... .......... .......... .......... 67% 17.2M 15s
324950K .......... .......... .......... .......... .......... 67% 17.2M 15s
325000K .......... .......... .......... .......... .......... 67% 21.0M 15s
325050K .......... .......... .......... .......... .......... 67% 19.6M 15s
325100K .......... .......... .......... .......... .......... 67% 15.3M 15s
325150K .......... .......... .......... .......... .......... 67% 14.0M 15s
325200K .......... .......... .......... .......... .......... 67% 12.7M 15s
325250K .......... .......... .......... .......... .......... 67% 13.4M 15s
325300K .......... .......... .......... .......... .......... 67% 87.8M 15s
325350K .......... .......... .......... .......... .......... 67% 10.5M 15s
325400K .......... .......... .......... .......... .......... 67% 35.3M 14s
325450K .......... .......... .......... .......... .......... 67% 15.9M 14s
325500K .......... .......... .......... .......... .......... 67% 21.4M 14s
325550K .......... .......... .......... .......... .......... 67% 14.2M 14s
325600K .......... .......... .......... .......... .......... 67% 17.9M 14s
325650K .......... .......... .......... .......... .......... 67% 15.6M 14s
325700K .......... .......... .......... .......... .......... 67% 13.1M 14s
325750K .......... .......... .......... .......... .......... 67% 16.5M 14s
325800K .......... .......... .......... .......... .......... 67% 19.4M 14s
325850K .......... .......... .......... .......... .......... 67% 11.5M 14s
325900K .......... .......... .......... .......... .......... 67% 15.8M 14s
325950K .......... .......... .......... .......... .......... 67% 13.9M 14s
326000K .......... .......... .......... .......... .......... 67% 25.9M 14s
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326100K .......... .......... .......... .......... .......... 67% 67.0M 14s
326150K .......... .......... .......... .......... .......... 67% 69.3M 14s
326200K .......... .......... .......... .......... .......... 67% 11.1M 14s
326250K .......... .......... .......... .......... .......... 67% 69.8M 14s
326300K .......... .......... .......... .......... .......... 67% 84.0M 14s
326350K .......... .......... .......... .......... .......... 67% 46.7M 14s
326400K .......... .......... .......... .......... .......... 67% 34.7M 14s
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326500K .......... .......... .......... .......... .......... 67% 30.8M 14s
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326650K .......... .......... .......... .......... .......... 67% 29.9M 14s
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326800K .......... .......... .......... .......... .......... 68% 26.7M 14s
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326900K .......... .......... .......... .......... .......... 68% 30.3M 14s
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327000K .......... .......... .......... .......... .......... 68% 27.8M 14s
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327100K .......... .......... .......... .......... .......... 68% 17.6M 14s
327150K .......... .......... .......... .......... .......... 68% 29.8M 14s
327200K .......... .......... .......... .......... .......... 68% 16.2M 14s
327250K .......... .......... .......... .......... .......... 68% 79.0M 14s
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327400K .......... .......... .......... .......... .......... 68% 85.4M 14s
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327500K .......... .......... .......... .......... .......... 68% 14.1M 14s
327550K .......... .......... .......... .......... .......... 68% 81.5M 14s
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327800K .......... .......... .......... .......... .......... 68% 68.0M 14s
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327900K .......... .......... .......... .......... .......... 68%  119M 14s
327950K .......... .......... .......... .......... .......... 68% 27.0M 14s
328000K .......... .......... .......... .......... .......... 68% 41.5M 14s
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328100K .......... .......... .......... .......... .......... 68% 22.1M 14s
328150K .......... .......... .......... .......... .......... 68% 33.1M 14s
328200K .......... .......... .......... .......... .......... 68% 20.5M 14s
328250K .......... .......... .......... .......... .......... 68% 37.5M 14s
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328600K .......... .......... .......... .......... .......... 68% 31.9M 14s
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329000K .......... .......... .......... .......... .......... 68% 16.4M 14s
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329100K .......... .......... .......... .......... .......... 68% 37.9M 14s
329150K .......... .......... .......... .......... .......... 68% 56.2M 14s
329200K .......... .......... .......... .......... .......... 68% 30.8M 14s
329250K .......... .......... .......... .......... .......... 68% 47.3M 14s
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330000K .......... .......... .......... .......... .......... 68% 31.1M 14s
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330100K .......... .......... .......... .......... .......... 68% 35.2M 14s
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330200K .......... .......... .......... .......... .......... 68% 40.1M 14s
330250K .......... .......... .......... .......... .......... 68%  113M 14s
330300K .......... .......... .......... .......... .......... 68% 39.7M 14s
330350K .......... .......... .......... .......... .......... 68% 56.8M 14s
330400K .......... .......... .......... .......... .......... 68% 54.6M 14s
330450K .......... .......... .......... .......... .......... 68% 51.6M 14s
330500K .......... .......... .......... .......... .......... 68% 31.7M 14s
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330600K .......... .......... .......... .......... .......... 68% 29.3M 14s
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330700K .......... .......... .......... .......... .......... 68% 29.9M 14s
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330800K .......... .......... .......... .......... .......... 68% 30.5M 14s
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330900K .......... .......... .......... .......... .......... 68% 33.0M 14s
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331450K .......... .......... .......... .......... .......... 68% 29.9M 14s
331500K .......... .......... .......... .......... .......... 68% 30.8M 14s
331550K .......... .......... .......... .......... .......... 68% 42.0M 14s
331600K .......... .......... .......... .......... .......... 69% 37.3M 14s
331650K .......... .......... .......... .......... .......... 69% 95.4M 14s
331700K .......... .......... .......... .......... .......... 69% 13.9M 14s
331750K .......... .......... .......... .......... .......... 69%  141M 14s
331800K .......... .......... .......... .......... .......... 69% 23.8M 14s
331850K .......... .......... .......... .......... .......... 69%  124M 14s
331900K .......... .......... .......... .......... .......... 69%  145M 14s
331950K .......... .......... .......... .......... .......... 69%  126M 14s
332000K .......... .......... .......... .......... .......... 69% 37.9M 14s
332050K .......... .......... .......... .......... .......... 69%  112M 14s
332100K .......... .......... .......... .......... .......... 69% 30.7M 14s
332150K .......... .......... .......... .......... .......... 69% 33.4M 14s
332200K .......... .......... .......... .......... .......... 69% 27.1M 14s
332250K .......... .......... .......... .......... .......... 69% 38.8M 14s
332300K .......... .......... .......... .......... .......... 69% 38.3M 14s
332350K .......... .......... .......... .......... .......... 69% 28.9M 14s
332400K .......... .......... .......... .......... .......... 69% 42.1M 14s
332450K .......... .......... .......... .......... .......... 69% 36.4M 14s
332500K .......... .......... .......... .......... .......... 69% 28.0M 14s
332550K .......... .......... .......... .......... .......... 69% 48.6M 14s
332600K .......... .......... .......... .......... .......... 69% 32.0M 14s
332650K .......... .......... .......... .......... .......... 69% 42.4M 14s
332700K .......... .......... .......... .......... .......... 69% 26.2M 14s
332750K .......... .......... .......... .......... .......... 69% 29.0M 14s
332800K .......... .......... .......... .......... .......... 69% 37.9M 14s
332850K .......... .......... .......... .......... .......... 69% 33.9M 14s
332900K .......... .......... .......... .......... .......... 69% 29.3M 14s
332950K .......... .......... .......... .......... .......... 69% 22.3M 14s
333000K .......... .......... .......... .......... .......... 69% 35.7M 14s
333050K .......... .......... .......... .......... .......... 69% 31.4M 14s
333100K .......... .......... .......... .......... .......... 69% 33.8M 14s
333150K .......... .......... .......... .......... .......... 69% 19.7M 14s
333200K .......... .......... .......... .......... .......... 69% 28.8M 14s
333250K .......... .......... .......... .......... .......... 69% 26.0M 14s
333300K .......... .......... .......... .......... .......... 69% 33.3M 14s
333350K .......... .......... .......... .......... .......... 69% 97.9M 14s
333400K .......... .......... .......... .......... .......... 69% 15.4M 14s
333450K .......... .......... .......... .......... .......... 69% 59.1M 14s
333500K .......... .......... .......... .......... .......... 69% 39.4M 14s
333550K .......... .......... .......... .......... .......... 69% 29.8M 14s
333600K .......... .......... .......... .......... .......... 69% 79.0M 14s
333650K .......... .......... .......... .......... .......... 69% 29.8M 14s
333700K .......... .......... .......... .......... .......... 69% 32.4M 14s
333750K .......... .......... .......... .......... .......... 69% 30.4M 13s
333800K .......... .......... .......... .......... .......... 69% 29.4M 13s
333850K .......... .......... .......... .......... .......... 69% 28.4M 13s
333900K .......... .......... .......... .......... .......... 69% 21.1M 13s
333950K .......... .......... .......... .......... .......... 69% 31.8M 13s
334000K .......... .......... .......... .......... .......... 69% 34.0M 13s
334050K .......... .......... .......... .......... .......... 69% 24.8M 13s
334100K .......... .......... .......... .......... .......... 69% 30.2M 13s
334150K .......... .......... .......... .......... .......... 69% 24.6M 13s
334200K .......... .......... .......... .......... .......... 69% 27.0M 13s
334250K .......... .......... .......... .......... .......... 69% 28.8M 13s
334300K .......... .......... .......... .......... .......... 69% 31.8M 13s
334350K .......... .......... .......... .......... .......... 69% 26.8M 13s
334400K .......... .......... .......... .......... .......... 69% 22.8M 13s
334450K .......... .......... .......... .......... .......... 69% 28.2M 13s
334500K .......... .......... .......... .......... .......... 69% 29.8M 13s
334550K .......... .......... .......... .......... .......... 69% 27.5M 13s
334600K .......... .......... .......... .......... .......... 69% 34.1M 13s
334650K .......... .......... .......... .......... .......... 69% 55.9M 13s
334700K .......... .......... .......... .......... .......... 69% 15.4M 13s
334750K .......... .......... .......... .......... .......... 69%  115M 13s
334800K .......... .......... .......... .......... .......... 69% 36.1M 13s
334850K .......... .......... .......... .......... .......... 69% 28.8M 13s
334900K .......... .......... .......... .......... .......... 69%  113M 13s
334950K .......... .......... .......... .......... .......... 69% 31.4M 13s
335000K .......... .......... .......... .......... .......... 69% 64.3M 13s
335050K .......... .......... .......... .......... .......... 69% 22.3M 13s
335100K .......... .......... .......... .......... .......... 69% 23.2M 13s
335150K .......... .......... .......... .......... .......... 69% 30.2M 13s
335200K .......... .......... .......... .......... .......... 69% 19.9M 13s
335250K .......... .......... .......... .......... .......... 69% 29.5M 13s
335300K .......... .......... .......... .......... .......... 69% 20.6M 13s
335350K .......... .......... .......... .......... .......... 69% 19.0M 13s
335400K .......... .......... .......... .......... .......... 69% 19.1M 13s
335450K .......... .......... .......... .......... .......... 69% 17.2M 13s
335500K .......... .......... .......... .......... .......... 69% 18.6M 13s
335550K .......... .......... .......... .......... .......... 69% 14.5M 13s
335600K .......... .......... .......... .......... .......... 69% 17.4M 13s
335650K .......... .......... .......... .......... .......... 69% 25.8M 13s
335700K .......... .......... .......... .......... .......... 69% 16.5M 13s
335750K .......... .......... .......... .......... .......... 69% 10.1M 13s
335800K .......... .......... .......... .......... .......... 69% 28.9M 13s
335850K .......... .......... .......... .......... .......... 69% 19.7M 13s
335900K .......... .......... .......... .......... .......... 69% 22.3M 13s
335950K .......... .......... .......... .......... .......... 69% 17.2M 13s
336000K .......... .......... .......... .......... .......... 69% 17.9M 13s
336050K .......... .......... .......... .......... .......... 69% 18.7M 13s
336100K .......... .......... .......... .......... .......... 69% 17.1M 13s
336150K .......... .......... .......... .......... .......... 69% 15.2M 13s
336200K .......... .......... .......... .......... .......... 69% 18.3M 13s
336250K .......... .......... .......... .......... .......... 69% 14.4M 13s
336300K .......... .......... .......... .......... .......... 69% 19.8M 13s
336350K .......... .......... .......... .......... .......... 69% 12.3M 13s
336400K .......... .......... .......... .......... .......... 70% 15.8M 13s
336450K .......... .......... .......... .......... .......... 70% 11.4M 13s
336500K .......... .......... .......... .......... .......... 70% 10.6M 13s
336550K .......... .......... .......... .......... .......... 70% 23.4M 13s
336600K .......... .......... .......... .......... .......... 70% 19.4M 13s
336650K .......... .......... .......... .......... .......... 70% 23.9M 13s
336700K .......... .......... .......... .......... .......... 70% 13.5M 13s
336750K .......... .......... .......... .......... .......... 70% 21.2M 13s
336800K .......... .......... .......... .......... .......... 70% 12.3M 13s
336850K .......... .......... .......... .......... .......... 70% 15.2M 13s
336900K .......... .......... .......... .......... .......... 70% 15.8M 13s
336950K .......... .......... .......... .......... .......... 70% 17.6M 13s
337000K .......... .......... .......... .......... .......... 70% 11.8M 13s
337050K .......... .......... .......... .......... .......... 70% 18.2M 13s
337100K .......... .......... .......... .......... .......... 70% 13.1M 13s
337150K .......... .......... .......... .......... .......... 70% 14.5M 13s
337200K .......... .......... .......... .......... .......... 70% 13.0M 13s
337250K .......... .......... .......... .......... .......... 70% 79.5M 13s
337300K .......... .......... .......... .......... .......... 70% 15.7M 13s
337350K .......... .......... .......... .......... .......... 70% 18.8M 13s
337400K .......... .......... .......... .......... .......... 70% 22.6M 13s
337450K .......... .......... .......... .......... .......... 70% 13.3M 13s
337500K .......... .......... .......... .......... .......... 70% 15.8M 13s
337550K .......... .......... .......... .......... .......... 70% 11.8M 13s
337600K .......... .......... .......... .......... .......... 70% 14.4M 13s
337650K .......... .......... .......... .......... .......... 70% 13.9M 13s
337700K .......... .......... .......... .......... .......... 70% 16.1M 13s
337750K .......... .......... .......... .......... .......... 70% 14.6M 13s
337800K .......... .......... .......... .......... .......... 70% 19.3M 13s
337850K .......... .......... .......... .......... .......... 70% 14.1M 13s
337900K .......... .......... .......... .......... .......... 70% 29.6M 13s
337950K .......... .......... .......... .......... .......... 70% 25.1M 13s
338000K .......... .......... .......... .......... .......... 70% 25.8M 13s
338050K .......... .......... .......... .......... .......... 70% 14.1M 13s
338100K .......... .......... .......... .......... .......... 70% 71.3M 13s
338150K .......... .......... .......... .......... .......... 70% 80.2M 13s
338200K .......... .......... .......... .......... .......... 70% 22.0M 13s
338250K .......... .......... .......... .......... .......... 70% 74.9M 13s
338300K .......... .......... .......... .......... .......... 70% 37.6M 13s
338350K .......... .......... .......... .......... .......... 70% 24.0M 13s
338400K .......... .......... .......... .......... .......... 70% 23.6M 13s
338450K .......... .......... .......... .......... .......... 70% 24.0M 13s
338500K .......... .......... .......... .......... .......... 70% 32.6M 13s
338550K .......... .......... .......... .......... .......... 70% 21.2M 13s
338600K .......... .......... .......... .......... .......... 70% 29.5M 13s
338650K .......... .......... .......... .......... .......... 70% 27.2M 13s
338700K .......... .......... .......... .......... .......... 70% 21.0M 13s
338750K .......... .......... .......... .......... .......... 70% 33.1M 13s
338800K .......... .......... .......... .......... .......... 70% 17.8M 13s
338850K .......... .......... .......... .......... .......... 70% 34.0M 13s
338900K .......... .......... .......... .......... .......... 70% 30.9M 13s
338950K .......... .......... .......... .......... .......... 70% 23.4M 13s
339000K .......... .......... .......... .......... .......... 70% 27.1M 13s
339050K .......... .......... .......... .......... .......... 70% 25.5M 13s
339100K .......... .......... .......... .......... .......... 70% 23.8M 13s
339150K .......... .......... .......... .......... .......... 70% 34.4M 13s
339200K .......... .......... .......... .......... .......... 70% 28.0M 13s
339250K .......... .......... .......... .......... .......... 70% 22.2M 13s
339300K .......... .......... .......... .......... .......... 70% 18.2M 13s
339350K .......... .......... .......... .......... .......... 70% 65.2M 13s
339400K .......... .......... .......... .......... .......... 70% 22.6M 13s
339450K .......... .......... .......... .......... .......... 70% 35.3M 13s
339500K .......... .......... .......... .......... .......... 70% 38.6M 13s
339550K .......... .......... .......... .......... .......... 70% 29.8M 13s
339600K .......... .......... .......... .......... .......... 70% 20.0M 13s
339650K .......... .......... .......... .......... .......... 70% 16.5M 13s
339700K .......... .......... .......... .......... .......... 70% 18.1M 13s
339750K .......... .......... .......... .......... .......... 70% 20.4M 13s
339800K .......... .......... .......... .......... .......... 70% 19.3M 13s
339850K .......... .......... .......... .......... .......... 70% 14.2M 13s
339900K .......... .......... .......... .......... .......... 70% 16.5M 13s
339950K .......... .......... .......... .......... .......... 70% 17.2M 13s
340000K .......... .......... .......... .......... .......... 70% 19.3M 13s
340050K .......... .......... .......... .......... .......... 70% 18.7M 13s
340100K .......... .......... .......... .......... .......... 70% 16.1M 13s
340150K .......... .......... .......... .......... .......... 70% 17.3M 13s
340200K .......... .......... .......... .......... .......... 70% 13.6M 13s
340250K .......... .......... .......... .......... .......... 70% 46.5M 13s
340300K .......... .......... .......... .......... .......... 70% 17.1M 13s
340350K .......... .......... .......... .......... .......... 70% 9.54M 13s
340400K .......... .......... .......... .......... .......... 70% 74.0M 13s
340450K .......... .......... .......... .......... .......... 70% 32.9M 13s
340500K .......... .......... .......... .......... .......... 70% 70.9M 13s
340550K .......... .......... .......... .......... .......... 70% 26.7M 13s
340600K .......... .......... .......... .......... .......... 70% 22.3M 13s
340650K .......... .......... .......... .......... .......... 70% 20.8M 13s
340700K .......... .......... .......... .......... .......... 70% 18.0M 13s
340750K .......... .......... .......... .......... .......... 70% 18.4M 13s
340800K .......... .......... .......... .......... .......... 70% 19.0M 13s
340850K .......... .......... .......... .......... .......... 70% 19.2M 13s
340900K .......... .......... .......... .......... .......... 70% 19.0M 13s
340950K .......... .......... .......... .......... .......... 70% 21.2M 13s
341000K .......... .......... .......... .......... .......... 70% 25.3M 13s
341050K .......... .......... .......... .......... .......... 70% 27.9M 13s
341100K .......... .......... .......... .......... .......... 70% 14.1M 13s
341150K .......... .......... .......... .......... .......... 70% 29.1M 13s
341200K .......... .......... .......... .......... .......... 71% 16.5M 13s
341250K .......... .......... .......... .......... .......... 71% 27.4M 13s
341300K .......... .......... .......... .......... .......... 71% 26.1M 13s
341350K .......... .......... .......... .......... .......... 71% 66.6M 13s
341400K .......... .......... .......... .......... .......... 71% 13.5M 13s
341450K .......... .......... .......... .......... .......... 71% 63.2M 13s
341500K .......... .......... .......... .......... .......... 71% 38.5M 13s
341550K .......... .......... .......... .......... .......... 71% 35.6M 13s
341600K .......... .......... .......... .......... .......... 71% 54.7M 13s
341650K .......... .......... .......... .......... .......... 71% 28.9M 13s
341700K .......... .......... .......... .......... .......... 71% 27.0M 13s
341750K .......... .......... .......... .......... .......... 71% 25.2M 13s
341800K .......... .......... .......... .......... .......... 71% 27.5M 13s
341850K .......... .......... .......... .......... .......... 71% 18.8M 13s
341900K .......... .......... .......... .......... .......... 71% 20.3M 13s
341950K .......... .......... .......... .......... .......... 71% 19.9M 13s
342000K .......... .......... .......... .......... .......... 71% 18.5M 13s
342050K .......... .......... .......... .......... .......... 71% 20.0M 13s
342100K .......... .......... .......... .......... .......... 71% 18.3M 13s
342150K .......... .......... .......... .......... .......... 71% 17.0M 13s
342200K .......... .......... .......... .......... .......... 71% 19.2M 13s
342250K .......... .......... .......... .......... .......... 71% 16.6M 13s
342300K .......... .......... .......... .......... .......... 71% 19.8M 13s
342350K .......... .......... .......... .......... .......... 71% 21.2M 13s
342400K .......... .......... .......... .......... .......... 71% 22.1M 13s
342450K .......... .......... .......... .......... .......... 71% 20.3M 13s
342500K .......... .......... .......... .......... .......... 71% 22.9M 13s
342550K .......... .......... .......... .......... .......... 71% 19.6M 13s
342600K .......... .......... .......... .......... .......... 71% 19.1M 13s
342650K .......... .......... .......... .......... .......... 71% 15.9M 13s
342700K .......... .......... .......... .......... .......... 71% 91.6M 13s
342750K .......... .......... .......... .......... .......... 71% 29.3M 13s
342800K .......... .......... .......... .......... .......... 71% 45.4M 12s
342850K .......... .......... .......... .......... .......... 71% 24.4M 12s
342900K .......... .......... .......... .......... .......... 71% 23.3M 12s
342950K .......... .......... .......... .......... .......... 71% 19.8M 12s
343000K .......... .......... .......... .......... .......... 71% 37.0M 12s
343050K .......... .......... .......... .......... .......... 71% 21.5M 12s
343100K .......... .......... .......... .......... .......... 71% 21.6M 12s
343150K .......... .......... .......... .......... .......... 71% 33.3M 12s
343200K .......... .......... .......... .......... .......... 71% 22.2M 12s
343250K .......... .......... .......... .......... .......... 71% 24.5M 12s
343300K .......... .......... .......... .......... .......... 71% 26.9M 12s
343350K .......... .......... .......... .......... .......... 71% 22.9M 12s
343400K .......... .......... .......... .......... .......... 71% 26.9M 12s
343450K .......... .......... .......... .......... .......... 71% 20.3M 12s
343500K .......... .......... .......... .......... .......... 71% 26.7M 12s
343550K .......... .......... .......... .......... .......... 71% 20.1M 12s
343600K .......... .......... .......... .......... .......... 71% 23.9M 12s
343650K .......... .......... .......... .......... .......... 71% 25.9M 12s
343700K .......... .......... .......... .......... .......... 71% 24.6M 12s
343750K .......... .......... .......... .......... .......... 71% 63.7M 12s
343800K .......... .......... .......... .......... .......... 71% 30.1M 12s
343850K .......... .......... .......... .......... .......... 71% 18.3M 12s
343900K .......... .......... .......... .......... .......... 71% 30.7M 12s
343950K .......... .......... .......... .......... .......... 71% 22.1M 12s
344000K .......... .......... .......... .......... .......... 71% 76.4M 12s
344050K .......... .......... .......... .......... .......... 71% 26.9M 12s
344100K .......... .......... .......... .......... .......... 71% 37.6M 12s
344150K .......... .......... .......... .......... .......... 71% 27.9M 12s
344200K .......... .......... .......... .......... .......... 71% 20.2M 12s
344250K .......... .......... .......... .......... .......... 71% 19.7M 12s
344300K .......... .......... .......... .......... .......... 71% 31.9M 12s
344350K .......... .......... .......... .......... .......... 71% 18.8M 12s
344400K .......... .......... .......... .......... .......... 71% 19.5M 12s
344450K .......... .......... .......... .......... .......... 71% 23.1M 12s
344500K .......... .......... .......... .......... .......... 71% 21.3M 12s
344550K .......... .......... .......... .......... .......... 71% 30.2M 12s
344600K .......... .......... .......... .......... .......... 71% 23.2M 12s
344650K .......... .......... .......... .......... .......... 71% 22.7M 12s
344700K .......... .......... .......... .......... .......... 71% 20.9M 12s
344750K .......... .......... .......... .......... .......... 71% 24.2M 12s
344800K .......... .......... .......... .......... .......... 71% 32.9M 12s
344850K .......... .......... .......... .......... .......... 71% 22.2M 12s
344900K .......... .......... .......... .......... .......... 71% 21.2M 12s
344950K .......... .......... .......... .......... .......... 71% 29.2M 12s
345000K .......... .......... .......... .......... .......... 71% 13.8M 12s
345050K .......... .......... .......... .......... .......... 71% 64.8M 12s
345100K .......... .......... .......... .......... .......... 71% 23.4M 12s
345150K .......... .......... .......... .......... .......... 71% 22.1M 12s
345200K .......... .......... .......... .......... .......... 71% 25.6M 12s
345250K .......... .......... .......... .......... .......... 71% 41.2M 12s
345300K .......... .......... .......... .......... .......... 71% 22.1M 12s
345350K .......... .......... .......... .......... .......... 71% 26.7M 12s
345400K .......... .......... .......... .......... .......... 71% 19.4M 12s
345450K .......... .......... .......... .......... .......... 71% 18.8M 12s
345500K .......... .......... .......... .......... .......... 71% 21.3M 12s
345550K .......... .......... .......... .......... .......... 71% 33.4M 12s
345600K .......... .......... .......... .......... .......... 71% 20.0M 12s
345650K .......... .......... .......... .......... .......... 71% 21.5M 12s
345700K .......... .......... .......... .......... .......... 71% 13.3M 12s
345750K .......... .......... .......... .......... .......... 71% 17.4M 12s
345800K .......... .......... .......... .......... .......... 71% 20.8M 12s
345850K .......... .......... .......... .......... .......... 71% 24.3M 12s
345900K .......... .......... .......... .......... .......... 71% 16.9M 12s
345950K .......... .......... .......... .......... .......... 71% 15.2M 12s
346000K .......... .......... .......... .......... .......... 72% 25.8M 12s
346050K .......... .......... .......... .......... .......... 72% 72.9M 12s
346100K .......... .......... .......... .......... .......... 72% 9.96M 12s
346150K .......... .......... .......... .......... .......... 72% 72.9M 12s
346200K .......... .......... .......... .......... .......... 72% 28.6M 12s
346250K .......... .......... .......... .......... .......... 72% 20.6M 12s
346300K .......... .......... .......... .......... .......... 72% 77.4M 12s
346350K .......... .......... .......... .......... .......... 72% 19.5M 12s
346400K .......... .......... .......... .......... .......... 72% 36.1M 12s
346450K .......... .......... .......... .......... .......... 72% 19.6M 12s
346500K .......... .......... .......... .......... .......... 72% 20.3M 12s
346550K .......... .......... .......... .......... .......... 72% 19.2M 12s
346600K .......... .......... .......... .......... .......... 72% 16.1M 12s
346650K .......... .......... .......... .......... .......... 72% 17.9M 12s
346700K .......... .......... .......... .......... .......... 72% 16.4M 12s
346750K .......... .......... .......... .......... .......... 72% 18.1M 12s
346800K .......... .......... .......... .......... .......... 72% 22.5M 12s
346850K .......... .......... .......... .......... .......... 72% 21.1M 12s
346900K .......... .......... .......... .......... .......... 72% 19.0M 12s
346950K .......... .......... .......... .......... .......... 72% 25.3M 12s
347000K .......... .......... .......... .......... .......... 72% 19.6M 12s
347050K .......... .......... .......... .......... .......... 72% 31.6M 12s
347100K .......... .......... .......... .......... .......... 72% 14.6M 12s
347150K .......... .......... .......... .......... .......... 72% 25.2M 12s
347200K .......... .......... .......... .......... .......... 72% 17.5M 12s
347250K .......... .......... .......... .......... .......... 72% 29.1M 12s
347300K .......... .......... .......... .......... .......... 72% 16.1M 12s
347350K .......... .......... .......... .......... .......... 72% 56.6M 12s
347400K .......... .......... .......... .......... .......... 72% 18.2M 12s
347450K .......... .......... .......... .......... .......... 72% 17.2M 12s
347500K .......... .......... .......... .......... .......... 72% 18.1M 12s
347550K .......... .......... .......... .......... .......... 72% 17.2M 12s
347600K .......... .......... .......... .......... .......... 72% 12.4M 12s
347650K .......... .......... .......... .......... .......... 72% 12.9M 12s
347700K .......... .......... .......... .......... .......... 72% 14.3M 12s
347750K .......... .......... .......... .......... .......... 72% 16.3M 12s
347800K .......... .......... .......... .......... .......... 72% 12.1M 12s
347850K .......... .......... .......... .......... .......... 72% 15.3M 12s
347900K .......... .......... .......... .......... .......... 72% 18.3M 12s
347950K .......... .......... .......... .......... .......... 72% 12.8M 12s
348000K .......... .......... .......... .......... .......... 72% 17.3M 12s
348050K .......... .......... .......... .......... .......... 72% 13.4M 12s
348100K .......... .......... .......... .......... .......... 72% 22.1M 12s
348150K .......... .......... .......... .......... .......... 72% 23.4M 12s
348200K .......... .......... .......... .......... .......... 72% 15.0M 12s
348250K .......... .......... .......... .......... .......... 72% 16.2M 12s
348300K .......... .......... .......... .......... .......... 72% 18.8M 12s
348350K .......... .......... .......... .......... .......... 72% 11.2M 12s
348400K .......... .......... .......... .......... .......... 72% 19.4M 12s
348450K .......... .......... .......... .......... .......... 72% 9.03M 12s
348500K .......... .......... .......... .......... .......... 72% 18.2M 12s
348550K .......... .......... .......... .......... .......... 72% 12.8M 12s
348600K .......... .......... .......... .......... .......... 72% 10.8M 12s
348650K .......... .......... .......... .......... .......... 72% 11.8M 12s
348700K .......... .......... .......... .......... .......... 72% 20.3M 12s
348750K .......... .......... .......... .......... .......... 72% 11.5M 12s
348800K .......... .......... .......... .......... .......... 72% 12.6M 12s
348850K .......... .......... .......... .......... .......... 72% 25.5M 12s
348900K .......... .......... .......... .......... .......... 72% 23.2M 12s
348950K .......... .......... .......... .......... .......... 72% 15.0M 12s
349000K .......... .......... .......... .......... .......... 72% 21.1M 12s
349050K .......... .......... .......... .......... .......... 72% 20.8M 12s
349100K .......... .......... .......... .......... .......... 72% 20.2M 12s
349150K .......... .......... .......... .......... .......... 72% 19.2M 12s
349200K .......... .......... .......... .......... .......... 72% 13.9M 12s
349250K .......... .......... .......... .......... .......... 72% 17.9M 12s
349300K .......... .......... .......... .......... .......... 72% 19.9M 12s
349350K .......... .......... .......... .......... .......... 72% 14.8M 12s
349400K .......... .......... .......... .......... .......... 72% 17.6M 12s
349450K .......... .......... .......... .......... .......... 72% 12.5M 12s
349500K .......... .......... .......... .......... .......... 72% 33.7M 12s
349550K .......... .......... .......... .......... .......... 72% 29.3M 12s
349600K .......... .......... .......... .......... .......... 72% 30.1M 12s
349650K .......... .......... .......... .......... .......... 72% 29.0M 12s
349700K .......... .......... .......... .......... .......... 72%  152M 12s
349750K .......... .......... .......... .......... .......... 72% 28.5M 12s
349800K .......... .......... .......... .......... .......... 72% 15.6M 12s
349850K .......... .......... .......... .......... .......... 72% 16.7M 12s
349900K .......... .......... .......... .......... .......... 72% 53.3M 12s
349950K .......... .......... .......... .......... .......... 72% 31.3M 12s
350000K .......... .......... .......... .......... .......... 72% 46.5M 12s
350050K .......... .......... .......... .......... .......... 72% 25.2M 12s
350100K .......... .......... .......... .......... .......... 72% 23.1M 12s
350150K .......... .......... .......... .......... .......... 72% 20.6M 12s
350200K .......... .......... .......... .......... .......... 72% 21.0M 12s
350250K .......... .......... .......... .......... .......... 72% 20.2M 12s
350300K .......... .......... .......... .......... .......... 72% 17.2M 12s
350350K .......... .......... .......... .......... .......... 72% 19.8M 12s
350400K .......... .......... .......... .......... .......... 72% 28.8M 12s
350450K .......... .......... .......... .......... .......... 72% 18.4M 12s
350500K .......... .......... .......... .......... .......... 72% 22.4M 12s
350550K .......... .......... .......... .......... .......... 72% 21.0M 12s
350600K .......... .......... .......... .......... .......... 72% 25.1M 12s
350650K .......... .......... .......... .......... .......... 72% 22.8M 12s
350700K .......... .......... .......... .......... .......... 72% 21.0M 12s
350750K .......... .......... .......... .......... .......... 72% 18.3M 12s
350800K .......... .......... .......... .......... .......... 72% 33.3M 12s
350850K .......... .......... .......... .......... .......... 73% 22.2M 12s
350900K .......... .......... .......... .......... .......... 73% 17.6M 12s
350950K .......... .......... .......... .......... .......... 73% 12.5M 12s
351000K .......... .......... .......... .......... .......... 73% 46.7M 12s
351050K .......... .......... .......... .......... .......... 73% 27.8M 12s
351100K .......... .......... .......... .......... .......... 73% 20.3M 12s
351150K .......... .......... .......... .......... .......... 73% 32.7M 12s
351200K .......... .......... .......... .......... .......... 73% 23.2M 12s
351250K .......... .......... .......... .......... .......... 73% 24.6M 12s
351300K .......... .......... .......... .......... .......... 73% 19.9M 12s
351350K .......... .......... .......... .......... .......... 73% 18.9M 12s
351400K .......... .......... .......... .......... .......... 73% 16.7M 12s
351450K .......... .......... .......... .......... .......... 73% 21.1M 12s
351500K .......... .......... .......... .......... .......... 73% 19.0M 12s
351550K .......... .......... .......... .......... .......... 73% 31.6M 12s
351600K .......... .......... .......... .......... .......... 73% 14.5M 12s
351650K .......... .......... .......... .......... .......... 73% 28.5M 12s
351700K .......... .......... .......... .......... .......... 73% 19.1M 12s
351750K .......... .......... .......... .......... .......... 73% 26.4M 12s
351800K .......... .......... .......... .......... .......... 73% 24.1M 12s
351850K .......... .......... .......... .......... .......... 73% 21.3M 12s
351900K .......... .......... .......... .......... .......... 73% 19.2M 12s
351950K .......... .......... .......... .......... .......... 73% 15.0M 12s
352000K .......... .......... .......... .......... .......... 73% 70.5M 12s
352050K .......... .......... .......... .......... .......... 73% 22.0M 12s
352100K .......... .......... .......... .......... .......... 73% 17.1M 12s
352150K .......... .......... .......... .......... .......... 73% 30.6M 12s
352200K .......... .......... .......... .......... .......... 73% 64.3M 11s
352250K .......... .......... .......... .......... .......... 73% 36.3M 11s
352300K .......... .......... .......... .......... .......... 73% 30.3M 11s
352350K .......... .......... .......... .......... .......... 73% 19.9M 11s
352400K .......... .......... .......... .......... .......... 73% 34.7M 11s
352450K .......... .......... .......... .......... .......... 73% 20.0M 11s
352500K .......... .......... .......... .......... .......... 73% 28.7M 11s
352550K .......... .......... .......... .......... .......... 73% 28.6M 11s
352600K .......... .......... .......... .......... .......... 73% 17.6M 11s
352650K .......... .......... .......... .......... .......... 73% 17.6M 11s
352700K .......... .......... .......... .......... .......... 73% 17.9M 11s
352750K .......... .......... .......... .......... .......... 73% 32.9M 11s
352800K .......... .......... .......... .......... .......... 73% 22.6M 11s
352850K .......... .......... .......... .......... .......... 73% 23.7M 11s
352900K .......... .......... .......... .......... .......... 73% 25.2M 11s
352950K .......... .......... .......... .......... .......... 73% 21.2M 11s
353000K .......... .......... .......... .......... .......... 73% 25.3M 11s
353050K .......... .......... .......... .......... .......... 73% 31.8M 11s
353100K .......... .......... .......... .......... .......... 73% 27.4M 11s
353150K .......... .......... .......... .......... .......... 73% 15.2M 11s
353200K .......... .......... .......... .......... .......... 73% 69.8M 11s
353250K .......... .......... .......... .......... .......... 73% 58.4M 11s
353300K .......... .......... .......... .......... .......... 73% 24.1M 11s
353350K .......... .......... .......... .......... .......... 73% 29.3M 11s
353400K .......... .......... .......... .......... .......... 73% 46.1M 11s
353450K .......... .......... .......... .......... .......... 73% 38.3M 11s
353500K .......... .......... .......... .......... .......... 73% 29.6M 11s
353550K .......... .......... .......... .......... .......... 73% 34.4M 11s
353600K .......... .......... .......... .......... .......... 73% 19.8M 11s
353650K .......... .......... .......... .......... .......... 73% 26.0M 11s
353700K .......... .......... .......... .......... .......... 73% 31.0M 11s
353750K .......... .......... .......... .......... .......... 73% 21.1M 11s
353800K .......... .......... .......... .......... .......... 73% 29.2M 11s
353850K .......... .......... .......... .......... .......... 73% 18.1M 11s
353900K .......... .......... .......... .......... .......... 73% 21.1M 11s
353950K .......... .......... .......... .......... .......... 73% 19.5M 11s
354000K .......... .......... .......... .......... .......... 73% 32.7M 11s
354050K .......... .......... .......... .......... .......... 73% 20.8M 11s
354100K .......... .......... .......... .......... .......... 73% 21.3M 11s
354150K .......... .......... .......... .......... .......... 73% 28.2M 11s
354200K .......... .......... .......... .......... .......... 73% 18.7M 11s
354250K .......... .......... .......... .......... .......... 73% 28.3M 11s
354300K .......... .......... .......... .......... .......... 73% 30.7M 11s
354350K .......... .......... .......... .......... .......... 73% 23.7M 11s
354400K .......... .......... .......... .......... .......... 73% 23.5M 11s
354450K .......... .......... .......... .......... .......... 73% 60.4M 11s
354500K .......... .......... .......... .......... .......... 73% 17.3M 11s
354550K .......... .......... .......... .......... .......... 73% 68.3M 11s
354600K .......... .......... .......... .......... .......... 73% 27.1M 11s
354650K .......... .......... .......... .......... .......... 73% 78.9M 11s
354700K .......... .......... .......... .......... .......... 73% 71.2M 11s
354750K .......... .......... .......... .......... .......... 73% 57.2M 11s
354800K .......... .......... .......... .......... .......... 73% 51.7M 11s
354850K .......... .......... .......... .......... .......... 73% 23.6M 11s
354900K .......... .......... .......... .......... .......... 73% 26.8M 11s
354950K .......... .......... .......... .......... .......... 73% 22.1M 11s
355000K .......... .......... .......... .......... .......... 73% 33.1M 11s
355050K .......... .......... .......... .......... .......... 73% 24.1M 11s
355100K .......... .......... .......... .......... .......... 73% 19.8M 11s
355150K .......... .......... .......... .......... .......... 73% 25.0M 11s
355200K .......... .......... .......... .......... .......... 73% 22.4M 11s
355250K .......... .......... .......... .......... .......... 73% 22.5M 11s
355300K .......... .......... .......... .......... .......... 73% 29.1M 11s
355350K .......... .......... .......... .......... .......... 73% 18.8M 11s
355400K .......... .......... .......... .......... .......... 73% 26.9M 11s
355450K .......... .......... .......... .......... .......... 73% 25.3M 11s
355500K .......... .......... .......... .......... .......... 73% 27.6M 11s
355550K .......... .......... .......... .......... .......... 73% 24.5M 11s
355600K .......... .......... .......... .......... .......... 73% 21.0M 11s
355650K .......... .......... .......... .......... .......... 74% 28.6M 11s
355700K .......... .......... .......... .......... .......... 74% 25.4M 11s
355750K .......... .......... .......... .......... .......... 74% 25.9M 11s
355800K .......... .......... .......... .......... .......... 74% 13.6M 11s
355850K .......... .......... .......... .......... .......... 74% 52.8M 11s
355900K .......... .......... .......... .......... .......... 74% 26.7M 11s
355950K .......... .......... .......... .......... .......... 74% 22.4M 11s
356000K .......... .......... .......... .......... .......... 74% 61.6M 11s
356050K .......... .......... .......... .......... .......... 74% 20.1M 11s
356100K .......... .......... .......... .......... .......... 74% 22.4M 11s
356150K .......... .......... .......... .......... .......... 74% 20.8M 11s
356200K .......... .......... .......... .......... .......... 74% 17.3M 11s
356250K .......... .......... .......... .......... .......... 74% 18.1M 11s
356300K .......... .......... .......... .......... .......... 74% 34.6M 11s
356350K .......... .......... .......... .......... .......... 74% 18.3M 11s
356400K .......... .......... .......... .......... .......... 74% 19.4M 11s
356450K .......... .......... .......... .......... .......... 74% 16.4M 11s
356500K .......... .......... .......... .......... .......... 74% 16.4M 11s
356550K .......... .......... .......... .......... .......... 74% 20.0M 11s
356600K .......... .......... .......... .......... .......... 74% 19.9M 11s
356650K .......... .......... .......... .......... .......... 74% 18.9M 11s
356700K .......... .......... .......... .......... .......... 74% 15.6M 11s
356750K .......... .......... .......... .......... .......... 74% 27.3M 11s
356800K .......... .......... .......... .......... .......... 74% 77.4M 11s
356850K .......... .......... .......... .......... .......... 74% 29.3M 11s
356900K .......... .......... .......... .......... .......... 74% 45.1M 11s
356950K .......... .......... .......... .......... .......... 74% 17.8M 11s
357000K .......... .......... .......... .......... .......... 74% 80.8M 11s
357050K .......... .......... .......... .......... .......... 74% 26.3M 11s
357100K .......... .......... .......... .......... .......... 74% 63.9M 11s
357150K .......... .......... .......... .......... .......... 74% 36.2M 11s
357200K .......... .......... .......... .......... .......... 74% 24.7M 11s
357250K .......... .......... .......... .......... .......... 74% 18.6M 11s
357300K .......... .......... .......... .......... .......... 74% 27.0M 11s
357350K .......... .......... .......... .......... .......... 74% 20.2M 11s
357400K .......... .......... .......... .......... .......... 74% 34.6M 11s
357450K .......... .......... .......... .......... .......... 74% 18.1M 11s
357500K .......... .......... .......... .......... .......... 74% 30.9M 11s
357550K .......... .......... .......... .......... .......... 74% 19.9M 11s
357600K .......... .......... .......... .......... .......... 74% 27.1M 11s
357650K .......... .......... .......... .......... .......... 74% 27.0M 11s
357700K .......... .......... .......... .......... .......... 74% 18.7M 11s
357750K .......... .......... .......... .......... .......... 74% 30.2M 11s
357800K .......... .......... .......... .......... .......... 74% 12.6M 11s
357850K .......... .......... .......... .......... .......... 74% 60.4M 11s
357900K .......... .......... .......... .......... .......... 74% 22.2M 11s
357950K .......... .......... .......... .......... .......... 74% 24.4M 11s
358000K .......... .......... .......... .......... .......... 74% 22.5M 11s
358050K .......... .......... .......... .......... .......... 74% 17.4M 11s
358100K .......... .......... .......... .......... .......... 74% 18.4M 11s
358150K .......... .......... .......... .......... .......... 74% 18.4M 11s
358200K .......... .......... .......... .......... .......... 74% 15.5M 11s
358250K .......... .......... .......... .......... .......... 74% 19.2M 11s
358300K .......... .......... .......... .......... .......... 74% 19.8M 11s
358350K .......... .......... .......... .......... .......... 74% 18.8M 11s
358400K .......... .......... .......... .......... .......... 74% 19.3M 11s
358450K .......... .......... .......... .......... .......... 74% 21.0M 11s
358500K .......... .......... .......... .......... .......... 74% 20.0M 11s
358550K .......... .......... .......... .......... .......... 74% 22.4M 11s
358600K .......... .......... .......... .......... .......... 74% 28.2M 11s
358650K .......... .......... .......... .......... .......... 74% 20.5M 11s
358700K .......... .......... .......... .......... .......... 74%  102M 11s
358750K .......... .......... .......... .......... .......... 74% 23.5M 11s
358800K .......... .......... .......... .......... .......... 74% 64.9M 11s
358850K .......... .......... .......... .......... .......... 74% 28.6M 11s
358900K .......... .......... .......... .......... .......... 74% 35.1M 11s
358950K .......... .......... .......... .......... .......... 74% 19.7M 11s
359000K .......... .......... .......... .......... .......... 74% 15.7M 11s
359050K .......... .......... .......... .......... .......... 74% 22.0M 11s
359100K .......... .......... .......... .......... .......... 74% 15.2M 11s
359150K .......... .......... .......... .......... .......... 74% 19.6M 11s
359200K .......... .......... .......... .......... .......... 74% 14.0M 11s
359250K .......... .......... .......... .......... .......... 74% 19.0M 11s
359300K .......... .......... .......... .......... .......... 74% 14.4M 11s
359350K .......... .......... .......... .......... .......... 74% 19.2M 11s
359400K .......... .......... .......... .......... .......... 74% 13.5M 11s
359450K .......... .......... .......... .......... .......... 74% 14.2M 11s
359500K .......... .......... .......... .......... .......... 74% 24.5M 11s
359550K .......... .......... .......... .......... .......... 74% 12.1M 11s
359600K .......... .......... .......... .......... .......... 74% 25.9M 11s
359650K .......... .......... .......... .......... .......... 74% 17.6M 11s
359700K .......... .......... .......... .......... .......... 74% 20.1M 11s
359750K .......... .......... .......... .......... .......... 74% 27.1M 11s
359800K .......... .......... .......... .......... .......... 74% 26.9M 11s
359850K .......... .......... .......... .......... .......... 74% 18.1M 11s
359900K .......... .......... .......... .......... .......... 74% 21.9M 11s
359950K .......... .......... .......... .......... .......... 74% 19.2M 11s
360000K .......... .......... .......... .......... .......... 74% 20.5M 11s
360050K .......... .......... .......... .......... .......... 74% 18.0M 11s
360100K .......... .......... .......... .......... .......... 74% 13.9M 11s
360150K .......... .......... .......... .......... .......... 74% 20.0M 11s
360200K .......... .......... .......... .......... .......... 74% 16.3M 11s
360250K .......... .......... .......... .......... .......... 74% 16.6M 11s
360300K .......... .......... .......... .......... .......... 74% 15.5M 11s
360350K .......... .......... .......... .......... .......... 74% 8.55M 11s
360400K .......... .......... .......... .......... .......... 74% 69.4M 11s
360450K .......... .......... .......... .......... .......... 75% 18.3M 11s
360500K .......... .......... .......... .......... .......... 75% 17.9M 11s
360550K .......... .......... .......... .......... .......... 75% 18.6M 11s
360600K .......... .......... .......... .......... .......... 75% 14.2M 11s
360650K .......... .......... .......... .......... .......... 75% 19.8M 11s
360700K .......... .......... .......... .......... .......... 75% 18.0M 11s
360750K .......... .......... .......... .......... .......... 75% 14.2M 11s
360800K .......... .......... .......... .......... .......... 75% 13.2M 11s
360850K .......... .......... .......... .......... .......... 75% 9.47M 11s
360900K .......... .......... .......... .......... .......... 75% 13.6M 11s
360950K .......... .......... .......... .......... .......... 75% 11.1M 11s
361000K .......... .......... .......... .......... .......... 75% 14.7M 11s
361050K .......... .......... .......... .......... .......... 75% 14.1M 11s
361100K .......... .......... .......... .......... .......... 75% 15.1M 11s
361150K .......... .......... .......... .......... .......... 75% 9.75M 11s
361200K .......... .......... .......... .......... .......... 75% 72.4M 11s
361250K .......... .......... .......... .......... .......... 75% 15.8M 11s
361300K .......... .......... .......... .......... .......... 75% 19.1M 11s
361350K .......... .......... .......... .......... .......... 75% 21.1M 11s
361400K .......... .......... .......... .......... .......... 75% 25.1M 11s
361450K .......... .......... .......... .......... .......... 75% 14.6M 11s
361500K .......... .......... .......... .......... .......... 75% 18.9M 11s
361550K .......... .......... .......... .......... .......... 75% 19.6M 11s
361600K .......... .......... .......... .......... .......... 75% 15.8M 11s
361650K .......... .......... .......... .......... .......... 75% 17.8M 11s
361700K .......... .......... .......... .......... .......... 75% 18.2M 11s
361750K .......... .......... .......... .......... .......... 75% 12.6M 11s
361800K .......... .......... .......... .......... .......... 75% 16.7M 10s
361850K .......... .......... .......... .......... .......... 75% 13.4M 10s
361900K .......... .......... .......... .......... .......... 75% 17.9M 10s
361950K .......... .......... .......... .......... .......... 75% 16.1M 10s
362000K .......... .......... .......... .......... .......... 75% 19.7M 10s
362050K .......... .......... .......... .......... .......... 75% 19.9M 10s
362100K .......... .......... .......... .......... .......... 75% 10.6M 10s
362150K .......... .......... .......... .......... .......... 75% 75.2M 10s
362200K .......... .......... .......... .......... .......... 75% 33.7M 10s
362250K .......... .......... .......... .......... .......... 75% 22.2M 10s
362300K .......... .......... .......... .......... .......... 75% 21.0M 10s
362350K .......... .......... .......... .......... .......... 75% 18.8M 10s
362400K .......... .......... .......... .......... .......... 75% 20.3M 10s
362450K .......... .......... .......... .......... .......... 75% 16.5M 10s
362500K .......... .......... .......... .......... .......... 75% 22.0M 10s
362550K .......... .......... .......... .......... .......... 75% 22.0M 10s
362600K .......... .......... .......... .......... .......... 75% 16.5M 10s
362650K .......... .......... .......... .......... .......... 75% 18.3M 10s
362700K .......... .......... .......... .......... .......... 75% 14.2M 10s
362750K .......... .......... .......... .......... .......... 75% 18.1M 10s
362800K .......... .......... .......... .......... .......... 75% 18.8M 10s
362850K .......... .......... .......... .......... .......... 75% 19.9M 10s
362900K .......... .......... .......... .......... .......... 75% 28.8M 10s
362950K .......... .......... .......... .......... .......... 75% 18.8M 10s
363000K .......... .......... .......... .......... .......... 75% 15.1M 10s
363050K .......... .......... .......... .......... .......... 75% 64.0M 10s
363100K .......... .......... .......... .......... .......... 75% 68.1M 10s
363150K .......... .......... .......... .......... .......... 75% 18.2M 10s
363200K .......... .......... .......... .......... .......... 75% 45.6M 10s
363250K .......... .......... .......... .......... .......... 75% 23.4M 10s
363300K .......... .......... .......... .......... .......... 75% 53.8M 10s
363350K .......... .......... .......... .......... .......... 75% 25.3M 10s
363400K .......... .......... .......... .......... .......... 75% 29.2M 10s
363450K .......... .......... .......... .......... .......... 75% 23.4M 10s
363500K .......... .......... .......... .......... .......... 75% 32.6M 10s
363550K .......... .......... .......... .......... .......... 75% 29.0M 10s
363600K .......... .......... .......... .......... .......... 75% 23.7M 10s
363650K .......... .......... .......... .......... .......... 75% 32.1M 10s
363700K .......... .......... .......... .......... .......... 75% 23.7M 10s
363750K .......... .......... .......... .......... .......... 75% 37.2M 10s
363800K .......... .......... .......... .......... .......... 75% 20.9M 10s
363850K .......... .......... .......... .......... .......... 75% 19.5M 10s
363900K .......... .......... .......... .......... .......... 75% 33.8M 10s
363950K .......... .......... .......... .......... .......... 75% 23.9M 10s
364000K .......... .......... .......... .......... .......... 75% 24.1M 10s
364050K .......... .......... .......... .......... .......... 75% 37.7M 10s
364100K .......... .......... .......... .......... .......... 75% 21.4M 10s
364150K .......... .......... .......... .......... .......... 75% 18.9M 10s
364200K .......... .......... .......... .......... .......... 75% 13.4M 10s
364250K .......... .......... .......... .......... .......... 75% 21.5M 10s
364300K .......... .......... .......... .......... .......... 75% 13.0M 10s
364350K .......... .......... .......... .......... .......... 75% 67.3M 10s
364400K .......... .......... .......... .......... .......... 75% 48.1M 10s
364450K .......... .......... .......... .......... .......... 75% 40.4M 10s
364500K .......... .......... .......... .......... .......... 75% 24.6M 10s
364550K .......... .......... .......... .......... .......... 75% 30.4M 10s
364600K .......... .......... .......... .......... .......... 75% 17.7M 10s
364650K .......... .......... .......... .......... .......... 75% 16.4M 10s
364700K .......... .......... .......... .......... .......... 75% 16.7M 10s
364750K .......... .......... .......... .......... .......... 75% 17.1M 10s
364800K .......... .......... .......... .......... .......... 75% 21.3M 10s
364850K .......... .......... .......... .......... .......... 75% 19.8M 10s
364900K .......... .......... .......... .......... .......... 75% 20.2M 10s
364950K .......... .......... .......... .......... .......... 75% 11.8M 10s
365000K .......... .......... .......... .......... .......... 75% 18.0M 10s
365050K .......... .......... .......... .......... .......... 75% 15.9M 10s
365100K .......... .......... .......... .......... .......... 75% 15.8M 10s
365150K .......... .......... .......... .......... .......... 75% 23.4M 10s
365200K .......... .......... .......... .......... .......... 75% 22.8M 10s
365250K .......... .......... .......... .......... .......... 76% 17.0M 10s
365300K .......... .......... .......... .......... .......... 76% 74.4M 10s
365350K .......... .......... .......... .......... .......... 76% 26.8M 10s
365400K .......... .......... .......... .......... .......... 76% 18.7M 10s
365450K .......... .......... .......... .......... .......... 76% 26.3M 10s
365500K .......... .......... .......... .......... .......... 76% 30.6M 10s
365550K .......... .......... .......... .......... .......... 76% 28.9M 10s
365600K .......... .......... .......... .......... .......... 76% 18.8M 10s
365650K .......... .......... .......... .......... .......... 76% 23.6M 10s
365700K .......... .......... .......... .......... .......... 76% 18.1M 10s
365750K .......... .......... .......... .......... .......... 76% 20.8M 10s
365800K .......... .......... .......... .......... .......... 76% 20.1M 10s
365850K .......... .......... .......... .......... .......... 76% 20.2M 10s
365900K .......... .......... .......... .......... .......... 76% 18.1M 10s
365950K .......... .......... .......... .......... .......... 76% 12.5M 10s
366000K .......... .......... .......... .......... .......... 76% 25.6M 10s
366050K .......... .......... .......... .......... .......... 76% 27.3M 10s
366100K .......... .......... .......... .......... .......... 76% 19.1M 10s
366150K .......... .......... .......... .......... .......... 76% 23.1M 10s
366200K .......... .......... .......... .......... .......... 76% 15.2M 10s
366250K .......... .......... .......... .......... .......... 76% 19.2M 10s
366300K .......... .......... .......... .......... .......... 76% 21.7M 10s
366350K .......... .......... .......... .......... .......... 76% 26.9M 10s
366400K .......... .......... .......... .......... .......... 76% 20.0M 10s
366450K .......... .......... .......... .......... .......... 76% 18.6M 10s
366500K .......... .......... .......... .......... .......... 76% 34.6M 10s
366550K .......... .......... .......... .......... .......... 76% 19.5M 10s
366600K .......... .......... .......... .......... .......... 76% 16.3M 10s
366650K .......... .......... .......... .......... .......... 76% 13.0M 10s
366700K .......... .......... .......... .......... .......... 76% 12.2M 10s
366750K .......... .......... .......... .......... .......... 76% 13.1M 10s
366800K .......... .......... .......... .......... .......... 76% 12.6M 10s
366850K .......... .......... .......... .......... .......... 76% 13.9M 10s
366900K .......... .......... .......... .......... .......... 76% 14.1M 10s
366950K .......... .......... .......... .......... .......... 76% 14.2M 10s
367000K .......... .......... .......... .......... .......... 76% 18.2M 10s
367050K .......... .......... .......... .......... .......... 76% 21.4M 10s
367100K .......... .......... .......... .......... .......... 76% 17.0M 10s
367150K .......... .......... .......... .......... .......... 76% 26.8M 10s
367200K .......... .......... .......... .......... .......... 76% 23.2M 10s
367250K .......... .......... .......... .......... .......... 76% 73.9M 10s
367300K .......... .......... .......... .......... .......... 76% 27.0M 10s
367350K .......... .......... .......... .......... .......... 76% 35.6M 10s
367400K .......... .......... .......... .......... .......... 76% 26.9M 10s
367450K .......... .......... .......... .......... .......... 76% 23.7M 10s
367500K .......... .......... .......... .......... .......... 76% 29.1M 10s
367550K .......... .......... .......... .......... .......... 76% 20.8M 10s
367600K .......... .......... .......... .......... .......... 76% 15.6M 10s
367650K .......... .......... .......... .......... .......... 76% 32.9M 10s
367700K .......... .......... .......... .......... .......... 76% 20.0M 10s
367750K .......... .......... .......... .......... .......... 76% 18.9M 10s
367800K .......... .......... .......... .......... .......... 76% 17.1M 10s
367850K .......... .......... .......... .......... .......... 76% 17.2M 10s
367900K .......... .......... .......... .......... .......... 76% 18.7M 10s
367950K .......... .......... .......... .......... .......... 76% 18.3M 10s
368000K .......... .......... .......... .......... .......... 76% 23.2M 10s
368050K .......... .......... .......... .......... .......... 76% 32.6M 10s
368100K .......... .......... .......... .......... .......... 76% 19.4M 10s
368150K .......... .......... .......... .......... .......... 76% 16.6M 10s
368200K .......... .......... .......... .......... .......... 76% 12.9M 10s
368250K .......... .......... .......... .......... .......... 76% 20.2M 10s
368300K .......... .......... .......... .......... .......... 76% 32.0M 10s
368350K .......... .......... .......... .......... .......... 76% 26.3M 10s
368400K .......... .......... .......... .......... .......... 76% 18.7M 10s
368450K .......... .......... .......... .......... .......... 76% 41.6M 10s
368500K .......... .......... .......... .......... .......... 76% 17.1M 10s
368550K .......... .......... .......... .......... .......... 76% 20.8M 10s
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368650K .......... .......... .......... .......... .......... 76% 14.5M 10s
368700K .......... .......... .......... .......... .......... 76% 17.8M 10s
368750K .......... .......... .......... .......... .......... 76% 13.3M 10s
368800K .......... .......... .......... .......... .......... 76% 20.2M 10s
368850K .......... .......... .......... .......... .......... 76% 14.5M 10s
368900K .......... .......... .......... .......... .......... 76% 20.1M 10s
368950K .......... .......... .......... .......... .......... 76% 15.3M 10s
369000K .......... .......... .......... .......... .......... 76% 14.1M 10s
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369100K .......... .......... .......... .......... .......... 76% 9.64M 10s
369150K .......... .......... .......... .......... .......... 76% 15.7M 10s
369200K .......... .......... .......... .......... .......... 76% 29.6M 10s
369250K .......... .......... .......... .......... .......... 76% 81.9M 10s
369300K .......... .......... .......... .......... .......... 76% 29.1M 10s
369350K .......... .......... .......... .......... .......... 76% 20.2M 10s
369400K .......... .......... .......... .......... .......... 76% 22.1M 10s
369450K .......... .......... .......... .......... .......... 76% 17.4M 10s
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369550K .......... .......... .......... .......... .......... 76% 22.8M 10s
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369850K .......... .......... .......... .......... .......... 76% 13.7M 10s
369900K .......... .......... .......... .......... .......... 76% 20.8M 10s
369950K .......... .......... .......... .......... .......... 76% 15.2M 10s
370000K .......... .......... .......... .......... .......... 76% 11.0M 10s
370050K .......... .......... .......... .......... .......... 77% 70.5M 10s
370100K .......... .......... .......... .......... .......... 77% 18.2M 10s
370150K .......... .......... .......... .......... .......... 77% 27.5M 10s
370200K .......... .......... .......... .......... .......... 77% 18.2M 10s
370250K .......... .......... .......... .......... .......... 77% 24.3M 10s
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370600K .......... .......... .......... .......... .......... 77% 17.7M 10s
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371000K .......... .......... .......... .......... .......... 77% 9.48M 10s
371050K .......... .......... .......... .......... .......... 77% 74.5M 10s
371100K .......... .......... .......... .......... .......... 77% 21.8M 10s
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371200K .......... .......... .......... .......... .......... 77% 17.9M 10s
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371500K .......... .......... .......... .......... .......... 77% 13.6M 10s
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371600K .......... .......... .......... .......... .......... 77% 11.7M 10s
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371750K .......... .......... .......... .......... .......... 77% 38.1M 10s
371800K .......... .......... .......... .......... .......... 77% 74.9M 9s
371850K .......... .......... .......... .......... .......... 77% 13.8M 9s
371900K .......... .......... .......... .......... .......... 77% 76.5M 9s
371950K .......... .......... .......... .......... .......... 77% 22.1M 9s
372000K .......... .......... .......... .......... .......... 77% 23.1M 9s
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372100K .......... .......... .......... .......... .......... 77% 21.7M 9s
372150K .......... .......... .......... .......... .......... 77% 19.9M 9s
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372250K .......... .......... .......... .......... .......... 77% 20.0M 9s
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372500K .......... .......... .......... .......... .......... 77% 21.2M 9s
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372700K .......... .......... .......... .......... .......... 77% 16.6M 9s
372750K .......... .......... .......... .......... .......... 77% 13.3M 9s
372800K .......... .......... .......... .......... .......... 77% 30.5M 9s
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373000K .......... .......... .......... .......... .......... 77% 22.6M 9s
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373100K .......... .......... .......... .......... .......... 77% 12.4M 9s
373150K .......... .......... .......... .......... .......... 77% 14.0M 9s
373200K .......... .......... .......... .......... .......... 77% 11.8M 9s
373250K .......... .......... .......... .......... .......... 77% 19.0M 9s
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373400K .......... .......... .......... .......... .......... 77% 16.0M 9s
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373650K .......... .......... .......... .......... .......... 77% 21.0M 9s
373700K .......... .......... .......... .......... .......... 77% 26.7M 9s
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373800K .......... .......... .......... .......... .......... 77% 52.2M 9s
373850K .......... .......... .......... .......... .......... 77% 15.8M 9s
373900K .......... .......... .......... .......... .......... 77% 23.9M 9s
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374000K .......... .......... .......... .......... .......... 77% 19.1M 9s
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374100K .......... .......... .......... .......... .......... 77% 13.8M 9s
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374200K .......... .......... .......... .......... .......... 77% 13.6M 9s
374250K .......... .......... .......... .......... .......... 77% 19.1M 9s
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374400K .......... .......... .......... .......... .......... 77% 19.6M 9s
374450K .......... .......... .......... .......... .......... 77% 27.7M 9s
374500K .......... .......... .......... .......... .......... 77% 24.5M 9s
374550K .......... .......... .......... .......... .......... 77% 18.8M 9s
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374650K .......... .......... .......... .......... .......... 77% 46.7M 9s
374700K .......... .......... .......... .......... .......... 77% 14.6M 9s
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374800K .......... .......... .......... .......... .......... 77% 14.6M 9s
374850K .......... .......... .......... .......... .......... 78% 11.7M 9s
374900K .......... .......... .......... .......... .......... 78% 12.8M 9s
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375000K .......... .......... .......... .......... .......... 78% 17.9M 9s
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375100K .......... .......... .......... .......... .......... 78% 14.5M 9s
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375200K .......... .......... .......... .......... .......... 78% 10.6M 9s
375250K .......... .......... .......... .......... .......... 78% 80.0M 9s
375300K .......... .......... .......... .......... .......... 78% 40.5M 9s
375350K .......... .......... .......... .......... .......... 78% 16.5M 9s
375400K .......... .......... .......... .......... .......... 78% 21.9M 9s
375450K .......... .......... .......... .......... .......... 78% 24.1M 9s
375500K .......... .......... .......... .......... .......... 78% 27.8M 9s
375550K .......... .......... .......... .......... .......... 78% 20.9M 9s
375600K .......... .......... .......... .......... .......... 78% 19.8M 9s
375650K .......... .......... .......... .......... .......... 78% 19.1M 9s
375700K .......... .......... .......... .......... .......... 78% 14.1M 9s
375750K .......... .......... .......... .......... .......... 78% 17.0M 9s
375800K .......... .......... .......... .......... .......... 78% 17.8M 9s
375850K .......... .......... .......... .......... .......... 78% 22.3M 9s
375900K .......... .......... .......... .......... .......... 78% 22.6M 9s
375950K .......... .......... .......... .......... .......... 78% 18.0M 9s
376000K .......... .......... .......... .......... .......... 78% 23.9M 9s
376050K .......... .......... .......... .......... .......... 78% 21.5M 9s
376100K .......... .......... .......... .......... .......... 78% 14.2M 9s
376150K .......... .......... .......... .......... .......... 78% 39.3M 9s
376200K .......... .......... .......... .......... .......... 78% 24.6M 9s
376250K .......... .......... .......... .......... .......... 78% 78.4M 9s
376300K .......... .......... .......... .......... .......... 78% 15.5M 9s
376350K .......... .......... .......... .......... .......... 78% 70.5M 9s
376400K .......... .......... .......... .......... .......... 78% 41.1M 9s
376450K .......... .......... .......... .......... .......... 78% 29.4M 9s
376500K .......... .......... .......... .......... .......... 78% 41.1M 9s
376550K .......... .......... .......... .......... .......... 78% 27.4M 9s
376600K .......... .......... .......... .......... .......... 78% 29.3M 9s
376650K .......... .......... .......... .......... .......... 78% 18.9M 9s
376700K .......... .......... .......... .......... .......... 78% 30.1M 9s
376750K .......... .......... .......... .......... .......... 78% 28.8M 9s
376800K .......... .......... .......... .......... .......... 78% 29.5M 9s
376850K .......... .......... .......... .......... .......... 78% 22.2M 9s
376900K .......... .......... .......... .......... .......... 78% 24.2M 9s
376950K .......... .......... .......... .......... .......... 78% 20.5M 9s
377000K .......... .......... .......... .......... .......... 78% 29.2M 9s
377050K .......... .......... .......... .......... .......... 78% 29.0M 9s
377100K .......... .......... .......... .......... .......... 78% 30.0M 9s
377150K .......... .......... .......... .......... .......... 78% 23.5M 9s
377200K .......... .......... .......... .......... .......... 78% 20.5M 9s
377250K .......... .......... .......... .......... .......... 78% 33.1M 9s
377300K .......... .......... .......... .......... .......... 78% 19.4M 9s
377350K .......... .......... .......... .......... .......... 78% 23.1M 9s
377400K .......... .......... .......... .......... .......... 78% 15.8M 9s
377450K .......... .......... .......... .......... .......... 78% 22.5M 9s
377500K .......... .......... .......... .......... .......... 78% 13.2M 9s
377550K .......... .......... .......... .......... .......... 78% 88.1M 9s
377600K .......... .......... .......... .......... .......... 78% 22.0M 9s
377650K .......... .......... .......... .......... .......... 78% 93.5M 9s
377700K .......... .......... .......... .......... .......... 78% 40.1M 9s
377750K .......... .......... .......... .......... .......... 78% 26.9M 9s
377800K .......... .......... .......... .......... .......... 78% 41.9M 9s
377850K .......... .......... .......... .......... .......... 78% 19.8M 9s
377900K .......... .......... .......... .......... .......... 78% 36.8M 9s
377950K .......... .......... .......... .......... .......... 78% 24.7M 9s
378000K .......... .......... .......... .......... .......... 78% 30.8M 9s
378050K .......... .......... .......... .......... .......... 78% 37.2M 9s
378100K .......... .......... .......... .......... .......... 78% 21.4M 9s
378150K .......... .......... .......... .......... .......... 78% 30.3M 9s
378200K .......... .......... .......... .......... .......... 78% 30.8M 9s
378250K .......... .......... .......... .......... .......... 78% 19.0M 9s
378300K .......... .......... .......... .......... .......... 78% 25.9M 9s
378350K .......... .......... .......... .......... .......... 78% 32.8M 9s
378400K .......... .......... .......... .......... .......... 78% 19.7M 9s
378450K .......... .......... .......... .......... .......... 78% 30.9M 9s
378500K .......... .......... .......... .......... .......... 78% 17.0M 9s
378550K .......... .......... .......... .......... .......... 78% 28.9M 9s
378600K .......... .......... .......... .......... .......... 78% 16.5M 9s
378650K .......... .......... .......... .......... .......... 78% 84.3M 9s
378700K .......... .......... .......... .......... .......... 78% 27.0M 9s
378750K .......... .......... .......... .......... .......... 78% 27.9M 9s
378800K .......... .......... .......... .......... .......... 78% 21.9M 9s
378850K .......... .......... .......... .......... .......... 78% 67.3M 9s
378900K .......... .......... .......... .......... .......... 78% 67.1M 9s
378950K .......... .......... .......... .......... .......... 78% 28.8M 9s
379000K .......... .......... .......... .......... .......... 78% 31.1M 9s
379050K .......... .......... .......... .......... .......... 78% 77.0M 9s
379100K .......... .......... .......... .......... .......... 78% 26.2M 9s
379150K .......... .......... .......... .......... .......... 78% 41.1M 9s
379200K .......... .......... .......... .......... .......... 78% 19.8M 9s
379250K .......... .......... .......... .......... .......... 78% 27.2M 9s
379300K .......... .......... .......... .......... .......... 78% 35.1M 9s
379350K .......... .......... .......... .......... .......... 78% 23.4M 9s
379400K .......... .......... .......... .......... .......... 78% 32.0M 9s
379450K .......... .......... .......... .......... .......... 78% 24.9M 9s
379500K .......... .......... .......... .......... .......... 78% 31.1M 9s
379550K .......... .......... .......... .......... .......... 78% 34.7M 9s
379600K .......... .......... .......... .......... .......... 78% 24.3M 9s
379650K .......... .......... .......... .......... .......... 79% 41.8M 9s
379700K .......... .......... .......... .......... .......... 79% 21.4M 9s
379750K .......... .......... .......... .......... .......... 79% 28.8M 9s
379800K .......... .......... .......... .......... .......... 79% 35.6M 9s
379850K .......... .......... .......... .......... .......... 79% 18.9M 9s
379900K .......... .......... .......... .......... .......... 79% 32.2M 9s
379950K .......... .......... .......... .......... .......... 79% 27.6M 9s
380000K .......... .......... .......... .......... .......... 79% 21.1M 9s
380050K .......... .......... .......... .......... .......... 79% 35.4M 9s
380100K .......... .......... .......... .......... .......... 79% 31.4M 9s
380150K .......... .......... .......... .......... .......... 79% 26.5M 9s
380200K .......... .......... .......... .......... .......... 79% 85.5M 9s
380250K .......... .......... .......... .......... .......... 79% 20.7M 9s
380300K .......... .......... .......... .......... .......... 79% 39.8M 9s
380350K .......... .......... .......... .......... .......... 79% 98.8M 9s
380400K .......... .......... .......... .......... .......... 79% 33.5M 9s
380450K .......... .......... .......... .......... .......... 79% 55.0M 9s
380500K .......... .......... .......... .......... .......... 79% 39.6M 9s
380550K .......... .......... .......... .......... .......... 79% 57.2M 9s
380600K .......... .......... .......... .......... .......... 79% 36.7M 9s
380650K .......... .......... .......... .......... .......... 79% 30.5M 9s
380700K .......... .......... .......... .......... .......... 79% 18.7M 9s
380750K .......... .......... .......... .......... .......... 79% 27.0M 9s
380800K .......... .......... .......... .......... .......... 79% 25.4M 9s
380850K .......... .......... .......... .......... .......... 79% 25.2M 9s
380900K .......... .......... .......... .......... .......... 79% 23.2M 9s
380950K .......... .......... .......... .......... .......... 79% 24.8M 9s
381000K .......... .......... .......... .......... .......... 79% 24.3M 9s
381050K .......... .......... .......... .......... .......... 79% 26.4M 9s
381100K .......... .......... .......... .......... .......... 79% 22.1M 9s
381150K .......... .......... .......... .......... .......... 79% 38.1M 9s
381200K .......... .......... .......... .......... .......... 79% 23.4M 9s
381250K .......... .......... .......... .......... .......... 79% 20.8M 9s
381300K .......... .......... .......... .......... .......... 79% 21.5M 9s
381350K .......... .......... .......... .......... .......... 79% 21.8M 9s
381400K .......... .......... .......... .......... .......... 79% 24.9M 9s
381450K .......... .......... .......... .......... .......... 79% 28.9M 9s
381500K .......... .......... .......... .......... .......... 79% 29.9M 9s
381550K .......... .......... .......... .......... .......... 79% 13.0M 9s
381600K .......... .......... .......... .......... .......... 79% 95.9M 9s
381650K .......... .......... .......... .......... .......... 79% 22.5M 9s
381700K .......... .......... .......... .......... .......... 79% 44.7M 9s
381750K .......... .......... .......... .......... .......... 79% 27.1M 9s
381800K .......... .......... .......... .......... .......... 79% 23.8M 9s
381850K .......... .......... .......... .......... .......... 79% 24.9M 9s
381900K .......... .......... .......... .......... .......... 79% 17.0M 8s
381950K .......... .......... .......... .......... .......... 79% 34.9M 8s
382000K .......... .......... .......... .......... .......... 79% 25.2M 8s
382050K .......... .......... .......... .......... .......... 79% 15.8M 8s
382100K .......... .......... .......... .......... .......... 79% 59.2M 8s
382150K .......... .......... .......... .......... .......... 79% 57.0M 8s
382200K .......... .......... .......... .......... .......... 79% 27.9M 8s
382250K .......... .......... .......... .......... .......... 79% 27.3M 8s
382300K .......... .......... .......... .......... .......... 79% 23.2M 8s
382350K .......... .......... .......... .......... .......... 79% 26.9M 8s
382400K .......... .......... .......... .......... .......... 79% 32.6M 8s
382450K .......... .......... .......... .......... .......... 79% 18.7M 8s
382500K .......... .......... .......... .......... .......... 79% 30.1M 8s
382550K .......... .......... .......... .......... .......... 79% 17.6M 8s
382600K .......... .......... .......... .......... .......... 79% 28.0M 8s
382650K .......... .......... .......... .......... .......... 79% 17.4M 8s
382700K .......... .......... .......... .......... .......... 79% 29.3M 8s
382750K .......... .......... .......... .......... .......... 79% 25.5M 8s
382800K .......... .......... .......... .......... .......... 79% 35.0M 8s
382850K .......... .......... .......... .......... .......... 79% 21.9M 8s
382900K .......... .......... .......... .......... .......... 79% 22.3M 8s
382950K .......... .......... .......... .......... .......... 79% 23.3M 8s
383000K .......... .......... .......... .......... .......... 79% 14.7M 8s
383050K .......... .......... .......... .......... .......... 79% 18.8M 8s
383100K .......... .......... .......... .......... .......... 79% 65.4M 8s
383150K .......... .......... .......... .......... .......... 79% 13.4M 8s
383200K .......... .......... .......... .......... .......... 79% 33.8M 8s
383250K .......... .......... .......... .......... .......... 79% 83.5M 8s
383300K .......... .......... .......... .......... .......... 79% 44.6M 8s
383350K .......... .......... .......... .......... .......... 79% 16.6M 8s
383400K .......... .......... .......... .......... .......... 79% 26.4M 8s
383450K .......... .......... .......... .......... .......... 79% 21.6M 8s
383500K .......... .......... .......... .......... .......... 79% 18.3M 8s
383550K .......... .......... .......... .......... .......... 79% 18.3M 8s
383600K .......... .......... .......... .......... .......... 79% 15.0M 8s
383650K .......... .......... .......... .......... .......... 79% 19.3M 8s
383700K .......... .......... .......... .......... .......... 79% 13.9M 8s
383750K .......... .......... .......... .......... .......... 79% 14.5M 8s
383800K .......... .......... .......... .......... .......... 79% 14.6M 8s
383850K .......... .......... .......... .......... .......... 79% 13.0M 8s
383900K .......... .......... .......... .......... .......... 79% 21.4M 8s
383950K .......... .......... .......... .......... .......... 79% 11.8M 8s
384000K .......... .......... .......... .......... .......... 79% 23.8M 8s
384050K .......... .......... .......... .......... .......... 79% 82.3M 8s
384100K .......... .......... .......... .......... .......... 79% 27.9M 8s
384150K .......... .......... .......... .......... .......... 79% 20.0M 8s
384200K .......... .......... .......... .......... .......... 79% 14.5M 8s
384250K .......... .......... .......... .......... .......... 79% 30.8M 8s
384300K .......... .......... .......... .......... .......... 79% 19.0M 8s
384350K .......... .......... .......... .......... .......... 79% 27.0M 8s
384400K .......... .......... .......... .......... .......... 79% 17.1M 8s
384450K .......... .......... .......... .......... .......... 80% 16.7M 8s
384500K .......... .......... .......... .......... .......... 80% 22.3M 8s
384550K .......... .......... .......... .......... .......... 80% 19.2M 8s
384600K .......... .......... .......... .......... .......... 80% 17.2M 8s
384650K .......... .......... .......... .......... .......... 80% 20.0M 8s
384700K .......... .......... .......... .......... .......... 80% 16.8M 8s
384750K .......... .......... .......... .......... .......... 80% 18.1M 8s
384800K .......... .......... .......... .......... .......... 80% 12.7M 8s
384850K .......... .......... .......... .......... .......... 80% 18.9M 8s
384900K .......... .......... .......... .......... .......... 80% 18.9M 8s
384950K .......... .......... .......... .......... .......... 80% 22.5M 8s
385000K .......... .......... .......... .......... .......... 80% 11.8M 8s
385050K .......... .......... .......... .......... .......... 80% 27.5M 8s
385100K .......... .......... .......... .......... .......... 80% 18.4M 8s
385150K .......... .......... .......... .......... .......... 80% 16.7M 8s
385200K .......... .......... .......... .......... .......... 80% 14.1M 8s
385250K .......... .......... .......... .......... .......... 80% 18.0M 8s
385300K .......... .......... .......... .......... .......... 80% 14.5M 8s
385350K .......... .......... .......... .......... .......... 80% 12.6M 8s
385400K .......... .......... .......... .......... .......... 80% 13.0M 8s
385450K .......... .......... .......... .......... .......... 80% 13.3M 8s
385500K .......... .......... .......... .......... .......... 80% 13.4M 8s
385550K .......... .......... .......... .......... .......... 80% 12.8M 8s
385600K .......... .......... .......... .......... .......... 80% 13.6M 8s
385650K .......... .......... .......... .......... .......... 80% 16.0M 8s
385700K .......... .......... .......... .......... .......... 80% 12.3M 8s
385750K .......... .......... .......... .......... .......... 80% 14.0M 8s
385800K .......... .......... .......... .......... .......... 80% 24.2M 8s
385850K .......... .......... .......... .......... .......... 80% 10.1M 8s
385900K .......... .......... .......... .......... .......... 80% 11.5M 8s
385950K .......... .......... .......... .......... .......... 80% 7.88M 8s
386000K .......... .......... .......... .......... .......... 80% 10.5M 8s
386050K .......... .......... .......... .......... .......... 80% 9.32M 8s
386100K .......... .......... .......... .......... .......... 80% 7.56M 8s
386150K .......... .......... .......... .......... .......... 80% 9.25M 8s
386200K .......... .......... .......... .......... .......... 80% 9.08M 8s
386250K .......... .......... .......... .......... .......... 80% 11.2M 8s
386300K .......... .......... .......... .......... .......... 80% 83.0M 8s
386350K .......... .......... .......... .......... .......... 80% 16.9M 8s
386400K .......... .......... .......... .......... .......... 80% 17.2M 8s
386450K .......... .......... .......... .......... .......... 80% 14.2M 8s
386500K .......... .......... .......... .......... .......... 80% 14.7M 8s
386550K .......... .......... .......... .......... .......... 80% 13.0M 8s
386600K .......... .......... .......... .......... .......... 80% 10.1M 8s
386650K .......... .......... .......... .......... .......... 80% 12.1M 8s
386700K .......... .......... .......... .......... .......... 80% 9.93M 8s
386750K .......... .......... .......... .......... .......... 80% 12.2M 8s
386800K .......... .......... .......... .......... .......... 80% 10.9M 8s
386850K .......... .......... .......... .......... .......... 80% 9.78M 8s
386900K .......... .......... .......... .......... .......... 80% 18.0M 8s
386950K .......... .......... .......... .......... .......... 80% 14.7M 8s
387000K .......... .......... .......... .......... .......... 80% 16.5M 8s
387050K .......... .......... .......... .......... .......... 80% 21.0M 8s
387100K .......... .......... .......... .......... .......... 80% 10.6M 8s
387150K .......... .......... .......... .......... .......... 80% 18.3M 8s
387200K .......... .......... .......... .......... .......... 80% 11.1M 8s
387250K .......... .......... .......... .......... .......... 80% 15.8M 8s
387300K .......... .......... .......... .......... .......... 80% 14.2M 8s
387350K .......... .......... .......... .......... .......... 80% 13.5M 8s
387400K .......... .......... .......... .......... .......... 80% 12.8M 8s
387450K .......... .......... .......... .......... .......... 80% 10.5M 8s
387500K .......... .......... .......... .......... .......... 80% 10.8M 8s
387550K .......... .......... .......... .......... .......... 80% 14.8M 8s
387600K .......... .......... .......... .......... .......... 80% 23.9M 8s
387650K .......... .......... .......... .......... .......... 80% 17.9M 8s
387700K .......... .......... .......... .......... .......... 80% 16.3M 8s
387750K .......... .......... .......... .......... .......... 80% 18.0M 8s
387800K .......... .......... .......... .......... .......... 80% 15.7M 8s
387850K .......... .......... .......... .......... .......... 80% 13.6M 8s
387900K .......... .......... .......... .......... .......... 80% 14.0M 8s
387950K .......... .......... .......... .......... .......... 80% 11.2M 8s
388000K .......... .......... .......... .......... .......... 80% 13.1M 8s
388050K .......... .......... .......... .......... .......... 80% 15.2M 8s
388100K .......... .......... .......... .......... .......... 80% 12.3M 8s
388150K .......... .......... .......... .......... .......... 80% 16.6M 8s
388200K .......... .......... .......... .......... .......... 80% 18.9M 8s
388250K .......... .......... .......... .......... .......... 80% 23.6M 8s
388300K .......... .......... .......... .......... .......... 80% 20.7M 8s
388350K .......... .......... .......... .......... .......... 80% 20.9M 8s
388400K .......... .......... .......... .......... .......... 80% 29.7M 8s
388450K .......... .......... .......... .......... .......... 80% 17.8M 8s
388500K .......... .......... .......... .......... .......... 80% 27.5M 8s
388550K .......... .......... .......... .......... .......... 80% 18.5M 8s
388600K .......... .......... .......... .......... .......... 80% 15.5M 8s
388650K .......... .......... .......... .......... .......... 80% 18.1M 8s
388700K .......... .......... .......... .......... .......... 80% 11.8M 8s
388750K .......... .......... .......... .......... .......... 80% 18.1M 8s
388800K .......... .......... .......... .......... .......... 80% 20.3M 8s
388850K .......... .......... .......... .......... .......... 80% 13.5M 8s
388900K .......... .......... .......... .......... .......... 80% 18.9M 8s
388950K .......... .......... .......... .......... .......... 80% 20.1M 8s
389000K .......... .......... .......... .......... .......... 80% 14.8M 8s
389050K .......... .......... .......... .......... .......... 80% 15.9M 8s
389100K .......... .......... .......... .......... .......... 80% 25.8M 8s
389150K .......... .......... .......... .......... .......... 80% 26.0M 8s
389200K .......... .......... .......... .......... .......... 80% 14.9M 8s
389250K .......... .......... .......... .......... .......... 80% 33.9M 8s
389300K .......... .......... .......... .......... .......... 81% 27.1M 8s
389350K .......... .......... .......... .......... .......... 81% 67.0M 8s
389400K .......... .......... .......... .......... .......... 81% 36.7M 8s
389450K .......... .......... .......... .......... .......... 81% 26.9M 8s
389500K .......... .......... .......... .......... .......... 81% 25.3M 8s
389550K .......... .......... .......... .......... .......... 81% 21.0M 8s
389600K .......... .......... .......... .......... .......... 81% 26.6M 8s
389650K .......... .......... .......... .......... .......... 81% 23.3M 8s
389700K .......... .......... .......... .......... .......... 81% 20.0M 8s
389750K .......... .......... .......... .......... .......... 81% 34.8M 8s
389800K .......... .......... .......... .......... .......... 81% 22.0M 8s
389850K .......... .......... .......... .......... .......... 81% 18.2M 8s
389900K .......... .......... .......... .......... .......... 81% 20.5M 8s
389950K .......... .......... .......... .......... .......... 81% 20.4M 8s
390000K .......... .......... .......... .......... .......... 81% 32.4M 8s
390050K .......... .......... .......... .......... .......... 81% 18.0M 8s
390100K .......... .......... .......... .......... .......... 81% 18.9M 8s
390150K .......... .......... .......... .......... .......... 81% 23.2M 8s
390200K .......... .......... .......... .......... .......... 81% 28.3M 8s
390250K .......... .......... .......... .......... .......... 81% 25.3M 8s
390300K .......... .......... .......... .......... .......... 81% 11.2M 8s
390350K .......... .......... .......... .......... .......... 81% 61.8M 8s
390400K .......... .......... .......... .......... .......... 81% 77.3M 8s
390450K .......... .......... .......... .......... .......... 81% 19.5M 8s
390500K .......... .......... .......... .......... .......... 81% 80.3M 8s
390550K .......... .......... .......... .......... .......... 81% 77.0M 8s
390600K .......... .......... .......... .......... .......... 81% 72.2M 8s
390650K .......... .......... .......... .......... .......... 81% 72.9M 8s
390700K .......... .......... .......... .......... .......... 81% 26.6M 8s
390750K .......... .......... .......... .......... .......... 81% 29.5M 8s
390800K .......... .......... .......... .......... .......... 81% 34.8M 8s
390850K .......... .......... .......... .......... .......... 81% 23.4M 8s
390900K .......... .......... .......... .......... .......... 81% 25.4M 8s
390950K .......... .......... .......... .......... .......... 81% 26.4M 8s
391000K .......... .......... .......... .......... .......... 81% 19.1M 8s
391050K .......... .......... .......... .......... .......... 81% 31.4M 8s
391100K .......... .......... .......... .......... .......... 81% 22.2M 8s
391150K .......... .......... .......... .......... .......... 81% 32.3M 8s
391200K .......... .......... .......... .......... .......... 81% 19.0M 8s
391250K .......... .......... .......... .......... .......... 81% 27.1M 8s
391300K .......... .......... .......... .......... .......... 81% 37.8M 8s
391350K .......... .......... .......... .......... .......... 81% 24.7M 8s
391400K .......... .......... .......... .......... .......... 81% 28.8M 8s
391450K .......... .......... .......... .......... .......... 81% 22.0M 8s
391500K .......... .......... .......... .......... .......... 81% 40.0M 8s
391550K .......... .......... .......... .......... .......... 81% 40.7M 8s
391600K .......... .......... .......... .......... .......... 81% 17.8M 8s
391650K .......... .......... .......... .......... .......... 81% 25.6M 8s
391700K .......... .......... .......... .......... .......... 81% 54.9M 8s
391750K .......... .......... .......... .......... .......... 81% 12.1M 8s
391800K .......... .......... .......... .......... .......... 81% 75.2M 8s
391850K .......... .......... .......... .......... .......... 81% 32.9M 8s
391900K .......... .......... .......... .......... .......... 81% 77.9M 8s
391950K .......... .......... .......... .......... .......... 81% 21.1M 8s
392000K .......... .......... .......... .......... .......... 81% 38.6M 8s
392050K .......... .......... .......... .......... .......... 81% 25.4M 8s
392100K .......... .......... .......... .......... .......... 81% 17.8M 8s
392150K .......... .......... .......... .......... .......... 81% 22.5M 8s
392200K .......... .......... .......... .......... .......... 81% 18.5M 8s
392250K .......... .......... .......... .......... .......... 81% 16.8M 8s
392300K .......... .......... .......... .......... .......... 81% 17.1M 8s
392350K .......... .......... .......... .......... .......... 81% 14.6M 8s
392400K .......... .......... .......... .......... .......... 81% 18.9M 8s
392450K .......... .......... .......... .......... .......... 81% 17.4M 8s
392500K .......... .......... .......... .......... .......... 81% 17.0M 8s
392550K .......... .......... .......... .......... .......... 81% 18.4M 8s
392600K .......... .......... .......... .......... .......... 81% 13.0M 7s
392650K .......... .......... .......... .......... .......... 81% 27.7M 7s
392700K .......... .......... .......... .......... .......... 81% 23.8M 7s
392750K .......... .......... .......... .......... .......... 81% 33.2M 7s
392800K .......... .......... .......... .......... .......... 81% 33.0M 7s
392850K .......... .......... .......... .......... .......... 81% 32.9M 7s
392900K .......... .......... .......... .......... .......... 81% 18.7M 7s
392950K .......... .......... .......... .......... .......... 81% 65.7M 7s
393000K .......... .......... .......... .......... .......... 81% 60.2M 7s
393050K .......... .......... .......... .......... .......... 81% 38.2M 7s
393100K .......... .......... .......... .......... .......... 81% 24.2M 7s
393150K .......... .......... .......... .......... .......... 81% 21.2M 7s
393200K .......... .......... .......... .......... .......... 81% 11.5M 7s
393250K .......... .......... .......... .......... .......... 81% 18.1M 7s
393300K .......... .......... .......... .......... .......... 81% 15.5M 7s
393350K .......... .......... .......... .......... .......... 81% 12.8M 7s
393400K .......... .......... .......... .......... .......... 81% 15.2M 7s
393450K .......... .......... .......... .......... .......... 81% 11.5M 7s
393500K .......... .......... .......... .......... .......... 81% 11.9M 7s
393550K .......... .......... .......... .......... .......... 81% 11.9M 7s
393600K .......... .......... .......... .......... .......... 81% 11.9M 7s
393650K .......... .......... .......... .......... .......... 81% 13.2M 7s
393700K .......... .......... .......... .......... .......... 81% 6.94M 7s
393750K .......... .......... .......... .......... .......... 81% 10.8M 7s
393800K .......... .......... .......... .......... .......... 81% 13.2M 7s
393850K .......... .......... .......... .......... .......... 81% 11.5M 7s
393900K .......... .......... .......... .......... .......... 81% 11.5M 7s
393950K .......... .......... .......... .......... .......... 81% 8.44M 7s
394000K .......... .......... .......... .......... .......... 81% 11.5M 7s
394050K .......... .......... .......... .......... .......... 81% 11.5M 7s
394100K .......... .......... .......... .......... .......... 82% 9.40M 7s
394150K .......... .......... .......... .......... .......... 82% 12.3M 7s
394200K .......... .......... .......... .......... .......... 82% 18.6M 7s
394250K .......... .......... .......... .......... .......... 82% 11.0M 7s
394300K .......... .......... .......... .......... .......... 82% 18.3M 7s
394350K .......... .......... .......... .......... .......... 82% 18.6M 7s
394400K .......... .......... .......... .......... .......... 82% 20.1M 7s
394450K .......... .......... .......... .......... .......... 82% 14.7M 7s
394500K .......... .......... .......... .......... .......... 82% 15.2M 7s
394550K .......... .......... .......... .......... .......... 82% 14.6M 7s
394600K .......... .......... .......... .......... .......... 82% 14.7M 7s
394650K .......... .......... .......... .......... .......... 82% 11.6M 7s
394700K .......... .......... .......... .......... .......... 82% 14.3M 7s
394750K .......... .......... .......... .......... .......... 82% 15.2M 7s
394800K .......... .......... .......... .......... .......... 82% 15.1M 7s
394850K .......... .......... .......... .......... .......... 82% 7.84M 7s
394900K .......... .......... .......... .......... .......... 82% 28.4M 7s
394950K .......... .......... .......... .......... .......... 82% 10.6M 7s
395000K .......... .......... .......... .......... .......... 82% 27.3M 7s
395050K .......... .......... .......... .......... .......... 82% 37.4M 7s
395100K .......... .......... .......... .......... .......... 82% 18.7M 7s
395150K .......... .......... .......... .......... .......... 82% 27.1M 7s
395200K .......... .......... .......... .......... .......... 82% 12.2M 7s
395250K .......... .......... .......... .......... .......... 82% 17.4M 7s
395300K .......... .......... .......... .......... .......... 82% 21.5M 7s
395350K .......... .......... .......... .......... .......... 82% 13.0M 7s
395400K .......... .......... .......... .......... .......... 82% 13.5M 7s
395450K .......... .......... .......... .......... .......... 82% 19.1M 7s
395500K .......... .......... .......... .......... .......... 82% 19.0M 7s
395550K .......... .......... .......... .......... .......... 82% 22.4M 7s
395600K .......... .......... .......... .......... .......... 82% 11.5M 7s
395650K .......... .......... .......... .......... .......... 82% 11.1M 7s
395700K .......... .......... .......... .......... .......... 82% 29.8M 7s
395750K .......... .......... .......... .......... .......... 82% 26.6M 7s
395800K .......... .......... .......... .......... .......... 82% 18.9M 7s
395850K .......... .......... .......... .......... .......... 82% 14.6M 7s
395900K .......... .......... .......... .......... .......... 82% 14.1M 7s
395950K .......... .......... .......... .......... .......... 82% 12.9M 7s
396000K .......... .......... .......... .......... .......... 82% 14.2M 7s
396050K .......... .......... .......... .......... .......... 82% 18.2M 7s
396100K .......... .......... .......... .......... .......... 82% 14.6M 7s
396150K .......... .......... .......... .......... .......... 82% 12.2M 7s
396200K .......... .......... .......... .......... .......... 82% 13.2M 7s
396250K .......... .......... .......... .......... .......... 82% 11.9M 7s
396300K .......... .......... .......... .......... .......... 82% 16.1M 7s
396350K .......... .......... .......... .......... .......... 82% 9.97M 7s
396400K .......... .......... .......... .......... .......... 82% 22.6M 7s
396450K .......... .......... .......... .......... .......... 82% 13.6M 7s
396500K .......... .......... .......... .......... .......... 82% 25.1M 7s
396550K .......... .......... .......... .......... .......... 82% 38.0M 7s
396600K .......... .......... .......... .......... .......... 82% 20.8M 7s
396650K .......... .......... .......... .......... .......... 82% 18.9M 7s
396700K .......... .......... .......... .......... .......... 82% 17.3M 7s
396750K .......... .......... .......... .......... .......... 82% 23.5M 7s
396800K .......... .......... .......... .......... .......... 82% 17.0M 7s
396850K .......... .......... .......... .......... .......... 82% 19.5M 7s
396900K .......... .......... .......... .......... .......... 82% 18.9M 7s
396950K .......... .......... .......... .......... .......... 82% 15.1M 7s
397000K .......... .......... .......... .......... .......... 82% 21.2M 7s
397050K .......... .......... .......... .......... .......... 82% 18.2M 7s
397100K .......... .......... .......... .......... .......... 82% 17.5M 7s
397150K .......... .......... .......... .......... .......... 82% 15.1M 7s
397200K .......... .......... .......... .......... .......... 82% 15.3M 7s
397250K .......... .......... .......... .......... .......... 82% 19.1M 7s
397300K .......... .......... .......... .......... .......... 82% 20.1M 7s
397350K .......... .......... .......... .......... .......... 82% 26.8M 7s
397400K .......... .......... .......... .......... .......... 82% 17.4M 7s
397450K .......... .......... .......... .......... .......... 82% 64.4M 7s
397500K .......... .......... .......... .......... .......... 82% 40.3M 7s
397550K .......... .......... .......... .......... .......... 82% 25.3M 7s
397600K .......... .......... .......... .......... .......... 82% 22.4M 7s
397650K .......... .......... .......... .......... .......... 82% 20.0M 7s
397700K .......... .......... .......... .......... .......... 82% 18.2M 7s
397750K .......... .......... .......... .......... .......... 82% 25.2M 7s
397800K .......... .......... .......... .......... .......... 82% 23.0M 7s
397850K .......... .......... .......... .......... .......... 82% 19.2M 7s
397900K .......... .......... .......... .......... .......... 82% 20.9M 7s
397950K .......... .......... .......... .......... .......... 82% 15.8M 7s
398000K .......... .......... .......... .......... .......... 82% 32.0M 7s
398050K .......... .......... .......... .......... .......... 82% 23.7M 7s
398100K .......... .......... .......... .......... .......... 82% 18.0M 7s
398150K .......... .......... .......... .......... .......... 82% 23.1M 7s
398200K .......... .......... .......... .......... .......... 82% 18.1M 7s
398250K .......... .......... .......... .......... .......... 82% 25.5M 7s
398300K .......... .......... .......... .......... .......... 82% 27.3M 7s
398350K .......... .......... .......... .......... .......... 82% 19.6M 7s
398400K .......... .......... .......... .......... .......... 82% 15.0M 7s
398450K .......... .......... .......... .......... .......... 82% 22.8M 7s
398500K .......... .......... .......... .......... .......... 82% 40.1M 7s
398550K .......... .......... .......... .......... .......... 82% 19.5M 7s
398600K .......... .......... .......... .......... .......... 82% 53.7M 7s
398650K .......... .......... .......... .......... .......... 82% 29.2M 7s
398700K .......... .......... .......... .......... .......... 82% 21.1M 7s
398750K .......... .......... .......... .......... .......... 82% 23.5M 7s
398800K .......... .......... .......... .......... .......... 82% 19.9M 7s
398850K .......... .......... .......... .......... .......... 82% 18.0M 7s
398900K .......... .......... .......... .......... .......... 83% 34.8M 7s
398950K .......... .......... .......... .......... .......... 83% 18.5M 7s
399000K .......... .......... .......... .......... .......... 83% 23.5M 7s
399050K .......... .......... .......... .......... .......... 83% 19.0M 7s
399100K .......... .......... .......... .......... .......... 83% 18.4M 7s
399150K .......... .......... .......... .......... .......... 83% 17.8M 7s
399200K .......... .......... .......... .......... .......... 83% 13.0M 7s
399250K .......... .......... .......... .......... .......... 83% 18.7M 7s
399300K .......... .......... .......... .......... .......... 83% 22.6M 7s
399350K .......... .......... .......... .......... .......... 83% 20.8M 7s
399400K .......... .......... .......... .......... .......... 83% 23.2M 7s
399450K .......... .......... .......... .......... .......... 83% 23.5M 7s
399500K .......... .......... .......... .......... .......... 83% 12.0M 7s
399550K .......... .......... .......... .......... .......... 83% 76.2M 7s
399600K .......... .......... .......... .......... .......... 83% 26.2M 7s
399650K .......... .......... .......... .......... .......... 83% 24.0M 7s
399700K .......... .......... .......... .......... .......... 83% 14.0M 7s
399750K .......... .......... .......... .......... .......... 83% 19.0M 7s
399800K .......... .......... .......... .......... .......... 83% 20.1M 7s
399850K .......... .......... .......... .......... .......... 83% 10.3M 7s
399900K .......... .......... .......... .......... .......... 83% 14.3M 7s
399950K .......... .......... .......... .......... .......... 83% 13.0M 7s
400000K .......... .......... .......... .......... .......... 83% 10.6M 7s
400050K .......... .......... .......... .......... .......... 83% 14.7M 7s
400100K .......... .......... .......... .......... .......... 83% 12.9M 7s
400150K .......... .......... .......... .......... .......... 83% 13.4M 7s
400200K .......... .......... .......... .......... .......... 83% 16.3M 7s
400250K .......... .......... .......... .......... .......... 83% 19.7M 7s
400300K .......... .......... .......... .......... .......... 83% 10.6M 7s
400350K .......... .......... .......... .......... .......... 83% 37.8M 7s
400400K .......... .......... .......... .......... .......... 83% 53.4M 7s
400450K .......... .......... .......... .......... .......... 83% 23.7M 7s
400500K .......... .......... .......... .......... .......... 83% 25.9M 7s
400550K .......... .......... .......... .......... .......... 83% 25.0M 7s
400600K .......... .......... .......... .......... .......... 83% 21.6M 7s
400650K .......... .......... .......... .......... .......... 83% 24.3M 7s
400700K .......... .......... .......... .......... .......... 83% 19.3M 7s
400750K .......... .......... .......... .......... .......... 83% 19.0M 7s
400800K .......... .......... .......... .......... .......... 83% 18.3M 7s
400850K .......... .......... .......... .......... .......... 83% 19.8M 7s
400900K .......... .......... .......... .......... .......... 83% 23.6M 7s
400950K .......... .......... .......... .......... .......... 83% 21.0M 7s
401000K .......... .......... .......... .......... .......... 83% 18.8M 7s
401050K .......... .......... .......... .......... .......... 83% 21.0M 7s
401100K .......... .......... .......... .......... .......... 83% 16.7M 7s
401150K .......... .......... .......... .......... .......... 83% 31.3M 7s
401200K .......... .......... .......... .......... .......... 83% 13.4M 7s
401250K .......... .......... .......... .......... .......... 83% 25.9M 7s
401300K .......... .......... .......... .......... .......... 83% 13.5M 7s
401350K .......... .......... .......... .......... .......... 83% 16.2M 7s
401400K .......... .......... .......... .......... .......... 83% 35.9M 7s
401450K .......... .......... .......... .......... .......... 83% 29.3M 7s
401500K .......... .......... .......... .......... .......... 83% 16.0M 7s
401550K .......... .......... .......... .......... .......... 83% 35.2M 7s
401600K .......... .......... .......... .......... .......... 83% 28.0M 7s
401650K .......... .......... .......... .......... .......... 83% 25.0M 7s
401700K .......... .......... .......... .......... .......... 83% 17.6M 7s
401750K .......... .......... .......... .......... .......... 83% 15.2M 7s
401800K .......... .......... .......... .......... .......... 83% 19.9M 7s
401850K .......... .......... .......... .......... .......... 83% 18.5M 7s
401900K .......... .......... .......... .......... .......... 83% 13.4M 7s
401950K .......... .......... .......... .......... .......... 83% 17.5M 7s
402000K .......... .......... .......... .......... .......... 83% 16.6M 7s
402050K .......... .......... .......... .......... .......... 83% 13.3M 7s
402100K .......... .......... .......... .......... .......... 83% 17.6M 7s
402150K .......... .......... .......... .......... .......... 83% 13.7M 7s
402200K .......... .......... .......... .......... .......... 83% 14.0M 7s
402250K .......... .......... .......... .......... .......... 83% 10.0M 7s
402300K .......... .......... .......... .......... .......... 83% 69.5M 7s
402350K .......... .......... .......... .......... .......... 83% 25.9M 7s
402400K .......... .......... .......... .......... .......... 83% 16.6M 7s
402450K .......... .......... .......... .......... .......... 83% 27.1M 7s
402500K .......... .......... .......... .......... .......... 83% 30.7M 7s
402550K .......... .......... .......... .......... .......... 83% 31.6M 7s
402600K .......... .......... .......... .......... .......... 83% 21.3M 7s
402650K .......... .......... .......... .......... .......... 83% 23.6M 7s
402700K .......... .......... .......... .......... .......... 83% 16.6M 7s
402750K .......... .......... .......... .......... .......... 83% 19.7M 7s
402800K .......... .......... .......... .......... .......... 83% 31.5M 7s
402850K .......... .......... .......... .......... .......... 83% 14.1M 7s
402900K .......... .......... .......... .......... .......... 83% 32.8M 7s
402950K .......... .......... .......... .......... .......... 83% 18.0M 7s
403000K .......... .......... .......... .......... .......... 83% 18.0M 7s
403050K .......... .......... .......... .......... .......... 83% 15.6M 7s
403100K .......... .......... .......... .......... .......... 83% 17.2M 7s
403150K .......... .......... .......... .......... .......... 83% 18.0M 7s
403200K .......... .......... .......... .......... .......... 83% 27.6M 7s
403250K .......... .......... .......... .......... .......... 83% 36.6M 7s
403300K .......... .......... .......... .......... .......... 83% 72.9M 7s
403350K .......... .......... .......... .......... .......... 83% 31.4M 7s
403400K .......... .......... .......... .......... .......... 83% 10.1M 7s
403450K .......... .......... .......... .......... .......... 83% 61.5M 7s
403500K .......... .......... .......... .......... .......... 83% 13.5M 7s
403550K .......... .......... .......... .......... .......... 83% 76.8M 7s
403600K .......... .......... .......... .......... .......... 83% 15.4M 6s
403650K .......... .......... .......... .......... .......... 83% 31.6M 6s
403700K .......... .......... .......... .......... .......... 84% 14.1M 6s
403750K .......... .......... .......... .......... .......... 84% 27.5M 6s
403800K .......... .......... .......... .......... .......... 84% 13.1M 6s
403850K .......... .......... .......... .......... .......... 84% 16.7M 6s
403900K .......... .......... .......... .......... .......... 84% 14.3M 6s
403950K .......... .......... .......... .......... .......... 84% 10.9M 6s
404000K .......... .......... .......... .......... .......... 84% 21.5M 6s
404050K .......... .......... .......... .......... .......... 84% 18.2M 6s
404100K .......... .......... .......... .......... .......... 84% 11.8M 6s
404150K .......... .......... .......... .......... .......... 84% 17.2M 6s
404200K .......... .......... .......... .......... .......... 84% 9.19M 6s
404250K .......... .......... .......... .......... .......... 84% 21.6M 6s
404300K .......... .......... .......... .......... .......... 84% 11.5M 6s
404350K .......... .......... .......... .......... .......... 84% 26.6M 6s
404400K .......... .......... .......... .......... .......... 84% 14.5M 6s
404450K .......... .......... .......... .......... .......... 84% 22.4M 6s
404500K .......... .......... .......... .......... .......... 84% 16.0M 6s
404550K .......... .......... .......... .......... .......... 84% 21.1M 6s
404600K .......... .......... .......... .......... .......... 84% 14.6M 6s
404650K .......... .......... .......... .......... .......... 84% 19.7M 6s
404700K .......... .......... .......... .......... .......... 84% 15.6M 6s
404750K .......... .......... .......... .......... .......... 84% 16.5M 6s
404800K .......... .......... .......... .......... .......... 84% 17.6M 6s
404850K .......... .......... .......... .......... .......... 84% 11.7M 6s
404900K .......... .......... .......... .......... .......... 84% 20.1M 6s
404950K .......... .......... .......... .......... .......... 84% 13.9M 6s
405000K .......... .......... .......... .......... .......... 84% 16.4M 6s
405050K .......... .......... .......... .......... .......... 84% 17.2M 6s
405100K .......... .......... .......... .......... .......... 84% 14.6M 6s
405150K .......... .......... .......... .......... .......... 84% 29.6M 6s
405200K .......... .......... .......... .......... .......... 84% 31.1M 6s
405250K .......... .......... .......... .......... .......... 84% 28.3M 6s
405300K .......... .......... .......... .......... .......... 84% 28.9M 6s
405350K .......... .......... .......... .......... .......... 84% 31.9M 6s
405400K .......... .......... .......... .......... .......... 84% 34.9M 6s
405450K .......... .......... .......... .......... .......... 84% 34.3M 6s
405500K .......... .......... .......... .......... .......... 84% 37.7M 6s
405550K .......... .......... .......... .......... .......... 84% 36.9M 6s
405600K .......... .......... .......... .......... .......... 84% 29.3M 6s
405650K .......... .......... .......... .......... .......... 84% 31.8M 6s
405700K .......... .......... .......... .......... .......... 84% 27.1M 6s
405750K .......... .......... .......... .......... .......... 84% 29.2M 6s
405800K .......... .......... .......... .......... .......... 84% 26.8M 6s
405850K .......... .......... .......... .......... .......... 84% 31.4M 6s
405900K .......... .......... .......... .......... .......... 84% 34.0M 6s
405950K .......... .......... .......... .......... .......... 84% 26.9M 6s
406000K .......... .......... .......... .......... .......... 84% 35.3M 6s
406050K .......... .......... .......... .......... .......... 84% 29.4M 6s
406100K .......... .......... .......... .......... .......... 84% 30.1M 6s
406150K .......... .......... .......... .......... .......... 84% 31.0M 6s
406200K .......... .......... .......... .......... .......... 84% 30.9M 6s
406250K .......... .......... .......... .......... .......... 84% 34.2M 6s
406300K .......... .......... .......... .......... .......... 84% 77.4M 6s
406350K .......... .......... .......... .......... .......... 84% 27.6M 6s
406400K .......... .......... .......... .......... .......... 84% 29.2M 6s
406450K .......... .......... .......... .......... .......... 84% 13.5M 6s
406500K .......... .......... .......... .......... .......... 84% 79.7M 6s
406550K .......... .......... .......... .......... .......... 84% 26.9M 6s
406600K .......... .......... .......... .......... .......... 84% 57.0M 6s
406650K .......... .......... .......... .......... .......... 84% 25.2M 6s
406700K .......... .......... .......... .......... .......... 84% 19.8M 6s
406750K .......... .......... .......... .......... .......... 84% 19.0M 6s
406800K .......... .......... .......... .......... .......... 84% 20.1M 6s
406850K .......... .......... .......... .......... .......... 84% 18.2M 6s
406900K .......... .......... .......... .......... .......... 84% 19.9M 6s
406950K .......... .......... .......... .......... .......... 84% 13.2M 6s
407000K .......... .......... .......... .......... .......... 84% 21.2M 6s
407050K .......... .......... .......... .......... .......... 84% 23.8M 6s
407100K .......... .......... .......... .......... .......... 84% 19.5M 6s
407150K .......... .......... .......... .......... .......... 84% 24.2M 6s
407200K .......... .......... .......... .......... .......... 84% 12.1M 6s
407250K .......... .......... .......... .......... .......... 84% 19.1M 6s
407300K .......... .......... .......... .......... .......... 84% 25.9M 6s
407350K .......... .......... .......... .......... .......... 84% 11.5M 6s
407400K .......... .......... .......... .......... .......... 84% 74.8M 6s
407450K .......... .......... .......... .......... .......... 84% 16.8M 6s
407500K .......... .......... .......... .......... .......... 84% 22.3M 6s
407550K .......... .......... .......... .......... .......... 84% 23.3M 6s
407600K .......... .......... .......... .......... .......... 84% 14.0M 6s
407650K .......... .......... .......... .......... .......... 84% 13.5M 6s
407700K .......... .......... .......... .......... .......... 84% 13.0M 6s
407750K .......... .......... .......... .......... .......... 84% 16.4M 6s
407800K .......... .......... .......... .......... .......... 84% 14.6M 6s
407850K .......... .......... .......... .......... .......... 84% 11.9M 6s
407900K .......... .......... .......... .......... .......... 84% 13.6M 6s
407950K .......... .......... .......... .......... .......... 84% 13.3M 6s
408000K .......... .......... .......... .......... .......... 84% 13.2M 6s
408050K .......... .......... .......... .......... .......... 84% 9.08M 6s
408100K .......... .......... .......... .......... .......... 84% 13.0M 6s
408150K .......... .......... .......... .......... .......... 84% 31.1M 6s
408200K .......... .......... .......... .......... .......... 84% 17.8M 6s
408250K .......... .......... .......... .......... .......... 84% 21.2M 6s
408300K .......... .......... .......... .......... .......... 84% 20.8M 6s
408350K .......... .......... .......... .......... .......... 84% 19.4M 6s
408400K .......... .......... .......... .......... .......... 84% 14.0M 6s
408450K .......... .......... .......... .......... .......... 84% 17.7M 6s
408500K .......... .......... .......... .......... .......... 85% 20.5M 6s
408550K .......... .......... .......... .......... .......... 85% 14.9M 6s
408600K .......... .......... .......... .......... .......... 85% 18.1M 6s
408650K .......... .......... .......... .......... .......... 85% 20.0M 6s
408700K .......... .......... .......... .......... .......... 85% 18.1M 6s
408750K .......... .......... .......... .......... .......... 85% 19.5M 6s
408800K .......... .......... .......... .......... .......... 85% 21.3M 6s
408850K .......... .......... .......... .......... .......... 85% 16.0M 6s
408900K .......... .......... .......... .......... .......... 85% 17.2M 6s
408950K .......... .......... .......... .......... .......... 85% 17.8M 6s
409000K .......... .......... .......... .......... .......... 85% 28.4M 6s
409050K .......... .......... .......... .......... .......... 85% 21.4M 6s
409100K .......... .......... .......... .......... .......... 85% 43.9M 6s
409150K .......... .......... .......... .......... .......... 85% 36.7M 6s
409200K .......... .......... .......... .......... .......... 85% 26.4M 6s
409250K .......... .......... .......... .......... .......... 85% 28.8M 6s
409300K .......... .......... .......... .......... .......... 85% 19.1M 6s
409350K .......... .......... .......... .......... .......... 85% 18.9M 6s
409400K .......... .......... .......... .......... .......... 85% 16.4M 6s
409450K .......... .......... .......... .......... .......... 85% 17.3M 6s
409500K .......... .......... .......... .......... .......... 85% 31.7M 6s
409550K .......... .......... .......... .......... .......... 85% 18.7M 6s
409600K .......... .......... .......... .......... .......... 85% 15.8M 6s
409650K .......... .......... .......... .......... .......... 85% 17.2M 6s
409700K .......... .......... .......... .......... .......... 85% 18.1M 6s
409750K .......... .......... .......... .......... .......... 85% 21.1M 6s
409800K .......... .......... .......... .......... .......... 85% 16.3M 6s
409850K .......... .......... .......... .......... .......... 85% 28.2M 6s
409900K .......... .......... .......... .......... .......... 85% 23.4M 6s
409950K .......... .......... .......... .......... .......... 85% 21.1M 6s
410000K .......... .......... .......... .......... .......... 85% 26.2M 6s
410050K .......... .......... .......... .......... .......... 85% 17.2M 6s
410100K .......... .......... .......... .......... .......... 85% 31.1M 6s
410150K .......... .......... .......... .......... .......... 85% 20.9M 6s
410200K .......... .......... .......... .......... .......... 85% 21.8M 6s
410250K .......... .......... .......... .......... .......... 85% 18.2M 6s
410300K .......... .......... .......... .......... .......... 85% 19.1M 6s
410350K .......... .......... .......... .......... .......... 85% 13.6M 6s
410400K .......... .......... .......... .......... .......... 85% 19.1M 6s
410450K .......... .......... .......... .......... .......... 85% 19.2M 6s
410500K .......... .......... .......... .......... .......... 85% 14.1M 6s
410550K .......... .......... .......... .......... .......... 85% 20.8M 6s
410600K .......... .......... .......... .......... .......... 85% 20.7M 6s
410650K .......... .......... .......... .......... .......... 85% 13.5M 6s
410700K .......... .......... .......... .......... .......... 85% 16.7M 6s
410750K .......... .......... .......... .......... .......... 85% 29.2M 6s
410800K .......... .......... .......... .......... .......... 85% 11.8M 6s
410850K .......... .......... .......... .......... .......... 85% 80.6M 6s
410900K .......... .......... .......... .......... .......... 85% 24.0M 6s
410950K .......... .......... .......... .......... .......... 85% 83.2M 6s
411000K .......... .......... .......... .......... .......... 85% 25.9M 6s
411050K .......... .......... .......... .......... .......... 85% 33.7M 6s
411100K .......... .......... .......... .......... .......... 85% 28.9M 6s
411150K .......... .......... .......... .......... .......... 85% 25.6M 6s
411200K .......... .......... .......... .......... .......... 85% 21.5M 6s
411250K .......... .......... .......... .......... .......... 85% 14.1M 6s
411300K .......... .......... .......... .......... .......... 85% 30.1M 6s
411350K .......... .......... .......... .......... .......... 85% 16.9M 6s
411400K .......... .......... .......... .......... .......... 85% 22.0M 6s
411450K .......... .......... .......... .......... .......... 85% 17.1M 6s
411500K .......... .......... .......... .......... .......... 85% 28.0M 6s
411550K .......... .......... .......... .......... .......... 85% 18.4M 6s
411600K .......... .......... .......... .......... .......... 85% 18.5M 6s
411650K .......... .......... .......... .......... .......... 85% 30.7M 6s
411700K .......... .......... .......... .......... .......... 85% 20.5M 6s
411750K .......... .......... .......... .......... .......... 85% 25.5M 6s
411800K .......... .......... .......... .......... .......... 85% 26.1M 6s
411850K .......... .......... .......... .......... .......... 85% 15.0M 6s
411900K .......... .......... .......... .......... .......... 85% 14.7M 6s
411950K .......... .......... .......... .......... .......... 85% 65.0M 6s
412000K .......... .......... .......... .......... .......... 85% 42.0M 6s
412050K .......... .......... .......... .......... .......... 85% 30.6M 6s
412100K .......... .......... .......... .......... .......... 85% 26.1M 6s
412150K .......... .......... .......... .......... .......... 85% 22.0M 6s
412200K .......... .......... .......... .......... .......... 85% 14.9M 6s
412250K .......... .......... .......... .......... .......... 85% 13.5M 6s
412300K .......... .......... .......... .......... .......... 85% 12.2M 6s
412350K .......... .......... .......... .......... .......... 85% 13.5M 6s
412400K .......... .......... .......... .......... .......... 85% 12.7M 6s
412450K .......... .......... .......... .......... .......... 85% 13.2M 6s
412500K .......... .......... .......... .......... .......... 85% 15.1M 6s
412550K .......... .......... .......... .......... .......... 85% 14.9M 6s
412600K .......... .......... .......... .......... .......... 85% 14.4M 6s
412650K .......... .......... .......... .......... .......... 85% 26.2M 6s
412700K .......... .......... .......... .......... .......... 85% 20.8M 6s
412750K .......... .......... .......... .......... .......... 85% 22.0M 6s
412800K .......... .......... .......... .......... .......... 85% 19.6M 6s
412850K .......... .......... .......... .......... .......... 85% 24.6M 6s
412900K .......... .......... .......... .......... .......... 85% 50.5M 6s
412950K .......... .......... .......... .......... .......... 85% 22.2M 6s
413000K .......... .......... .......... .......... .......... 85% 25.3M 6s
413050K .......... .......... .......... .......... .......... 85% 31.3M 6s
413100K .......... .......... .......... .......... .......... 85% 21.3M 6s
413150K .......... .......... .......... .......... .......... 85% 35.2M 6s
413200K .......... .......... .......... .......... .......... 85% 18.9M 6s
413250K .......... .......... .......... .......... .......... 85% 31.5M 6s
413300K .......... .......... .......... .......... .......... 86% 26.7M 6s
413350K .......... .......... .......... .......... .......... 86% 16.6M 6s
413400K .......... .......... .......... .......... .......... 86% 30.8M 6s
413450K .......... .......... .......... .......... .......... 86% 17.0M 6s
413500K .......... .......... .......... .......... .......... 86% 27.4M 6s
413550K .......... .......... .......... .......... .......... 86% 24.8M 6s
413600K .......... .......... .......... .......... .......... 86% 29.3M 6s
413650K .......... .......... .......... .......... .......... 86% 23.6M 6s
413700K .......... .......... .......... .......... .......... 86% 19.8M 6s
413750K .......... .......... .......... .......... .......... 86% 22.7M 6s
413800K .......... .......... .......... .......... .......... 86% 31.9M 6s
413850K .......... .......... .......... .......... .......... 86% 11.1M 6s
413900K .......... .......... .......... .......... .......... 86% 61.5M 6s
413950K .......... .......... .......... .......... .......... 86% 74.9M 6s
414000K .......... .......... .......... .......... .......... 86% 61.0M 6s
414050K .......... .......... .......... .......... .......... 86% 14.3M 6s
414100K .......... .......... .......... .......... .......... 86% 64.8M 6s
414150K .......... .......... .......... .......... .......... 86% 76.9M 6s
414200K .......... .......... .......... .......... .......... 86% 28.2M 6s
414250K .......... .......... .......... .......... .......... 86% 24.8M 6s
414300K .......... .......... .......... .......... .......... 86% 30.7M 6s
414350K .......... .......... .......... .......... .......... 86% 18.0M 6s
414400K .......... .......... .......... .......... .......... 86% 29.7M 6s
414450K .......... .......... .......... .......... .......... 86% 21.0M 6s
414500K .......... .......... .......... .......... .......... 86% 18.9M 6s
414550K .......... .......... .......... .......... .......... 86% 23.7M 6s
414600K .......... .......... .......... .......... .......... 86% 19.9M 6s
414650K .......... .......... .......... .......... .......... 86% 27.1M 5s
414700K .......... .......... .......... .......... .......... 86% 19.7M 5s
414750K .......... .......... .......... .......... .......... 86% 23.8M 5s
414800K .......... .......... .......... .......... .......... 86% 25.4M 5s
414850K .......... .......... .......... .......... .......... 86% 20.9M 5s
414900K .......... .......... .......... .......... .......... 86% 17.8M 5s
414950K .......... .......... .......... .......... .......... 86% 17.1M 5s
415000K .......... .......... .......... .......... .......... 86% 23.4M 5s
415050K .......... .......... .......... .......... .......... 86% 20.5M 5s
415100K .......... .......... .......... .......... .......... 86% 12.5M 5s
415150K .......... .......... .......... .......... .......... 86% 73.3M 5s
415200K .......... .......... .......... .......... .......... 86% 27.5M 5s
415250K .......... .......... .......... .......... .......... 86% 24.1M 5s
415300K .......... .......... .......... .......... .......... 86% 37.4M 5s
415350K .......... .......... .......... .......... .......... 86% 15.6M 5s
415400K .......... .......... .......... .......... .......... 86% 16.4M 5s
415450K .......... .......... .......... .......... .......... 86% 14.0M 5s
415500K .......... .......... .......... .......... .......... 86% 15.8M 5s
415550K .......... .......... .......... .......... .......... 86% 12.7M 5s
415600K .......... .......... .......... .......... .......... 86% 14.7M 5s
415650K .......... .......... .......... .......... .......... 86% 12.9M 5s
415700K .......... .......... .......... .......... .......... 86% 13.6M 5s
415750K .......... .......... .......... .......... .......... 86% 15.1M 5s
415800K .......... .......... .......... .......... .......... 86% 10.9M 5s
415850K .......... .......... .......... .......... .......... 86% 12.6M 5s
415900K .......... .......... .......... .......... .......... 86% 15.1M 5s
415950K .......... .......... .......... .......... .......... 86% 14.7M 5s
416000K .......... .......... .......... .......... .......... 86% 20.8M 5s
416050K .......... .......... .......... .......... .......... 86% 17.1M 5s
416100K .......... .......... .......... .......... .......... 86% 13.8M 5s
416150K .......... .......... .......... .......... .......... 86% 15.7M 5s
416200K .......... .......... .......... .......... .......... 86% 16.6M 5s
416250K .......... .......... .......... .......... .......... 86% 14.4M 5s
416300K .......... .......... .......... .......... .......... 86% 12.8M 5s
416350K .......... .......... .......... .......... .......... 86% 13.5M 5s
416400K .......... .......... .......... .......... .......... 86% 13.1M 5s
416450K .......... .......... .......... .......... .......... 86% 13.5M 5s
416500K .......... .......... .......... .......... .......... 86% 14.1M 5s
416550K .......... .......... .......... .......... .......... 86% 15.3M 5s
416600K .......... .......... .......... .......... .......... 86% 9.05M 5s
416650K .......... .......... .......... .......... .......... 86% 31.8M 5s
416700K .......... .......... .......... .......... .......... 86% 29.8M 5s
416750K .......... .......... .......... .......... .......... 86% 38.7M 5s
416800K .......... .......... .......... .......... .......... 86% 42.4M 5s
416850K .......... .......... .......... .......... .......... 86% 45.1M 5s
416900K .......... .......... .......... .......... .......... 86% 40.7M 5s
416950K .......... .......... .......... .......... .......... 86% 46.5M 5s
417000K .......... .......... .......... .......... .......... 86% 52.2M 5s
417050K .......... .......... .......... .......... .......... 86% 36.5M 5s
417100K .......... .......... .......... .......... .......... 86% 45.8M 5s
417150K .......... .......... .......... .......... .......... 86% 48.4M 5s
417200K .......... .......... .......... .......... .......... 86% 43.9M 5s
417250K .......... .......... .......... .......... .......... 86% 41.7M 5s
417300K .......... .......... .......... .......... .......... 86% 53.0M 5s
417350K .......... .......... .......... .......... .......... 86% 35.9M 5s
417400K .......... .......... .......... .......... .......... 86% 32.9M 5s
417450K .......... .......... .......... .......... .......... 86% 37.8M 5s
417500K .......... .......... .......... .......... .......... 86% 61.7M 5s
417550K .......... .......... .......... .......... .......... 86% 37.5M 5s
417600K .......... .......... .......... .......... .......... 86% 28.5M 5s
417650K .......... .......... .......... .......... .......... 86%  102M 5s
417700K .......... .......... .......... .......... .......... 86% 31.4M 5s
417750K .......... .......... .......... .......... .......... 86% 62.7M 5s
417800K .......... .......... .......... .......... .......... 86% 48.8M 5s
417850K .......... .......... .......... .......... .......... 86% 23.2M 5s
417900K .......... .......... .......... .......... .......... 86% 33.4M 5s
417950K .......... .......... .......... .......... .......... 86% 35.4M 5s
418000K .......... .......... .......... .......... .......... 86% 47.5M 5s
418050K .......... .......... .......... .......... .......... 86% 37.6M 5s
418100K .......... .......... .......... .......... .......... 87% 37.6M 5s
418150K .......... .......... .......... .......... .......... 87% 42.7M 5s
418200K .......... .......... .......... .......... .......... 87% 36.2M 5s
418250K .......... .......... .......... .......... .......... 87% 36.2M 5s
418300K .......... .......... .......... .......... .......... 87% 9.97M 5s
418350K .......... .......... .......... .......... .......... 87% 97.5M 5s
418400K .......... .......... .......... .......... .......... 87% 13.3M 5s
418450K .......... .......... .......... .......... .......... 87% 16.5M 5s
418500K .......... .......... .......... .......... .......... 87% 17.1M 5s
418550K .......... .......... .......... .......... .......... 87% 14.6M 5s
418600K .......... .......... .......... .......... .......... 87% 11.2M 5s
418650K .......... .......... .......... .......... .......... 87% 14.6M 5s
418700K .......... .......... .......... .......... .......... 87% 11.9M 5s
418750K .......... .......... .......... .......... .......... 87% 15.2M 5s
418800K .......... .......... .......... .......... .......... 87% 11.6M 5s
418850K .......... .......... .......... .......... .......... 87% 13.0M 5s
418900K .......... .......... .......... .......... .......... 87% 11.4M 5s
418950K .......... .......... .......... .......... .......... 87% 11.9M 5s
419000K .......... .......... .......... .......... .......... 87% 11.6M 5s
419050K .......... .......... .......... .......... .......... 87% 31.0M 5s
419100K .......... .......... .......... .......... .......... 87% 37.0M 5s
419150K .......... .......... .......... .......... .......... 87% 18.8M 5s
419200K .......... .......... .......... .......... .......... 87% 18.9M 5s
419250K .......... .......... .......... .......... .......... 87% 22.2M 5s
419300K .......... .......... .......... .......... .......... 87% 22.5M 5s
419350K .......... .......... .......... .......... .......... 87% 17.2M 5s
419400K .......... .......... .......... .......... .......... 87% 20.0M 5s
419450K .......... .......... .......... .......... .......... 87% 12.3M 5s
419500K .......... .......... .......... .......... .......... 87% 17.2M 5s
419550K .......... .......... .......... .......... .......... 87% 20.4M 5s
419600K .......... .......... .......... .......... .......... 87% 18.2M 5s
419650K .......... .......... .......... .......... .......... 87% 18.6M 5s
419700K .......... .......... .......... .......... .......... 87% 13.4M 5s
419750K .......... .......... .......... .......... .......... 87% 18.2M 5s
419800K .......... .......... .......... .......... .......... 87% 19.9M 5s
419850K .......... .......... .......... .......... .......... 87% 16.3M 5s
419900K .......... .......... .......... .......... .......... 87% 16.5M 5s
419950K .......... .......... .......... .......... .......... 87% 22.3M 5s
420000K .......... .......... .......... .......... .......... 87% 29.7M 5s
420050K .......... .......... .......... .......... .......... 87% 13.2M 5s
420100K .......... .......... .......... .......... .......... 87% 59.6M 5s
420150K .......... .......... .......... .......... .......... 87% 30.9M 5s
420200K .......... .......... .......... .......... .......... 87% 62.8M 5s
420250K .......... .......... .......... .......... .......... 87% 43.9M 5s
420300K .......... .......... .......... .......... .......... 87% 28.0M 5s
420350K .......... .......... .......... .......... .......... 87% 27.8M 5s
420400K .......... .......... .......... .......... .......... 87% 20.7M 5s
420450K .......... .......... .......... .......... .......... 87% 27.1M 5s
420500K .......... .......... .......... .......... .......... 87% 25.0M 5s
420550K .......... .......... .......... .......... .......... 87% 26.6M 5s
420600K .......... .......... .......... .......... .......... 87% 31.2M 5s
420650K .......... .......... .......... .......... .......... 87% 33.7M 5s
420700K .......... .......... .......... .......... .......... 87% 24.1M 5s
420750K .......... .......... .......... .......... .......... 87% 21.9M 5s
420800K .......... .......... .......... .......... .......... 87% 34.1M 5s
420850K .......... .......... .......... .......... .......... 87% 25.5M 5s
420900K .......... .......... .......... .......... .......... 87% 34.3M 5s
420950K .......... .......... .......... .......... .......... 87% 22.6M 5s
421000K .......... .......... .......... .......... .......... 87% 19.4M 5s
421050K .......... .......... .......... .......... .......... 87% 33.5M 5s
421100K .......... .......... .......... .......... .......... 87% 22.7M 5s
421150K .......... .......... .......... .......... .......... 87% 33.9M 5s
421200K .......... .......... .......... .......... .......... 87% 21.0M 5s
421250K .......... .......... .......... .......... .......... 87% 33.8M 5s
421300K .......... .......... .......... .......... .......... 87% 71.0M 5s
421350K .......... .......... .......... .......... .......... 87% 19.9M 5s
421400K .......... .......... .......... .......... .......... 87% 19.1M 5s
421450K .......... .......... .......... .......... .......... 87% 49.7M 5s
421500K .......... .......... .......... .......... .......... 87% 35.2M 5s
421550K .......... .......... .......... .......... .......... 87% 36.6M 5s
421600K .......... .......... .......... .......... .......... 87% 34.5M 5s
421650K .......... .......... .......... .......... .......... 87% 29.3M 5s
421700K .......... .......... .......... .......... .......... 87% 37.0M 5s
421750K .......... .......... .......... .......... .......... 87% 27.1M 5s
421800K .......... .......... .......... .......... .......... 87% 23.7M 5s
421850K .......... .......... .......... .......... .......... 87% 15.1M 5s
421900K .......... .......... .......... .......... .......... 87% 18.0M 5s
421950K .......... .......... .......... .......... .......... 87% 18.1M 5s
422000K .......... .......... .......... .......... .......... 87% 13.1M 5s
422050K .......... .......... .......... .......... .......... 87% 21.1M 5s
422100K .......... .......... .......... .......... .......... 87% 19.2M 5s
422150K .......... .......... .......... .......... .......... 87% 14.4M 5s
422200K .......... .......... .......... .......... .......... 87% 19.1M 5s
422250K .......... .......... .......... .......... .......... 87% 20.2M 5s
422300K .......... .......... .......... .......... .......... 87% 13.4M 5s
422350K .......... .......... .......... .......... .......... 87% 28.5M 5s
422400K .......... .......... .......... .......... .......... 87% 10.4M 5s
422450K .......... .......... .......... .......... .......... 87% 63.0M 5s
422500K .......... .......... .......... .......... .......... 87% 23.7M 5s
422550K .......... .......... .......... .......... .......... 87% 20.4M 5s
422600K .......... .......... .......... .......... .......... 87% 32.2M 5s
422650K .......... .......... .......... .......... .......... 87% 31.7M 5s
422700K .......... .......... .......... .......... .......... 87% 23.6M 5s
422750K .......... .......... .......... .......... .......... 87% 22.1M 5s
422800K .......... .......... .......... .......... .......... 87% 29.5M 5s
422850K .......... .......... .......... .......... .......... 87% 18.1M 5s
422900K .......... .......... .......... .......... .......... 88% 16.9M 5s
422950K .......... .......... .......... .......... .......... 88% 21.2M 5s
423000K .......... .......... .......... .......... .......... 88% 32.9M 5s
423050K .......... .......... .......... .......... .......... 88% 17.7M 5s
423100K .......... .......... .......... .......... .......... 88% 17.1M 5s
423150K .......... .......... .......... .......... .......... 88% 19.9M 5s
423200K .......... .......... .......... .......... .......... 88% 18.1M 5s
423250K .......... .......... .......... .......... .......... 88% 27.4M 5s
423300K .......... .......... .......... .......... .......... 88% 18.0M 5s
423350K .......... .......... .......... .......... .......... 88% 27.7M 5s
423400K .......... .......... .......... .......... .......... 88% 27.4M 5s
423450K .......... .......... .......... .......... .......... 88% 17.1M 5s
423500K .......... .......... .......... .......... .......... 88% 79.0M 5s
423550K .......... .......... .......... .......... .......... 88% 20.9M 5s
423600K .......... .......... .......... .......... .......... 88% 23.7M 5s
423650K .......... .......... .......... .......... .......... 88% 73.2M 5s
423700K .......... .......... .......... .......... .......... 88% 14.8M 5s
423750K .......... .......... .......... .......... .......... 88% 74.3M 5s
423800K .......... .......... .......... .......... .......... 88% 59.0M 5s
423850K .......... .......... .......... .......... .......... 88% 59.5M 5s
423900K .......... .......... .......... .......... .......... 88% 34.9M 5s
423950K .......... .......... .......... .......... .......... 88% 45.3M 5s
424000K .......... .......... .......... .......... .......... 88% 31.2M 5s
424050K .......... .......... .......... .......... .......... 88% 41.0M 5s
424100K .......... .......... .......... .......... .......... 88% 19.9M 5s
424150K .......... .......... .......... .......... .......... 88% 30.1M 5s
424200K .......... .......... .......... .......... .......... 88% 16.8M 5s
424250K .......... .......... .......... .......... .......... 88% 30.9M 5s
424300K .......... .......... .......... .......... .......... 88% 17.9M 5s
424350K .......... .......... .......... .......... .......... 88% 26.0M 5s
424400K .......... .......... .......... .......... .......... 88% 19.9M 5s
424450K .......... .......... .......... .......... .......... 88% 19.1M 5s
424500K .......... .......... .......... .......... .......... 88% 32.8M 5s
424550K .......... .......... .......... .......... .......... 88% 19.9M 5s
424600K .......... .......... .......... .......... .......... 88% 31.0M 5s
424650K .......... .......... .......... .......... .......... 88% 18.4M 5s
424700K .......... .......... .......... .......... .......... 88% 19.7M 5s
424750K .......... .......... .......... .......... .......... 88% 27.9M 5s
424800K .......... .......... .......... .......... .......... 88% 30.2M 5s
424850K .......... .......... .......... .......... .......... 88% 22.8M 5s
424900K .......... .......... .......... .......... .......... 88% 22.2M 5s
424950K .......... .......... .......... .......... .......... 88% 13.8M 5s
425000K .......... .......... .......... .......... .......... 88% 76.2M 5s
425050K .......... .......... .......... .......... .......... 88% 75.2M 5s
425100K .......... .......... .......... .......... .......... 88% 23.1M 5s
425150K .......... .......... .......... .......... .......... 88% 79.3M 5s
425200K .......... .......... .......... .......... .......... 88% 22.6M 5s
425250K .......... .......... .......... .......... .......... 88% 33.1M 5s
425300K .......... .......... .......... .......... .......... 88% 28.8M 5s
425350K .......... .......... .......... .......... .......... 88% 28.6M 5s
425400K .......... .......... .......... .......... .......... 88% 23.5M 5s
425450K .......... .......... .......... .......... .......... 88% 22.2M 5s
425500K .......... .......... .......... .......... .......... 88% 23.2M 5s
425550K .......... .......... .......... .......... .......... 88% 30.7M 5s
425600K .......... .......... .......... .......... .......... 88% 17.8M 5s
425650K .......... .......... .......... .......... .......... 88% 17.0M 5s
425700K .......... .......... .......... .......... .......... 88% 17.3M 5s
425750K .......... .......... .......... .......... .......... 88% 18.8M 5s
425800K .......... .......... .......... .......... .......... 88% 29.8M 5s
425850K .......... .......... .......... .......... .......... 88% 20.3M 5s
425900K .......... .......... .......... .......... .......... 88% 16.0M 5s
425950K .......... .......... .......... .......... .......... 88% 18.2M 5s
426000K .......... .......... .......... .......... .......... 88% 31.1M 4s
426050K .......... .......... .......... .......... .......... 88% 23.3M 4s
426100K .......... .......... .......... .......... .......... 88% 17.5M 4s
426150K .......... .......... .......... .......... .......... 88% 15.3M 4s
426200K .......... .......... .......... .......... .......... 88% 11.7M 4s
426250K .......... .......... .......... .......... .......... 88% 23.5M 4s
426300K .......... .......... .......... .......... .......... 88% 79.5M 4s
426350K .......... .......... .......... .......... .......... 88% 12.5M 4s
426400K .......... .......... .......... .......... .......... 88% 17.0M 4s
426450K .......... .......... .......... .......... .......... 88% 25.1M 4s
426500K .......... .......... .......... .......... .......... 88% 21.0M 4s
426550K .......... .......... .......... .......... .......... 88% 15.9M 4s
426600K .......... .......... .......... .......... .......... 88% 13.9M 4s
426650K .......... .......... .......... .......... .......... 88% 15.9M 4s
426700K .......... .......... .......... .......... .......... 88% 14.0M 4s
426750K .......... .......... .......... .......... .......... 88% 17.4M 4s
426800K .......... .......... .......... .......... .......... 88% 13.2M 4s
426850K .......... .......... .......... .......... .......... 88% 14.3M 4s
426900K .......... .......... .......... .......... .......... 88% 16.3M 4s
426950K .......... .......... .......... .......... .......... 88% 12.3M 4s
427000K .......... .......... .......... .......... .......... 88% 13.6M 4s
427050K .......... .......... .......... .......... .......... 88% 19.6M 4s
427100K .......... .......... .......... .......... .......... 88% 21.5M 4s
427150K .......... .......... .......... .......... .......... 88% 12.6M 4s
427200K .......... .......... .......... .......... .......... 88% 13.1M 4s
427250K .......... .......... .......... .......... .......... 88% 87.5M 4s
427300K .......... .......... .......... .......... .......... 88% 28.8M 4s
427350K .......... .......... .......... .......... .......... 88% 18.2M 4s
427400K .......... .......... .......... .......... .......... 88% 25.4M 4s
427450K .......... .......... .......... .......... .......... 88% 24.1M 4s
427500K .......... .......... .......... .......... .......... 88% 22.2M 4s
427550K .......... .......... .......... .......... .......... 88% 24.0M 4s
427600K .......... .......... .......... .......... .......... 88% 21.2M 4s
427650K .......... .......... .......... .......... .......... 88% 13.1M 4s
427700K .......... .......... .......... .......... .......... 89% 17.9M 4s
427750K .......... .......... .......... .......... .......... 89% 23.2M 4s
427800K .......... .......... .......... .......... .......... 89% 33.5M 4s
427850K .......... .......... .......... .......... .......... 89% 21.2M 4s
427900K .......... .......... .......... .......... .......... 89% 19.0M 4s
427950K .......... .......... .......... .......... .......... 89% 18.0M 4s
428000K .......... .......... .......... .......... .......... 89% 24.1M 4s
428050K .......... .......... .......... .......... .......... 89% 23.5M 4s
428100K .......... .......... .......... .......... .......... 89% 29.4M 4s
428150K .......... .......... .......... .......... .......... 89% 14.0M 4s
428200K .......... .......... .......... .......... .......... 89% 36.0M 4s
428250K .......... .......... .......... .......... .......... 89% 51.3M 4s
428300K .......... .......... .......... .......... .......... 89% 28.1M 4s
428350K .......... .......... .......... .......... .......... 89% 33.2M 4s
428400K .......... .......... .......... .......... .......... 89% 20.1M 4s
428450K .......... .......... .......... .......... .......... 89% 17.4M 4s
428500K .......... .......... .......... .......... .......... 89% 14.5M 4s
428550K .......... .......... .......... .......... .......... 89% 13.6M 4s
428600K .......... .......... .......... .......... .......... 89% 13.6M 4s
428650K .......... .......... .......... .......... .......... 89% 13.6M 4s
428700K .......... .......... .......... .......... .......... 89% 13.0M 4s
428750K .......... .......... .......... .......... .......... 89% 14.6M 4s
428800K .......... .......... .......... .......... .......... 89% 14.0M 4s
428850K .......... .......... .......... .......... .......... 89% 13.2M 4s
428900K .......... .......... .......... .......... .......... 89% 22.3M 4s
428950K .......... .......... .......... .......... .......... 89% 12.3M 4s
429000K .......... .......... .......... .......... .......... 89% 22.0M 4s
429050K .......... .......... .......... .......... .......... 89% 19.0M 4s
429100K .......... .......... .......... .......... .......... 89% 17.2M 4s
429150K .......... .......... .......... .......... .......... 89% 16.6M 4s
429200K .......... .......... .......... .......... .......... 89% 19.2M 4s
429250K .......... .......... .......... .......... .......... 89% 16.4M 4s
429300K .......... .......... .......... .......... .......... 89% 17.3M 4s
429350K .......... .......... .......... .......... .......... 89% 16.0M 4s
429400K .......... .......... .......... .......... .......... 89% 12.9M 4s
429450K .......... .......... .......... .......... .......... 89% 19.1M 4s
429500K .......... .......... .......... .......... .......... 89% 13.1M 4s
429550K .......... .......... .......... .......... .......... 89% 17.3M 4s
429600K .......... .......... .......... .......... .......... 89% 19.3M 4s
429650K .......... .......... .......... .......... .......... 89% 15.0M 4s
429700K .......... .......... .......... .......... .......... 89% 15.2M 4s
429750K .......... .......... .......... .......... .......... 89% 76.4M 4s
429800K .......... .......... .......... .......... .......... 89% 22.9M 4s
429850K .......... .......... .......... .......... .......... 89% 20.4M 4s
429900K .......... .......... .......... .......... .......... 89% 15.2M 4s
429950K .......... .......... .......... .......... .......... 89% 68.0M 4s
430000K .......... .......... .......... .......... .......... 89% 23.1M 4s
430050K .......... .......... .......... .......... .......... 89% 52.9M 4s
430100K .......... .......... .......... .......... .......... 89% 20.1M 4s
430150K .......... .......... .......... .......... .......... 89% 31.2M 4s
430200K .......... .......... .......... .......... .......... 89% 17.4M 4s
430250K .......... .......... .......... .......... .......... 89% 27.7M 4s
430300K .......... .......... .......... .......... .......... 89% 24.8M 4s
430350K .......... .......... .......... .......... .......... 89% 22.1M 4s
430400K .......... .......... .......... .......... .......... 89% 26.9M 4s
430450K .......... .......... .......... .......... .......... 89% 22.1M 4s
430500K .......... .......... .......... .......... .......... 89% 22.2M 4s
430550K .......... .......... .......... .......... .......... 89% 17.1M 4s
430600K .......... .......... .......... .......... .......... 89% 26.3M 4s
430650K .......... .......... .......... .......... .......... 89% 19.4M 4s
430700K .......... .......... .......... .......... .......... 89% 18.8M 4s
430750K .......... .......... .......... .......... .......... 89% 35.3M 4s
430800K .......... .......... .......... .......... .......... 89% 26.9M 4s
430850K .......... .......... .......... .......... .......... 89% 17.8M 4s
430900K .......... .......... .......... .......... .......... 89% 25.2M 4s
430950K .......... .......... .......... .......... .......... 89% 18.3M 4s
431000K .......... .......... .......... .......... .......... 89% 24.5M 4s
431050K .......... .......... .......... .......... .......... 89% 83.8M 4s
431100K .......... .......... .......... .......... .......... 89% 20.5M 4s
431150K .......... .......... .......... .......... .......... 89% 32.5M 4s
431200K .......... .......... .......... .......... .......... 89% 20.0M 4s
431250K .......... .......... .......... .......... .......... 89% 30.9M 4s
431300K .......... .......... .......... .......... .......... 89% 15.6M 4s
431350K .......... .......... .......... .......... .......... 89% 21.4M 4s
431400K .......... .......... .......... .......... .......... 89% 20.7M 4s
431450K .......... .......... .......... .......... .......... 89% 18.3M 4s
431500K .......... .......... .......... .......... .......... 89% 13.3M 4s
431550K .......... .......... .......... .......... .......... 89% 22.1M 4s
431600K .......... .......... .......... .......... .......... 89% 18.1M 4s
431650K .......... .......... .......... .......... .......... 89% 18.1M 4s
431700K .......... .......... .......... .......... .......... 89% 17.1M 4s
431750K .......... .......... .......... .......... .......... 89% 17.3M 4s
431800K .......... .......... .......... .......... .......... 89% 17.9M 4s
431850K .......... .......... .......... .......... .......... 89% 31.1M 4s
431900K .......... .......... .......... .......... .......... 89% 31.5M 4s
431950K .......... .......... .......... .......... .......... 89% 25.0M 4s
432000K .......... .......... .......... .......... .......... 89% 42.4M 4s
432050K .......... .......... .......... .......... .......... 89% 75.8M 4s
432100K .......... .......... .......... .......... .......... 89% 13.4M 4s
432150K .......... .......... .......... .......... .......... 89% 73.9M 4s
432200K .......... .......... .......... .......... .......... 89% 27.0M 4s
432250K .......... .......... .......... .......... .......... 89% 59.6M 4s
432300K .......... .......... .......... .......... .......... 89% 22.9M 4s
432350K .......... .......... .......... .......... .......... 89% 24.9M 4s
432400K .......... .......... .......... .......... .......... 89% 27.8M 4s
432450K .......... .......... .......... .......... .......... 89% 17.2M 4s
432500K .......... .......... .......... .......... .......... 89% 22.4M 4s
432550K .......... .......... .......... .......... .......... 90% 19.2M 4s
432600K .......... .......... .......... .......... .......... 90% 13.3M 4s
432650K .......... .......... .......... .......... .......... 90% 17.2M 4s
432700K .......... .......... .......... .......... .......... 90% 13.5M 4s
432750K .......... .......... .......... .......... .......... 90% 20.0M 4s
432800K .......... .......... .......... .......... .......... 90% 21.4M 4s
432850K .......... .......... .......... .......... .......... 90% 14.5M 4s
432900K .......... .......... .......... .......... .......... 90% 21.0M 4s
432950K .......... .......... .......... .......... .......... 90% 19.7M 4s
433000K .......... .......... .......... .......... .......... 90% 19.4M 4s
433050K .......... .......... .......... .......... .......... 90% 24.3M 4s
433100K .......... .......... .......... .......... .......... 90% 7.59M 4s
433150K .......... .......... .......... .......... .......... 90% 77.3M 4s
433200K .......... .......... .......... .......... .......... 90% 30.9M 4s
433250K .......... .......... .......... .......... .......... 90% 25.1M 4s
433300K .......... .......... .......... .......... .......... 90% 56.1M 4s
433350K .......... .......... .......... .......... .......... 90% 20.4M 4s
433400K .......... .......... .......... .......... .......... 90% 18.2M 4s
433450K .......... .......... .......... .......... .......... 90% 13.6M 4s
433500K .......... .......... .......... .......... .......... 90% 18.2M 4s
433550K .......... .......... .......... .......... .......... 90% 12.1M 4s
433600K .......... .......... .......... .......... .......... 90% 13.1M 4s
433650K .......... .......... .......... .......... .......... 90% 13.3M 4s
433700K .......... .......... .......... .......... .......... 90% 13.0M 4s
433750K .......... .......... .......... .......... .......... 90% 14.6M 4s
433800K .......... .......... .......... .......... .......... 90% 16.6M 4s
433850K .......... .......... .......... .......... .......... 90% 15.1M 4s
433900K .......... .......... .......... .......... .......... 90% 11.5M 4s
433950K .......... .......... .......... .......... .......... 90% 7.19M 4s
434000K .......... .......... .......... .......... .......... 90% 31.1M 4s
434050K .......... .......... .......... .......... .......... 90% 18.1M 4s
434100K .......... .......... .......... .......... .......... 90% 12.6M 4s
434150K .......... .......... .......... .......... .......... 90% 19.1M 4s
434200K .......... .......... .......... .......... .......... 90% 13.1M 4s
434250K .......... .......... .......... .......... .......... 90% 13.6M 4s
434300K .......... .......... .......... .......... .......... 90% 13.1M 4s
434350K .......... .......... .......... .......... .......... 90% 13.1M 4s
434400K .......... .......... .......... .......... .......... 90% 19.3M 4s
434450K .......... .......... .......... .......... .......... 90% 13.6M 4s
434500K .......... .......... .......... .......... .......... 90% 13.0M 4s
434550K .......... .......... .......... .......... .......... 90% 16.7M 4s
434600K .......... .......... .......... .......... .......... 90% 21.4M 4s
434650K .......... .......... .......... .......... .......... 90% 19.0M 4s
434700K .......... .......... .......... .......... .......... 90% 49.6M 4s
434750K .......... .......... .......... .......... .......... 90% 33.1M 4s
434800K .......... .......... .......... .......... .......... 90% 55.2M 4s
434850K .......... .......... .......... .......... .......... 90% 24.1M 4s
434900K .......... .......... .......... .......... .......... 90% 26.9M 4s
434950K .......... .......... .......... .......... .......... 90% 27.5M 4s
435000K .......... .......... .......... .......... .......... 90% 23.3M 4s
435050K .......... .......... .......... .......... .......... 90% 30.5M 4s
435100K .......... .......... .......... .......... .......... 90% 20.9M 4s
435150K .......... .......... .......... .......... .......... 90% 28.8M 4s
435200K .......... .......... .......... .......... .......... 90% 22.4M 4s
435250K .......... .......... .......... .......... .......... 90% 29.1M 4s
435300K .......... .......... .......... .......... .......... 90% 23.3M 4s
435350K .......... .......... .......... .......... .......... 90% 25.3M 4s
435400K .......... .......... .......... .......... .......... 90% 32.1M 4s
435450K .......... .......... .......... .......... .......... 90% 19.6M 4s
435500K .......... .......... .......... .......... .......... 90% 23.4M 4s
435550K .......... .......... .......... .......... .......... 90% 35.9M 4s
435600K .......... .......... .......... .......... .......... 90% 17.0M 4s
435650K .......... .......... .......... .......... .......... 90% 30.1M 4s
435700K .......... .......... .......... .......... .......... 90% 13.8M 4s
435750K .......... .......... .......... .......... .......... 90% 76.1M 4s
435800K .......... .......... .......... .......... .......... 90% 12.5M 4s
435850K .......... .......... .......... .......... .......... 90% 33.0M 4s
435900K .......... .......... .......... .......... .......... 90% 52.7M 4s
435950K .......... .......... .......... .......... .......... 90% 20.7M 4s
436000K .......... .......... .......... .......... .......... 90% 28.4M 4s
436050K .......... .......... .......... .......... .......... 90% 17.5M 4s
436100K .......... .......... .......... .......... .......... 90% 18.0M 4s
436150K .......... .......... .......... .......... .......... 90% 17.9M 4s
436200K .......... .......... .......... .......... .......... 90% 13.7M 4s
436250K .......... .......... .......... .......... .......... 90% 13.5M 4s
436300K .......... .......... .......... .......... .......... 90% 19.1M 4s
436350K .......... .......... .......... .......... .......... 90% 11.6M 4s
436400K .......... .......... .......... .......... .......... 90% 14.9M 4s
436450K .......... .......... .......... .......... .......... 90% 15.2M 4s
436500K .......... .......... .......... .......... .......... 90% 16.9M 4s
436550K .......... .......... .......... .......... .......... 90% 7.02M 4s
436600K .......... .......... .......... .......... .......... 90% 16.5M 4s
436650K .......... .......... .......... .......... .......... 90% 26.3M 4s
436700K .......... .......... .......... .......... .......... 90% 25.2M 4s
436750K .......... .......... .......... .......... .......... 90% 14.6M 4s
436800K .......... .......... .......... .......... .......... 90% 13.3M 4s
436850K .......... .......... .......... .......... .......... 90% 9.65M 4s
436900K .......... .......... .......... .......... .......... 90% 13.5M 4s
436950K .......... .......... .......... .......... .......... 90% 12.6M 4s
437000K .......... .......... .......... .......... .......... 90% 12.7M 4s
437050K .......... .......... .......... .......... .......... 90% 11.0M 4s
437100K .......... .......... .......... .......... .......... 90% 13.8M 4s
437150K .......... .......... .......... .......... .......... 90% 15.3M 4s
437200K .......... .......... .......... .......... .......... 90% 23.6M 4s
437250K .......... .......... .......... .......... .......... 90% 20.6M 4s
437300K .......... .......... .......... .......... .......... 90% 22.2M 4s
437350K .......... .......... .......... .......... .......... 91% 12.9M 4s
437400K .......... .......... .......... .......... .......... 91% 51.7M 4s
437450K .......... .......... .......... .......... .......... 91% 26.2M 4s
437500K .......... .......... .......... .......... .......... 91% 19.7M 4s
437550K .......... .......... .......... .......... .......... 91% 25.4M 4s
437600K .......... .......... .......... .......... .......... 91% 16.0M 4s
437650K .......... .......... .......... .......... .......... 91% 16.5M 4s
437700K .......... .......... .......... .......... .......... 91% 12.6M 3s
437750K .......... .......... .......... .......... .......... 91% 16.0M 3s
437800K .......... .......... .......... .......... .......... 91% 23.0M 3s
437850K .......... .......... .......... .......... .......... 91% 13.3M 3s
437900K .......... .......... .......... .......... .......... 91% 18.6M 3s
437950K .......... .......... .......... .......... .......... 91% 16.0M 3s
438000K .......... .......... .......... .......... .......... 91% 18.8M 3s
438050K .......... .......... .......... .......... .......... 91% 16.7M 3s
438100K .......... .......... .......... .......... .......... 91% 10.7M 3s
438150K .......... .......... .......... .......... .......... 91% 80.3M 3s
438200K .......... .......... .......... .......... .......... 91% 13.6M 3s
438250K .......... .......... .......... .......... .......... 91% 18.3M 3s
438300K .......... .......... .......... .......... .......... 91% 18.3M 3s
438350K .......... .......... .......... .......... .......... 91% 18.4M 3s
438400K .......... .......... .......... .......... .......... 91% 19.9M 3s
438450K .......... .......... .......... .......... .......... 91% 12.6M 3s
438500K .......... .......... .......... .......... .......... 91% 16.5M 3s
438550K .......... .......... .......... .......... .......... 91% 17.4M 3s
438600K .......... .......... .......... .......... .......... 91% 11.5M 3s
438650K .......... .......... .......... .......... .......... 91% 17.0M 3s
438700K .......... .......... .......... .......... .......... 91% 11.7M 3s
438750K .......... .......... .......... .......... .......... 91% 13.2M 3s
438800K .......... .......... .......... .......... .......... 91% 19.3M 3s
438850K .......... .......... .......... .......... .......... 91% 34.1M 3s
438900K .......... .......... .......... .......... .......... 91% 20.4M 3s
438950K .......... .......... .......... .......... .......... 91% 21.7M 3s
439000K .......... .......... .......... .......... .......... 91% 22.4M 3s
439050K .......... .......... .......... .......... .......... 91% 79.8M 3s
439100K .......... .......... .......... .......... .......... 91% 17.3M 3s
439150K .......... .......... .......... .......... .......... 91% 42.2M 3s
439200K .......... .......... .......... .......... .......... 91% 27.1M 3s
439250K .......... .......... .......... .......... .......... 91% 35.6M 3s
439300K .......... .......... .......... .......... .......... 91% 33.1M 3s
439350K .......... .......... .......... .......... .......... 91% 19.1M 3s
439400K .......... .......... .......... .......... .......... 91% 31.5M 3s
439450K .......... .......... .......... .......... .......... 91% 18.9M 3s
439500K .......... .......... .......... .......... .......... 91% 29.3M 3s
439550K .......... .......... .......... .......... .......... 91% 34.9M 3s
439600K .......... .......... .......... .......... .......... 91% 19.9M 3s
439650K .......... .......... .......... .......... .......... 91% 38.9M 3s
439700K .......... .......... .......... .......... .......... 91% 31.6M 3s
439750K .......... .......... .......... .......... .......... 91% 29.8M 3s
439800K .......... .......... .......... .......... .......... 91% 34.6M 3s
439850K .......... .......... .......... .......... .......... 91% 23.5M 3s
439900K .......... .......... .......... .......... .......... 91% 41.7M 3s
439950K .......... .......... .......... .......... .......... 91% 25.5M 3s
440000K .......... .......... .......... .......... .......... 91% 30.5M 3s
440050K .......... .......... .......... .......... .......... 91% 25.0M 3s
440100K .......... .......... .......... .......... .......... 91% 22.2M 3s
440150K .......... .......... .......... .......... .......... 91% 35.0M 3s
440200K .......... .......... .......... .......... .......... 91% 31.2M 3s
440250K .......... .......... .......... .......... .......... 91% 44.8M 3s
440300K .......... .......... .......... .......... .......... 91% 12.8M 3s
440350K .......... .......... .......... .......... .......... 91% 64.5M 3s
440400K .......... .......... .......... .......... .......... 91% 80.2M 3s
440450K .......... .......... .......... .......... .......... 91% 21.4M 3s
440500K .......... .......... .......... .......... .......... 91% 80.6M 3s
440550K .......... .......... .......... .......... .......... 91% 36.1M 3s
440600K .......... .......... .......... .......... .......... 91% 33.7M 3s
440650K .......... .......... .......... .......... .......... 91% 45.5M 3s
440700K .......... .......... .......... .......... .......... 91% 21.8M 3s
440750K .......... .......... .......... .......... .......... 91% 35.0M 3s
440800K .......... .......... .......... .......... .......... 91% 20.8M 3s
440850K .......... .......... .......... .......... .......... 91% 17.6M 3s
440900K .......... .......... .......... .......... .......... 91% 21.4M 3s
440950K .......... .......... .......... .......... .......... 91% 17.9M 3s
441000K .......... .......... .......... .......... .......... 91% 24.1M 3s
441050K .......... .......... .......... .......... .......... 91% 23.5M 3s
441100K .......... .......... .......... .......... .......... 91% 22.4M 3s
441150K .......... .......... .......... .......... .......... 91% 22.0M 3s
441200K .......... .......... .......... .......... .......... 91% 17.0M 3s
441250K .......... .......... .......... .......... .......... 91% 27.4M 3s
441300K .......... .......... .......... .......... .......... 91% 20.7M 3s
441350K .......... .......... .......... .......... .......... 91% 15.0M 3s
441400K .......... .......... .......... .......... .......... 91% 15.6M 3s
441450K .......... .......... .......... .......... .......... 91% 30.7M 3s
441500K .......... .......... .......... .......... .......... 91% 19.0M 3s
441550K .......... .......... .......... .......... .......... 91% 17.8M 3s
441600K .......... .......... .......... .......... .......... 91% 14.0M 3s
441650K .......... .......... .......... .......... .......... 91% 14.6M 3s
441700K .......... .......... .......... .......... .......... 91% 11.4M 3s
441750K .......... .......... .......... .......... .......... 91% 16.7M 3s
441800K .......... .......... .......... .......... .......... 91% 9.99M 3s
441850K .......... .......... .......... .......... .......... 91% 16.6M 3s
441900K .......... .......... .......... .......... .......... 91% 11.5M 3s
441950K .......... .......... .......... .......... .......... 91% 13.9M 3s
442000K .......... .......... .......... .......... .......... 91% 22.3M 3s
442050K .......... .......... .......... .......... .......... 91% 16.6M 3s
442100K .......... .......... .......... .......... .......... 91% 63.5M 3s
442150K .......... .......... .......... .......... .......... 92% 17.7M 3s
442200K .......... .......... .......... .......... .......... 92% 47.4M 3s
442250K .......... .......... .......... .......... .......... 92% 29.0M 3s
442300K .......... .......... .......... .......... .......... 92% 34.5M 3s
442350K .......... .......... .......... .......... .......... 92% 22.1M 3s
442400K .......... .......... .......... .......... .......... 92% 29.3M 3s
442450K .......... .......... .......... .......... .......... 92% 8.94M 3s
442500K .......... .......... .......... .......... .......... 92% 31.9M 3s
442550K .......... .......... .......... .......... .......... 92% 24.5M 3s
442600K .......... .......... .......... .......... .......... 92% 22.1M 3s
442650K .......... .......... .......... .......... .......... 92% 27.0M 3s
442700K .......... .......... .......... .......... .......... 92% 35.6M 3s
442750K .......... .......... .......... .......... .......... 92% 27.5M 3s
442800K .......... .......... .......... .......... .......... 92% 28.0M 3s
442850K .......... .......... .......... .......... .......... 92% 22.0M 3s
442900K .......... .......... .......... .......... .......... 92% 31.2M 3s
442950K .......... .......... .......... .......... .......... 92% 22.0M 3s
443000K .......... .......... .......... .......... .......... 92% 34.4M 3s
443050K .......... .......... .......... .......... .......... 92% 17.2M 3s
443100K .......... .......... .......... .......... .......... 92% 12.3M 3s
443150K .......... .......... .......... .......... .......... 92% 86.7M 3s
443200K .......... .......... .......... .......... .......... 92% 21.2M 3s
443250K .......... .......... .......... .......... .......... 92% 12.6M 3s
443300K .......... .......... .......... .......... .......... 92% 17.1M 3s
443350K .......... .......... .......... .......... .......... 92% 14.1M 3s
443400K .......... .......... .......... .......... .......... 92% 14.5M 3s
443450K .......... .......... .......... .......... .......... 92% 9.01M 3s
443500K .......... .......... .......... .......... .......... 92% 14.8M 3s
443550K .......... .......... .......... .......... .......... 92% 10.8M 3s
443600K .......... .......... .......... .......... .......... 92% 11.1M 3s
443650K .......... .......... .......... .......... .......... 92% 9.88M 3s
443700K .......... .......... .......... .......... .......... 92% 8.88M 3s
443750K .......... .......... .......... .......... .......... 92% 9.17M 3s
443800K .......... .......... .......... .......... .......... 92% 17.2M 3s
443850K .......... .......... .......... .......... .......... 92% 12.2M 3s
443900K .......... .......... .......... .......... .......... 92% 13.3M 3s
443950K .......... .......... .......... .......... .......... 92% 13.2M 3s
444000K .......... .......... .......... .......... .......... 92% 16.5M 3s
444050K .......... .......... .......... .......... .......... 92% 10.2M 3s
444100K .......... .......... .......... .......... .......... 92% 12.1M 3s
444150K .......... .......... .......... .......... .......... 92% 14.1M 3s
444200K .......... .......... .......... .......... .......... 92% 12.1M 3s
444250K .......... .......... .......... .......... .......... 92% 15.2M 3s
444300K .......... .......... .......... .......... .......... 92% 19.3M 3s
444350K .......... .......... .......... .......... .......... 92% 13.1M 3s
444400K .......... .......... .......... .......... .......... 92% 72.8M 3s
444450K .......... .......... .......... .......... .......... 92% 22.5M 3s
444500K .......... .......... .......... .......... .......... 92% 31.5M 3s
444550K .......... .......... .......... .......... .......... 92% 25.3M 3s
444600K .......... .......... .......... .......... .......... 92% 21.5M 3s
444650K .......... .......... .......... .......... .......... 92% 16.0M 3s
444700K .......... .......... .......... .......... .......... 92% 19.1M 3s
444750K .......... .......... .......... .......... .......... 92% 21.5M 3s
444800K .......... .......... .......... .......... .......... 92% 17.0M 3s
444850K .......... .......... .......... .......... .......... 92% 18.2M 3s
444900K .......... .......... .......... .......... .......... 92% 14.9M 3s
444950K .......... .......... .......... .......... .......... 92% 18.9M 3s
445000K .......... .......... .......... .......... .......... 92% 19.2M 3s
445050K .......... .......... .......... .......... .......... 92% 15.5M 3s
445100K .......... .......... .......... .......... .......... 92% 17.3M 3s
445150K .......... .......... .......... .......... .......... 92% 36.0M 3s
445200K .......... .......... .......... .......... .......... 92% 27.0M 3s
445250K .......... .......... .......... .......... .......... 92% 24.8M 3s
445300K .......... .......... .......... .......... .......... 92% 25.5M 3s
445350K .......... .......... .......... .......... .......... 92% 24.5M 3s
445400K .......... .......... .......... .......... .......... 92% 21.3M 3s
445450K .......... .......... .......... .......... .......... 92% 32.7M 3s
445500K .......... .......... .......... .......... .......... 92% 25.8M 3s
445550K .......... .......... .......... .......... .......... 92% 20.9M 3s
445600K .......... .......... .......... .......... .......... 92% 17.8M 3s
445650K .......... .......... .......... .......... .......... 92% 19.5M 3s
445700K .......... .......... .......... .......... .......... 92% 20.9M 3s
445750K .......... .......... .......... .......... .......... 92% 14.8M 3s
445800K .......... .......... .......... .......... .......... 92% 17.3M 3s
445850K .......... .......... .......... .......... .......... 92% 15.0M 3s
445900K .......... .......... .......... .......... .......... 92% 21.5M 3s
445950K .......... .......... .......... .......... .......... 92% 13.5M 3s
446000K .......... .......... .......... .......... .......... 92% 18.0M 3s
446050K .......... .......... .......... .......... .......... 92% 19.8M 3s
446100K .......... .......... .......... .......... .......... 92% 17.4M 3s
446150K .......... .......... .......... .......... .......... 92% 22.7M 3s
446200K .......... .......... .......... .......... .......... 92% 12.3M 3s
446250K .......... .......... .......... .......... .......... 92% 74.7M 3s
446300K .......... .......... .......... .......... .......... 92% 25.5M 3s
446350K .......... .......... .......... .......... .......... 92% 68.2M 3s
446400K .......... .......... .......... .......... .......... 92% 26.0M 3s
446450K .......... .......... .......... .......... .......... 92% 32.9M 3s
446500K .......... .......... .......... .......... .......... 92% 21.8M 3s
446550K .......... .......... .......... .......... .......... 92% 25.4M 3s
446600K .......... .......... .......... .......... .......... 92% 22.4M 3s
446650K .......... .......... .......... .......... .......... 92% 30.9M 3s
446700K .......... .......... .......... .......... .......... 92% 20.5M 3s
446750K .......... .......... .......... .......... .......... 92% 29.4M 3s
446800K .......... .......... .......... .......... .......... 92% 24.3M 3s
446850K .......... .......... .......... .......... .......... 92% 24.7M 3s
446900K .......... .......... .......... .......... .......... 92% 18.6M 3s
446950K .......... .......... .......... .......... .......... 93% 29.5M 3s
447000K .......... .......... .......... .......... .......... 93% 19.6M 3s
447050K .......... .......... .......... .......... .......... 93% 17.9M 3s
447100K .......... .......... .......... .......... .......... 93% 28.6M 3s
447150K .......... .......... .......... .......... .......... 93% 17.3M 3s
447200K .......... .......... .......... .......... .......... 93% 29.2M 3s
447250K .......... .......... .......... .......... .......... 93% 37.7M 3s
447300K .......... .......... .......... .......... .......... 93% 15.3M 3s
447350K .......... .......... .......... .......... .......... 93% 17.4M 3s
447400K .......... .......... .......... .......... .......... 93% 81.0M 3s
447450K .......... .......... .......... .......... .......... 93% 44.6M 3s
447500K .......... .......... .......... .......... .......... 93% 20.9M 3s
447550K .......... .......... .......... .......... .......... 93% 74.5M 3s
447600K .......... .......... .......... .......... .......... 93% 48.7M 3s
447650K .......... .......... .......... .......... .......... 93% 45.2M 3s
447700K .......... .......... .......... .......... .......... 93% 29.2M 3s
447750K .......... .......... .......... .......... .......... 93% 31.6M 3s
447800K .......... .......... .......... .......... .......... 93% 28.9M 3s
447850K .......... .......... .......... .......... .......... 93% 29.2M 3s
447900K .......... .......... .......... .......... .......... 93% 27.4M 3s
447950K .......... .......... .......... .......... .......... 93% 19.9M 3s
448000K .......... .......... .......... .......... .......... 93% 28.8M 3s
448050K .......... .......... .......... .......... .......... 93% 27.9M 3s
448100K .......... .......... .......... .......... .......... 93% 22.3M 3s
448150K .......... .......... .......... .......... .......... 93% 29.0M 3s
448200K .......... .......... .......... .......... .......... 93% 25.4M 3s
448250K .......... .......... .......... .......... .......... 93% 31.6M 3s
448300K .......... .......... .......... .......... .......... 93% 21.3M 3s
448350K .......... .......... .......... .......... .......... 93% 25.0M 3s
448400K .......... .......... .......... .......... .......... 93% 17.4M 3s
448450K .......... .......... .......... .......... .......... 93% 27.0M 3s
448500K .......... .......... .......... .......... .......... 93% 23.0M 3s
448550K .......... .......... .......... .......... .......... 93% 34.0M 3s
448600K .......... .......... .......... .......... .......... 93% 27.9M 3s
448650K .......... .......... .......... .......... .......... 93% 27.9M 3s
448700K .......... .......... .......... .......... .......... 93% 23.2M 3s
448750K .......... .......... .......... .......... .......... 93% 18.4M 3s
448800K .......... .......... .......... .......... .......... 93% 36.7M 3s
448850K .......... .......... .......... .......... .......... 93% 36.5M 3s
448900K .......... .......... .......... .......... .......... 93% 71.7M 3s
448950K .......... .......... .......... .......... .......... 93% 35.0M 3s
449000K .......... .......... .......... .......... .......... 93% 50.1M 3s
449050K .......... .......... .......... .......... .......... 93% 33.5M 3s
449100K .......... .......... .......... .......... .......... 93% 23.4M 3s
449150K .......... .......... .......... .......... .......... 93% 31.4M 3s
449200K .......... .......... .......... .......... .......... 93% 24.0M 3s
449250K .......... .......... .......... .......... .......... 93% 31.3M 3s
449300K .......... .......... .......... .......... .......... 93% 28.9M 3s
449350K .......... .......... .......... .......... .......... 93% 25.6M 3s
449400K .......... .......... .......... .......... .......... 93% 32.8M 3s
449450K .......... .......... .......... .......... .......... 93% 23.6M 3s
449500K .......... .......... .......... .......... .......... 93% 29.9M 3s
449550K .......... .......... .......... .......... .......... 93% 31.5M 3s
449600K .......... .......... .......... .......... .......... 93% 22.2M 2s
449650K .......... .......... .......... .......... .......... 93% 31.3M 2s
449700K .......... .......... .......... .......... .......... 93% 28.7M 2s
449750K .......... .......... .......... .......... .......... 93% 25.3M 2s
449800K .......... .......... .......... .......... .......... 93% 37.2M 2s
449850K .......... .......... .......... .......... .......... 93% 17.2M 2s
449900K .......... .......... .......... .......... .......... 93% 31.6M 2s
449950K .......... .......... .......... .......... .......... 93% 26.7M 2s
450000K .......... .......... .......... .......... .......... 93% 47.7M 2s
450050K .......... .......... .......... .......... .......... 93% 38.1M 2s
450100K .......... .......... .......... .......... .......... 93% 14.4M 2s
450150K .......... .......... .......... .......... .......... 93% 43.6M 2s
450200K .......... .......... .......... .......... .......... 93% 29.1M 2s
450250K .......... .......... .......... .......... .......... 93% 31.1M 2s
450300K .......... .......... .......... .......... .......... 93% 51.4M 2s
450350K .......... .......... .......... .......... .......... 93% 23.4M 2s
450400K .......... .......... .......... .......... .......... 93% 23.9M 2s
450450K .......... .......... .......... .......... .......... 93% 24.1M 2s
450500K .......... .......... .......... .......... .......... 93% 19.6M 2s
450550K .......... .......... .......... .......... .......... 93% 22.7M 2s
450600K .......... .......... .......... .......... .......... 93% 13.5M 2s
450650K .......... .......... .......... .......... .......... 93% 21.5M 2s
450700K .......... .......... .......... .......... .......... 93% 14.3M 2s
450750K .......... .......... .......... .......... .......... 93% 20.0M 2s
450800K .......... .......... .......... .......... .......... 93% 21.6M 2s
450850K .......... .......... .......... .......... .......... 93% 15.5M 2s
450900K .......... .......... .......... .......... .......... 93% 21.2M 2s
450950K .......... .......... .......... .......... .......... 93% 23.1M 2s
451000K .......... .......... .......... .......... .......... 93% 13.9M 2s
451050K .......... .......... .......... .......... .......... 93% 27.8M 2s
451100K .......... .......... .......... .......... .......... 93% 20.6M 2s
451150K .......... .......... .......... .......... .......... 93% 17.0M 2s
451200K .......... .......... .......... .......... .......... 93% 13.5M 2s
451250K .......... .......... .......... .......... .......... 93% 22.3M 2s
451300K .......... .......... .......... .......... .......... 93% 47.1M 2s
451350K .......... .......... .......... .......... .......... 93% 17.9M 2s
451400K .......... .......... .......... .......... .......... 93% 81.9M 2s
451450K .......... .......... .......... .......... .......... 93% 21.9M 2s
451500K .......... .......... .......... .......... .......... 93% 22.5M 2s
451550K .......... .......... .......... .......... .......... 93% 17.8M 2s
451600K .......... .......... .......... .......... .......... 93% 18.9M 2s
451650K .......... .......... .......... .......... .......... 93% 26.9M 2s
451700K .......... .......... .......... .......... .......... 93% 17.1M 2s
451750K .......... .......... .......... .......... .......... 94% 19.1M 2s
451800K .......... .......... .......... .......... .......... 94% 17.2M 2s
451850K .......... .......... .......... .......... .......... 94% 19.7M 2s
451900K .......... .......... .......... .......... .......... 94% 27.6M 2s
451950K .......... .......... .......... .......... .......... 94% 20.9M 2s
452000K .......... .......... .......... .......... .......... 94% 20.0M 2s
452050K .......... .......... .......... .......... .......... 94% 20.9M 2s
452100K .......... .......... .......... .......... .......... 94% 16.8M 2s
452150K .......... .......... .......... .......... .......... 94% 23.6M 2s
452200K .......... .......... .......... .......... .......... 94% 14.4M 2s
452250K .......... .......... .......... .......... .......... 94% 22.1M 2s
452300K .......... .......... .......... .......... .......... 94% 16.7M 2s
452350K .......... .......... .......... .......... .......... 94% 14.7M 2s
452400K .......... .......... .......... .......... .......... 94% 38.6M 2s
452450K .......... .......... .......... .......... .......... 94% 15.6M 2s
452500K .......... .......... .......... .......... .......... 94% 16.4M 2s
452550K .......... .......... .......... .......... .......... 94% 25.1M 2s
452600K .......... .......... .......... .......... .......... 94% 13.0M 2s
452650K .......... .......... .......... .......... .......... 94% 19.1M 2s
452700K .......... .......... .......... .......... .......... 94% 13.0M 2s
452750K .......... .......... .......... .......... .......... 94% 18.2M 2s
452800K .......... .......... .......... .......... .......... 94% 14.0M 2s
452850K .......... .......... .......... .......... .......... 94% 16.0M 2s
452900K .......... .......... .......... .......... .......... 94% 17.2M 2s
452950K .......... .......... .......... .......... .......... 94% 12.8M 2s
453000K .......... .......... .......... .......... .......... 94% 12.9M 2s
453050K .......... .......... .......... .......... .......... 94% 12.9M 2s
453100K .......... .......... .......... .......... .......... 94% 16.9M 2s
453150K .......... .......... .......... .......... .......... 94%  112M 2s
453200K .......... .......... .......... .......... .......... 94% 24.1M 2s
453250K .......... .......... .......... .......... .......... 94% 20.1M 2s
453300K .......... .......... .......... .......... .......... 94% 35.1M 2s
453350K .......... .......... .......... .......... .......... 94% 20.1M 2s
453400K .......... .......... .......... .......... .......... 94% 22.1M 2s
453450K .......... .......... .......... .......... .......... 94% 18.7M 2s
453500K .......... .......... .......... .......... .......... 94% 20.2M 2s
453550K .......... .......... .......... .......... .......... 94% 18.0M 2s
453600K .......... .......... .......... .......... .......... 94% 19.8M 2s
453650K .......... .......... .......... .......... .......... 94% 19.8M 2s
453700K .......... .......... .......... .......... .......... 94% 17.1M 2s
453750K .......... .......... .......... .......... .......... 94% 25.5M 2s
453800K .......... .......... .......... .......... .......... 94% 20.0M 2s
453850K .......... .......... .......... .......... .......... 94% 20.3M 2s
453900K .......... .......... .......... .......... .......... 94% 17.1M 2s
453950K .......... .......... .......... .......... .......... 94% 13.6M 2s
454000K .......... .......... .......... .......... .......... 94% 23.5M 2s
454050K .......... .......... .......... .......... .......... 94% 14.2M 2s
454100K .......... .......... .......... .......... .......... 94% 27.7M 2s
454150K .......... .......... .......... .......... .......... 94% 48.3M 2s
454200K .......... .......... .......... .......... .......... 94% 13.1M 2s
454250K .......... .......... .......... .......... .......... 94% 27.0M 2s
454300K .......... .......... .......... .......... .......... 94% 23.3M 2s
454350K .......... .......... .......... .......... .......... 94% 15.0M 2s
454400K .......... .......... .......... .......... .......... 94% 17.1M 2s
454450K .......... .......... .......... .......... .......... 94% 16.0M 2s
454500K .......... .......... .......... .......... .......... 94% 11.4M 2s
454550K .......... .......... .......... .......... .......... 94% 19.3M 2s
454600K .......... .......... .......... .......... .......... 94% 12.9M 2s
454650K .......... .......... .......... .......... .......... 94% 21.2M 2s
454700K .......... .......... .......... .......... .......... 94% 11.6M 2s
454750K .......... .......... .......... .......... .......... 94% 16.4M 2s
454800K .......... .......... .......... .......... .......... 94% 16.6M 2s
454850K .......... .......... .......... .......... .......... 94% 21.3M 2s
454900K .......... .......... .......... .......... .......... 94% 21.7M 2s
454950K .......... .......... .......... .......... .......... 94% 26.1M 2s
455000K .......... .......... .......... .......... .......... 94% 23.1M 2s
455050K .......... .......... .......... .......... .......... 94% 57.0M 2s
455100K .......... .......... .......... .......... .......... 94% 27.5M 2s
455150K .......... .......... .......... .......... .......... 94% 35.4M 2s
455200K .......... .......... .......... .......... .......... 94% 26.4M 2s
455250K .......... .......... .......... .......... .......... 94% 23.7M 2s
455300K .......... .......... .......... .......... .......... 94% 26.8M 2s
455350K .......... .......... .......... .......... .......... 94% 18.5M 2s
455400K .......... .......... .......... .......... .......... 94% 32.1M 2s
455450K .......... .......... .......... .......... .......... 94% 21.2M 2s
455500K .......... .......... .......... .......... .......... 94% 21.8M 2s
455550K .......... .......... .......... .......... .......... 94% 29.5M 2s
455600K .......... .......... .......... .......... .......... 94% 16.6M 2s
455650K .......... .......... .......... .......... .......... 94% 17.7M 2s
455700K .......... .......... .......... .......... .......... 94% 17.3M 2s
455750K .......... .......... .......... .......... .......... 94% 32.3M 2s
455800K .......... .......... .......... .......... .......... 94% 16.8M 2s
455850K .......... .......... .......... .......... .......... 94% 28.1M 2s
455900K .......... .......... .......... .......... .......... 94% 17.7M 2s
455950K .......... .......... .......... .......... .......... 94% 21.4M 2s
456000K .......... .......... .......... .......... .......... 94% 26.2M 2s
456050K .......... .......... .......... .......... .......... 94% 17.6M 2s
456100K .......... .......... .......... .......... .......... 94% 32.2M 2s
456150K .......... .......... .......... .......... .......... 94% 76.2M 2s
456200K .......... .......... .......... .......... .......... 94% 31.1M 2s
456250K .......... .......... .......... .......... .......... 94% 44.7M 2s
456300K .......... .......... .......... .......... .......... 94% 29.5M 2s
456350K .......... .......... .......... .......... .......... 94% 62.0M 2s
456400K .......... .......... .......... .......... .......... 94% 25.2M 2s
456450K .......... .......... .......... .......... .......... 94% 23.9M 2s
456500K .......... .......... .......... .......... .......... 94% 17.9M 2s
456550K .......... .......... .......... .......... .......... 95% 20.0M 2s
456600K .......... .......... .......... .......... .......... 95% 22.1M 2s
456650K .......... .......... .......... .......... .......... 95% 22.2M 2s
456700K .......... .......... .......... .......... .......... 95% 19.5M 2s
456750K .......... .......... .......... .......... .......... 95% 19.8M 2s
456800K .......... .......... .......... .......... .......... 95% 18.0M 2s
456850K .......... .......... .......... .......... .......... 95% 18.3M 2s
456900K .......... .......... .......... .......... .......... 95% 18.5M 2s
456950K .......... .......... .......... .......... .......... 95% 15.8M 2s
457000K .......... .......... .......... .......... .......... 95% 22.0M 2s
457050K .......... .......... .......... .......... .......... 95% 32.9M 2s
457100K .......... .......... .......... .......... .......... 95% 21.4M 2s
457150K .......... .......... .......... .......... .......... 95% 10.8M 2s
457200K .......... .......... .......... .......... .......... 95% 56.8M 2s
457250K .......... .......... .......... .......... .......... 95% 30.6M 2s
457300K .......... .......... .......... .......... .......... 95% 22.4M 2s
457350K .......... .......... .......... .......... .......... 95% 37.7M 2s
457400K .......... .......... .......... .......... .......... 95% 26.9M 2s
457450K .......... .......... .......... .......... .......... 95% 25.1M 2s
457500K .......... .......... .......... .......... .......... 95% 18.2M 2s
457550K .......... .......... .......... .......... .......... 95% 17.9M 2s
457600K .......... .......... .......... .......... .......... 95% 26.3M 2s
457650K .......... .......... .......... .......... .......... 95% 15.9M 2s
457700K .......... .......... .......... .......... .......... 95% 21.5M 2s
457750K .......... .......... .......... .......... .......... 95% 25.1M 2s
457800K .......... .......... .......... .......... .......... 95% 29.5M 2s
457850K .......... .......... .......... .......... .......... 95% 15.9M 2s
457900K .......... .......... .......... .......... .......... 95% 30.2M 2s
457950K .......... .......... .......... .......... .......... 95% 18.8M 2s
458000K .......... .......... .......... .......... .......... 95% 19.7M 2s
458050K .......... .......... .......... .......... .......... 95% 17.7M 2s
458100K .......... .......... .......... .......... .......... 95% 23.0M 2s
458150K .......... .......... .......... .......... .......... 95% 13.9M 2s
458200K .......... .......... .......... .......... .......... 95% 19.2M 2s
458250K .......... .......... .......... .......... .......... 95% 17.8M 2s
458300K .......... .......... .......... .......... .......... 95% 17.3M 2s
458350K .......... .......... .......... .......... .......... 95% 58.3M 2s
458400K .......... .......... .......... .......... .......... 95% 22.7M 2s
458450K .......... .......... .......... .......... .......... 95% 18.6M 2s
458500K .......... .......... .......... .......... .......... 95% 22.3M 2s
458550K .......... .......... .......... .......... .......... 95% 25.6M 2s
458600K .......... .......... .......... .......... .......... 95% 14.1M 2s
458650K .......... .......... .......... .......... .......... 95% 14.5M 2s
458700K .......... .......... .......... .......... .......... 95% 16.8M 2s
458750K .......... .......... .......... .......... .......... 95% 15.8M 2s
458800K .......... .......... .......... .......... .......... 95% 12.2M 2s
458850K .......... .......... .......... .......... .......... 95% 17.4M 2s
458900K .......... .......... .......... .......... .......... 95% 13.4M 2s
458950K .......... .......... .......... .......... .......... 95% 18.1M 2s
459000K .......... .......... .......... .......... .......... 95% 15.5M 2s
459050K .......... .......... .......... .......... .......... 95% 23.8M 2s
459100K .......... .......... .......... .......... .......... 95% 10.5M 2s
459150K .......... .......... .......... .......... .......... 95% 16.3M 2s
459200K .......... .......... .......... .......... .......... 95% 26.9M 2s
459250K .......... .......... .......... .......... .......... 95% 20.8M 2s
459300K .......... .......... .......... .......... .......... 95% 13.5M 2s
459350K .......... .......... .......... .......... .......... 95% 15.1M 2s
459400K .......... .......... .......... .......... .......... 95% 14.0M 2s
459450K .......... .......... .......... .......... .......... 95% 14.0M 2s
459500K .......... .......... .......... .......... .......... 95% 15.7M 2s
459550K .......... .......... .......... .......... .......... 95% 13.9M 2s
459600K .......... .......... .......... .......... .......... 95% 14.0M 2s
459650K .......... .......... .......... .......... .......... 95% 13.6M 2s
459700K .......... .......... .......... .......... .......... 95% 12.7M 2s
459750K .......... .......... .......... .......... .......... 95% 14.2M 2s
459800K .......... .......... .......... .......... .......... 95% 16.8M 2s
459850K .......... .......... .......... .......... .......... 95% 12.3M 2s
459900K .......... .......... .......... .......... .......... 95% 25.2M 2s
459950K .......... .......... .......... .......... .......... 95% 42.5M 2s
460000K .......... .......... .......... .......... .......... 95% 22.5M 2s
460050K .......... .......... .......... .......... .......... 95% 24.3M 2s
460100K .......... .......... .......... .......... .......... 95% 19.0M 2s
460150K .......... .......... .......... .......... .......... 95% 20.3M 2s
460200K .......... .......... .......... .......... .......... 95% 12.6M 2s
460250K .......... .......... .......... .......... .......... 95% 20.0M 2s
460300K .......... .......... .......... .......... .......... 95% 19.1M 2s
460350K .......... .......... .......... .......... .......... 95% 15.7M 2s
460400K .......... .......... .......... .......... .......... 95% 13.7M 2s
460450K .......... .......... .......... .......... .......... 95% 14.3M 2s
460500K .......... .......... .......... .......... .......... 95% 19.2M 2s
460550K .......... .......... .......... .......... .......... 95% 13.9M 2s
460600K .......... .......... .......... .......... .......... 95% 17.7M 2s
460650K .......... .......... .......... .......... .......... 95% 23.8M 2s
460700K .......... .......... .......... .......... .......... 95% 22.4M 2s
460750K .......... .......... .......... .......... .......... 95% 17.5M 2s
460800K .......... .......... .......... .......... .......... 95% 63.2M 2s
460850K .......... .......... .......... .......... .......... 95% 27.8M 2s
460900K .......... .......... .......... .......... .......... 95% 23.6M 2s
460950K .......... .......... .......... .......... .......... 95% 23.9M 2s
461000K .......... .......... .......... .......... .......... 95% 20.8M 2s
461050K .......... .......... .......... .......... .......... 95% 23.1M 2s
461100K .......... .......... .......... .......... .......... 95% 17.5M 2s
461150K .......... .......... .......... .......... .......... 95% 19.7M 2s
461200K .......... .......... .......... .......... .......... 95% 20.1M 2s
461250K .......... .......... .......... .......... .......... 95% 19.8M 2s
461300K .......... .......... .......... .......... .......... 95% 19.9M 2s
461350K .......... .......... .......... .......... .......... 96% 14.1M 2s
461400K .......... .......... .......... .......... .......... 96% 20.2M 2s
461450K .......... .......... .......... .......... .......... 96% 18.8M 2s
461500K .......... .......... .......... .......... .......... 96% 18.2M 2s
461550K .......... .......... .......... .......... .......... 96% 30.4M 2s
461600K .......... .......... .......... .......... .......... 96% 20.3M 2s
461650K .......... .......... .......... .......... .......... 96% 12.0M 2s
461700K .......... .......... .......... .......... .......... 96% 25.7M 2s
461750K .......... .......... .......... .......... .......... 96% 32.4M 2s
461800K .......... .......... .......... .......... .......... 96% 17.5M 1s
461850K .......... .......... .......... .......... .......... 96% 68.0M 1s
461900K .......... .......... .......... .......... .......... 96% 16.4M 1s
461950K .......... .......... .......... .......... .......... 96% 25.6M 1s
462000K .......... .......... .......... .......... .......... 96% 25.1M 1s
462050K .......... .......... .......... .......... .......... 96% 20.6M 1s
462100K .......... .......... .......... .......... .......... 96% 16.5M 1s
462150K .......... .......... .......... .......... .......... 96% 17.7M 1s
462200K .......... .......... .......... .......... .......... 96% 17.0M 1s
462250K .......... .......... .......... .......... .......... 96% 13.5M 1s
462300K .......... .......... .......... .......... .......... 96% 15.2M 1s
462350K .......... .......... .......... .......... .......... 96% 16.8M 1s
462400K .......... .......... .......... .......... .......... 96% 19.2M 1s
462450K .......... .......... .......... .......... .......... 96% 13.6M 1s
462500K .......... .......... .......... .......... .......... 96% 19.9M 1s
462550K .......... .......... .......... .......... .......... 96% 14.7M 1s
462600K .......... .......... .......... .......... .......... 96% 13.4M 1s
462650K .......... .......... .......... .......... .......... 96% 17.6M 1s
462700K .......... .......... .......... .......... .......... 96% 19.6M 1s
462750K .......... .......... .......... .......... .......... 96% 25.4M 1s
462800K .......... .......... .......... .......... .......... 96% 20.9M 1s
462850K .......... .......... .......... .......... .......... 96% 18.0M 1s
462900K .......... .......... .......... .......... .......... 96% 18.0M 1s
462950K .......... .......... .......... .......... .......... 96% 13.0M 1s
463000K .......... .......... .......... .......... .......... 96% 16.9M 1s
463050K .......... .......... .......... .......... .......... 96% 16.9M 1s
463100K .......... .......... .......... .......... .......... 96% 13.0M 1s
463150K .......... .......... .......... .......... .......... 96% 19.0M 1s
463200K .......... .......... .......... .......... .......... 96% 13.9M 1s
463250K .......... .......... .......... .......... .......... 96% 22.3M 1s
463300K .......... .......... .......... .......... .......... 96% 26.1M 1s
463350K .......... .......... .......... .......... .......... 96% 12.2M 1s
463400K .......... .......... .......... .......... .......... 96% 15.4M 1s
463450K .......... .......... .......... .......... .......... 96% 15.6M 1s
463500K .......... .......... .......... .......... .......... 96% 18.6M 1s
463550K .......... .......... .......... .......... .......... 96% 30.4M 1s
463600K .......... .......... .......... .......... .......... 96% 22.4M 1s
463650K .......... .......... .......... .......... .......... 96% 21.2M 1s
463700K .......... .......... .......... .......... .......... 96% 20.3M 1s
463750K .......... .......... .......... .......... .......... 96% 23.6M 1s
463800K .......... .......... .......... .......... .......... 96% 25.1M 1s
463850K .......... .......... .......... .......... .......... 96% 22.8M 1s
463900K .......... .......... .......... .......... .......... 96% 18.2M 1s
463950K .......... .......... .......... .......... .......... 96% 18.0M 1s
464000K .......... .......... .......... .......... .......... 96% 16.6M 1s
464050K .......... .......... .......... .......... .......... 96% 32.4M 1s
464100K .......... .......... .......... .......... .......... 96% 13.8M 1s
464150K .......... .......... .......... .......... .......... 96% 32.9M 1s
464200K .......... .......... .......... .......... .......... 96% 13.5M 1s
464250K .......... .......... .......... .......... .......... 96% 29.8M 1s
464300K .......... .......... .......... .......... .......... 96% 24.5M 1s
464350K .......... .......... .......... .......... .......... 96% 27.4M 1s
464400K .......... .......... .......... .......... .......... 96% 17.8M 1s
464450K .......... .......... .......... .......... .......... 96% 61.8M 1s
464500K .......... .......... .......... .......... .......... 96% 16.3M 1s
464550K .......... .......... .......... .......... .......... 96% 76.5M 1s
464600K .......... .......... .......... .......... .......... 96% 50.6M 1s
464650K .......... .......... .......... .......... .......... 96% 28.1M 1s
464700K .......... .......... .......... .......... .......... 96% 24.1M 1s
464750K .......... .......... .......... .......... .......... 96% 27.0M 1s
464800K .......... .......... .......... .......... .......... 96% 28.4M 1s
464850K .......... .......... .......... .......... .......... 96% 18.8M 1s
464900K .......... .......... .......... .......... .......... 96% 17.7M 1s
464950K .......... .......... .......... .......... .......... 96% 28.5M 1s
465000K .......... .......... .......... .......... .......... 96% 19.8M 1s
465050K .......... .......... .......... .......... .......... 96% 34.0M 1s
465100K .......... .......... .......... .......... .......... 96% 18.8M 1s
465150K .......... .......... .......... .......... .......... 96% 20.8M 1s
465200K .......... .......... .......... .......... .......... 96% 32.4M 1s
465250K .......... .......... .......... .......... .......... 96% 22.2M 1s
465300K .......... .......... .......... .......... .......... 96% 29.9M 1s
465350K .......... .......... .......... .......... .......... 96% 18.7M 1s
465400K .......... .......... .......... .......... .......... 96% 18.9M 1s
465450K .......... .......... .......... .......... .......... 96% 23.1M 1s
465500K .......... .......... .......... .......... .......... 96% 21.9M 1s
465550K .......... .......... .......... .......... .......... 96% 19.8M 1s
465600K .......... .......... .......... .......... .......... 96% 12.9M 1s
465650K .......... .......... .......... .......... .......... 96% 73.0M 1s
465700K .......... .......... .......... .......... .......... 96% 26.7M 1s
465750K .......... .......... .......... .......... .......... 96% 42.3M 1s
465800K .......... .......... .......... .......... .......... 96% 41.7M 1s
465850K .......... .......... .......... .......... .......... 96% 20.8M 1s
465900K .......... .......... .......... .......... .......... 96% 30.9M 1s
465950K .......... .......... .......... .......... .......... 96% 18.0M 1s
466000K .......... .......... .......... .......... .......... 96% 31.5M 1s
466050K .......... .......... .......... .......... .......... 96% 21.0M 1s
466100K .......... .......... .......... .......... .......... 96% 20.9M 1s
466150K .......... .......... .......... .......... .......... 97% 22.4M 1s
466200K .......... .......... .......... .......... .......... 97% 18.7M 1s
466250K .......... .......... .......... .......... .......... 97% 29.3M 1s
466300K .......... .......... .......... .......... .......... 97% 28.2M 1s
466350K .......... .......... .......... .......... .......... 97% 16.8M 1s
466400K .......... .......... .......... .......... .......... 97% 31.4M 1s
466450K .......... .......... .......... .......... .......... 97% 17.4M 1s
466500K .......... .......... .......... .......... .......... 97% 23.9M 1s
466550K .......... .......... .......... .......... .......... 97% 20.9M 1s
466600K .......... .......... .......... .......... .......... 97% 8.75M 1s
466650K .......... .......... .......... .......... .......... 97% 67.1M 1s
466700K .......... .......... .......... .......... .......... 97% 14.4M 1s
466750K .......... .......... .......... .......... .......... 97% 17.0M 1s
466800K .......... .......... .......... .......... .......... 97% 17.2M 1s
466850K .......... .......... .......... .......... .......... 97% 11.7M 1s
466900K .......... .......... .......... .......... .......... 97% 13.8M 1s
466950K .......... .......... .......... .......... .......... 97% 12.3M 1s
467000K .......... .......... .......... .......... .......... 97% 10.0M 1s
467050K .......... .......... .......... .......... .......... 97% 11.6M 1s
467100K .......... .......... .......... .......... .......... 97% 12.0M 1s
467150K .......... .......... .......... .......... .......... 97% 11.9M 1s
467200K .......... .......... .......... .......... .......... 97% 12.4M 1s
467250K .......... .......... .......... .......... .......... 97% 20.6M 1s
467300K .......... .......... .......... .......... .......... 97% 83.5M 1s
467350K .......... .......... .......... .......... .......... 97% 17.2M 1s
467400K .......... .......... .......... .......... .......... 97% 27.7M 1s
467450K .......... .......... .......... .......... .......... 97% 14.1M 1s
467500K .......... .......... .......... .......... .......... 97% 18.6M 1s
467550K .......... .......... .......... .......... .......... 97% 11.7M 1s
467600K .......... .......... .......... .......... .......... 97% 13.0M 1s
467650K .......... .......... .......... .......... .......... 97% 15.0M 1s
467700K .......... .......... .......... .......... .......... 97% 12.9M 1s
467750K .......... .......... .......... .......... .......... 97% 13.3M 1s
467800K .......... .......... .......... .......... .......... 97% 16.0M 1s
467850K .......... .......... .......... .......... .......... 97% 11.8M 1s
467900K .......... .......... .......... .......... .......... 97% 24.4M 1s
467950K .......... .......... .......... .......... .......... 97% 10.4M 1s
468000K .......... .......... .......... .......... .......... 97% 12.2M 1s
468050K .......... .......... .......... .......... .......... 97% 14.0M 1s
468100K .......... .......... .......... .......... .......... 97% 12.3M 1s
468150K .......... .......... .......... .......... .......... 97% 12.7M 1s
468200K .......... .......... .......... .......... .......... 97% 8.64M 1s
468250K .......... .......... .......... .......... .......... 97% 11.9M 1s
468300K .......... .......... .......... .......... .......... 97% 11.9M 1s
468350K .......... .......... .......... .......... .......... 97% 8.80M 1s
468400K .......... .......... .......... .......... .......... 97% 12.7M 1s
468450K .......... .......... .......... .......... .......... 97% 13.6M 1s
468500K .......... .......... .......... .......... .......... 97% 22.8M 1s
468550K .......... .......... .......... .......... .......... 97% 12.9M 1s
468600K .......... .......... .......... .......... .......... 97% 17.5M 1s
468650K .......... .......... .......... .......... .......... 97% 26.6M 1s
468700K .......... .......... .......... .......... .......... 97% 17.3M 1s
468750K .......... .......... .......... .......... .......... 97% 31.7M 1s
468800K .......... .......... .......... .......... .......... 97% 36.0M 1s
468850K .......... .......... .......... .......... .......... 97% 37.2M 1s
468900K .......... .......... .......... .......... .......... 97% 42.6M 1s
468950K .......... .......... .......... .......... .......... 97% 27.1M 1s
469000K .......... .......... .......... .......... .......... 97% 38.9M 1s
469050K .......... .......... .......... .......... .......... 97% 28.7M 1s
469100K .......... .......... .......... .......... .......... 97% 31.5M 1s
469150K .......... .......... .......... .......... .......... 97% 33.9M 1s
469200K .......... .......... .......... .......... .......... 97% 32.9M 1s
469250K .......... .......... .......... .......... .......... 97% 29.9M 1s
469300K .......... .......... .......... .......... .......... 97% 23.4M 1s
469350K .......... .......... .......... .......... .......... 97% 27.9M 1s
469400K .......... .......... .......... .......... .......... 97% 27.1M 1s
469450K .......... .......... .......... .......... .......... 97% 35.5M 1s
469500K .......... .......... .......... .......... .......... 97%  105M 1s
469550K .......... .......... .......... .......... .......... 97% 28.2M 1s
469600K .......... .......... .......... .......... .......... 97% 31.3M 1s
469650K .......... .......... .......... .......... .......... 97% 74.3M 1s
469700K .......... .......... .......... .......... .......... 97% 43.0M 1s
469750K .......... .......... .......... .......... .......... 97% 70.1M 1s
469800K .......... .......... .......... .......... .......... 97% 51.5M 1s
469850K .......... .......... .......... .......... .......... 97% 33.5M 1s
469900K .......... .......... .......... .......... .......... 97% 92.0M 1s
469950K .......... .......... .......... .......... .......... 97% 48.6M 1s
470000K .......... .......... .......... .......... .......... 97% 54.0M 1s
470050K .......... .......... .......... .......... .......... 97% 51.9M 1s
470100K .......... .......... .......... .......... .......... 97% 26.8M 1s
470150K .......... .......... .......... .......... .......... 97%  111M 1s
470200K .......... .......... .......... .......... .......... 97% 30.0M 1s
470250K .......... .......... .......... .......... .......... 97% 82.2M 1s
470300K .......... .......... .......... .......... .......... 97% 72.8M 1s
470350K .......... .......... .......... .......... .......... 97% 20.2M 1s
470400K .......... .......... .......... .......... .......... 97%  113M 1s
470450K .......... .......... .......... .......... .......... 97% 46.8M 1s
470500K .......... .......... .......... .......... .......... 97% 72.9M 1s
470550K .......... .......... .......... .......... .......... 97% 46.5M 1s
470600K .......... .......... .......... .......... .......... 97% 35.8M 1s
470650K .......... .......... .......... .......... .......... 97% 44.1M 1s
470700K .......... .......... .......... .......... .......... 97% 33.8M 1s
470750K .......... .......... .......... .......... .......... 97% 36.2M 1s
470800K .......... .......... .......... .......... .......... 97% 45.8M 1s
470850K .......... .......... .......... .......... .......... 97% 31.1M 1s
470900K .......... .......... .......... .......... .......... 97% 31.1M 1s
470950K .......... .......... .......... .......... .......... 97% 19.0M 1s
471000K .......... .......... .......... .......... .......... 98% 36.4M 1s
471050K .......... .......... .......... .......... .......... 98% 46.0M 1s
471100K .......... .......... .......... .......... .......... 98% 21.3M 1s
471150K .......... .......... .......... .......... .......... 98% 37.8M 1s
471200K .......... .......... .......... .......... .......... 98% 28.8M 1s
471250K .......... .......... .......... .......... .......... 98% 36.0M 1s
471300K .......... .......... .......... .......... .......... 98% 30.4M 1s
471350K .......... .......... .......... .......... .......... 98% 31.7M 1s
471400K .......... .......... .......... .......... .......... 98% 42.3M 1s
471450K .......... .......... .......... .......... .......... 98% 35.6M 1s
471500K .......... .......... .......... .......... .......... 98% 36.2M 1s
471550K .......... .......... .......... .......... .......... 98% 26.6M 1s
471600K .......... .......... .......... .......... .......... 98% 39.5M 1s
471650K .......... .......... .......... .......... .......... 98% 42.7M 1s
471700K .......... .......... .......... .......... .......... 98% 35.3M 1s
471750K .......... .......... .......... .......... .......... 98% 28.0M 1s
471800K .......... .......... .......... .......... .......... 98% 39.4M 1s
471850K .......... .......... .......... .......... .......... 98% 60.8M 1s
471900K .......... .......... .......... .......... .......... 98% 30.5M 1s
471950K .......... .......... .......... .......... .......... 98% 95.4M 1s
472000K .......... .......... .......... .......... .......... 98% 30.7M 1s
472050K .......... .......... .......... .......... .......... 98%  112M 1s
472100K .......... .......... .......... .......... .......... 98% 21.0M 1s
472150K .......... .......... .......... .......... .......... 98% 57.2M 1s
472200K .......... .......... .......... .......... .......... 98% 98.8M 1s
472250K .......... .......... .......... .......... .......... 98% 56.8M 1s
472300K .......... .......... .......... .......... .......... 98% 58.0M 1s
472350K .......... .......... .......... .......... .......... 98% 55.6M 1s
472400K .......... .......... .......... .......... .......... 98% 79.5M 1s
472450K .......... .......... .......... .......... .......... 98% 49.9M 1s
472500K .......... .......... .......... .......... .......... 98% 30.2M 1s
472550K .......... .......... .......... .......... .......... 98% 32.1M 1s
472600K .......... .......... .......... .......... .......... 98% 32.8M 1s
472650K .......... .......... .......... .......... .......... 98% 24.6M 1s
472700K .......... .......... .......... .......... .......... 98% 29.9M 1s
472750K .......... .......... .......... .......... .......... 98% 37.9M 1s
472800K .......... .......... .......... .......... .......... 98% 34.7M 1s
472850K .......... .......... .......... .......... .......... 98% 25.6M 1s
472900K .......... .......... .......... .......... .......... 98% 25.3M 1s
472950K .......... .......... .......... .......... .......... 98% 37.2M 1s
473000K .......... .......... .......... .......... .......... 98% 20.2M 1s
473050K .......... .......... .......... .......... .......... 98% 35.9M 1s
473100K .......... .......... .......... .......... .......... 98% 27.2M 1s
473150K .......... .......... .......... .......... .......... 98% 30.5M 1s
473200K .......... .......... .......... .......... .......... 98% 24.0M 1s
473250K .......... .......... .......... .......... .......... 98% 26.7M 1s
473300K .......... .......... .......... .......... .......... 98% 31.7M 1s
473350K .......... .......... .......... .......... .......... 98% 25.4M 1s
473400K .......... .......... .......... .......... .......... 98% 29.2M 1s
473450K .......... .......... .......... .......... .......... 98% 24.0M 1s
473500K .......... .......... .......... .......... .......... 98% 40.3M 1s
473550K .......... .......... .......... .......... .......... 98% 35.1M 1s
473600K .......... .......... .......... .......... .......... 98% 47.9M 1s
473650K .......... .......... .......... .......... .......... 98% 17.3M 1s
473700K .......... .......... .......... .......... .......... 98% 97.9M 1s
473750K .......... .......... .......... .......... .......... 98% 27.6M 1s
473800K .......... .......... .......... .......... .......... 98% 60.7M 1s
473850K .......... .......... .......... .......... .......... 98% 67.3M 1s
473900K .......... .......... .......... .......... .......... 98% 35.1M 1s
473950K .......... .......... .......... .......... .......... 98% 64.6M 1s
474000K .......... .......... .......... .......... .......... 98% 34.5M 1s
474050K .......... .......... .......... .......... .......... 98% 38.1M 1s
474100K .......... .......... .......... .......... .......... 98% 33.2M 1s
474150K .......... .......... .......... .......... .......... 98% 33.2M 1s
474200K .......... .......... .......... .......... .......... 98% 17.2M 1s
474250K .......... .......... .......... .......... .......... 98% 26.0M 0s
474300K .......... .......... .......... .......... .......... 98% 27.3M 0s
474350K .......... .......... .......... .......... .......... 98% 20.7M 0s
474400K .......... .......... .......... .......... .......... 98% 44.7M 0s
474450K .......... .......... .......... .......... .......... 98% 28.1M 0s
474500K .......... .......... .......... .......... .......... 98% 47.9M 0s
474550K .......... .......... .......... .......... .......... 98% 20.8M 0s
474600K .......... .......... .......... .......... .......... 98% 29.6M 0s
474650K .......... .......... .......... .......... .......... 98% 30.3M 0s
474700K .......... .......... .......... .......... .......... 98% 17.8M 0s
474750K .......... .......... .......... .......... .......... 98% 38.9M 0s
474800K .......... .......... .......... .......... .......... 98% 41.2M 0s
474850K .......... .......... .......... .......... .......... 98% 24.4M 0s
474900K .......... .......... .......... .......... .......... 98% 41.9M 0s
474950K .......... .......... .......... .......... .......... 98% 19.2M 0s
475000K .......... .......... .......... .......... .......... 98% 26.5M 0s
475050K .......... .......... .......... .......... .......... 98% 70.4M 0s
475100K .......... .......... .......... .......... .......... 98% 23.4M 0s
475150K .......... .......... .......... .......... .......... 98% 72.6M 0s
475200K .......... .......... .......... .......... .......... 98% 13.2M 0s
475250K .......... .......... .......... .......... .......... 98% 77.9M 0s
475300K .......... .......... .......... .......... .......... 98% 76.5M 0s
475350K .......... .......... .......... .......... .......... 98% 39.9M 0s
475400K .......... .......... .......... .......... .......... 98% 57.2M 0s
475450K .......... .......... .......... .......... .......... 98% 30.7M 0s
475500K .......... .......... .......... .......... .......... 98%  121M 0s
475550K .......... .......... .......... .......... .......... 98% 47.5M 0s
475600K .......... .......... .......... .......... .......... 98% 34.3M 0s
475650K .......... .......... .......... .......... .......... 98% 37.3M 0s
475700K .......... .......... .......... .......... .......... 98% 27.4M 0s
475750K .......... .......... .......... .......... .......... 98% 37.4M 0s
475800K .......... .......... .......... .......... .......... 99% 36.0M 0s
475850K .......... .......... .......... .......... .......... 99% 37.9M 0s
475900K .......... .......... .......... .......... .......... 99% 36.6M 0s
475950K .......... .......... .......... .......... .......... 99% 35.7M 0s
476000K .......... .......... .......... .......... .......... 99% 27.6M 0s
476050K .......... .......... .......... .......... .......... 99% 30.7M 0s
476100K .......... .......... .......... .......... .......... 99% 40.0M 0s
476150K .......... .......... .......... .......... .......... 99% 42.9M 0s
476200K .......... .......... .......... .......... .......... 99% 21.7M 0s
476250K .......... .......... .......... .......... .......... 99% 45.3M 0s
476300K .......... .......... .......... .......... .......... 99% 38.4M 0s
476350K .......... .......... .......... .......... .......... 99% 35.0M 0s
476400K .......... .......... .......... .......... .......... 99% 33.8M 0s
476450K .......... .......... .......... .......... .......... 99% 23.1M 0s
476500K .......... .......... .......... .......... .......... 99% 31.4M 0s
476550K .......... .......... .......... .......... .......... 99% 42.1M 0s
476600K .......... .......... .......... .......... .......... 99% 29.5M 0s
476650K .......... .......... .......... .......... .......... 99% 36.6M 0s
476700K .......... .......... .......... .......... .......... 99% 54.9M 0s
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476800K .......... .......... .......... .......... .......... 99% 32.7M 0s
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476900K .......... .......... .......... .......... .......... 99% 73.3M 0s
476950K .......... .......... .......... .......... .......... 99% 27.1M 0s
477000K .......... .......... .......... .......... .......... 99% 58.2M 0s
477050K .......... .......... .......... .......... .......... 99% 80.2M 0s
477100K .......... .......... .......... .......... .......... 99% 47.4M 0s
477150K .......... .......... .......... .......... .......... 99% 73.2M 0s
477200K .......... .......... .......... .......... .......... 99% 62.1M 0s
477250K .......... .......... .......... .......... .......... 99% 72.4M 0s
477300K .......... .......... .......... .......... .......... 99% 75.2M 0s
477350K .......... .......... .......... .......... .......... 99% 65.7M 0s
477400K .......... .......... .......... .......... .......... 99% 62.5M 0s
477450K .......... .......... .......... .......... .......... 99% 34.0M 0s
477500K .......... .......... .......... .......... .......... 99% 53.5M 0s
477550K .......... .......... .......... .......... .......... 99% 34.3M 0s
477600K .......... .......... .......... .......... .......... 99% 28.2M 0s
477650K .......... .......... .......... .......... .......... 99% 40.1M 0s
477700K .......... .......... .......... .......... .......... 99% 35.5M 0s
477750K .......... .......... .......... .......... .......... 99% 45.3M 0s
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477850K .......... .......... .......... .......... .......... 99% 49.8M 0s
477900K .......... .......... .......... .......... .......... 99% 31.5M 0s
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478000K .......... .......... .......... .......... .......... 99% 42.7M 0s
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478100K .......... .......... .......... .......... .......... 99% 42.6M 0s
478150K .......... .......... .......... .......... .......... 99% 40.1M 0s
478200K .......... .......... .......... .......... .......... 99% 34.8M 0s
478250K .......... .......... .......... .......... .......... 99% 43.2M 0s
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478850K .......... .......... .......... .......... .......... 99% 31.0M 0s
478900K .......... .......... .......... .......... .......... 99% 97.5M 0s
478950K .......... .......... .......... .......... .......... 99% 13.9M 0s
479000K .......... .......... .......... .......... .......... 99%  108M 0s
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479100K .......... .......... .......... .......... .......... 99% 95.4M 0s
479150K .......... .......... .......... .......... .......... 99% 31.8M 0s
479200K .......... .......... .......... .......... .......... 99% 60.7M 0s
479250K .......... .......... .......... .......... .......... 99% 90.6M 0s
479300K .......... .......... .......... .......... .......... 99% 31.3M 0s
479350K .......... .......... .......... .......... .......... 99% 92.8M 0s
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479450K .......... .......... .......... .......... .......... 99% 98.6M 0s
479500K .......... .......... .......... .......... .......... 99% 37.9M 0s
479550K .......... .......... .......... .......... .......... 99% 31.0M 0s
479600K .......... .......... .......... .......... .......... 99% 46.5M 0s
479650K .......... .......... .......... .......... .......... 99% 26.8M 0s
479700K .......... .......... .......... .......... .......... 99% 24.8M 0s
479750K .......... .......... .......... .......... .......... 99% 42.1M 0s
479800K .......... .......... .......... .......... .......... 99% 27.4M 0s
479850K .......... .......... .......... .......... .......... 99% 34.7M 0s
479900K .......... .......... .......... .......... .......... 99% 21.9M 0s
479950K .......... .......... .......... .......... .......... 99% 37.4M 0s
480000K .......... .......... .......... .......... .......... 99% 38.5M 0s
480050K .......... .......... .......... .......... .......... 99% 26.3M 0s
480100K .......... .......... .......... .......... .......... 99% 26.9M 0s
480150K .......... .......... .......... .......... .......... 99% 44.1M 0s
480200K .......... .......... .......... .......... .......... 99% 37.9M 0s
480250K .......... .......... .......... .......... .......... 99% 28.2M 0s
480300K .......... .......... .......... .......... .......... 99% 32.6M 0s
480350K .......... .......... .......... .......... .......... 99% 34.4M 0s
480400K .......... .......... .......... .......... .......... 99% 23.0M 0s
480450K .......... .......... .......... .......... .......... 99% 37.2M 0s
480500K .......... .......... .......... .......... .......... 99% 43.8M 0s
480550K .......... .......... .......... .......... .......... 99% 26.0M 0s
480600K .......... .......                                    100% 65.0M=38s

2024-04-28 13:00:11 (12.5 MB/s) - ‘ESPbeta-macos-arm64.tgz’ saved [492152537/492152537]

+ tar -xf ESPbeta-macos-arm64.tgz
+ cd ESPbeta
+ rm -rf /Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/EngSketchPad/data/Slugs
++ uname -a
+ [[ Darwin VIGGEN.MIT.EDU 23.3.0 Darwin Kernel Version 23.3.0: Wed Dec 20 21:30:27 PST 2023; root:xnu-10002.81.5~7/RELEASE_ARM64_T8103 arm64 == *\D\a\r\w\i\n* ]]
+ ./setup.command
Custom icon assigned to '/Users/jenkins/Desktop/ESP125.command' based on '/Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/EngSketchPad/ESP/esp_logo.png'.
Custom icon assigned to '/Users/jenkins/Desktop/runESP125.command' based on '/Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/EngSketchPad/ESP/esp_logo.png'.
Patching '/Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/Python-3.11.9/bin/idle3.11'
Patching '/Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/Python-3.11.9/bin/pyftsubset'
Patching '/Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/Python-3.11.9/bin/test_op4'
Patching '/Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/Python-3.11.9/bin/ttx'
Patching '/Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/Python-3.11.9/bin/wingproj'
Patching '/Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/Python-3.11.9/bin/test_op2'
Patching '/Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/Python-3.11.9/bin/pip3'
Patching '/Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/Python-3.11.9/bin/test_bdf'
Patching '/Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/Python-3.11.9/bin/undill'
Patching '/Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/Python-3.11.9/bin/bdf'
Patching '/Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/Python-3.11.9/bin/run_om_test'
Patching '/Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/Python-3.11.9/bin/f90nml'
Patching '/Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/Python-3.11.9/bin/webview'
Patching '/Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/Python-3.11.9/bin/fonttools'
Patching '/Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/Python-3.11.9/bin/openmdao'
Patching '/Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/Python-3.11.9/bin/pyNastranGUI'
Patching '/Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/Python-3.11.9/bin/f2py'
Patching '/Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/Python-3.11.9/bin/pydoc3.11'
Patching '/Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/Python-3.11.9/bin/2to3-3.11'
Patching '/Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/Python-3.11.9/bin/pip3.11'
Patching '/Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/Python-3.11.9/bin/test_pynastrangui'
Patching '/Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/Python-3.11.9/bin/numba'
Patching '/Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/Python-3.11.9/bin/normalizer'
Patching '/Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/Python-3.11.9/bin/virtualenv'
Patching '/Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/Python-3.11.9/bin/reset_notebook'
Patching '/Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/Python-3.11.9/bin/abaqus_to_nastran'
Patching '/Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/Python-3.11.9/bin/get_gprof'
Patching '/Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/Python-3.11.9/bin/format_converter'
Patching '/Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/Python-3.11.9/bin/pyftmerge'
Patching '/Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/Python-3.11.9/bin/python3.11-config'
Patching '/Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/Python-3.11.9/bin/f06'
Patching '/Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/Python-3.11.9/bin/get_objgraph'
Patching '/Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/Python-3.11.9/lib/python3.11/config-3.11-darwin/Makefile'
Patching '/Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/Python-3.11.9/lib/python3.11/config-3.11-darwin/python-config.py'
Patching '/Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/Python-3.11.9/lib/pkgconfig/python-3.11-embed.pc'
Patching '/Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/Python-3.11.9/lib/pkgconfig/python-3.11.pc'
Patching '/Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/Python-3.11.9/lib/python3.11/_sysconfigdata__darwin_darwin.py'
Patching '/Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/Python-3.11.9/lib/python3.11/site-packages/mpi4py/mpi.cfg'
Patching 'bin/ompi_info'
Patching 'bin/orte-info'
Patching 'lib/libmpi.40.dylib'
Patching 'lib/libopen-pal.40.dylib'
Patching 'lib/openmpi/mca_io_romio321.so'
Patching 'lib/openmpi/mca_pmix_pmix3x.so'
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/orte.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/openmpi/ortecc-wrapper-data.txt'
+ rm -rf '/Users/jenkins/Desktop/*ESPbeta.command'
+ source /Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/EngSketchPad/ESPenv.sh
++ export ESP_ARCH=DARWIN64
++ ESP_ARCH=DARWIN64
++ export ESP_ROOT=/Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/EngSketchPad
++ ESP_ROOT=/Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/EngSketchPad
++ export CASROOT=/Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/OpenCASCADE-7.8.0
++ CASROOT=/Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/OpenCASCADE-7.8.0
++ export CARARCH=.
++ CARARCH=.
++ export CASREV=7.8
++ CASREV=7.8
++ export PATH=.:/Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/EngSketchPad/bin:/Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/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/ESPbeta/EngSketchPad/bin:/Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/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/ESPbeta/Python-3.11.9/include/python3.11
++ PYTHONINC=/Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/Python-3.11.9/include/python3.11
++ export 'PYTHONLIB=-L/Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/Python-3.11.9/lib -lpython3.11'
++ PYTHONLIB='-L/Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/Python-3.11.9/lib -lpython3.11'
++ export PYTHONPATH=/Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/EngSketchPad/lib:/Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/EngSketchPad/pyESP:/Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/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/ESPbeta/EngSketchPad/lib:/Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/EngSketchPad/pyESP:/Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/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/ESPbeta/EngSketchPad/src/CAPS/udunits/udunits2.xml
++ UDUNITS2_XML_PATH=/Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/EngSketchPad/src/CAPS/udunits/udunits2.xml
++ export CAPS_GLYPH=/Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/EngSketchPad/src/CAPS/aim/pointwise/glyph
++ CAPS_GLYPH=/Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/EngSketchPad/src/CAPS/aim/pointwise/glyph
++ export 'SLUGS_START=open -a /Applications/Safari.app /Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/EngSketchPad/SLUGS/Slugs.html'
++ SLUGS_START='open -a /Applications/Safari.app /Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/EngSketchPad/SLUGS/Slugs.html'
++ export 'ESP_START=open -a /Applications/Safari.app;sleep 1;open -a /Applications/Safari.app /Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/EngSketchPad/ESP/ESP-localhost7681.html'
++ ESP_START='open -a /Applications/Safari.app;sleep 1;open -a /Applications/Safari.app /Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/EngSketchPad/ESP/ESP-localhost7681.html'
++ export 'WV_START=open -a /Applications/Safari.app /Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/EngSketchPad/wvClient/wv.html'
++ WV_START='open -a /Applications/Safari.app /Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/EngSketchPad/wvClient/wv.html'
+ which python
/Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/Python-3.11.9/bin/python
+ python --version
Python 3.11.9
+ export CSMDATA=/Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/EngSketchPad/data
+ CSMDATA=/Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/EngSketchPad/data
+ cd /Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/EngSketchPad/bin
++ uname -a
+ [[ Darwin VIGGEN.MIT.EDU 23.3.0 Darwin Kernel Version 23.3.0: Wed Dec 20 21:30:27 PST 2023; root:xnu-10002.81.5~7/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/ESPbeta/EngSketchPad/data/basic/expressions
+ ./serveESP -batch -verify -outLevel 0 /Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/EngSketchPad/data/basic/expressions
WARNING:: cannot open "/Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/EngSketchPad/data/basic/verify_7.8.0/expressions.vfy", so verification is being skipped
ERROR:: (func_arg_out_of_bounds) in Branch Brch_000152 at [[/Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/EngSketchPad/data/basic/expressions.csm:169]]
        ibeg must be be between 1 and strlen(str) when evaluating "slice(e3,0,999)"
ERROR:: problem evaluating argument 2 (slice(e3,0,999)) for Branch 152 (set)
    --> catching signal -258 (func_arg_out_of_bounds)
ERROR:: (func_arg_out_of_bounds) in Branch Brch_000158 at [[/Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/EngSketchPad/data/basic/expressions.csm:176]]
        ibeg must be be between 1 and strlen(str) when evaluating "slice(e3,14,999)"
ERROR:: problem evaluating argument 2 (slice(e3,14,999)) for Branch 158 (set)
    --> catching signal -258 (func_arg_out_of_bounds)
ERROR:: (func_arg_out_of_bounds) in Branch Brch_000164 at [[/Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/EngSketchPad/data/basic/expressions.csm:183]]
        iend must not be less than ibeg when evaluating "slice(e3,4,-1)"
ERROR:: problem evaluating argument 2 (slice(e3,4,-1)) for Branch 164 (set)
    --> catching signal -258 (func_arg_out_of_bounds)
ERROR:: (illegal_pmtr_index) in Branch Brch_000317 at [[/Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/EngSketchPad/data/basic/expressions.csm:384]]
        index must be between 1 and 2
    --> catching signal -262 (illegal_pmtr_index)
ERROR:: (illegal_pmtr_index) in Branch Brch_000332 at [[/Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/EngSketchPad/data/basic/expressions.csm:402]]
        index must be between 1 and 2
    --> catching signal -262 (illegal_pmtr_index)
ERROR:: (illegal_pmtr_index) in Branch Brch_000346 at [[/Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/EngSketchPad/data/basic/expressions.csm:418]]
        row index must be between 1 and 2
    --> catching signal -262 (illegal_pmtr_index)
ERROR:: (illegal_pmtr_index) in Branch Brch_000360 at [[/Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/EngSketchPad/data/basic/expressions.csm:434]]
        row index must be between 1 and 2
    --> catching signal -262 (illegal_pmtr_index)
ERROR:: (illegal_pmtr_index) in Branch Brch_000367 at [[/Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/EngSketchPad/data/basic/expressions.csm:442]]
        row index must be between 1 and 2
    --> catching signal -262 (illegal_pmtr_index)
ERROR:: (illegal_pmtr_index) in Branch Brch_000374 at [[/Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/EngSketchPad/data/basic/expressions.csm:450]]
        column index must be between 1 and 3
    --> catching signal -262 (illegal_pmtr_index)
ERROR:: (illegal_pmtr_index) in Branch Brch_000381 at [[/Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/EngSketchPad/data/basic/expressions.csm:458]]
        column index must be between 1 and 3
    --> catching signal -262 (illegal_pmtr_index)
ERROR:: (UNKNOWN) in Branch Brch_001805 at [[/Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/EngSketchPad/data/basic/expressions.csm:1914]]
        signal 1 thrown by user
    --> catching signal 1 (UNKNOWN)
ERROR:: (illegal_value) in Branch Brch_001813 at [[/Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/EngSketchPad/data/basic/expressions.csm:1924]]
        vertex and base must be different
    --> catching signal -225 (illegal_value)
==> serveESP completed successfully with no verification data

real	0m2.436s
user	0m0.166s
sys	0m0.043s
+ set +x

=============================================
ESP verification case 01 passed (as expected)
=============================================

+ expectSuccess 02 /Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/EngSketchPad/data/basic/demo2
+ ./serveESP -batch -verify -outLevel 0 /Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/EngSketchPad/data/basic/demo2
WARNING:: cannot open "/Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/EngSketchPad/data/basic/verify_7.8.0/demo2.vfy", so verification is being skipped
==> serveESP completed successfully with no verification data

real	0m0.224s
user	0m0.252s
sys	0m0.029s
+ set +x

=============================================
ESP verification case 02 passed (as expected)
=============================================

+ expectSuccess 03 /Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/EngSketchPad/data/legacy/tutorial1_whole
+ ./serveESP -batch -verify -outLevel 0 /Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/EngSketchPad/data/legacy/tutorial1_whole
WARNING:: cannot open "/Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/EngSketchPad/data/legacy/verify_7.8.0/tutorial1_whole.vfy", so verification is being skipped
==> serveESP completed successfully with no verification data

real	0m1.287s
user	0m1.967s
sys	0m0.648s
+ set +x

=============================================
ESP verification case 03 passed (as expected)
=============================================

+ expectSuccess 04 /Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/EngSketchPad/data/basic/design2
+ ./serveESP -batch -verify -outLevel 0 /Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/EngSketchPad/data/basic/design2
WARNING:: cannot open "/Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/EngSketchPad/data/basic/verify_7.8.0/design2.vfy", so verification is being skipped
==> serveESP completed successfully with no verification data

real	0m0.317s
user	0m0.356s
sys	0m0.034s
+ set +x

=============================================
ESP verification case 04 passed (as expected)
=============================================

+ expectSuccess 05 /Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/EngSketchPad/data/basic/design3
+ ./serveESP -batch -verify -outLevel 0 /Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/EngSketchPad/data/basic/design3
WARNING:: cannot open "/Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/EngSketchPad/data/basic/verify_7.8.0/design3.vfy", so verification is being skipped
==> serveESP completed successfully with no verification data

real	0m0.327s
user	0m0.450s
sys	0m0.036s
+ set +x

=============================================
ESP verification case 05 passed (as expected)
=============================================

+ expectSuccess 06 /Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/EngSketchPad/data/legacy/tutorial2
+ ./serveESP -batch -verify -outLevel 0 /Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/EngSketchPad/data/legacy/tutorial2
WARNING:: cannot open "/Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/EngSketchPad/data/legacy/verify_7.8.0/tutorial2.vfy", so verification is being skipped
==> serveESP completed successfully with no verification data

real	0m0.319s
user	0m0.455s
sys	0m0.017s
+ set +x

=============================================
ESP verification case 06 passed (as expected)
=============================================

+ expectSuccess 07 /Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/EngSketchPad/data/legacy/tutorial3
+ ./serveESP -batch -verify -outLevel 0 /Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/EngSketchPad/data/legacy/tutorial3
WARNING:: cannot open "/Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/EngSketchPad/data/legacy/verify_7.8.0/tutorial3.vfy", so verification is being skipped
==> serveESP completed successfully with no verification data

real	0m1.868s
user	0m3.530s
sys	0m0.364s
+ set +x

=============================================
ESP verification case 07 passed (as expected)
=============================================

+ expectSuccess 08 /Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/EngSketchPad/data/CAPS/myPlane
+ ./serveESP -batch -verify -outLevel 0 /Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/EngSketchPad/data/CAPS/myPlane
WARNING:: cannot open "/Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/EngSketchPad/data/CAPS/verify_7.8.0/myPlane.vfy", so verification is being skipped
==> serveESP completed successfully with 12 warnings and no verification data

real	0m14.423s
user	0m26.887s
sys	0m1.319s
+ set +x

=============================================
ESP verification case 08 passed (as expected)
=============================================

+ expectSuccess 09 /Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/EngSketchPad/data/bottle
+ ./serveESP -batch -verify -outLevel 0 /Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/EngSketchPad/data/bottle
WARNING:: cannot open "/Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/EngSketchPad/data/verify_7.8.0/bottle.vfy", so verification is being skipped
==> serveESP completed successfully with no verification data

real	0m0.336s
user	0m0.407s
sys	0m0.012s
+ set +x

=============================================
ESP verification case 09 passed (as expected)
=============================================

+ expectSuccess 10 /Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/EngSketchPad/data/basic/wingMultiModel
+ ./serveESP -batch -verify -outLevel 0 /Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/EngSketchPad/data/basic/wingMultiModel
WARNING:: cannot open "/Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/EngSketchPad/data/basic/verify_7.8.0/wingMultiModel.vfy", so verification is being skipped
==> serveESP completed successfully with 4 warnings and no verification data

real	0m15.698s
user	0m49.406s
sys	0m22.620s
+ set +x

=============================================
ESP verification case 10 passed (as expected)
=============================================

+ expectSuccess 11 /Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/EngSketchPad/data/basic/bullet
+ ./serveESP -batch -verify -outLevel 0 /Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/EngSketchPad/data/basic/bullet
WARNING:: cannot open "/Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/EngSketchPad/data/basic/verify_7.8.0/bullet.vfy", so verification is being skipped
WARNING:: 8 _hist and/or __trace__ attributes removed
WARNING:: 8 _hist and/or __trace__ attributes removed
==> serveESP completed successfully with 1 warnings and no verification data

real	0m0.286s
user	0m0.233s
sys	0m0.018s
+ set +x

=============================================
ESP verification case 11 passed (as expected)
=============================================

+ expectSuccess 12 /Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/EngSketchPad/data/basic/connect5
+ ./serveESP -batch -verify -outLevel 0 /Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/EngSketchPad/data/basic/connect5
WARNING:: cannot open "/Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/EngSketchPad/data/basic/verify_7.8.0/connect5.vfy", so verification is being skipped
==> serveESP completed successfully with no verification data

real	0m0.362s
user	0m0.555s
sys	0m0.007s
+ set +x

=============================================
ESP verification case 12 passed (as expected)
=============================================

+ expectSuccess 13 /Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/EngSketchPad/data/basic/group2
+ ./serveESP -batch -verify -outLevel 0 /Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/EngSketchPad/data/basic/group2
WARNING:: cannot open "/Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/EngSketchPad/data/basic/verify_7.8.0/group2.vfy", so verification is being skipped
==> serveESP completed successfully with no verification data

real	0m0.149s
user	0m0.163s
sys	0m0.006s
+ set +x

=============================================
ESP verification case 13 passed (as expected)
=============================================

+ expectSuccess 14 /Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/EngSketchPad/data/basic/csm3
+ ./serveESP -batch -verify -outLevel 0 /Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/EngSketchPad/data/basic/csm3
WARNING:: cannot open "/Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/EngSketchPad/data/basic/verify_7.8.0/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
==> serveESP completed successfully with no verification data

real	0m0.332s
user	0m0.331s
sys	0m0.010s
+ set +x

=============================================
ESP verification case 14 passed (as expected)
=============================================

+ cd /Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/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 71 tests in 1.009s

OK
+ cd /Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/EngSketchPad/pyESP/testOCSM
+ source /Users/jenkins/workspace/ESP_bPreBuilt/JenkinsESP/test_pyOCSM.sh
++ set -x
++ python -u test_pyOCSM.py -skipHelp

real	0m3.421s
user	0m5.181s
sys	0m0.081s
++ set +x
=================================================
test_pyOCSM.py passed (as expected)
=================================================
+ cd /Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/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
..........--> 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 -> __numRemaining__ (EG_attributeDel)!
 EGADS Error: No Attribute -> __numRemaining__ (EG_attributeDel)!
 EGADS Error: No Attribute -> _body (EG_attributeDel)!
 EGADS Error: No Attribute -> _nface (EG_attributeDel)!
 EGADS Error: No Attribute -> __trace__ (EG_attributeDel)!
 EGADS Error: No Attribute -> _body (EG_attributeDel)!
 EGADS Error: No Attribute -> _nface (EG_attributeDel)!
 EGADS Error: No Attribute -> __trace__ (EG_attributeDel)!
 EGADS Error: No Attribute -> _body (EG_attributeDel)!
 EGADS Error: No Attribute -> _nface (EG_attributeDel)!
 EGADS Error: No Attribute -> __trace__ (EG_attributeDel)!
 EGADS Error: No Attribute -> _body (EG_attributeDel)!
 EGADS Error: No Attribute -> _nface (EG_attributeDel)!
 EGADS Error: No Attribute -> __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 -> __numRemaining__ (EG_attributeDel)!
 EGADS Error: No Attribute -> _body (EG_attributeDel)!
 EGADS Error: No Attribute -> _nface (EG_attributeDel)!
 EGADS Error: No Attribute -> __trace__ (EG_attributeDel)!
 EGADS Error: No Attribute -> _body (EG_attributeDel)!
 EGADS Error: No Attribute -> _nface (EG_attributeDel)!
 EGADS Error: No Attribute -> __trace__ (EG_attributeDel)!
 EGADS Error: No Attribute -> _body (EG_attributeDel)!
 EGADS Error: No Attribute -> _nface (EG_attributeDel)!
 EGADS Error: No Attribute -> __trace__ (EG_attributeDel)!
 EGADS Error: No Attribute -> _body (EG_attributeDel)!
 EGADS Error: No Attribute -> _nface (EG_attributeDel)!
 EGADS Error: No Attribute -> __trace__ (EG_attributeDel)!
 EGADS Error: No Attribute -> __numRemaining__ (EG_attributeDel)!
. EGADS Info: 0 Objects, 0 Reference in Use (of 0) at Close!
.--> 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 8.785s

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/ESPbeta/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 9.17.15
AFLR2    : Version Date   04/23/24 @ 12:51AM
AFLR2    : Compile OS     Darwin 23.4.0 arm64
AFLR2    : Compile Date   04/23/24 @ 12:51AM
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          =     0.038   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          =     0.036   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 9.17.15
AFLR2    : Version Date   04/23/24 @ 12:51AM
AFLR2    : Compile OS     Darwin 23.4.0 arm64
AFLR2    : Compile Date   04/23/24 @ 12:51AM
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 9.17.15
AFLR2    : Version Date   04/23/24 @ 12:51AM
AFLR2    : Compile OS     Darwin 23.4.0 arm64
AFLR2    : Compile Date   04/23/24 @ 12:51AM
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          =     0.036   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 9.17.15
AFLR2    : Version Date   04/23/24 @ 12:51AM
AFLR2    : Compile OS     Darwin 23.4.0 arm64
AFLR2    : Compile Date   04/23/24 @ 12:51AM
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 9.17.15
AFLR2    : Version Date   04/23/24 @ 12:51AM
AFLR2    : Compile OS     Darwin 23.4.0 arm64
AFLR2    : Compile Date   04/23/24 @ 12:51AM
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 9.17.15
AFLR2    : Version Date   04/23/24 @ 12:51AM
AFLR2    : Compile OS     Darwin 23.4.0 arm64
AFLR2    : Compile Date   04/23/24 @ 12:51AM
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 9.17.15
AFLR2    : Version Date   04/23/24 @ 12:51AM
AFLR2    : Compile OS     Darwin 23.4.0 arm64
AFLR2    : Compile Date   04/23/24 @ 12:51AM
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:61955)
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 9.17.15
AFLR2    : Version Date   04/23/24 @ 12:51AM
AFLR2    : Compile OS     Darwin 23.4.0 arm64
AFLR2    : Compile Date   04/23/24 @ 12:51AM
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 11.5.14
AFLR4    : Version Date   04/18/24 @ 12:45PM
AFLR4    : Compile OS     Darwin 23.4.0 arm64
AFLR4    : Compile Date   04/18/24 @ 03:04PM
AFLR4    : Copyright 1994-2021, D.L. Marcum
AFLR4    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.8.0
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 1.25
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.8.0
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 1.25
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.8.0
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 1.25
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.8.0
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 1.25
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.8.0
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 1.25
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.8.0
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 1.25
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.8.0
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 1.25
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------
Getting volume mesh for body 2 (of 7)

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------
Getting volume mesh for body 3 (of 7)

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------
Getting volume mesh for body 4 (of 7)

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------
Getting volume mesh for body 5 (of 7)

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------
Getting volume mesh for body 6 (of 7)

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------
Getting volume mesh for body 7 (of 7)

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.8.0
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:61955)
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 9.17.15
AFLR2    : Version Date   04/23/24 @ 12:51AM
AFLR2    : Compile OS     Darwin 23.4.0 arm64
AFLR2    : Compile Date   04/23/24 @ 12:51AM
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 11.5.14
AFLR4    : Version Date   04/18/24 @ 12:45PM
AFLR4    : Compile OS     Darwin 23.4.0 arm64
AFLR4    : Compile Date   04/18/24 @ 03:04PM
AFLR4    : Copyright 1994-2021, D.L. Marcum
AFLR4    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------
Volume mesh:
	Number of nodes          = 16607
	Number of elements       = 94482
	Number of triangles      = 7926
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 86556
	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 1.25
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.8.0
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 1.25
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.8.0
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 1.25
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.8.0
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 1.25
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.8.0
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 1.25
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.8.0
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 1.25
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.8.0
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 1.25
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------
Getting volume mesh for body 2 (of 2)

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.8.0
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 1.25
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.8.0
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 1.25
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.8.0
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 1.25
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.8.0
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 1.25
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------
Getting volume mesh for body 2 (of 3)

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------
Getting volume mesh for body 3 (of 3)

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.8.0
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 1.25
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.8.0
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 1.25
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.8.0
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 1.25
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.8.0
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 1.25
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.8.0
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 1.25
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------
Getting volume mesh for body 2 (of 4)

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------
Getting volume mesh for body 3 (of 4)

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------
Getting volume mesh for body 4 (of 4)

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.8.0
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 1.25
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.8.0
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 1.25
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.8.0
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 1.25
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.8.0
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 1.25
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.8.0
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 1.25
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.8.0
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 1.25
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------
Getting volume mesh for body 2 (of 5)

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------
Getting volume mesh for body 3 (of 5)

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------
Getting volume mesh for body 4 (of 5)

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------
Getting volume mesh for body 5 (of 5)

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.8.0
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 1.25
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.8.0
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 1.25
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.8.0
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 1.25
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.8.0
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 1.25
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.8.0
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 1.25
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.8.0
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 1.25
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.8.0
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 1.25
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------
Getting volume mesh for body 2 (of 6)

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------
Getting volume mesh for body 3 (of 6)

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------
Getting volume mesh for body 4 (of 6)

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------
Getting volume mesh for body 5 (of 6)

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------
Getting volume mesh for body 6 (of 6)

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.8.0
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 1.25
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.8.0
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 1.25
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.8.0
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 1.25
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.8.0
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 1.25
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.8.0
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 1.25
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.8.0
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 1.25
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.8.0
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 1.25
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.8.0
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 1.25
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------
Getting volume mesh for body 2 (of 7)

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------
Getting volume mesh for body 3 (of 7)

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------
Getting volume mesh for body 4 (of 7)

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------
Getting volume mesh for body 5 (of 7)

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------
Getting volume mesh for body 6 (of 7)

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------
Getting volume mesh for body 7 (of 7)

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.8.0
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 1.25
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.8.0
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 1.25
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.8.0
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 1.25
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.8.0
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 1.25
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.8.0
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 1.25
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.8.0
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 1.25
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.8.0
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 1.25
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.8.0
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 1.25
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.8.0
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 1.25
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------
Getting volume mesh for body 2 (of 19)

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------
Getting volume mesh for body 3 (of 19)

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------
Getting volume mesh for body 4 (of 19)

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------
Getting volume mesh for body 5 (of 19)

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------
Getting volume mesh for body 6 (of 19)

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------
Getting volume mesh for body 7 (of 19)

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------
Getting volume mesh for body 8 (of 19)

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------
Getting volume mesh for body 9 (of 19)

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------
Getting volume mesh for body 10 (of 19)

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------
Getting volume mesh for body 11 (of 19)

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------
Getting volume mesh for body 12 (of 19)

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------
Getting volume mesh for body 13 (of 19)

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------
Getting volume mesh for body 14 (of 19)

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------
Getting volume mesh for body 15 (of 19)

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------
Getting volume mesh for body 16 (of 19)

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------
Getting volume mesh for body 17 (of 19)

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------
Getting volume mesh for body 18 (of 19)

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------
Getting volume mesh for body 19 (of 19)

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.8.0
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 1.25
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.8.0
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 1.25
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.8.0
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 1.25
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.8.0
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 1.25
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.8.0
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 1.25
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.8.0
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 1.25
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.8.0
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 1.25
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.8.0
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 1.25
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.8.0
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 1.25
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.8.0
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 1.25
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.8.0
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 1.25
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.8.0
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 1.25
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.8.0
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 1.25
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.8.0
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 1.25
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.8.0
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 1.25
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.8.0
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 1.25
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.8.0
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 1.25
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.8.0
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 1.25
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.8.0
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 1.25
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.8.0
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 1.25
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.8.0
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 1.25
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------
Getting volume mesh for body 2 (of 2)

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.8.0
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 1.25
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.8.0
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 1.25
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.8.0
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 1.25
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.8.0
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 1.25
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------
Getting volume mesh for body 2 (of 3)

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------
Getting volume mesh for body 3 (of 3)

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.8.0
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 1.25
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.8.0
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 1.25
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.8.0
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 1.25
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.8.0
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 1.25
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.8.0
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 1.25
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------
Getting volume mesh for body 2 (of 3)

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------
Getting volume mesh for body 3 (of 3)

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.8.0
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 1.25
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.8.0
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 1.25
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.8.0
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 1.25
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.8.0
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 1.25
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.8.0
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 1.25
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------
Getting volume mesh for body 2 (of 3)

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------
Getting volume mesh for body 3 (of 3)

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.8.0
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 1.25
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.8.0
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 1.25
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.8.0
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 1.25
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.8.0
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 1.25
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.8.0
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 1.25
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------
Getting volume mesh for body 2 (of 3)

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------
Getting volume mesh for body 3 (of 3)

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.8.0
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 1.25
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.8.0
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 1.25
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.8.0
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 1.25
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.8.0
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 1.25
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.8.0
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 1.25
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------
Getting volume mesh for body 2 (of 3)

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------
Getting volume mesh for body 3 (of 3)

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.8.0
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 1.25
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.8.0
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 1.25
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.8.0
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 1.25
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.8.0
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 1.25
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------
Volume mesh:
	Number of nodes          = 1510
	Number of elements       = 7821
	Number of triangles      = 1986
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 5835
	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 1.25
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------
Getting volume mesh for body 2 (of 3)

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------
Getting volume mesh for body 3 (of 3)

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------
Volume mesh:
	Number of nodes          = 1574
	Number of elements       = 7945
	Number of triangles      = 2110
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 5835
	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 1.25
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------
Volume mesh for body 1 (of 3):
	Number of nodes          = 1170
	Number of elements       = 6155
	Number of triangles      = 1308
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 4847
	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 1.25
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------
Volume mesh for body 2 (of 3):
	Number of nodes          = 360
	Number of elements       = 1630
	Number of triangles      = 718
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 912
	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 1.25
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.8.0
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 1.25
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.8.0
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 1.25
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------
Getting volume mesh for body 2 (of 2)

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.8.0
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 1.25
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.8.0
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 1.25
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.8.0
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 1.25
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.8.0
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 1.25
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------
Getting volume mesh for body 2 (of 5)

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------
Getting volume mesh for body 3 (of 5)

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------
Getting volume mesh for body 4 (of 5)

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------
Getting volume mesh for body 5 (of 5)

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.8.0
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 1.25
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.8.0
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 1.25
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.8.0
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 1.25
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.8.0
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 1.25
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.8.0
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 1.25
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.8.0
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 1.25
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.8.0
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 1.25
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------
Getting volume mesh for body 2 (of 2)

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.8.0
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 1.25
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.8.0
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 1.25
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.8.0
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 = 3
	Name = Farfield, index = 1
	Name = Wing1, index = 2
	Name = trailingEdge, index = 3
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 3
	Name = Farfield, index = 1
	Name = Wing1, index = 2
	Name = trailingEdge, index = 3
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 1.25
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------
Volume mesh:
	Number of nodes          = 2838
	Number of elements       = 12404
	Number of triangles      = 5452
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 6952
	Number of pyramids       = 0
	Number of prisms         = 0
	Number of hexahedrals    = 0
Getting volume mesh

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------
Volume mesh:
	Number of nodes          = 2494
	Number of elements       = 10977
	Number of triangles      = 4552
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 6425
	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 = 3
	Name = Farfield, index = 1
	Name = Wing1, index = 2
	Name = trailingEdge, index = 3
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 3
	Name = Farfield, index = 1
	Name = Wing1, index = 2
	Name = trailingEdge, index = 3
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 1.25
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------
Volume mesh:
	Number of nodes          = 2838
	Number of elements       = 12404
	Number of triangles      = 5452
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 6952
	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 = 3
	Name = Farfield, index = 1
	Name = Wing1, index = 2
	Name = trailingEdge, index = 3
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 3
	Name = Farfield, index = 1
	Name = Wing1, index = 2
	Name = trailingEdge, index = 3
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 = 3
	Name = Farfield, index = 1
	Name = Wing1, index = 2
	Name = trailingEdge, index = 3
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 3
	Name = Farfield, index = 1
	Name = Wing1, index = 2
	Name = trailingEdge, index = 3
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 = 3
	Name = Farfield, index = 1
	Name = Wing1, index = 2
	Name = trailingEdge, index = 3
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 3
	Name = Farfield, index = 1
	Name = Wing1, index = 2
	Name = trailingEdge, index = 3
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 1.25
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------
Volume mesh:
	Number of nodes          = 2494
	Number of elements       = 10977
	Number of triangles      = 4552
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 6425
	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 = 3
	Name = Farfield, index = 1
	Name = Wing1, index = 2
	Name = trailingEdge, index = 3
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 3
	Name = Farfield, index = 1
	Name = Wing1, index = 2
	Name = trailingEdge, index = 3
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 = 3
	Name = Farfield, index = 1
	Name = Wing1, index = 2
	Name = trailingEdge, index = 3
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 3
	Name = Farfield, index = 1
	Name = Wing1, index = 2
	Name = trailingEdge, index = 3
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 1.25
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------
Volume mesh:
	Number of nodes          = 2838
	Number of elements       = 12404
	Number of triangles      = 5452
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 6952
	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 = 3
	Name = Farfield, index = 1
	Name = Wing1, index = 2
	Name = trailingEdge, index = 3
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 3
	Name = Farfield, index = 1
	Name = Wing1, index = 2
	Name = trailingEdge, index = 3
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 1.25
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------
Volume mesh:
	Number of nodes          = 2494
	Number of elements       = 10977
	Number of triangles      = 4552
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 6425
	Number of pyramids       = 0
	Number of prisms         = 0
	Number of hexahedrals    = 0

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 = 3
	Name = Farfield, index = 1
	Name = Wing1, index = 2
	Name = trailingEdge, index = 3
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 3
	Name = Farfield, index = 1
	Name = Wing1, index = 2
	Name = trailingEdge, index = 3
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 1.25
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------
Volume mesh:
	Number of nodes          = 2838
	Number of elements       = 12404
	Number of triangles      = 5452
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 6952
	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 1.25
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------
Volume mesh:
	Number of nodes          = 2494
	Number of elements       = 10977
	Number of triangles      = 4552
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 6425
	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 1.25
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.8.0
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 1.25
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.8.0
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 1.25
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------
Volume mesh:
	Number of nodes          = 60123
	Number of elements       = 350900
	Number of triangles      = 12928
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 337972
	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 1.25
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------
Volume mesh:
	Number of nodes          = 59547
	Number of elements       = 346940
	Number of triangles      = 12428
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 334512
	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 1.25
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------
Volume mesh:
	Number of nodes          = 60123
	Number of elements       = 350400
	Number of triangles      = 12428
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 337972
	Number of pyramids       = 0
	Number of prisms         = 0
	Number of hexahedrals    = 0

Writing Tecplot file ....
Finished writing Tecplot file

ok
test_MultiBody_quad (test_aflr4.TestAFLR4.test_MultiBody_quad) ... 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
ok
test_SingleBody_output (test_aflr4.TestAFLR4.test_SingleBody_output) ... 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 = 3
	Name = Farfield, index = 1
	Name = Wing1, index = 2
	Name = trailingEdge, index = 3

Getting mesh sizing parameters
	Mesh sizing name - trailingEdge
	Done getting mesh sizing parameters
ok
test_all (test_aflr4.TestAFLR4.test_all) ... ERROR:: BAD STATUS = -276 from matsol (called from solveSketchOrig:61955)
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_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_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 = 3
	Name = Farfield, index = 1
	Name = Wing1, index = 2
	Name = trailingEdge, index = 3
ok
test_journal (test_aflr4.TestAFLR4.test_journal) ... ERROR:: BAD STATUS = -276 from matsol (called from solveSketchOrig:61955)
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:61955)
ERROR:: BAD STATUS = -276 from matsol (called from solveSketchOrig:61955)
 CAPS Info: Hit last success -- going live!
ERROR:: BAD STATUS = -276 from matsol (called from solveSketchOrig:61955)
 CAPS Info: Hit last success -- going live!
ERROR:: BAD STATUS = -276 from matsol (called from solveSketchOrig:61955)
 CAPS Info: Hit last success -- going live!
ERROR:: BAD STATUS = -276 from matsol (called from solveSketchOrig:61955)
 CAPS Info: Hit last success -- going live!
ERROR:: BAD STATUS = -276 from matsol (called from solveSketchOrig:61955)
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:61955)
 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:61955)
 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:61955)
 CAPS Info: Hit last success -- going live!
ERROR:: BAD STATUS = -276 from matsol (called from solveSketchOrig:61955)
 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:61955)
 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:61955)
ok
test_phase (test_aflr4.TestAFLR4.test_phase) ... ERROR:: BAD STATUS = -276 from matsol (called from solveSketchOrig:61955)
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:61955)
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_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 = 3
	Name = Farfield, index = 1
	Name = Wing1, index = 2
	Name = trailingEdge, index = 3

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_setInput (test_aflr4.TestAFLR4.test_setInput) ...  EGADS Info: 0 Objects, 0 Reference in Use (of 0) at Close!
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 > autoInputs.out
 Executing: ./aero.csh > 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  > autoInputs.out
 Executing: ./aero.csh > aero.out
 Executing: ./aero.csh > 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  > autoInputs.out
 Executing: ./aero.csh > 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  > autoInputs.out
 o Evaluating Cart3D functionals and/or gradients
   ATTENTION: using static geometry ../inputs/Components.i.tri
   (13:03:01) Running aero.csh on 2 core(s) in M0.5A1B0_DP1
   (13:03:02) 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
   (13:03:02) Running aero.csh on 2 core(s) in M0.5A1B0_DP1
   (13:03:04) 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
   (13:03:04) Linearizing cut-cells
   (13:03:04) ... done
   o Number of simultaneous xsensit jobs:  1
   (13:03:04) Computing gradients
   (13:03:12) ... 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
   (13:03:13) Running aero.csh on 2 core(s) in M0.5A1B0_DP1
   (13:03:14) 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
   (13:03:15) Running aero.csh on 2 core(s) in M0.5A1B0_DP1
   (13:03:16) 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
   (13:03:16) Running aero.csh on 2 core(s) in M0.5A1B0_DP1
   (13:03:18) 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
   (13:03:18) Linearizing cut-cells
   (13:03:18) ... done
   o Number of simultaneous xsensit jobs:  1
   (13:03:18) Computing gradients
   (13:03:26) ... 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
   (13:03:27) Running aero.csh on 2 core(s) in M0.5A1B0_DP1
   (13:03:28) 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
   (13:03:28) Running aero.csh on 2 core(s) in M0.5A1B0_DP1
   (13:03:29) 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
   (13:03:30) Running aero.csh on 2 core(s) in M0.5A1B0_DP1
   (13:03:31) 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
   (13:03:31) Linearizing cut-cells
   (13:03:31) ... done
   o Number of simultaneous xsensit jobs:  1
   (13:03:31) Computing gradients
   (13:03:35) ... 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
   (13:03:35) Running aero.csh on 2 core(s) in M0.5A1B0_DP1
   (13:03:36) 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
   (13:03:37) Running aero.csh on 2 core(s) in M0.5A1B0_DP1
   (13:03:38) 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
   (13:03:38) Running aero.csh on 2 core(s) in M0.5A1B0_DP1
   (13:03:39) 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
   (13:03:39) Linearizing cut-cells
   (13:03:39) ... done
   o Number of simultaneous xsensit jobs:  1
   (13:03:39) Computing gradients
   (13:03:44) ... 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
   (13:03:44) Running aero.csh on 2 core(s) in M0.5A1B0_DP1
   (13:03:45) 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
   (13:03:46) Running aero.csh on 2 core(s) in M0.5A1B0_DP1
   (13:03:47) 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
   (13:03:47) Running aero.csh on 2 core(s) in M0.5A1B0_DP1
   (13:03:48) 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
   (13:03:48) Linearizing cut-cells
   (13:03:48) ... done
   o Number of simultaneous xsensit jobs:  1
   (13:03:48) Computing gradients
   (13:03:52) ... 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
   (13:03:53) Running aero.csh on 2 core(s) in M0.5A1B0_DP1
   (13:03:54) 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
   (13:03:54) Running aero.csh on 2 core(s) in M0.5A1B0_DP1
   (13:03:55) 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
   (13:03:56) Running aero.csh on 2 core(s) in M0.5A1B0_DP1
   (13:03:57) 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
   (13:03:57) Linearizing cut-cells
   (13:03:57) ... done
   o Number of simultaneous xsensit jobs:  1
   (13:03:57) Computing gradients
   (13:04:01) ... 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
   (13:04:01) Running aero.csh on 2 core(s) in M0.5A1B0_DP1
   (13:04:02) 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
   (13:04:03) Running aero.csh on 2 core(s) in M0.5A1B0_DP1
   (13:04:04) 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
   (13:04:04) Running aero.csh on 2 core(s) in M0.5A1B0_DP1
   (13:04:05) 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
   (13:04:05) Linearizing cut-cells
   (13:04:05) ... done
   o Number of simultaneous xsensit jobs:  1
   (13:04:06) Computing gradients
   (13:04:10) ... 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
   (13:04:10) Running aero.csh on 2 core(s) in M0.5A1B0_DP1
   (13:04:11) 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
   (13:04:12) Running aero.csh on 2 core(s) in M0.5A1B0_DP1
   (13:04:13) 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
   (13:04:13) Running aero.csh on 2 core(s) in M0.5A1B0_DP1
   (13:04:14) 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
   (13:04:14) Linearizing cut-cells
   (13:04:14) ... done
   o Number of simultaneous xsensit jobs:  1
   (13:04:14) Computing gradients
   (13:04:18) ... 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
   (13:04:19) Running aero.csh on 2 core(s) in M0.5A1B0_DP1
   (13:04:20) 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  > autoInputs.out
 o Evaluating Cart3D functionals and/or gradients
   ATTENTION: using static geometry ../inputs/Components.i.tri
   (13:04:21) Running aero.csh on 2 core(s) in M0.5A1B0_DP1
   (13:04:22) 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
   (13:04:23) Running aero.csh on 2 core(s) in M0.5A1B0_DP1
   (13:04:24) 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
   (13:04:25) Linearizing cut-cells
   (13:04:27) ... done
   o Number of simultaneous xsensit jobs:  2
   (13:04:27) Computing gradients
              Adjusted OMP_NUM_THREADS to 1 for xsensit
   (13:04:35) ... 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
   (13:04:35) Running aero.csh on 2 core(s) in M0.5A1B0_DP1
   (13:04:36) aero.csh done
 o case M0.5A1B0_DP1, averaging data over 1 cycle(s)
ok
test_Output (test_cbaero.TestCBAERO.test_Output) ... Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = Wing1, index = 1
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 2
	Name = Wing1, index = 1
	Name = trailingEdge, index = 2

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_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 = 3
	Name = Farfield, index = 1
	Name = Wing1, index = 2
	Name = trailingEdge, index = 3

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:61955)
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
 1E2491C40 EGADS Info: Face #3 -> Edge #9 (9) Internally in Loop 4 7, sen = -1!
 1E2491C40 EGADS Info: Face #3 -> Edge #9 (9) Internally in Loop 7 4, sen = 1!
 1740EF000 EGADS Info: Face #5 -> Edge #17 (9) Internally in Loop 7 4, sen = -1!
 1740EF000 EGADS Info: Face #5 -> 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
 1E2491C40 EGADS Info: Face #3 -> Edge #9 (9) Internally in Loop 4 7, sen = -1!
 1E2491C40 EGADS Info: Face #3 -> Edge #9 (9) Internally in Loop 7 4, sen = 1!
 1740EF000 EGADS Info: Face #5 -> Edge #17 (9) Internally in Loop 7 4, sen = -1!
 1740EF000 EGADS Info: Face #5 -> 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
 1740EF000 EGADS Info: Face #3 -> Edge #9 (9) Internally in Loop 4 7, sen = -1!
 1740EF000 EGADS Info: Face #3 -> Edge #9 (9) Internally in Loop 7 4, sen = 1!
 1E2491C40 EGADS Info: Face #5 -> Edge #17 (9) Internally in Loop 7 4, sen = -1!
 1E2491C40 EGADS Info: Face #5 -> 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
 1E2491C40 EGADS Info: Face #3 -> Edge #9 (9) Internally in Loop 4 7, sen = -1!
 1E2491C40 EGADS Info: Face #3 -> Edge #9 (9) Internally in Loop 7 4, sen = 1!
 1740EF000 EGADS Info: Face #5 -> Edge #17 (9) Internally in Loop 7 4, sen = -1!
 1740EF000 EGADS Info: Face #5 -> 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 = 3
	Name = Farfield, index = 1
	Name = Wing1, index = 2
	Name = trailingEdge, index = 3
ok
test_journal (test_egadsTess.TestEGADS.test_journal) ... ERROR:: BAD STATUS = -276 from matsol (called from solveSketchOrig:61955)
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:61955)
ERROR:: BAD STATUS = -276 from matsol (called from solveSketchOrig:61955)
 CAPS Info: Hit last success -- going live!
ERROR:: BAD STATUS = -276 from matsol (called from solveSketchOrig:61955)
 CAPS Info: Hit last success -- going live!
ERROR:: BAD STATUS = -276 from matsol (called from solveSketchOrig:61955)
 CAPS Info: Hit last success -- going live!
ERROR:: BAD STATUS = -276 from matsol (called from solveSketchOrig:61955)
 CAPS Info: Hit last success -- going live!
ERROR:: BAD STATUS = -276 from matsol (called from solveSketchOrig:61955)
 CAPS Info: Hit last success -- going live!
ERROR:: BAD STATUS = -276 from matsol (called from solveSketchOrig:61955)
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:61955)
 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:61955)
 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:61955)
 CAPS Info: Hit last success -- going live!
ERROR:: BAD STATUS = -276 from matsol (called from solveSketchOrig:61955)
 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:61955)
 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:61955)
 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:61955)
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:61955)
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:61955)
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 = 3
	Name = Farfield, index = 1
	Name = Wing1, index = 2
	Name = trailingEdge, index = 3

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 = 3
	Name = Farfield, index = 1
	Name = Wing1, index = 2
	Name = trailingEdge, index = 3

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    = 7800
Number of elements = 15596
Number of triangle elements      = 15596
Number of quadrilateral elements = 0
Body 2 (of 3)
Number of nodes    = 5906
Number of elements = 11808
Number of triangle elements      = 11808
Number of quadrilateral elements = 0
Body 3 (of 3)
Number of nodes    = 542
Number of elements = 1080
Number of triangle elements      = 1080
Number of quadrilateral elements = 0
----------------------------
Total number of nodes    = 14248
Total number of elements = 28484
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 - 14248, elements - 28484
Getting volume mesh

Generating volume mesh using TetGen.....

Tetgen input string = pYq1.500/0.000T1.00e-16A
Delaunizing vertices...
Delaunay seconds:  0.09112
Creating surface mesh ...
Surface mesh seconds:  0.011987
Recovering boundaries...
Boundary recovery seconds:  0.062298
Removing exterior tetrahedra ...
Spreading region attributes.
Exterior tets removal seconds:  0.019192
Recovering Delaunayness...
Delaunay recovery seconds:  0.035647
Refining mesh...
  18992 insertions, added 13405 points, 688228 tetrahedra in queue.
  6324 insertions, added 2619 points, 589108 tetrahedra in queue.
  8430 insertions, added 2014 points, 124223 tetrahedra in queue.
Refinement seconds:  1.12267
Smoothing vertices...
Mesh smoothing seconds:  0.933787
Improving mesh...
Mesh improvement seconds:  0.025642

Writing nodes.
Writing elements.
Writing faces.
Writing edges.

Output seconds:  0.005433
Total running seconds:  2.30808

Statistics:

  Input points: 14248
  Input facets: 28484
  Input segments: 42726
  Input holes: 2
  Input regions: 0

  Mesh points: 33028
  Mesh tetrahedra: 159264
  Mesh faces: 332770
  Mesh faces on exterior boundary: 28484
  Mesh faces on input facets: 28484
  Mesh edges on input segments: 42726
  Steiner points inside domain: 18780

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    = 7800
Number of elements = 15596
Number of triangle elements      = 15596
Number of quadrilateral elements = 0
Body 2 (of 3)
Number of nodes    = 5906
Number of elements = 11808
Number of triangle elements      = 11808
Number of quadrilateral elements = 0
Body 3 (of 3)
Number of nodes    = 542
Number of elements = 1080
Number of triangle elements      = 1080
Number of quadrilateral elements = 0
----------------------------
Total number of nodes    = 14248
Total number of elements = 28484
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 - 14248, elements - 28484
Getting volume mesh

Generating volume mesh using TetGen.....

Tetgen input string = pYq1.500/0.000T1.00e-16A
Delaunizing vertices...
Delaunay seconds:  0.091661
Creating surface mesh ...
Surface mesh seconds:  0.012561
Recovering boundaries...
Boundary recovery seconds:  0.062103
Removing exterior tetrahedra ...
Spreading region attributes.
Exterior tets removal seconds:  0.019175
Recovering Delaunayness...
Delaunay recovery seconds:  0.036284
Refining mesh...
  18992 insertions, added 13405 points, 688228 tetrahedra in queue.
  6324 insertions, added 2619 points, 589108 tetrahedra in queue.
  8430 insertions, added 2014 points, 124223 tetrahedra in queue.
Refinement seconds:  1.122
Smoothing vertices...
Mesh smoothing seconds:  0.930479
Improving mesh...
Mesh improvement seconds:  0.025187

Writing nodes.
Writing elements.
Writing faces.
Writing edges.

Output seconds:  0.005927
Total running seconds:  2.30571

Statistics:

  Input points: 14248
  Input facets: 28484
  Input segments: 42726
  Input holes: 2
  Input regions: 0

  Mesh points: 33028
  Mesh tetrahedra: 159264
  Mesh faces: 332770
  Mesh faces on exterior boundary: 28484
  Mesh faces on input facets: 28484
  Mesh edges on input segments: 42726
  Steiner points inside domain: 18780

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/ESPbeta/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/ESPbeta/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/ESPbeta/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 - 5097, elements - 10182
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 - 5097, elements - 10182
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 - 14248, elements - 28484
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
===> 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
===> 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
===> 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
===> 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
===> 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
===> 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
===> 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
===> 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
===> 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
===> 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
===> 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
===> 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
===> 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
===> 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
===> 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
===> 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
===> 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
===> 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
===> 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
===> 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
===> 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
===> 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
===> 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
===> 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
===> 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
===> 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
===> 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
===> 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
===> 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
===> 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
===> 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
===> 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
===> 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
===> 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
===> 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 9.17.15
AFLR2    : Version Date   04/23/24 @ 12:51AM
AFLR2    : Compile OS     Darwin 23.4.0 arm64
AFLR2    : Compile Date   04/23/24 @ 12:51AM
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 9.17.15
AFLR2    : Version Date   04/23/24 @ 12:51AM
AFLR2    : Compile OS     Darwin 23.4.0 arm64
AFLR2    : Compile Date   04/23/24 @ 12:51AM
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 11.5.14
AFLR4    : Version Date   04/18/24 @ 12:45PM
AFLR4    : Compile OS     Darwin 23.4.0 arm64
AFLR4    : Compile Date   04/18/24 @ 03:04PM
AFLR4    : Copyright 1994-2021, D.L. Marcum
AFLR4    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------
Volume mesh:
	Number of nodes          = 1579
	Number of elements       = 8634
	Number of triangles      = 1240
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 7394
	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 1.25
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.8.0
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 1.25
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.8.0
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 = 3
	Name = Farfield, index = 1
	Name = Wing1, index = 2
	Name = trailingEdge, index = 3
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 3
	Name = Farfield, index = 1
	Name = Wing1, index = 2
	Name = trailingEdge, index = 3
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 1.25
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------
Volume mesh:
	Number of nodes          = 15766
	Number of elements       = 90668
	Number of triangles      = 4632
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 86036
	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 1.25
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------
Volume mesh:
	Number of nodes          = 1579
	Number of elements       = 8634
	Number of triangles      = 1240
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 7394
	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 1.25
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.8.0
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 1.25
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.8.0
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 9.17.15
AFLR2    : Version Date   04/23/24 @ 12:51AM
AFLR2    : Compile OS     Darwin 23.4.0 arm64
AFLR2    : Compile Date   04/23/24 @ 12:51AM
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 11.5.14
AFLR4    : Version Date   04/18/24 @ 12:45PM
AFLR4    : Compile OS     Darwin 23.4.0 arm64
AFLR4    : Compile Date   04/18/24 @ 03:04PM
AFLR4    : Copyright 1994-2021, D.L. Marcum
AFLR4    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.8.0
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       11.5089842                0    0.00183652568
EGADS    :     11     Yes         12.36195       2.82842712                0
EGADS    :     12     Yes               10                0                0
EGADS    :     13     Yes       11.6329932       2.82842712     0.0493703791
EGADS    :     14     Yes       11.5080047                0                0
EGADS    :     15     Yes       12.3611301       2.82842712                0
EGADS    :     16     Yes         12.36195                0                0
EGADS    :     17     Yes       11.6329932                0     0.0493703791
EGADS    :     18     Yes       12.3611301                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 = 14.1421
AFLR4    : Min Ref Bounding Box Length = 0.890888
AFLR4    : Reference Length            = 0.890888
AFLR4    : BL Thickness                = 0
AFLR4    : FarField Spacing            = 15.6122
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=     12428
AFLR43   : Nodes             =      6220
 
 
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   =      6220         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   =      6220         0
AFLR3 IG : Nodes, Elements   =         8        10
AFLR3 IG : Nodes, Elements   =      1246      7333
AFLR3 IG : Nodes, Elements   =      2492     16261
AFLR3 IG : Nodes, Elements   =      3738     25026
AFLR3 IG : Nodes, Elements   =      4984     34312
AFLR3 IG : Nodes, Elements   =      6227     43517
AFLR3 IG : Nodes, Elements   =      6227     43439
AFLR3 IG : Nodes, Elements   =      6227     43476
AFLR3 IG : Nodes, Elements   =      6227     43444
AFLR3 IG : Nodes, Elements   =      6220     26114
AFLR3 IG : Nodes, Elements   =      6220     26132
AFLR3 IG : Nodes, Elements   =      6220     21569
AFLR3 IG : Nodes, Elements   =      6220     19193
 
AFLR3    : CPU Time          =     0.081   seconds
 
AFLR3 GG : ISOTROPIC VOLUME GRID GENERATION
 
AFLR3 GG : Nodes, Elements   =      6220     19193
AFLR3 GG : Nodes, Elements   =      9101     28053
AFLR3 GG : Nodes, Elements   =      9101     39640
AFLR3 GG : Nodes, Elements   =      9101     36690
AFLR3 GG : Nodes, Elements   =      9101     35155
AFLR3 GG : Nodes, Elements   =     11687     43216
AFLR3 GG : Nodes, Elements   =     11687     54497
AFLR3 GG : Nodes, Elements   =     11687     51170
AFLR3 GG : Nodes, Elements   =     11687     50185
AFLR3 GG : Nodes, Elements   =     14519     58970
AFLR3 GG : Nodes, Elements   =     14519     71103
AFLR3 GG : Nodes, Elements   =     14519     67722
AFLR3 GG : Nodes, Elements   =     14519     66894
AFLR3 GG : Nodes, Elements   =     17597     76360
AFLR3 GG : Nodes, Elements   =     17597     89686
AFLR3 GG : Nodes, Elements   =     17597     86040
AFLR3 GG : Nodes, Elements   =     17597     85134
AFLR3 GG : Nodes, Elements   =     20802     94942
AFLR3 GG : Nodes, Elements   =     20802    108532
AFLR3 GG : Nodes, Elements   =     20802    104847
AFLR3 GG : Nodes, Elements   =     20802    104019
AFLR3 GG : Nodes, Elements   =     24174    114290
AFLR3 GG : Nodes, Elements   =     24174    128631
AFLR3 GG : Nodes, Elements   =     24174    124801
AFLR3 GG : Nodes, Elements   =     24174    123982
AFLR3 GG : Nodes, Elements   =     27742    134809
AFLR3 GG : Nodes, Elements   =     27742    150037
AFLR3 GG : Nodes, Elements   =     27742    145948
AFLR3 GG : Nodes, Elements   =     27742    145081
AFLR3 GG : Nodes, Elements   =     31383    156143
AFLR3 GG : Nodes, Elements   =     31383    171588
AFLR3 GG : Nodes, Elements   =     31383    167421
AFLR3 GG : Nodes, Elements   =     31383    166536
AFLR3 GG : Nodes, Elements   =     35115    177837
AFLR3 GG : Nodes, Elements   =     35115    193748
AFLR3 GG : Nodes, Elements   =     35115    189548
AFLR3 GG : Nodes, Elements   =     35115    188723
AFLR3 GG : Nodes, Elements   =     38948    200319
AFLR3 GG : Nodes, Elements   =     38948    216342
AFLR3 GG : Nodes, Elements   =     38948    212298
AFLR3 GG : Nodes, Elements   =     38948    211481
AFLR3 GG : Nodes, Elements   =     42740    222940
AFLR3 GG : Nodes, Elements   =     42740    239184
AFLR3 GG : Nodes, Elements   =     42740    234883
AFLR3 GG : Nodes, Elements   =     42740    234060
AFLR3 GG : Nodes, Elements   =     46416    245151
AFLR3 GG : Nodes, Elements   =     46416    260680
AFLR3 GG : Nodes, Elements   =     46416    256642
AFLR3 GG : Nodes, Elements   =     46416    255866
AFLR3 GG : Nodes, Elements   =     50035    266777
AFLR3 GG : Nodes, Elements   =     50035    281993
AFLR3 GG : Nodes, Elements   =     50035    278055
AFLR3 GG : Nodes, Elements   =     50035    277383
AFLR3 GG : Nodes, Elements   =     53591    288088
AFLR3 GG : Nodes, Elements   =     53591    303095
AFLR3 GG : Nodes, Elements   =     53591    299307
AFLR3 GG : Nodes, Elements   =     53591    298569
AFLR3 GG : Nodes, Elements   =     57005    308827
AFLR3 GG : Nodes, Elements   =     57005    323244
AFLR3 GG : Nodes, Elements   =     57005    319601
AFLR3 GG : Nodes, Elements   =     57005    318957
AFLR3 GG : Nodes, Elements   =     60293    328832
AFLR3 GG : Nodes, Elements   =     60293    342689
AFLR3 GG : Nodes, Elements   =     60293    339197
AFLR3 GG : Nodes, Elements   =     60293    338647
AFLR3 GG : Nodes, Elements   =     63359    347851
AFLR3 GG : Nodes, Elements   =     63359    360783
AFLR3 GG : Nodes, Elements   =     63359    357437
AFLR3 GG : Nodes, Elements   =     63359    356932
AFLR3 GG : Nodes, Elements   =     66259    365641
AFLR3 GG : Nodes, Elements   =     66259    377775
AFLR3 GG : Nodes, Elements   =     66259    374741
AFLR3 GG : Nodes, Elements   =     66259    374315
AFLR3 GG : Nodes, Elements   =     68879    382177
AFLR3 GG : Nodes, Elements   =     68879    393099
AFLR3 GG : Nodes, Elements   =     68879    390371
AFLR3 GG : Nodes, Elements   =     68879    390020
AFLR3 GG : Nodes, Elements   =     71152    396844
AFLR3 GG : Nodes, Elements   =     71152    406357
AFLR3 GG : Nodes, Elements   =     71152    403836
AFLR3 GG : Nodes, Elements   =     71152    403561
AFLR3 GG : Nodes, Elements   =     73068    409315
AFLR3 GG : Nodes, Elements   =     73068    417362
AFLR3 GG : Nodes, Elements   =     73068    415318
AFLR3 GG : Nodes, Elements   =     73068    415069
AFLR3 GG : Nodes, Elements   =     74529    419454
AFLR3 GG : Nodes, Elements   =     74529    425587
AFLR3 GG : Nodes, Elements   =     74529    423928
AFLR3 GG : Nodes, Elements   =     74529    423776
AFLR3 GG : Nodes, Elements   =     75631    427084
AFLR3 GG : Nodes, Elements   =     75631    431714
AFLR3 GG : Nodes, Elements   =     75631    430512
AFLR3 GG : Nodes, Elements   =     75631    430423
AFLR3 GG : Nodes, Elements   =     76419    432787
AFLR3 GG : Nodes, Elements   =     76419    436211
AFLR3 GG : Nodes, Elements   =     76419    435175
AFLR3 GG : Nodes, Elements   =     76419    435106
AFLR3 GG : Nodes, Elements   =     76934    436651
AFLR3 GG : Nodes, Elements   =     76934    438851
AFLR3 GG : Nodes, Elements   =     76934    438238
AFLR3 GG : Nodes, Elements   =     76934    438198
AFLR3 GG : Nodes, Elements   =     77241    439119
AFLR3 GG : Nodes, Elements   =     77241    440474
AFLR3 GG : Nodes, Elements   =     77241    440052
AFLR3 GG : Nodes, Elements   =     77241    440022
AFLR3 GG : Nodes, Elements   =     77416    440547
AFLR3 GG : Nodes, Elements   =     77416    441274
AFLR3 GG : Nodes, Elements   =     77416    441066
AFLR3 GG : Nodes, Elements   =     77416    441056
AFLR3 GG : Nodes, Elements   =     77509    441335
AFLR3 GG : Nodes, Elements   =     77509    441739
AFLR3 GG : Nodes, Elements   =     77509    441625
AFLR3 GG : Nodes, Elements   =     77509    441612
AFLR3 GG : Nodes, Elements   =     77549    441732
AFLR3 GG : Nodes, Elements   =     77549    441904
AFLR3 GG : Nodes, Elements   =     77549    441849
AFLR3 GG : Nodes, Elements   =     77549    441848
AFLR3 GG : Nodes, Elements   =     77559    441878
AFLR3 GG : Nodes, Elements   =     77559    441913
AFLR3 GG : Nodes, Elements   =     77559    441902
AFLR3 GG : Nodes, Elements   =     77564    441917
AFLR3 GG : Nodes, Elements   =     77564    441932
AFLR3 GG : Nodes, Elements   =     77564    441928
AFLR3 GG : Nodes, Elements   =     77565    441931
AFLR3 GG : Nodes, Elements   =     77565    441938
AFLR3 GG : Nodes, Elements   =     77565    441933
AFLR3 GG : Nodes, Elements   =     77595    442023
AFLR3 GG : Nodes, Elements   =     77595    442128
AFLR3 GG : Nodes, Elements   =     77595    442098
AFLR3 GG : Nodes, Elements   =     77595    442094
AFLR3 GG : Nodes, Elements   =     77599    442106
AFLR3 GG : Nodes, Elements   =     77599    442119
AFLR3 GG : Nodes, Elements   =     77599    442116
AFLR3 GG : Nodes, Elements   =     77599    442115
AFLR3 GG : Nodes, Elements   =     77600    442118
AFLR3 GG : Nodes, Elements   =     77600    442125
AFLR3 GG : Nodes, Elements   =     77600    442121
 
AFLR3    : CPU Time          =     2.336   seconds
 
AFLR3 QI : QUALITY IMPROVEMENT
 
AFLR3 QI : Nodes, Elements   =     77600    442121
AFLR3 QI : Nodes, Elements   =     76105    433678
AFLR3 QI : Nodes, Elements   =     75842    432198
AFLR3 QI : Nodes, Elements   =     75829    432123
AFLR3 QI : Nodes, Elements   =     75827    432113
AFLR3 QI : Nodes, Elements   =     75826    432107
AFLR3 QI : Nodes, Elements   =     75826    436049
AFLR3 QI : Nodes, Elements   =     75826    431912
AFLR3 QI : Nodes, Elements   =     75826    431430
AFLR3 QI : Nodes, Elements   =     75826    431831
AFLR3 QI : Nodes, Elements   =     75826    431146
AFLR3 QI : Nodes, Elements   =     75826    430921
AFLR3 QI : Nodes, Elements   =     75826    431306
AFLR3 QI : Nodes, Elements   =     75826    430921
AFLR3 QI : Nodes, Elements   =     75826    430900
AFLR3 QI : Nodes, Elements   =     75826    431192
AFLR3 QI : Nodes, Elements   =     75826    430885
AFLR3 QI : Nodes, Elements   =     75826    430832
AFLR3 QI : Nodes, Elements   =     75826    431117
AFLR3 QI : Nodes, Elements   =     75826    430836
AFLR3 QI : Nodes, Elements   =     75826    430821
AFLR3 QI : Nodes, Elements   =     75831    430843
AFLR3 QI : Nodes, Elements   =     75831    431136
AFLR3 QI : Nodes, Elements   =     75831    430863
AFLR3 QI : Nodes, Elements   =     75831    430845
AFLR3 QI : Nodes, Elements   =     75831    431106
AFLR3 QI : Nodes, Elements   =     75831    430850
AFLR3 QI : Nodes, Elements   =     75831    430821
 
AFLR3    : CPU Time          =     0.796   seconds
 
AFLR3 QRG: QUALITY GRID RE-GENERATION
 
AFLR3 QRG: Nodes, Elements   =     75831    430821
AFLR3 QRG: Nodes, Elements   =     75839    430867
AFLR3 QRG: Nodes, Elements   =     75842    430887
AFLR3 QRG: Nodes, Elements   =     75841    430884
AFLR3 QRG: Nodes, Elements   =     75841    430883
AFLR3 QRG: Nodes, Elements   =     75848    430923
AFLR3 QRG: Nodes, Elements   =     75847    430916
 
AFLR3    : CPU Time          =     0.031   seconds
 
AFLR3    : DONE

UG3      : DIHEDRAL ANGLE CHECK

UG3      : No. Tet Elems     =    430916
UG3      : Min, Max Ang      =     1.198     173.5
UG3      : Average Angle     =      70.2
UG3      : No. Angle>160.0   =        54
UG3      : No. Angle>179.9   =         0

UG3      : VOL CHECK

UG3      : Total-Volume      =  2.12e+06

UG3      : No. Tet Elems     =    430916
UG3      : Min Vol           =  6.52e-10
UG3      : Average Vol       =      4.92
UG3      : Total-Tet-Vol     =  2.12e+06
UG3      : No. Vol<TOL       =         0

UG3      : Q VOL-LENGTH-RATIO CHECK
                      2/3        2
UG3      : Q = c * Vol   / sum( L  )
UG3      : 0 <= Q <= 1

UG3      : No. Tet Elems     =    430916
UG3      : Min, Max Q        =     0.073         1
UG3      : Average Q         =     0.892
UG3      : No. Q<       0.1  =        27
UG3      : No. Q<      0.01  =         0

OVERALL  : CPU Time          =     3.453   seconds

UG3      : DIHEDRAL ANGLE CHECK

UG3      : No. Tet Elems     =    430916
UG3      : Min, Max Ang      =     1.198     173.5
UG3      : Average Angle     =      70.2
UG3      : No. Angle>160.0   =        54
UG3      : No. Angle>179.9   =         0

UG3      : VOL CHECK

UG3      : Total-Volume      =  2.12e+06

UG3      : No. Tet Elems     =    430916
UG3      : Min Vol           =  6.52e-10
UG3      : Average Vol       =      4.92
UG3      : Total-Tet-Vol     =  2.12e+06
UG3      : No. Vol<TOL       =         0

UG3      : Q VOL-LENGTH-RATIO CHECK
                      2/3        2
UG3      : Q = c * Vol   / sum( L  )
UG3      : 0 <= Q <= 1
UG3      : Note that L includes scaling for BL-aspect=ratio

UG3      : No. Tet Elems     =    430916
UG3      : Min, Max Q        =     0.189         1
UG3      : Average Q         =      0.85
UG3      : No. Q<       0.1  =         0
UG3      : No. Q<      0.01  =         0

UG3      : CPU Time          =     0.000   seconds

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.8.0
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          = 75847
	Number of elements       = 443344
	Number of triangles      = 12428
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 430916
	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 1.25
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------
Volume mesh:
	Number of nodes          = 75847
	Number of elements       = 443344
	Number of triangles      = 12428
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 430916
	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 1.25
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------
Volume mesh:
	Number of nodes          = 75847
	Number of elements       = 443344
	Number of triangles      = 12428
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 430916
	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 1.25
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------
Volume mesh:
	Number of nodes          = 75847
	Number of elements       = 443344
	Number of triangles      = 12428
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 430916
	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:61955)
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)
 1E2491C40 EGADS Info: Face #3 -> Edge #9 (9) Internally in Loop 4 7, sen = -1!
 1740EF000 EGADS Info: Face #5 -> Edge #17 (9) Internally in Loop 7 4, sen = -1!
 1E2491C40 EGADS Info: Face #3 -> Edge #9 (9) Internally in Loop 7 4, sen = 1!
 1740EF000 EGADS Info: Face #5 -> 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 = 3
	Name = Farfield, index = 1
	Name = Wing1, index = 2
	Name = trailingEdge, index = 3

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 - 9583, elements - 19158
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 - 9583, elements - 19158
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 = 3
	Name = Farfield, index = 1
	Name = Wing1, index = 2
	Name = trailingEdge, index = 3

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 - 9583, elements - 19158
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 = 3
	Name = Farfield, index = 1
	Name = Wing1, index = 2
	Name = trailingEdge, index = 3

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 = 3
	Name = Farfield, index = 1
	Name = Wing1, index = 2
	Name = trailingEdge, index = 3

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 = 3
	Name = Farfield, index = 1
	Name = Wing1, index = 2
	Name = trailingEdge, index = 3

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 - 9583, elements - 19158
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 = 3
	Name = Farfield, index = 1
	Name = Wing1, index = 2
	Name = trailingEdge, index = 3

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 = 3
	Name = Farfield, index = 1
	Name = Wing1, index = 2
	Name = trailingEdge, index = 3

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 - 9583, elements - 19158
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 = 3
	Name = Farfield, index = 1
	Name = Wing1, index = 2
	Name = trailingEdge, index = 3

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 = 3
	Name = Farfield, index = 1
	Name = Wing1, index = 2
	Name = trailingEdge, index = 3

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!
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 = 3
	Name = Farfield, index = 1
	Name = Wing1, index = 2
	Name = trailingEdge, index = 3

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    = 9583
Number of elements = 19158
Number of triangle elements      = 19158
Number of quadrilateral elements = 0
----------------------------
Total number of nodes    = 9583
Total number of elements = 19158
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 2
	Name = Farfield, index = 1
	Name = Wing1, index = 2
Number of surface: nodes - 9583, elements - 19158
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 - 9583, elements - 19158
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_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 -> [0.345898, 1.652951, -0.041403]
	- weight -> 476456.149985
	- weightMomentOfInertia -> [304902.643270, 98963.803823, 69822.813293, 6179.981375, 19723.152208, 370546.335525]
ok

----------------------------------------------------------------------
Ran 143 tests in 400.421s

OK (skipped=10)
+ cd /Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/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/ESPbeta/EngSketchPad/CAPSexamples/regressionTest/cCAPSlog.txt
./avlTest test;
+ ./avlTest 0
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/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	0m0.427s
user	0m0.264s
sys	0m0.076s
+ status=0
+ set +x

=============================================
CAPS verification (using c-executables) case ./avlTest passed (as expected)
=============================================


=================================================
+ echo './msesTest test;'
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/EngSketchPad/CAPSexamples/regressionTest/cCAPSlog.txt
./msesTest test;
+ ./msesTest 0
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/EngSketchPad/CAPSexamples/regressionTest/cCAPSlog.txt


Attention: msesTest is hard coded to look for ../csmData/airfoilSection.csm

Value of CL = 0.276892 

real	0m1.235s
user	0m1.112s
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/ESPbeta/EngSketchPad/CAPSexamples/regressionTest/cCAPSlog.txt
./frictionTest test;
+ ./frictionTest 0
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/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 , >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	0m0.401s
user	0m0.163s
sys	0m0.026s
+ 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/ESPbeta/EngSketchPad/CAPSexamples/regressionTest/cCAPSlog.txt
./fun3dAFLR2Test test;
+ ./fun3dAFLR2Test 0
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/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 9.17.15
AFLR2    : Version Date   04/23/24 @ 12:51AM
AFLR2    : Compile OS     Darwin 23.4.0 arm64
AFLR2    : Compile Date   04/23/24 @ 12:51AM
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	0m0.845s
user	0m0.643s
sys	0m0.347s
+ status=0
+ set +x

=============================================
CAPS verification (using c-executables) case ./fun3dAFLR2Test passed (as expected)
=============================================


=================================================
+ echo './fun3dTetgenTest test;'
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/EngSketchPad/CAPSexamples/regressionTest/cCAPSlog.txt
./fun3dTetgenTest test;
+ ./fun3dTetgenTest 0
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/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:  0.097041
Creating surface mesh ...
Surface mesh seconds:  0.02308
Recovering boundaries...
Boundary recovery seconds:  0.072249
Removing exterior tetrahedra ...
Spreading region attributes.
Exterior tets removal seconds:  0.020816
Recovering Delaunayness...
Delaunay recovery seconds:  0.040843
Refining mesh...
  21316 insertions, added 16799 points, 789925 tetrahedra in queue.
  7098 insertions, added 2909 points, 350791 tetrahedra in queue.
Refinement seconds:  0.788714
Smoothing vertices...
Mesh smoothing seconds:  1.05045
Improving mesh...
Mesh improvement seconds:  0.028816

Writing nodes.
Writing elements.
Writing faces.
Writing edges.

Output seconds:  0.004582
Total running seconds:  2.12687

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	0m3.850s
user	0m4.277s
sys	0m0.113s
+ 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/ESPbeta/EngSketchPad/CAPSexamples/regressionTest/cCAPSlog.txt
./interferenceTest test;
+ ./interferenceTest
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/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	0m2.243s
user	0m3.879s
sys	0m0.044s
+ status=0
+ set +x

=============================================
CAPS verification (using c-executables) case ./interferenceTest passed (as expected)
=============================================


=================================================
+ echo './hsmCantileverPlateTest test;'
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/EngSketchPad/CAPSexamples/regressionTest/cCAPSlog.txt
./hsmCantileverPlateTest test;
+ ./hsmCantileverPlateTest 0
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/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
->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	0m0.434s
user	0m0.235s
sys	0m0.026s
+ status=0
+ set +x

=============================================
CAPS verification (using c-executables) case ./hsmCantileverPlateTest passed (as expected)
=============================================


=================================================
+ echo './hsmSimplePlateTest test;'
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/EngSketchPad/CAPSexamples/regressionTest/cCAPSlog.txt
./hsmSimplePlateTest test;
+ ./hsmSimplePlateTest 0
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/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
->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	0m0.493s
user	0m0.408s
sys	0m0.025s
+ status=0
+ set +x

=============================================
CAPS verification (using c-executables) case ./hsmSimplePlateTest passed (as expected)
=============================================


=================================================
+ echo './hsmJoinedPlateTest test;'
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/EngSketchPad/CAPSexamples/regressionTest/cCAPSlog.txt
./hsmJoinedPlateTest test;
+ ./hsmJoinedPlateTest 0
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/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
->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	0m0.314s
user	0m0.209s
sys	0m0.027s
+ 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/ESPbeta/Python-3.11.9/bin/python
=================================================

No options provided...defaulting to ALL
Running.... LINEARAERO PyTests

avl: /Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/EngSketchPad/bin/avl

=================================================
+ echo 'avl_PyTest.py test;'
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
avl_PyTest.py test;
+ python -u avl_PyTest.py -outLevel=0
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/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	0m0.473s
user	0m0.595s
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/ESPbeta/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/ESPbeta/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	0m5.896s
user	0m6.113s
sys	0m5.373s
+ 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/ESPbeta/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/ESPbeta/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	0m16.815s
user	0m8.531s
sys	0m8.277s
+ 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/ESPbeta/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/ESPbeta/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	0m0.562s
user	0m0.667s
sys	0m0.202s
+ 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/ESPbeta/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/ESPbeta/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	0m0.469s
user	0m0.596s
sys	0m0.182s
+ 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/ESPbeta/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/ESPbeta/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
	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_<=_FACTR*EPSMCH             
Optimization Complete
-----------------------------------
Optimized values: [-5.50424967] [2.89504288]

real	0m13.665s
user	0m4.350s
sys	0m0.864s
+ status=0
+ set +x

=================================================
CAPS verification (using pyCAPS) case avl_OpenMDAO_3_PyTest.py passed (as expected)
=================================================

friction: /Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/EngSketchPad/bin/friction

=================================================
+ echo 'friction_PyTest.py test;'
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
friction_PyTest.py test;
+ python -u friction_PyTest.py -outLevel=0
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
Loading AIM
Setting Mach & 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	0m0.303s
user	0m0.391s
sys	0m0.073s
+ 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/ESPbeta/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
tsfoil_PyTest.py test;
+ python -u tsfoil_PyTest.py -outLevel=0
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/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 =  0.933407
Cd =  0.000284
Cd Wave =  0.0
Cm =  -0.203436
Cp _Critcal =  -1.303869

real	0m0.358s
user	0m0.459s
sys	0m0.060s
+ status=0
+ set +x

=================================================
CAPS verification (using pyCAPS) case tsfoil_PyTest.py passed (as expected)
=================================================

mses: /Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/EngSketchPad/bin/mses

=================================================
+ echo 'mses_PyTest.py test;'
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
mses_PyTest.py test;
+ python -u mses_PyTest.py -outLevel=0 -noPlotData
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
Cl =  0.3783791085548177
Cd =  0.007775858417209677
Cm =  0.005262636995835036

real	0m1.906s
user	0m2.117s
sys	0m0.092s
+ 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/ESPbeta/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/ESPbeta/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt

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_<=_FACTR*EPSMCH             
Optimization Complete
-----------------------------------
Optimized values: [-0.00019629]

real	0m14.136s
user	0m14.186s
sys	0m0.338s
+ status=0
+ set +x

=================================================
CAPS verification (using pyCAPS) case mses_OpenMDAO_3_PyTest.py passed (as expected)
=================================================

xfoil: /Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/EngSketchPad/bin/xfoil

=================================================
+ echo 'xfoil_PyTest.py test;'
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
xfoil_PyTest.py test;
+ python -u xfoil_PyTest.py -outLevel=0 -noPlotData
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/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	0m1.981s
user	0m2.212s
sys	0m0.075s
+ 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/ESPbeta/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
egadsTess_PyTest.py test;
+ python -u egadsTess_PyTest.py -outLevel=0
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/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	0m3.951s
user	0m10.498s
sys	0m6.098s
+ 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/ESPbeta/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/ESPbeta/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	0m2.133s
user	0m2.670s
sys	0m0.052s
+ 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/ESPbeta/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/ESPbeta/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	0m4.910s
user	0m7.764s
sys	0m0.128s
+ 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/ESPbeta/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/ESPbeta/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	0m1.852s
user	0m2.228s
sys	0m0.078s
+ 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/ESPbeta/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
aflr2_PyTest.py test;
+ python -u aflr2_PyTest.py -outLevel=0
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/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 9.17.15
AFLR2    : Version Date   04/23/24 @ 12:51AM
AFLR2    : Compile OS     Darwin 23.4.0 arm64
AFLR2    : Compile Date   04/23/24 @ 12:51AM
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	0m0.464s
user	0m0.701s
sys	0m0.367s
+ 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/ESPbeta/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
aflr4_PyTest.py test;
+ python -u aflr4_PyTest.py -outLevel=0
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/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

Writing Tecplot file ....
Finished writing Tecplot file


Writing ASCII STL file ....
Finished writing ASCII STL file


Writing ugrid file ....
Finished writing ugrid file


real	0m0.725s
user	0m0.931s
sys	0m0.102s
+ 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/ESPbeta/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/ESPbeta/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	0m1.247s
user	0m1.445s
sys	0m0.273s
+ 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/ESPbeta/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/ESPbeta/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	0m3.752s
user	0m6.976s
sys	0m0.321s
+ 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/ESPbeta/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/ESPbeta/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	0m4.801s
user	0m4.926s
sys	0m0.170s
+ 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/ESPbeta/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/ESPbeta/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 9.17.15
AFLR2    : Version Date   04/23/24 @ 12:51AM
AFLR2    : Compile OS     Darwin 23.4.0 arm64
AFLR2    : Compile Date   04/23/24 @ 12:51AM
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 11.5.14
AFLR4    : Version Date   04/18/24 @ 12:45PM
AFLR4    : Compile OS     Darwin 23.4.0 arm64
AFLR4    : Compile Date   04/18/24 @ 03:04PM
AFLR4    : Copyright 1994-2021, D.L. Marcum
AFLR4    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.8.0
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	0m6.763s
user	0m6.845s
sys	0m0.208s
+ 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/ESPbeta/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/ESPbeta/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 9.17.15
AFLR2    : Version Date   04/23/24 @ 12:51AM
AFLR2    : Compile OS     Darwin 23.4.0 arm64
AFLR2    : Compile Date   04/23/24 @ 12:51AM
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 11.5.14
AFLR4    : Version Date   04/18/24 @ 12:45PM
AFLR4    : Compile OS     Darwin 23.4.0 arm64
AFLR4    : Compile Date   04/18/24 @ 03:04PM
AFLR4    : Copyright 1994-2021, D.L. Marcum
AFLR4    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.8.0
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	0m14.650s
user	0m14.614s
sys	0m0.481s
+ 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/ESPbeta/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/ESPbeta/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	0m4.113s
user	0m10.670s
sys	0m5.096s
+ 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/ESPbeta/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/ESPbeta/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	0m6.057s
user	0m6.132s
sys	0m0.221s
+ 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/ESPbeta/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/ESPbeta/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 9.17.15
AFLR2    : Version Date   04/23/24 @ 12:51AM
AFLR2    : Compile OS     Darwin 23.4.0 arm64
AFLR2    : Compile Date   04/23/24 @ 12:51AM
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 11.5.14
AFLR4    : Version Date   04/18/24 @ 12:45PM
AFLR4    : Compile OS     Darwin 23.4.0 arm64
AFLR4    : Compile Date   04/18/24 @ 03:04PM
AFLR4    : Copyright 1994-2021, D.L. Marcum
AFLR4    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.8.0
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
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:  0.025353
Creating surface mesh ...
Surface mesh seconds:  0.000746
Recovering boundaries...
Boundary recovery seconds:  0.003919
Removing exterior tetrahedra ...
Spreading region attributes.
Exterior tets removal seconds:  0.000388
Recovering Delaunayness...
Delaunay recovery seconds:  0.000978
Refining mesh...
Refinement seconds:  0.013763
Smoothing vertices...
Mesh smoothing seconds:  0.024728
Improving mesh...
Mesh improvement seconds:  0.001274

Writing nodes.
Writing elements.
Writing faces.
Writing edges.

Output seconds:  0.000144
Total running seconds:  0.071343

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	0m0.417s
user	0m0.603s
sys	0m0.090s
+ 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/ESPbeta/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
tetgen_PyTest.py test;
+ python -u tetgen_PyTest.py -outLevel=0
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/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:  0.013609
Creating surface mesh ...
Surface mesh seconds:  0.001815
Recovering boundaries...
Boundary recovery seconds:  0.041832
Removing exterior tetrahedra ...
Spreading region attributes.
Exterior tets removal seconds:  0.00281
Suppressing Steiner points ...
Steiner suppression seconds:  3e-06
Recovering Delaunayness...
Delaunay recovery seconds:  0.005468
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:  0.372342
Smoothing vertices...
Mesh smoothing seconds:  0.199763
Improving mesh...
Mesh improvement seconds:  0.006467
Jettisoning redundant points.

Writing nodes.
Writing elements.
Writing faces.
Writing edges.

Output seconds:  0.000641
Total running seconds:  0.644888

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	0m1.413s
user	0m1.692s
sys	0m0.129s
+ 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/ESPbeta/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/ESPbeta/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
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:  0.156442
Creating surface mesh ...
Surface mesh seconds:  0.004842
Recovering boundaries...
Boundary recovery seconds:  0.060492
Removing exterior tetrahedra ...
Spreading region attributes.
Exterior tets removal seconds:  0.004242
Recovering Delaunayness...
Delaunay recovery seconds:  0.034869
Refining mesh...
Refinement seconds:  0.142231
Smoothing vertices...
Mesh smoothing seconds:  0.162691
Improving mesh...
Mesh improvement seconds:  0.005492
Jettisoning redundant points.

Writing nodes.
Writing elements.
Writing faces.
Writing edges.

Output seconds:  0.00102
Total running seconds:  0.572553

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 FAST file ....
Finished writing FAST file


real	0m1.273s
user	0m1.498s
sys	0m0.092s
+ 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/ESPbeta/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/ESPbeta/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
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:  0.15765
Creating surface mesh ...
Surface mesh seconds:  0.005894
Recovering boundaries...
Boundary recovery seconds:  0.061857
Removing exterior tetrahedra ...
Spreading region attributes.
Exterior tets removal seconds:  0.003877
Recovering Delaunayness...
Delaunay recovery seconds:  0.067799
Refining mesh...
Refinement seconds:  0.287502
Smoothing vertices...
Mesh smoothing seconds:  0.338179
Improving mesh...
Mesh improvement seconds:  0.010293

Writing nodes.
Writing elements.
Writing faces.
Writing edges.

Output seconds:  0.001386
Total running seconds:  0.934644

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


real	0m1.642s
user	0m1.865s
sys	0m0.093s
+ 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/ESPbeta/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
delaundo_PyTest.py test;
+ python -u delaundo_PyTest.py -outLevel=0
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/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	0m0.483s
user	0m0.658s
sys	0m0.284s
+ 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/ESPbeta/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/ESPbeta/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 9.17.15
AFLR2    : Version Date   04/23/24 @ 12:51AM
AFLR2    : Compile OS     Darwin 23.4.0 arm64
AFLR2    : Compile Date   04/23/24 @ 12:51AM
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: https://su2code.github.io                        |
|                                                                       |
| The SU2 Project is maintained by the SU2 Foundation                   |
| (http://su2foundation.org)                                            |
-------------------------------------------------------------------------
| 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 <http://www.gnu.org/licenses/>.   |
-------------------------------------------------------------------------

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 & 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 https://su2code.github.io/docs_v7/Build-SU2-Linux-MacOS/#compiler-optimizations
WARNING: SU2 was not compiled for an AVX-capable architecture. Performance could be better,
         see https://su2code.github.io/docs_v7/Build-SU2-Linux-MacOS/#compiler-optimizations
WARNING: SU2 was not compiled for an AVX-capable architecture. Performance could be better,
         see https://su2code.github.io/docs_v7/Build-SU2-Linux-MacOS/#compiler-optimizations
+----------------------------------------------------------------------------------------------------------------------------------------------+
|   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|  2.0437e-02|   -0.385358|    2.453598|    1.625650|    5.369499|    0.360138|
|           0|           0|           1|  0.0000e+00|  0.0000e+00|  2.0416e-02|   -0.512634|    2.087781|    1.374671|    4.973554|    1.183036|
|           0|           0|           2|  0.0000e+00|  0.0000e+00|  2.0150e-02|   -0.792582|    1.733529|    1.142729|    4.657622|    3.896320|
|           0|           0|           3|  0.0000e+00|  0.0000e+00|  1.9999e-02|   -0.880738|    1.486539|    1.023158|    4.334759|   14.592265|
|           0|           0|           4|  0.0000e+00|  0.0000e+00|  1.9854e-02|   -0.987528|    1.351478|    0.932491|    4.191092|  111.166022|
|           0|           0|           5|  0.0000e+00|  0.0000e+00|  1.9739e-02|   -1.104038|    1.188715|    0.874764|    3.951825| -483.924340|
|           0|           0|           6|  0.0000e+00|  0.0000e+00|  1.9695e-02|   -1.178622|    1.124587|    0.844310|    3.820426|  127.331200|
|           0|           0|           7|  0.0000e+00|  0.0000e+00|  1.9723e-02|   -1.243517|    1.097463|    0.824869|    3.768858|   40.162273|
|           0|           0|           8|  0.0000e+00|  0.0000e+00|  1.9725e-02|   -1.287932|    1.075843|    0.810639|    3.733440|   25.154653|
|           0|           0|           9|  0.0000e+00|  0.0000e+00|  1.9688e-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|         < -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	0m0.932s
user	0m0.996s
sys	0m0.489s
+ 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/ESPbeta/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/ESPbeta/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 9.17.15
AFLR2    : Version Date   04/23/24 @ 12:51AM
AFLR2    : Compile OS     Darwin 23.4.0 arm64
AFLR2    : Compile Date   04/23/24 @ 12:51AM
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: https://su2code.github.io                        |
|                                                                       |
| The SU2 Project is maintained by the SU2 Foundation                   |
| (http://su2foundation.org)                                            |
-------------------------------------------------------------------------
| 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 <http://www.gnu.org/licenses/>.   |
-------------------------------------------------------------------------

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 & 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 https://su2code.github.io/docs_v7/Build-SU2-Linux-MacOS/#compiler-optimizations
WARNING: SU2 was not compiled for an AVX-capable architecture. Performance could be better,
         see https://su2code.github.io/docs_v7/Build-SU2-Linux-MacOS/#compiler-optimizations
WARNING: SU2 was not compiled for an AVX-capable architecture. Performance could be better,
         see https://su2code.github.io/docs_v7/Build-SU2-Linux-MacOS/#compiler-optimizations
+----------------------------------------------------------------------------------------------------------------------------------------------+
|   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|  5.5566e-02|    0.071067|    2.739763|    1.616077|    5.599701|    0.055267|
|           0|           0|           1|  0.0000e+00|  0.0000e+00|  5.3465e-02|   -0.447576|    2.193837|    1.571349|    5.070382|    0.046028|
|           0|           0|           2|  0.0000e+00|  0.0000e+00|  5.2598e-02|   -0.561159|    2.074597|    1.490746|    4.953698|    0.033910|
|           0|           0|           3|  0.0000e+00|  0.0000e+00|  5.2002e-02|   -0.723326|    1.921155|    1.390756|    4.790278|    0.049695|
|           0|           0|           4|  0.0000e+00|  0.0000e+00|  5.1626e-02|   -0.876572|    1.825653|    1.275093|    4.637161|    0.133976|
|           0|           0|           5|  0.0000e+00|  0.0000e+00|  5.1518e-02|   -1.029177|    1.759196|    1.156078|    4.482282|    0.368542|
|           0|           0|           6|  0.0000e+00|  0.0000e+00|  5.1306e-02|   -1.215334|    1.704909|    1.114966|    4.286060|    0.974759|
|           0|           0|           7|  0.0000e+00|  0.0000e+00|  5.1152e-02|   -1.329970|    1.644937|    1.145030|    4.116982|    2.716332|
|           0|           0|           8|  0.0000e+00|  0.0000e+00|  5.1038e-02|   -1.270672|    1.570739|    1.155400|    4.139480|   16.569216|
|           0|           0|           9|  0.0000e+00|  0.0000e+00|  5.0983e-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|         < -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	0m1.471s
user	0m1.560s
sys	0m0.783s
+ 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/ESPbeta/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/ESPbeta/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 9.17.15
AFLR2    : Version Date   04/23/24 @ 12:51AM
AFLR2    : Compile OS     Darwin 23.4.0 arm64
AFLR2    : Compile Date   04/23/24 @ 12:51AM
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 11.5.14
AFLR4    : Version Date   04/18/24 @ 12:45PM
AFLR4    : Compile OS     Darwin 23.4.0 arm64
AFLR4    : Compile Date   04/18/24 @ 03:04PM
AFLR4    : Copyright 1994-2021, D.L. Marcum
AFLR4    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.8.0
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: https://su2code.github.io                        |
|                                                                       |
| The SU2 Project is maintained by the SU2 Foundation                   |
| (http://su2foundation.org)                                            |
-------------------------------------------------------------------------
| 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 <http://www.gnu.org/licenses/>.   |
-------------------------------------------------------------------------

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 & 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 https://su2code.github.io/docs_v7/Build-SU2-Linux-MacOS/#compiler-optimizations
WARNING: SU2 was not compiled for an AVX-capable architecture. Performance could be better,
         see https://su2code.github.io/docs_v7/Build-SU2-Linux-MacOS/#compiler-optimizations
WARNING: SU2 was not compiled for an AVX-capable architecture. Performance could be better,
         see https://su2code.github.io/docs_v7/Build-SU2-Linux-MacOS/#compiler-optimizations
+----------------------------------------------------------------------------------------------------------------------------------------------+
|   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|  6.1032e-01|   -0.059021|    2.303387|    2.039067|    5.431874|    1.970398|
|           0|           0|           1|  0.0000e+00|  0.0000e+00|  6.0715e-01|    0.002899|    2.488448|    2.194491|    5.502382|    2.658900|
|           0|           0|           2|  0.0000e+00|  0.0000e+00|  6.0534e-01|    0.026727|    2.569164|    2.438598|    5.519932|    4.074903|
|           0|           0|           3|  0.0000e+00|  0.0000e+00|  6.0455e-01|   -0.027928|    2.600852|    2.572666|    5.452520|    6.012667|
|           0|           0|           4|  0.0000e+00|  0.0000e+00|  6.0406e-01|   -0.066798|    2.611567|    2.619922|    5.409363|    7.697173|
|           0|           0|           5|  0.0000e+00|  0.0000e+00|  6.0272e-01|   -0.081876|    2.604321|    2.627463|    5.405669|    8.898085|
|           0|           0|           6|  0.0000e+00|  0.0000e+00|  6.0187e-01|   -0.109417|    2.568028|    2.631615|    5.384249|    9.783851|
|           0|           0|           7|  0.0000e+00|  0.0000e+00|  5.9845e-01|   -0.154243|    2.498102|    2.636523|    5.332167|   10.298250|
|           0|           0|           8|  0.0000e+00|  0.0000e+00|  5.9867e-01|   -0.209194|    2.421734|    2.624341|    5.261991|   10.394140|
|           0|           0|           9|  0.0000e+00|  0.0000e+00|  5.9861e-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|          < -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	0m17.024s
user	0m16.895s
sys	0m0.404s
+ 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/ESPbeta/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/ESPbeta/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 9.17.15
AFLR2    : Version Date   04/23/24 @ 12:51AM
AFLR2    : Compile OS     Darwin 23.4.0 arm64
AFLR2    : Compile Date   04/23/24 @ 12:51AM
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 11.5.14
AFLR4    : Version Date   04/18/24 @ 12:45PM
AFLR4    : Compile OS     Darwin 23.4.0 arm64
AFLR4    : Compile Date   04/18/24 @ 03:04PM
AFLR4    : Copyright 1994-2021, D.L. Marcum
AFLR4    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.8.0
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: https://su2code.github.io                        |
|                                                                       |
| The SU2 Project is maintained by the SU2 Foundation                   |
| (http://su2foundation.org)                                            |
-------------------------------------------------------------------------
| 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 <http://www.gnu.org/licenses/>.   |
-------------------------------------------------------------------------

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 & 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 https://su2code.github.io/docs_v7/Build-SU2-Linux-MacOS/#compiler-optimizations
WARNING: SU2 was not compiled for an AVX-capable architecture. Performance could be better,
         see https://su2code.github.io/docs_v7/Build-SU2-Linux-MacOS/#compiler-optimizations
WARNING: SU2 was not compiled for an AVX-capable architecture. Performance could be better,
         see https://su2code.github.io/docs_v7/Build-SU2-Linux-MacOS/#compiler-optimizations
+----------------------------------------------------------------------------------------------------------------------------------------------+
|   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|  9.1547e-01|   -0.459271|    1.871877|    1.655308|    5.031624|    0.762262|
|           0|           0|           1|  0.0000e+00|  0.0000e+00|  9.1105e-01|   -0.456941|    2.040681|    1.747831|    5.043074|    1.447848|
|           0|           0|           2|  0.0000e+00|  0.0000e+00|  9.0895e-01|   -0.398416|    2.120447|    1.970735|    5.091930|    3.304023|
|           0|           0|           3|  0.0000e+00|  0.0000e+00|  9.0905e-01|   -0.382713|    2.165329|    2.106879|    5.096084|    7.146675|
|           0|           0|           4|  0.0000e+00|  0.0000e+00|  9.0730e-01|   -0.387623|    2.192520|    2.179204|    5.084553|   12.977091|
|           0|           0|           5|  0.0000e+00|  0.0000e+00|  9.0694e-01|   -0.395260|    2.209372|    2.208904|    5.080255|   20.307648|
|           0|           0|           6|  0.0000e+00|  0.0000e+00|  9.0600e-01|   -0.386688|    2.193854|    2.231688|    5.091259|   28.440654|
|           0|           0|           7|  0.0000e+00|  0.0000e+00|  9.0547e-01|   -0.387582|    2.150321|    2.255497|    5.085909|   33.542538|
|           0|           0|           8|  0.0000e+00|  0.0000e+00|  9.0499e-01|   -0.424592|    2.094097|    2.270673|    5.038598|   31.887370|
|           0|           0|           9|  0.0000e+00|  0.0000e+00|  9.0463e-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|          < -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: https://su2code.github.io                        |
|                                                                       |
| The SU2 Project is maintained by the SU2 Foundation                   |
| (http://su2foundation.org)                                            |
-------------------------------------------------------------------------
| 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 <http://www.gnu.org/licenses/>.   |
-------------------------------------------------------------------------

----------------- 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 4.175909 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: https://su2code.github.io                        |
|                                                                       |
| The SU2 Project is maintained by the SU2 Foundation                   |
| (http://su2foundation.org)                                            |
-------------------------------------------------------------------------
| 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 <http://www.gnu.org/licenses/>.   |
-------------------------------------------------------------------------

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 & 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 https://su2code.github.io/docs_v7/Build-SU2-Linux-MacOS/#compiler-optimizations
WARNING: SU2 was not compiled for an AVX-capable architecture. Performance could be better,
         see https://su2code.github.io/docs_v7/Build-SU2-Linux-MacOS/#compiler-optimizations
WARNING: SU2 was not compiled for an AVX-capable architecture. Performance could be better,
         see https://su2code.github.io/docs_v7/Build-SU2-Linux-MacOS/#compiler-optimizations
+----------------------------------------------------------------------------------------------------------------------------------------------+
|   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|  9.1407e-01|   -0.398750|    1.977474|    1.644084|    5.092145|    1.923782|
|           0|           0|           1|  0.0000e+00|  0.0000e+00|  9.1040e-01|   -0.248975|    2.258948|    1.976579|    5.257848|    2.578720|
|           0|           0|           2|  0.0000e+00|  0.0000e+00|  9.0680e-01|   -0.198142|    2.347683|    2.225644|    5.300689|    3.981171|
|           0|           0|           3|  0.0000e+00|  0.0000e+00|  9.0480e-01|   -0.214514|    2.375555|    2.358260|    5.270011|    5.965906|
|           0|           0|           4|  0.0000e+00|  0.0000e+00|  9.0350e-01|   -0.239435|    2.394864|    2.421022|    5.239901|    7.849147|
|           0|           0|           5|  0.0000e+00|  0.0000e+00|  9.0277e-01|   -0.262371|    2.404237|    2.445537|    5.228001|    9.366346|
|           0|           0|           6|  0.0000e+00|  0.0000e+00|  9.0215e-01|   -0.284513|    2.389017|    2.460376|    5.215548|   10.610658|
|           0|           0|           7|  0.0000e+00|  0.0000e+00|  9.0181e-01|   -0.311476|    2.344163|    2.476241|    5.184871|   11.527148|
|           0|           0|           8|  0.0000e+00|  0.0000e+00|  9.0161e-01|   -0.361259|    2.273271|    2.486137|    5.118277|   12.003369|
|           0|           0|           9|  0.0000e+00|  0.0000e+00|  9.0102e-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|          < -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	0m39.785s
user	0m38.668s
sys	0m1.250s
+ 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/ESPbeta/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/ESPbeta/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: https://su2code.github.io                        |
|                                                                       |
| The SU2 Project is maintained by the SU2 Foundation                   |
| (http://su2foundation.org)                                            |
-------------------------------------------------------------------------
| 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 <http://www.gnu.org/licenses/>.   |
-------------------------------------------------------------------------

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 & 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 https://su2code.github.io/docs_v7/Build-SU2-Linux-MacOS/#compiler-optimizations
WARNING: SU2 was not compiled for an AVX-capable architecture. Performance could be better,
         see https://su2code.github.io/docs_v7/Build-SU2-Linux-MacOS/#compiler-optimizations
WARNING: SU2 was not compiled for an AVX-capable architecture. Performance could be better,
         see https://su2code.github.io/docs_v7/Build-SU2-Linux-MacOS/#compiler-optimizations
+----------------------------------------------------------------------------------------------------------------------------------------------+
|   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|  3.6413e-02|   -1.163068|    1.073873|    1.341547|    4.312268|    0.062082|
|           0|           0|           1|  0.0000e+00|  0.0000e+00|  3.6143e-02|   -1.558471|    0.813117|    0.969484|    3.926501|    0.143132|
|           0|           0|           2|  0.0000e+00|  0.0000e+00|  3.5861e-02|   -1.599269|    0.950037|    1.012154|    3.879885|    0.386300|
|           0|           0|           3|  0.0000e+00|  0.0000e+00|  3.5490e-02|   -1.661284|    1.005970|    1.023067|    3.797319|    0.981260|
|           0|           0|           4|  0.0000e+00|  0.0000e+00|  3.5330e-02|   -1.658421|    1.009907|    0.965279|    3.792658|    2.399755|
|           0|           0|           5|  0.0000e+00|  0.0000e+00|  3.5180e-02|   -1.630602|    0.996801|    0.859556|    3.833204|    6.390579|
|           0|           0|           6|  0.0000e+00|  0.0000e+00|  3.5040e-02|   -1.628009|    1.002770|    0.822847|    3.846297|   27.872536|
|           0|           0|           7|  0.0000e+00|  0.0000e+00|  3.4988e-02|   -1.646113|    1.024424|    0.882502|    3.830202|  -48.293527|
|           0|           0|           8|  0.0000e+00|  0.0000e+00|  3.4907e-02|   -1.672152|    1.033657|    0.939200|    3.797228|  -22.113788|
|           0|           0|           9|  0.0000e+00|  0.0000e+00|  3.4815e-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|         < -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	0m1.096s
user	0m1.217s
sys	0m0.545s
+ 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/ESPbeta/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/ESPbeta/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:  0.013384
Creating surface mesh ...
Surface mesh seconds:  0.001792
Recovering boundaries...
Boundary recovery seconds:  0.03534
Removing exterior tetrahedra ...
Spreading region attributes.
Exterior tets removal seconds:  0.002362
Suppressing Steiner points ...
Steiner suppression seconds:  5e-06
Recovering Delaunayness...
Delaunay recovery seconds:  0.00561
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:  0.309771
Smoothing vertices...
Mesh smoothing seconds:  0.202438
Improving mesh...
Mesh improvement seconds:  0.006627
Jettisoning redundant points.

Writing nodes.
Writing elements.
Writing faces.
Writing edges.

Output seconds:  0.000658
Total running seconds:  0.578115

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: https://su2code.github.io                        |
|                                                                       |
| The SU2 Project is maintained by the SU2 Foundation                   |
| (http://su2foundation.org)                                            |
-------------------------------------------------------------------------
| 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 <http://www.gnu.org/licenses/>.   |
-------------------------------------------------------------------------

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 & 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 https://su2code.github.io/docs_v7/Build-SU2-Linux-MacOS/#compiler-optimizations
WARNING: SU2 was not compiled for an AVX-capable architecture. Performance could be better,
         see https://su2code.github.io/docs_v7/Build-SU2-Linux-MacOS/#compiler-optimizations
WARNING: SU2 was not compiled for an AVX-capable architecture. Performance could be better,
         see https://su2code.github.io/docs_v7/Build-SU2-Linux-MacOS/#compiler-optimizations
+----------------------------------------------------------------------------------------------------------------------------------------------+
|   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|  1.1149e-01|    0.614349|    3.046325|    2.089422|    6.105244|    1.831854|
|           0|           0|           1|  0.0000e+00|  0.0000e+00|  1.1023e-01|    0.764583|    3.258604|    2.974732|    6.265552|    2.165840|
|           0|           0|           2|  0.0000e+00|  0.0000e+00|  1.0989e-01|    0.642409|    3.278261|    3.214494|    6.139447|    3.169947|
|           0|           0|           3|  0.0000e+00|  0.0000e+00|  1.0957e-01|    0.541917|    3.250446|    3.272037|    6.028748|    4.533401|
|           0|           0|           4|  0.0000e+00|  0.0000e+00|  1.0938e-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|         < -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	0m2.761s
user	0m2.893s
sys	0m0.266s
+ 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/ESPbeta/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/ESPbeta/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 2
	Name = x43A, index = 1
	Name = Farfield, 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    = 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 = 2
	Name = x43A, index = 1
	Name = Farfield, index = 2
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:  0.033862
Creating surface mesh ...
Surface mesh seconds:  0.008273
Recovering boundaries...
Warning:  2 segments are not recovered.
Boundary recovery seconds:  0.110614
Removing exterior tetrahedra ...
Spreading region attributes.
Exterior tets removal seconds:  0.006728
Suppressing Steiner points ...
Steiner suppression seconds:  7e-06
Recovering Delaunayness...
Delaunay recovery seconds:  0.014906
Refining mesh...
  12647 insertions, added 5257 points, 11940 tetrahedra in queue.
Refinement seconds:  0.342086
Smoothing vertices...
Mesh smoothing seconds:  0.261519
Improving mesh...
Mesh improvement seconds:  0.010301
Jettisoning redundant points.

Writing nodes.
Writing elements.
Writing faces.
Writing edges.

Output seconds:  0.002174
Total running seconds:  0.790755

Statistics:

  Input points: 9486
  Input facets: 18968
  Input segments: 28452
  Input holes: 1
  Input regions: 0

  Mesh points: 14929
  Mesh tetrahedra: 61505
  Mesh faces: 132494
  Mesh faces on exterior boundary: 18968
  Mesh faces on input facets: 18968
  Mesh edges on input segments: 28452
  Steiner points inside domain: 5443

Done meshing using TetGen!

Writing SU2 file ....
Finished writing SU2 file

Getting CFD boundary conditions
	Boundary condition name - Farfield
	Boundary condition name - x43A
	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)"


Running SU2......

-------------------------------------------------------------------------
|    ___ _   _ ___                                                      |
|   / __| | | |_  )   Release 8.0.0 "Harrier"                           |
|   \__ \ |_| |/ /                                                      |
|   |___/\___//___|   Suite (Computational Fluid Dynamics Code)         |
|                                                                       |
-------------------------------------------------------------------------
| SU2 Project Website: https://su2code.github.io                        |
|                                                                       |
| The SU2 Project is maintained by the SU2 Foundation                   |
| (http://su2foundation.org)                                            |
-------------------------------------------------------------------------
| 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 <http://www.gnu.org/licenses/>.   |
-------------------------------------------------------------------------

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.
Reference origin for moment evaluation is (0, 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: ../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|
+-----------------------------------------------------------------------+
|                          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.
14929 grid points.
61505 volume elements.
2 surface markers.
7616 boundary elements in index 0 (Marker = BC_1).
11352 boundary elements in index 1 (Marker = BC_2).
61505 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: 0.523696. Standard deviation K: 2.57688.
Checking for periodicity.
Computing mesh quality statistics for the dual control volumes.
+--------------------------------------------------------------+
|           Mesh Quality Metric|        Minimum|        Maximum|
+--------------------------------------------------------------+
|    Orthogonality Angle (deg.)|        2.01085|        85.2046|
|     CV Face Area Aspect Ratio|        1.41431|        3475.64|
|           CV Sub-Volume Ratio|              1|         768690|
+--------------------------------------------------------------+
Setting the multigrid structure.
+-------------------------------------------+
|  MG Level|       CVs|Aggl. Rate|       CFL|
+-------------------------------------------+
|         0|     14929|    1/1.00|        10|
|         1|      2715|     1/5.5|   8.49841|
|         2|       490|    1/5.54|   7.20395|
+-------------------------------------------+
Finding max control volume width.
Semi-span length = 30 m.
Wetted area = 13596.3 m^2.
Area projection in the x-plane = 761.676 m^2, y-plane = 2062.27 m^2, z-plane = 5463.61 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 & 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|        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 https://su2code.github.io/docs_v7/Build-SU2-Linux-MacOS/#compiler-optimizations
WARNING: SU2 was not compiled for an AVX-capable architecture. Performance could be better,
         see https://su2code.github.io/docs_v7/Build-SU2-Linux-MacOS/#compiler-optimizations
WARNING: SU2 was not compiled for an AVX-capable architecture. Performance could be better,
         see https://su2code.github.io/docs_v7/Build-SU2-Linux-MacOS/#compiler-optimizations
+----------------------------------------------------------------------------------------------------------------------------------------------+
|   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|  2.1112e-01|    2.730238|    5.664282|    4.727966|    8.729713|   -0.338259|
|           0|           0|           1|  0.0000e+00|  0.0000e+00|  2.0470e-01|    3.172855|    6.235351|    5.708733|    9.163474|   -0.117122|
|           0|           0|           2|  0.0000e+00|  0.0000e+00|  2.0272e-01|    3.313832|    6.405575|    5.809826|    9.273948|   -0.036095|
|           0|           0|           3|  0.0000e+00|  0.0000e+00|  2.0168e-01|    3.301504|    6.396712|    5.682129|    9.288613|   -0.015822|
|           0|           0|           4|  0.0000e+00|  0.0000e+00|  2.0066e-01|    3.134853|    6.203812|    5.540269|    9.119715|   -0.030764|

----------------------------- Solver Exit -------------------------------

Maximum number of iterations reached (ITER = 5) before convergence.
+-----------------------------------------------------------------------+
|      Convergence Field     |     Value    |   Criterion  |  Converged |
+-----------------------------------------------------------------------+
|                    rms[Rho]|       3.13485|         < -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 124 non-physical points in the solution.
Warning: 58 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 =  -3.688941 Cd =  119.911192
Cmx =  35.034239 Cmy =  8986.683762 Cmz =  192.445678
Cx =  119.939922 Cy =  1.734147 Cz =  2.591782

real	0m5.518s
user	0m7.257s
sys	0m0.928s
+ 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/ESPbeta/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
cart3d_PyTest.py test;
+ python -u cart3d_PyTest.py -outLevel=0
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/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  > autoInputs.out
 Executing: ./aero.csh > 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	0m8.726s
user	0m15.491s
sys	0m0.356s
+ 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/ESPbeta/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/ESPbeta/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
----------------------------------------
>>> 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 > autoInputs.out
 o Evaluating Cart3D functionals and/or gradients
   ATTENTION: using static geometry ../inputs/Components.i.tri
   (13:11:22) Running aero.csh on 2 core(s) in M0.5901A2B0_DP1
   (13:11:23) aero.csh done
 o case M0.5901A2B0_DP1, averaging data over 1 cycle(s)
>>> CL2 [0.01631562]  CL 0.12773309
----------------------------------------
----------------------------------------
>>> alpha [2.]
>>> CL2 [0.01631562]  CL 0.12773309
----------------------------------------
========================================
 o Evaluating Cart3D functionals and/or gradients
   ATTENTION: using static geometry ../inputs/Components.i.tri
   (13:11:24) Running aero.csh on 2 core(s) in M0.5901A2B0_DP1
   (13:11:26) 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
   (13:11:26) Linearizing cut-cells
   (13:11:26) ... done
   o Number of simultaneous xsensit jobs:  1
   (13:11:26) Computing gradients
   (13:11:30) ... done
 o case M0.5901A2B0_DP1, averaging data over 1 cycle(s)
>>> 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
----------------------------------------
>>> alpha [1.98427373]
 o Evaluating Cart3D functionals and/or gradients
   ATTENTION: using static geometry ../inputs/Components.i.tri
   (13:11:31) Running aero.csh on 2 core(s) in M0.5901A1.98427B0_DP1
   (13:11:32) aero.csh done
 o case M0.5901A1.98427B0_DP1, averaging data over 1 cycle(s)
>>> CL2 [0.01606724]  CL 0.12675617
----------------------------------------
========================================
 o Evaluating Cart3D functionals and/or gradients
   ATTENTION: using static geometry ../inputs/Components.i.tri
   (13:11:33) Running aero.csh on 2 core(s) in M0.5901A1.98427B0_DP1
   (13:11:35) 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
   (13:11:35) Linearizing cut-cells
   (13:11:35) ... done
   o Number of simultaneous xsensit jobs:  1
   (13:11:35) Computing gradients
   (13:11:39) ... done
 o case M0.5901A1.98427B0_DP1, averaging data over 1 cycle(s)
>>> CL2_alpha [[0.01560329]]
========================================

At iterate    1    f=  1.60672D-02    |proj g|=  1.56033D-02
----------------------------------------
>>> alpha [-0.01099175]
 o Evaluating Cart3D functionals and/or gradients
   ATTENTION: using static geometry ../inputs/Components.i.tri
   (13:11:39) Running aero.csh on 2 core(s) in M0.5901A-0.0109917B0_DP1
   (13:11:41) aero.csh done
 o case M0.5901A-0.0109917B0_DP1, averaging data over 1 cycle(s)
>>> CL2 [6.05653711e-06]  CL 0.00246101
----------------------------------------
========================================
 o Evaluating Cart3D functionals and/or gradients
   ATTENTION: using static geometry ../inputs/Components.i.tri
   (13:11:42) Running aero.csh on 2 core(s) in M0.5901A-0.0109917B0_DP1
   (13:11:43) 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
   (13:11:44) Linearizing cut-cells
   (13:11:44) ... done
   o Number of simultaneous xsensit jobs:  1
   (13:11:44) Computing gradients
   (13:11:48) ... done
 o case M0.5901A-0.0109917B0_DP1, averaging data over 1 cycle(s)
>>> CL2_alpha [[0.00031042]]
========================================

At iterate    2    f=  6.05654D-06    |proj g|=  3.10424D-04
----------------------------------------
>>> alpha [-0.05149286]
 o Evaluating Cart3D functionals and/or gradients
   ATTENTION: using static geometry ../inputs/Components.i.tri
   (13:11:48) Running aero.csh on 2 core(s) in M0.5901A-0.0514929B0_DP1
   (13:11:50) aero.csh done
 o case M0.5901A-0.0514929B0_DP1, averaging data over 1 cycle(s)
>>> CL2 [2.59817062e-10]  CL 1.612e-05
----------------------------------------
========================================
 o Evaluating Cart3D functionals and/or gradients
   ATTENTION: using static geometry ../inputs/Components.i.tri
   (13:11:51) Running aero.csh on 2 core(s) in M0.5901A-0.0514929B0_DP1
   (13:11:52) 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
   (13:11:53) Linearizing cut-cells
   (13:11:53) ... done
   o Number of simultaneous xsensit jobs:  1
   (13:11:53) Computing gradients
   (13:11:57) ... done
 o case M0.5901A-0.0514929B0_DP1, averaging data over 1 cycle(s)
>>> CL2_alpha [[2.03612433e-06]]
========================================

At iterate    3    f=  2.59817D-10    |proj g|=  2.03612D-06
----------------------------------------
>>> alpha [-0.05176027]
 o Evaluating Cart3D functionals and/or gradients
   ATTENTION: using static geometry ../inputs/Components.i.tri
   (13:11:57) Running aero.csh on 2 core(s) in M0.5901A-0.0517603B0_DP1
   (13:11:59) aero.csh done
 o case M0.5901A-0.0517603B0_DP1, averaging data over 1 cycle(s)
>>> CL2 [9.25766089e-15]  CL 1e-07
----------------------------------------
========================================
 o Evaluating Cart3D functionals and/or gradients
   ATTENTION: using static geometry ../inputs/Components.i.tri
   (13:12:00) Running aero.csh on 2 core(s) in M0.5901A-0.0517603B0_DP1
   (13:12:01) 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
   (13:12:02) Linearizing cut-cells
   (13:12:02) ... done
   o Number of simultaneous xsensit jobs:  1
   (13:12:02) Computing gradients
   (13:12:06) ... done
 o case M0.5901A-0.0517603B0_DP1, averaging data over 1 cycle(s)
>>> 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_<=_PGTOL            
Optimization Complete
-----------------------------------
Optimized value: [-0.05176027]

real	0m45.783s
user	0m31.196s
sys	0m5.131s
+ 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/ESPbeta/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/ESPbeta/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
----------------------------------------
>>> 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 > autoInputs.out
 o Evaluating Cart3D functionals and/or gradients
   ATTENTION: using static geometry ../inputs/Components.i.tri
   (13:12:08) Running aero.csh on 2 core(s) in M0.5901A0B0_DP1
   (13:12:16) aero.csh done
 o case M0.5901A0B0_DP1, averaging data over 1 cycle(s)
>>> CL2 [0.00411365]  CL 0.0641354
----------------------------------------
----------------------------------------
>>> twist [4.]
>>> CL2 [0.00411365]  CL 0.0641354
----------------------------------------
========================================
 o Evaluating Cart3D functionals and/or gradients
   ATTENTION: using static geometry ../inputs/Components.i.tri
   (13:12:16) Running aero.csh on 2 core(s) in M0.5901A0B0_DP1
   (13:12:27) 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
   (13:12:28) Linearizing cut-cells
   (13:12:30) ... done
   o Number of simultaneous xsensit jobs:  1
   (13:12:30) Computing gradients
   (13:12:34) ... done
 o case M0.5901A0B0_DP1, averaging data over 1 cycle(s)
>>> 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
----------------------------------------
>>> 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 > autoInputs.out
 o Evaluating Cart3D functionals and/or gradients
   ATTENTION: using static geometry ../inputs/Components.i.tri
   (13:12:35) Running aero.csh on 2 core(s) in M0.5901A0B0_DP1
   (13:12:43) aero.csh done
 o case M0.5901A0B0_DP1, averaging data over 1 cycle(s)
>>> CL2 [0.0041123]  CL 0.0641197
----------------------------------------
========================================
 o Evaluating Cart3D functionals and/or gradients
   ATTENTION: using static geometry ../inputs/Components.i.tri
   (13:12:43) Running aero.csh on 2 core(s) in M0.5901A0B0_DP1
   (13:12:54) 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
   (13:12:55) Linearizing cut-cells
   (13:12:57) ... done
   o Number of simultaneous xsensit jobs:  1
   (13:12:57) Computing gradients
   (13:13:01) ... done
 o case M0.5901A0B0_DP1, averaging data over 1 cycle(s)
>>> CL2_twist [[0.00210014]]
========================================

At iterate    1    f=  4.11230D-03    |proj g|=  2.10014D-03
----------------------------------------
>>> 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 > autoInputs.out
 o Evaluating Cart3D functionals and/or gradients
   ATTENTION: using static geometry ../inputs/Components.i.tri
   (13:13:02) Running aero.csh on 2 core(s) in M0.5901A0B0_DP1
   (13:13:10) aero.csh done
 o case M0.5901A0B0_DP1, averaging data over 1 cycle(s)
>>> CL2 [0.00998113]  CL -0.0999038
----------------------------------------
========================================
 o Evaluating Cart3D functionals and/or gradients
   ATTENTION: using static geometry ../inputs/Components.i.tri
   (13:13:11) Running aero.csh on 2 core(s) in M0.5901A0B0_DP1
   (13:13:21) 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
   (13:13:22) Linearizing cut-cells
   (13:13:24) ... done
   o Number of simultaneous xsensit jobs:  1
   (13:13:24) Computing gradients
   (13:13:28) ... done
 o case M0.5901A0B0_DP1, averaging data over 1 cycle(s)
>>> CL2_twist [[-0.00319688]]
========================================
----------------------------------------
>>> 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 > autoInputs.out
 o Evaluating Cart3D functionals and/or gradients
   ATTENTION: using static geometry ../inputs/Components.i.tri
   (13:13:29) Running aero.csh on 2 core(s) in M0.5901A0B0_DP1
   (13:13:37) aero.csh done
 o case M0.5901A0B0_DP1, averaging data over 1 cycle(s)
>>> CL2 [4.79392926e-08]  CL -0.00022338
----------------------------------------
========================================
 o Evaluating Cart3D functionals and/or gradients
   ATTENTION: using static geometry ../inputs/Components.i.tri
   (13:13:37) Running aero.csh on 2 core(s) in M0.5901A0B0_DP1
   (13:13:48) 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
   (13:13:48) Linearizing cut-cells
   (13:13:51) ... done
   o Number of simultaneous xsensit jobs:  1
   (13:13:51) Computing gradients
   (13:13:55) ... done
 o case M0.5901A0B0_DP1, averaging data over 1 cycle(s)
>>> CL2_twist [[-7.2473947e-06]]
========================================

At iterate    2    f=  4.79393D-08    |proj g|=  7.24739D-06
----------------------------------------
>>> 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 > autoInputs.out
 o Evaluating Cart3D functionals and/or gradients
   ATTENTION: using static geometry ../inputs/Components.i.tri
   (13:13:56) Running aero.csh on 2 core(s) in M0.5901A0B0_DP1
   (13:14:03) aero.csh done
 o case M0.5901A0B0_DP1, averaging data over 1 cycle(s)
>>> CL2 [2.18169714e-08]  CL 0.00015117
----------------------------------------
========================================
 o Evaluating Cart3D functionals and/or gradients
   ATTENTION: using static geometry ../inputs/Components.i.tri
   (13:14:04) Running aero.csh on 2 core(s) in M0.5901A0B0_DP1
   (13:14:15) 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
   (13:14:15) Linearizing cut-cells
   (13:14:17) ... done
   o Number of simultaneous xsensit jobs:  1
   (13:14:17) Computing gradients
   (13:14:21) ... done
 o case M0.5901A0B0_DP1, averaging data over 1 cycle(s)
>>> 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_<=_FACTR*EPSMCH             
Optimization Complete
-----------------------------------
Optimized values: [-0.12922018]

real	2m15.598s
user	3m4.258s
sys	0m5.766s
+ 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/ESPbeta/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/ESPbeta/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 9.17.15
AFLR2    : Version Date   04/23/24 @ 12:51AM
AFLR2    : Compile OS     Darwin 23.4.0 arm64
AFLR2    : Compile Date   04/23/24 @ 12:51AM
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 11.5.14
AFLR4    : Version Date   04/18/24 @ 12:45PM
AFLR4    : Compile OS     Darwin 23.4.0 arm64
AFLR4    : Compile Date   04/18/24 @ 03:04PM
AFLR4    : Copyright 1994-2021, D.L. Marcum
AFLR4    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.8.0
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	0m5.657s
user	0m5.599s
sys	0m0.348s
+ 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/ESPbeta/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
masstran_PyTest.py test;
+ python -u masstran_PyTest.py -outLevel=0
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/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	0m3.763s
user	0m5.136s
sys	0m9.460s
+ 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/ESPbeta/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/ESPbeta/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	0m0.273s
user	0m0.333s
sys	0m0.073s
+ 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/ESPbeta/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/ESPbeta/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
->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	0m0.417s
user	0m0.643s
sys	0m0.051s
+ 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/ESPbeta/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/ESPbeta/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
->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	0m0.351s
user	0m0.512s
sys	0m0.050s
+ 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/ESPbeta/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/ESPbeta/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	0m6.946s
user	0m13.134s
sys	0m6.614s
+ 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/ESPbeta/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/ESPbeta/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	0m0.398s
user	0m0.541s
sys	0m0.108s
+ 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/ESPbeta/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/ESPbeta/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	0m0.491s
user	0m0.688s
sys	0m0.106s
+ 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/ESPbeta/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/ESPbeta/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	0m22.488s
user	0m22.312s
sys	0m0.436s
+ 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/ESPbeta/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/ESPbeta/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	0m0.716s
user	0m0.824s
sys	0m0.196s
+ 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/ESPbeta/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/ESPbeta/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	0m0.576s
user	0m0.766s
sys	0m0.114s
+ 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/ESPbeta/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
astros_PyTest.py test;
+ python -u astros_PyTest.py -outLevel=0
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/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	0m8.969s
user	0m10.050s
sys	0m10.542s
+ 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/ESPbeta/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/ESPbeta/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	0m0.484s
user	0m0.684s
sys	0m0.105s
+ 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/ESPbeta/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/ESPbeta/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	0m0.478s
user	0m0.675s
sys	0m0.107s
+ 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/ESPbeta/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/ESPbeta/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	0m0.579s
user	0m0.768s
sys	0m0.113s
+ 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/ESPbeta/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/ESPbeta/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	0m0.495s
user	0m0.691s
sys	0m0.108s
+ 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/ESPbeta/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/ESPbeta/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	0m0.480s
user	0m0.678s
sys	0m0.107s
+ 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/ESPbeta/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/ESPbeta/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	0m0.693s
user	0m0.826s
sys	0m0.171s
+ status=0
+ set +x

=================================================
CAPS verification (using pyCAPS) case astros_Trim_15degree.py passed (as expected)
=================================================

Running.... AEROELASTIC PyTests


=================================================
+ echo 'aeroelasticSimple_Pressure_SU2_and_Astros.py test;'
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/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/ESPbeta/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 9.17.15
AFLR2    : Version Date   04/23/24 @ 12:51AM
AFLR2    : Compile OS     Darwin 23.4.0 arm64
AFLR2    : Compile Date   04/23/24 @ 12:51AM
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 11.5.14
AFLR4    : Version Date   04/18/24 @ 12:45PM
AFLR4    : Compile OS     Darwin 23.4.0 arm64
AFLR4    : Compile Date   04/18/24 @ 03:04PM
AFLR4    : Copyright 1994-2021, D.L. Marcum
AFLR4    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.8.0
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    : Auto Mode Turned OFF

OVERALL  : CPU Time          =     0.073   seconds
Body 1 (of 1)
Number of nodes    = 9343
Number of elements = 18682
Number of triangle elements      = 18682
Number of quadrilateral elements = 0
----------------------------
Total number of nodes    = 9343
Total number of elements = 18682
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 9.17.15
AFLR2    : Version Date   04/23/24 @ 12:51AM
AFLR2    : Compile OS     Darwin 23.4.0 arm64
AFLR2    : Compile Date   04/23/24 @ 12:51AM
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 11.5.14
AFLR4    : Version Date   04/18/24 @ 12:45PM
AFLR4    : Compile OS     Darwin 23.4.0 arm64
AFLR4    : Compile Date   04/18/24 @ 03:04PM
AFLR4    : Copyright 1994-2021, D.L. Marcum
AFLR4    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------
Volume mesh:
	Number of nodes          = 57531
	Number of elements       = 331031
	Number of triangles      = 18682
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 312349
	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: https://su2code.github.io                        |
|                                                                       |
| The SU2 Project is maintained by the SU2 Foundation                   |
| (http://su2foundation.org)                                            |
-------------------------------------------------------------------------
| 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 <http://www.gnu.org/licenses/>.   |
-------------------------------------------------------------------------

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.
57531 grid points.
312349 volume elements.
3 surface markers.
12288 boundary elements in index 0 (Marker = BC_1).
5867 boundary elements in index 1 (Marker = BC_2).
527 boundary elements in index 2 (Marker = BC_3).
312349 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: 102.753. Mean K: 0.74689. Standard deviation K: 4.38956.
Checking for periodicity.
Computing mesh quality statistics for the dual control volumes.
+--------------------------------------------------------------+
|           Mesh Quality Metric|        Minimum|        Maximum|
+--------------------------------------------------------------+
|    Orthogonality Angle (deg.)|        48.3512|        86.0919|
|     CV Face Area Aspect Ratio|        1.11561|        35.2066|
|           CV Sub-Volume Ratio|              1|        18.8559|
+--------------------------------------------------------------+
Setting the multigrid structure.
+-------------------------------------------+
|  MG Level|       CVs|Aggl. Rate|       CFL|
+-------------------------------------------+
|         0|     57531|    1/1.00|        10|
|         1|      9779|    1/5.88|   8.30913|
|         2|      1716|     1/5.7|   6.97784|
+-------------------------------------------+
Finding max control volume width.
Semi-span length = 3.87298 m.
Wetted area = 9.04169 m^2.
Area projection in the x-plane = 0.644461 m^2, y-plane = 0.295795 m^2, z-plane = 4.29819 m^2.
Max. coordinate in the x-direction = 2.53651 m, y-direction = 3.87298 m, z-direction = 0.379751 m.
Min. coordinate in the x-direction = 0 m, y-direction = -2.86125e-18 m, z-direction = -0.0467278 m.
Checking if Euler & 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 https://su2code.github.io/docs_v7/Build-SU2-Linux-MacOS/#compiler-optimizations
WARNING: SU2 was not compiled for an AVX-capable architecture. Performance could be better,
         see https://su2code.github.io/docs_v7/Build-SU2-Linux-MacOS/#compiler-optimizations
WARNING: SU2 was not compiled for an AVX-capable architecture. Performance could be better,
         see https://su2code.github.io/docs_v7/Build-SU2-Linux-MacOS/#compiler-optimizations
+----------------------------------------------------------------------------------------------------------------------------------------------+
|   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|  9.7828e-01|   -1.299765|    0.996854|    0.627451|    4.169341|   -0.962501|
|           0|           0|           1|  0.0000e+00|  0.0000e+00|  9.7350e-01|   -1.689451|    0.841935|    0.460737|    3.766643|   -0.517631|
|           0|           0|           2|  0.0000e+00|  0.0000e+00|  9.6989e-01|   -1.703013|    0.658675|    0.298032|    3.753378|    1.611420|

----------------------------- Solver Exit -------------------------------

Maximum number of iterations reached (ITER = 3) before convergence.
+-----------------------------------------------------------------------+
|      Convergence Field     |     Value    |   Criterion  |  Converged |
+-----------------------------------------------------------------------+
|                    rms[Rho]|      -1.70301|         < -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 = 273
 CAPS Info: Bound 'Skin_Top' Normalized Integrated 'Pressure'
            Rank 0: src = 3.100922e+09, tgt = 3.100922e+09, diff = 1.828803e+02
Reading SU2 AeroLoad File - surface_flow_aeroelasticSimple_Pressure_SA.csv
	Number of variables = 16
	Number of data points = 273
 CAPS Info: Bound 'Skin_Bottom' Normalized Integrated 'Pressure'
            Rank 0: src = 3.018738e+09, tgt = 3.018738e+09, diff = 2.203347e+02
Reading SU2 AeroLoad File - surface_flow_aeroelasticSimple_Pressure_SA.csv
	Number of variables = 16
	Number of data points = 273
 CAPS Info: Bound 'Skin_Tip' Normalized Integrated 'Pressure'
            Rank 0: src = 4.338994e+07, tgt = 4.338994e+07, diff = 3.559001e-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

real	0m10.370s
user	0m10.622s
sys	0m0.914s
+ 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/ESPbeta/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/ESPbeta/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 9.17.15
AFLR2    : Version Date   04/23/24 @ 12:51AM
AFLR2    : Compile OS     Darwin 23.4.0 arm64
AFLR2    : Compile Date   04/23/24 @ 12:51AM
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 11.5.14
AFLR4    : Version Date   04/18/24 @ 12:45PM
AFLR4    : Compile OS     Darwin 23.4.0 arm64
AFLR4    : Compile Date   04/18/24 @ 03:04PM
AFLR4    : Copyright 1994-2021, D.L. Marcum
AFLR4    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.8.0
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    : Auto Mode Turned OFF

OVERALL  : CPU Time          =     0.073   seconds
Body 1 (of 1)
Number of nodes    = 9343
Number of elements = 18682
Number of triangle elements      = 18682
Number of quadrilateral elements = 0
----------------------------
Total number of nodes    = 9343
Total number of elements = 18682
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 9.17.15
AFLR2    : Version Date   04/23/24 @ 12:51AM
AFLR2    : Compile OS     Darwin 23.4.0 arm64
AFLR2    : Compile Date   04/23/24 @ 12:51AM
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 11.5.14
AFLR4    : Version Date   04/18/24 @ 12:45PM
AFLR4    : Compile OS     Darwin 23.4.0 arm64
AFLR4    : Compile Date   04/18/24 @ 03:04PM
AFLR4    : Copyright 1994-2021, D.L. Marcum
AFLR4    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------
Volume mesh:
	Number of nodes          = 57531
	Number of elements       = 331031
	Number of triangles      = 18682
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 312349
	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: https://su2code.github.io                        |
|                                                                       |
| The SU2 Project is maintained by the SU2 Foundation                   |
| (http://su2foundation.org)                                            |
-------------------------------------------------------------------------
| 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 <http://www.gnu.org/licenses/>.   |
-------------------------------------------------------------------------

----------------- 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.
57531 grid points.
312349 volume elements.
3 surface markers.
12288 boundary elements in index 0 (Marker = BC_1).
5867 boundary elements in index 1 (Marker = BC_2).
527 boundary elements in index 2 (Marker = BC_3).
312349 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 9.609306 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: https://su2code.github.io                        |
|                                                                       |
| The SU2 Project is maintained by the SU2 Foundation                   |
| (http://su2foundation.org)                                            |
-------------------------------------------------------------------------
| 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 <http://www.gnu.org/licenses/>.   |
-------------------------------------------------------------------------

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.
57531 grid points.
312349 volume elements.
3 surface markers.
12288 boundary elements in index 0 (Marker = BC_1).
5867 boundary elements in index 1 (Marker = BC_2).
527 boundary elements in index 2 (Marker = BC_3).
312349 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 1 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: 84.836. Mean K: 0.75089. Standard deviation K: 3.83533.
Checking for periodicity.
Computing mesh quality statistics for the dual control volumes.
+--------------------------------------------------------------+
|           Mesh Quality Metric|        Minimum|        Maximum|
+--------------------------------------------------------------+
|    Orthogonality Angle (deg.)|        41.5576|        86.1004|
|     CV Face Area Aspect Ratio|        1.11561|        33.3076|
|           CV Sub-Volume Ratio|              1|        68.3008|
+--------------------------------------------------------------+
Setting the multigrid structure.
+-------------------------------------------+
|  MG Level|       CVs|Aggl. Rate|       CFL|
+-------------------------------------------+
|         0|     57531|    1/1.00|        10|
|         1|      9779|    1/5.88|   8.30913|
|         2|      1716|     1/5.7|   6.97784|
+-------------------------------------------+
Finding max control volume width.
Semi-span length = 3.89964 m.
Wetted area = 11.4382 m^2.
Area projection in the x-plane = 2.82758 m^2, y-plane = 1.25436 m^2, z-plane = 4.17954 m^2.
Max. coordinate in the x-direction = 2.53729 m, y-direction = 3.89964 m, z-direction = 0.526515 m.
Min. coordinate in the x-direction = 0.000170858 m, y-direction = -2.86125e-18 m, z-direction = -0.705261 m.
Checking if Euler & 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 https://su2code.github.io/docs_v7/Build-SU2-Linux-MacOS/#compiler-optimizations
WARNING: SU2 was not compiled for an AVX-capable architecture. Performance could be better,
         see https://su2code.github.io/docs_v7/Build-SU2-Linux-MacOS/#compiler-optimizations
WARNING: SU2 was not compiled for an AVX-capable architecture. Performance could be better,
         see https://su2code.github.io/docs_v7/Build-SU2-Linux-MacOS/#compiler-optimizations
+----------------------------------------------------------------------------------------------------------------------------------------------+
|   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|  9.7503e-01|   -0.622071|    1.813033|    1.305623|    4.847034|    0.070229|
|           0|           0|           1|  0.0000e+00|  0.0000e+00|  9.7311e-01|   -1.089888|    1.515924|    1.156988|    4.382145|    0.058664|
|           0|           0|           2|  0.0000e+00|  0.0000e+00|  9.6988e-01|   -1.096792|    1.282257|    0.955302|    4.370060|    0.133547|

----------------------------- Solver Exit -------------------------------

Maximum number of iterations reached (ITER = 3) before convergence.
+-----------------------------------------------------------------------+
|      Convergence Field     |     Value    |   Criterion  |  Converged |
+-----------------------------------------------------------------------+
|                    rms[Rho]|      -1.09679|         < -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	0m24.131s
user	0m24.054s
sys	0m1.582s
+ 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/ESPbeta/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/ESPbeta/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 9.17.15
AFLR2    : Version Date   04/23/24 @ 12:51AM
AFLR2    : Compile OS     Darwin 23.4.0 arm64
AFLR2    : Compile Date   04/23/24 @ 12:51AM
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 11.5.14
AFLR4    : Version Date   04/18/24 @ 12:45PM
AFLR4    : Compile OS     Darwin 23.4.0 arm64
AFLR4    : Compile Date   04/18/24 @ 03:04PM
AFLR4    : Copyright 1994-2021, D.L. Marcum
AFLR4    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.8.0
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    : Auto Mode Turned OFF

OVERALL  : CPU Time          =     0.036   seconds
Body 1 (of 1)
Number of nodes    = 2592
Number of elements = 5180
Number of triangle elements      = 5180
Number of quadrilateral elements = 0
----------------------------
Total number of nodes    = 2592
Total number of elements = 5180
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 9.17.15
AFLR2    : Version Date   04/23/24 @ 12:51AM
AFLR2    : Compile OS     Darwin 23.4.0 arm64
AFLR2    : Compile Date   04/23/24 @ 12:51AM
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 11.5.14
AFLR4    : Version Date   04/18/24 @ 12:45PM
AFLR4    : Compile OS     Darwin 23.4.0 arm64
AFLR4    : Compile Date   04/18/24 @ 03:04PM
AFLR4    : Copyright 1994-2021, D.L. Marcum
AFLR4    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------
Volume mesh:
	Number of nodes          = 10490
	Number of elements       = 59345
	Number of triangles      = 5180
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 54165
	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: https://su2code.github.io                        |
|                                                                       |
| The SU2 Project is maintained by the SU2 Foundation                   |
| (http://su2foundation.org)                                            |
-------------------------------------------------------------------------
| 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 <http://www.gnu.org/licenses/>.   |
-------------------------------------------------------------------------

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.
10490 grid points.
54165 volume elements.
3 surface markers.
3448 boundary elements in index 0 (Marker = BC_1).
1565 boundary elements in index 1 (Marker = BC_2).
167 boundary elements in index 2 (Marker = BC_3).
54165 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: 51.6883. Mean K: 0.709733. Standard deviation K: 3.22588.
Checking for periodicity.
Computing mesh quality statistics for the dual control volumes.
+--------------------------------------------------------------+
|           Mesh Quality Metric|        Minimum|        Maximum|
+--------------------------------------------------------------+
|    Orthogonality Angle (deg.)|        44.3316|         85.098|
|     CV Face Area Aspect Ratio|        1.16221|        27.4272|
|           CV Sub-Volume Ratio|              1|        81.5516|
+--------------------------------------------------------------+
Setting the multigrid structure.
+-------------------------------------------+
|  MG Level|       CVs|Aggl. Rate|       CFL|
+-------------------------------------------+
|         0|     10490|    1/1.00|        10|
|         1|      1870|    1/5.61|   8.44202|
|         2|       389|    1/4.81|    7.5031|
+-------------------------------------------+
Finding max control volume width.
Semi-span length = 3.87298 m.
Wetted area = 7.82006 m^2.
Area projection in the x-plane = 0.576038 m^2, y-plane = 0.250011 m^2, z-plane = 3.65657 m^2.
Max. coordinate in the x-direction = 2.53651 m, y-direction = 3.87298 m, z-direction = 0.37624 m.
Min. coordinate in the x-direction = 0 m, y-direction = -2.47212e-18 m, z-direction = -0.0403729 m.
Checking if Euler & 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 https://su2code.github.io/docs_v7/Build-SU2-Linux-MacOS/#compiler-optimizations
WARNING: SU2 was not compiled for an AVX-capable architecture. Performance could be better,
         see https://su2code.github.io/docs_v7/Build-SU2-Linux-MacOS/#compiler-optimizations
WARNING: SU2 was not compiled for an AVX-capable architecture. Performance could be better,
         see https://su2code.github.io/docs_v7/Build-SU2-Linux-MacOS/#compiler-optimizations
+----------------------------------------------------------------------------------------------------------------------------------------------+
|   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|  1.5914e-01|   -0.750102|    1.605585|    1.225778|    4.719004|   -1.220061|
|           0|           0|           1|  0.0000e+00|  0.0000e+00|  1.5813e-01|   -1.054063|    1.501703|    1.099411|    4.403235|   -0.967223|
|           0|           0|           2|  0.0000e+00|  0.0000e+00|  1.5731e-01|   -1.154784|    1.382975|    0.974644|    4.298316|   -0.248219|

----------------------------- Solver Exit -------------------------------

Maximum number of iterations reached (ITER = 3) before convergence.
+-----------------------------------------------------------------------+
|      Convergence Field     |     Value    |   Criterion  |  Converged |
+-----------------------------------------------------------------------+
|                    rms[Rho]|      -1.15478|         < -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 = 89
 CAPS Info: Bound 'Skin_Top' Normalized Integrated 'Pressure'
            Rank 0: src = 3.095732e+09, tgt = 3.095732e+09, diff = 1.167212e+02
Reading SU2 AeroLoad File - surface_flow_aeroelasticSimple_Iterative.csv
	Number of variables = 16
	Number of data points = 89
 CAPS Info: Bound 'Skin_Bottom' Normalized Integrated 'Pressure'
            Rank 0: src = 3.014252e+09, tgt = 3.014252e+09, diff = 2.113069e+02
Reading SU2 AeroLoad File - surface_flow_aeroelasticSimple_Iterative.csv
	Number of variables = 16
	Number of data points = 89
 CAPS Info: Bound 'Skin_Tip' Normalized Integrated 'Pressure'
            Rank 0: src = 3.928484e+07, tgt = 3.928484e+07, diff = 7.997701e-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: https://su2code.github.io                        |
|                                                                       |
| The SU2 Project is maintained by the SU2 Foundation                   |
| (http://su2foundation.org)                                            |
-------------------------------------------------------------------------
| 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 <http://www.gnu.org/licenses/>.   |
-------------------------------------------------------------------------

----------------- 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.
10490 grid points.
54165 volume elements.
3 surface markers.
3448 boundary elements in index 0 (Marker = BC_1).
1565 boundary elements in index 1 (Marker = BC_2).
167 boundary elements in index 2 (Marker = BC_3).
54165 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 0.573760 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: https://su2code.github.io                        |
|                                                                       |
| The SU2 Project is maintained by the SU2 Foundation                   |
| (http://su2foundation.org)                                            |
-------------------------------------------------------------------------
| 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 <http://www.gnu.org/licenses/>.   |
-------------------------------------------------------------------------

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.
10490 grid points.
54165 volume elements.
3 surface markers.
3448 boundary elements in index 0 (Marker = BC_1).
1565 boundary elements in index 1 (Marker = BC_2).
167 boundary elements in index 2 (Marker = BC_3).
54165 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 749 TETRAHEDRON volume elements.
There has been a re-orientation of 26 TRIANGLE surface elements.
Identifying edges and vertices.
Setting the control volume structure.
Volume of the computational grid: 64498.3.
Searching for the closest normal neighbors to the surfaces.
Storing a mapping from global to local point index.
Compute the surface curvature.
Max K: 22.0948. Mean K: 0.527216. Standard deviation K: 1.7157.
Checking for periodicity.
Computing mesh quality statistics for the dual control volumes.
+--------------------------------------------------------------+
|           Mesh Quality Metric|        Minimum|        Maximum|
+--------------------------------------------------------------+
|    Orthogonality Angle (deg.)|         7.2469|        85.7269|
|     CV Face Area Aspect Ratio|        1.16376|        323.111|
|           CV Sub-Volume Ratio|              1|          13009|
+--------------------------------------------------------------+
Setting the multigrid structure.
+-------------------------------------------+
|  MG Level|       CVs|Aggl. Rate|       CFL|
+-------------------------------------------+
|         0|     10490|    1/1.00|        10|
|         1|      1870|    1/5.61|   8.44202|
|         2|       389|    1/4.81|    7.5031|
+-------------------------------------------+
Finding max control volume width.
Semi-span length = 4.41037 m.
Wetted area = 165.297 m^2.
Area projection in the x-plane = 64.0735 m^2, y-plane = 33.8815 m^2, z-plane = 4.99829 m^2.
Max. coordinate in the x-direction = 2.77394 m, y-direction = 4.41037 m, z-direction = 16.2689 m.
Min. coordinate in the x-direction = -0.658365 m, y-direction = -0.0470459 m, z-direction = -19.3812 m.
Checking if Euler & 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 https://su2code.github.io/docs_v7/Build-SU2-Linux-MacOS/#compiler-optimizations
WARNING: SU2 was not compiled for an AVX-capable architecture. Performance could be better,
         see https://su2code.github.io/docs_v7/Build-SU2-Linux-MacOS/#compiler-optimizations
WARNING: SU2 was not compiled for an AVX-capable architecture. Performance could be better,
         see https://su2code.github.io/docs_v7/Build-SU2-Linux-MacOS/#compiler-optimizations
+----------------------------------------------------------------------------------------------------------------------------------------------+
|   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|  1.6746e-01|    1.816485|    4.769066|    4.879546|    7.285591|   -0.019238|
|           0|           0|           1|  0.0000e+00|  0.0000e+00|  1.6553e-01|    2.241333|    4.856618|    4.845215|    7.696248|   -0.040086|
|           0|           0|           2|  0.0000e+00|  0.0000e+00|  1.6908e-01|    2.384284|    4.932235|    4.860433|    7.812202|   -0.053014|

----------------------------- Solver Exit -------------------------------

Maximum number of iterations reached (ITER = 3) before convergence.
+-----------------------------------------------------------------------+
|      Convergence Field     |     Value    |   Criterion  |  Converged |
+-----------------------------------------------------------------------+
|                    rms[Rho]|       2.38428|         < -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 27 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 = 89
 CAPS Info: Bound 'Skin_Top' Normalized Integrated 'Pressure'
            Rank 0: src = 2.016562e+09, tgt = 2.016562e+09, diff = 3.305119e+02
Reading SU2 AeroLoad File - surface_flow_aeroelasticSimple_Iterative.csv
	Number of variables = 16
	Number of data points = 89
 CAPS Info: Bound 'Skin_Bottom' Normalized Integrated 'Pressure'
            Rank 0: src = 1.492384e+09, tgt = 1.492384e+09, diff = 4.421872e+02
Reading SU2 AeroLoad File - surface_flow_aeroelasticSimple_Iterative.csv
	Number of variables = 16
	Number of data points = 89
 CAPS Info: Bound 'Skin_Tip' Normalized Integrated 'Pressure'
            Rank 0: src = 2.354248e+07, tgt = 2.354248e+07, diff = 6.210823e-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: https://su2code.github.io                        |
|                                                                       |
| The SU2 Project is maintained by the SU2 Foundation                   |
| (http://su2foundation.org)                                            |
-------------------------------------------------------------------------
| 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 <http://www.gnu.org/licenses/>.   |
-------------------------------------------------------------------------

----------------- 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.
10490 grid points.
54165 volume elements.
3 surface markers.
3448 boundary elements in index 0 (Marker = BC_1).
1565 boundary elements in index 1 (Marker = BC_2).
167 boundary elements in index 2 (Marker = BC_3).
54165 tetrahedra.

----------------------- Preprocessing computations ----------------------
Setting local point connectivity.
Checking the numerical grid orientation of the interior elements.
There has been a re-orientation of 749 TETRAHEDRON volume elements.
There has been a re-orientation of 26 TRIANGLE surface elements.
Identify edges and vertices.
Setting the bound control volume structure.
Volume of the computational grid: 64498.3.
  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 0.714321 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: https://su2code.github.io                        |
|                                                                       |
| The SU2 Project is maintained by the SU2 Foundation                   |
| (http://su2foundation.org)                                            |
-------------------------------------------------------------------------
| 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 <http://www.gnu.org/licenses/>.   |
-------------------------------------------------------------------------

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.
10490 grid points.
54165 volume elements.
3 surface markers.
3448 boundary elements in index 0 (Marker = BC_1).
1565 boundary elements in index 1 (Marker = BC_2).
167 boundary elements in index 2 (Marker = BC_3).
54165 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 7226 TETRAHEDRON volume elements.
There has been a re-orientation of 206 TRIANGLE surface elements.
Identifying edges and vertices.
Setting the control volume structure.
Volume of the computational grid: 66889.1.
Searching for the closest normal neighbors to the surfaces.
Storing a mapping from global to local point index.
Compute the surface curvature.
Max K: 273.938. Mean K: 1.56756. Standard deviation K: 9.44503.
Checking for periodicity.
Computing mesh quality statistics for the dual control volumes.
+--------------------------------------------------------------+
|           Mesh Quality Metric|        Minimum|        Maximum|
+--------------------------------------------------------------+
|    Orthogonality Angle (deg.)|       0.764151|        84.0172|
|     CV Face Area Aspect Ratio|        1.22546|        165.439|
|           CV Sub-Volume Ratio|              1|         500673|
+--------------------------------------------------------------+
Setting the multigrid structure.
+-------------------------------------------+
|  MG Level|       CVs|Aggl. Rate|       CFL|
+-------------------------------------------+
|         0|     10490|    1/1.00|        10|
|         1|      1874|     1/5.6|   8.44804|
|         2|       394|    1/4.76|   7.53511|
+-------------------------------------------+
Finding max control volume width.
Semi-span length = 5.82231 m.
Wetted area = 324.882 m^2.
Area projection in the x-plane = 143.505 m^2, y-plane = 129.703 m^2, z-plane = 26.6043 m^2.
Max. coordinate in the x-direction = 8.09968 m, y-direction = 5.82231 m, z-direction = 29.9711 m.
Min. coordinate in the x-direction = 0.0260146 m, y-direction = -0.933278 m, z-direction = -41.6074 m.
Checking if Euler & 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 https://su2code.github.io/docs_v7/Build-SU2-Linux-MacOS/#compiler-optimizations
WARNING: SU2 was not compiled for an AVX-capable architecture. Performance could be better,
         see https://su2code.github.io/docs_v7/Build-SU2-Linux-MacOS/#compiler-optimizations
WARNING: SU2 was not compiled for an AVX-capable architecture. Performance could be better,
         see https://su2code.github.io/docs_v7/Build-SU2-Linux-MacOS/#compiler-optimizations
+----------------------------------------------------------------------------------------------------------------------------------------------+
|   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|  1.6443e-01|    2.533258|    5.487132|    5.285803|    8.002364|    0.610334|
|           0|           0|           1|  0.0000e+00|  0.0000e+00|  1.7144e-01|    2.546660|    5.300889|    5.160160|    7.964705|    0.450573|
|           0|           0|           2|  0.0000e+00|  0.0000e+00|  1.7281e-01|    2.637735|    5.231933|    5.225949|    8.013544|    0.420275|

----------------------------- Solver Exit -------------------------------

Maximum number of iterations reached (ITER = 3) before convergence.
+-----------------------------------------------------------------------+
|      Convergence Field     |     Value    |   Criterion  |  Converged |
+-----------------------------------------------------------------------+
|                    rms[Rho]|       2.63773|         < -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 149 non-physical points in the solution.
Warning: 13 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 = 89
 CAPS Info: Bound 'Skin_Top' Normalized Integrated 'Pressure'
            Rank 0: src = 1.529337e+09, tgt = 1.529336e+09, diff = 3.412616e+01
Reading SU2 AeroLoad File - surface_flow_aeroelasticSimple_Iterative.csv
	Number of variables = 16
	Number of data points = 89
 CAPS Info: Bound 'Skin_Bottom' Normalized Integrated 'Pressure'
            Rank 0: src = 1.234296e+09, tgt = 1.234296e+09, diff = 1.286251e+02
Reading SU2 AeroLoad File - surface_flow_aeroelasticSimple_Iterative.csv
	Number of variables = 16
	Number of data points = 89
 CAPS Info: Bound 'Skin_Tip' Normalized Integrated 'Pressure'
            Rank 0: src = 5.628084e+06, tgt = 5.628084e+06, diff = 4.735513e-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: https://su2code.github.io                        |
|                                                                       |
| The SU2 Project is maintained by the SU2 Foundation                   |
| (http://su2foundation.org)                                            |
-------------------------------------------------------------------------
| 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 <http://www.gnu.org/licenses/>.   |
-------------------------------------------------------------------------

----------------- 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.
10490 grid points.
54165 volume elements.
3 surface markers.
3448 boundary elements in index 0 (Marker = BC_1).
1565 boundary elements in index 1 (Marker = BC_2).
167 boundary elements in index 2 (Marker = BC_3).
54165 tetrahedra.

----------------------- Preprocessing computations ----------------------
Setting local point connectivity.
Checking the numerical grid orientation of the interior elements.
There has been a re-orientation of 7226 TETRAHEDRON volume elements.
There has been a re-orientation of 206 TRIANGLE surface elements.
Identify edges and vertices.
Setting the bound control volume structure.
Volume of the computational grid: 66889.1.
  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 22.182963 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: https://su2code.github.io                        |
|                                                                       |
| The SU2 Project is maintained by the SU2 Foundation                   |
| (http://su2foundation.org)                                            |
-------------------------------------------------------------------------
| 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 <http://www.gnu.org/licenses/>.   |
-------------------------------------------------------------------------

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.
10490 grid points.
54165 volume elements.
3 surface markers.
3448 boundary elements in index 0 (Marker = BC_1).
1565 boundary elements in index 1 (Marker = BC_2).
167 boundary elements in index 2 (Marker = BC_3).
54165 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 21656 TETRAHEDRON volume elements.
There has been a re-orientation of 781 TRIANGLE surface elements.
Identifying edges and vertices.
Setting the control volume structure.
Volume of the computational grid: 9.57518e+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: 64.2172. Mean K: 1.24404. Standard deviation K: 4.50057.
Checking for periodicity.
Computing mesh quality statistics for the dual control volumes.
+--------------------------------------------------------------+
|           Mesh Quality Metric|        Minimum|        Maximum|
+--------------------------------------------------------------+
|    Orthogonality Angle (deg.)|       0.199724|        82.2754|
|     CV Face Area Aspect Ratio|        1.51901|        568.479|
|           CV Sub-Volume Ratio|              1|         363347|
+--------------------------------------------------------------+
Setting the multigrid structure.
+-------------------------------------------+
|  MG Level|       CVs|Aggl. Rate|       CFL|
+-------------------------------------------+
|         0|     10490|    1/1.00|        10|
|         1|      1867|    1/5.62|   8.43751|
|         2|       383|    1/4.87|   7.46432|
+-------------------------------------------+
Finding max control volume width.
Semi-span length = 1.89332 m.
Wetted area = 3244.51 m^2.
Area projection in the x-plane = 382.333 m^2, y-plane = 822.101 m^2, z-plane = 47.4578 m^2.
Max. coordinate in the x-direction = 3.14656 m, y-direction = 1.89332 m, z-direction = 335.653 m.
Min. coordinate in the x-direction = -0.577333 m, y-direction = -20.5655 m, z-direction = -2.52092 m.
Checking if Euler & 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 https://su2code.github.io/docs_v7/Build-SU2-Linux-MacOS/#compiler-optimizations
WARNING: SU2 was not compiled for an AVX-capable architecture. Performance could be better,
         see https://su2code.github.io/docs_v7/Build-SU2-Linux-MacOS/#compiler-optimizations
WARNING: SU2 was not compiled for an AVX-capable architecture. Performance could be better,
         see https://su2code.github.io/docs_v7/Build-SU2-Linux-MacOS/#compiler-optimizations
+----------------------------------------------------------------------------------------------------------------------------------------------+
|   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|  1.6624e-01|    4.230882|    7.196541|    7.171336|    9.699988|   -0.009721|
|           0|           0|           1|  0.0000e+00|  0.0000e+00|  1.7191e-01|    4.757294|    7.278987|    7.271916|   10.158721|   -0.008032|
|           0|           0|           2|  0.0000e+00|  0.0000e+00|  1.7365e-01|    4.810154|    7.321114|    7.265251|   10.179303|   -0.008305|

----------------------------- Solver Exit -------------------------------

Maximum number of iterations reached (ITER = 3) before convergence.
+-----------------------------------------------------------------------+
|      Convergence Field     |     Value    |   Criterion  |  Converged |
+-----------------------------------------------------------------------+
|                    rms[Rho]|       4.81015|         < -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 430 non-physical points in the solution.
Warning: 43 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 =  -157.195727
Cd =  18928.839931

real	0m34.213s
user	0m33.477s
sys	0m1.720s
+ 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/ESPbeta/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/ESPbeta/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 9.17.15
AFLR2    : Version Date   04/23/24 @ 12:51AM
AFLR2    : Compile OS     Darwin 23.4.0 arm64
AFLR2    : Compile Date   04/23/24 @ 12:51AM
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 11.5.14
AFLR4    : Version Date   04/18/24 @ 12:45PM
AFLR4    : Compile OS     Darwin 23.4.0 arm64
AFLR4    : Compile Date   04/18/24 @ 03:04PM
AFLR4    : Copyright 1994-2021, D.L. Marcum
AFLR4    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.8.0
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    : Auto Mode Turned OFF

OVERALL  : CPU Time          =     0.036   seconds
Body 1 (of 1)
Number of nodes    = 2592
Number of elements = 5180
Number of triangle elements      = 5180
Number of quadrilateral elements = 0
----------------------------
Total number of nodes    = 2592
Total number of elements = 5180
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 9.17.15
AFLR2    : Version Date   04/23/24 @ 12:51AM
AFLR2    : Compile OS     Darwin 23.4.0 arm64
AFLR2    : Compile Date   04/23/24 @ 12:51AM
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 11.5.14
AFLR4    : Version Date   04/18/24 @ 12:45PM
AFLR4    : Compile OS     Darwin 23.4.0 arm64
AFLR4    : Compile Date   04/18/24 @ 03:04PM
AFLR4    : Copyright 1994-2021, D.L. Marcum
AFLR4    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------
Volume mesh:
	Number of nodes          = 10490
	Number of elements       = 59345
	Number of triangles      = 5180
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 54165
	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: https://su2code.github.io                        |
|                                                                       |
| The SU2 Project is maintained by the SU2 Foundation                   |
| (http://su2foundation.org)                                            |
-------------------------------------------------------------------------
| 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 <http://www.gnu.org/licenses/>.   |
-------------------------------------------------------------------------

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.
10490 grid points.
54165 volume elements.
3 surface markers.
3448 boundary elements in index 0 (Marker = BC_1).
1565 boundary elements in index 1 (Marker = BC_2).
167 boundary elements in index 2 (Marker = BC_3).
54165 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: 51.6883. Mean K: 0.709733. Standard deviation K: 3.22588.
Checking for periodicity.
Computing mesh quality statistics for the dual control volumes.
+--------------------------------------------------------------+
|           Mesh Quality Metric|        Minimum|        Maximum|
+--------------------------------------------------------------+
|    Orthogonality Angle (deg.)|        44.3316|         85.098|
|     CV Face Area Aspect Ratio|        1.16221|        27.4272|
|           CV Sub-Volume Ratio|              1|        81.5516|
+--------------------------------------------------------------+
Setting the multigrid structure.
+-------------------------------------------+
|  MG Level|       CVs|Aggl. Rate|       CFL|
+-------------------------------------------+
|         0|     10490|    1/1.00|        10|
|         1|      1870|    1/5.61|   8.44202|
|         2|       389|    1/4.81|    7.5031|
+-------------------------------------------+
Finding max control volume width.
Semi-span length = 3.87298 m.
Wetted area = 7.82006 m^2.
Area projection in the x-plane = 0.576038 m^2, y-plane = 0.250011 m^2, z-plane = 3.65657 m^2.
Max. coordinate in the x-direction = 2.53651 m, y-direction = 3.87298 m, z-direction = 0.37624 m.
Min. coordinate in the x-direction = 0 m, y-direction = -2.47212e-18 m, z-direction = -0.0403729 m.
Checking if Euler & 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 https://su2code.github.io/docs_v7/Build-SU2-Linux-MacOS/#compiler-optimizations
WARNING: SU2 was not compiled for an AVX-capable architecture. Performance could be better,
         see https://su2code.github.io/docs_v7/Build-SU2-Linux-MacOS/#compiler-optimizations
WARNING: SU2 was not compiled for an AVX-capable architecture. Performance could be better,
         see https://su2code.github.io/docs_v7/Build-SU2-Linux-MacOS/#compiler-optimizations
+----------------------------------------------------------------------------------------------------------------------------------------------+
|   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|  1.5807e-01|   -0.750102|    1.605585|    1.225778|    4.719004|   -1.220061|
|           0|           0|           1|  0.0000e+00|  0.0000e+00|  1.5780e-01|   -1.054063|    1.501703|    1.099411|    4.403235|   -0.967223|
|           0|           0|           2|  0.0000e+00|  0.0000e+00|  1.5747e-01|   -1.154784|    1.382975|    0.974644|    4.298316|   -0.248219|

----------------------------- Solver Exit -------------------------------

Maximum number of iterations reached (ITER = 3) before convergence.
+-----------------------------------------------------------------------+
|      Convergence Field     |     Value    |   Criterion  |  Converged |
+-----------------------------------------------------------------------+
|                    rms[Rho]|      -1.15478|         < -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 = 89
 CAPS Info: Bound 'Skin_Top' Normalized Integrated 'Pressure'
            Rank 0: src = 3.095732e+09, tgt = 3.095732e+09, diff = 6.981874e+01
Reading SU2 AeroLoad File - surface_flow_aeroelastic_Iterative.csv
	Number of variables = 16
	Number of data points = 89
 CAPS Info: Bound 'Skin_Bottom' Normalized Integrated 'Pressure'
            Rank 0: src = 3.014252e+09, tgt = 3.014252e+09, diff = 1.062183e+02
Reading SU2 AeroLoad File - surface_flow_aeroelastic_Iterative.csv
	Number of variables = 16
	Number of data points = 89
 CAPS Info: Bound 'Skin_Tip' Normalized Integrated 'Pressure'
            Rank 0: src = 3.928484e+07, tgt = 3.928484e+07, diff = 3.600868e+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: https://su2code.github.io                        |
|                                                                       |
| The SU2 Project is maintained by the SU2 Foundation                   |
| (http://su2foundation.org)                                            |
-------------------------------------------------------------------------
| 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 <http://www.gnu.org/licenses/>.   |
-------------------------------------------------------------------------

----------------- 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.
10490 grid points.
54165 volume elements.
3 surface markers.
3448 boundary elements in index 0 (Marker = BC_1).
1565 boundary elements in index 1 (Marker = BC_2).
167 boundary elements in index 2 (Marker = BC_3).
54165 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 0.867414 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: https://su2code.github.io                        |
|                                                                       |
| The SU2 Project is maintained by the SU2 Foundation                   |
| (http://su2foundation.org)                                            |
-------------------------------------------------------------------------
| 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 <http://www.gnu.org/licenses/>.   |
-------------------------------------------------------------------------

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.
10490 grid points.
54165 volume elements.
3 surface markers.
3448 boundary elements in index 0 (Marker = BC_1).
1565 boundary elements in index 1 (Marker = BC_2).
167 boundary elements in index 2 (Marker = BC_3).
54165 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 12500 TETRAHEDRON volume elements.
There has been a re-orientation of 531 TRIANGLE surface elements.
Identifying edges and vertices.
Setting the control volume structure.
Volume of the computational grid: 106612.
Searching for the closest normal neighbors to the surfaces.
Storing a mapping from global to local point index.
Compute the surface curvature.
Max K: 182.951. Mean K: 1.9499. Standard deviation K: 9.51189.
Checking for periodicity.
Computing mesh quality statistics for the dual control volumes.
+--------------------------------------------------------------+
|           Mesh Quality Metric|        Minimum|        Maximum|
+--------------------------------------------------------------+
|    Orthogonality Angle (deg.)|        2.24714|        85.0345|
|     CV Face Area Aspect Ratio|        1.18189|        299.436|
|           CV Sub-Volume Ratio|              1|        73833.9|
+--------------------------------------------------------------+
Setting the multigrid structure.
+-------------------------------------------+
|  MG Level|       CVs|Aggl. Rate|       CFL|
+-------------------------------------------+
|         0|     10490|    1/1.00|        10|
|         1|      1870|    1/5.61|   8.44202|
|         2|       384|    1/4.87|   7.47081|
+-------------------------------------------+
Finding max control volume width.
Semi-span length = 11.1394 m.
Wetted area = 1268.81 m^2.
Area projection in the x-plane = 401.821 m^2, y-plane = 370.824 m^2, z-plane = 51.2847 m^2.
Max. coordinate in the x-direction = 3.33392 m, y-direction = 11.1394 m, z-direction = 41.5039 m.
Min. coordinate in the x-direction = -12.3774 m, y-direction = -0.516728 m, z-direction = -65.2783 m.
Checking if Euler & 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 https://su2code.github.io/docs_v7/Build-SU2-Linux-MacOS/#compiler-optimizations
WARNING: SU2 was not compiled for an AVX-capable architecture. Performance could be better,
         see https://su2code.github.io/docs_v7/Build-SU2-Linux-MacOS/#compiler-optimizations
WARNING: SU2 was not compiled for an AVX-capable architecture. Performance could be better,
         see https://su2code.github.io/docs_v7/Build-SU2-Linux-MacOS/#compiler-optimizations
+----------------------------------------------------------------------------------------------------------------------------------------------+
|   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|  1.6685e-01|    2.926740|    5.883462|    6.290990|    8.395846|   -0.006174|
|           0|           0|           1|  0.0000e+00|  0.0000e+00|  1.7272e-01|    3.384735|    5.930721|    6.086129|    8.759759|    0.191208|
|           0|           0|           2|  0.0000e+00|  0.0000e+00|  1.7393e-01|    3.465079|    6.005837|    6.089910|    8.822063|    0.206208|

----------------------------- Solver Exit -------------------------------

Maximum number of iterations reached (ITER = 3) before convergence.
+-----------------------------------------------------------------------+
|      Convergence Field     |     Value    |   Criterion  |  Converged |
+-----------------------------------------------------------------------+
|                    rms[Rho]|       3.46508|         < -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 269 non-physical points in the solution.
Warning: 8 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 = 89
 CAPS Info: Bound 'Skin_Top' Normalized Integrated 'Pressure'
            Rank 0: src = 1.313302e+09, tgt = 1.313301e+09, diff = 4.393883e+02
Reading SU2 AeroLoad File - surface_flow_aeroelastic_Iterative.csv
	Number of variables = 16
	Number of data points = 89
 CAPS Info: Bound 'Skin_Bottom' Normalized Integrated 'Pressure'
            Rank 0: src = 1.043453e+09, tgt = 1.043453e+09, diff = 9.408228e+01
Reading SU2 AeroLoad File - surface_flow_aeroelastic_Iterative.csv
	Number of variables = 16
	Number of data points = 89
 CAPS Info: Bound 'Skin_Tip' Normalized Integrated 'Pressure'
            Rank 0: src = 1.297344e+07, tgt = 1.297352e+07, diff = 8.441779e+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: https://su2code.github.io                        |
|                                                                       |
| The SU2 Project is maintained by the SU2 Foundation                   |
| (http://su2foundation.org)                                            |
-------------------------------------------------------------------------
| 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 <http://www.gnu.org/licenses/>.   |
-------------------------------------------------------------------------

----------------- 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.
10490 grid points.
54165 volume elements.
3 surface markers.
3448 boundary elements in index 0 (Marker = BC_1).
1565 boundary elements in index 1 (Marker = BC_2).
167 boundary elements in index 2 (Marker = BC_3).
54165 tetrahedra.

----------------------- Preprocessing computations ----------------------
Setting local point connectivity.
Checking the numerical grid orientation of the interior elements.
There has been a re-orientation of 12500 TETRAHEDRON volume elements.
There has been a re-orientation of 531 TRIANGLE surface elements.
Identify edges and vertices.
Setting the bound control volume structure.
Volume of the computational grid: 106612.
  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 21.640784 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: https://su2code.github.io                        |
|                                                                       |
| The SU2 Project is maintained by the SU2 Foundation                   |
| (http://su2foundation.org)                                            |
-------------------------------------------------------------------------
| 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 <http://www.gnu.org/licenses/>.   |
-------------------------------------------------------------------------

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.
10490 grid points.
54165 volume elements.
3 surface markers.
3448 boundary elements in index 0 (Marker = BC_1).
1565 boundary elements in index 1 (Marker = BC_2).
167 boundary elements in index 2 (Marker = BC_3).
54165 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 31813 TETRAHEDRON volume elements.
There has been a re-orientation of 1516 TRIANGLE surface elements.
Identifying edges and vertices.
Setting the control volume structure.
Volume of the computational grid: 1.29593e+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: 11.0516. Mean K: 0.307357. Standard deviation K: 0.990298.
Checking for periodicity.
Computing mesh quality statistics for the dual control volumes.
+--------------------------------------------------------------+
|           Mesh Quality Metric|        Minimum|        Maximum|
+--------------------------------------------------------------+
|    Orthogonality Angle (deg.)|       0.377156|        85.4318|
|     CV Face Area Aspect Ratio|        1.29339|         210999|
|           CV Sub-Volume Ratio|              1|         175159|
+--------------------------------------------------------------+
Setting the multigrid structure.
+-------------------------------------------+
|  MG Level|       CVs|Aggl. Rate|       CFL|
+-------------------------------------------+
|         0|     10490|    1/1.00|        10|
|         1|      1872|     1/5.6|   8.44503|
|         2|       383|    1/4.89|   7.46432|
+-------------------------------------------+
Finding max control volume width.
Semi-span length = 13.3552 m.
Wetted area = 709349 m^2.
Area projection in the x-plane = 464091 m^2, y-plane = 80491.9 m^2, z-plane = 5144.82 m^2.
Max. coordinate in the x-direction = 33.2369 m, y-direction = 13.3552 m, z-direction = 5208.87 m.
Min. coordinate in the x-direction = -32.8266 m, y-direction = -377.133 m, z-direction = -0.0403729 m.
Checking if Euler & 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 https://su2code.github.io/docs_v7/Build-SU2-Linux-MacOS/#compiler-optimizations
WARNING: SU2 was not compiled for an AVX-capable architecture. Performance could be better,
         see https://su2code.github.io/docs_v7/Build-SU2-Linux-MacOS/#compiler-optimizations
WARNING: SU2 was not compiled for an AVX-capable architecture. Performance could be better,
         see https://su2code.github.io/docs_v7/Build-SU2-Linux-MacOS/#compiler-optimizations
+----------------------------------------------------------------------------------------------------------------------------------------------+
|   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|  1.6351e-01|    6.490649|    9.452455|    9.631451|   11.959755|   -0.034218|
|           0|           0|           1|  0.0000e+00|  0.0000e+00|  1.7135e-01|    6.894879|    9.409837|    9.483196|   12.282706|   -0.034168|
|           0|           0|           2|  0.0000e+00|  0.0000e+00|  1.7310e-01|    6.982612|    9.479394|    9.493776|   12.359902|   -0.033133|

----------------------------- Solver Exit -------------------------------

Maximum number of iterations reached (ITER = 3) before convergence.
+-----------------------------------------------------------------------+
|      Convergence Field     |     Value    |   Criterion  |  Converged |
+-----------------------------------------------------------------------+
|                    rms[Rho]|       6.98261|         < -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 410 non-physical points in the solution.
Warning: 34 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 = 89
 CAPS Info: Bound 'Skin_Top' Normalized Integrated 'Pressure'
            Rank 0: src = 1.777310e+09, tgt = 1.777309e+09, diff = 6.371447e+02
Reading SU2 AeroLoad File - surface_flow_aeroelastic_Iterative.csv
	Number of variables = 16
	Number of data points = 89
 CAPS Info: Bound 'Skin_Bottom' Normalized Integrated 'Pressure'
            Rank 0: src = 1.287029e+09, tgt = 1.287029e+09, diff = 5.623313e+00
Reading SU2 AeroLoad File - surface_flow_aeroelastic_Iterative.csv
	Number of variables = 16
	Number of data points = 89
 CAPS Info: Bound 'Skin_Tip' Normalized Integrated 'Pressure'
            Rank 0: src = 5.336473e+06, tgt = 5.336475e+06, diff = 1.633793e+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: https://su2code.github.io                        |
|                                                                       |
| The SU2 Project is maintained by the SU2 Foundation                   |
| (http://su2foundation.org)                                            |
-------------------------------------------------------------------------
| 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 <http://www.gnu.org/licenses/>.   |
-------------------------------------------------------------------------

----------------- 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.
10490 grid points.
54165 volume elements.
3 surface markers.
3448 boundary elements in index 0 (Marker = BC_1).
1565 boundary elements in index 1 (Marker = BC_2).
167 boundary elements in index 2 (Marker = BC_3).
54165 tetrahedra.

----------------------- Preprocessing computations ----------------------
Setting local point connectivity.
Checking the numerical grid orientation of the interior elements.
There has been a re-orientation of 31813 TETRAHEDRON volume elements.
There has been a re-orientation of 1516 TRIANGLE surface elements.
Identify edges and vertices.
Setting the bound control volume structure.
Volume of the computational grid: 1.29593e+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.

WARNING: Convexity is not checked for 3D elements (issue #1171).


Completed in 22.186779 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: https://su2code.github.io                        |
|                                                                       |
| The SU2 Project is maintained by the SU2 Foundation                   |
| (http://su2foundation.org)                                            |
-------------------------------------------------------------------------
| 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 <http://www.gnu.org/licenses/>.   |
-------------------------------------------------------------------------

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.
10490 grid points.
54165 volume elements.
3 surface markers.
3448 boundary elements in index 0 (Marker = BC_1).
1565 boundary elements in index 1 (Marker = BC_2).
167 boundary elements in index 2 (Marker = BC_3).
54165 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 17632 TETRAHEDRON volume elements.
There has been a re-orientation of 1516 TRIANGLE surface elements.
Identifying edges and vertices.
Setting the control volume structure.
Volume of the computational grid: 7.55067e+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: 42.7789. Mean K: 0.268641. Standard deviation K: 1.44892.
Checking for periodicity.
Computing mesh quality statistics for the dual control volumes.
+--------------------------------------------------------------+
|           Mesh Quality Metric|        Minimum|        Maximum|
+--------------------------------------------------------------+
|    Orthogonality Angle (deg.)|       0.228375|        84.0716|
|     CV Face Area Aspect Ratio|        1.69341|    3.29101e+07|
|           CV Sub-Volume Ratio|              1|    8.95906e+08|
+--------------------------------------------------------------+
Setting the multigrid structure.
+-------------------------------------------+
|  MG Level|       CVs|Aggl. Rate|       CFL|
+-------------------------------------------+
|         0|     10490|    1/1.00|        10|
|         1|      1889|    1/5.55|   8.47052|
|         2|       397|    1/4.76|   7.55418|
+-------------------------------------------+
Finding max control volume width.
Semi-span length = 79.3623 m.
Wetted area = 19427 m^2.
Area projection in the x-plane = 6431.92 m^2, y-plane = 5648.53 m^2, z-plane = 632.165 m^2.
Max. coordinate in the x-direction = 4.33646 m, y-direction = 79.3623 m, z-direction = 16.332 m.
Min. coordinate in the x-direction = -40.9042 m, y-direction = -2.63233 m, z-direction = -834.953 m.
Checking if Euler & 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 https://su2code.github.io/docs_v7/Build-SU2-Linux-MacOS/#compiler-optimizations
WARNING: SU2 was not compiled for an AVX-capable architecture. Performance could be better,
         see https://su2code.github.io/docs_v7/Build-SU2-Linux-MacOS/#compiler-optimizations
WARNING: SU2 was not compiled for an AVX-capable architecture. Performance could be better,
         see https://su2code.github.io/docs_v7/Build-SU2-Linux-MacOS/#compiler-optimizations
+----------------------------------------------------------------------------------------------------------------------------------------------+
|   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|  1.6530e-01|    8.934634|   11.901490|   11.850216|   14.403740|   -0.199529|
|           0|           0|           1|  0.0000e+00|  0.0000e+00|  1.7228e-01|    9.335753|   11.918618|   11.861994|   14.764113|   -0.167720|
|           0|           0|           2|  0.0000e+00|  0.0000e+00|  1.7469e-01|    9.369968|   11.908253|   11.855002|   14.795135|   -0.168770|

----------------------------- Solver Exit -------------------------------

Maximum number of iterations reached (ITER = 3) before convergence.
+-----------------------------------------------------------------------+
|      Convergence Field     |     Value    |   Criterion  |  Converged |
+-----------------------------------------------------------------------+
|                    rms[Rho]|       9.36997|         < -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 605 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	1m16.501s
user	1m21.259s
sys	0m8.401s
+ 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/ESPbeta/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/ESPbeta/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 9.17.15
AFLR2    : Version Date   04/23/24 @ 12:51AM
AFLR2    : Compile OS     Darwin 23.4.0 arm64
AFLR2    : Compile Date   04/23/24 @ 12:51AM
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 11.5.14
AFLR4    : Version Date   04/18/24 @ 12:45PM
AFLR4    : Compile OS     Darwin 23.4.0 arm64
AFLR4    : Compile Date   04/18/24 @ 03:04PM
AFLR4    : Copyright 1994-2021, D.L. Marcum
AFLR4    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.8.0
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    : Auto Mode Turned OFF

OVERALL  : CPU Time          =     0.073   seconds
Body 1 (of 1)
Number of nodes    = 9343
Number of elements = 18682
Number of triangle elements      = 18682
Number of quadrilateral elements = 0
----------------------------
Total number of nodes    = 9343
Total number of elements = 18682
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 9.17.15
AFLR2    : Version Date   04/23/24 @ 12:51AM
AFLR2    : Compile OS     Darwin 23.4.0 arm64
AFLR2    : Compile Date   04/23/24 @ 12:51AM
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 11.5.14
AFLR4    : Version Date   04/18/24 @ 12:45PM
AFLR4    : Compile OS     Darwin 23.4.0 arm64
AFLR4    : Compile Date   04/18/24 @ 03:04PM
AFLR4    : Copyright 1994-2021, D.L. Marcum
AFLR4    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------
Volume mesh:
	Number of nodes          = 57531
	Number of elements       = 331031
	Number of triangles      = 18682
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 312349
	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: https://su2code.github.io                        |
|                                                                       |
| The SU2 Project is maintained by the SU2 Foundation                   |
| (http://su2foundation.org)                                            |
-------------------------------------------------------------------------
| 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 <http://www.gnu.org/licenses/>.   |
-------------------------------------------------------------------------

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.
57531 grid points.
312349 volume elements.
3 surface markers.
12288 boundary elements in index 0 (Marker = BC_1).
5867 boundary elements in index 1 (Marker = BC_2).
527 boundary elements in index 2 (Marker = BC_3).
312349 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: 102.753. Mean K: 0.74689. Standard deviation K: 4.38956.
Checking for periodicity.
Computing mesh quality statistics for the dual control volumes.
+--------------------------------------------------------------+
|           Mesh Quality Metric|        Minimum|        Maximum|
+--------------------------------------------------------------+
|    Orthogonality Angle (deg.)|        48.3512|        86.0919|
|     CV Face Area Aspect Ratio|        1.11561|        35.2066|
|           CV Sub-Volume Ratio|              1|        18.8559|
+--------------------------------------------------------------+
Setting the multigrid structure.
+-------------------------------------------+
|  MG Level|       CVs|Aggl. Rate|       CFL|
+-------------------------------------------+
|         0|     57531|    1/1.00|        10|
|         1|      9779|    1/5.88|   8.30913|
|         2|      1716|     1/5.7|   6.97784|
+-------------------------------------------+
Finding max control volume width.
Semi-span length = 3.87298 m.
Wetted area = 9.04169 m^2.
Area projection in the x-plane = 0.644461 m^2, y-plane = 0.295795 m^2, z-plane = 4.29819 m^2.
Max. coordinate in the x-direction = 2.53651 m, y-direction = 3.87298 m, z-direction = 0.379751 m.
Min. coordinate in the x-direction = 0 m, y-direction = -2.86125e-18 m, z-direction = -0.0467278 m.
Checking if Euler & 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 https://su2code.github.io/docs_v7/Build-SU2-Linux-MacOS/#compiler-optimizations
WARNING: SU2 was not compiled for an AVX-capable architecture. Performance could be better,
         see https://su2code.github.io/docs_v7/Build-SU2-Linux-MacOS/#compiler-optimizations
WARNING: SU2 was not compiled for an AVX-capable architecture. Performance could be better,
         see https://su2code.github.io/docs_v7/Build-SU2-Linux-MacOS/#compiler-optimizations
+----------------------------------------------------------------------------------------------------------------------------------------------+
|   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|  9.8433e-01|   -1.299765|    0.996854|    0.627451|    4.169341|   -0.962501|
|           0|           0|           1|  0.0000e+00|  0.0000e+00|  9.7649e-01|   -1.689451|    0.841935|    0.460737|    3.766643|   -0.517631|
|           0|           0|           2|  0.0000e+00|  0.0000e+00|  9.7319e-01|   -1.703013|    0.658675|    0.298032|    3.753378|    1.611420|

----------------------------- Solver Exit -------------------------------

Maximum number of iterations reached (ITER = 3) before convergence.
+-----------------------------------------------------------------------+
|      Convergence Field     |     Value    |   Criterion  |  Converged |
+-----------------------------------------------------------------------+
|                    rms[Rho]|      -1.70301|         < -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 = 273
 CAPS Info: Bound 'Skin_Top' Normalized Integrated 'Temperature'
            Rank 0: src = 1.497349e+03, tgt = 1.497349e+03, diff = 5.478862e-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 = 273
 CAPS Info: Bound 'Skin_Bottom' Normalized Integrated 'Temperature'
            Rank 0: src = 1.453938e+03, tgt = 1.453938e+03, diff = 6.644339e-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 = 273
 CAPS Info: Bound 'Skin_Tip' Normalized Integrated 'Temperature'
            Rank 0: src = 2.083892e+01, tgt = 2.083892e+01, diff = 5.435652e-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	0m9.986s
user	0m10.492s
sys	0m0.885s
+ 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/ESPbeta/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
gp.py test;
+ python -u gp.py -outLevel=0
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/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	0m1.865s
user	0m1.374s
sys	0m0.103s
+ 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/ESPbeta/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
qp.py test;
+ python -u qp.py -outLevel=0
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/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	0m0.719s
user	0m1.246s
sys	0m0.049s
+ 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/ESPbeta/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
sp.py test;
+ python -u sp.py -outLevel=0
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/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	0m0.707s
user	0m1.234s
sys	0m0.051s
+ 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/ESPbeta/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
boydBox.py test;
+ python -u boydBox.py -outLevel=0
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/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	0m0.622s
user	0m1.149s
sys	0m0.049s
+ 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/ESPbeta/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
hoburg_gp.py test;
+ python -u hoburg_gp.py -outLevel=0
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/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	0m4.671s
user	0m5.177s
sys	0m0.053s
+ 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/ESPbeta/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
hoburg_blackbox.py test;
+ python -u hoburg_blackbox.py -outLevel=0
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/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	0m18.726s
user	0m19.182s
sys	0m0.086s
+ 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/ESPbeta/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
pyCAPS/sizeWing.py test;
+ python -u pyCAPS/sizeWing.py -outLevel=0
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/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	0m0.887s
user	0m1.386s
sys	0m0.078s
+ status=0
+ set +x

=================================================
CAPS verification (using pyCAPS) case pyCAPS/sizeWing.py passed (as expected)
=================================================

avl: /Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/EngSketchPad/bin/avl

=================================================
+ echo 'pyCAPS/optTaperAvl.py test;'
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
pyCAPS/optTaperAvl.py test;
+ python -u pyCAPS/optTaperAvl.py -outLevel=0
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/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	0m3.316s
user	0m2.707s
sys	0m1.115s
+ 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/ESPbeta/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
pyCAPS/optWingAvl.py test;
+ python -u pyCAPS/optWingAvl.py -outLevel=0
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
nrock 2
Starting iteration 0 at 0.1482 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: [<Quantity(0.060834734963571835, 'dimensionless')>, <Quantity(-0.0014769756679916535, 'dimensionless')>]
Calling cvxopt.solvers.cp at 0.7434 seconds
Got sol from cvxopt at 0.7668 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: [<Quantity(0.06359341837018917, 'dimensionless')>, <Quantity(-0.0014812479862164052, 'dimensionless')>]
logspace stuff at 1.3549 seconds
Starting iteration 1 at 1.3699 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 1.3738 seconds
Got sol from cvxopt at 1.3806 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: [<Quantity(0.061358790088644755, 'dimensionless')>, <Quantity(-0.001469791715157931, 'dimensionless')>]
logspace stuff at 1.9784 seconds
Starting iteration 2 at 1.9958 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 1.9997 seconds
Got sol from cvxopt at 2.0068 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: [<Quantity(0.05073085616785211, 'dimensionless')>, <Quantity(-0.001419190987608232, 'dimensionless')>]
logspace stuff at 2.5999 seconds
Starting iteration 3 at 2.6177 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 2.6215 seconds
Got sol from cvxopt at 2.6284 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: [<Quantity(0.009583432732646058, 'dimensionless')>, <Quantity(-0.0013533445524760435, 'dimensionless')>]
logspace stuff at 3.2204 seconds
Starting iteration 4 at 3.2384 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 3.2424 seconds
Got sol from cvxopt at 3.2490 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: [<Quantity(-0.0008541793310445911, 'dimensionless')>, <Quantity(-0.0013850816280491784, 'dimensionless')>]
logspace stuff at 3.8423 seconds
Starting iteration 5 at 3.8598 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 3.8636 seconds
Got sol from cvxopt at 3.8706 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: [<Quantity(-6.436454802472014e-06, 'dimensionless')>, <Quantity(-0.0013814190268079951, 'dimensionless')>]
logspace stuff at 4.4536 seconds
Starting iteration 6 at 4.4715 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 4.4753 seconds
Got sol from cvxopt at 4.4820 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: [<Quantity(-5.709581030188815e-07, 'dimensionless')>, <Quantity(-0.0013813957758107565, 'dimensionless')>]
logspace stuff at 5.0685 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	0m5.943s
user	0m4.385s
sys	0m1.975s
+ 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/ESPbeta/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
pyCAPS/GPSize.py test;
+ python -u pyCAPS/GPSize.py -outLevel=0
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/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	0m4.824s
user	0m5.274s
sys	0m0.122s
+ status=0
+ set +x

=================================================
CAPS verification (using pyCAPS) case pyCAPS/GPSize.py passed (as expected)
=================================================

mses: /Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/EngSketchPad/bin/mses

=================================================
+ echo 'pyCAPS/MSES.py test;'
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
pyCAPS/MSES.py test;
+ python -u pyCAPS/MSES.py -outLevel=0
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/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	3m28.522s
user	3m24.728s
sys	0m3.887s
+ 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/ESPbeta/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
pyCAPS/Camber.py test;
+ python -u pyCAPS/Camber.py -outLevel=0
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/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	11m10.718s
user	10m57.545s
sys	0m12.219s
+ 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/ESPbeta/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
pyCAPS/CMConstraint.py test;
+ python -u pyCAPS/CMConstraint.py -outLevel=0
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/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	3m41.493s
user	3m37.783s
sys	0m3.789s
+ status=0
+ set +x

=================================================
CAPS verification (using pyCAPS) case pyCAPS/CMConstraint.py passed (as expected)
=================================================

Traceback (most recent call last):
  File "<string>", line 1, in <module>
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
+ mkdir -p /Users/jenkins/workspace/ESP_bPreBuilt/test/plugs
+ cd /Users/jenkins/workspace/ESP_bPreBuilt/test/plugs
+ find /Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/EngSketchPad/data/Plugs -name 'plugs0*.csm'
+ sort -f
+ awk '{ n=split($0, a, ";"); for(i=1; i<=n; i+=2) print a[i] }' /Users/jenkins/workspace/ESP_bPreBuilt/JenkinsESP/data/plugs/plugsFailure.txt
+ cp /Users/jenkins/workspace/ESP_bPreBuilt/JenkinsESP/data/plugs/plugsIgnore.txt .
+ set +x
Testing CSM files:
data/Plugs/plugs0a.csm
data/Plugs/plugs0b.csm
data/Plugs/plugs0c.csm
data/Plugs/plugs0d.csm
total 46632
-rw-r--r--  1 jenkins  staff   1.2M Apr 27 18:02 ASTRO.D01
-rw-r--r--  1 jenkins  staff   277K Apr 27 18:02 ASTRO.IDX
-rwxr-xr-x  1 jenkins  staff   130K Apr 27 18:03 ESPxddm
-rwxr-xr-x  1 jenkins  staff   212K Apr 27 18:03 Slugs
-rwxr-xr-x  1 jenkins  staff    86K Apr 27 18:03 TestFit
-rwxr-xr-x  1 jenkins  staff   1.6M Apr 27 18:02 avl
-rwxr-xr-x  1 jenkins  staff    51K Apr 28 10:39 cart3dTest
-rwxr-xr-x  1 jenkins  staff    51K Apr 28 10:39 egads2cart
-rwxr-xr-x  1 jenkins  staff    70K Apr 27 18:03 egads2cgt
-rwxr-xr-x  1 jenkins  staff   403K Apr 27 18:02 friction
-rwxr-xr-x  1 jenkins  staff    10M Apr 27 18:02 mastros.exe
-rwxr-xr-x  1 jenkins  staff   749K Apr 27 18:02 mses
-rwxr-xr-x  1 jenkins  staff   1.4M Apr 27 18:02 mset
-rwxr-xr-x  1 jenkins  staff    51K Apr 28 10:39 phaseUtil
-rw-r--r--  1 jenkins  staff   1.6K Apr 28 13:00 pod.egads
-rw-r--r--  1 jenkins  staff     0B Apr 28 13:00 port7681.jrnl
-rwxr-xr-x  1 jenkins  staff   1.2M Apr 27 18:02 pplot
-rwxr-xr-x  1 jenkins  staff   1.1M Apr 27 18:02 pxplot
-rwxr-xr-x  1 jenkins  staff    68K Apr 28 10:39 sensCSM
-rwxr-xr-x  1 jenkins  staff   192K Apr 27 18:03 serveCSM
-rwxr-xr-x  1 jenkins  staff   176K Apr 27 18:03 serveESP
-rwxr-xr-x  1 jenkins  staff    52K Apr 27 18:03 vCurvature
-rwxr-xr-x  1 jenkins  staff    51K Apr 27 18:03 vGeom
-rwxr-xr-x  1 jenkins  staff    53K Apr 27 18:03 vTess
-rwxr-xr-x  1 jenkins  staff   1.7M Apr 27 18:03 vTesstatic
-rw-r--r--  1 jenkins  staff   195K Apr 28 13:00 wingMultiModel.bdf
-rwxr-xr-x  1 jenkins  staff   1.7M Apr 27 18:02 xfoil
( 1 / 4 )
data/Plugs/plugs0a.csm;
++ /Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/EngSketchPad/bin/serveCSM /Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/EngSketchPad/data/Plugs/plugs0a.csm -outLevel 0 -plugs 25 -plot /Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/EngSketchPad/data/Plugs/plugs0.cloud -batch -verify -jrnl /Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/EngSketchPad/data/Plugs/buildFinal.jrnl
WARNING:: cannot open "/Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/EngSketchPad/data/Plugs/verify_7.8.0/plugs0a.vfy", so verification is being skipped

===================================
PLUGS with 4562 points in the cloud
===================================


PLUGS phase1: match bounding boxes


PLUGS phase2: match cloud points
Starting pass 1 (of 25) of phase2
    Pass  1 converged, dmax= 5.416e-07,     rmsbest= 6.132e-04, reclass= 4562, unclass=    0
Starting pass 2 (of 25) of phase2
    Pass  2 converged, dmax= 5.366e-07,     rmsbest= 7.097e-04, reclass=    2, unclass=    0
Starting pass 3 (of 25) of phase2

    Phase2 passes converged because points are classified same as previous pass


==> Opening input journal file "/Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/EngSketchPad/data/Plugs/buildFinal.jrnl"


==> Closing input journal file

==> serveCSM completed successfully with no verification data

real	0m4.384s
user	0m4.390s
sys	0m0.234s
++ set +x
data/Plugs/plugs0a                  passed (as expected)
--------------------------------------------------------------------------------------------------
( 2 / 4 )
data/Plugs/plugs0b.csm;
++ /Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/EngSketchPad/bin/serveCSM /Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/EngSketchPad/data/Plugs/plugs0b.csm -outLevel 0 -plugs 25 -plot /Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/EngSketchPad/data/Plugs/plugs0.cloud -batch -verify -jrnl /Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/EngSketchPad/data/Plugs/buildFinal.jrnl
WARNING:: cannot open "/Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/EngSketchPad/data/Plugs/verify_7.8.0/plugs0b.vfy", so verification is being skipped

===================================
PLUGS with 4562 points in the cloud
===================================


PLUGS phase1: match bounding boxes


PLUGS phase2: match cloud points
Starting pass 1 (of 25) of phase2
    Pass  1 converged, dmax= 3.039e-07,     rmsbest= 4.036e-02, reclass= 4562, unclass=    0
Starting pass 2 (of 25) of phase2
    Pass  2 converged, dmax= 2.814e-07,     rmsbest= 1.924e-03, reclass= 1033, unclass=    0
Starting pass 3 (of 25) of phase2
    Pass  3 converged, dmax= 4.494e-07,     rmsbest= 5.920e-04, reclass=  473, unclass=    0
Starting pass 4 (of 25) of phase2
    Pass  4 converged, dmax= 5.366e-07,     rmsbest= 7.097e-04, reclass=   17, unclass=    0
Starting pass 5 (of 25) of phase2

    Phase2 passes converged because points are classified same as previous pass


==> Opening input journal file "/Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/EngSketchPad/data/Plugs/buildFinal.jrnl"


==> Closing input journal file

==> serveCSM completed successfully with no verification data

real	0m3.917s
user	0m4.891s
sys	0m0.026s
++ set +x
data/Plugs/plugs0b                  passed (as expected)
--------------------------------------------------------------------------------------------------
( 3 / 4 )
data/Plugs/plugs0c.csm;
++ /Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/EngSketchPad/bin/serveCSM /Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/EngSketchPad/data/Plugs/plugs0c.csm -outLevel 0 -plugs 25 -plot /Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/EngSketchPad/data/Plugs/plugs0.cloud -batch -verify -jrnl /Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/EngSketchPad/data/Plugs/buildFinal.jrnl
WARNING:: cannot open "/Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/EngSketchPad/data/Plugs/verify_7.8.0/plugs0c.vfy", so verification is being skipped

===================================
PLUGS with 4562 points in the cloud
===================================


PLUGS phase1: match bounding boxes


PLUGS phase2: match cloud points
Starting pass 1 (of 25) of phase2
    Pass  1 ran out of iterations,          rmsbest= 1.677e-01, reclass= 4562, unclass=  554
Starting pass 2 (of 25) of phase2
    Pass  2 converged, dmax= 4.016e-07,     rmsbest= 6.330e-02, reclass= 1676, unclass=    0
Starting pass 3 (of 25) of phase2
    Pass  3 converged, dmax= 1.881e-07,     rmsbest= 8.736e-03, reclass=  791, unclass=    0
Starting pass 4 (of 25) of phase2
    Pass  4 converged, dmax= 3.081e-07,     rmsbest= 1.037e-03, reclass=  428, unclass=    0
Starting pass 5 (of 25) of phase2
    Pass  5 converged, dmax= 5.816e-07,     rmsbest= 7.097e-04, reclass=  109, unclass=    0
Starting pass 6 (of 25) of phase2

    Phase2 passes converged because points are classified same as previous pass


==> Opening input journal file "/Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/EngSketchPad/data/Plugs/buildFinal.jrnl"


==> Closing input journal file

==> serveCSM completed successfully with no verification data

real	0m12.259s
user	0m19.423s
sys	0m0.055s
++ set +x
data/Plugs/plugs0c                  passed (as expected)
--------------------------------------------------------------------------------------------------
( 4 / 4 )
data/Plugs/plugs0d.csm;
++ /Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/EngSketchPad/bin/serveCSM /Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/EngSketchPad/data/Plugs/plugs0d.csm -outLevel 0 -plugs 25 -plot /Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/EngSketchPad/data/Plugs/plugs0.cloud -batch -verify -jrnl /Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/EngSketchPad/data/Plugs/buildFinal.jrnl
WARNING:: cannot open "/Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/EngSketchPad/data/Plugs/verify_7.8.0/plugs0d.vfy", so verification is being skipped

===================================
PLUGS with 4562 points in the cloud
===================================


PLUGS phase1: match bounding boxes


PLUGS phase2: match cloud points
Starting pass 1 (of 25) of phase2
    Pass  1 ran out of iterations,          rmsbest= 1.677e-01, reclass= 4562, unclass=  554
Starting pass 2 (of 25) of phase2
    Pass  2 converged, dmax= 4.016e-07,     rmsbest= 6.330e-02, reclass= 1676, unclass=    0
Starting pass 3 (of 25) of phase2
    Pass  3 converged, dmax= 1.881e-07,     rmsbest= 8.736e-03, reclass=  791, unclass=    0
Starting pass 4 (of 25) of phase2
    Pass  4 converged, dmax= 3.081e-07,     rmsbest= 1.037e-03, reclass=  428, unclass=    0
Starting pass 5 (of 25) of phase2
    Pass  5 converged, dmax= 5.816e-07,     rmsbest= 7.097e-04, reclass=  109, unclass=    0
Starting pass 6 (of 25) of phase2

    Phase2 passes converged because points are classified same as previous pass


==> Opening input journal file "/Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/EngSketchPad/data/Plugs/buildFinal.jrnl"


==> Closing input journal file

==> serveCSM completed successfully with no verification data

real	0m12.216s
user	0m19.343s
sys	0m0.052s
++ set +x
data/Plugs/plugs0d                  passed (as expected)
--------------------------------------------------------------------------------------------------
[Execution node] check if [viggen] is in [[windows10x64]]
Run condition [Execution node ] preventing perform for step [Execute Windows batch command]
[GNU C Compiler (gcc)] Parsing console log (workspace: '/Users/jenkins/workspace/ESP_bPreBuilt')
[GNU C Compiler (gcc)] Successfully parsed console log
[GNU C Compiler (gcc)] -> found 0 issues (skipped 0 duplicates)
[GNU C Compiler (gcc)] Skipping post processing
[GNU C Compiler (gcc)] No filter has been set, publishing all 0 issues
[GNU C Compiler (gcc)] Repository miner is not configured, skipping repository mining
[Clang] Parsing console log (workspace: '/Users/jenkins/workspace/ESP_bPreBuilt')
[Clang] -> found 0 issues (skipped 0 duplicates)
[Clang] Parsing console log (workspace: '/Users/jenkins/workspace/ESP_bPreBuilt')
[Clang] -> found 0 issues (skipped 0 duplicates)
[Clang] Successfully parsed console log
[Clang] -> found 0 issues (skipped 0 duplicates)
[Clang] Parsing console log (workspace: '/Users/jenkins/workspace/ESP_bPreBuilt')
[Clang] Skipping post processing
[Clang] No filter has been set, publishing all 0 issues
[Clang] Repository miner is not configured, skipping repository mining
[Static Analysis] Successfully parsed console log
[Static Analysis] -> found 0 issues (skipped 0 duplicates)
[Static Analysis] Parsing console log (workspace: '/Users/jenkins/workspace/ESP_bPreBuilt')
[Static Analysis] Successfully parsed console log
[Static Analysis] -> found 0 issues (skipped 0 duplicates)
[Static Analysis] Skipping post processing
[Static Analysis] No filter has been set, publishing all 0 issues
[Static Analysis] Repository miner is not configured, skipping repository mining
[Static Analysis] Successfully parsed console log
[Static Analysis] -> found 0 issues (skipped 0 duplicates)
[Static Analysis] Successfully parsed console log
[Static Analysis] -> found 0 issues (skipped 0 duplicates)
[Static Analysis] Successfully parsed console log
[Static Analysis] -> found 0 issues (skipped 0 duplicates)
[Static Analysis] Parsing console log (workspace: '/Users/jenkins/workspace/ESP_bPreBuilt')
[Static Analysis] Skipping post processing
[Static Analysis] No filter has been set, publishing all 0 issues
[Static Analysis] Repository miner is not configured, skipping repository mining
[Static Analysis] Reference build recorder is not configured
[Static Analysis] No valid reference build found
[Static Analysis] All reported issues will be considered outstanding
[Static Analysis] No quality gates have been set - skipping
[Static Analysis] Health report is disabled - skipping
[Static Analysis] Created analysis result for 0 issues (found 0 new issues, fixed 0 issues)
[Static Analysis] Attaching ResultAction with ID 'analysis' to build 'ESP_bPreBuilt/ESPVersion=beta,buildnode=viggen #69'.
[Checks API] No suitable checks publisher found.
[WS-CLEANUP] Deleting project workspace...
[WS-CLEANUP] Deferred wipeout is used...
[WS-CLEANUP] done
Finished: SUCCESS