Started by upstream project "ESP_bPreBuilt" build number 66
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...
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 '2024-03-06T16:57:01.039 -0500' --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 2473

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 '2024-03-06T16:57:01.039 -0500' --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 850

No changes for svn+ssh://acdl.mit.edu/home/svnroot/OpenCSM/trunk/Jenkins since the previous build
No changes for svn+ssh://acdl.mit.edu/home/svnroot/JenkinsESP since the previous build
[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/jenkins15866061803855717224.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=11.5.9
++ SU2_VERSION=8.0.0
++ TETGEN_VERSION=1.6.0
++ VSP_VERSION=3.34.0
++ export PYTHON_VERSION=3.11.6
++ PYTHON_VERSION=3.11.6
++ 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
++ [[ 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_11.5.9
++ AFLR=/Users/jenkins/util/AFLR/aflr_lib_11.5.9
++ [[ 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 ]]
++ 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-3.11.6/bin/python3 /Users/jenkins/workspace/ESP_bPreBuilt/ESP//bin/python
++ ln -s /Users/jenkins/util/ESP/Python/ESP_Python-3.11.6/bin/python3-config /Users/jenkins/workspace/ESP_bPreBuilt/ESP//bin/python-config
++ ln -s /Users/jenkins/util/ESP/Python/ESP_Python-3.11.6/bin/virtualenv /Users/jenkins/workspace/ESP_bPreBuilt/ESP//bin/virtualenv
+++ ls /Users/jenkins/util/ESP/Python/ESP_Python-3.11.6/bin/analyze-build /Users/jenkins/util/ESP/Python/ESP_Python-3.11.6/bin/analyze-c++ /Users/jenkins/util/ESP/Python/ESP_Python-3.11.6/bin/analyze-cc /Users/jenkins/util/ESP/Python/ESP_Python-3.11.6/bin/intercept-build /Users/jenkins/util/ESP/Python/ESP_Python-3.11.6/bin/intercept-c++ /Users/jenkins/util/ESP/Python/ESP_Python-3.11.6/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-${PYTHON_VERSION}/bin/intercept-*`'
+++ basename /Users/jenkins/util/ESP/Python/ESP_Python-3.11.6/bin/analyze-build
+++ basename /Users/jenkins/util/ESP/Python/ESP_Python-3.11.6/bin/analyze-build
++ ln -s /Users/jenkins/util/ESP/Python/ESP_Python-3.11.6/bin/analyze-build /Users/jenkins/workspace/ESP_bPreBuilt/ESP//bin/analyze-build
++ for i in '`ls /Users/jenkins/util/ESP/Python/ESP_Python-${PYTHON_VERSION}/bin/analyze-* /Users/jenkins/util/ESP/Python/ESP_Python-${PYTHON_VERSION}/bin/intercept-*`'
+++ basename /Users/jenkins/util/ESP/Python/ESP_Python-3.11.6/bin/analyze-c++
+++ basename /Users/jenkins/util/ESP/Python/ESP_Python-3.11.6/bin/analyze-c++
++ ln -s /Users/jenkins/util/ESP/Python/ESP_Python-3.11.6/bin/analyze-c++ /Users/jenkins/workspace/ESP_bPreBuilt/ESP//bin/analyze-c++
++ for i in '`ls /Users/jenkins/util/ESP/Python/ESP_Python-${PYTHON_VERSION}/bin/analyze-* /Users/jenkins/util/ESP/Python/ESP_Python-${PYTHON_VERSION}/bin/intercept-*`'
+++ basename /Users/jenkins/util/ESP/Python/ESP_Python-3.11.6/bin/analyze-cc
+++ basename /Users/jenkins/util/ESP/Python/ESP_Python-3.11.6/bin/analyze-cc
++ ln -s /Users/jenkins/util/ESP/Python/ESP_Python-3.11.6/bin/analyze-cc /Users/jenkins/workspace/ESP_bPreBuilt/ESP//bin/analyze-cc
++ for i in '`ls /Users/jenkins/util/ESP/Python/ESP_Python-${PYTHON_VERSION}/bin/analyze-* /Users/jenkins/util/ESP/Python/ESP_Python-${PYTHON_VERSION}/bin/intercept-*`'
+++ basename /Users/jenkins/util/ESP/Python/ESP_Python-3.11.6/bin/intercept-build
+++ basename /Users/jenkins/util/ESP/Python/ESP_Python-3.11.6/bin/intercept-build
++ ln -s /Users/jenkins/util/ESP/Python/ESP_Python-3.11.6/bin/intercept-build /Users/jenkins/workspace/ESP_bPreBuilt/ESP//bin/intercept-build
++ for i in '`ls /Users/jenkins/util/ESP/Python/ESP_Python-${PYTHON_VERSION}/bin/analyze-* /Users/jenkins/util/ESP/Python/ESP_Python-${PYTHON_VERSION}/bin/intercept-*`'
+++ basename /Users/jenkins/util/ESP/Python/ESP_Python-3.11.6/bin/intercept-c++
+++ basename /Users/jenkins/util/ESP/Python/ESP_Python-3.11.6/bin/intercept-c++
++ ln -s /Users/jenkins/util/ESP/Python/ESP_Python-3.11.6/bin/intercept-c++ /Users/jenkins/workspace/ESP_bPreBuilt/ESP//bin/intercept-c++
++ for i in '`ls /Users/jenkins/util/ESP/Python/ESP_Python-${PYTHON_VERSION}/bin/analyze-* /Users/jenkins/util/ESP/Python/ESP_Python-${PYTHON_VERSION}/bin/intercept-*`'
+++ basename /Users/jenkins/util/ESP/Python/ESP_Python-3.11.6/bin/intercept-cc
+++ basename /Users/jenkins/util/ESP/Python/ESP_Python-3.11.6/bin/intercept-cc
++ ln -s /Users/jenkins/util/ESP/Python/ESP_Python-3.11.6/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-3.11.6/include/python3.11 -I/Users/jenkins/util/ESP/Python/ESP_Python-3.11.6/include/python3.11'
++ PYTHONINC='. -I/Users/jenkins/util/ESP/Python/ESP_Python-3.11.6/include/python3.11 -I/Users/jenkins/util/ESP/Python/ESP_Python-3.11.6/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-3.11.6/lib -lpython3.11 -ldl -framework CoreFoundation'
++ PYTHONLIB='-L/Users/jenkins/util/ESP/Python/ESP_Python-3.11.6/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-3.11.6/lib -lpython3.11 -ldl -framework CoreFoundation -Wl,-w'
++ PYTHONLIB='-L/Users/jenkins/util/ESP/Python/ESP_Python-3.11.6/lib -lpython3.11 -ldl -framework CoreFoundation -Wl,-w'
++ export PYTHONUNBUFFERED=true
++ PYTHONUNBUFFERED=true
++ export PYTHONFAULTHANDLER=true
++ PYTHONFAULTHANDLER=true
++ python --version
Python 3.11.6
++ [[ '' == \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
--2024-03-06 16:57:09--  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: 516790230 (493M) [application/x-gzip]
Saving to: ‘ESPbeta-macos-arm64.tgz’

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  9200K .......... .......... .......... .......... ..........  1% 8.11M 23s
  9250K .......... .......... .......... .......... ..........  1% 11.9M 23s
  9300K .......... .......... .......... .......... ..........  1% 17.1M 23s
  9350K .......... .......... .......... .......... ..........  1% 8.27M 23s
  9400K .......... .......... .......... .......... ..........  1% 6.80M 24s
  9450K .......... .......... .......... .......... ..........  1% 8.82M 24s
  9500K .......... .......... .......... .......... ..........  1% 9.69M 24s
  9550K .......... .......... .......... .......... ..........  1% 10.2M 24s
  9600K .......... .......... .......... .......... ..........  1% 9.94M 24s
  9650K .......... .......... .......... .......... ..........  1% 10.1M 24s
  9700K .......... .......... .......... .......... ..........  1% 18.2M 24s
  9750K .......... .......... .......... .......... ..........  1% 39.2M 24s
  9800K .......... .......... .......... .......... ..........  1% 37.0M 24s
  9850K .......... .......... .......... .......... ..........  1% 34.1M 24s
  9900K .......... .......... .......... .......... ..........  1% 23.1M 24s
  9950K .......... .......... .......... .......... ..........  1% 95.0M 24s
 10000K .......... .......... .......... .......... ..........  1% 49.4M 24s
 10050K .......... .......... .......... .......... ..........  2% 20.6M 24s
 10100K .......... .......... .......... .......... ..........  2% 37.4M 24s
 10150K .......... .......... .......... .......... ..........  2% 23.5M 24s
 10200K .......... .......... .......... .......... ..........  2% 12.8M 24s
 10250K .......... .......... .......... .......... ..........  2% 15.0M 24s
 10300K .......... .......... .......... .......... ..........  2% 28.8M 24s
 10350K .......... .......... .......... .......... ..........  2% 15.3M 24s
 10400K .......... .......... .......... .......... ..........  2% 13.4M 24s
 10450K .......... .......... .......... .......... ..........  2% 13.8M 24s
 10500K .......... .......... .......... .......... ..........  2% 11.6M 24s
 10550K .......... .......... .......... .......... ..........  2% 12.9M 24s
 10600K .......... .......... .......... .......... ..........  2% 8.93M 24s
 10650K .......... .......... .......... .......... ..........  2% 9.89M 24s
 10700K .......... .......... .......... .......... ..........  2% 9.59M 25s
 10750K .......... .......... .......... .......... ..........  2% 10.4M 25s
 10800K .......... .......... .......... .......... ..........  2% 15.0M 25s
 10850K .......... .......... .......... .......... ..........  2% 12.1M 25s
 10900K .......... .......... .......... .......... ..........  2% 15.0M 25s
 10950K .......... .......... .......... .......... ..........  2% 13.3M 25s
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 11050K .......... .......... .......... .......... ..........  2% 15.1M 25s
 11100K .......... .......... .......... .......... ..........  2% 10.7M 25s
 11150K .......... .......... .......... .......... ..........  2% 11.7M 25s
 11200K .......... .......... .......... .......... ..........  2% 10.5M 25s
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 11300K .......... .......... .......... .......... ..........  2% 9.73M 25s
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 11400K .......... .......... .......... .......... ..........  2% 12.5M 25s
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 11550K .......... .......... .......... .......... ..........  2% 10.2M 26s
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 11650K .......... .......... .......... .......... ..........  2% 13.5M 26s
 11700K .......... .......... .......... .......... ..........  2% 10.9M 26s
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 11800K .......... .......... .......... .......... ..........  2% 11.1M 26s
 11850K .......... .......... .......... .......... ..........  2% 11.8M 26s
 11900K .......... .......... .......... .......... ..........  2% 14.8M 26s
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 12100K .......... .......... .......... .......... ..........  2% 15.1M 26s
 12150K .......... .......... .......... .......... ..........  2% 20.7M 26s
 12200K .......... .......... .......... .......... ..........  2% 13.4M 26s
 12250K .......... .......... .......... .......... ..........  2% 18.0M 26s
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 12350K .......... .......... .......... .......... ..........  2% 16.4M 26s
 12400K .......... .......... .......... .......... ..........  2% 18.8M 26s
 12450K .......... .......... .......... .......... ..........  2% 33.9M 26s
 12500K .......... .......... .......... .......... ..........  2% 50.9M 26s
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 12600K .......... .......... .......... .......... ..........  2% 13.5M 26s
 12650K .......... .......... .......... .......... ..........  2% 65.5M 26s
 12700K .......... .......... .......... .......... ..........  2% 39.6M 26s
 12750K .......... .......... .......... .......... ..........  2% 27.1M 26s
 12800K .......... .......... .......... .......... ..........  2% 17.0M 26s
 12850K .......... .......... .......... .......... ..........  2% 54.1M 26s
 12900K .......... .......... .......... .......... ..........  2% 22.0M 26s
 12950K .......... .......... .......... .......... ..........  2% 13.1M 26s
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 13050K .......... .......... .......... .......... ..........  2% 9.41M 26s
 13100K .......... .......... .......... .......... ..........  2% 7.91M 26s
 13150K .......... .......... .......... .......... ..........  2% 10.8M 26s
 13200K .......... .......... .......... .......... ..........  2% 10.7M 26s
 13250K .......... .......... .......... .......... ..........  2% 9.02M 27s
 13300K .......... .......... .......... .......... ..........  2% 11.7M 27s
 13350K .......... .......... .......... .......... ..........  2% 8.76M 27s
 13400K .......... .......... .......... .......... ..........  2% 11.0M 27s
 13450K .......... .......... .......... .......... ..........  2% 9.65M 27s
 13500K .......... .......... .......... .......... ..........  2% 10.1M 27s
 13550K .......... .......... .......... .......... ..........  2% 9.23M 27s
 13600K .......... .......... .......... .......... ..........  2% 10.4M 27s
 13650K .......... .......... .......... .......... ..........  2% 14.0M 27s
 13700K .......... .......... .......... .......... ..........  2% 12.9M 27s
 13750K .......... .......... .......... .......... ..........  2% 15.7M 27s
 13800K .......... .......... .......... .......... ..........  2% 14.5M 27s
 13850K .......... .......... .......... .......... ..........  2% 8.20M 27s
 13900K .......... .......... .......... .......... ..........  2% 13.9M 27s
 13950K .......... .......... .......... .......... ..........  2% 9.95M 27s
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 14050K .......... .......... .......... .......... ..........  2% 10.7M 27s
 14100K .......... .......... .......... .......... ..........  2% 18.0M 27s
 14150K .......... .......... .......... .......... ..........  2% 20.8M 27s
 14200K .......... .......... .......... .......... ..........  2% 12.6M 27s
 14250K .......... .......... .......... .......... ..........  2% 14.8M 28s
 14300K .......... .......... .......... .......... ..........  2% 28.8M 27s
 14350K .......... .......... .......... .......... ..........  2% 13.4M 27s
 14400K .......... .......... .......... .......... ..........  2% 19.9M 27s
 14450K .......... .......... .......... .......... ..........  2% 15.5M 27s
 14500K .......... .......... .......... .......... ..........  2% 18.8M 27s
 14550K .......... .......... .......... .......... ..........  2% 19.0M 27s
 14600K .......... .......... .......... .......... ..........  2% 15.5M 27s
 14650K .......... .......... .......... .......... ..........  2% 16.4M 27s
 14700K .......... .......... .......... .......... ..........  2% 15.6M 27s
 14750K .......... .......... .......... .......... ..........  2% 19.5M 27s
 14800K .......... .......... .......... .......... ..........  2% 19.7M 27s
 14850K .......... .......... .......... .......... ..........  2% 15.0M 27s
 14900K .......... .......... .......... .......... ..........  2% 17.0M 27s
 14950K .......... .......... .......... .......... ..........  2% 15.5M 27s
 15000K .......... .......... .......... .......... ..........  2% 18.9M 27s
 15050K .......... .......... .......... .......... ..........  2% 22.1M 27s
 15100K .......... .......... .......... .......... ..........  3% 14.4M 27s
 15150K .......... .......... .......... .......... ..........  3% 17.9M 27s
 15200K .......... .......... .......... .......... ..........  3% 11.7M 27s
 15250K .......... .......... .......... .......... ..........  3% 14.5M 28s
 15300K .......... .......... .......... .......... ..........  3% 15.0M 28s
 15350K .......... .......... .......... .......... ..........  3% 22.1M 28s
 15400K .......... .......... .......... .......... ..........  3% 15.6M 28s
 15450K .......... .......... .......... .......... ..........  3% 16.4M 28s
 15500K .......... .......... .......... .......... ..........  3% 17.1M 28s
 15550K .......... .......... .......... .......... ..........  3% 18.7M 27s
 15600K .......... .......... .......... .......... ..........  3% 13.0M 28s
 15650K .......... .......... .......... .......... ..........  3% 23.4M 28s
 15700K .......... .......... .......... .......... ..........  3% 13.5M 28s
 15750K .......... .......... .......... .......... ..........  3% 18.1M 28s
 15800K .......... .......... .......... .......... ..........  3% 15.0M 28s
 15850K .......... .......... .......... .......... ..........  3% 18.1M 28s
 15900K .......... .......... .......... .......... ..........  3% 18.6M 28s
 15950K .......... .......... .......... .......... ..........  3% 15.0M 28s
 16000K .......... .......... .......... .......... ..........  3% 22.1M 28s
 16050K .......... .......... .......... .......... ..........  3% 19.8M 27s
 16100K .......... .......... .......... .......... ..........  3% 17.9M 27s
 16150K .......... .......... .......... .......... ..........  3% 23.5M 27s
 16200K .......... .......... .......... .......... ..........  3% 18.7M 27s
 16250K .......... .......... .......... .......... ..........  3% 18.0M 27s
 16300K .......... .......... .......... .......... ..........  3% 18.9M 27s
 16350K .......... .......... .......... .......... ..........  3% 11.1M 27s
 16400K .......... .......... .......... .......... ..........  3% 93.2M 27s
 16450K .......... .......... .......... .......... ..........  3% 11.2M 27s
 16500K .......... .......... .......... .......... ..........  3% 12.5M 27s
 16550K .......... .......... .......... .......... ..........  3% 19.8M 27s
 16600K .......... .......... .......... .......... ..........  3% 20.2M 27s
 16650K .......... .......... .......... .......... ..........  3% 18.7M 27s
 16700K .......... .......... .......... .......... ..........  3% 13.7M 27s
 16750K .......... .......... .......... .......... ..........  3% 9.98M 28s
 16800K .......... .......... .......... .......... ..........  3% 29.7M 27s
 16850K .......... .......... .......... .......... ..........  3% 21.7M 27s
 16900K .......... .......... .......... .......... ..........  3% 18.8M 27s
 16950K .......... .......... .......... .......... ..........  3% 15.0M 27s
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 17050K .......... .......... .......... .......... ..........  3% 23.5M 27s
 17100K .......... .......... .......... .......... ..........  3% 17.1M 27s
 17150K .......... .......... .......... .......... ..........  3% 17.8M 27s
 17200K .......... .......... .......... .......... ..........  3% 17.8M 27s
 17250K .......... .......... .......... .......... ..........  3% 21.9M 27s
 17300K .......... .......... .......... .......... ..........  3% 19.7M 27s
 17350K .......... .......... .......... .......... ..........  3% 17.9M 27s
 17400K .......... .......... .......... .......... ..........  3% 17.8M 27s
 17450K .......... .......... .......... .......... ..........  3% 17.0M 27s
 17500K .......... .......... .......... .......... ..........  3% 21.9M 27s
 17550K .......... .......... .......... .......... ..........  3% 18.0M 27s
 17600K .......... .......... .......... .......... ..........  3% 30.8M 27s
 17650K .......... .......... .......... .......... ..........  3% 49.1M 27s
 17700K .......... .......... .......... .......... ..........  3% 44.8M 27s
 17750K .......... .......... .......... .......... ..........  3% 56.8M 27s
 17800K .......... .......... .......... .......... ..........  3% 21.5M 27s
 17850K .......... .......... .......... .......... ..........  3% 57.4M 27s
 17900K .......... .......... .......... .......... ..........  3% 23.5M 27s
 17950K .......... .......... .......... .......... ..........  3% 20.5M 27s
 18000K .......... .......... .......... .......... ..........  3%  125M 27s
 18050K .......... .......... .......... .......... ..........  3% 18.4M 27s
 18100K .......... .......... .......... .......... ..........  3% 35.5M 27s
 18150K .......... .......... .......... .......... ..........  3% 19.6M 27s
 18200K .......... .......... .......... .......... ..........  3% 19.5M 27s
 18250K .......... .......... .......... .......... ..........  3% 25.4M 27s
 18300K .......... .......... .......... .......... ..........  3% 26.5M 27s
 18350K .......... .......... .......... .......... ..........  3% 22.1M 27s
 18400K .......... .......... .......... .......... ..........  3% 24.8M 27s
 18450K .......... .......... .......... .......... ..........  3% 19.8M 27s
 18500K .......... .......... .......... .......... ..........  3% 29.0M 27s
 18550K .......... .......... .......... .......... ..........  3% 13.9M 27s
 18600K .......... .......... .......... .......... ..........  3% 22.0M 27s
 18650K .......... .......... .......... .......... ..........  3% 20.9M 27s
 18700K .......... .......... .......... .......... ..........  3% 18.7M 27s
 18750K .......... .......... .......... .......... ..........  3% 20.2M 27s
 18800K .......... .......... .......... .......... ..........  3% 19.0M 27s
 18850K .......... .......... .......... .......... ..........  3% 16.9M 27s
 18900K .......... .......... .......... .......... ..........  3% 19.5M 27s
 18950K .......... .......... .......... .......... ..........  3% 16.2M 27s
 19000K .......... .......... .......... .......... ..........  3% 20.7M 27s
 19050K .......... .......... .......... .......... ..........  3% 18.6M 27s
 19100K .......... .......... .......... .......... ..........  3% 13.4M 27s
 19150K .......... .......... .......... .......... ..........  3% 15.1M 27s
 19200K .......... .......... .......... .......... ..........  3% 11.7M 27s
 19250K .......... .......... .......... .......... ..........  3% 15.0M 27s
 19300K .......... .......... .......... .......... ..........  3% 13.8M 27s
 19350K .......... .......... .......... .......... ..........  3% 13.9M 27s
 19400K .......... .......... .......... .......... ..........  3% 14.5M 27s
 19450K .......... .......... .......... .......... ..........  3% 13.4M 27s
 19500K .......... .......... .......... .......... ..........  3% 14.1M 27s
 19550K .......... .......... .......... .......... ..........  3% 19.3M 27s
 19600K .......... .......... .......... .......... ..........  3% 19.3M 27s
 19650K .......... .......... .......... .......... ..........  3%  112M 27s
 19700K .......... .......... .......... .......... ..........  3% 42.4M 27s
 19750K .......... .......... .......... .......... ..........  3% 31.2M 27s
 19800K .......... .......... .......... .......... ..........  3% 41.5M 27s
 19850K .......... .......... .......... .......... ..........  3% 36.6M 27s
 19900K .......... .......... .......... .......... ..........  3% 42.2M 27s
 19950K .......... .......... .......... .......... ..........  3% 31.2M 27s
 20000K .......... .......... .......... .......... ..........  3% 43.9M 27s
 20050K .......... .......... .......... .......... ..........  3% 35.9M 27s
 20100K .......... .......... .......... .......... ..........  3% 41.4M 26s
 20150K .......... .......... .......... .......... ..........  4% 46.7M 26s
 20200K .......... .......... .......... .......... ..........  4% 34.2M 26s
 20250K .......... .......... .......... .......... ..........  4% 46.5M 26s
 20300K .......... .......... .......... .......... ..........  4% 46.2M 26s
 20350K .......... .......... .......... .......... ..........  4% 37.6M 26s
 20400K .......... .......... .......... .......... ..........  4% 37.0M 26s
 20450K .......... .......... .......... .......... ..........  4% 47.0M 26s
 20500K .......... .......... .......... .......... ..........  4% 38.2M 26s
 20550K .......... .......... .......... .......... ..........  4% 47.3M 26s
 20600K .......... .......... .......... .......... ..........  4% 31.6M 26s
 20650K .......... .......... .......... .......... ..........  4% 47.4M 26s
 20700K .......... .......... .......... .......... ..........  4% 37.8M 26s
 20750K .......... .......... .......... .......... ..........  4% 38.0M 26s
 20800K .......... .......... .......... .......... ..........  4% 46.4M 26s
 20850K .......... .......... .......... .......... ..........  4% 34.6M 26s
 20900K .......... .......... .......... .......... ..........  4% 47.3M 26s
 20950K .......... .......... .......... .......... ..........  4% 34.4M 26s
 21000K .......... .......... .......... .......... ..........  4% 47.4M 26s
 21050K .......... .......... .......... .......... ..........  4% 34.2M 26s
 21100K .......... .......... .......... .......... ..........  4% 46.7M 26s
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 21200K .......... .......... .......... .......... ..........  4%  362M 26s
 21250K .......... .......... .......... .......... ..........  4%  103M 26s
 21300K .......... .......... .......... .......... ..........  4% 49.1M 26s
 21350K .......... .......... .......... .......... ..........  4% 33.3M 26s
 21400K .......... .......... .......... .......... ..........  4% 42.4M 25s
 21450K .......... .......... .......... .......... ..........  4% 36.9M 25s
 21500K .......... .......... .......... .......... ..........  4% 43.9M 25s
 21550K .......... .......... .......... .......... ..........  4% 56.4M 25s
 21600K .......... .......... .......... .......... ..........  4% 39.3M 25s
 21650K .......... .......... .......... .......... ..........  4% 50.0M 25s
 21700K .......... .......... .......... .......... ..........  4% 38.2M 25s
 21750K .......... .......... .......... .......... ..........  4% 47.3M 25s
 21800K .......... .......... .......... .......... ..........  4% 37.5M 25s
 21850K .......... .......... .......... .......... ..........  4% 42.2M 25s
 21900K .......... .......... .......... .......... ..........  4% 52.8M 25s
 21950K .......... .......... .......... .......... ..........  4% 34.4M 25s
 22000K .......... .......... .......... .......... ..........  4% 54.3M 25s
 22050K .......... .......... .......... .......... ..........  4% 47.3M 25s
 22100K .......... .......... .......... .......... ..........  4% 47.3M 25s
 22150K .......... .......... .......... .......... ..........  4% 34.3M 25s
 22200K .......... .......... .......... .......... ..........  4% 42.3M 25s
 22250K .......... .......... .......... .......... ..........  4% 41.2M 25s
 22300K .......... .......... .......... .......... ..........  4% 21.4M 25s
 22350K .......... .......... .......... .......... ..........  4% 20.9M 25s
 22400K .......... .......... .......... .......... ..........  4% 19.2M 25s
 22450K .......... .......... .......... .......... ..........  4% 23.3M 25s
 22500K .......... .......... .......... .......... ..........  4% 20.9M 25s
 22550K .......... .......... .......... .......... ..........  4% 18.5M 25s
 22600K .......... .......... .......... .......... ..........  4% 12.0M 25s
 22650K .......... .......... .......... .......... ..........  4% 14.4M 25s
 22700K .......... .......... .......... .......... ..........  4% 11.2M 25s
 22750K .......... .......... .......... .......... ..........  4% 14.1M 25s
 22800K .......... .......... .......... .......... ..........  4% 12.9M 25s
 22850K .......... .......... .......... .......... ..........  4% 12.9M 25s
 22900K .......... .......... .......... .......... ..........  4% 12.1M 25s
 22950K .......... .......... .......... .......... ..........  4% 11.1M 25s
 23000K .......... .......... .......... .......... ..........  4% 12.1M 25s
 23050K .......... .......... .......... .......... ..........  4% 10.4M 25s
 23100K .......... .......... .......... .......... ..........  4% 11.8M 25s
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 50650K .......... .......... .......... .......... .......... 10% 24.7M 32s
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 50750K .......... .......... .......... .......... .......... 10% 26.7M 32s
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 51050K .......... .......... .......... .......... .......... 10% 22.2M 32s
 51100K .......... .......... .......... .......... .......... 10% 11.1M 32s
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 93800K .......... .......... .......... .......... .......... 18% 8.35M 35s
 93850K .......... .......... .......... .......... .......... 18% 7.23M 35s
 93900K .......... .......... .......... .......... .......... 18% 10.4M 35s
 93950K .......... .......... .......... .......... .......... 18% 8.24M 35s
 94000K .......... .......... .......... .......... .......... 18% 9.61M 35s
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 95150K .......... .......... .......... .......... .......... 18% 11.0M 35s
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 95250K .......... .......... .......... .......... .......... 18% 12.1M 35s
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100000K .......... .......... .......... .......... .......... 19% 12.1M 35s
100050K .......... .......... .......... .......... .......... 19% 9.45M 35s
100100K .......... .......... .......... .......... .......... 19% 9.38M 35s
100150K .......... .......... .......... .......... .......... 19% 12.1M 35s
100200K .......... .......... .......... .......... .......... 19% 7.98M 35s
100250K .......... .......... .......... .......... .......... 19% 8.41M 35s
100300K .......... .......... .......... .......... .......... 19% 7.13M 35s
100350K .......... .......... .......... .......... .......... 19% 4.60M 35s
100400K .......... .......... .......... .......... .......... 19% 6.43M 35s
100450K .......... .......... .......... .......... .......... 19% 6.67M 35s
100500K .......... .......... .......... .......... .......... 19% 13.4M 35s
100550K .......... .......... .......... .......... .......... 19% 17.3M 35s
100600K .......... .......... .......... .......... .......... 19% 13.4M 35s
100650K .......... .......... .......... .......... .......... 19% 7.83M 35s
100700K .......... .......... .......... .......... .......... 19% 7.22M 35s
100750K .......... .......... .......... .......... .......... 19% 8.43M 35s
100800K .......... .......... .......... .......... .......... 19% 7.71M 35s
100850K .......... .......... .......... .......... .......... 19% 5.91M 35s
100900K .......... .......... .......... .......... .......... 20% 9.39M 35s
100950K .......... .......... .......... .......... .......... 20% 8.56M 35s
101000K .......... .......... .......... .......... .......... 20% 8.42M 35s
101050K .......... .......... .......... .......... .......... 20% 8.80M 35s
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101150K .......... .......... .......... .......... .......... 20% 6.58M 35s
101200K .......... .......... .......... .......... .......... 20% 5.88M 35s
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101300K .......... .......... .......... .......... .......... 20% 5.91M 35s
101350K .......... .......... .......... .......... .......... 20% 4.40M 35s
101400K .......... .......... .......... .......... .......... 20% 4.14M 35s
101450K .......... .......... .......... .......... .......... 20% 17.0M 35s
101500K .......... .......... .......... .......... .......... 20% 19.9M 35s
101550K .......... .......... .......... .......... .......... 20% 30.8M 35s
101600K .......... .......... .......... .......... .......... 20% 9.89M 35s
101650K .......... .......... .......... .......... .......... 20% 41.4M 35s
101700K .......... .......... .......... .......... .......... 20% 17.8M 35s
101750K .......... .......... .......... .......... .......... 20% 13.5M 35s
101800K .......... .......... .......... .......... .......... 20% 12.7M 35s
101850K .......... .......... .......... .......... .......... 20% 14.7M 35s
101900K .......... .......... .......... .......... .......... 20% 11.0M 35s
101950K .......... .......... .......... .......... .......... 20% 13.2M 35s
102000K .......... .......... .......... .......... .......... 20% 12.7M 35s
102050K .......... .......... .......... .......... .......... 20% 17.8M 35s
102100K .......... .......... .......... .......... .......... 20% 11.1M 35s
102150K .......... .......... .......... .......... .......... 20% 13.4M 35s
102200K .......... .......... .......... .......... .......... 20% 12.9M 35s
102250K .......... .......... .......... .......... .......... 20% 11.4M 35s
102300K .......... .......... .......... .......... .......... 20% 11.1M 35s
102350K .......... .......... .......... .......... .......... 20% 7.52M 35s
102400K .......... .......... .......... .......... .......... 20% 8.98M 35s
102450K .......... .......... .......... .......... .......... 20% 6.65M 35s
102500K .......... .......... .......... .......... .......... 20% 8.42M 35s
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102700K .......... .......... .......... .......... .......... 20% 23.2M 35s
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102800K .......... .......... .......... .......... .......... 20% 28.4M 35s
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103000K .......... .......... .......... .......... .......... 20% 17.0M 35s
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103100K .......... .......... .......... .......... .......... 20% 10.7M 35s
103150K .......... .......... .......... .......... .......... 20% 10.5M 35s
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103250K .......... .......... .......... .......... .......... 20% 9.92M 35s
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103650K .......... .......... .......... .......... .......... 20% 83.6M 35s
103700K .......... .......... .......... .......... .......... 20% 25.4M 35s
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103800K .......... .......... .......... .......... .......... 20% 16.2M 35s
103850K .......... .......... .......... .......... .......... 20% 22.3M 35s
103900K .......... .......... .......... .......... .......... 20% 16.9M 35s
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104000K .......... .......... .......... .......... .......... 20% 12.1M 35s
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104100K .......... .......... .......... .......... .......... 20% 8.14M 35s
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104900K .......... .......... .......... .......... .......... 20% 15.7M 35s
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105000K .......... .......... .......... .......... .......... 20% 16.3M 35s
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105100K .......... .......... .......... .......... .......... 20% 11.1M 34s
105150K .......... .......... .......... .......... .......... 20% 8.99M 34s
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105250K .......... .......... .......... .......... .......... 20% 7.88M 35s
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105400K .......... .......... .......... .......... .......... 20% 7.73M 35s
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105500K .......... .......... .......... .......... .......... 20% 8.77M 35s
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105600K .......... .......... .......... .......... .......... 20% 6.90M 35s
105650K .......... .......... .......... .......... .......... 20% 10.4M 35s
105700K .......... .......... .......... .......... .......... 20% 18.2M 35s
105750K .......... .......... .......... .......... .......... 20% 12.1M 35s
105800K .......... .......... .......... .......... .......... 20% 8.81M 35s
105850K .......... .......... .......... .......... .......... 20% 9.81M 35s
105900K .......... .......... .......... .......... .......... 20% 11.8M 35s
105950K .......... .......... .......... .......... .......... 21% 12.2M 35s
106000K .......... .......... .......... .......... .......... 21% 14.1M 34s
106050K .......... .......... .......... .......... .......... 21% 11.4M 34s
106100K .......... .......... .......... .......... .......... 21% 10.3M 34s
106150K .......... .......... .......... .......... .......... 21% 12.2M 34s
106200K .......... .......... .......... .......... .......... 21% 8.05M 34s
106250K .......... .......... .......... .......... .......... 21% 9.22M 34s
106300K .......... .......... .......... .......... .......... 21% 8.80M 34s
106350K .......... .......... .......... .......... .......... 21% 11.4M 34s
106400K .......... .......... .......... .......... .......... 21% 14.4M 34s
106450K .......... .......... .......... .......... .......... 21% 5.96M 34s
106500K .......... .......... .......... .......... .......... 21% 13.7M 34s
106550K .......... .......... .......... .......... .......... 21% 16.3M 34s
106600K .......... .......... .......... .......... .......... 21% 12.5M 34s
106650K .......... .......... .......... .......... .......... 21% 16.3M 34s
106700K .......... .......... .......... .......... .......... 21% 12.6M 34s
106750K .......... .......... .......... .......... .......... 21% 9.40M 34s
106800K .......... .......... .......... .......... .......... 21% 20.7M 34s
106850K .......... .......... .......... .......... .......... 21% 12.2M 34s
106900K .......... .......... .......... .......... .......... 21% 13.9M 34s
106950K .......... .......... .......... .......... .......... 21% 10.6M 34s
107000K .......... .......... .......... .......... .......... 21% 12.1M 34s
107050K .......... .......... .......... .......... .......... 21% 11.4M 34s
107100K .......... .......... .......... .......... .......... 21% 11.7M 34s
107150K .......... .......... .......... .......... .......... 21% 13.0M 34s
107200K .......... .......... .......... .......... .......... 21% 10.7M 34s
107250K .......... .......... .......... .......... .......... 21% 13.0M 34s
107300K .......... .......... .......... .......... .......... 21% 19.0M 34s
107350K .......... .......... .......... .......... .......... 21% 8.78M 34s
107400K .......... .......... .......... .......... .......... 21% 9.23M 34s
107450K .......... .......... .......... .......... .......... 21% 8.60M 34s
107500K .......... .......... .......... .......... .......... 21% 12.1M 34s
107550K .......... .......... .......... .......... .......... 21% 11.8M 34s
107600K .......... .......... .......... .......... .......... 21% 7.57M 34s
107650K .......... .......... .......... .......... .......... 21% 11.8M 34s
107700K .......... .......... .......... .......... .......... 21% 9.66M 34s
107750K .......... .......... .......... .......... .......... 21% 12.9M 34s
107800K .......... .......... .......... .......... .......... 21% 15.2M 34s
107850K .......... .......... .......... .......... .......... 21% 9.68M 34s
107900K .......... .......... .......... .......... .......... 21% 9.37M 34s
107950K .......... .......... .......... .......... .......... 21% 9.27M 34s
108000K .......... .......... .......... .......... .......... 21% 12.3M 34s
108050K .......... .......... .......... .......... .......... 21% 9.26M 34s
108100K .......... .......... .......... .......... .......... 21% 7.30M 34s
108150K .......... .......... .......... .......... .......... 21% 6.25M 34s
108200K .......... .......... .......... .......... .......... 21% 6.23M 34s
108250K .......... .......... .......... .......... .......... 21% 12.0M 34s
108300K .......... .......... .......... .......... .......... 21% 8.93M 34s
108350K .......... .......... .......... .......... .......... 21% 10.6M 34s
108400K .......... .......... .......... .......... .......... 21% 8.60M 34s
108450K .......... .......... .......... .......... .......... 21% 6.67M 34s
108500K .......... .......... .......... .......... .......... 21% 8.03M 34s
108550K .......... .......... .......... .......... .......... 21% 8.10M 34s
108600K .......... .......... .......... .......... .......... 21% 5.68M 34s
108650K .......... .......... .......... .......... .......... 21% 3.89M 34s
108700K .......... .......... .......... .......... .......... 21% 6.68M 34s
108750K .......... .......... .......... .......... .......... 21% 9.73M 34s
108800K .......... .......... .......... .......... .......... 21% 10.2M 34s
108850K .......... .......... .......... .......... .......... 21% 7.91M 34s
108900K .......... .......... .......... .......... .......... 21% 14.5M 34s
108950K .......... .......... .......... .......... .......... 21% 10.2M 34s
109000K .......... .......... .......... .......... .......... 21% 13.5M 34s
109050K .......... .......... .......... .......... .......... 21% 15.9M 34s
109100K .......... .......... .......... .......... .......... 21% 10.4M 34s
109150K .......... .......... .......... .......... .......... 21% 16.4M 34s
109200K .......... .......... .......... .......... .......... 21% 10.1M 34s
109250K .......... .......... .......... .......... .......... 21% 14.5M 34s
109300K .......... .......... .......... .......... .......... 21% 10.5M 34s
109350K .......... .......... .......... .......... .......... 21% 19.5M 34s
109400K .......... .......... .......... .......... .......... 21% 14.6M 34s
109450K .......... .......... .......... .......... .......... 21% 7.81M 34s
109500K .......... .......... .......... .......... .......... 21% 8.58M 34s
109550K .......... .......... .......... .......... .......... 21% 9.78M 34s
109600K .......... .......... .......... .......... .......... 21% 7.15M 34s
109650K .......... .......... .......... .......... .......... 21% 9.19M 34s
109700K .......... .......... .......... .......... .......... 21% 5.97M 34s
109750K .......... .......... .......... .......... .......... 21% 10.6M 34s
109800K .......... .......... .......... .......... .......... 21% 11.7M 34s
109850K .......... .......... .......... .......... .......... 21% 7.45M 34s
109900K .......... .......... .......... .......... .......... 21% 8.59M 34s
109950K .......... .......... .......... .......... .......... 21% 12.1M 34s
110000K .......... .......... .......... .......... .......... 21% 9.20M 34s
110050K .......... .......... .......... .......... .......... 21% 8.03M 34s
110100K .......... .......... .......... .......... .......... 21% 10.4M 34s
110150K .......... .......... .......... .......... .......... 21% 15.0M 34s
110200K .......... .......... .......... .......... .......... 21% 10.5M 34s
110250K .......... .......... .......... .......... .......... 21% 11.4M 34s
110300K .......... .......... .......... .......... .......... 21% 11.5M 34s
110350K .......... .......... .......... .......... .......... 21% 9.70M 34s
110400K .......... .......... .......... .......... .......... 21% 11.4M 34s
110450K .......... .......... .......... .......... .......... 21% 8.70M 34s
110500K .......... .......... .......... .......... .......... 21% 10.2M 34s
110550K .......... .......... .......... .......... .......... 21% 8.45M 34s
110600K .......... .......... .......... .......... .......... 21% 5.07M 34s
110650K .......... .......... .......... .......... .......... 21% 3.81M 34s
110700K .......... .......... .......... .......... .......... 21% 2.79M 34s
110750K .......... .......... .......... .......... .......... 21% 4.75M 34s
110800K .......... .......... .......... .......... .......... 21% 6.97M 34s
110850K .......... .......... .......... .......... .......... 21% 5.43M 34s
110900K .......... .......... .......... .......... .......... 21% 5.59M 34s
110950K .......... .......... .......... .......... .......... 21% 5.68M 34s
111000K .......... .......... .......... .......... .......... 22% 21.3M 34s
111050K .......... .......... .......... .......... .......... 22% 21.3M 34s
111100K .......... .......... .......... .......... .......... 22% 8.99M 34s
111150K .......... .......... .......... .......... .......... 22% 11.1M 34s
111200K .......... .......... .......... .......... .......... 22% 7.27M 34s
111250K .......... .......... .......... .......... .......... 22% 11.8M 34s
111300K .......... .......... .......... .......... .......... 22% 11.4M 34s
111350K .......... .......... .......... .......... .......... 22% 10.5M 34s
111400K .......... .......... .......... .......... .......... 22% 11.8M 34s
111450K .......... .......... .......... .......... .......... 22% 9.44M 34s
111500K .......... .......... .......... .......... .......... 22% 11.1M 34s
111550K .......... .......... .......... .......... .......... 22% 7.51M 34s
111600K .......... .......... .......... .......... .......... 22% 10.5M 34s
111650K .......... .......... .......... .......... .......... 22% 13.4M 34s
111700K .......... .......... .......... .......... .......... 22% 11.8M 34s
111750K .......... .......... .......... .......... .......... 22% 10.4M 34s
111800K .......... .......... .......... .......... .......... 22% 8.55M 34s
111850K .......... .......... .......... .......... .......... 22% 8.78M 34s
111900K .......... .......... .......... .......... .......... 22% 8.59M 34s
111950K .......... .......... .......... .......... .......... 22% 6.54M 34s
112000K .......... .......... .......... .......... .......... 22% 10.2M 34s
112050K .......... .......... .......... .......... .......... 22% 8.58M 34s
112100K .......... .......... .......... .......... .......... 22% 10.5M 34s
112150K .......... .......... .......... .......... .......... 22% 23.3M 34s
112200K .......... .......... .......... .......... .......... 22% 26.7M 34s
112250K .......... .......... .......... .......... .......... 22% 35.1M 34s
112300K .......... .......... .......... .......... .......... 22% 12.8M 34s
112350K .......... .......... .......... .......... .......... 22% 68.3M 34s
112400K .......... .......... .......... .......... .......... 22% 56.1M 34s
112450K .......... .......... .......... .......... .......... 22% 21.3M 34s
112500K .......... .......... .......... .......... .......... 22% 22.5M 34s
112550K .......... .......... .......... .......... .......... 22% 16.4M 34s
112600K .......... .......... .......... .......... .......... 22% 14.3M 34s
112650K .......... .......... .......... .......... .......... 22% 13.0M 34s
112700K .......... .......... .......... .......... .......... 22% 15.0M 34s
112750K .......... .......... .......... .......... .......... 22% 15.7M 34s
112800K .......... .......... .......... .......... .......... 22% 19.8M 34s
112850K .......... .......... .......... .......... .......... 22% 15.6M 34s
112900K .......... .......... .......... .......... .......... 22% 17.1M 34s
112950K .......... .......... .......... .......... .......... 22% 12.6M 34s
113000K .......... .......... .......... .......... .......... 22% 11.7M 34s
113050K .......... .......... .......... .......... .......... 22% 11.5M 34s
113100K .......... .......... .......... .......... .......... 22% 9.75M 34s
113150K .......... .......... .......... .......... .......... 22% 9.53M 34s
113200K .......... .......... .......... .......... .......... 22% 7.91M 34s
113250K .......... .......... .......... .......... .......... 22% 8.55M 34s
113300K .......... .......... .......... .......... .......... 22% 8.21M 34s
113350K .......... .......... .......... .......... .......... 22% 5.56M 34s
113400K .......... .......... .......... .......... .......... 22% 6.53M 34s
113450K .......... .......... .......... .......... .......... 22% 5.69M 34s
113500K .......... .......... .......... .......... .......... 22% 6.12M 34s
113550K .......... .......... .......... .......... .......... 22% 6.41M 34s
113600K .......... .......... .......... .......... .......... 22% 18.6M 34s
113650K .......... .......... .......... .......... .......... 22% 22.6M 34s
113700K .......... .......... .......... .......... .......... 22% 24.9M 34s
113750K .......... .......... .......... .......... .......... 22% 45.8M 34s
113800K .......... .......... .......... .......... .......... 22% 19.7M 34s
113850K .......... .......... .......... .......... .......... 22% 30.7M 34s
113900K .......... .......... .......... .......... .......... 22% 22.2M 34s
113950K .......... .......... .......... .......... .......... 22% 20.4M 34s
114000K .......... .......... .......... .......... .......... 22% 32.1M 34s
114050K .......... .......... .......... .......... .......... 22% 26.5M 34s
114100K .......... .......... .......... .......... .......... 22% 23.5M 34s
114150K .......... .......... .......... .......... .......... 22% 22.3M 34s
114200K .......... .......... .......... .......... .......... 22% 24.7M 34s
114250K .......... .......... .......... .......... .......... 22% 24.9M 34s
114300K .......... .......... .......... .......... .......... 22% 26.7M 34s
114350K .......... .......... .......... .......... .......... 22% 19.8M 34s
114400K .......... .......... .......... .......... .......... 22% 31.7M 34s
114450K .......... .......... .......... .......... .......... 22% 23.3M 34s
114500K .......... .......... .......... .......... .......... 22% 26.6M 34s
114550K .......... .......... .......... .......... .......... 22% 28.7M 34s
114600K .......... .......... .......... .......... .......... 22% 19.9M 34s
114650K .......... .......... .......... .......... .......... 22% 11.5M 34s
114700K .......... .......... .......... .......... .......... 22% 10.4M 34s
114750K .......... .......... .......... .......... .......... 22% 9.72M 34s
114800K .......... .......... .......... .......... .......... 22% 4.99M 34s
114850K .......... .......... .......... .......... .......... 22% 4.37M 34s
114900K .......... .......... .......... .......... .......... 22% 3.78M 34s
114950K .......... .......... .......... .......... .......... 22% 2.05M 34s
115000K .......... .......... .......... .......... .......... 22% 10.3M 34s
115050K .......... .......... .......... .......... .......... 22% 23.6M 34s
115100K .......... .......... .......... .......... .......... 22% 21.4M 34s
115150K .......... .......... .......... .......... .......... 22% 41.8M 34s
115200K .......... .......... .......... .......... .......... 22% 23.4M 34s
115250K .......... .......... .......... .......... .......... 22% 15.4M 34s
115300K .......... .......... .......... .......... .......... 22% 11.5M 34s
115350K .......... .......... .......... .......... .......... 22% 11.8M 34s
115400K .......... .......... .......... .......... .......... 22% 14.9M 34s
115450K .......... .......... .......... .......... .......... 22% 9.83M 34s
115500K .......... .......... .......... .......... .......... 22% 11.4M 34s
115550K .......... .......... .......... .......... .......... 22% 9.49M 34s
115600K .......... .......... .......... .......... .......... 22% 8.36M 34s
115650K .......... .......... .......... .......... .......... 22% 8.78M 34s
115700K .......... .......... .......... .......... .......... 22% 6.75M 34s
115750K .......... .......... .......... .......... .......... 22% 8.98M 34s
115800K .......... .......... .......... .......... .......... 22% 8.20M 34s
115850K .......... .......... .......... .......... .......... 22% 14.2M 34s
115900K .......... .......... .......... .......... .......... 22% 20.2M 34s
115950K .......... .......... .......... .......... .......... 22% 14.0M 34s
116000K .......... .......... .......... .......... .......... 22% 35.3M 34s
116050K .......... .......... .......... .......... .......... 23% 22.3M 34s
116100K .......... .......... .......... .......... .......... 23% 19.9M 34s
116150K .......... .......... .......... .......... .......... 23% 23.3M 34s
116200K .......... .......... .......... .......... .......... 23% 17.1M 34s
116250K .......... .......... .......... .......... .......... 23% 23.7M 34s
116300K .......... .......... .......... .......... .......... 23% 17.7M 34s
116350K .......... .......... .......... .......... .......... 23% 19.7M 34s
116400K .......... .......... .......... .......... .......... 23% 23.5M 34s
116450K .......... .......... .......... .......... .......... 23% 18.1M 34s
116500K .......... .......... .......... .......... .......... 23% 14.8M 34s
116550K .......... .......... .......... .......... .......... 23% 9.20M 34s
116600K .......... .......... .......... .......... .......... 23% 9.17M 34s
116650K .......... .......... .......... .......... .......... 23% 10.8M 34s
116700K .......... .......... .......... .......... .......... 23% 6.94M 34s
116750K .......... .......... .......... .......... .......... 23% 13.0M 34s
116800K .......... .......... .......... .......... .......... 23% 9.89M 34s
116850K .......... .......... .......... .......... .......... 23% 8.37M 34s
116900K .......... .......... .......... .......... .......... 23% 9.18M 34s
116950K .......... .......... .......... .......... .......... 23% 7.52M 34s
117000K .......... .......... .......... .......... .......... 23% 12.1M 34s
117050K .......... .......... .......... .......... .......... 23% 12.1M 34s
117100K .......... .......... .......... .......... .......... 23% 11.4M 34s
117150K .......... .......... .......... .......... .......... 23% 12.2M 34s
117200K .......... .......... .......... .......... .......... 23% 10.8M 34s
117250K .......... .......... .......... .......... .......... 23% 10.3M 34s
117300K .......... .......... .......... .......... .......... 23% 12.2M 34s
117350K .......... .......... .......... .......... .......... 23% 11.2M 34s
117400K .......... .......... .......... .......... .......... 23% 11.7M 34s
117450K .......... .......... .......... .......... .......... 23% 8.94M 34s
117500K .......... .......... .......... .......... .......... 23% 11.8M 34s
117550K .......... .......... .......... .......... .......... 23% 9.21M 34s
117600K .......... .......... .......... .......... .......... 23% 9.62M 34s
117650K .......... .......... .......... .......... .......... 23% 14.9M 34s
117700K .......... .......... .......... .......... .......... 23% 9.21M 34s
117750K .......... .......... .......... .......... .......... 23% 11.2M 34s
117800K .......... .......... .......... .......... .......... 23% 8.32M 34s
117850K .......... .......... .......... .......... .......... 23% 10.9M 34s
117900K .......... .......... .......... .......... .......... 23% 12.1M 34s
117950K .......... .......... .......... .......... .......... 23% 10.7M 34s
118000K .......... .......... .......... .......... .......... 23% 7.99M 34s
118050K .......... .......... .......... .......... .......... 23% 12.9M 34s
118100K .......... .......... .......... .......... .......... 23% 11.1M 34s
118150K .......... .......... .......... .......... .......... 23% 12.2M 34s
118200K .......... .......... .......... .......... .......... 23% 12.1M 34s
118250K .......... .......... .......... .......... .......... 23% 15.6M 34s
118300K .......... .......... .......... .......... .......... 23% 8.99M 34s
118350K .......... .......... .......... .......... .......... 23% 10.5M 34s
118400K .......... .......... .......... .......... .......... 23% 12.1M 34s
118450K .......... .......... .......... .......... .......... 23% 9.93M 34s
118500K .......... .......... .......... .......... .......... 23% 10.6M 34s
118550K .......... .......... .......... .......... .......... 23% 10.4M 34s
118600K .......... .......... .......... .......... .......... 23% 8.56M 34s
118650K .......... .......... .......... .......... .......... 23% 9.41M 34s
118700K .......... .......... .......... .......... .......... 23% 7.69M 34s
118750K .......... .......... .......... .......... .......... 23% 8.40M 34s
118800K .......... .......... .......... .......... .......... 23% 8.83M 34s
118850K .......... .......... .......... .......... .......... 23% 14.6M 34s
118900K .......... .......... .......... .......... .......... 23% 20.6M 34s
118950K .......... .......... .......... .......... .......... 23% 27.9M 34s
119000K .......... .......... .......... .......... .......... 23% 25.6M 34s
119050K .......... .......... .......... .......... .......... 23% 19.9M 34s
119100K .......... .......... .......... .......... .......... 23% 14.3M 34s
119150K .......... .......... .......... .......... .......... 23% 17.1M 34s
119200K .......... .......... .......... .......... .......... 23% 14.4M 34s
119250K .......... .......... .......... .......... .......... 23% 18.0M 34s
119300K .......... .......... .......... .......... .......... 23% 17.8M 34s
119350K .......... .......... .......... .......... .......... 23% 13.3M 34s
119400K .......... .......... .......... .......... .......... 23% 19.7M 34s
119450K .......... .......... .......... .......... .......... 23% 9.41M 34s
119500K .......... .......... .......... .......... .......... 23% 15.5M 34s
119550K .......... .......... .......... .......... .......... 23% 10.7M 34s
119600K .......... .......... .......... .......... .......... 23% 8.01M 34s
119650K .......... .......... .......... .......... .......... 23% 7.54M 34s
119700K .......... .......... .......... .......... .......... 23% 8.77M 34s
119750K .......... .......... .......... .......... .......... 23% 7.86M 34s
119800K .......... .......... .......... .......... .......... 23% 7.69M 34s
119850K .......... .......... .......... .......... .......... 23% 5.21M 34s
119900K .......... .......... .......... .......... .......... 23% 7.12M 34s
119950K .......... .......... .......... .......... .......... 23% 5.75M 34s
120000K .......... .......... .......... .......... .......... 23% 6.54M 34s
120050K .......... .......... .......... .......... .......... 23% 7.12M 34s
120100K .......... .......... .......... .......... .......... 23% 13.4M 34s
120150K .......... .......... .......... .......... .......... 23% 15.2M 34s
120200K .......... .......... .......... .......... .......... 23% 20.4M 34s
120250K .......... .......... .......... .......... .......... 23% 26.7M 34s
120300K .......... .......... .......... .......... .......... 23% 21.9M 34s
120350K .......... .......... .......... .......... .......... 23% 17.8M 34s
120400K .......... .......... .......... .......... .......... 23% 15.8M 34s
120450K .......... .......... .......... .......... .......... 23% 6.72M 34s
120500K .......... .......... .......... .......... .......... 23% 8.75M 34s
120550K .......... .......... .......... .......... .......... 23% 9.43M 34s
120600K .......... .......... .......... .......... .......... 23% 7.85M 34s
120650K .......... .......... .......... .......... .......... 23% 7.89M 34s
120700K .......... .......... .......... .......... .......... 23% 7.50M 34s
120750K .......... .......... .......... .......... .......... 23% 6.59M 34s
120800K .......... .......... .......... .......... .......... 23% 4.99M 34s
120850K .......... .......... .......... .......... .......... 23% 5.02M 34s
120900K .......... .......... .......... .......... .......... 23% 5.59M 34s
120950K .......... .......... .......... .......... .......... 23% 4.27M 34s
121000K .......... .......... .......... .......... .......... 23% 10.2M 34s
121050K .......... .......... .......... .......... .......... 23% 23.5M 34s
121100K .......... .......... .......... .......... .......... 24% 9.16M 34s
121150K .......... .......... .......... .......... .......... 24% 11.5M 34s
121200K .......... .......... .......... .......... .......... 24% 6.96M 34s
121250K .......... .......... .......... .......... .......... 24% 9.98M 34s
121300K .......... .......... .......... .......... .......... 24% 9.56M 34s
121350K .......... .......... .......... .......... .......... 24% 7.90M 34s
121400K .......... .......... .......... .......... .......... 24% 7.99M 34s
121450K .......... .......... .......... .......... .......... 24% 6.27M 34s
121500K .......... .......... .......... .......... .......... 24% 6.57M 34s
121550K .......... .......... .......... .......... .......... 24% 9.42M 34s
121600K .......... .......... .......... .......... .......... 24% 7.70M 34s
121650K .......... .......... .......... .......... .......... 24% 6.29M 34s
121700K .......... .......... .......... .......... .......... 24% 4.90M 34s
121750K .......... .......... .......... .......... .......... 24% 4.19M 34s
121800K .......... .......... .......... .......... .......... 24% 3.26M 34s
121850K .......... .......... .......... .......... .......... 24% 8.15M 34s
121900K .......... .......... .......... .......... .......... 24% 10.5M 34s
121950K .......... .......... .......... .......... .......... 24% 9.18M 34s
122000K .......... .......... .......... .......... .......... 24% 7.40M 34s
122050K .......... .......... .......... .......... .......... 24% 8.59M 34s
122100K .......... .......... .......... .......... .......... 24% 6.66M 34s
122150K .......... .......... .......... .......... .......... 24% 6.55M 34s
122200K .......... .......... .......... .......... .......... 24% 6.99M 34s
122250K .......... .......... .......... .......... .......... 24% 7.94M 34s
122300K .......... .......... .......... .......... .......... 24% 14.0M 34s
122350K .......... .......... .......... .......... .......... 24% 11.5M 34s
122400K .......... .......... .......... .......... .......... 24% 15.7M 34s
122450K .......... .......... .......... .......... .......... 24% 9.42M 34s
122500K .......... .......... .......... .......... .......... 24% 12.9M 34s
122550K .......... .......... .......... .......... .......... 24% 15.3M 34s
122600K .......... .......... .......... .......... .......... 24% 10.2M 34s
122650K .......... .......... .......... .......... .......... 24% 16.8M 34s
122700K .......... .......... .......... .......... .......... 24% 12.9M 34s
122750K .......... .......... .......... .......... .......... 24% 15.1M 34s
122800K .......... .......... .......... .......... .......... 24% 12.2M 34s
122850K .......... .......... .......... .......... .......... 24% 10.6M 34s
122900K .......... .......... .......... .......... .......... 24% 7.99M 34s
122950K .......... .......... .......... .......... .......... 24% 8.97M 34s
123000K .......... .......... .......... .......... .......... 24% 11.4M 34s
123050K .......... .......... .......... .......... .......... 24% 7.41M 34s
123100K .......... .......... .......... .......... .......... 24% 8.03M 34s
123150K .......... .......... .......... .......... .......... 24% 9.87M 34s
123200K .......... .......... .......... .......... .......... 24% 6.87M 34s
123250K .......... .......... .......... .......... .......... 24% 7.68M 34s
123300K .......... .......... .......... .......... .......... 24% 5.77M 34s
123350K .......... .......... .......... .......... .......... 24% 5.65M 34s
123400K .......... .......... .......... .......... .......... 24% 6.59M 34s
123450K .......... .......... .......... .......... .......... 24% 5.97M 34s
123500K .......... .......... .......... .......... .......... 24% 7.33M 34s
123550K .......... .......... .......... .......... .......... 24% 19.7M 34s
123600K .......... .......... .......... .......... .......... 24% 23.7M 34s
123650K .......... .......... .......... .......... .......... 24% 37.3M 34s
123700K .......... .......... .......... .......... .......... 24% 13.7M 34s
123750K .......... .......... .......... .......... .......... 24% 38.0M 34s
123800K .......... .......... .......... .......... .......... 24% 19.8M 34s
123850K .......... .......... .......... .......... .......... 24% 12.9M 34s
123900K .......... .......... .......... .......... .......... 24% 17.0M 34s
123950K .......... .......... .......... .......... .......... 24% 8.16M 34s
124000K .......... .......... .......... .......... .......... 24% 12.6M 34s
124050K .......... .......... .......... .......... .......... 24% 9.41M 34s
124100K .......... .......... .......... .......... .......... 24% 8.99M 34s
124150K .......... .......... .......... .......... .......... 24% 12.1M 34s
124200K .......... .......... .......... .......... .......... 24% 10.2M 34s
124250K .......... .......... .......... .......... .......... 24% 12.6M 34s
124300K .......... .......... .......... .......... .......... 24% 7.26M 34s
124350K .......... .......... .......... .......... .......... 24% 5.24M 34s
124400K .......... .......... .......... .......... .......... 24% 12.4M 34s
124450K .......... .......... .......... .......... .......... 24% 7.03M 34s
124500K .......... .......... .......... .......... .......... 24% 11.1M 34s
124550K .......... .......... .......... .......... .......... 24% 10.3M 34s
124600K .......... .......... .......... .......... .......... 24% 8.28M 34s
124650K .......... .......... .......... .......... .......... 24% 7.71M 34s
124700K .......... .......... .......... .......... .......... 24% 7.50M 34s
124750K .......... .......... .......... .......... .......... 24% 8.63M 34s
124800K .......... .......... .......... .......... .......... 24% 7.63M 34s
124850K .......... .......... .......... .......... .......... 24% 7.18M 34s
124900K .......... .......... .......... .......... .......... 24% 6.86M 34s
124950K .......... .......... .......... .......... .......... 24% 6.12M 34s
125000K .......... .......... .......... .......... .......... 24% 6.96M 34s
125050K .......... .......... .......... .......... .......... 24% 6.51M 34s
125100K .......... .......... .......... .......... .......... 24% 6.50M 34s
125150K .......... .......... .......... .......... .......... 24% 16.8M 34s
125200K .......... .......... .......... .......... .......... 24% 24.6M 34s
125250K .......... .......... .......... .......... .......... 24% 26.3M 34s
125300K .......... .......... .......... .......... .......... 24% 35.0M 34s
125350K .......... .......... .......... .......... .......... 24% 14.1M 34s
125400K .......... .......... .......... .......... .......... 24% 21.8M 34s
125450K .......... .......... .......... .......... .......... 24% 7.19M 34s
125500K .......... .......... .......... .......... .......... 24% 8.69M 34s
125550K .......... .......... .......... .......... .......... 24% 7.18M 34s
125600K .......... .......... .......... .......... .......... 24% 6.92M 34s
125650K .......... .......... .......... .......... .......... 24% 10.8M 34s
125700K .......... .......... .......... .......... .......... 24% 6.81M 34s
125750K .......... .......... .......... .......... .......... 24% 16.1M 34s
125800K .......... .......... .......... .......... .......... 24% 8.39M 34s
125850K .......... .......... .......... .......... .......... 24% 6.44M 34s
125900K .......... .......... .......... .......... .......... 24% 8.85M 34s
125950K .......... .......... .......... .......... .......... 24% 8.30M 34s
126000K .......... .......... .......... .......... .......... 24% 6.26M 34s
126050K .......... .......... .......... .......... .......... 24% 13.0M 34s
126100K .......... .......... .......... .......... .......... 24% 10.2M 34s
126150K .......... .......... .......... .......... .......... 25% 9.58M 34s
126200K .......... .......... .......... .......... .......... 25% 11.3M 34s
126250K .......... .......... .......... .......... .......... 25% 10.6M 34s
126300K .......... .......... .......... .......... .......... 25% 12.2M 33s
126350K .......... .......... .......... .......... .......... 25% 9.25M 33s
126400K .......... .......... .......... .......... .......... 25% 19.8M 33s
126450K .......... .......... .......... .......... .......... 25% 23.4M 33s
126500K .......... .......... .......... .......... .......... 25% 25.3M 33s
126550K .......... .......... .......... .......... .......... 25% 23.0M 33s
126600K .......... .......... .......... .......... .......... 25% 11.7M 33s
126650K .......... .......... .......... .......... .......... 25% 11.6M 33s
126700K .......... .......... .......... .......... .......... 25% 7.63M 33s
126750K .......... .......... .......... .......... .......... 25% 9.06M 33s
126800K .......... .......... .......... .......... .......... 25% 9.03M 33s
126850K .......... .......... .......... .......... .......... 25% 6.91M 33s
126900K .......... .......... .......... .......... .......... 25% 7.62M 33s
126950K .......... .......... .......... .......... .......... 25% 6.02M 33s
127000K .......... .......... .......... .......... .......... 25% 12.2M 33s
127050K .......... .......... .......... .......... .......... 25% 31.5M 33s
127100K .......... .......... .......... .......... .......... 25% 16.4M 33s
127150K .......... .......... .......... .......... .......... 25% 34.0M 33s
127200K .......... .......... .......... .......... .......... 25% 13.0M 33s
127250K .......... .......... .......... .......... .......... 25% 18.1M 33s
127300K .......... .......... .......... .......... .......... 25% 18.6M 33s
127350K .......... .......... .......... .......... .......... 25% 17.1M 33s
127400K .......... .......... .......... .......... .......... 25% 20.8M 33s
127450K .......... .......... .......... .......... .......... 25% 17.2M 33s
127500K .......... .......... .......... .......... .......... 25% 18.7M 33s
127550K .......... .......... .......... .......... .......... 25% 16.4M 33s
127600K .......... .......... .......... .......... .......... 25% 18.7M 33s
127650K .......... .......... .......... .......... .......... 25% 19.9M 33s
127700K .......... .......... .......... .......... .......... 25% 19.0M 33s
127750K .......... .......... .......... .......... .......... 25% 9.68M 33s
127800K .......... .......... .......... .......... .......... 25% 11.8M 33s
127850K .......... .......... .......... .......... .......... 25% 13.5M 33s
127900K .......... .......... .......... .......... .......... 25% 9.46M 33s
127950K .......... .......... .......... .......... .......... 25% 13.5M 33s
128000K .......... .......... .......... .......... .......... 25% 15.0M 33s
128050K .......... .......... .......... .......... .......... 25% 16.4M 33s
128100K .......... .......... .......... .......... .......... 25% 14.6M 33s
128150K .......... .......... .......... .......... .......... 25% 15.2M 33s
128200K .......... .......... .......... .......... .......... 25% 11.7M 33s
128250K .......... .......... .......... .......... .......... 25% 13.5M 33s
128300K .......... .......... .......... .......... .......... 25% 11.1M 33s
128350K .......... .......... .......... .......... .......... 25% 8.64M 33s
128400K .......... .......... .......... .......... .......... 25% 9.26M 33s
128450K .......... .......... .......... .......... .......... 25% 7.81M 33s
128500K .......... .......... .......... .......... .......... 25% 8.27M 33s
128550K .......... .......... .......... .......... .......... 25% 9.56M 33s
128600K .......... .......... .......... .......... .......... 25% 8.25M 33s
128650K .......... .......... .......... .......... .......... 25% 15.1M 33s
128700K .......... .......... .......... .......... .......... 25% 33.9M 33s
128750K .......... .......... .......... .......... .......... 25% 31.1M 33s
128800K .......... .......... .......... .......... .......... 25% 21.7M 33s
128850K .......... .......... .......... .......... .......... 25% 21.3M 33s
128900K .......... .......... .......... .......... .......... 25% 18.6M 33s
128950K .......... .......... .......... .......... .......... 25% 17.1M 33s
129000K .......... .......... .......... .......... .......... 25% 17.9M 33s
129050K .......... .......... .......... .......... .......... 25% 15.0M 33s
129100K .......... .......... .......... .......... .......... 25% 9.47M 33s
129150K .......... .......... .......... .......... .......... 25% 9.96M 33s
129200K .......... .......... .......... .......... .......... 25% 8.46M 33s
129250K .......... .......... .......... .......... .......... 25% 11.5M 33s
129300K .......... .......... .......... .......... .......... 25% 9.11M 33s
129350K .......... .......... .......... .......... .......... 25% 7.70M 33s
129400K .......... .......... .......... .......... .......... 25% 8.09M 33s
129450K .......... .......... .......... .......... .......... 25% 10.3M 33s
129500K .......... .......... .......... .......... .......... 25% 11.9M 33s
129550K .......... .......... .......... .......... .......... 25% 13.1M 33s
129600K .......... .......... .......... .......... .......... 25% 10.5M 33s
129650K .......... .......... .......... .......... .......... 25% 12.6M 33s
129700K .......... .......... .......... .......... .......... 25% 9.04M 33s
129750K .......... .......... .......... .......... .......... 25% 6.92M 33s
129800K .......... .......... .......... .......... .......... 25% 5.86M 33s
129850K .......... .......... .......... .......... .......... 25% 5.93M 33s
129900K .......... .......... .......... .......... .......... 25% 10.5M 33s
129950K .......... .......... .......... .......... .......... 25% 8.06M 33s
130000K .......... .......... .......... .......... .......... 25% 8.60M 33s
130050K .......... .......... .......... .......... .......... 25% 7.92M 33s
130100K .......... .......... .......... .......... .......... 25% 7.13M 33s
130150K .......... .......... .......... .......... .......... 25% 7.48M 33s
130200K .......... .......... .......... .......... .......... 25% 6.79M 33s
130250K .......... .......... .......... .......... .......... 25% 7.05M 33s
130300K .......... .......... .......... .......... .......... 25% 11.5M 33s
130350K .......... .......... .......... .......... .......... 25% 6.87M 33s
130400K .......... .......... .......... .......... .......... 25% 13.1M 33s
130450K .......... .......... .......... .......... .......... 25% 9.72M 33s
130500K .......... .......... .......... .......... .......... 25% 13.1M 33s
130550K .......... .......... .......... .......... .......... 25% 9.47M 33s
130600K .......... .......... .......... .......... .......... 25% 10.4M 33s
130650K .......... .......... .......... .......... .......... 25% 12.7M 33s
130700K .......... .......... .......... .......... .......... 25% 9.53M 33s
130750K .......... .......... .......... .......... .......... 25% 10.2M 33s
130800K .......... .......... .......... .......... .......... 25% 11.5M 33s
130850K .......... .......... .......... .......... .......... 25% 10.2M 33s
130900K .......... .......... .......... .......... .......... 25% 12.6M 33s
130950K .......... .......... .......... .......... .......... 25% 8.28M 33s
131000K .......... .......... .......... .......... .......... 25% 5.26M 33s
131050K .......... .......... .......... .......... .......... 25% 5.64M 33s
131100K .......... .......... .......... .......... .......... 25% 5.79M 33s
131150K .......... .......... .......... .......... .......... 25% 7.21M 33s
131200K .......... .......... .......... .......... .......... 26% 5.62M 33s
131250K .......... .......... .......... .......... .......... 26% 8.51M 33s
131300K .......... .......... .......... .......... .......... 26% 17.1M 33s
131350K .......... .......... .......... .......... .......... 26% 22.0M 33s
131400K .......... .......... .......... .......... .......... 26% 17.1M 33s
131450K .......... .......... .......... .......... .......... 26% 16.3M 33s
131500K .......... .......... .......... .......... .......... 26% 16.5M 33s
131550K .......... .......... .......... .......... .......... 26% 13.4M 33s
131600K .......... .......... .......... .......... .......... 26% 11.1M 33s
131650K .......... .......... .......... .......... .......... 26% 13.0M 33s
131700K .......... .......... .......... .......... .......... 26% 14.0M 33s
131750K .......... .......... .......... .......... .......... 26% 13.5M 33s
131800K .......... .......... .......... .......... .......... 26% 12.3M 33s
131850K .......... .......... .......... .......... .......... 26% 8.41M 33s
131900K .......... .......... .......... .......... .......... 26% 7.32M 33s
131950K .......... .......... .......... .......... .......... 26% 5.92M 33s
132000K .......... .......... .......... .......... .......... 26% 5.87M 33s
132050K .......... .......... .......... .......... .......... 26% 5.72M 33s
132100K .......... .......... .......... .......... .......... 26% 4.61M 33s
132150K .......... .......... .......... .......... .......... 26% 8.98M 33s
132200K .......... .......... .......... .......... .......... 26% 9.36M 33s
132250K .......... .......... .......... .......... .......... 26% 86.0M 33s
132300K .......... .......... .......... .......... .......... 26% 16.1M 33s
132350K .......... .......... .......... .......... .......... 26% 15.5M 33s
132400K .......... .......... .......... .......... .......... 26% 20.3M 33s
132450K .......... .......... .......... .......... .......... 26% 16.0M 33s
132500K .......... .......... .......... .......... .......... 26% 20.2M 33s
132550K .......... .......... .......... .......... .......... 26% 18.1M 33s
132600K .......... .......... .......... .......... .......... 26% 12.9M 33s
132650K .......... .......... .......... .......... .......... 26% 12.7M 33s
132700K .......... .......... .......... .......... .......... 26% 15.5M 33s
132750K .......... .......... .......... .......... .......... 26% 11.8M 33s
132800K .......... .......... .......... .......... .......... 26% 11.1M 33s
132850K .......... .......... .......... .......... .......... 26% 8.97M 33s
132900K .......... .......... .......... .......... .......... 26% 11.1M 33s
132950K .......... .......... .......... .......... .......... 26% 12.6M 33s
133000K .......... .......... .......... .......... .......... 26% 14.6M 33s
133050K .......... .......... .......... .......... .......... 26% 14.6M 33s
133100K .......... .......... .......... .......... .......... 26% 9.70M 33s
133150K .......... .......... .......... .......... .......... 26% 9.06M 33s
133200K .......... .......... .......... .......... .......... 26% 9.45M 33s
133250K .......... .......... .......... .......... .......... 26% 14.6M 33s
133300K .......... .......... .......... .......... .......... 26% 13.6M 33s
133350K .......... .......... .......... .......... .......... 26% 8.76M 33s
133400K .......... .......... .......... .......... .......... 26% 17.1M 33s
133450K .......... .......... .......... .......... .......... 26% 14.9M 33s
133500K .......... .......... .......... .......... .......... 26% 17.4M 33s
133550K .......... .......... .......... .......... .......... 26% 13.3M 33s
133600K .......... .......... .......... .......... .......... 26% 13.9M 33s
133650K .......... .......... .......... .......... .......... 26% 13.1M 33s
133700K .......... .......... .......... .......... .......... 26% 10.1M 33s
133750K .......... .......... .......... .......... .......... 26% 15.0M 33s
133800K .......... .......... .......... .......... .......... 26% 13.6M 33s
133850K .......... .......... .......... .......... .......... 26% 11.4M 33s
133900K .......... .......... .......... .......... .......... 26% 15.6M 33s
133950K .......... .......... .......... .......... .......... 26% 12.0M 33s
134000K .......... .......... .......... .......... .......... 26% 12.9M 33s
134050K .......... .......... .......... .......... .......... 26% 13.9M 33s
134100K .......... .......... .......... .......... .......... 26% 16.3M 33s
134150K .......... .......... .......... .......... .......... 26% 15.0M 33s
134200K .......... .......... .......... .......... .......... 26% 9.40M 33s
134250K .......... .......... .......... .......... .......... 26% 14.7M 33s
134300K .......... .......... .......... .......... .......... 26% 10.1M 33s
134350K .......... .......... .......... .......... .......... 26% 8.53M 33s
134400K .......... .......... .......... .......... .......... 26% 9.30M 33s
134450K .......... .......... .......... .......... .......... 26% 5.05M 33s
134500K .......... .......... .......... .......... .......... 26% 5.11M 33s
134550K .......... .......... .......... .......... .......... 26% 4.51M 33s
134600K .......... .......... .......... .......... .......... 26% 4.05M 33s
134650K .......... .......... .......... .......... .......... 26% 4.92M 33s
134700K .......... .......... .......... .......... .......... 26% 7.20M 33s
134750K .......... .......... .......... .......... .......... 26% 12.8M 33s
134800K .......... .......... .......... .......... .......... 26% 8.36M 33s
134850K .......... .......... .......... .......... .......... 26% 7.03M 33s
134900K .......... .......... .......... .......... .......... 26% 7.53M 33s
134950K .......... .......... .......... .......... .......... 26% 8.61M 33s
135000K .......... .......... .......... .......... .......... 26% 7.77M 33s
135050K .......... .......... .......... .......... .......... 26% 9.35M 33s
135100K .......... .......... .......... .......... .......... 26% 6.18M 33s
135150K .......... .......... .......... .......... .......... 26% 9.64M 33s
135200K .......... .......... .......... .......... .......... 26% 6.03M 33s
135250K .......... .......... .......... .......... .......... 26% 8.30M 33s
135300K .......... .......... .......... .......... .......... 26% 19.6M 33s
135350K .......... .......... .......... .......... .......... 26% 15.1M 33s
135400K .......... .......... .......... .......... .......... 26% 21.3M 33s
135450K .......... .......... .......... .......... .......... 26% 22.5M 33s
135500K .......... .......... .......... .......... .......... 26% 13.9M 33s
135550K .......... .......... .......... .......... .......... 26% 25.4M 33s
135600K .......... .......... .......... .......... .......... 26% 11.8M 33s
135650K .......... .......... .......... .......... .......... 26% 9.66M 33s
135700K .......... .......... .......... .......... .......... 26% 9.75M 33s
135750K .......... .......... .......... .......... .......... 26% 9.70M 33s
135800K .......... .......... .......... .......... .......... 26% 7.78M 33s
135850K .......... .......... .......... .......... .......... 26% 11.7M 33s
135900K .......... .......... .......... .......... .......... 26% 9.93M 33s
135950K .......... .......... .......... .......... .......... 26% 12.1M 33s
136000K .......... .......... .......... .......... .......... 26% 11.7M 33s
136050K .......... .......... .......... .......... .......... 26% 13.8M 33s
136100K .......... .......... .......... .......... .......... 26% 11.1M 33s
136150K .......... .......... .......... .......... .......... 26% 12.2M 33s
136200K .......... .......... .......... .......... .......... 26% 8.34M 33s
136250K .......... .......... .......... .......... .......... 27% 7.67M 33s
136300K .......... .......... .......... .......... .......... 27% 8.38M 33s
136350K .......... .......... .......... .......... .......... 27% 8.57M 33s
136400K .......... .......... .......... .......... .......... 27% 8.21M 33s
136450K .......... .......... .......... .......... .......... 27% 8.96M 33s
136500K .......... .......... .......... .......... .......... 27% 13.4M 33s
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137000K .......... .......... .......... .......... .......... 27% 12.4M 33s
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137100K .......... .......... .......... .......... .......... 27% 7.91M 33s
137150K .......... .......... .......... .......... .......... 27% 9.03M 33s
137200K .......... .......... .......... .......... .......... 27% 8.06M 33s
137250K .......... .......... .......... .......... .......... 27% 9.21M 33s
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137400K .......... .......... .......... .......... .......... 27% 36.9M 33s
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137500K .......... .......... .......... .......... .......... 27% 59.8M 33s
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137800K .......... .......... .......... .......... .......... 27% 15.6M 33s
137850K .......... .......... .......... .......... .......... 27% 10.5M 33s
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138000K .......... .......... .......... .......... .......... 27% 10.2M 33s
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138100K .......... .......... .......... .......... .......... 27% 8.98M 33s
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140000K .......... .......... .......... .......... .......... 27% 11.8M 32s
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142150K .......... .......... .......... .......... .......... 28% 13.9M 32s
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143000K .......... .......... .......... .......... .......... 28% 17.9M 32s
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143150K .......... .......... .......... .......... .......... 28% 17.0M 32s
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149250K .......... .......... .......... .......... .......... 29% 26.7M 32s
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150000K .......... .......... .......... .......... .......... 29% 25.1M 32s
150050K .......... .......... .......... .......... .......... 29% 21.1M 32s
150100K .......... .......... .......... .......... .......... 29% 18.0M 32s
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150200K .......... .......... .......... .......... .......... 29% 19.5M 32s
150250K .......... .......... .......... .......... .......... 29% 17.9M 32s
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150350K .......... .......... .......... .......... .......... 29% 10.1M 32s
150400K .......... .......... .......... .......... .......... 29% 27.2M 32s
150450K .......... .......... .......... .......... .......... 29% 15.1M 32s
150500K .......... .......... .......... .......... .......... 29% 15.0M 32s
150550K .......... .......... .......... .......... .......... 29% 18.8M 32s
150600K .......... .......... .......... .......... .......... 29% 14.5M 32s
150650K .......... .......... .......... .......... .......... 29% 12.9M 32s
150700K .......... .......... .......... .......... .......... 29% 13.4M 32s
150750K .......... .......... .......... .......... .......... 29% 14.5M 32s
150800K .......... .......... .......... .......... .......... 29% 11.4M 32s
150850K .......... .......... .......... .......... .......... 29% 8.72M 32s
150900K .......... .......... .......... .......... .......... 29% 13.0M 32s
150950K .......... .......... .......... .......... .......... 29% 10.4M 32s
151000K .......... .......... .......... .......... .......... 29% 8.95M 32s
151050K .......... .......... .......... .......... .......... 29% 9.66M 32s
151100K .......... .......... .......... .......... .......... 29% 9.91M 32s
151150K .......... .......... .......... .......... .......... 29% 12.6M 32s
151200K .......... .......... .......... .......... .......... 29% 8.75M 32s
151250K .......... .......... .......... .......... .......... 29% 11.2M 32s
151300K .......... .......... .......... .......... .......... 29% 11.9M 32s
151350K .......... .......... .......... .......... .......... 29% 9.35M 32s
151400K .......... .......... .......... .......... .......... 30% 11.4M 32s
151450K .......... .......... .......... .......... .......... 30% 8.20M 32s
151500K .......... .......... .......... .......... .......... 30% 16.4M 32s
151550K .......... .......... .......... .......... .......... 30% 12.1M 32s
151600K .......... .......... .......... .......... .......... 30% 12.0M 32s
151650K .......... .......... .......... .......... .......... 30% 14.0M 32s
151700K .......... .......... .......... .......... .......... 30% 12.5M 32s
151750K .......... .......... .......... .......... .......... 30% 14.5M 32s
151800K .......... .......... .......... .......... .......... 30% 16.3M 32s
151850K .......... .......... .......... .......... .......... 30% 12.1M 32s
151900K .......... .......... .......... .......... .......... 30% 13.8M 32s
151950K .......... .......... .......... .......... .......... 30% 9.44M 32s
152000K .......... .......... .......... .......... .......... 30% 9.47M 32s
152050K .......... .......... .......... .......... .......... 30% 8.34M 32s
152100K .......... .......... .......... .......... .......... 30% 6.74M 32s
152150K .......... .......... .......... .......... .......... 30% 9.80M 32s
152200K .......... .......... .......... .......... .......... 30% 8.03M 32s
152250K .......... .......... .......... .......... .......... 30% 7.89M 32s
152300K .......... .......... .......... .......... .......... 30% 8.41M 32s
152350K .......... .......... .......... .......... .......... 30% 8.37M 32s
152400K .......... .......... .......... .......... .......... 30% 7.12M 32s
152450K .......... .......... .......... .......... .......... 30% 5.42M 32s
152500K .......... .......... .......... .......... .......... 30% 5.93M 32s
152550K .......... .......... .......... .......... .......... 30% 6.00M 32s
152600K .......... .......... .......... .......... .......... 30% 5.36M 32s
152650K .......... .......... .......... .......... .......... 30% 6.00M 32s
152700K .......... .......... .......... .......... .......... 30% 4.76M 32s
152750K .......... .......... .......... .......... .......... 30% 8.85M 32s
152800K .......... .......... .......... .......... .......... 30% 20.7M 32s
152850K .......... .......... .......... .......... .......... 30% 21.7M 32s
152900K .......... .......... .......... .......... .......... 30% 28.9M 32s
152950K .......... .......... .......... .......... .......... 30% 32.3M 32s
153000K .......... .......... .......... .......... .......... 30% 28.3M 32s
153050K .......... .......... .......... .......... .......... 30% 26.9M 32s
153100K .......... .......... .......... .......... .......... 30% 16.3M 32s
153150K .......... .......... .......... .......... .......... 30% 53.1M 32s
153200K .......... .......... .......... .......... .......... 30% 19.0M 32s
153250K .......... .......... .......... .......... .......... 30% 21.5M 32s
153300K .......... .......... .......... .......... .......... 30% 19.7M 32s
153350K .......... .......... .......... .......... .......... 30% 17.1M 32s
153400K .......... .......... .......... .......... .......... 30% 14.5M 32s
153450K .......... .......... .......... .......... .......... 30% 14.5M 32s
153500K .......... .......... .......... .......... .......... 30% 11.3M 32s
153550K .......... .......... .......... .......... .......... 30% 14.1M 32s
153600K .......... .......... .......... .......... .......... 30% 9.65M 31s
153650K .......... .......... .......... .......... .......... 30% 9.59M 31s
153700K .......... .......... .......... .......... .......... 30% 9.64M 31s
153750K .......... .......... .......... .......... .......... 30% 12.2M 31s
153800K .......... .......... .......... .......... .......... 30% 15.1M 31s
153850K .......... .......... .......... .......... .......... 30% 11.8M 31s
153900K .......... .......... .......... .......... .......... 30% 16.9M 31s
153950K .......... .......... .......... .......... .......... 30% 15.2M 31s
154000K .......... .......... .......... .......... .......... 30% 17.6M 31s
154050K .......... .......... .......... .......... .......... 30% 12.6M 31s
154100K .......... .......... .......... .......... .......... 30% 8.53M 31s
154150K .......... .......... .......... .......... .......... 30% 7.29M 31s
154200K .......... .......... .......... .......... .......... 30% 10.2M 31s
154250K .......... .......... .......... .......... .......... 30% 10.8M 31s
154300K .......... .......... .......... .......... .......... 30% 9.92M 31s
154350K .......... .......... .......... .......... .......... 30% 8.21M 31s
154400K .......... .......... .......... .......... .......... 30% 8.01M 31s
154450K .......... .......... .......... .......... .......... 30% 9.44M 31s
154500K .......... .......... .......... .......... .......... 30% 14.4M 31s
154550K .......... .......... .......... .......... .......... 30% 11.9M 31s
154600K .......... .......... .......... .......... .......... 30% 8.14M 31s
154650K .......... .......... .......... .......... .......... 30% 10.2M 31s
154700K .......... .......... .......... .......... .......... 30% 8.23M 31s
154750K .......... .......... .......... .......... .......... 30% 8.40M 31s
154800K .......... .......... .......... .......... .......... 30% 7.54M 31s
154850K .......... .......... .......... .......... .......... 30% 7.84M 31s
154900K .......... .......... .......... .......... .......... 30% 8.22M 31s
154950K .......... .......... .......... .......... .......... 30% 6.61M 31s
155000K .......... .......... .......... .......... .......... 30% 9.24M 31s
155050K .......... .......... .......... .......... .......... 30% 5.73M 31s
155100K .......... .......... .......... .......... .......... 30% 6.85M 31s
155150K .......... .......... .......... .......... .......... 30% 14.3M 31s
155200K .......... .......... .......... .......... .......... 30% 10.7M 31s
155250K .......... .......... .......... .......... .......... 30% 12.5M 31s
155300K .......... .......... .......... .......... .......... 30% 15.7M 31s
155350K .......... .......... .......... .......... .......... 30% 11.8M 31s
155400K .......... .......... .......... .......... .......... 30% 13.4M 31s
155450K .......... .......... .......... .......... .......... 30% 11.0M 31s
155500K .......... .......... .......... .......... .......... 30% 12.9M 31s
155550K .......... .......... .......... .......... .......... 30% 10.5M 31s
155600K .......... .......... .......... .......... .......... 30% 6.06M 31s
155650K .......... .......... .......... .......... .......... 30% 14.8M 31s
155700K .......... .......... .......... .......... .......... 30% 6.75M 31s
155750K .......... .......... .......... .......... .......... 30% 11.5M 31s
155800K .......... .......... .......... .......... .......... 30% 12.0M 31s
155850K .......... .......... .......... .......... .......... 30% 12.2M 31s
155900K .......... .......... .......... .......... .......... 30% 12.1M 31s
155950K .......... .......... .......... .......... .......... 30% 11.5M 31s
156000K .......... .......... .......... .......... .......... 30% 9.85M 31s
156050K .......... .......... .......... .......... .......... 30% 13.8M 31s
156100K .......... .......... .......... .......... .......... 30% 9.89M 31s
156150K .......... .......... .......... .......... .......... 30% 14.4M 31s
156200K .......... .......... .......... .......... .......... 30% 14.5M 31s
156250K .......... .......... .......... .......... .......... 30% 16.2M 31s
156300K .......... .......... .......... .......... .......... 30% 15.7M 31s
156350K .......... .......... .......... .......... .......... 30% 11.7M 31s
156400K .......... .......... .......... .......... .......... 30% 15.6M 31s
156450K .......... .......... .......... .......... .......... 31% 11.1M 31s
156500K .......... .......... .......... .......... .......... 31% 12.0M 31s
156550K .......... .......... .......... .......... .......... 31% 7.40M 31s
156600K .......... .......... .......... .......... .......... 31% 4.22M 31s
156650K .......... .......... .......... .......... .......... 31% 7.89M 31s
156700K .......... .......... .......... .......... .......... 31% 5.71M 31s
156750K .......... .......... .......... .......... .......... 31% 5.73M 31s
156800K .......... .......... .......... .......... .......... 31% 6.60M 31s
156850K .......... .......... .......... .......... .......... 31% 7.29M 31s
156900K .......... .......... .......... .......... .......... 31% 6.40M 31s
156950K .......... .......... .......... .......... .......... 31% 13.1M 31s
157000K .......... .......... .......... .......... .......... 31% 9.95M 31s
157050K .......... .......... .......... .......... .......... 31% 10.6M 31s
157100K .......... .......... .......... .......... .......... 31% 11.8M 31s
157150K .......... .......... .......... .......... .......... 31% 9.66M 31s
157200K .......... .......... .......... .......... .......... 31% 11.7M 31s
157250K .......... .......... .......... .......... .......... 31% 10.5M 31s
157300K .......... .......... .......... .......... .......... 31% 9.97M 31s
157350K .......... .......... .......... .......... .......... 31% 6.07M 31s
157400K .......... .......... .......... .......... .......... 31% 7.02M 31s
157450K .......... .......... .......... .......... .......... 31% 7.25M 31s
157500K .......... .......... .......... .......... .......... 31% 6.33M 31s
157550K .......... .......... .......... .......... .......... 31% 8.40M 31s
157600K .......... .......... .......... .......... .......... 31% 13.7M 31s
157650K .......... .......... .......... .......... .......... 31% 22.6M 31s
157700K .......... .......... .......... .......... .......... 31% 12.4M 31s
157750K .......... .......... .......... .......... .......... 31% 14.0M 31s
157800K .......... .......... .......... .......... .......... 31% 8.17M 31s
157850K .......... .......... .......... .......... .......... 31% 6.97M 31s
157900K .......... .......... .......... .......... .......... 31% 11.8M 31s
157950K .......... .......... .......... .......... .......... 31% 9.41M 31s
158000K .......... .......... .......... .......... .......... 31% 10.8M 31s
158050K .......... .......... .......... .......... .......... 31% 11.8M 31s
158100K .......... .......... .......... .......... .......... 31% 8.22M 31s
158150K .......... .......... .......... .......... .......... 31% 11.4M 31s
158200K .......... .......... .......... .......... .......... 31% 7.15M 31s
158250K .......... .......... .......... .......... .......... 31% 20.1M 31s
158300K .......... .......... .......... .......... .......... 31% 12.1M 31s
158350K .......... .......... .......... .......... .......... 31% 8.95M 31s
158400K .......... .......... .......... .......... .......... 31% 10.5M 31s
158450K .......... .......... .......... .......... .......... 31% 8.21M 31s
158500K .......... .......... .......... .......... .......... 31% 11.5M 31s
158550K .......... .......... .......... .......... .......... 31% 9.19M 31s
158600K .......... .......... .......... .......... .......... 31% 8.41M 31s
158650K .......... .......... .......... .......... .......... 31% 7.69M 31s
158700K .......... .......... .......... .......... .......... 31% 8.53M 31s
158750K .......... .......... .......... .......... .......... 31% 9.20M 31s
158800K .......... .......... .......... .......... .......... 31% 14.4M 31s
158850K .......... .......... .......... .......... .......... 31% 10.1M 31s
158900K .......... .......... .......... .......... .......... 31% 12.2M 31s
158950K .......... .......... .......... .......... .......... 31% 10.2M 31s
159000K .......... .......... .......... .......... .......... 31% 15.7M 31s
159050K .......... .......... .......... .......... .......... 31% 15.5M 31s
159100K .......... .......... .......... .......... .......... 31% 13.4M 31s
159150K .......... .......... .......... .......... .......... 31% 12.2M 31s
159200K .......... .......... .......... .......... .......... 31% 11.5M 31s
159250K .......... .......... .......... .......... .......... 31% 14.4M 31s
159300K .......... .......... .......... .......... .......... 31% 10.8M 31s
159350K .......... .......... .......... .......... .......... 31% 10.7M 31s
159400K .......... .......... .......... .......... .......... 31% 10.7M 31s
159450K .......... .......... .......... .......... .......... 31% 8.78M 31s
159500K .......... .......... .......... .......... .......... 31% 11.4M 31s
159550K .......... .......... .......... .......... .......... 31% 10.8M 31s
159600K .......... .......... .......... .......... .......... 31% 10.2M 31s
159650K .......... .......... .......... .......... .......... 31% 10.5M 31s
159700K .......... .......... .......... .......... .......... 31% 11.8M 31s
159750K .......... .......... .......... .......... .......... 31% 19.6M 31s
159800K .......... .......... .......... .......... .......... 31% 20.6M 31s
159850K .......... .......... .......... .......... .......... 31% 12.5M 31s
159900K .......... .......... .......... .......... .......... 31% 14.4M 31s
159950K .......... .......... .......... .......... .......... 31% 9.86M 31s
160000K .......... .......... .......... .......... .......... 31% 15.0M 31s
160050K .......... .......... .......... .......... .......... 31% 17.0M 31s
160100K .......... .......... .......... .......... .......... 31% 12.1M 31s
160150K .......... .......... .......... .......... .......... 31% 12.1M 31s
160200K .......... .......... .......... .......... .......... 31% 12.5M 31s
160250K .......... .......... .......... .......... .......... 31% 11.5M 31s
160300K .......... .......... .......... .......... .......... 31% 16.4M 31s
160350K .......... .......... .......... .......... .......... 31% 10.1M 31s
160400K .......... .......... .......... .......... .......... 31% 14.6M 31s
160450K .......... .......... .......... .......... .......... 31% 17.5M 31s
160500K .......... .......... .......... .......... .......... 31% 26.0M 31s
160550K .......... .......... .......... .......... .......... 31% 19.5M 31s
160600K .......... .......... .......... .......... .......... 31% 21.8M 31s
160650K .......... .......... .......... .......... .......... 31% 21.9M 31s
160700K .......... .......... .......... .......... .......... 31% 12.1M 31s
160750K .......... .......... .......... .......... .......... 31% 17.8M 31s
160800K .......... .......... .......... .......... .......... 31% 23.5M 31s
160850K .......... .......... .......... .......... .......... 31% 13.8M 31s
160900K .......... .......... .......... .......... .......... 31% 13.9M 31s
160950K .......... .......... .......... .......... .......... 31% 15.6M 31s
161000K .......... .......... .......... .......... .......... 31% 18.9M 31s
161050K .......... .......... .......... .......... .......... 31% 15.6M 31s
161100K .......... .......... .......... .......... .......... 31% 13.3M 31s
161150K .......... .......... .......... .......... .......... 31% 16.3M 31s
161200K .......... .......... .......... .......... .......... 31% 14.0M 31s
161250K .......... .......... .......... .......... .......... 31% 14.5M 31s
161300K .......... .......... .......... .......... .......... 31% 15.1M 31s
161350K .......... .......... .......... .......... .......... 31% 11.8M 31s
161400K .......... .......... .......... .......... .......... 31% 9.69M 31s
161450K .......... .......... .......... .......... .......... 32% 12.1M 31s
161500K .......... .......... .......... .......... .......... 32% 11.1M 31s
161550K .......... .......... .......... .......... .......... 32% 9.53M 31s
161600K .......... .......... .......... .......... .......... 32% 9.97M 31s
161650K .......... .......... .......... .......... .......... 32% 13.6M 31s
161700K .......... .......... .......... .......... .......... 32% 9.77M 31s
161750K .......... .......... .......... .......... .......... 32% 11.5M 31s
161800K .......... .......... .......... .......... .......... 32% 7.92M 31s
161850K .......... .......... .......... .......... .......... 32% 6.32M 31s
161900K .......... .......... .......... .......... .......... 32% 6.04M 31s
161950K .......... .......... .......... .......... .......... 32% 4.72M 31s
162000K .......... .......... .......... .......... .......... 32% 3.90M 31s
162050K .......... .......... .......... .......... .......... 32% 3.25M 31s
162100K .......... .......... .......... .......... .......... 32% 3.51M 31s
162150K .......... .......... .......... .......... .......... 32% 3.73M 31s
162200K .......... .......... .......... .......... .......... 32% 3.99M 31s
162250K .......... .......... .......... .......... .......... 32% 14.0M 31s
162300K .......... .......... .......... .......... .......... 32% 18.3M 31s
162350K .......... .......... .......... .......... .......... 32% 16.3M 31s
162400K .......... .......... .......... .......... .......... 32% 11.8M 31s
162450K .......... .......... .......... .......... .......... 32% 10.7M 31s
162500K .......... .......... .......... .......... .......... 32% 15.1M 31s
162550K .......... .......... .......... .......... .......... 32% 10.4M 31s
162600K .......... .......... .......... .......... .......... 32% 11.4M 31s
162650K .......... .......... .......... .......... .......... 32% 8.42M 31s
162700K .......... .......... .......... .......... .......... 32% 7.84M 31s
162750K .......... .......... .......... .......... .......... 32% 9.48M 31s
162800K .......... .......... .......... .......... .......... 32% 11.5M 31s
162850K .......... .......... .......... .......... .......... 32% 6.94M 31s
162900K .......... .......... .......... .......... .......... 32% 6.61M 31s
162950K .......... .......... .......... .......... .......... 32% 5.60M 31s
163000K .......... .......... .......... .......... .......... 32% 6.35M 31s
163050K .......... .......... .......... .......... .......... 32% 6.44M 31s
163100K .......... .......... .......... .......... .......... 32% 8.38M 31s
163150K .......... .......... .......... .......... .......... 32% 9.66M 31s
163200K .......... .......... .......... .......... .......... 32% 8.18M 31s
163250K .......... .......... .......... .......... .......... 32% 8.42M 31s
163300K .......... .......... .......... .......... .......... 32% 7.52M 31s
163350K .......... .......... .......... .......... .......... 32% 10.2M 31s
163400K .......... .......... .......... .......... .......... 32% 9.03M 31s
163450K .......... .......... .......... .......... .......... 32% 6.20M 31s
163500K .......... .......... .......... .......... .......... 32% 7.56M 31s
163550K .......... .......... .......... .......... .......... 32% 7.01M 31s
163600K .......... .......... .......... .......... .......... 32% 4.54M 31s
163650K .......... .......... .......... .......... .......... 32% 7.59M 31s
163700K .......... .......... .......... .......... .......... 32% 15.7M 31s
163750K .......... .......... .......... .......... .......... 32% 17.0M 31s
163800K .......... .......... .......... .......... .......... 32% 16.3M 31s
163850K .......... .......... .......... .......... .......... 32% 13.4M 31s
163900K .......... .......... .......... .......... .......... 32% 10.5M 31s
163950K .......... .......... .......... .......... .......... 32% 7.54M 31s
164000K .......... .......... .......... .......... .......... 32% 7.27M 31s
164050K .......... .......... .......... .......... .......... 32% 12.9M 31s
164100K .......... .......... .......... .......... .......... 32% 7.87M 31s
164150K .......... .......... .......... .......... .......... 32% 7.13M 31s
164200K .......... .......... .......... .......... .......... 32% 7.78M 31s
164250K .......... .......... .......... .......... .......... 32% 9.71M 31s
164300K .......... .......... .......... .......... .......... 32% 8.42M 31s
164350K .......... .......... .......... .......... .......... 32% 6.72M 31s
164400K .......... .......... .......... .......... .......... 32% 11.4M 31s
164450K .......... .......... .......... .......... .......... 32% 8.76M 31s
164500K .......... .......... .......... .......... .......... 32% 9.41M 31s
164550K .......... .......... .......... .......... .......... 32% 11.3M 31s
164600K .......... .......... .......... .......... .......... 32% 8.39M 31s
164650K .......... .......... .......... .......... .......... 32% 15.0M 31s
164700K .......... .......... .......... .......... .......... 32% 6.60M 31s
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165000K .......... .......... .......... .......... .......... 32% 12.6M 31s
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178700K .......... .......... .......... .......... .......... 35% 11.4M 30s
178750K .......... .......... .......... .......... .......... 35% 6.54M 30s
178800K .......... .......... .......... .......... .......... 35% 6.91M 30s
178850K .......... .......... .......... .......... .......... 35% 6.02M 30s
178900K .......... .......... .......... .......... .......... 35% 6.97M 30s
178950K .......... .......... .......... .......... .......... 35% 6.04M 30s
179000K .......... .......... .......... .......... .......... 35% 6.55M 30s
179050K .......... .......... .......... .......... .......... 35% 11.6M 30s
179100K .......... .......... .......... .......... .......... 35% 18.5M 30s
179150K .......... .......... .......... .......... .......... 35% 26.9M 30s
179200K .......... .......... .......... .......... .......... 35% 34.4M 30s
179250K .......... .......... .......... .......... .......... 35% 20.0M 30s
179300K .......... .......... .......... .......... .......... 35% 13.5M 30s
179350K .......... .......... .......... .......... .......... 35% 12.1M 30s
179400K .......... .......... .......... .......... .......... 35% 7.59M 30s
179450K .......... .......... .......... .......... .......... 35% 9.70M 30s
179500K .......... .......... .......... .......... .......... 35% 11.4M 30s
179550K .......... .......... .......... .......... .......... 35% 12.7M 30s
179600K .......... .......... .......... .......... .......... 35% 10.8M 30s
179650K .......... .......... .......... .......... .......... 35% 10.7M 30s
179700K .......... .......... .......... .......... .......... 35% 8.97M 30s
179750K .......... .......... .......... .......... .......... 35% 8.76M 30s
179800K .......... .......... .......... .......... .......... 35% 6.71M 30s
179850K .......... .......... .......... .......... .......... 35% 6.37M 30s
179900K .......... .......... .......... .......... .......... 35% 6.09M 30s
179950K .......... .......... .......... .......... .......... 35% 7.60M 30s
180000K .......... .......... .......... .......... .......... 35% 12.9M 30s
180050K .......... .......... .......... .......... .......... 35% 8.59M 30s
180100K .......... .......... .......... .......... .......... 35% 7.14M 30s
180150K .......... .......... .......... .......... .......... 35% 10.5M 29s
180200K .......... .......... .......... .......... .......... 35% 9.73M 29s
180250K .......... .......... .......... .......... .......... 35% 9.14M 29s
180300K .......... .......... .......... .......... .......... 35% 11.1M 29s
180350K .......... .......... .......... .......... .......... 35% 9.91M 29s
180400K .......... .......... .......... .......... .......... 35% 12.6M 29s
180450K .......... .......... .......... .......... .......... 35% 10.2M 29s
180500K .......... .......... .......... .......... .......... 35% 24.7M 29s
180550K .......... .......... .......... .......... .......... 35% 38.8M 29s
180600K .......... .......... .......... .......... .......... 35% 24.1M 29s
180650K .......... .......... .......... .......... .......... 35% 35.7M 29s
180700K .......... .......... .......... .......... .......... 35% 23.8M 29s
180750K .......... .......... .......... .......... .......... 35% 40.3M 29s
180800K .......... .......... .......... .......... .......... 35% 18.6M 29s
180850K .......... .......... .......... .......... .......... 35% 16.0M 29s
180900K .......... .......... .......... .......... .......... 35% 18.3M 29s
180950K .......... .......... .......... .......... .......... 35% 18.3M 29s
181000K .......... .......... .......... .......... .......... 35% 16.0M 29s
181050K .......... .......... .......... .......... .......... 35% 15.9M 29s
181100K .......... .......... .......... .......... .......... 35% 17.5M 29s
181150K .......... .......... .......... .......... .......... 35% 17.1M 29s
181200K .......... .......... .......... .......... .......... 35% 15.8M 29s
181250K .......... .......... .......... .......... .......... 35% 14.9M 29s
181300K .......... .......... .......... .......... .......... 35% 16.3M 29s
181350K .......... .......... .......... .......... .......... 35% 12.2M 29s
181400K .......... .......... .......... .......... .......... 35% 16.0M 29s
181450K .......... .......... .......... .......... .......... 35% 12.5M 29s
181500K .......... .......... .......... .......... .......... 35% 5.05M 29s
181550K .......... .......... .......... .......... .......... 35% 4.30M 29s
181600K .......... .......... .......... .......... .......... 35% 3.08M 29s
181650K .......... .......... .......... .......... .......... 36% 6.76M 29s
181700K .......... .......... .......... .......... .......... 36% 19.6M 29s
181750K .......... .......... .......... .......... .......... 36% 11.5M 29s
181800K .......... .......... .......... .......... .......... 36% 19.0M 29s
181850K .......... .......... .......... .......... .......... 36% 12.9M 29s
181900K .......... .......... .......... .......... .......... 36% 15.1M 29s
181950K .......... .......... .......... .......... .......... 36% 18.6M 29s
182000K .......... .......... .......... .......... .......... 36% 17.0M 29s
182050K .......... .......... .......... .......... .......... 36% 19.9M 29s
182100K .......... .......... .......... .......... .......... 36% 13.8M 29s
182150K .......... .......... .......... .......... .......... 36% 16.4M 29s
182200K .......... .......... .......... .......... .......... 36% 13.8M 29s
182250K .......... .......... .......... .......... .......... 36% 13.6M 29s
182300K .......... .......... .......... .......... .......... 36% 16.3M 29s
182350K .......... .......... .......... .......... .......... 36% 12.5M 29s
182400K .......... .......... .......... .......... .......... 36% 17.0M 29s
182450K .......... .......... .......... .......... .......... 36% 13.9M 29s
182500K .......... .......... .......... .......... .......... 36% 9.97M 29s
182550K .......... .......... .......... .......... .......... 36% 8.56M 29s
182600K .......... .......... .......... .......... .......... 36% 10.7M 29s
182650K .......... .......... .......... .......... .......... 36% 11.7M 29s
182700K .......... .......... .......... .......... .......... 36% 10.7M 29s
182750K .......... .......... .......... .......... .......... 36% 11.4M 29s
182800K .......... .......... .......... .......... .......... 36% 8.95M 29s
182850K .......... .......... .......... .......... .......... 36% 6.79M 29s
182900K .......... .......... .......... .......... .......... 36% 10.5M 29s
182950K .......... .......... .......... .......... .......... 36% 5.21M 29s
183000K .......... .......... .......... .......... .......... 36% 7.15M 29s
183050K .......... .......... .......... .......... .......... 36% 7.09M 29s
183100K .......... .......... .......... .......... .......... 36% 5.13M 29s
183150K .......... .......... .......... .......... .......... 36% 7.13M 29s
183200K .......... .......... .......... .......... .......... 36% 6.77M 29s
183250K .......... .......... .......... .......... .......... 36% 17.8M 29s
183300K .......... .......... .......... .......... .......... 36% 34.3M 29s
183350K .......... .......... .......... .......... .......... 36% 11.7M 29s
183400K .......... .......... .......... .......... .......... 36% 15.2M 29s
183450K .......... .......... .......... .......... .......... 36% 16.5M 29s
183500K .......... .......... .......... .......... .......... 36% 16.1M 29s
183550K .......... .......... .......... .......... .......... 36% 10.2M 29s
183600K .......... .......... .......... .......... .......... 36% 6.98M 29s
183650K .......... .......... .......... .......... .......... 36% 9.17M 29s
183700K .......... .......... .......... .......... .......... 36% 12.5M 29s
183750K .......... .......... .......... .......... .......... 36% 14.9M 29s
183800K .......... .......... .......... .......... .......... 36% 9.68M 29s
183850K .......... .......... .......... .......... .......... 36% 10.2M 29s
183900K .......... .......... .......... .......... .......... 36% 17.3M 29s
183950K .......... .......... .......... .......... .......... 36% 12.7M 29s
184000K .......... .......... .......... .......... .......... 36% 12.8M 29s
184050K .......... .......... .......... .......... .......... 36% 12.1M 29s
184100K .......... .......... .......... .......... .......... 36% 17.4M 29s
184150K .......... .......... .......... .......... .......... 36% 7.55M 29s
184200K .......... .......... .......... .......... .......... 36% 9.19M 29s
184250K .......... .......... .......... .......... .......... 36% 9.61M 29s
184300K .......... .......... .......... .......... .......... 36% 10.2M 29s
184350K .......... .......... .......... .......... .......... 36% 6.61M 29s
184400K .......... .......... .......... .......... .......... 36% 7.02M 29s
184450K .......... .......... .......... .......... .......... 36% 8.61M 29s
184500K .......... .......... .......... .......... .......... 36% 7.91M 29s
184550K .......... .......... .......... .......... .......... 36% 11.9M 29s
184600K .......... .......... .......... .......... .......... 36% 22.1M 29s
184650K .......... .......... .......... .......... .......... 36% 41.7M 29s
184700K .......... .......... .......... .......... .......... 36% 33.7M 29s
184750K .......... .......... .......... .......... .......... 36% 23.3M 29s
184800K .......... .......... .......... .......... .......... 36% 21.9M 29s
184850K .......... .......... .......... .......... .......... 36% 18.0M 29s
184900K .......... .......... .......... .......... .......... 36% 19.8M 29s
184950K .......... .......... .......... .......... .......... 36% 14.9M 29s
185000K .......... .......... .......... .......... .......... 36% 12.7M 29s
185050K .......... .......... .......... .......... .......... 36% 20.9M 29s
185100K .......... .......... .......... .......... .......... 36% 13.2M 29s
185150K .......... .......... .......... .......... .......... 36% 14.9M 29s
185200K .......... .......... .......... .......... .......... 36% 13.4M 29s
185250K .......... .......... .......... .......... .......... 36% 14.4M 29s
185300K .......... .......... .......... .......... .......... 36% 12.7M 29s
185350K .......... .......... .......... .......... .......... 36% 6.99M 29s
185400K .......... .......... .......... .......... .......... 36% 9.98M 29s
185450K .......... .......... .......... .......... .......... 36% 7.14M 29s
185500K .......... .......... .......... .......... .......... 36% 8.65M 29s
185550K .......... .......... .......... .......... .......... 36% 7.04M 29s
185600K .......... .......... .......... .......... .......... 36% 6.58M 29s
185650K .......... .......... .......... .......... .......... 36% 24.6M 29s
185700K .......... .......... .......... .......... .......... 36% 18.9M 29s
185750K .......... .......... .......... .......... .......... 36% 31.4M 29s
185800K .......... .......... .......... .......... .......... 36% 20.9M 29s
185850K .......... .......... .......... .......... .......... 36% 17.6M 29s
185900K .......... .......... .......... .......... .......... 36% 16.6M 29s
185950K .......... .......... .......... .......... .......... 36% 14.7M 29s
186000K .......... .......... .......... .......... .......... 36% 15.4M 29s
186050K .......... .......... .......... .......... .......... 36% 18.0M 29s
186100K .......... .......... .......... .......... .......... 36% 15.2M 29s
186150K .......... .......... .......... .......... .......... 36% 21.7M 29s
186200K .......... .......... .......... .......... .......... 36% 14.6M 29s
186250K .......... .......... .......... .......... .......... 36% 13.8M 29s
186300K .......... .......... .......... .......... .......... 36% 17.1M 29s
186350K .......... .......... .......... .......... .......... 36% 12.6M 29s
186400K .......... .......... .......... .......... .......... 36% 15.0M 29s
186450K .......... .......... .......... .......... .......... 36% 14.6M 29s
186500K .......... .......... .......... .......... .......... 36% 13.0M 29s
186550K .......... .......... .......... .......... .......... 36% 14.9M 29s
186600K .......... .......... .......... .......... .......... 36% 13.1M 29s
186650K .......... .......... .......... .......... .......... 36% 9.01M 29s
186700K .......... .......... .......... .......... .......... 37% 15.7M 29s
186750K .......... .......... .......... .......... .......... 37% 15.6M 29s
186800K .......... .......... .......... .......... .......... 37% 12.5M 29s
186850K .......... .......... .......... .......... .......... 37% 12.9M 29s
186900K .......... .......... .......... .......... .......... 37% 13.5M 29s
186950K .......... .......... .......... .......... .......... 37% 9.91M 29s
187000K .......... .......... .......... .......... .......... 37% 11.8M 29s
187050K .......... .......... .......... .......... .......... 37% 10.2M 29s
187100K .......... .......... .......... .......... .......... 37% 11.6M 29s
187150K .......... .......... .......... .......... .......... 37% 12.8M 29s
187200K .......... .......... .......... .......... .......... 37% 9.93M 29s
187250K .......... .......... .......... .......... .......... 37% 10.8M 29s
187300K .......... .......... .......... .......... .......... 37% 12.6M 29s
187350K .......... .......... .......... .......... .......... 37% 9.49M 29s
187400K .......... .......... .......... .......... .......... 37% 10.3M 29s
187450K .......... .......... .......... .......... .......... 37% 13.4M 29s
187500K .......... .......... .......... .......... .......... 37% 13.9M 29s
187550K .......... .......... .......... .......... .......... 37% 14.4M 29s
187600K .......... .......... .......... .......... .......... 37% 12.1M 29s
187650K .......... .......... .......... .......... .......... 37% 11.8M 29s
187700K .......... .......... .......... .......... .......... 37% 12.1M 29s
187750K .......... .......... .......... .......... .......... 37% 13.6M 29s
187800K .......... .......... .......... .......... .......... 37% 12.9M 29s
187850K .......... .......... .......... .......... .......... 37% 9.83M 29s
187900K .......... .......... .......... .......... .......... 37% 12.5M 29s
187950K .......... .......... .......... .......... .......... 37% 9.95M 29s
188000K .......... .......... .......... .......... .......... 37% 11.7M 29s
188050K .......... .......... .......... .......... .......... 37% 11.4M 29s
188100K .......... .......... .......... .......... .......... 37% 8.71M 29s
188150K .......... .......... .......... .......... .......... 37% 11.9M 29s
188200K .......... .......... .......... .......... .......... 37% 8.64M 29s
188250K .......... .......... .......... .......... .......... 37% 29.2M 29s
188300K .......... .......... .......... .......... .......... 37% 14.5M 29s
188350K .......... .......... .......... .......... .......... 37% 16.2M 29s
188400K .......... .......... .......... .......... .......... 37% 13.0M 29s
188450K .......... .......... .......... .......... .......... 37% 26.9M 29s
188500K .......... .......... .......... .......... .......... 37% 10.2M 29s
188550K .......... .......... .......... .......... .......... 37% 17.8M 29s
188600K .......... .......... .......... .......... .......... 37% 14.5M 29s
188650K .......... .......... .......... .......... .......... 37% 12.6M 29s
188700K .......... .......... .......... .......... .......... 37% 11.0M 29s
188750K .......... .......... .......... .......... .......... 37% 13.4M 29s
188800K .......... .......... .......... .......... .......... 37% 10.1M 29s
188850K .......... .......... .......... .......... .......... 37% 10.5M 29s
188900K .......... .......... .......... .......... .......... 37% 11.9M 29s
188950K .......... .......... .......... .......... .......... 37% 9.93M 29s
189000K .......... .......... .......... .......... .......... 37% 10.7M 29s
189050K .......... .......... .......... .......... .......... 37% 9.66M 29s
189100K .......... .......... .......... .......... .......... 37% 8.58M 29s
189150K .......... .......... .......... .......... .......... 37% 8.55M 29s
189200K .......... .......... .......... .......... .......... 37% 9.23M 29s
189250K .......... .......... .......... .......... .......... 37% 8.01M 29s
189300K .......... .......... .......... .......... .......... 37% 7.86M 29s
189350K .......... .......... .......... .......... .......... 37% 5.92M 29s
189400K .......... .......... .......... .......... .......... 37% 6.13M 29s
189450K .......... .......... .......... .......... .......... 37% 4.88M 29s
189500K .......... .......... .......... .......... .......... 37% 6.52M 29s
189550K .......... .......... .......... .......... .......... 37% 11.8M 29s
189600K .......... .......... .......... .......... .......... 37% 20.9M 29s
189650K .......... .......... .......... .......... .......... 37% 11.8M 29s
189700K .......... .......... .......... .......... .......... 37% 6.88M 29s
189750K .......... .......... .......... .......... .......... 37% 10.8M 29s
189800K .......... .......... .......... .......... .......... 37% 4.61M 29s
189850K .......... .......... .......... .......... .......... 37% 2.30M 29s
189900K .......... .......... .......... .......... .......... 37% 3.56M 29s
189950K .......... .......... .......... .......... .......... 37% 15.2M 29s
190000K .......... .......... .......... .......... .......... 37% 7.63M 29s
190050K .......... .......... .......... .......... .......... 37% 6.01M 29s
190100K .......... .......... .......... .......... .......... 37% 4.64M 29s
190150K .......... .......... .......... .......... .......... 37% 5.15M 29s
190200K .......... .......... .......... .......... .......... 37% 5.47M 29s
190250K .......... .......... .......... .......... .......... 37% 8.23M 29s
190300K .......... .......... .......... .......... .......... 37% 7.86M 29s
190350K .......... .......... .......... .......... .......... 37% 7.30M 29s
190400K .......... .......... .......... .......... .......... 37% 8.55M 29s
190450K .......... .......... .......... .......... .......... 37% 13.5M 29s
190500K .......... .......... .......... .......... .......... 37% 37.0M 29s
190550K .......... .......... .......... .......... .......... 37% 18.8M 29s
190600K .......... .......... .......... .......... .......... 37% 52.2M 29s
190650K .......... .......... .......... .......... .......... 37% 20.9M 29s
190700K .......... .......... .......... .......... .......... 37% 16.1M 29s
190750K .......... .......... .......... .......... .......... 37% 15.6M 29s
190800K .......... .......... .......... .......... .......... 37% 23.6M 29s
190850K .......... .......... .......... .......... .......... 37% 15.1M 28s
190900K .......... .......... .......... .......... .......... 37% 10.0M 28s
190950K .......... .......... .......... .......... .......... 37% 8.95M 28s
191000K .......... .......... .......... .......... .......... 37% 12.1M 28s
191050K .......... .......... .......... .......... .......... 37% 12.6M 28s
191100K .......... .......... .......... .......... .......... 37% 11.4M 28s
191150K .......... .......... .......... .......... .......... 37% 11.8M 28s
191200K .......... .......... .......... .......... .......... 37% 11.1M 28s
191250K .......... .......... .......... .......... .......... 37% 13.4M 28s
191300K .......... .......... .......... .......... .......... 37% 13.1M 28s
191350K .......... .......... .......... .......... .......... 37% 11.7M 28s
191400K .......... .......... .......... .......... .......... 37% 72.7M 28s
191450K .......... .......... .......... .......... .......... 37% 20.8M 28s
191500K .......... .......... .......... .......... .......... 37% 16.3M 28s
191550K .......... .......... .......... .......... .......... 37% 20.6M 28s
191600K .......... .......... .......... .......... .......... 37% 10.4M 28s
191650K .......... .......... .......... .......... .......... 37% 10.2M 28s
191700K .......... .......... .......... .......... .......... 37% 7.39M 28s
191750K .......... .......... .......... .......... .......... 38% 10.4M 28s
191800K .......... .......... .......... .......... .......... 38% 8.96M 28s
191850K .......... .......... .......... .......... .......... 38% 8.03M 28s
191900K .......... .......... .......... .......... .......... 38% 6.05M 28s
191950K .......... .......... .......... .......... .......... 38% 12.2M 28s
192000K .......... .......... .......... .......... .......... 38% 15.1M 28s
192050K .......... .......... .......... .......... .......... 38% 28.7M 28s
192100K .......... .......... .......... .......... .......... 38% 10.8M 28s
192150K .......... .......... .......... .......... .......... 38% 10.4M 28s
192200K .......... .......... .......... .......... .......... 38% 8.57M 28s
192250K .......... .......... .......... .......... .......... 38% 7.13M 28s
192300K .......... .......... .......... .......... .......... 38% 6.75M 28s
192350K .......... .......... .......... .......... .......... 38% 6.10M 28s
192400K .......... .......... .......... .......... .......... 38% 7.43M 28s
192450K .......... .......... .......... .......... .......... 38% 6.41M 28s
192500K .......... .......... .......... .......... .......... 38% 12.2M 28s
192550K .......... .......... .......... .......... .......... 38% 16.3M 28s
192600K .......... .......... .......... .......... .......... 38% 13.4M 28s
192650K .......... .......... .......... .......... .......... 38% 18.0M 28s
192700K .......... .......... .......... .......... .......... 38% 10.7M 28s
192750K .......... .......... .......... .......... .......... 38% 12.5M 28s
192800K .......... .......... .......... .......... .......... 38% 10.2M 28s
192850K .......... .......... .......... .......... .......... 38% 9.02M 28s
192900K .......... .......... .......... .......... .......... 38% 9.01M 28s
192950K .......... .......... .......... .......... .......... 38% 8.19M 28s
193000K .......... .......... .......... .......... .......... 38% 7.12M 28s
193050K .......... .......... .......... .......... .......... 38% 7.16M 28s
193100K .......... .......... .......... .......... .......... 38% 6.18M 28s
193150K .......... .......... .......... .......... .......... 38% 7.25M 28s
193200K .......... .......... .......... .......... .......... 38% 4.20M 28s
193250K .......... .......... .......... .......... .......... 38% 5.75M 28s
193300K .......... .......... .......... .......... .......... 38% 7.60M 28s
193350K .......... .......... .......... .......... .......... 38% 9.87M 28s
193400K .......... .......... .......... .......... .......... 38% 12.5M 28s
193450K .......... .......... .......... .......... .......... 38% 8.56M 28s
193500K .......... .......... .......... .......... .......... 38% 12.2M 28s
193550K .......... .......... .......... .......... .......... 38% 8.00M 28s
193600K .......... .......... .......... .......... .......... 38% 10.2M 28s
193650K .......... .......... .......... .......... .......... 38% 10.5M 28s
193700K .......... .......... .......... .......... .......... 38% 10.3M 28s
193750K .......... .......... .......... .......... .......... 38% 10.8M 28s
193800K .......... .......... .......... .......... .......... 38% 11.4M 28s
193850K .......... .......... .......... .......... .......... 38% 9.39M 28s
193900K .......... .......... .......... .......... .......... 38% 11.8M 28s
193950K .......... .......... .......... .......... .......... 38% 12.1M 28s
194000K .......... .......... .......... .......... .......... 38% 14.4M 28s
194050K .......... .......... .......... .......... .......... 38% 13.5M 28s
194100K .......... .......... .......... .......... .......... 38% 15.7M 28s
194150K .......... .......... .......... .......... .......... 38% 11.0M 28s
194200K .......... .......... .......... .......... .......... 38% 11.7M 28s
194250K .......... .......... .......... .......... .......... 38% 12.3M 28s
194300K .......... .......... .......... .......... .......... 38% 13.3M 28s
194350K .......... .......... .......... .......... .......... 38% 10.8M 28s
194400K .......... .......... .......... .......... .......... 38% 15.9M 28s
194450K .......... .......... .......... .......... .......... 38% 11.1M 28s
194500K .......... .......... .......... .......... .......... 38% 12.1M 28s
194550K .......... .......... .......... .......... .......... 38% 10.9M 28s
194600K .......... .......... .......... .......... .......... 38% 7.55M 28s
194650K .......... .......... .......... .......... .......... 38% 7.86M 28s
194700K .......... .......... .......... .......... .......... 38% 9.42M 28s
194750K .......... .......... .......... .......... .......... 38% 10.5M 28s
194800K .......... .......... .......... .......... .......... 38% 9.21M 28s
194850K .......... .......... .......... .......... .......... 38% 9.70M 28s
194900K .......... .......... .......... .......... .......... 38% 11.8M 28s
194950K .......... .......... .......... .......... .......... 38% 11.1M 28s
195000K .......... .......... .......... .......... .......... 38% 10.8M 28s
195050K .......... .......... .......... .......... .......... 38% 12.2M 28s
195100K .......... .......... .......... .......... .......... 38% 11.8M 28s
195150K .......... .......... .......... .......... .......... 38% 12.6M 28s
195200K .......... .......... .......... .......... .......... 38% 9.70M 28s
195250K .......... .......... .......... .......... .......... 38% 12.5M 28s
195300K .......... .......... .......... .......... .......... 38% 34.0M 28s
195350K .......... .......... .......... .......... .......... 38% 9.67M 28s
195400K .......... .......... .......... .......... .......... 38% 8.67M 28s
195450K .......... .......... .......... .......... .......... 38% 6.29M 28s
195500K .......... .......... .......... .......... .......... 38% 8.79M 28s
195550K .......... .......... .......... .......... .......... 38% 6.65M 28s
195600K .......... .......... .......... .......... .......... 38% 5.87M 28s
195650K .......... .......... .......... .......... .......... 38% 12.6M 28s
195700K .......... .......... .......... .......... .......... 38% 8.98M 28s
195750K .......... .......... .......... .......... .......... 38% 10.8M 28s
195800K .......... .......... .......... .......... .......... 38% 9.43M 28s
195850K .......... .......... .......... .......... .......... 38% 8.98M 28s
195900K .......... .......... .......... .......... .......... 38% 8.04M 28s
195950K .......... .......... .......... .......... .......... 38% 11.5M 28s
196000K .......... .......... .......... .......... .......... 38% 8.68M 28s
196050K .......... .......... .......... .......... .......... 38% 10.7M 28s
196100K .......... .......... .......... .......... .......... 38% 8.53M 28s
196150K .......... .......... .......... .......... .......... 38% 11.8M 28s
196200K .......... .......... .......... .......... .......... 38% 8.28M 28s
196250K .......... .......... .......... .......... .......... 38% 9.65M 28s
196300K .......... .......... .......... .......... .......... 38% 10.3M 28s
196350K .......... .......... .......... .......... .......... 38% 9.45M 28s
196400K .......... .......... .......... .......... .......... 38% 5.63M 28s
196450K .......... .......... .......... .......... .......... 38% 3.78M 28s
196500K .......... .......... .......... .......... .......... 38% 6.07M 28s
196550K .......... .......... .......... .......... .......... 38% 8.07M 28s
196600K .......... .......... .......... .......... .......... 38% 9.18M 28s
196650K .......... .......... .......... .......... .......... 38% 7.88M 28s
196700K .......... .......... .......... .......... .......... 38% 7.27M 28s
196750K .......... .......... .......... .......... .......... 38% 8.77M 28s
196800K .......... .......... .......... .......... .......... 39% 10.6M 28s
196850K .......... .......... .......... .......... .......... 39% 8.16M 28s
196900K .......... .......... .......... .......... .......... 39% 7.19M 28s
196950K .......... .......... .......... .......... .......... 39% 5.90M 28s
197000K .......... .......... .......... .......... .......... 39% 4.97M 28s
197050K .......... .......... .......... .......... .......... 39% 6.73M 28s
197100K .......... .......... .......... .......... .......... 39% 7.40M 28s
197150K .......... .......... .......... .......... .......... 39% 6.97M 28s
197200K .......... .......... .......... .......... .......... 39% 3.98M 28s
197250K .......... .......... .......... .......... .......... 39% 3.91M 28s
197300K .......... .......... .......... .......... .......... 39% 3.50M 28s
197350K .......... .......... .......... .......... .......... 39% 8.90M 28s
197400K .......... .......... .......... .......... .......... 39% 25.5M 28s
197450K .......... .......... .......... .......... .......... 39% 31.6M 28s
197500K .......... .......... .......... .......... .......... 39% 23.0M 28s
197550K .......... .......... .......... .......... .......... 39% 49.0M 28s
197600K .......... .......... .......... .......... .......... 39% 20.0M 28s
197650K .......... .......... .......... .......... .......... 39% 74.7M 28s
197700K .......... .......... .......... .......... .......... 39% 21.1M 28s
197750K .......... .......... .......... .......... .......... 39% 15.5M 28s
197800K .......... .......... .......... .......... .......... 39% 18.7M 28s
197850K .......... .......... .......... .......... .......... 39% 11.4M 28s
197900K .......... .......... .......... .......... .......... 39% 11.4M 28s
197950K .......... .......... .......... .......... .......... 39% 9.40M 28s
198000K .......... .......... .......... .......... .......... 39% 10.5M 28s
198050K .......... .......... .......... .......... .......... 39% 8.81M 28s
198100K .......... .......... .......... .......... .......... 39% 9.48M 28s
198150K .......... .......... .......... .......... .......... 39% 7.89M 28s
198200K .......... .......... .......... .......... .......... 39% 9.15M 28s
198250K .......... .......... .......... .......... .......... 39% 11.8M 28s
198300K .......... .......... .......... .......... .......... 39% 14.4M 28s
198350K .......... .......... .......... .......... .......... 39% 15.5M 28s
198400K .......... .......... .......... .......... .......... 39% 18.2M 28s
198450K .......... .......... .......... .......... .......... 39% 13.8M 28s
198500K .......... .......... .......... .......... .......... 39% 15.8M 28s
198550K .......... .......... .......... .......... .......... 39% 11.9M 28s
198600K .......... .......... .......... .......... .......... 39% 10.1M 28s
198650K .......... .......... .......... .......... .......... 39% 11.4M 28s
198700K .......... .......... .......... .......... .......... 39% 6.75M 28s
198750K .......... .......... .......... .......... .......... 39% 14.0M 28s
198800K .......... .......... .......... .......... .......... 39% 9.15M 28s
198850K .......... .......... .......... .......... .......... 39% 5.41M 28s
198900K .......... .......... .......... .......... .......... 39% 6.19M 28s
198950K .......... .......... .......... .......... .......... 39% 5.06M 28s
199000K .......... .......... .......... .......... .......... 39% 4.41M 28s
199050K .......... .......... .......... .......... .......... 39% 14.7M 28s
199100K .......... .......... .......... .......... .......... 39% 9.60M 28s
199150K .......... .......... .......... .......... .......... 39% 12.5M 28s
199200K .......... .......... .......... .......... .......... 39% 7.44M 28s
199250K .......... .......... .......... .......... .......... 39% 10.5M 28s
199300K .......... .......... .......... .......... .......... 39% 9.20M 28s
199350K .......... .......... .......... .......... .......... 39% 7.65M 28s
199400K .......... .......... .......... .......... .......... 39% 6.81M 28s
199450K .......... .......... .......... .......... .......... 39% 8.91M 28s
199500K .......... .......... .......... .......... .......... 39% 8.80M 28s
199550K .......... .......... .......... .......... .......... 39% 7.70M 28s
199600K .......... .......... .......... .......... .......... 39% 9.40M 28s
199650K .......... .......... .......... .......... .......... 39% 11.7M 28s
199700K .......... .......... .......... .......... .......... 39% 9.89M 28s
199750K .......... .......... .......... .......... .......... 39% 10.8M 28s
199800K .......... .......... .......... .......... .......... 39% 11.4M 28s
199850K .......... .......... .......... .......... .......... 39% 7.24M 28s
199900K .......... .......... .......... .......... .......... 39% 8.28M 28s
199950K .......... .......... .......... .......... .......... 39% 6.36M 28s
200000K .......... .......... .......... .......... .......... 39% 7.99M 28s
200050K .......... .......... .......... .......... .......... 39% 10.4M 28s
200100K .......... .......... .......... .......... .......... 39% 8.00M 28s
200150K .......... .......... .......... .......... .......... 39% 9.40M 28s
200200K .......... .......... .......... .......... .......... 39% 6.00M 28s
200250K .......... .......... .......... .......... .......... 39% 8.61M 28s
200300K .......... .......... .......... .......... .......... 39% 6.08M 28s
200350K .......... .......... .......... .......... .......... 39% 5.64M 28s
200400K .......... .......... .......... .......... .......... 39% 7.57M 28s
200450K .......... .......... .......... .......... .......... 39% 7.58M 28s
200500K .......... .......... .......... .......... .......... 39% 6.97M 28s
200550K .......... .......... .......... .......... .......... 39% 7.80M 28s
200600K .......... .......... .......... .......... .......... 39% 5.38M 28s
200650K .......... .......... .......... .......... .......... 39% 3.34M 28s
200700K .......... .......... .......... .......... .......... 39% 2.65M 28s
200750K .......... .......... .......... .......... .......... 39% 3.53M 28s
200800K .......... .......... .......... .......... .......... 39% 14.3M 28s
200850K .......... .......... .......... .......... .......... 39% 16.5M 28s
200900K .......... .......... .......... .......... .......... 39% 19.6M 28s
200950K .......... .......... .......... .......... .......... 39% 12.9M 28s
201000K .......... .......... .......... .......... .......... 39% 11.6M 28s
201050K .......... .......... .......... .......... .......... 39% 9.31M 28s
201100K .......... .......... .......... .......... .......... 39% 8.10M 28s
201150K .......... .......... .......... .......... .......... 39% 9.34M 28s
201200K .......... .......... .......... .......... .......... 39% 8.24M 28s
201250K .......... .......... .......... .......... .......... 39% 14.5M 28s
201300K .......... .......... .......... .......... .......... 39% 10.0M 28s
201350K .......... .......... .......... .......... .......... 39% 9.25M 28s
201400K .......... .......... .......... .......... .......... 39% 10.9M 28s
201450K .......... .......... .......... .......... .......... 39% 9.63M 28s
201500K .......... .......... .......... .......... .......... 39% 10.7M 28s
201550K .......... .......... .......... .......... .......... 39% 11.6M 28s
201600K .......... .......... .......... .......... .......... 39% 8.71M 28s
201650K .......... .......... .......... .......... .......... 39% 7.71M 28s
201700K .......... .......... .......... .......... .......... 39% 6.48M 28s
201750K .......... .......... .......... .......... .......... 39% 6.74M 28s
201800K .......... .......... .......... .......... .......... 39% 6.53M 28s
201850K .......... .......... .......... .......... .......... 40% 4.46M 28s
201900K .......... .......... .......... .......... .......... 40% 7.38M 28s
201950K .......... .......... .......... .......... .......... 40% 13.1M 28s
202000K .......... .......... .......... .......... .......... 40% 45.3M 28s
202050K .......... .......... .......... .......... .......... 40% 22.2M 28s
202100K .......... .......... .......... .......... .......... 40% 18.5M 28s
202150K .......... .......... .......... .......... .......... 40% 19.1M 28s
202200K .......... .......... .......... .......... .......... 40% 10.9M 28s
202250K .......... .......... .......... .......... .......... 40% 12.1M 28s
202300K .......... .......... .......... .......... .......... 40% 10.5M 28s
202350K .......... .......... .......... .......... .......... 40% 8.58M 28s
202400K .......... .......... .......... .......... .......... 40% 11.8M 28s
202450K .......... .......... .......... .......... .......... 40% 8.15M 28s
202500K .......... .......... .......... .......... .......... 40% 8.31M 28s
202550K .......... .......... .......... .......... .......... 40% 6.19M 28s
202600K .......... .......... .......... .......... .......... 40% 4.49M 28s
202650K .......... .......... .......... .......... .......... 40% 5.51M 28s
202700K .......... .......... .......... .......... .......... 40% 7.37M 28s
202750K .......... .......... .......... .......... .......... 40% 6.09M 28s
202800K .......... .......... .......... .......... .......... 40% 6.28M 28s
202850K .......... .......... .......... .......... .......... 40% 5.48M 28s
202900K .......... .......... .......... .......... .......... 40% 6.46M 28s
202950K .......... .......... .......... .......... .......... 40% 5.12M 28s
203000K .......... .......... .......... .......... .......... 40% 5.62M 28s
203050K .......... .......... .......... .......... .......... 40% 13.8M 28s
203100K .......... .......... .......... .......... .......... 40% 24.2M 28s
203150K .......... .......... .......... .......... .......... 40% 18.0M 28s
203200K .......... .......... .......... .......... .......... 40% 8.49M 28s
203250K .......... .......... .......... .......... .......... 40% 9.66M 28s
203300K .......... .......... .......... .......... .......... 40% 8.36M 28s
203350K .......... .......... .......... .......... .......... 40% 7.83M 28s
203400K .......... .......... .......... .......... .......... 40% 7.26M 28s
203450K .......... .......... .......... .......... .......... 40% 6.75M 28s
203500K .......... .......... .......... .......... .......... 40% 8.56M 28s
203550K .......... .......... .......... .......... .......... 40% 6.87M 28s
203600K .......... .......... .......... .......... .......... 40% 7.40M 28s
203650K .......... .......... .......... .......... .......... 40% 7.71M 28s
203700K .......... .......... .......... .......... .......... 40% 8.18M 28s
203750K .......... .......... .......... .......... .......... 40% 14.5M 28s
203800K .......... .......... .......... .......... .......... 40% 24.6M 28s
203850K .......... .......... .......... .......... .......... 40% 24.6M 28s
203900K .......... .......... .......... .......... .......... 40% 33.1M 28s
203950K .......... .......... .......... .......... .......... 40% 24.6M 28s
204000K .......... .......... .......... .......... .......... 40% 15.8M 28s
204050K .......... .......... .......... .......... .......... 40% 34.4M 28s
204100K .......... .......... .......... .......... .......... 40% 15.0M 28s
204150K .......... .......... .......... .......... .......... 40% 16.9M 28s
204200K .......... .......... .......... .......... .......... 40% 18.6M 28s
204250K .......... .......... .......... .......... .......... 40% 19.6M 28s
204300K .......... .......... .......... .......... .......... 40% 17.8M 28s
204350K .......... .......... .......... .......... .......... 40% 15.5M 28s
204400K .......... .......... .......... .......... .......... 40% 13.9M 28s
204450K .......... .......... .......... .......... .......... 40% 5.74M 28s
204500K .......... .......... .......... .......... .......... 40% 6.73M 28s
204550K .......... .......... .......... .......... .......... 40% 6.54M 28s
204600K .......... .......... .......... .......... .......... 40% 4.65M 28s
204650K .......... .......... .......... .......... .......... 40% 9.31M 28s
204700K .......... .......... .......... .......... .......... 40% 9.91M 28s
204750K .......... .......... .......... .......... .......... 40% 6.87M 28s
204800K .......... .......... .......... .......... .......... 40% 7.27M 28s
204850K .......... .......... .......... .......... .......... 40% 4.82M 28s
204900K .......... .......... .......... .......... .......... 40% 4.03M 28s
204950K .......... .......... .......... .......... .......... 40% 3.18M 28s
205000K .......... .......... .......... .......... .......... 40% 3.87M 28s
205050K .......... .......... .......... .......... .......... 40% 3.43M 28s
205100K .......... .......... .......... .......... .......... 40% 3.07M 28s
205150K .......... .......... .......... .......... .......... 40% 10.2M 28s
205200K .......... .......... .......... .......... .......... 40% 18.0M 28s
205250K .......... .......... .......... .......... .......... 40% 18.6M 28s
205300K .......... .......... .......... .......... .......... 40% 16.6M 28s
205350K .......... .......... .......... .......... .......... 40% 14.3M 28s
205400K .......... .......... .......... .......... .......... 40% 13.4M 28s
205450K .......... .......... .......... .......... .......... 40% 12.1M 28s
205500K .......... .......... .......... .......... .......... 40% 13.0M 28s
205550K .......... .......... .......... .......... .......... 40% 9.69M 28s
205600K .......... .......... .......... .......... .......... 40% 8.59M 28s
205650K .......... .......... .......... .......... .......... 40% 8.26M 28s
205700K .......... .......... .......... .......... .......... 40% 6.76M 28s
205750K .......... .......... .......... .......... .......... 40% 11.7M 28s
205800K .......... .......... .......... .......... .......... 40% 11.0M 28s
205850K .......... .......... .......... .......... .......... 40% 9.20M 28s
205900K .......... .......... .......... .......... .......... 40% 10.4M 28s
205950K .......... .......... .......... .......... .......... 40% 13.0M 28s
206000K .......... .......... .......... .......... .......... 40% 14.9M 28s
206050K .......... .......... .......... .......... .......... 40% 11.0M 28s
206100K .......... .......... .......... .......... .......... 40% 6.18M 28s
206150K .......... .......... .......... .......... .......... 40% 6.00M 28s
206200K .......... .......... .......... .......... .......... 40% 4.41M 28s
206250K .......... .......... .......... .......... .......... 40% 4.79M 28s
206300K .......... .......... .......... .......... .......... 40% 2.91M 28s
206350K .......... .......... .......... .......... .......... 40% 2.86M 28s
206400K .......... .......... .......... .......... .......... 40% 13.9M 28s
206450K .......... .......... .......... .......... .......... 40% 13.9M 28s
206500K .......... .......... .......... .......... .......... 40% 73.6M 28s
206550K .......... .......... .......... .......... .......... 40% 20.6M 28s
206600K .......... .......... .......... .......... .......... 40% 21.9M 28s
206650K .......... .......... .......... .......... .......... 40% 12.2M 28s
206700K .......... .......... .......... .......... .......... 40% 25.0M 28s
206750K .......... .......... .......... .......... .......... 40% 16.3M 28s
206800K .......... .......... .......... .......... .......... 40% 15.0M 28s
206850K .......... .......... .......... .......... .......... 40% 16.3M 27s
206900K .......... .......... .......... .......... .......... 41% 18.7M 27s
206950K .......... .......... .......... .......... .......... 41% 11.4M 27s
207000K .......... .......... .......... .......... .......... 41% 17.8M 27s
207050K .......... .......... .......... .......... .......... 41% 16.3M 27s
207100K .......... .......... .......... .......... .......... 41% 12.7M 27s
207150K .......... .......... .......... .......... .......... 41% 15.4M 27s
207200K .......... .......... .......... .......... .......... 41% 12.1M 27s
207250K .......... .......... .......... .......... .......... 41% 11.5M 27s
207300K .......... .......... .......... .......... .......... 41% 14.4M 27s
207350K .......... .......... .......... .......... .......... 41% 11.0M 27s
207400K .......... .......... .......... .......... .......... 41% 13.5M 27s
207450K .......... .......... .......... .......... .......... 41% 10.2M 27s
207500K .......... .......... .......... .......... .......... 41% 10.2M 27s
207550K .......... .......... .......... .......... .......... 41% 11.2M 27s
207600K .......... .......... .......... .......... .......... 41% 9.91M 27s
207650K .......... .......... .......... .......... .......... 41% 10.8M 27s
207700K .......... .......... .......... .......... .......... 41% 8.62M 27s
207750K .......... .......... .......... .......... .......... 41% 13.1M 27s
207800K .......... .......... .......... .......... .......... 41% 21.5M 27s
207850K .......... .......... .......... .......... .......... 41% 12.6M 27s
207900K .......... .......... .......... .......... .......... 41% 6.97M 27s
207950K .......... .......... .......... .......... .......... 41% 11.7M 27s
208000K .......... .......... .......... .......... .......... 41% 10.8M 27s
208050K .......... .......... .......... .......... .......... 41% 9.97M 27s
208100K .......... .......... .......... .......... .......... 41% 8.08M 27s
208150K .......... .......... .......... .......... .......... 41% 8.10M 27s
208200K .......... .......... .......... .......... .......... 41% 6.29M 27s
208250K .......... .......... .......... .......... .......... 41% 9.24M 27s
208300K .......... .......... .......... .......... .......... 41% 10.8M 27s
208350K .......... .......... .......... .......... .......... 41% 13.5M 27s
208400K .......... .......... .......... .......... .......... 41% 12.4M 27s
208450K .......... .......... .......... .......... .......... 41% 15.1M 27s
208500K .......... .......... .......... .......... .......... 41% 17.1M 27s
208550K .......... .......... .......... .......... .......... 41% 20.0M 27s
208600K .......... .......... .......... .......... .......... 41% 13.4M 27s
208650K .......... .......... .......... .......... .......... 41% 13.3M 27s
208700K .......... .......... .......... .......... .......... 41% 9.75M 27s
208750K .......... .......... .......... .......... .......... 41% 8.78M 27s
208800K .......... .......... .......... .......... .......... 41% 9.00M 27s
208850K .......... .......... .......... .......... .......... 41% 7.74M 27s
208900K .......... .......... .......... .......... .......... 41% 7.94M 27s
208950K .......... .......... .......... .......... .......... 41% 7.44M 27s
209000K .......... .......... .......... .......... .......... 41% 9.93M 27s
209050K .......... .......... .......... .......... .......... 41% 11.1M 27s
209100K .......... .......... .......... .......... .......... 41% 9.42M 27s
209150K .......... .......... .......... .......... .......... 41% 12.1M 27s
209200K .......... .......... .......... .......... .......... 41% 8.38M 27s
209250K .......... .......... .......... .......... .......... 41% 8.53M 27s
209300K .......... .......... .......... .......... .......... 41% 9.89M 27s
209350K .......... .......... .......... .......... .......... 41% 9.68M 27s
209400K .......... .......... .......... .......... .......... 41% 10.8M 27s
209450K .......... .......... .......... .......... .......... 41% 10.5M 27s
209500K .......... .......... .......... .......... .......... 41% 11.1M 27s
209550K .......... .......... .......... .......... .......... 41% 10.1M 27s
209600K .......... .......... .......... .......... .......... 41% 8.59M 27s
209650K .......... .......... .......... .......... .......... 41% 9.15M 27s
209700K .......... .......... .......... .......... .......... 41% 7.84M 27s
209750K .......... .......... .......... .......... .......... 41% 9.92M 27s
209800K .......... .......... .......... .......... .......... 41% 9.89M 27s
209850K .......... .......... .......... .......... .......... 41% 9.45M 27s
209900K .......... .......... .......... .......... .......... 41% 9.64M 27s
209950K .......... .......... .......... .......... .......... 41% 7.87M 27s
210000K .......... .......... .......... .......... .......... 41% 10.7M 27s
210050K .......... .......... .......... .......... .......... 41% 8.56M 27s
210100K .......... .......... .......... .......... .......... 41% 8.37M 27s
210150K .......... .......... .......... .......... .......... 41% 9.25M 27s
210200K .......... .......... .......... .......... .......... 41% 6.31M 27s
210250K .......... .......... .......... .......... .......... 41% 6.12M 27s
210300K .......... .......... .......... .......... .......... 41% 5.34M 27s
210350K .......... .......... .......... .......... .......... 41% 9.62M 27s
210400K .......... .......... .......... .......... .......... 41% 9.22M 27s
210450K .......... .......... .......... .......... .......... 41% 11.7M 27s
210500K .......... .......... .......... .......... .......... 41% 11.1M 27s
210550K .......... .......... .......... .......... .......... 41% 15.3M 27s
210600K .......... .......... .......... .......... .......... 41% 8.62M 27s
210650K .......... .......... .......... .......... .......... 41% 8.36M 27s
210700K .......... .......... .......... .......... .......... 41% 5.29M 27s
210750K .......... .......... .......... .......... .......... 41% 4.58M 27s
210800K .......... .......... .......... .......... .......... 41% 5.33M 27s
210850K .......... .......... .......... .......... .......... 41% 4.15M 27s
210900K .......... .......... .......... .......... .......... 41% 11.1M 27s
210950K .......... .......... .......... .......... .......... 41% 8.37M 27s
211000K .......... .......... .......... .......... .......... 41% 7.40M 27s
211050K .......... .......... .......... .......... .......... 41% 5.92M 27s
211100K .......... .......... .......... .......... .......... 41% 5.28M 27s
211150K .......... .......... .......... .......... .......... 41% 5.23M 27s
211200K .......... .......... .......... .......... .......... 41% 4.27M 27s
211250K .......... .......... .......... .......... .......... 41% 5.51M 27s
211300K .......... .......... .......... .......... .......... 41% 5.84M 27s
211350K .......... .......... .......... .......... .......... 41% 4.30M 27s
211400K .......... .......... .......... .......... .......... 41% 8.18M 27s
211450K .......... .......... .......... .......... .......... 41% 18.5M 27s
211500K .......... .......... .......... .......... .......... 41% 18.8M 27s
211550K .......... .......... .......... .......... .......... 41% 17.2M 27s
211600K .......... .......... .......... .......... .......... 41% 15.2M 27s
211650K .......... .......... .......... .......... .......... 41% 13.3M 27s
211700K .......... .......... .......... .......... .......... 41% 17.3M 27s
211750K .......... .......... .......... .......... .......... 41% 15.0M 27s
211800K .......... .......... .......... .......... .......... 41% 14.0M 27s
211850K .......... .......... .......... .......... .......... 41% 12.2M 27s
211900K .......... .......... .......... .......... .......... 41% 12.7M 27s
211950K .......... .......... .......... .......... .......... 42% 9.67M 27s
212000K .......... .......... .......... .......... .......... 42% 6.57M 27s
212050K .......... .......... .......... .......... .......... 42% 7.75M 27s
212100K .......... .......... .......... .......... .......... 42% 9.21M 27s
212150K .......... .......... .......... .......... .......... 42% 6.92M 27s
212200K .......... .......... .......... .......... .......... 42% 4.95M 27s
212250K .......... .......... .......... .......... .......... 42% 6.58M 27s
212300K .......... .......... .......... .......... .......... 42% 7.37M 27s
212350K .......... .......... .......... .......... .......... 42% 5.54M 27s
212400K .......... .......... .......... .......... .......... 42% 9.48M 27s
212450K .......... .......... .......... .......... .......... 42% 9.74M 27s
212500K .......... .......... .......... .......... .......... 42% 8.65M 27s
212550K .......... .......... .......... .......... .......... 42% 8.42M 27s
212600K .......... .......... .......... .......... .......... 42% 5.93M 27s
212650K .......... .......... .......... .......... .......... 42% 9.35M 27s
212700K .......... .......... .......... .......... .......... 42% 9.09M 27s
212750K .......... .......... .......... .......... .......... 42% 8.34M 27s
212800K .......... .......... .......... .......... .......... 42% 8.46M 27s
212850K .......... .......... .......... .......... .......... 42% 7.24M 27s
212900K .......... .......... .......... .......... .......... 42% 12.1M 27s
212950K .......... .......... .......... .......... .......... 42% 9.04M 27s
213000K .......... .......... .......... .......... .......... 42% 12.5M 27s
213050K .......... .......... .......... .......... .......... 42% 12.6M 27s
213100K .......... .......... .......... .......... .......... 42% 7.40M 27s
213150K .......... .......... .......... .......... .......... 42% 9.71M 27s
213200K .......... .......... .......... .......... .......... 42% 6.37M 27s
213250K .......... .......... .......... .......... .......... 42% 8.67M 27s
213300K .......... .......... .......... .......... .......... 42% 4.73M 27s
213350K .......... .......... .......... .......... .......... 42% 5.99M 27s
213400K .......... .......... .......... .......... .......... 42% 5.84M 27s
213450K .......... .......... .......... .......... .......... 42% 5.49M 27s
213500K .......... .......... .......... .......... .......... 42% 6.89M 27s
213550K .......... .......... .......... .......... .......... 42% 19.7M 27s
213600K .......... .......... .......... .......... .......... 42% 17.8M 27s
213650K .......... .......... .......... .......... .......... 42% 21.0M 27s
213700K .......... .......... .......... .......... .......... 42% 26.8M 27s
213750K .......... .......... .......... .......... .......... 42% 17.9M 27s
213800K .......... .......... .......... .......... .......... 42% 11.3M 27s
213850K .......... .......... .......... .......... .......... 42% 9.87M 27s
213900K .......... .......... .......... .......... .......... 42% 9.14M 27s
213950K .......... .......... .......... .......... .......... 42% 6.50M 27s
214000K .......... .......... .......... .......... .......... 42% 7.12M 27s
214050K .......... .......... .......... .......... .......... 42% 7.31M 27s
214100K .......... .......... .......... .......... .......... 42% 6.22M 27s
214150K .......... .......... .......... .......... .......... 42% 9.48M 27s
214200K .......... .......... .......... .......... .......... 42% 8.08M 27s
214250K .......... .......... .......... .......... .......... 42% 10.2M 27s
214300K .......... .......... .......... .......... .......... 42% 7.40M 27s
214350K .......... .......... .......... .......... .......... 42% 5.51M 27s
214400K .......... .......... .......... .......... .......... 42% 6.36M 27s
214450K .......... .......... .......... .......... .......... 42% 5.14M 27s
214500K .......... .......... .......... .......... .......... 42% 22.3M 27s
214550K .......... .......... .......... .......... .......... 42% 26.4M 27s
214600K .......... .......... .......... .......... .......... 42% 18.7M 27s
214650K .......... .......... .......... .......... .......... 42% 78.9M 27s
214700K .......... .......... .......... .......... .......... 42% 20.6M 27s
214750K .......... .......... .......... .......... .......... 42% 31.0M 27s
214800K .......... .......... .......... .......... .......... 42% 20.7M 27s
214850K .......... .......... .......... .......... .......... 42% 23.6M 27s
214900K .......... .......... .......... .......... .......... 42% 19.8M 27s
214950K .......... .......... .......... .......... .......... 42% 19.5M 27s
215000K .......... .......... .......... .......... .......... 42% 18.0M 27s
215050K .......... .......... .......... .......... .......... 42% 23.6M 27s
215100K .......... .......... .......... .......... .......... 42% 15.6M 27s
215150K .......... .......... .......... .......... .......... 42% 20.4M 27s
215200K .......... .......... .......... .......... .......... 42% 13.5M 27s
215250K .......... .......... .......... .......... .......... 42% 16.4M 27s
215300K .......... .......... .......... .......... .......... 42% 16.2M 27s
215350K .......... .......... .......... .......... .......... 42% 15.0M 27s
215400K .......... .......... .......... .......... .......... 42% 16.2M 27s
215450K .......... .......... .......... .......... .......... 42% 11.5M 27s
215500K .......... .......... .......... .......... .......... 42% 15.9M 27s
215550K .......... .......... .......... .......... .......... 42% 10.9M 27s
215600K .......... .......... .......... .......... .......... 42% 12.1M 27s
215650K .......... .......... .......... .......... .......... 42% 17.9M 27s
215700K .......... .......... .......... .......... .......... 42% 11.0M 27s
215750K .......... .......... .......... .......... .......... 42% 13.0M 27s
215800K .......... .......... .......... .......... .......... 42% 16.3M 27s
215850K .......... .......... .......... .......... .......... 42% 9.90M 27s
215900K .......... .......... .......... .......... .......... 42% 13.8M 27s
215950K .......... .......... .......... .......... .......... 42% 7.19M 27s
216000K .......... .......... .......... .......... .......... 42% 13.6M 27s
216050K .......... .......... .......... .......... .......... 42% 8.96M 27s
216100K .......... .......... .......... .......... .......... 42% 6.84M 27s
216150K .......... .......... .......... .......... .......... 42% 9.46M 27s
216200K .......... .......... .......... .......... .......... 42% 9.43M 27s
216250K .......... .......... .......... .......... .......... 42% 7.57M 27s
216300K .......... .......... .......... .......... .......... 42% 7.26M 27s
216350K .......... .......... .......... .......... .......... 42% 10.7M 27s
216400K .......... .......... .......... .......... .......... 42% 11.0M 27s
216450K .......... .......... .......... .......... .......... 42% 10.1M 27s
216500K .......... .......... .......... .......... .......... 42% 10.5M 27s
216550K .......... .......... .......... .......... .......... 42% 13.0M 27s
216600K .......... .......... .......... .......... .......... 42% 6.32M 27s
216650K .......... .......... .......... .......... .......... 42% 5.85M 27s
216700K .......... .......... .......... .......... .......... 42% 9.67M 27s
216750K .......... .......... .......... .......... .......... 42% 9.95M 27s
216800K .......... .......... .......... .......... .......... 42% 14.4M 27s
216850K .......... .......... .......... .......... .......... 42% 15.1M 27s
216900K .......... .......... .......... .......... .......... 42% 14.5M 27s
216950K .......... .......... .......... .......... .......... 42% 18.5M 27s
217000K .......... .......... .......... .......... .......... 43% 11.2M 27s
217050K .......... .......... .......... .......... .......... 43% 12.0M 27s
217100K .......... .......... .......... .......... .......... 43% 8.21M 27s
217150K .......... .......... .......... .......... .......... 43% 6.31M 27s
217200K .......... .......... .......... .......... .......... 43% 5.45M 27s
217250K .......... .......... .......... .......... .......... 43% 8.93M 27s
217300K .......... .......... .......... .......... .......... 43% 8.81M 27s
217350K .......... .......... .......... .......... .......... 43% 6.87M 27s
217400K .......... .......... .......... .......... .......... 43% 9.43M 27s
217450K .......... .......... .......... .......... .......... 43% 7.26M 27s
217500K .......... .......... .......... .......... .......... 43% 12.5M 27s
217550K .......... .......... .......... .......... .......... 43% 26.2M 27s
217600K .......... .......... .......... .......... .......... 43% 17.5M 27s
217650K .......... .......... .......... .......... .......... 43% 79.5M 27s
217700K .......... .......... .......... .......... .......... 43% 26.5M 27s
217750K .......... .......... .......... .......... .......... 43% 21.2M 27s
217800K .......... .......... .......... .......... .......... 43% 26.3M 27s
217850K .......... .......... .......... .......... .......... 43% 19.8M 27s
217900K .......... .......... .......... .......... .......... 43% 24.8M 27s
217950K .......... .......... .......... .......... .......... 43% 12.9M 27s
218000K .......... .......... .......... .......... .......... 43% 12.6M 27s
218050K .......... .......... .......... .......... .......... 43% 16.3M 27s
218100K .......... .......... .......... .......... .......... 43% 8.55M 27s
218150K .......... .......... .......... .......... .......... 43% 8.14M 27s
218200K .......... .......... .......... .......... .......... 43% 7.59M 27s
218250K .......... .......... .......... .......... .......... 43% 7.57M 27s
218300K .......... .......... .......... .......... .......... 43% 6.46M 27s
218350K .......... .......... .......... .......... .......... 43% 6.76M 27s
218400K .......... .......... .......... .......... .......... 43% 6.21M 27s
218450K .......... .......... .......... .......... .......... 43% 7.12M 27s
218500K .......... .......... .......... .......... .......... 43% 10.7M 27s
218550K .......... .......... .......... .......... .......... 43% 9.19M 27s
218600K .......... .......... .......... .......... .......... 43% 6.98M 27s
218650K .......... .......... .......... .......... .......... 43% 12.5M 27s
218700K .......... .......... .......... .......... .......... 43% 9.21M 27s
218750K .......... .......... .......... .......... .......... 43% 8.27M 27s
218800K .......... .......... .......... .......... .......... 43% 10.4M 27s
218850K .......... .......... .......... .......... .......... 43% 5.83M 27s
218900K .......... .......... .......... .......... .......... 43% 6.02M 27s
218950K .......... .......... .......... .......... .......... 43% 5.77M 27s
219000K .......... .......... .......... .......... .......... 43% 6.43M 27s
219050K .......... .......... .......... .......... .......... 43% 6.41M 27s
219100K .......... .......... .......... .......... .......... 43% 10.0M 27s
219150K .......... .......... .......... .......... .......... 43% 17.8M 27s
219200K .......... .......... .......... .......... .......... 43% 15.4M 27s
219250K .......... .......... .......... .......... .......... 43% 13.5M 27s
219300K .......... .......... .......... .......... .......... 43% 14.4M 27s
219350K .......... .......... .......... .......... .......... 43% 7.41M 27s
219400K .......... .......... .......... .......... .......... 43% 8.98M 27s
219450K .......... .......... .......... .......... .......... 43% 7.28M 27s
219500K .......... .......... .......... .......... .......... 43% 6.64M 27s
219550K .......... .......... .......... .......... .......... 43% 7.23M 27s
219600K .......... .......... .......... .......... .......... 43% 4.64M 27s
219650K .......... .......... .......... .......... .......... 43% 7.56M 27s
219700K .......... .......... .......... .......... .......... 43% 6.53M 27s
219750K .......... .......... .......... .......... .......... 43% 7.12M 26s
219800K .......... .......... .......... .......... .......... 43% 7.72M 26s
219850K .......... .......... .......... .......... .......... 43% 6.19M 26s
219900K .......... .......... .......... .......... .......... 43% 7.27M 26s
219950K .......... .......... .......... .......... .......... 43% 5.56M 26s
220000K .......... .......... .......... .......... .......... 43% 6.71M 26s
220050K .......... .......... .......... .......... .......... 43% 6.34M 26s
220100K .......... .......... .......... .......... .......... 43% 9.41M 26s
220150K .......... .......... .......... .......... .......... 43% 10.5M 26s
220200K .......... .......... .......... .......... .......... 43% 9.38M 26s
220250K .......... .......... .......... .......... .......... 43% 11.4M 26s
220300K .......... .......... .......... .......... .......... 43% 7.99M 26s
220350K .......... .......... .......... .......... .......... 43% 8.19M 26s
220400K .......... .......... .......... .......... .......... 43% 7.40M 26s
220450K .......... .......... .......... .......... .......... 43% 7.24M 26s
220500K .......... .......... .......... .......... .......... 43% 5.27M 26s
220550K .......... .......... .......... .......... .......... 43% 5.52M 26s
220600K .......... .......... .......... .......... .......... 43% 7.58M 26s
220650K .......... .......... .......... .......... .......... 43% 21.4M 26s
220700K .......... .......... .......... .......... .......... 43% 22.0M 26s
220750K .......... .......... .......... .......... .......... 43% 11.5M 26s
220800K .......... .......... .......... .......... .......... 43% 19.9M 26s
220850K .......... .......... .......... .......... .......... 43% 16.2M 26s
220900K .......... .......... .......... .......... .......... 43% 22.2M 26s
220950K .......... .......... .......... .......... .......... 43% 11.4M 26s
221000K .......... .......... .......... .......... .......... 43% 16.2M 26s
221050K .......... .......... .......... .......... .......... 43% 15.0M 26s
221100K .......... .......... .......... .......... .......... 43% 14.4M 26s
221150K .......... .......... .......... .......... .......... 43% 8.66M 26s
221200K .......... .......... .......... .......... .......... 43% 17.6M 26s
221250K .......... .......... .......... .......... .......... 43% 12.9M 26s
221300K .......... .......... .......... .......... .......... 43% 13.4M 26s
221350K .......... .......... .......... .......... .......... 43% 15.0M 26s
221400K .......... .......... .......... .......... .......... 43% 17.0M 26s
221450K .......... .......... .......... .......... .......... 43% 15.7M 26s
221500K .......... .......... .......... .......... .......... 43% 15.8M 26s
221550K .......... .......... .......... .......... .......... 43% 16.5M 26s
221600K .......... .......... .......... .......... .......... 43% 12.1M 26s
221650K .......... .......... .......... .......... .......... 43% 12.1M 26s
221700K .......... .......... .......... .......... .......... 43% 11.7M 26s
221750K .......... .......... .......... .......... .......... 43% 13.1M 26s
221800K .......... .......... .......... .......... .......... 43% 12.3M 26s
221850K .......... .......... .......... .......... .......... 43% 10.2M 26s
221900K .......... .......... .......... .......... .......... 43% 11.5M 26s
221950K .......... .......... .......... .......... .......... 43% 9.42M 26s
222000K .......... .......... .......... .......... .......... 43% 9.75M 26s
222050K .......... .......... .......... .......... .......... 44% 11.7M 26s
222100K .......... .......... .......... .......... .......... 44% 10.1M 26s
222150K .......... .......... .......... .......... .......... 44% 8.07M 26s
222200K .......... .......... .......... .......... .......... 44% 9.01M 26s
222250K .......... .......... .......... .......... .......... 44% 11.8M 26s
222300K .......... .......... .......... .......... .......... 44% 11.3M 26s
222350K .......... .......... .......... .......... .......... 44% 9.68M 26s
222400K .......... .......... .......... .......... .......... 44% 12.6M 26s
222450K .......... .......... .......... .......... .......... 44% 7.99M 26s
222500K .......... .......... .......... .......... .......... 44% 8.64M 26s
222550K .......... .......... .......... .......... .......... 44% 11.1M 26s
222600K .......... .......... .......... .......... .......... 44% 7.34M 26s
222650K .......... .......... .......... .......... .......... 44% 5.91M 26s
222700K .......... .......... .......... .......... .......... 44% 5.48M 26s
222750K .......... .......... .......... .......... .......... 44% 11.7M 26s
222800K .......... .......... .......... .......... .......... 44% 11.8M 26s
222850K .......... .......... .......... .......... .......... 44% 7.54M 26s
222900K .......... .......... .......... .......... .......... 44% 9.09M 26s
222950K .......... .......... .......... .......... .......... 44% 7.28M 26s
223000K .......... .......... .......... .......... .......... 44% 9.19M 26s
223050K .......... .......... .......... .......... .......... 44% 9.67M 26s
223100K .......... .......... .......... .......... .......... 44% 7.58M 26s
223150K .......... .......... .......... .......... .......... 44% 11.2M 26s
223200K .......... .......... .......... .......... .......... 44% 18.4M 26s
223250K .......... .......... .......... .......... .......... 44% 14.0M 26s
223300K .......... .......... .......... .......... .......... 44% 16.5M 26s
223350K .......... .......... .......... .......... .......... 44% 9.01M 26s
223400K .......... .......... .......... .......... .......... 44% 11.8M 26s
223450K .......... .......... .......... .......... .......... 44% 9.42M 26s
223500K .......... .......... .......... .......... .......... 44% 9.37M 26s
223550K .......... .......... .......... .......... .......... 44% 8.57M 26s
223600K .......... .......... .......... .......... .......... 44% 9.21M 26s
223650K .......... .......... .......... .......... .......... 44% 7.87M 26s
223700K .......... .......... .......... .......... .......... 44% 9.38M 26s
223750K .......... .......... .......... .......... .......... 44% 10.2M 26s
223800K .......... .......... .......... .......... .......... 44% 10.4M 26s
223850K .......... .......... .......... .......... .......... 44% 8.99M 26s
223900K .......... .......... .......... .......... .......... 44% 8.79M 26s
223950K .......... .......... .......... .......... .......... 44% 6.37M 26s
224000K .......... .......... .......... .......... .......... 44% 12.5M 26s
224050K .......... .......... .......... .......... .......... 44% 13.5M 26s
224100K .......... .......... .......... .......... .......... 44% 11.7M 26s
224150K .......... .......... .......... .......... .......... 44% 16.3M 26s
224200K .......... .......... .......... .......... .......... 44% 10.1M 26s
224250K .......... .......... .......... .......... .......... 44% 9.88M 26s
224300K .......... .......... .......... .......... .......... 44% 8.79M 26s
224350K .......... .......... .......... .......... .......... 44% 7.89M 26s
224400K .......... .......... .......... .......... .......... 44% 7.00M 26s
224450K .......... .......... .......... .......... .......... 44% 3.58M 26s
224500K .......... .......... .......... .......... .......... 44% 3.16M 26s
224550K .......... .......... .......... .......... .......... 44% 3.82M 26s
224600K .......... .......... .......... .......... .......... 44% 15.0M 26s
224650K .......... .......... .......... .......... .......... 44% 26.1M 26s
224700K .......... .......... .......... .......... .......... 44% 24.4M 26s
224750K .......... .......... .......... .......... .......... 44% 26.3M 26s
224800K .......... .......... .......... .......... .......... 44% 21.6M 26s
224850K .......... .......... .......... .......... .......... 44% 24.0M 26s
224900K .......... .......... .......... .......... .......... 44% 23.3M 26s
224950K .......... .......... .......... .......... .......... 44% 22.8M 26s
225000K .......... .......... .......... .......... .......... 44% 19.9M 26s
225050K .......... .......... .......... .......... .......... 44% 13.7M 26s
225100K .......... .......... .......... .......... .......... 44% 12.9M 26s
225150K .......... .......... .......... .......... .......... 44% 15.0M 26s
225200K .......... .......... .......... .......... .......... 44% 13.0M 26s
225250K .......... .......... .......... .......... .......... 44% 15.0M 26s
225300K .......... .......... .......... .......... .......... 44% 12.6M 26s
225350K .......... .......... .......... .......... .......... 44% 10.4M 26s
225400K .......... .......... .......... .......... .......... 44% 9.54M 26s
225450K .......... .......... .......... .......... .......... 44% 12.8M 26s
225500K .......... .......... .......... .......... .......... 44% 17.1M 26s
225550K .......... .......... .......... .......... .......... 44% 9.43M 26s
225600K .......... .......... .......... .......... .......... 44% 10.3M 26s
225650K .......... .......... .......... .......... .......... 44% 12.7M 26s
225700K .......... .......... .......... .......... .......... 44% 8.25M 26s
225750K .......... .......... .......... .......... .......... 44% 10.2M 26s
225800K .......... .......... .......... .......... .......... 44% 10.5M 26s
225850K .......... .......... .......... .......... .......... 44% 9.13M 26s
225900K .......... .......... .......... .......... .......... 44% 8.56M 26s
225950K .......... .......... .......... .......... .......... 44% 8.19M 26s
226000K .......... .......... .......... .......... .......... 44% 6.11M 26s
226050K .......... .......... .......... .......... .......... 44% 6.40M 26s
226100K .......... .......... .......... .......... .......... 44% 4.48M 26s
226150K .......... .......... .......... .......... .......... 44% 5.54M 26s
226200K .......... .......... .......... .......... .......... 44% 8.25M 26s
226250K .......... .......... .......... .......... .......... 44% 17.7M 26s
226300K .......... .......... .......... .......... .......... 44% 23.7M 26s
226350K .......... .......... .......... .......... .......... 44% 24.7M 26s
226400K .......... .......... .......... .......... .......... 44% 16.3M 26s
226450K .......... .......... .......... .......... .......... 44% 10.5M 26s
226500K .......... .......... .......... .......... .......... 44% 13.8M 26s
226550K .......... .......... .......... .......... .......... 44% 10.1M 26s
226600K .......... .......... .......... .......... .......... 44% 5.99M 26s
226650K .......... .......... .......... .......... .......... 44% 4.61M 26s
226700K .......... .......... .......... .......... .......... 44% 3.05M 26s
226750K .......... .......... .......... .......... .......... 44% 6.25M 26s
226800K .......... .......... .......... .......... .......... 44% 9.33M 26s
226850K .......... .......... .......... .......... .......... 44% 7.56M 26s
226900K .......... .......... .......... .......... .......... 44% 9.72M 26s
226950K .......... .......... .......... .......... .......... 44% 8.51M 26s
227000K .......... .......... .......... .......... .......... 44% 9.02M 26s
227050K .......... .......... .......... .......... .......... 44% 8.61M 26s
227100K .......... .......... .......... .......... .......... 45% 9.73M 26s
227150K .......... .......... .......... .......... .......... 45% 21.6M 26s
227200K .......... .......... .......... .......... .......... 45% 11.1M 26s
227250K .......... .......... .......... .......... .......... 45% 8.56M 26s
227300K .......... .......... .......... .......... .......... 45% 6.85M 26s
227350K .......... .......... .......... .......... .......... 45% 5.32M 26s
227400K .......... .......... .......... .......... .......... 45% 5.49M 26s
227450K .......... .......... .......... .......... .......... 45% 3.94M 26s
227500K .......... .......... .......... .......... .......... 45% 4.32M 26s
227550K .......... .......... .......... .......... .......... 45% 4.15M 26s
227600K .......... .......... .......... .......... .......... 45% 9.50M 26s
227650K .......... .......... .......... .......... .......... 45% 28.6M 26s
227700K .......... .......... .......... .......... .......... 45% 16.8M 26s
227750K .......... .......... .......... .......... .......... 45% 49.2M 26s
227800K .......... .......... .......... .......... .......... 45% 23.1M 26s
227850K .......... .......... .......... .......... .......... 45% 15.8M 26s
227900K .......... .......... .......... .......... .......... 45% 23.3M 26s
227950K .......... .......... .......... .......... .......... 45% 9.59M 26s
228000K .......... .......... .......... .......... .......... 45% 14.3M 26s
228050K .......... .......... .......... .......... .......... 45% 15.5M 26s
228100K .......... .......... .......... .......... .......... 45% 9.46M 26s
228150K .......... .......... .......... .......... .......... 45% 13.9M 26s
228200K .......... .......... .......... .......... .......... 45% 9.17M 26s
228250K .......... .......... .......... .......... .......... 45% 7.99M 26s
228300K .......... .......... .......... .......... .......... 45% 6.61M 26s
228350K .......... .......... .......... .......... .......... 45% 5.49M 26s
228400K .......... .......... .......... .......... .......... 45% 6.51M 26s
228450K .......... .......... .......... .......... .......... 45% 5.74M 26s
228500K .......... .......... .......... .......... .......... 45% 11.8M 26s
228550K .......... .......... .......... .......... .......... 45% 8.37M 26s
228600K .......... .......... .......... .......... .......... 45% 8.00M 26s
228650K .......... .......... .......... .......... .......... 45% 10.5M 26s
228700K .......... .......... .......... .......... .......... 45% 7.12M 26s
228750K .......... .......... .......... .......... .......... 45% 9.65M 26s
228800K .......... .......... .......... .......... .......... 45% 7.29M 26s
228850K .......... .......... .......... .......... .......... 45% 6.24M 26s
228900K .......... .......... .......... .......... .......... 45% 14.5M 26s
228950K .......... .......... .......... .......... .......... 45% 20.4M 26s
229000K .......... .......... .......... .......... .......... 45% 14.2M 26s
229050K .......... .......... .......... .......... .......... 45% 15.3M 26s
229100K .......... .......... .......... .......... .......... 45% 9.84M 26s
229150K .......... .......... .......... .......... .......... 45% 11.1M 26s
229200K .......... .......... .......... .......... .......... 45% 8.99M 26s
229250K .......... .......... .......... .......... .......... 45% 11.1M 26s
229300K .......... .......... .......... .......... .......... 45% 9.94M 26s
229350K .......... .......... .......... .......... .......... 45% 6.51M 26s
229400K .......... .......... .......... .......... .......... 45% 9.18M 26s
229450K .......... .......... .......... .......... .......... 45% 6.64M 26s
229500K .......... .......... .......... .......... .......... 45% 7.56M 26s
229550K .......... .......... .......... .......... .......... 45% 6.34M 26s
229600K .......... .......... .......... .......... .......... 45% 6.53M 26s
229650K .......... .......... .......... .......... .......... 45% 6.32M 26s
229700K .......... .......... .......... .......... .......... 45% 7.09M 26s
229750K .......... .......... .......... .......... .......... 45% 8.37M 26s
229800K .......... .......... .......... .......... .......... 45% 8.06M 26s
229850K .......... .......... .......... .......... .......... 45% 5.92M 26s
229900K .......... .......... .......... .......... .......... 45% 6.11M 26s
229950K .......... .......... .......... .......... .......... 45% 4.10M 26s
230000K .......... .......... .......... .......... .......... 45% 3.54M 26s
230050K .......... .......... .......... .......... .......... 45% 4.51M 26s
230100K .......... .......... .......... .......... .......... 45% 10.5M 26s
230150K .......... .......... .......... .......... .......... 45% 12.9M 26s
230200K .......... .......... .......... .......... .......... 45% 9.18M 26s
230250K .......... .......... .......... .......... .......... 45% 12.1M 26s
230300K .......... .......... .......... .......... .......... 45% 10.1M 26s
230350K .......... .......... .......... .......... .......... 45% 11.5M 26s
230400K .......... .......... .......... .......... .......... 45% 10.6M 26s
230450K .......... .......... .......... .......... .......... 45% 8.95M 26s
230500K .......... .......... .......... .......... .......... 45% 9.89M 26s
230550K .......... .......... .......... .......... .......... 45% 8.58M 26s
230600K .......... .......... .......... .......... .......... 45% 5.98M 26s
230650K .......... .......... .......... .......... .......... 45% 5.68M 26s
230700K .......... .......... .......... .......... .......... 45% 5.03M 26s
230750K .......... .......... .......... .......... .......... 45% 6.49M 26s
230800K .......... .......... .......... .......... .......... 45% 8.74M 26s
230850K .......... .......... .......... .......... .......... 45% 16.5M 26s
230900K .......... .......... .......... .......... .......... 45% 10.0M 26s
230950K .......... .......... .......... .......... .......... 45% 39.2M 26s
231000K .......... .......... .......... .......... .......... 45% 14.5M 26s
231050K .......... .......... .......... .......... .......... 45% 12.6M 26s
231100K .......... .......... .......... .......... .......... 45% 24.2M 26s
231150K .......... .......... .......... .......... .......... 45% 15.3M 26s
231200K .......... .......... .......... .......... .......... 45% 15.7M 26s
231250K .......... .......... .......... .......... .......... 45% 13.9M 26s
231300K .......... .......... .......... .......... .......... 45% 17.2M 26s
231350K .......... .......... .......... .......... .......... 45% 12.6M 26s
231400K .......... .......... .......... .......... .......... 45% 13.5M 26s
231450K .......... .......... .......... .......... .......... 45% 9.94M 26s
231500K .......... .......... .......... .......... .......... 45% 12.5M 26s
231550K .......... .......... .......... .......... .......... 45% 12.2M 26s
231600K .......... .......... .......... .......... .......... 45% 10.7M 26s
231650K .......... .......... .......... .......... .......... 45% 10.5M 26s
231700K .......... .......... .......... .......... .......... 45% 9.01M 26s
231750K .......... .......... .......... .......... .......... 45% 10.8M 26s
231800K .......... .......... .......... .......... .......... 45% 7.44M 26s
231850K .......... .......... .......... .......... .......... 45% 14.4M 26s
231900K .......... .......... .......... .......... .......... 45% 23.6M 26s
231950K .......... .......... .......... .......... .......... 45% 10.2M 26s
232000K .......... .......... .......... .......... .......... 45% 13.2M 26s
232050K .......... .......... .......... .......... .......... 45% 14.3M 26s
232100K .......... .......... .......... .......... .......... 45% 10.4M 26s
232150K .......... .......... .......... .......... .......... 46% 14.0M 26s
232200K .......... .......... .......... .......... .......... 46% 12.6M 26s
232250K .......... .......... .......... .......... .......... 46% 14.3M 26s
232300K .......... .......... .......... .......... .......... 46% 12.9M 26s
232350K .......... .......... .......... .......... .......... 46% 9.40M 26s
232400K .......... .......... .......... .......... .......... 46% 8.77M 25s
232450K .......... .......... .......... .......... .......... 46% 8.79M 25s
232500K .......... .......... .......... .......... .......... 46% 9.68M 25s
232550K .......... .......... .......... .......... .......... 46% 9.23M 25s
232600K .......... .......... .......... .......... .......... 46% 8.23M 25s
232650K .......... .......... .......... .......... .......... 46% 6.10M 25s
232700K .......... .......... .......... .......... .......... 46% 4.51M 25s
232750K .......... .......... .......... .......... .......... 46% 5.51M 25s
232800K .......... .......... .......... .......... .......... 46% 4.94M 25s
232850K .......... .......... .......... .......... .......... 46% 7.75M 25s
232900K .......... .......... .......... .......... .......... 46% 26.5M 25s
232950K .......... .......... .......... .......... .......... 46% 23.5M 25s
233000K .......... .......... .......... .......... .......... 46% 27.1M 25s
233050K .......... .......... .......... .......... .......... 46% 23.0M 25s
233100K .......... .......... .......... .......... .......... 46% 16.3M 25s
233150K .......... .......... .......... .......... .......... 46% 16.1M 25s
233200K .......... .......... .......... .......... .......... 46% 10.6M 25s
233250K .......... .......... .......... .......... .......... 46% 9.41M 25s
233300K .......... .......... .......... .......... .......... 46% 8.70M 25s
233350K .......... .......... .......... .......... .......... 46% 6.73M 25s
233400K .......... .......... .......... .......... .......... 46% 8.98M 25s
233450K .......... .......... .......... .......... .......... 46% 6.63M 25s
233500K .......... .......... .......... .......... .......... 46% 5.73M 25s
233550K .......... .......... .......... .......... .......... 46% 11.0M 25s
233600K .......... .......... .......... .......... .......... 46% 8.31M 25s
233650K .......... .......... .......... .......... .......... 46% 7.80M 25s
233700K .......... .......... .......... .......... .......... 46% 9.41M 25s
233750K .......... .......... .......... .......... .......... 46% 9.42M 25s
233800K .......... .......... .......... .......... .......... 46% 11.5M 25s
233850K .......... .......... .......... .......... .......... 46% 9.62M 25s
233900K .......... .......... .......... .......... .......... 46% 10.4M 25s
233950K .......... .......... .......... .......... .......... 46% 9.22M 25s
234000K .......... .......... .......... .......... .......... 46% 12.1M 25s
234050K .......... .......... .......... .......... .......... 46% 11.8M 25s
234100K .......... .......... .......... .......... .......... 46% 7.14M 25s
234150K .......... .......... .......... .......... .......... 46% 7.55M 25s
234200K .......... .......... .......... .......... .......... 46% 4.63M 25s
234250K .......... .......... .......... .......... .......... 46% 5.07M 25s
234300K .......... .......... .......... .......... .......... 46% 5.16M 25s
234350K .......... .......... .......... .......... .......... 46% 4.92M 25s
234400K .......... .......... .......... .......... .......... 46% 9.00M 25s
234450K .......... .......... .......... .......... .......... 46% 9.95M 25s
234500K .......... .......... .......... .......... .......... 46% 9.44M 25s
234550K .......... .......... .......... .......... .......... 46% 10.1M 25s
234600K .......... .......... .......... .......... .......... 46% 7.35M 25s
234650K .......... .......... .......... .......... .......... 46% 8.50M 25s
234700K .......... .......... .......... .......... .......... 46% 6.96M 25s
234750K .......... .......... .......... .......... .......... 46% 8.45M 25s
234800K .......... .......... .......... .......... .......... 46% 7.23M 25s
234850K .......... .......... .......... .......... .......... 46% 6.35M 25s
234900K .......... .......... .......... .......... .......... 46% 5.47M 25s
234950K .......... .......... .......... .......... .......... 46% 3.65M 25s
235000K .......... .......... .......... .......... .......... 46% 5.42M 25s
235050K .......... .......... .......... .......... .......... 46% 5.20M 25s
235100K .......... .......... .......... .......... .......... 46% 12.9M 25s
235150K .......... .......... .......... .......... .......... 46% 15.4M 25s
235200K .......... .......... .......... .......... .......... 46% 14.4M 25s
235250K .......... .......... .......... .......... .......... 46% 11.9M 25s
235300K .......... .......... .......... .......... .......... 46% 11.0M 25s
235350K .......... .......... .......... .......... .......... 46% 9.59M 25s
235400K .......... .......... .......... .......... .......... 46% 10.8M 25s
235450K .......... .......... .......... .......... .......... 46% 8.37M 25s
235500K .......... .......... .......... .......... .......... 46% 12.5M 25s
235550K .......... .......... .......... .......... .......... 46% 8.22M 25s
235600K .......... .......... .......... .......... .......... 46% 9.90M 25s
235650K .......... .......... .......... .......... .......... 46% 8.53M 25s
235700K .......... .......... .......... .......... .......... 46% 7.54M 25s
235750K .......... .......... .......... .......... .......... 46% 5.92M 25s
235800K .......... .......... .......... .......... .......... 46% 7.05M 25s
235850K .......... .......... .......... .......... .......... 46% 11.4M 25s
235900K .......... .......... .......... .......... .......... 46% 15.0M 25s
235950K .......... .......... .......... .......... .......... 46% 15.1M 25s
236000K .......... .......... .......... .......... .......... 46% 15.7M 25s
236050K .......... .......... .......... .......... .......... 46% 11.8M 25s
236100K .......... .......... .......... .......... .......... 46% 15.7M 25s
236150K .......... .......... .......... .......... .......... 46% 13.4M 25s
236200K .......... .......... .......... .......... .......... 46% 11.5M 25s
236250K .......... .......... .......... .......... .......... 46% 12.0M 25s
236300K .......... .......... .......... .......... .......... 46% 13.4M 25s
236350K .......... .......... .......... .......... .......... 46% 8.93M 25s
236400K .......... .......... .......... .......... .......... 46% 7.92M 25s
236450K .......... .......... .......... .......... .......... 46% 5.31M 25s
236500K .......... .......... .......... .......... .......... 46% 5.50M 25s
236550K .......... .......... .......... .......... .......... 46% 6.05M 25s
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236650K .......... .......... .......... .......... .......... 46% 7.59M 25s
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236750K .......... .......... .......... .......... .......... 46% 7.53M 25s
236800K .......... .......... .......... .......... .......... 46% 8.40M 25s
236850K .......... .......... .......... .......... .......... 46% 6.40M 25s
236900K .......... .......... .......... .......... .......... 46% 6.29M 25s
236950K .......... .......... .......... .......... .......... 46% 5.19M 25s
237000K .......... .......... .......... .......... .......... 46% 6.90M 25s
237050K .......... .......... .......... .......... .......... 46% 7.16M 25s
237100K .......... .......... .......... .......... .......... 46% 18.5M 25s
237150K .......... .......... .......... .......... .......... 47% 24.6M 25s
237200K .......... .......... .......... .......... .......... 47% 19.5M 25s
237250K .......... .......... .......... .......... .......... 47% 22.1M 25s
237300K .......... .......... .......... .......... .......... 47% 21.9M 25s
237350K .......... .......... .......... .......... .......... 47% 14.9M 25s
237400K .......... .......... .......... .......... .......... 47% 20.7M 25s
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237500K .......... .......... .......... .......... .......... 47% 17.0M 25s
237550K .......... .......... .......... .......... .......... 47% 9.84M 25s
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237700K .......... .......... .......... .......... .......... 47% 12.6M 25s
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237850K .......... .......... .......... .......... .......... 47% 9.25M 25s
237900K .......... .......... .......... .......... .......... 47% 10.5M 25s
237950K .......... .......... .......... .......... .......... 47% 7.13M 25s
238000K .......... .......... .......... .......... .......... 47% 10.5M 25s
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238100K .......... .......... .......... .......... .......... 47% 7.14M 25s
238150K .......... .......... .......... .......... .......... 47% 6.99M 25s
238200K .......... .......... .......... .......... .......... 47% 8.18M 25s
238250K .......... .......... .......... .......... .......... 47% 10.4M 25s
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238400K .......... .......... .......... .......... .......... 47% 11.7M 25s
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238600K .......... .......... .......... .......... .......... 47% 10.5M 25s
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238700K .......... .......... .......... .......... .......... 47% 11.8M 25s
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238800K .......... .......... .......... .......... .......... 47% 18.9M 25s
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238900K .......... .......... .......... .......... .......... 47% 40.0M 25s
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239000K .......... .......... .......... .......... .......... 47% 52.8M 25s
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239100K .......... .......... .......... .......... .......... 47% 18.0M 25s
239150K .......... .......... .......... .......... .......... 47% 21.0M 25s
239200K .......... .......... .......... .......... .......... 47% 18.6M 25s
239250K .......... .......... .......... .......... .......... 47% 16.2M 25s
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240000K .......... .......... .......... .......... .......... 47% 18.7M 25s
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240100K .......... .......... .......... .......... .......... 47% 14.5M 25s
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240250K .......... .......... .......... .......... .......... 47% 8.75M 25s
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240700K .......... .......... .......... .......... .......... 47% 2.16M 25s
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240800K .......... .......... .......... .......... .......... 47% 2.33M 25s
240850K .......... .......... .......... .......... .......... 47% 9.00M 25s
240900K .......... .......... .......... .......... .......... 47% 11.4M 25s
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241000K .......... .......... .......... .......... .......... 47% 14.4M 25s
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241100K .......... .......... .......... .......... .......... 47% 12.4M 25s
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241300K .......... .......... .......... .......... .......... 47% 13.0M 25s
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241500K .......... .......... .......... .......... .......... 47% 8.98M 25s
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241600K .......... .......... .......... .......... .......... 47% 6.84M 25s
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241700K .......... .......... .......... .......... .......... 47% 9.59M 25s
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241800K .......... .......... .......... .......... .......... 47% 15.0M 25s
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242000K .......... .......... .......... .......... .......... 47% 11.1M 25s
242050K .......... .......... .......... .......... .......... 47% 13.0M 25s
242100K .......... .......... .......... .......... .......... 47% 9.41M 25s
242150K .......... .......... .......... .......... .......... 47% 9.19M 25s
242200K .......... .......... .......... .......... .......... 48% 4.11M 25s
242250K .......... .......... .......... .......... .......... 48% 3.15M 25s
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242350K .......... .......... .......... .......... .......... 48% 3.28M 25s
242400K .......... .......... .......... .......... .......... 48% 12.6M 25s
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242500K .......... .......... .......... .......... .......... 48% 10.5M 25s
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242650K .......... .......... .......... .......... .......... 48% 15.8M 25s
242700K .......... .......... .......... .......... .......... 48% 9.44M 25s
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242800K .......... .......... .......... .......... .......... 48% 11.7M 25s
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242900K .......... .......... .......... .......... .......... 48% 9.50M 25s
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243000K .......... .......... .......... .......... .......... 48% 9.18M 25s
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243100K .......... .......... .......... .......... .......... 48% 14.0M 25s
243150K .......... .......... .......... .......... .......... 48% 15.1M 25s
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243250K .......... .......... .......... .......... .......... 48% 14.9M 25s
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243350K .......... .......... .......... .......... .......... 48% 9.18M 25s
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243700K .......... .......... .......... .......... .......... 48% 5.26M 25s
243750K .......... .......... .......... .......... .......... 48% 8.28M 25s
243800K .......... .......... .......... .......... .......... 48% 13.4M 25s
243850K .......... .......... .......... .......... .......... 48% 11.5M 25s
243900K .......... .......... .......... .......... .......... 48% 8.79M 25s
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244000K .......... .......... .......... .......... .......... 48% 14.0M 25s
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244100K .......... .......... .......... .......... .......... 48% 7.13M 25s
244150K .......... .......... .......... .......... .......... 48% 12.6M 25s
244200K .......... .......... .......... .......... .......... 48% 9.17M 25s
244250K .......... .......... .......... .......... .......... 48% 10.0M 25s
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244700K .......... .......... .......... .......... .......... 48% 7.11M 25s
244750K .......... .......... .......... .......... .......... 48% 10.2M 25s
244800K .......... .......... .......... .......... .......... 48% 9.68M 25s
244850K .......... .......... .......... .......... .......... 48% 7.84M 25s
244900K .......... .......... .......... .......... .......... 48% 8.06M 25s
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245000K .......... .......... .......... .......... .......... 48% 6.54M 25s
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245100K .......... .......... .......... .......... .......... 48% 5.05M 25s
245150K .......... .......... .......... .......... .......... 48% 6.85M 25s
245200K .......... .......... .......... .......... .......... 48% 6.74M 25s
245250K .......... .......... .......... .......... .......... 48% 5.84M 25s
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245400K .......... .......... .......... .......... .......... 48% 8.20M 25s
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245800K .......... .......... .......... .......... .......... 48% 6.30M 25s
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245900K .......... .......... .......... .......... .......... 48% 9.70M 25s
245950K .......... .......... .......... .......... .......... 48% 6.64M 25s
246000K .......... .......... .......... .......... .......... 48% 8.76M 25s
246050K .......... .......... .......... .......... .......... 48% 5.00M 25s
246100K .......... .......... .......... .......... .......... 48% 13.7M 25s
246150K .......... .......... .......... .......... .......... 48% 11.7M 25s
246200K .......... .......... .......... .......... .......... 48% 11.1M 25s
246250K .......... .......... .......... .......... .......... 48% 10.5M 24s
246300K .......... .......... .......... .......... .......... 48% 15.1M 24s
246350K .......... .......... .......... .......... .......... 48% 9.17M 24s
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246450K .......... .......... .......... .......... .......... 48% 7.22M 24s
246500K .......... .......... .......... .......... .......... 48% 13.4M 24s
246550K .......... .......... .......... .......... .......... 48% 15.6M 24s
246600K .......... .......... .......... .......... .......... 48% 12.5M 24s
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246700K .......... .......... .......... .......... .......... 48% 9.20M 24s
246750K .......... .......... .......... .......... .......... 48% 15.7M 24s
246800K .......... .......... .......... .......... .......... 48% 10.1M 24s
246850K .......... .......... .......... .......... .......... 48% 8.60M 24s
246900K .......... .......... .......... .......... .......... 48% 6.96M 24s
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247000K .......... .......... .......... .......... .......... 48% 11.8M 24s
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247100K .......... .......... .......... .......... .......... 48% 8.71M 24s
247150K .......... .......... .......... .......... .......... 48% 12.1M 24s
247200K .......... .......... .......... .......... .......... 48% 9.35M 24s
247250K .......... .......... .......... .......... .......... 49% 7.56M 24s
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247550K .......... .......... .......... .......... .......... 49% 10.4M 24s
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247650K .......... .......... .......... .......... .......... 49% 12.6M 24s
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247800K .......... .......... .......... .......... .......... 49% 12.6M 24s
247850K .......... .......... .......... .......... .......... 49% 7.74M 24s
247900K .......... .......... .......... .......... .......... 49% 12.3M 24s
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248000K .......... .......... .......... .......... .......... 49% 14.1M 24s
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248100K .......... .......... .......... .......... .......... 49% 20.7M 24s
248150K .......... .......... .......... .......... .......... 49% 76.4M 24s
248200K .......... .......... .......... .......... .......... 49% 30.7M 24s
248250K .......... .......... .......... .......... .......... 49% 26.1M 24s
248300K .......... .......... .......... .......... .......... 49% 21.4M 24s
248350K .......... .......... .......... .......... .......... 49% 16.3M 24s
248400K .......... .......... .......... .......... .......... 49% 17.6M 24s
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248500K .......... .......... .......... .......... .......... 49% 12.9M 24s
248550K .......... .......... .......... .......... .......... 49% 8.82M 24s
248600K .......... .......... .......... .......... .......... 49% 9.93M 24s
248650K .......... .......... .......... .......... .......... 49% 10.4M 24s
248700K .......... .......... .......... .......... .......... 49% 7.87M 24s
248750K .......... .......... .......... .......... .......... 49% 7.71M 24s
248800K .......... .......... .......... .......... .......... 49% 5.99M 24s
248850K .......... .......... .......... .......... .......... 49% 8.43M 24s
248900K .......... .......... .......... .......... .......... 49% 5.98M 24s
248950K .......... .......... .......... .......... .......... 49% 11.0M 24s
249000K .......... .......... .......... .......... .......... 49% 9.38M 24s
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249100K .......... .......... .......... .......... .......... 49% 10.5M 24s
249150K .......... .......... .......... .......... .......... 49% 11.8M 24s
249200K .......... .......... .......... .......... .......... 49% 9.72M 24s
249250K .......... .......... .......... .......... .......... 49% 12.2M 24s
249300K .......... .......... .......... .......... .......... 49% 12.1M 24s
249350K .......... .......... .......... .......... .......... 49% 6.13M 24s
249400K .......... .......... .......... .......... .......... 49% 8.77M 24s
249450K .......... .......... .......... .......... .......... 49% 7.92M 24s
249500K .......... .......... .......... .......... .......... 49% 14.5M 24s
249550K .......... .......... .......... .......... .......... 49% 11.8M 24s
249600K .......... .......... .......... .......... .......... 49% 10.8M 24s
249650K .......... .......... .......... .......... .......... 49% 8.55M 24s
249700K .......... .......... .......... .......... .......... 49% 8.14M 24s
249750K .......... .......... .......... .......... .......... 49% 9.19M 24s
249800K .......... .......... .......... .......... .......... 49% 12.2M 24s
249850K .......... .......... .......... .......... .......... 49% 12.3M 24s
249900K .......... .......... .......... .......... .......... 49% 12.1M 24s
249950K .......... .......... .......... .......... .......... 49% 12.1M 24s
250000K .......... .......... .......... .......... .......... 49% 10.8M 24s
250050K .......... .......... .......... .......... .......... 49% 6.29M 24s
250100K .......... .......... .......... .......... .......... 49% 6.38M 24s
250150K .......... .......... .......... .......... .......... 49% 5.63M 24s
250200K .......... .......... .......... .......... .......... 49% 1.98M 24s
250250K .......... .......... .......... .......... .......... 49% 4.01M 24s
250300K .......... .......... .......... .......... .......... 49% 8.05M 24s
250350K .......... .......... .......... .......... .......... 49% 7.38M 24s
250400K .......... .......... .......... .......... .......... 49% 8.64M 24s
250450K .......... .......... .......... .......... .......... 49% 9.03M 24s
250500K .......... .......... .......... .......... .......... 49% 12.5M 24s
250550K .......... .......... .......... .......... .......... 49% 11.8M 24s
250600K .......... .......... .......... .......... .......... 49% 7.12M 24s
250650K .......... .......... .......... .......... .......... 49% 10.8M 24s
250700K .......... .......... .......... .......... .......... 49% 9.20M 24s
250750K .......... .......... .......... .......... .......... 49% 12.6M 24s
250800K .......... .......... .......... .......... .......... 49% 10.1M 24s
250850K .......... .......... .......... .......... .......... 49% 11.6M 24s
250900K .......... .......... .......... .......... .......... 49% 11.0M 24s
250950K .......... .......... .......... .......... .......... 49% 5.49M 24s
251000K .......... .......... .......... .......... .......... 49% 11.4M 24s
251050K .......... .......... .......... .......... .......... 49% 9.90M 24s
251100K .......... .......... .......... .......... .......... 49% 6.83M 24s
251150K .......... .......... .......... .......... .......... 49% 12.2M 24s
251200K .......... .......... .......... .......... .......... 49% 8.56M 24s
251250K .......... .......... .......... .......... .......... 49% 12.9M 24s
251300K .......... .......... .......... .......... .......... 49% 11.5M 24s
251350K .......... .......... .......... .......... .......... 49% 9.32M 24s
251400K .......... .......... .......... .......... .......... 49% 11.8M 24s
251450K .......... .......... .......... .......... .......... 49% 7.18M 24s
251500K .......... .......... .......... .......... .......... 49% 9.55M 24s
251550K .......... .......... .......... .......... .......... 49% 6.38M 24s
251600K .......... .......... .......... .......... .......... 49% 5.30M 24s
251650K .......... .......... .......... .......... .......... 49% 5.08M 24s
251700K .......... .......... .......... .......... .......... 49% 5.06M 24s
251750K .......... .......... .......... .......... .......... 49% 4.70M 24s
251800K .......... .......... .......... .......... .......... 49% 5.08M 24s
251850K .......... .......... .......... .......... .......... 49% 17.2M 24s
251900K .......... .......... .......... .......... .......... 49% 39.9M 24s
251950K .......... .......... .......... .......... .......... 49% 12.6M 24s
252000K .......... .......... .......... .......... .......... 49% 15.0M 24s
252050K .......... .......... .......... .......... .......... 49% 13.2M 24s
252100K .......... .......... .......... .......... .......... 49% 15.2M 24s
252150K .......... .......... .......... .......... .......... 49% 11.7M 24s
252200K .......... .......... .......... .......... .......... 49% 9.46M 24s
252250K .......... .......... .......... .......... .......... 49% 9.46M 24s
252300K .......... .......... .......... .......... .......... 50% 11.1M 24s
252350K .......... .......... .......... .......... .......... 50% 10.5M 24s
252400K .......... .......... .......... .......... .......... 50% 13.5M 24s
252450K .......... .......... .......... .......... .......... 50% 11.6M 24s
252500K .......... .......... .......... .......... .......... 50% 12.8M 24s
252550K .......... .......... .......... .......... .......... 50% 12.5M 24s
252600K .......... .......... .......... .......... .......... 50% 12.1M 24s
252650K .......... .......... .......... .......... .......... 50% 12.5M 24s
252700K .......... .......... .......... .......... .......... 50% 10.4M 24s
252750K .......... .......... .......... .......... .......... 50% 9.67M 24s
252800K .......... .......... .......... .......... .......... 50% 10.8M 24s
252850K .......... .......... .......... .......... .......... 50% 9.58M 24s
252900K .......... .......... .......... .......... .......... 50% 10.2M 24s
252950K .......... .......... .......... .......... .......... 50% 7.57M 24s
253000K .......... .......... .......... .......... .......... 50% 9.20M 24s
253050K .......... .......... .......... .......... .......... 50% 5.05M 24s
253100K .......... .......... .......... .......... .......... 50% 4.05M 24s
253150K .......... .......... .......... .......... .......... 50% 3.86M 24s
253200K .......... .......... .......... .......... .......... 50% 2.93M 24s
253250K .......... .......... .......... .......... .......... 50% 6.07M 24s
253300K .......... .......... .......... .......... .......... 50% 14.4M 24s
253350K .......... .......... .......... .......... .......... 50% 22.5M 24s
253400K .......... .......... .......... .......... .......... 50% 20.5M 24s
253450K .......... .......... .......... .......... .......... 50% 12.9M 24s
253500K .......... .......... .......... .......... .......... 50% 15.0M 24s
253550K .......... .......... .......... .......... .......... 50% 14.6M 24s
253600K .......... .......... .......... .......... .......... 50% 11.3M 24s
253650K .......... .......... .......... .......... .......... 50% 9.62M 24s
253700K .......... .......... .......... .......... .......... 50% 10.7M 24s
253750K .......... .......... .......... .......... .......... 50% 10.5M 24s
253800K .......... .......... .......... .......... .......... 50% 12.9M 24s
253850K .......... .......... .......... .......... .......... 50% 10.4M 24s
253900K .......... .......... .......... .......... .......... 50% 11.8M 24s
253950K .......... .......... .......... .......... .......... 50% 9.93M 24s
254000K .......... .......... .......... .......... .......... 50% 8.42M 24s
254050K .......... .......... .......... .......... .......... 50% 8.61M 24s
254100K .......... .......... .......... .......... .......... 50% 8.19M 24s
254150K .......... .......... .......... .......... .......... 50% 9.91M 24s
254200K .......... .......... .......... .......... .......... 50% 6.20M 24s
254250K .......... .......... .......... .......... .......... 50% 7.74M 24s
254300K .......... .......... .......... .......... .......... 50% 7.13M 24s
254350K .......... .......... .......... .......... .......... 50% 15.6M 24s
254400K .......... .......... .......... .......... .......... 50% 10.2M 24s
254450K .......... .......... .......... .......... .......... 50% 9.18M 24s
254500K .......... .......... .......... .......... .......... 50% 9.24M 24s
254550K .......... .......... .......... .......... .......... 50% 8.43M 24s
254600K .......... .......... .......... .......... .......... 50% 8.61M 24s
254650K .......... .......... .......... .......... .......... 50% 12.1M 24s
254700K .......... .......... .......... .......... .......... 50% 8.98M 24s
254750K .......... .......... .......... .......... .......... 50% 12.0M 24s
254800K .......... .......... .......... .......... .......... 50% 20.4M 24s
254850K .......... .......... .......... .......... .......... 50% 13.9M 24s
254900K .......... .......... .......... .......... .......... 50% 26.9M 24s
254950K .......... .......... .......... .......... .......... 50% 12.8M 24s
255000K .......... .......... .......... .......... .......... 50% 11.8M 24s
255050K .......... .......... .......... .......... .......... 50% 13.0M 24s
255100K .......... .......... .......... .......... .......... 50% 5.81M 24s
255150K .......... .......... .......... .......... .......... 50% 7.13M 24s
255200K .......... .......... .......... .......... .......... 50% 5.41M 24s
255250K .......... .......... .......... .......... .......... 50% 5.18M 24s
255300K .......... .......... .......... .......... .......... 50% 4.82M 24s
255350K .......... .......... .......... .......... .......... 50% 4.92M 24s
255400K .......... .......... .......... .......... .......... 50% 12.1M 24s
255450K .......... .......... .......... .......... .......... 50% 11.4M 24s
255500K .......... .......... .......... .......... .......... 50% 10.2M 24s
255550K .......... .......... .......... .......... .......... 50% 12.6M 24s
255600K .......... .......... .......... .......... .......... 50% 9.40M 24s
255650K .......... .......... .......... .......... .......... 50% 11.1M 24s
255700K .......... .......... .......... .......... .......... 50% 9.22M 24s
255750K .......... .......... .......... .......... .......... 50% 9.70M 24s
255800K .......... .......... .......... .......... .......... 50% 3.55M 24s
255850K .......... .......... .......... .......... .......... 50% 97.1M 24s
255900K .......... .......... .......... .......... .......... 50% 47.1M 24s
255950K .......... .......... .......... .......... .......... 50% 20.9M 24s
256000K .......... .......... .......... .......... .......... 50% 37.4M 24s
256050K .......... .......... .......... .......... .......... 50% 37.3M 24s
256100K .......... .......... .......... .......... .......... 50% 23.7M 24s
256150K .......... .......... .......... .......... .......... 50% 47.5M 24s
256200K .......... .......... .......... .......... .......... 50% 21.9M 24s
256250K .......... .......... .......... .......... .......... 50% 27.4M 24s
256300K .......... .......... .......... .......... .......... 50% 17.2M 24s
256350K .......... .......... .......... .......... .......... 50% 12.3M 24s
256400K .......... .......... .......... .......... .......... 50% 14.2M 24s
256450K .......... .......... .......... .......... .......... 50% 10.1M 24s
256500K .......... .......... .......... .......... .......... 50% 10.2M 24s
256550K .......... .......... .......... .......... .......... 50% 11.1M 24s
256600K .......... .......... .......... .......... .......... 50% 11.4M 24s
256650K .......... .......... .......... .......... .......... 50% 11.9M 24s
256700K .......... .......... .......... .......... .......... 50% 10.2M 24s
256750K .......... .......... .......... .......... .......... 50% 8.99M 24s
256800K .......... .......... .......... .......... .......... 50% 10.1M 24s
256850K .......... .......... .......... .......... .......... 50% 10.8M 24s
256900K .......... .......... .......... .......... .......... 50% 15.9M 24s
256950K .......... .......... .......... .......... .......... 50% 12.1M 24s
257000K .......... .......... .......... .......... .......... 50% 76.1M 24s
257050K .......... .......... .......... .......... .......... 50% 27.2M 24s
257100K .......... .......... .......... .......... .......... 50% 17.0M 24s
257150K .......... .......... .......... .......... .......... 50% 14.5M 24s
257200K .......... .......... .......... .......... .......... 50% 11.3M 24s
257250K .......... .......... .......... .......... .......... 50% 9.17M 24s
257300K .......... .......... .......... .......... .......... 50% 12.6M 24s
257350K .......... .......... .......... .......... .......... 51% 7.85M 24s
257400K .......... .......... .......... .......... .......... 51% 4.68M 24s
257450K .......... .......... .......... .......... .......... 51% 3.65M 24s
257500K .......... .......... .......... .......... .......... 51% 3.93M 24s
257550K .......... .......... .......... .......... .......... 51% 8.92M 24s
257600K .......... .......... .......... .......... .......... 51% 16.8M 24s
257650K .......... .......... .......... .......... .......... 51% 17.8M 24s
257700K .......... .......... .......... .......... .......... 51% 17.9M 23s
257750K .......... .......... .......... .......... .......... 51% 15.1M 23s
257800K .......... .......... .......... .......... .......... 51% 14.8M 23s
257850K .......... .......... .......... .......... .......... 51% 11.4M 23s
257900K .......... .......... .......... .......... .......... 51% 5.47M 23s
257950K .......... .......... .......... .......... .......... 51% 5.00M 23s
258000K .......... .......... .......... .......... .......... 51% 3.37M 23s
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258100K .......... .......... .......... .......... .......... 51% 2.13M 24s
258150K .......... .......... .......... .......... .......... 51% 2.57M 24s
258200K .......... .......... .......... .......... .......... 51% 6.13M 24s
258250K .......... .......... .......... .......... .......... 51% 13.5M 24s
258300K .......... .......... .......... .......... .......... 51% 74.4M 23s
258350K .......... .......... .......... .......... .......... 51% 28.5M 23s
258400K .......... .......... .......... .......... .......... 51% 21.3M 23s
258450K .......... .......... .......... .......... .......... 51% 10.6M 23s
258500K .......... .......... .......... .......... .......... 51% 9.01M 23s
258550K .......... .......... .......... .......... .......... 51% 9.01M 23s
258600K .......... .......... .......... .......... .......... 51% 6.68M 23s
258650K .......... .......... .......... .......... .......... 51% 7.40M 23s
258700K .......... .......... .......... .......... .......... 51% 5.24M 23s
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258900K .......... .......... .......... .......... .......... 51% 7.31M 23s
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259000K .......... .......... .......... .......... .......... 51% 7.54M 23s
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259100K .......... .......... .......... .......... .......... 51% 6.02M 23s
259150K .......... .......... .......... .......... .......... 51% 9.17M 23s
259200K .......... .......... .......... .......... .......... 51% 9.67M 23s
259250K .......... .......... .......... .......... .......... 51% 12.5M 23s
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259350K .......... .......... .......... .......... .......... 51% 9.71M 23s
259400K .......... .......... .......... .......... .......... 51% 13.1M 23s
259450K .......... .......... .......... .......... .......... 51% 8.94M 23s
259500K .......... .......... .......... .......... .......... 51% 11.9M 23s
259550K .......... .......... .......... .......... .......... 51% 9.97M 23s
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259900K .......... .......... .......... .......... .......... 51% 12.4M 23s
259950K .......... .......... .......... .......... .......... 51% 8.21M 23s
260000K .......... .......... .......... .......... .......... 51% 15.8M 23s
260050K .......... .......... .......... .......... .......... 51% 13.0M 23s
260100K .......... .......... .......... .......... .......... 51% 10.5M 23s
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260200K .......... .......... .......... .......... .......... 51% 11.5M 23s
260250K .......... .......... .......... .......... .......... 51% 12.7M 23s
260300K .......... .......... .......... .......... .......... 51% 12.3M 23s
260350K .......... .......... .......... .......... .......... 51% 10.2M 23s
260400K .......... .......... .......... .......... .......... 51% 15.8M 23s
260450K .......... .......... .......... .......... .......... 51% 6.13M 23s
260500K .......... .......... .......... .......... .......... 51% 11.2M 23s
260550K .......... .......... .......... .......... .......... 51% 12.3M 23s
260600K .......... .......... .......... .......... .......... 51% 7.08M 23s
260650K .......... .......... .......... .......... .......... 51% 8.47M 23s
260700K .......... .......... .......... .......... .......... 51% 9.05M 23s
260750K .......... .......... .......... .......... .......... 51% 27.0M 23s
260800K .......... .......... .......... .......... .......... 51% 13.7M 23s
260850K .......... .......... .......... .......... .......... 51% 15.6M 23s
260900K .......... .......... .......... .......... .......... 51% 21.9M 23s
260950K .......... .......... .......... .......... .......... 51% 14.4M 23s
261000K .......... .......... .......... .......... .......... 51% 19.9M 23s
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261100K .......... .......... .......... .......... .......... 51% 11.0M 23s
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261200K .......... .......... .......... .......... .......... 51% 11.7M 23s
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261300K .......... .......... .......... .......... .......... 51% 13.1M 23s
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261400K .......... .......... .......... .......... .......... 51% 15.7M 23s
261450K .......... .......... .......... .......... .......... 51% 7.88M 23s
261500K .......... .......... .......... .......... .......... 51% 7.88M 23s
261550K .......... .......... .......... .......... .......... 51% 9.68M 23s
261600K .......... .......... .......... .......... .......... 51% 7.17M 23s
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261800K .......... .......... .......... .......... .......... 51% 9.71M 23s
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261900K .......... .......... .......... .......... .......... 51% 10.4M 23s
261950K .......... .......... .......... .......... .......... 51% 9.19M 23s
262000K .......... .......... .......... .......... .......... 51% 9.33M 23s
262050K .......... .......... .......... .......... .......... 51% 23.0M 23s
262100K .......... .......... .......... .......... .......... 51% 13.7M 23s
262150K .......... .......... .......... .......... .......... 51% 57.9M 23s
262200K .......... .......... .......... .......... .......... 51% 9.58M 23s
262250K .......... .......... .......... .......... .......... 51% 11.9M 23s
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262350K .......... .......... .......... .......... .......... 51% 8.25M 23s
262400K .......... .......... .......... .......... .......... 52% 10.4M 23s
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262500K .......... .......... .......... .......... .......... 52% 10.5M 23s
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262600K .......... .......... .......... .......... .......... 52% 3.52M 23s
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262700K .......... .......... .......... .......... .......... 52% 3.17M 23s
262750K .......... .......... .......... .......... .......... 52% 7.15M 23s
262800K .......... .......... .......... .......... .......... 52% 7.17M 23s
262850K .......... .......... .......... .......... .......... 52% 4.67M 23s
262900K .......... .......... .......... .......... .......... 52% 6.12M 23s
262950K .......... .......... .......... .......... .......... 52% 6.30M 23s
263000K .......... .......... .......... .......... .......... 52% 7.38M 23s
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263100K .......... .......... .......... .......... .......... 52% 6.32M 23s
263150K .......... .......... .......... .......... .......... 52% 5.92M 23s
263200K .......... .......... .......... .......... .......... 52% 5.47M 23s
263250K .......... .......... .......... .......... .......... 52% 7.56M 23s
263300K .......... .......... .......... .......... .......... 52% 6.24M 23s
263350K .......... .......... .......... .......... .......... 52% 4.93M 23s
263400K .......... .......... .......... .......... .......... 52% 7.03M 23s
263450K .......... .......... .......... .......... .......... 52% 22.1M 23s
263500K .......... .......... .......... .......... .......... 52% 20.3M 23s
263550K .......... .......... .......... .......... .......... 52% 58.5M 23s
263600K .......... .......... .......... .......... .......... 52% 17.5M 23s
263650K .......... .......... .......... .......... .......... 52% 18.2M 23s
263700K .......... .......... .......... .......... .......... 52% 15.6M 23s
263750K .......... .......... .......... .......... .......... 52% 23.5M 23s
263800K .......... .......... .......... .......... .......... 52% 17.8M 23s
263850K .......... .......... .......... .......... .......... 52% 19.9M 23s
263900K .......... .......... .......... .......... .......... 52% 18.8M 23s
263950K .......... .......... .......... .......... .......... 52% 15.9M 23s
264000K .......... .......... .......... .......... .......... 52% 13.0M 23s
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264100K .......... .......... .......... .......... .......... 52% 15.1M 23s
264150K .......... .......... .......... .......... .......... 52% 12.5M 23s
264200K .......... .......... .......... .......... .......... 52% 10.8M 23s
264250K .......... .......... .......... .......... .......... 52% 14.0M 23s
264300K .......... .......... .......... .......... .......... 52% 10.8M 23s
264350K .......... .......... .......... .......... .......... 52% 9.93M 23s
264400K .......... .......... .......... .......... .......... 52% 13.1M 23s
264450K .......... .......... .......... .......... .......... 52% 10.3M 23s
264500K .......... .......... .......... .......... .......... 52% 16.3M 23s
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264650K .......... .......... .......... .......... .......... 52% 9.28M 23s
264700K .......... .......... .......... .......... .......... 52% 8.13M 23s
264750K .......... .......... .......... .......... .......... 52% 8.95M 23s
264800K .......... .......... .......... .......... .......... 52% 7.15M 23s
264850K .......... .......... .......... .......... .......... 52% 5.42M 23s
264900K .......... .......... .......... .......... .......... 52% 4.46M 23s
264950K .......... .......... .......... .......... .......... 52% 2.97M 23s
265000K .......... .......... .......... .......... .......... 52% 5.32M 23s
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265100K .......... .......... .......... .......... .......... 52% 3.92M 23s
265150K .......... .......... .......... .......... .......... 52% 10.8M 23s
265200K .......... .......... .......... .......... .......... 52% 11.2M 23s
265250K .......... .......... .......... .......... .......... 52% 12.8M 23s
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266000K .......... .......... .......... .......... .......... 52% 14.0M 23s
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266100K .......... .......... .......... .......... .......... 52% 9.61M 23s
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266250K .......... .......... .......... .......... .......... 52% 11.7M 23s
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267000K .......... .......... .......... .......... .......... 52% 8.21M 23s
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267100K .......... .......... .......... .......... .......... 52% 8.83M 23s
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267250K .......... .......... .......... .......... .......... 52% 18.7M 23s
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268250K .......... .......... .......... .......... .......... 53% 84.6M 23s
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269100K .......... .......... .......... .......... .......... 53% 23.2M 23s
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274250K .......... .......... .......... .......... .......... 54% 29.5M 22s
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275000K .......... .......... .......... .......... .......... 54% 27.5M 22s
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275100K .......... .......... .......... .......... .......... 54% 22.1M 22s
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275250K .......... .......... .......... .......... .......... 54% 23.8M 22s
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276250K .......... .......... .......... .......... .......... 54% 22.7M 22s
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276500K .......... .......... .......... .......... .......... 54% 13.3M 22s
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277000K .......... .......... .......... .......... .......... 54% 17.9M 21s
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277100K .......... .......... .......... .......... .......... 54% 14.5M 21s
277150K .......... .......... .......... .......... .......... 54% 31.1M 21s
277200K .......... .......... .......... .......... .......... 54% 27.4M 21s
277250K .......... .......... .......... .......... .......... 54% 65.1M 21s
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277800K .......... .......... .......... .......... .......... 55% 25.9M 21s
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278000K .......... .......... .......... .......... .......... 55% 28.9M 21s
278050K .......... .......... .......... .......... .......... 55% 38.1M 21s
278100K .......... .......... .......... .......... .......... 55% 28.7M 21s
278150K .......... .......... .......... .......... .......... 55% 33.8M 21s
278200K .......... .......... .......... .......... .......... 55% 25.4M 21s
278250K .......... .......... .......... .......... .......... 55% 40.2M 21s
278300K .......... .......... .......... .......... .......... 55% 30.7M 21s
278350K .......... .......... .......... .......... .......... 55% 26.7M 21s
278400K .......... .......... .......... .......... .......... 55% 22.5M 21s
278450K .......... .......... .......... .......... .......... 55% 35.4M 21s
278500K .......... .......... .......... .......... .......... 55% 25.7M 21s
278550K .......... .......... .......... .......... .......... 55% 32.8M 21s
278600K .......... .......... .......... .......... .......... 55% 24.2M 21s
278650K .......... .......... .......... .......... .......... 55% 27.7M 21s
278700K .......... .......... .......... .......... .......... 55% 15.7M 21s
278750K .......... .......... .......... .......... .......... 55% 25.8M 21s
278800K .......... .......... .......... .......... .......... 55% 16.7M 21s
278850K .......... .......... .......... .......... .......... 55% 13.9M 21s
278900K .......... .......... .......... .......... .......... 55% 21.0M 21s
278950K .......... .......... .......... .......... .......... 55% 15.1M 21s
279000K .......... .......... .......... .......... .......... 55% 23.2M 21s
279050K .......... .......... .......... .......... .......... 55% 18.9M 21s
279100K .......... .......... .......... .......... .......... 55% 14.4M 21s
279150K .......... .......... .......... .......... .......... 55% 19.7M 21s
279200K .......... .......... .......... .......... .......... 55% 18.6M 21s
279250K .......... .......... .......... .......... .......... 55% 17.0M 21s
279300K .......... .......... .......... .......... .......... 55% 23.8M 21s
279350K .......... .......... .......... .......... .......... 55% 20.4M 21s
279400K .......... .......... .......... .......... .......... 55% 16.2M 21s
279450K .......... .......... .......... .......... .......... 55% 19.9M 21s
279500K .......... .......... .......... .......... .......... 55% 32.9M 21s
279550K .......... .......... .......... .......... .......... 55% 38.7M 21s
279600K .......... .......... .......... .......... .......... 55% 10.4M 21s
279650K .......... .......... .......... .......... .......... 55% 93.4M 21s
279700K .......... .......... .......... .......... .......... 55% 72.6M 21s
279750K .......... .......... .......... .......... .......... 55% 33.5M 21s
279800K .......... .......... .......... .......... .......... 55% 95.4M 21s
279850K .......... .......... .......... .......... .......... 55% 46.8M 21s
279900K .......... .......... .......... .......... .......... 55% 26.0M 21s
279950K .......... .......... .......... .......... .......... 55% 35.9M 21s
280000K .......... .......... .......... .......... .......... 55% 29.0M 21s
280050K .......... .......... .......... .......... .......... 55% 26.8M 21s
280100K .......... .......... .......... .......... .......... 55% 33.4M 21s
280150K .......... .......... .......... .......... .......... 55% 27.0M 21s
280200K .......... .......... .......... .......... .......... 55% 29.3M 21s
280250K .......... .......... .......... .......... .......... 55% 27.8M 21s
280300K .......... .......... .......... .......... .......... 55% 30.7M 21s
280350K .......... .......... .......... .......... .......... 55% 31.9M 21s
280400K .......... .......... .......... .......... .......... 55% 28.2M 21s
280450K .......... .......... .......... .......... .......... 55% 30.9M 21s
280500K .......... .......... .......... .......... .......... 55% 31.4M 21s
280550K .......... .......... .......... .......... .......... 55% 22.6M 21s
280600K .......... .......... .......... .......... .......... 55% 32.5M 21s
280650K .......... .......... .......... .......... .......... 55% 37.1M 21s
280700K .......... .......... .......... .......... .......... 55% 27.5M 21s
280750K .......... .......... .......... .......... .......... 55% 27.6M 21s
280800K .......... .......... .......... .......... .......... 55% 31.4M 21s
280850K .......... .......... .......... .......... .......... 55% 25.1M 21s
280900K .......... .......... .......... .......... .......... 55% 42.9M 21s
280950K .......... .......... .......... .......... .......... 55% 28.9M 21s
281000K .......... .......... .......... .......... .......... 55% 33.9M 21s
281050K .......... .......... .......... .......... .......... 55% 50.2M 21s
281100K .......... .......... .......... .......... .......... 55% 45.8M 21s
281150K .......... .......... .......... .......... .......... 55% 25.0M 21s
281200K .......... .......... .......... .......... .......... 55% 78.8M 21s
281250K .......... .......... .......... .......... .......... 55% 33.5M 21s
281300K .......... .......... .......... .......... .......... 55% 43.8M 21s
281350K .......... .......... .......... .......... .......... 55% 70.8M 21s
281400K .......... .......... .......... .......... .......... 55% 40.3M 21s
281450K .......... .......... .......... .......... .......... 55% 38.0M 21s
281500K .......... .......... .......... .......... .......... 55% 28.5M 21s
281550K .......... .......... .......... .......... .......... 55% 52.0M 21s
281600K .......... .......... .......... .......... .......... 55% 27.1M 21s
281650K .......... .......... .......... .......... .......... 55% 30.7M 21s
281700K .......... .......... .......... .......... .......... 55% 31.0M 21s
281750K .......... .......... .......... .......... .......... 55% 32.0M 21s
281800K .......... .......... .......... .......... .......... 55% 39.4M 21s
281850K .......... .......... .......... .......... .......... 55% 23.6M 21s
281900K .......... .......... .......... .......... .......... 55% 30.8M 21s
281950K .......... .......... .......... .......... .......... 55% 32.6M 21s
282000K .......... .......... .......... .......... .......... 55% 32.9M 21s
282050K .......... .......... .......... .......... .......... 55% 26.3M 21s
282100K .......... .......... .......... .......... .......... 55% 28.6M 21s
282150K .......... .......... .......... .......... .......... 55% 25.1M 21s
282200K .......... .......... .......... .......... .......... 55% 26.7M 21s
282250K .......... .......... .......... .......... .......... 55% 25.0M 21s
282300K .......... .......... .......... .......... .......... 55% 34.1M 21s
282350K .......... .......... .......... .......... .......... 55% 23.5M 21s
282400K .......... .......... .......... .......... .......... 55% 31.3M 21s
282450K .......... .......... .......... .......... .......... 55% 24.6M 21s
282500K .......... .......... .......... .......... .......... 55% 23.9M 21s
282550K .......... .......... .......... .......... .......... 55% 13.3M 21s
282600K .......... .......... .......... .......... .......... 56% 22.2M 21s
282650K .......... .......... .......... .......... .......... 56% 15.2M 21s
282700K .......... .......... .......... .......... .......... 56% 18.4M 21s
282750K .......... .......... .......... .......... .......... 56% 26.9M 21s
282800K .......... .......... .......... .......... .......... 56% 15.1M 21s
282850K .......... .......... .......... .......... .......... 56% 10.1M 21s
282900K .......... .......... .......... .......... .......... 56% 11.5M 21s
282950K .......... .......... .......... .......... .......... 56% 12.5M 21s
283000K .......... .......... .......... .......... .......... 56% 12.1M 21s
283050K .......... .......... .......... .......... .......... 56% 12.7M 21s
283100K .......... .......... .......... .......... .......... 56% 11.2M 21s
283150K .......... .......... .......... .......... .......... 56% 13.9M 21s
283200K .......... .......... .......... .......... .......... 56% 12.6M 21s
283250K .......... .......... .......... .......... .......... 56% 11.8M 21s
283300K .......... .......... .......... .......... .......... 56% 11.3M 21s
283350K .......... .......... .......... .......... .......... 56% 12.4M 21s
283400K .......... .......... .......... .......... .......... 56% 19.7M 21s
283450K .......... .......... .......... .......... .......... 56% 16.6M 21s
283500K .......... .......... .......... .......... .......... 56% 12.4M 21s
283550K .......... .......... .......... .......... .......... 56% 23.3M 21s
283600K .......... .......... .......... .......... .......... 56% 8.21M 21s
283650K .......... .......... .......... .......... .......... 56% 61.5M 21s
283700K .......... .......... .......... .......... .......... 56% 18.8M 21s
283750K .......... .......... .......... .......... .......... 56% 14.7M 21s
283800K .......... .......... .......... .......... .......... 56% 15.8M 21s
283850K .......... .......... .......... .......... .......... 56% 17.8M 21s
283900K .......... .......... .......... .......... .......... 56% 11.8M 21s
283950K .......... .......... .......... .......... .......... 56% 9.77M 21s
284000K .......... .......... .......... .......... .......... 56% 19.5M 21s
284050K .......... .......... .......... .......... .......... 56% 23.3M 21s
284100K .......... .......... .......... .......... .......... 56% 14.4M 21s
284150K .......... .......... .......... .......... .......... 56% 22.0M 20s
284200K .......... .......... .......... .......... .......... 56% 16.5M 20s
284250K .......... .......... .......... .......... .......... 56% 19.7M 20s
284300K .......... .......... .......... .......... .......... 56% 16.4M 20s
284350K .......... .......... .......... .......... .......... 56% 17.0M 20s
284400K .......... .......... .......... .......... .......... 56% 17.8M 20s
284450K .......... .......... .......... .......... .......... 56% 17.9M 20s
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284550K .......... .......... .......... .......... .......... 56% 13.9M 20s
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284650K .......... .......... .......... .......... .......... 56% 20.8M 20s
284700K .......... .......... .......... .......... .......... 56% 13.9M 20s
284750K .......... .......... .......... .......... .......... 56% 10.3M 20s
284800K .......... .......... .......... .......... .......... 56% 13.8M 20s
284850K .......... .......... .......... .......... .......... 56% 11.4M 20s
284900K .......... .......... .......... .......... .......... 56% 13.8M 20s
284950K .......... .......... .......... .......... .......... 56% 13.0M 20s
285000K .......... .......... .......... .......... .......... 56% 15.5M 20s
285050K .......... .......... .......... .......... .......... 56% 15.8M 20s
285100K .......... .......... .......... .......... .......... 56% 13.9M 20s
285150K .......... .......... .......... .......... .......... 56% 12.9M 20s
285200K .......... .......... .......... .......... .......... 56% 16.3M 20s
285250K .......... .......... .......... .......... .......... 56% 13.5M 20s
285300K .......... .......... .......... .......... .......... 56% 17.1M 20s
285350K .......... .......... .......... .......... .......... 56% 15.6M 20s
285400K .......... .......... .......... .......... .......... 56% 31.0M 20s
285450K .......... .......... .......... .......... .......... 56% 17.9M 20s
285500K .......... .......... .......... .......... .......... 56% 70.2M 20s
285550K .......... .......... .......... .......... .......... 56% 73.3M 20s
285600K .......... .......... .......... .......... .......... 56% 29.7M 20s
285650K .......... .......... .......... .......... .......... 56% 47.5M 20s
285700K .......... .......... .......... .......... .......... 56% 31.6M 20s
285750K .......... .......... .......... .......... .......... 56% 30.4M 20s
285800K .......... .......... .......... .......... .......... 56% 36.7M 20s
285850K .......... .......... .......... .......... .......... 56% 33.8M 20s
285900K .......... .......... .......... .......... .......... 56% 34.0M 20s
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286000K .......... .......... .......... .......... .......... 56% 30.5M 20s
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286100K .......... .......... .......... .......... .......... 56% 31.0M 20s
286150K .......... .......... .......... .......... .......... 56% 32.2M 20s
286200K .......... .......... .......... .......... .......... 56% 28.3M 20s
286250K .......... .......... .......... .......... .......... 56% 31.2M 20s
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286400K .......... .......... .......... .......... .......... 56% 29.6M 20s
286450K .......... .......... .......... .......... .......... 56% 26.2M 20s
286500K .......... .......... .......... .......... .......... 56% 31.2M 20s
286550K .......... .......... .......... .......... .......... 56% 41.3M 20s
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286650K .......... .......... .......... .......... .......... 56% 31.4M 20s
286700K .......... .......... .......... .......... .......... 56% 30.7M 20s
286750K .......... .......... .......... .......... .......... 56% 26.4M 20s
286800K .......... .......... .......... .......... .......... 56% 25.8M 20s
286850K .......... .......... .......... .......... .......... 56% 29.2M 20s
286900K .......... .......... .......... .......... .......... 56% 22.4M 20s
286950K .......... .......... .......... .......... .......... 56% 31.1M 20s
287000K .......... .......... .......... .......... .......... 56% 30.0M 20s
287050K .......... .......... .......... .......... .......... 56% 19.1M 20s
287100K .......... .......... .......... .......... .......... 56% 29.6M 20s
287150K .......... .......... .......... .......... .......... 56% 16.9M 20s
287200K .......... .......... .......... .......... .......... 56% 65.2M 20s
287250K .......... .......... .......... .......... .......... 56% 28.5M 20s
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287350K .......... .......... .......... .......... .......... 56% 21.4M 20s
287400K .......... .......... .......... .......... .......... 56% 19.6M 20s
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287500K .......... .......... .......... .......... .......... 56% 19.8M 20s
287550K .......... .......... .......... .......... .......... 56% 17.8M 20s
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287650K .......... .......... .......... .......... .......... 57% 19.8M 20s
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287750K .......... .......... .......... .......... .......... 57% 19.6M 20s
287800K .......... .......... .......... .......... .......... 57% 23.1M 20s
287850K .......... .......... .......... .......... .......... 57% 15.7M 20s
287900K .......... .......... .......... .......... .......... 57% 21.5M 20s
287950K .......... .......... .......... .......... .......... 57% 13.6M 20s
288000K .......... .......... .......... .......... .......... 57% 29.3M 20s
288050K .......... .......... .......... .......... .......... 57% 26.3M 20s
288100K .......... .......... .......... .......... .......... 57% 46.3M 20s
288150K .......... .......... .......... .......... .......... 57% 13.8M 20s
288200K .......... .......... .......... .......... .......... 57% 48.8M 20s
288250K .......... .......... .......... .......... .......... 57% 30.0M 20s
288300K .......... .......... .......... .......... .......... 57% 36.8M 20s
288350K .......... .......... .......... .......... .......... 57% 30.5M 20s
288400K .......... .......... .......... .......... .......... 57% 23.6M 20s
288450K .......... .......... .......... .......... .......... 57% 21.5M 20s
288500K .......... .......... .......... .......... .......... 57% 18.8M 20s
288550K .......... .......... .......... .......... .......... 57% 25.0M 20s
288600K .......... .......... .......... .......... .......... 57% 18.0M 20s
288650K .......... .......... .......... .......... .......... 57% 12.7M 20s
288700K .......... .......... .......... .......... .......... 57% 17.0M 20s
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288800K .......... .......... .......... .......... .......... 57% 19.7M 20s
288850K .......... .......... .......... .......... .......... 57% 17.9M 20s
288900K .......... .......... .......... .......... .......... 57% 26.4M 20s
288950K .......... .......... .......... .......... .......... 57% 19.7M 20s
289000K .......... .......... .......... .......... .......... 57% 23.3M 20s
289050K .......... .......... .......... .......... .......... 57% 20.6M 20s
289100K .......... .......... .......... .......... .......... 57% 27.4M 20s
289150K .......... .......... .......... .......... .......... 57% 40.2M 20s
289200K .......... .......... .......... .......... .......... 57% 41.3M 20s
289250K .......... .......... .......... .......... .......... 57% 55.2M 20s
289300K .......... .......... .......... .......... .......... 57% 30.3M 20s
289350K .......... .......... .......... .......... .......... 57% 71.6M 20s
289400K .......... .......... .......... .......... .......... 57% 61.7M 20s
289450K .......... .......... .......... .......... .......... 57% 37.5M 20s
289500K .......... .......... .......... .......... .......... 57% 82.9M 20s
289550K .......... .......... .......... .......... .......... 57% 68.9M 20s
289600K .......... .......... .......... .......... .......... 57% 26.7M 20s
289650K .......... .......... .......... .......... .......... 57% 37.7M 20s
289700K .......... .......... .......... .......... .......... 57% 28.8M 20s
289750K .......... .......... .......... .......... .......... 57% 43.1M 20s
289800K .......... .......... .......... .......... .......... 57% 36.0M 20s
289850K .......... .......... .......... .......... .......... 57% 34.1M 20s
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289950K .......... .......... .......... .......... .......... 57% 32.3M 20s
290000K .......... .......... .......... .......... .......... 57% 37.4M 20s
290050K .......... .......... .......... .......... .......... 57% 37.9M 20s
290100K .......... .......... .......... .......... .......... 57% 37.2M 20s
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290200K .......... .......... .......... .......... .......... 57% 33.8M 20s
290250K .......... .......... .......... .......... .......... 57% 37.4M 20s
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290350K .......... .......... .......... .......... .......... 57% 35.6M 20s
290400K .......... .......... .......... .......... .......... 57% 53.4M 20s
290450K .......... .......... .......... .......... .......... 57% 26.8M 20s
290500K .......... .......... .......... .......... .......... 57% 37.2M 20s
290550K .......... .......... .......... .......... .......... 57% 30.7M 20s
290600K .......... .......... .......... .......... .......... 57% 26.5M 20s
290650K .......... .......... .......... .......... .......... 57% 53.7M 20s
290700K .......... .......... .......... .......... .......... 57% 17.8M 20s
290750K .......... .......... .......... .......... .......... 57% 20.0M 20s
290800K .......... .......... .......... .......... .......... 57% 13.1M 20s
290850K .......... .......... .......... .......... .......... 57% 85.8M 20s
290900K .......... .......... .......... .......... .......... 57% 21.8M 20s
290950K .......... .......... .......... .......... .......... 57% 46.9M 20s
291000K .......... .......... .......... .......... .......... 57% 20.7M 20s
291050K .......... .......... .......... .......... .......... 57% 42.3M 20s
291100K .......... .......... .......... .......... .......... 57% 28.8M 20s
291150K .......... .......... .......... .......... .......... 57% 19.8M 20s
291200K .......... .......... .......... .......... .......... 57% 25.1M 20s
291250K .......... .......... .......... .......... .......... 57% 34.2M 20s
291300K .......... .......... .......... .......... .......... 57% 26.6M 20s
291350K .......... .......... .......... .......... .......... 57% 21.9M 20s
291400K .......... .......... .......... .......... .......... 57% 25.6M 20s
291450K .......... .......... .......... .......... .......... 57% 21.4M 20s
291500K .......... .......... .......... .......... .......... 57% 29.2M 20s
291550K .......... .......... .......... .......... .......... 57% 31.1M 20s
291600K .......... .......... .......... .......... .......... 57% 23.1M 20s
291650K .......... .......... .......... .......... .......... 57% 35.5M 20s
291700K .......... .......... .......... .......... .......... 57% 23.1M 20s
291750K .......... .......... .......... .......... .......... 57% 24.4M 19s
291800K .......... .......... .......... .......... .......... 57% 24.9M 19s
291850K .......... .......... .......... .......... .......... 57% 28.7M 19s
291900K .......... .......... .......... .......... .......... 57% 22.0M 19s
291950K .......... .......... .......... .......... .......... 57% 25.0M 19s
292000K .......... .......... .......... .......... .......... 57% 62.5M 19s
292050K .......... .......... .......... .......... .......... 57% 12.4M 19s
292100K .......... .......... .......... .......... .......... 57% 95.9M 19s
292150K .......... .......... .......... .......... .......... 57% 20.1M 19s
292200K .......... .......... .......... .......... .......... 57% 29.4M 19s
292250K .......... .......... .......... .......... .......... 57% 68.3M 19s
292300K .......... .......... .......... .......... .......... 57% 22.3M 19s
292350K .......... .......... .......... .......... .......... 57% 16.1M 19s
292400K .......... .......... .......... .......... .......... 57% 23.2M 19s
292450K .......... .......... .......... .......... .......... 57% 18.8M 19s
292500K .......... .......... .......... .......... .......... 57% 16.5M 19s
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292600K .......... .......... .......... .......... .......... 57% 16.4M 19s
292650K .......... .......... .......... .......... .......... 57% 21.3M 19s
292700K .......... .......... .......... .......... .......... 58% 19.5M 19s
292750K .......... .......... .......... .......... .......... 58% 22.0M 19s
292800K .......... .......... .......... .......... .......... 58% 23.2M 19s
292850K .......... .......... .......... .......... .......... 58% 19.7M 19s
292900K .......... .......... .......... .......... .......... 58% 18.2M 19s
292950K .......... .......... .......... .......... .......... 58% 17.5M 19s
293000K .......... .......... .......... .......... .......... 58% 24.8M 19s
293050K .......... .......... .......... .......... .......... 58% 27.4M 19s
293100K .......... .......... .......... .......... .......... 58% 14.9M 19s
293150K .......... .......... .......... .......... .......... 58% 15.3M 19s
293200K .......... .......... .......... .......... .......... 58% 32.4M 19s
293250K .......... .......... .......... .......... .......... 58% 17.1M 19s
293300K .......... .......... .......... .......... .......... 58% 29.9M 19s
293350K .......... .......... .......... .......... .......... 58% 22.4M 19s
293400K .......... .......... .......... .......... .......... 58% 23.5M 19s
293450K .......... .......... .......... .......... .......... 58% 18.5M 19s
293500K .......... .......... .......... .......... .......... 58% 25.0M 19s
293550K .......... .......... .......... .......... .......... 58% 27.2M 19s
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293700K .......... .......... .......... .......... .......... 58% 25.6M 19s
293750K .......... .......... .......... .......... .......... 58% 30.5M 19s
293800K .......... .......... .......... .......... .......... 58% 21.9M 19s
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293900K .......... .......... .......... .......... .......... 58% 22.7M 19s
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294000K .......... .......... .......... .......... .......... 58% 24.8M 19s
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294100K .......... .......... .......... .......... .......... 58% 23.6M 19s
294150K .......... .......... .......... .......... .......... 58% 23.8M 19s
294200K .......... .......... .......... .......... .......... 58% 36.0M 19s
294250K .......... .......... .......... .......... .......... 58% 36.9M 19s
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294350K .......... .......... .......... .......... .......... 58% 93.5M 19s
294400K .......... .......... .......... .......... .......... 58%  109M 19s
294450K .......... .......... .......... .......... .......... 58% 90.1M 19s
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294550K .......... .......... .......... .......... .......... 58%  115M 19s
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294650K .......... .......... .......... .......... .......... 58% 46.8M 19s
294700K .......... .......... .......... .......... .......... 58% 31.1M 19s
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294800K .......... .......... .......... .......... .......... 58% 48.9M 19s
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294900K .......... .......... .......... .......... .......... 58% 37.4M 19s
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295000K .......... .......... .......... .......... .......... 58% 32.2M 19s
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295100K .......... .......... .......... .......... .......... 58% 30.5M 19s
295150K .......... .......... .......... .......... .......... 58% 33.8M 19s
295200K .......... .......... .......... .......... .......... 58% 25.0M 19s
295250K .......... .......... .......... .......... .......... 58% 37.4M 19s
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295400K .......... .......... .......... .......... .......... 58% 33.7M 19s
295450K .......... .......... .......... .......... .......... 58% 26.7M 19s
295500K .......... .......... .......... .......... .......... 58% 31.2M 19s
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295750K .......... .......... .......... .......... .......... 58% 13.0M 19s
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295850K .......... .......... .......... .......... .......... 58% 9.65M 19s
295900K .......... .......... .......... .......... .......... 58% 12.2M 19s
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296000K .......... .......... .......... .......... .......... 58% 11.9M 19s
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296100K .......... .......... .......... .......... .......... 58% 10.6M 19s
296150K .......... .......... .......... .......... .......... 58% 17.8M 19s
296200K .......... .......... .......... .......... .......... 58% 14.0M 19s
296250K .......... .......... .......... .......... .......... 58% 8.49M 19s
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296550K .......... .......... .......... .......... .......... 58% 30.8M 19s
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297000K .......... .......... .......... .......... .......... 58% 33.7M 19s
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297100K .......... .......... .......... .......... .......... 58% 19.2M 19s
297150K .......... .......... .......... .......... .......... 58% 33.7M 19s
297200K .......... .......... .......... .......... .......... 58% 17.2M 19s
297250K .......... .......... .......... .......... .......... 58% 28.9M 19s
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299200K .......... .......... .......... .......... .......... 59% 6.10M 19s
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299500K .......... .......... .......... .......... .......... 59% 18.1M 19s
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301800K .......... .......... .......... .......... .......... 59% 17.9M 18s
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302150K .......... .......... .......... .......... .......... 59% 19.3M 18s
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303250K .......... .......... .......... .......... .......... 60% 14.4M 18s
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303500K .......... .......... .......... .......... .......... 60% 6.82M 18s
303550K .......... .......... .......... .......... .......... 60% 9.55M 18s
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303700K .......... .......... .......... .......... .......... 60% 10.2M 18s
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303800K .......... .......... .......... .......... .......... 60% 16.5M 18s
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304000K .......... .......... .......... .......... .......... 60% 11.8M 18s
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305100K .......... .......... .......... .......... .......... 60% 51.1M 18s
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305250K .......... .......... .......... .......... .......... 60% 31.9M 18s
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305750K .......... .......... .......... .......... .......... 60% 40.5M 18s
305800K .......... .......... .......... .......... .......... 60% 18.0M 18s
305850K .......... .......... .......... .......... .......... 60% 31.9M 18s
305900K .......... .......... .......... .......... .......... 60% 20.4M 18s
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306000K .......... .......... .......... .......... .......... 60% 41.3M 18s
306050K .......... .......... .......... .......... .......... 60% 33.5M 18s
306100K .......... .......... .......... .......... .......... 60% 24.9M 18s
306150K .......... .......... .......... .......... .......... 60% 27.0M 18s
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306250K .......... .......... .......... .......... .......... 60% 23.8M 18s
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306400K .......... .......... .......... .......... .......... 60% 33.9M 18s
306450K .......... .......... .......... .......... .......... 60% 21.2M 18s
306500K .......... .......... .......... .......... .......... 60% 19.3M 18s
306550K .......... .......... .......... .......... .......... 60% 24.0M 18s
306600K .......... .......... .......... .......... .......... 60% 15.4M 18s
306650K .......... .......... .......... .......... .......... 60% 18.7M 18s
306700K .......... .......... .......... .......... .......... 60% 17.1M 18s
306750K .......... .......... .......... .......... .......... 60% 19.0M 18s
306800K .......... .......... .......... .......... .......... 60% 18.8M 18s
306850K .......... .......... .......... .......... .......... 60% 19.7M 18s
306900K .......... .......... .......... .......... .......... 60% 20.7M 18s
306950K .......... .......... .......... .......... .......... 60% 16.3M 18s
307000K .......... .......... .......... .......... .......... 60% 18.6M 18s
307050K .......... .......... .......... .......... .......... 60% 18.1M 18s
307100K .......... .......... .......... .......... .......... 60% 13.0M 18s
307150K .......... .......... .......... .......... .......... 60% 15.0M 18s
307200K .......... .......... .......... .......... .......... 60% 12.5M 18s
307250K .......... .......... .......... .......... .......... 60% 20.8M 18s
307300K .......... .......... .......... .......... .......... 60% 17.0M 18s
307350K .......... .......... .......... .......... .......... 60% 11.4M 18s
307400K .......... .......... .......... .......... .......... 60% 19.8M 18s
307450K .......... .......... .......... .......... .......... 60% 15.1M 18s
307500K .......... .......... .......... .......... .......... 60% 14.9M 18s
307550K .......... .......... .......... .......... .......... 60% 15.9M 18s
307600K .......... .......... .......... .......... .......... 60% 15.7M 18s
307650K .......... .......... .......... .......... .......... 60% 20.1M 18s
307700K .......... .......... .......... .......... .......... 60% 14.3M 18s
307750K .......... .......... .......... .......... .......... 60% 24.9M 18s
307800K .......... .......... .......... .......... .......... 60% 16.3M 18s
307850K .......... .......... .......... .......... .......... 61% 10.5M 18s
307900K .......... .......... .......... .......... .......... 61% 10.9M 18s
307950K .......... .......... .......... .......... .......... 61% 8.70M 18s
308000K .......... .......... .......... .......... .......... 61% 10.2M 18s
308050K .......... .......... .......... .......... .......... 61% 9.96M 18s
308100K .......... .......... .......... .......... .......... 61% 8.24M 18s
308150K .......... .......... .......... .......... .......... 61% 10.2M 18s
308200K .......... .......... .......... .......... .......... 61% 9.46M 18s
308250K .......... .......... .......... .......... .......... 61% 9.21M 18s
308300K .......... .......... .......... .......... .......... 61% 9.91M 18s
308350K .......... .......... .......... .......... .......... 61% 18.8M 18s
308400K .......... .......... .......... .......... .......... 61% 15.1M 18s
308450K .......... .......... .......... .......... .......... 61% 14.0M 18s
308500K .......... .......... .......... .......... .......... 61% 11.7M 18s
308550K .......... .......... .......... .......... .......... 61% 15.4M 18s
308600K .......... .......... .......... .......... .......... 61% 15.7M 18s
308650K .......... .......... .......... .......... .......... 61% 15.7M 18s
308700K .......... .......... .......... .......... .......... 61% 17.1M 18s
308750K .......... .......... .......... .......... .......... 61% 19.8M 18s
308800K .......... .......... .......... .......... .......... 61% 19.0M 18s
308850K .......... .......... .......... .......... .......... 61% 14.9M 18s
308900K .......... .......... .......... .......... .......... 61% 17.0M 18s
308950K .......... .......... .......... .......... .......... 61% 15.1M 18s
309000K .......... .......... .......... .......... .......... 61% 18.9M 17s
309050K .......... .......... .......... .......... .......... 61% 18.7M 17s
309100K .......... .......... .......... .......... .......... 61% 17.7M 17s
309150K .......... .......... .......... .......... .......... 61% 17.8M 17s
309200K .......... .......... .......... .......... .......... 61% 18.5M 17s
309250K .......... .......... .......... .......... .......... 61% 19.0M 17s
309300K .......... .......... .......... .......... .......... 61% 20.6M 17s
309350K .......... .......... .......... .......... .......... 61% 23.9M 17s
309400K .......... .......... .......... .......... .......... 61% 19.6M 17s
309450K .......... .......... .......... .......... .......... 61% 21.8M 17s
309500K .......... .......... .......... .......... .......... 61% 16.5M 17s
309550K .......... .......... .......... .......... .......... 61% 34.2M 17s
309600K .......... .......... .......... .......... .......... 61% 18.7M 17s
309650K .......... .......... .......... .......... .......... 61% 21.6M 17s
309700K .......... .......... .......... .......... .......... 61% 21.1M 17s
309750K .......... .......... .......... .......... .......... 61% 16.3M 17s
309800K .......... .......... .......... .......... .......... 61% 24.9M 17s
309850K .......... .......... .......... .......... .......... 61% 20.9M 17s
309900K .......... .......... .......... .......... .......... 61% 19.4M 17s
309950K .......... .......... .......... .......... .......... 61% 21.0M 17s
310000K .......... .......... .......... .......... .......... 61% 18.7M 17s
310050K .......... .......... .......... .......... .......... 61% 21.0M 17s
310100K .......... .......... .......... .......... .......... 61% 17.3M 17s
310150K .......... .......... .......... .......... .......... 61% 27.2M 17s
310200K .......... .......... .......... .......... .......... 61% 14.9M 17s
310250K .......... .......... .......... .......... .......... 61% 80.7M 17s
310300K .......... .......... .......... .......... .......... 61% 40.1M 17s
310350K .......... .......... .......... .......... .......... 61% 23.4M 17s
310400K .......... .......... .......... .......... .......... 61% 51.2M 17s
310450K .......... .......... .......... .......... .......... 61% 17.1M 17s
310500K .......... .......... .......... .......... .......... 61% 20.5M 17s
310550K .......... .......... .......... .......... .......... 61% 19.5M 17s
310600K .......... .......... .......... .......... .......... 61% 20.8M 17s
310650K .......... .......... .......... .......... .......... 61% 17.1M 17s
310700K .......... .......... .......... .......... .......... 61% 22.1M 17s
310750K .......... .......... .......... .......... .......... 61% 21.8M 17s
310800K .......... .......... .......... .......... .......... 61% 22.2M 17s
310850K .......... .......... .......... .......... .......... 61% 18.7M 17s
310900K .......... .......... .......... .......... .......... 61% 21.1M 17s
310950K .......... .......... .......... .......... .......... 61% 19.9M 17s
311000K .......... .......... .......... .......... .......... 61% 21.8M 17s
311050K .......... .......... .......... .......... .......... 61% 20.7M 17s
311100K .......... .......... .......... .......... .......... 61% 18.5M 17s
311150K .......... .......... .......... .......... .......... 61% 24.5M 17s
311200K .......... .......... .......... .......... .......... 61% 26.1M 17s
311250K .......... .......... .......... .......... .......... 61% 13.2M 17s
311300K .......... .......... .......... .......... .......... 61% 86.7M 17s
311350K .......... .......... .......... .......... .......... 61% 15.3M 17s
311400K .......... .......... .......... .......... .......... 61% 31.0M 17s
311450K .......... .......... .......... .......... .......... 61% 17.8M 17s
311500K .......... .......... .......... .......... .......... 61% 26.4M 17s
311550K .......... .......... .......... .......... .......... 61% 23.9M 17s
311600K .......... .......... .......... .......... .......... 61% 20.5M 17s
311650K .......... .......... .......... .......... .......... 61% 20.0M 17s
311700K .......... .......... .......... .......... .......... 61% 16.8M 17s
311750K .......... .......... .......... .......... .......... 61% 21.9M 17s
311800K .......... .......... .......... .......... .......... 61% 20.9M 17s
311850K .......... .......... .......... .......... .......... 61% 17.0M 17s
311900K .......... .......... .......... .......... .......... 61% 28.7M 17s
311950K .......... .......... .......... .......... .......... 61% 17.8M 17s
312000K .......... .......... .......... .......... .......... 61% 22.0M 17s
312050K .......... .......... .......... .......... .......... 61% 21.0M 17s
312100K .......... .......... .......... .......... .......... 61% 17.9M 17s
312150K .......... .......... .......... .......... .......... 61% 22.3M 17s
312200K .......... .......... .......... .......... .......... 61% 10.1M 17s
312250K .......... .......... .......... .......... .......... 61% 93.4M 17s
312300K .......... .......... .......... .......... .......... 61% 43.9M 17s
312350K .......... .......... .......... .......... .......... 61% 18.3M 17s
312400K .......... .......... .......... .......... .......... 61% 19.3M 17s
312450K .......... .......... .......... .......... .......... 61% 15.4M 17s
312500K .......... .......... .......... .......... .......... 61% 18.6M 17s
312550K .......... .......... .......... .......... .......... 61% 21.9M 17s
312600K .......... .......... .......... .......... .......... 61% 19.6M 17s
312650K .......... .......... .......... .......... .......... 61% 19.6M 17s
312700K .......... .......... .......... .......... .......... 61% 17.8M 17s
312750K .......... .......... .......... .......... .......... 61% 19.6M 17s
312800K .......... .......... .......... .......... .......... 61% 23.4M 17s
312850K .......... .......... .......... .......... .......... 61% 17.3M 17s
312900K .......... .......... .......... .......... .......... 62% 16.1M 17s
312950K .......... .......... .......... .......... .......... 62% 21.1M 17s
313000K .......... .......... .......... .......... .......... 62% 20.7M 17s
313050K .......... .......... .......... .......... .......... 62% 24.7M 17s
313100K .......... .......... .......... .......... .......... 62% 16.3M 17s
313150K .......... .......... .......... .......... .......... 62% 22.4M 17s
313200K .......... .......... .......... .......... .......... 62% 19.4M 17s
313250K .......... .......... .......... .......... .......... 62% 20.8M 17s
313300K .......... .......... .......... .......... .......... 62% 20.9M 17s
313350K .......... .......... .......... .......... .......... 62% 23.6M 17s
313400K .......... .......... .......... .......... .......... 62% 17.6M 17s
313450K .......... .......... .......... .......... .......... 62% 13.0M 17s
313500K .......... .......... .......... .......... .......... 62% 8.24M 17s
313550K .......... .......... .......... .......... .......... 62% 15.2M 17s
313600K .......... .......... .......... .......... .......... 62% 11.8M 17s
313650K .......... .......... .......... .......... .......... 62% 14.4M 17s
313700K .......... .......... .......... .......... .......... 62% 12.5M 17s
313750K .......... .......... .......... .......... .......... 62% 13.0M 17s
313800K .......... .......... .......... .......... .......... 62% 13.5M 17s
313850K .......... .......... .......... .......... .......... 62% 13.5M 17s
313900K .......... .......... .......... .......... .......... 62% 13.0M 17s
313950K .......... .......... .......... .......... .......... 62% 12.1M 17s
314000K .......... .......... .......... .......... .......... 62% 16.7M 17s
314050K .......... .......... .......... .......... .......... 62% 15.0M 17s
314100K .......... .......... .......... .......... .......... 62% 51.6M 17s
314150K .......... .......... .......... .......... .......... 62% 18.7M 17s
314200K .......... .......... .......... .......... .......... 62% 17.7M 17s
314250K .......... .......... .......... .......... .......... 62% 18.0M 17s
314300K .......... .......... .......... .......... .......... 62% 14.2M 17s
314350K .......... .......... .......... .......... .......... 62% 17.2M 17s
314400K .......... .......... .......... .......... .......... 62% 14.0M 17s
314450K .......... .......... .......... .......... .......... 62% 14.5M 17s
314500K .......... .......... .......... .......... .......... 62% 16.2M 17s
314550K .......... .......... .......... .......... .......... 62% 17.9M 17s
314600K .......... .......... .......... .......... .......... 62% 15.0M 17s
314650K .......... .......... .......... .......... .......... 62% 16.4M 17s
314700K .......... .......... .......... .......... .......... 62% 16.4M 17s
314750K .......... .......... .......... .......... .......... 62% 15.9M 17s
314800K .......... .......... .......... .......... .......... 62% 16.7M 17s
314850K .......... .......... .......... .......... .......... 62% 13.4M 17s
314900K .......... .......... .......... .......... .......... 62% 25.3M 17s
314950K .......... .......... .......... .......... .......... 62% 11.0M 17s
315000K .......... .......... .......... .......... .......... 62% 58.1M 17s
315050K .......... .......... .......... .......... .......... 62% 23.1M 17s
315100K .......... .......... .......... .......... .......... 62% 16.7M 17s
315150K .......... .......... .......... .......... .......... 62% 25.0M 17s
315200K .......... .......... .......... .......... .......... 62% 20.8M 17s
315250K .......... .......... .......... .......... .......... 62% 31.6M 17s
315300K .......... .......... .......... .......... .......... 62% 21.9M 17s
315350K .......... .......... .......... .......... .......... 62% 24.9M 17s
315400K .......... .......... .......... .......... .......... 62% 23.8M 17s
315450K .......... .......... .......... .......... .......... 62% 18.5M 17s
315500K .......... .......... .......... .......... .......... 62% 25.1M 17s
315550K .......... .......... .......... .......... .......... 62% 26.9M 17s
315600K .......... .......... .......... .......... .......... 62% 20.9M 17s
315650K .......... .......... .......... .......... .......... 62% 29.7M 17s
315700K .......... .......... .......... .......... .......... 62% 25.7M 17s
315750K .......... .......... .......... .......... .......... 62% 22.6M 17s
315800K .......... .......... .......... .......... .......... 62% 24.3M 17s
315850K .......... .......... .......... .......... .......... 62% 19.6M 17s
315900K .......... .......... .......... .......... .......... 62% 28.6M 17s
315950K .......... .......... .......... .......... .......... 62% 23.5M 17s
316000K .......... .......... .......... .......... .......... 62% 23.1M 17s
316050K .......... .......... .......... .......... .......... 62% 28.7M 17s
316100K .......... .......... .......... .......... .......... 62% 45.7M 17s
316150K .......... .......... .......... .......... .......... 62% 23.5M 17s
316200K .......... .......... .......... .......... .......... 62% 14.6M 17s
316250K .......... .......... .......... .......... .......... 62% 85.5M 17s
316300K .......... .......... .......... .......... .......... 62% 33.2M 17s
316350K .......... .......... .......... .......... .......... 62% 15.6M 17s
316400K .......... .......... .......... .......... .......... 62% 31.9M 17s
316450K .......... .......... .......... .......... .......... 62% 21.2M 17s
316500K .......... .......... .......... .......... .......... 62% 37.1M 17s
316550K .......... .......... .......... .......... .......... 62% 23.3M 17s
316600K .......... .......... .......... .......... .......... 62% 20.6M 17s
316650K .......... .......... .......... .......... .......... 62% 23.4M 17s
316700K .......... .......... .......... .......... .......... 62% 18.7M 17s
316750K .......... .......... .......... .......... .......... 62% 20.8M 17s
316800K .......... .......... .......... .......... .......... 62% 22.0M 17s
316850K .......... .......... .......... .......... .......... 62% 22.0M 17s
316900K .......... .......... .......... .......... .......... 62% 26.8M 17s
316950K .......... .......... .......... .......... .......... 62% 18.8M 17s
317000K .......... .......... .......... .......... .......... 62% 24.6M 17s
317050K .......... .......... .......... .......... .......... 62% 24.8M 17s
317100K .......... .......... .......... .......... .......... 62% 21.0M 17s
317150K .......... .......... .......... .......... .......... 62% 24.9M 17s
317200K .......... .......... .......... .......... .......... 62% 21.2M 17s
317250K .......... .......... .......... .......... .......... 62% 28.4M 17s
317300K .......... .......... .......... .......... .......... 62% 28.1M 17s
317350K .......... .......... .......... .......... .......... 62% 14.5M 17s
317400K .......... .......... .......... .......... .......... 62% 89.8M 17s
317450K .......... .......... .......... .......... .......... 62% 10.6M 17s
317500K .......... .......... .......... .......... .......... 62%  103M 17s
317550K .......... .......... .......... .......... .......... 62% 25.6M 17s
317600K .......... .......... .......... .......... .......... 62% 32.0M 17s
317650K .......... .......... .......... .......... .......... 62% 34.0M 17s
317700K .......... .......... .......... .......... .......... 62% 16.2M 17s
317750K .......... .......... .......... .......... .......... 62% 37.2M 17s
317800K .......... .......... .......... .......... .......... 62% 23.4M 16s
317850K .......... .......... .......... .......... .......... 62% 17.0M 16s
317900K .......... .......... .......... .......... .......... 63% 37.4M 16s
317950K .......... .......... .......... .......... .......... 63% 18.4M 16s
318000K .......... .......... .......... .......... .......... 63% 18.3M 16s
318050K .......... .......... .......... .......... .......... 63% 31.1M 16s
318100K .......... .......... .......... .......... .......... 63% 19.6M 16s
318150K .......... .......... .......... .......... .......... 63% 27.3M 16s
318200K .......... .......... .......... .......... .......... 63% 21.7M 16s
318250K .......... .......... .......... .......... .......... 63% 31.0M 16s
318300K .......... .......... .......... .......... .......... 63% 23.5M 16s
318350K .......... .......... .......... .......... .......... 63% 17.8M 16s
318400K .......... .......... .......... .......... .......... 63% 22.0M 16s
318450K .......... .......... .......... .......... .......... 63% 20.2M 16s
318500K .......... .......... .......... .......... .......... 63% 16.5M 16s
318550K .......... .......... .......... .......... .......... 63% 12.4M 16s
318600K .......... .......... .......... .......... .......... 63% 17.7M 16s
318650K .......... .......... .......... .......... .......... 63% 15.6M 16s
318700K .......... .......... .......... .......... .......... 63% 17.1M 16s
318750K .......... .......... .......... .......... .......... 63% 20.7M 16s
318800K .......... .......... .......... .......... .......... 63% 18.8M 16s
318850K .......... .......... .......... .......... .......... 63% 16.9M 16s
318900K .......... .......... .......... .......... .......... 63% 19.8M 16s
318950K .......... .......... .......... .......... .......... 63% 13.4M 16s
319000K .......... .......... .......... .......... .......... 63% 18.8M 16s
319050K .......... .......... .......... .......... .......... 63% 20.9M 16s
319100K .......... .......... .......... .......... .......... 63% 14.5M 16s
319150K .......... .......... .......... .......... .......... 63% 18.7M 16s
319200K .......... .......... .......... .......... .......... 63% 22.1M 16s
319250K .......... .......... .......... .......... .......... 63% 26.5M 16s
319300K .......... .......... .......... .......... .......... 63% 41.6M 16s
319350K .......... .......... .......... .......... .......... 63% 11.5M 16s
319400K .......... .......... .......... .......... .......... 63%  102M 16s
319450K .......... .......... .......... .......... .......... 63% 19.8M 16s
319500K .......... .......... .......... .......... .......... 63% 76.3M 16s
319550K .......... .......... .......... .......... .......... 63% 23.6M 16s
319600K .......... .......... .......... .......... .......... 63% 16.2M 16s
319650K .......... .......... .......... .......... .......... 63% 20.8M 16s
319700K .......... .......... .......... .......... .......... 63% 20.8M 16s
319750K .......... .......... .......... .......... .......... 63% 19.7M 16s
319800K .......... .......... .......... .......... .......... 63% 25.1M 16s
319850K .......... .......... .......... .......... .......... 63% 16.9M 16s
319900K .......... .......... .......... .......... .......... 63% 15.0M 16s
319950K .......... .......... .......... .......... .......... 63% 18.7M 16s
320000K .......... .......... .......... .......... .......... 63% 22.0M 16s
320050K .......... .......... .......... .......... .......... 63% 21.0M 16s
320100K .......... .......... .......... .......... .......... 63% 17.8M 16s
320150K .......... .......... .......... .......... .......... 63% 23.2M 16s
320200K .......... .......... .......... .......... .......... 63% 19.7M 16s
320250K .......... .......... .......... .......... .......... 63% 17.0M 16s
320300K .......... .......... .......... .......... .......... 63% 20.9M 16s
320350K .......... .......... .......... .......... .......... 63% 11.8M 16s
320400K .......... .......... .......... .......... .......... 63%  102M 16s
320450K .......... .......... .......... .......... .......... 63% 11.3M 16s
320500K .......... .......... .......... .......... .......... 63% 31.4M 16s
320550K .......... .......... .......... .......... .......... 63% 18.7M 16s
320600K .......... .......... .......... .......... .......... 63% 14.3M 16s
320650K .......... .......... .......... .......... .......... 63% 23.4M 16s
320700K .......... .......... .......... .......... .......... 63% 18.5M 16s
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334850K .......... .......... .......... .......... .......... 66% 13.3M 15s
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334950K .......... .......... .......... .......... .......... 66% 17.0M 15s
335000K .......... .......... .......... .......... .......... 66% 18.8M 15s
335050K .......... .......... .......... .......... .......... 66% 19.8M 15s
335100K .......... .......... .......... .......... .......... 66% 17.1M 15s
335150K .......... .......... .......... .......... .......... 66% 13.5M 15s
335200K .......... .......... .......... .......... .......... 66% 12.2M 15s
335250K .......... .......... .......... .......... .......... 66% 14.3M 15s
335300K .......... .......... .......... .......... .......... 66% 11.1M 15s
335350K .......... .......... .......... .......... .......... 66% 7.42M 15s
335400K .......... .......... .......... .......... .......... 66% 13.0M 15s
335450K .......... .......... .......... .......... .......... 66% 10.4M 15s
335500K .......... .......... .......... .......... .......... 66% 15.8M 15s
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335600K .......... .......... .......... .......... .......... 66% 12.2M 15s
335650K .......... .......... .......... .......... .......... 66% 14.4M 15s
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335750K .......... .......... .......... .......... .......... 66% 17.7M 15s
335800K .......... .......... .......... .......... .......... 66% 15.8M 15s
335850K .......... .......... .......... .......... .......... 66% 12.0M 15s
335900K .......... .......... .......... .......... .......... 66% 16.5M 15s
335950K .......... .......... .......... .......... .......... 66% 9.33M 15s
336000K .......... .......... .......... .......... .......... 66% 16.2M 15s
336050K .......... .......... .......... .......... .......... 66% 13.9M 15s
336100K .......... .......... .......... .......... .......... 66% 10.5M 15s
336150K .......... .......... .......... .......... .......... 66% 19.9M 15s
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336250K .......... .......... .......... .......... .......... 66% 15.6M 15s
336300K .......... .......... .......... .......... .......... 66% 17.4M 15s
336350K .......... .......... .......... .......... .......... 66% 14.9M 15s
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336450K .......... .......... .......... .......... .......... 66% 18.0M 15s
336500K .......... .......... .......... .......... .......... 66% 15.6M 15s
336550K .......... .......... .......... .......... .......... 66% 20.9M 14s
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336900K .......... .......... .......... .......... .......... 66% 76.7M 14s
336950K .......... .......... .......... .......... .......... 66% 13.8M 14s
337000K .......... .......... .......... .......... .......... 66% 31.0M 14s
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337100K .......... .......... .......... .......... .......... 66% 14.4M 14s
337150K .......... .......... .......... .......... .......... 66% 18.8M 14s
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337250K .......... .......... .......... .......... .......... 66% 20.0M 14s
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338100K .......... .......... .......... .......... .......... 67% 23.6M 14s
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338250K .......... .......... .......... .......... .......... 67% 21.0M 14s
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339100K .......... .......... .......... .......... .......... 67% 11.1M 14s
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339250K .......... .......... .......... .......... .......... 67% 28.6M 14s
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346250K .......... .......... .......... .......... .......... 68% 15.1M 14s
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346500K .......... .......... .......... .......... .......... 68% 19.1M 14s
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347000K .......... .......... .......... .......... .......... 68% 15.0M 13s
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347250K .......... .......... .......... .......... .......... 68% 27.1M 13s
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347900K .......... .......... .......... .......... .......... 68% 27.5M 13s
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348000K .......... .......... .......... .......... .......... 68% 29.3M 13s
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348100K .......... .......... .......... .......... .......... 68% 32.9M 13s
348150K .......... .......... .......... .......... .......... 68% 9.96M 13s
348200K .......... .......... .......... .......... .......... 69% 7.84M 13s
348250K .......... .......... .......... .......... .......... 69% 10.8M 13s
348300K .......... .......... .......... .......... .......... 69% 11.5M 13s
348350K .......... .......... .......... .......... .......... 69% 6.31M 13s
348400K .......... .......... .......... .......... .......... 69% 17.1M 13s
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348550K .......... .......... .......... .......... .......... 69% 11.5M 13s
348600K .......... .......... .......... .......... .......... 69% 8.72M 13s
348650K .......... .......... .......... .......... .......... 69% 7.04M 13s
348700K .......... .......... .......... .......... .......... 69% 6.54M 13s
348750K .......... .......... .......... .......... .......... 69% 14.5M 13s
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348850K .......... .......... .......... .......... .......... 69% 55.6M 13s
348900K .......... .......... .......... .......... .......... 69% 78.5M 13s
348950K .......... .......... .......... .......... .......... 69% 22.2M 13s
349000K .......... .......... .......... .......... .......... 69% 25.3M 13s
349050K .......... .......... .......... .......... .......... 69% 23.6M 13s
349100K .......... .......... .......... .......... .......... 69% 23.3M 13s
349150K .......... .......... .......... .......... .......... 69% 37.2M 13s
349200K .......... .......... .......... .......... .......... 69% 22.3M 13s
349250K .......... .......... .......... .......... .......... 69% 23.6M 13s
349300K .......... .......... .......... .......... .......... 69% 40.7M 13s
349350K .......... .......... .......... .......... .......... 69% 21.3M 13s
349400K .......... .......... .......... .......... .......... 69% 23.5M 13s
349450K .......... .......... .......... .......... .......... 69% 17.2M 13s
349500K .......... .......... .......... .......... .......... 69% 43.9M 13s
349550K .......... .......... .......... .......... .......... 69% 19.7M 13s
349600K .......... .......... .......... .......... .......... 69% 19.8M 13s
349650K .......... .......... .......... .......... .......... 69% 18.6M 13s
349700K .......... .......... .......... .......... .......... 69% 20.8M 13s
349750K .......... .......... .......... .......... .......... 69% 25.1M 13s
349800K .......... .......... .......... .......... .......... 69% 19.7M 13s
349850K .......... .......... .......... .......... .......... 69% 12.6M 13s
349900K .......... .......... .......... .......... .......... 69% 9.43M 13s
349950K .......... .......... .......... .......... .......... 69% 42.2M 13s
350000K .......... .......... .......... .......... .......... 69% 12.6M 13s
350050K .......... .......... .......... .......... .......... 69% 9.13M 13s
350100K .......... .......... .......... .......... .......... 69% 8.55M 13s
350150K .......... .......... .......... .......... .......... 69% 11.4M 13s
350200K .......... .......... .......... .......... .......... 69% 8.23M 13s
350250K .......... .......... .......... .......... .......... 69% 10.4M 13s
350300K .......... .......... .......... .......... .......... 69% 9.43M 13s
350350K .......... .......... .......... .......... .......... 69% 9.00M 13s
350400K .......... .......... .......... .......... .......... 69% 10.8M 13s
350450K .......... .......... .......... .......... .......... 69% 16.5M 13s
350500K .......... .......... .......... .......... .......... 69% 20.6M 13s
350550K .......... .......... .......... .......... .......... 69% 11.1M 13s
350600K .......... .......... .......... .......... .......... 69% 33.8M 13s
350650K .......... .......... .......... .......... .......... 69% 15.8M 13s
350700K .......... .......... .......... .......... .......... 69% 13.6M 13s
350750K .......... .......... .......... .......... .......... 69% 49.2M 13s
350800K .......... .......... .......... .......... .......... 69% 20.6M 13s
350850K .......... .......... .......... .......... .......... 69% 15.7M 13s
350900K .......... .......... .......... .......... .......... 69% 17.9M 13s
350950K .......... .......... .......... .......... .......... 69% 15.6M 13s
351000K .......... .......... .......... .......... .......... 69% 18.9M 13s
351050K .......... .......... .......... .......... .......... 69% 23.5M 13s
351100K .......... .......... .......... .......... .......... 69% 14.9M 13s
351150K .......... .......... .......... .......... .......... 69% 17.0M 13s
351200K .......... .......... .......... .......... .......... 69% 17.2M 13s
351250K .......... .......... .......... .......... .......... 69% 17.9M 13s
351300K .......... .......... .......... .......... .......... 69% 17.8M 13s
351350K .......... .......... .......... .......... .......... 69% 18.9M 13s
351400K .......... .......... .......... .......... .......... 69% 22.9M 13s
351450K .......... .......... .......... .......... .......... 69% 24.3M 13s
351500K .......... .......... .......... .......... .......... 69% 9.11M 13s
351550K .......... .......... .......... .......... .......... 69% 58.1M 13s
351600K .......... .......... .......... .......... .......... 69% 22.7M 13s
351650K .......... .......... .......... .......... .......... 69% 34.0M 13s
351700K .......... .......... .......... .......... .......... 69% 33.7M 13s
351750K .......... .......... .......... .......... .......... 69% 31.0M 13s
351800K .......... .......... .......... .......... .......... 69% 26.1M 13s
351850K .......... .......... .......... .......... .......... 69% 31.6M 13s
351900K .......... .......... .......... .......... .......... 69% 31.1M 13s
351950K .......... .......... .......... .......... .......... 69% 26.2M 13s
352000K .......... .......... .......... .......... .......... 69% 31.0M 13s
352050K .......... .......... .......... .......... .......... 69% 29.4M 13s
352100K .......... .......... .......... .......... .......... 69% 24.6M 13s
352150K .......... .......... .......... .......... .......... 69% 34.0M 13s
352200K .......... .......... .......... .......... .......... 69% 25.0M 13s
352250K .......... .......... .......... .......... .......... 69% 47.1M 13s
352300K .......... .......... .......... .......... .......... 69% 24.9M 13s
352350K .......... .......... .......... .......... .......... 69% 29.2M 13s
352400K .......... .......... .......... .......... .......... 69% 39.6M 13s
352450K .......... .......... .......... .......... .......... 69% 19.6M 13s
352500K .......... .......... .......... .......... .......... 69% 33.7M 13s
352550K .......... .......... .......... .......... .......... 69% 29.5M 13s
352600K .......... .......... .......... .......... .......... 69% 24.7M 13s
352650K .......... .......... .......... .......... .......... 69% 34.1M 13s
352700K .......... .......... .......... .......... .......... 69% 24.8M 13s
352750K .......... .......... .......... .......... .......... 69% 15.5M 13s
352800K .......... .......... .......... .......... .......... 69%  107M 13s
352850K .......... .......... .......... .......... .......... 69% 91.4M 13s
352900K .......... .......... .......... .......... .......... 69% 29.6M 13s
352950K .......... .......... .......... .......... .......... 69% 49.3M 13s
353000K .......... .......... .......... .......... .......... 69% 46.2M 13s
353050K .......... .......... .......... .......... .......... 69% 20.3M 13s
353100K .......... .......... .......... .......... .......... 69% 42.3M 13s
353150K .......... .......... .......... .......... .......... 69% 66.3M 13s
353200K .......... .......... .......... .......... .......... 69% 16.8M 13s
353250K .......... .......... .......... .......... .......... 70% 70.3M 13s
353300K .......... .......... .......... .......... .......... 70% 24.7M 13s
353350K .......... .......... .......... .......... .......... 70% 25.2M 13s
353400K .......... .......... .......... .......... .......... 70% 29.8M 13s
353450K .......... .......... .......... .......... .......... 70% 28.6M 13s
353500K .......... .......... .......... .......... .......... 70% 25.1M 13s
353550K .......... .......... .......... .......... .......... 70% 31.1M 13s
353600K .......... .......... .......... .......... .......... 70% 21.9M 13s
353650K .......... .......... .......... .......... .......... 70% 28.6M 13s
353700K .......... .......... .......... .......... .......... 70% 24.9M 13s
353750K .......... .......... .......... .......... .......... 70% 41.6M 13s
353800K .......... .......... .......... .......... .......... 70% 28.7M 13s
353850K .......... .......... .......... .......... .......... 70% 27.4M 13s
353900K .......... .......... .......... .......... .......... 70% 30.2M 13s
353950K .......... .......... .......... .......... .......... 70% 22.2M 13s
354000K .......... .......... .......... .......... .......... 70% 21.9M 13s
354050K .......... .......... .......... .......... .......... 70% 34.3M 13s
354100K .......... .......... .......... .......... .......... 70% 17.8M 13s
354150K .......... .......... .......... .......... .......... 70% 20.8M 13s
354200K .......... .......... .......... .......... .......... 70% 21.1M 13s
354250K .......... .......... .......... .......... .......... 70% 20.5M 13s
354300K .......... .......... .......... .......... .......... 70%  103M 13s
354350K .......... .......... .......... .......... .......... 70% 30.8M 13s
354400K .......... .......... .......... .......... .......... 70% 41.4M 13s
354450K .......... .......... .......... .......... .......... 70% 37.1M 13s
354500K .......... .......... .......... .......... .......... 70% 47.0M 13s
354550K .......... .......... .......... .......... .......... 70% 37.7M 13s
354600K .......... .......... .......... .......... .......... 70% 44.5M 13s
354650K .......... .......... .......... .......... .......... 70% 35.2M 13s
354700K .......... .......... .......... .......... .......... 70% 20.3M 13s
354750K .......... .......... .......... .......... .......... 70% 52.7M 13s
354800K .......... .......... .......... .......... .......... 70% 50.6M 13s
354850K .......... .......... .......... .......... .......... 70% 25.0M 13s
354900K .......... .......... .......... .......... .......... 70% 33.5M 13s
354950K .......... .......... .......... .......... .......... 70% 31.3M 13s
355000K .......... .......... .......... .......... .......... 70% 33.7M 13s
355050K .......... .......... .......... .......... .......... 70% 41.3M 13s
355100K .......... .......... .......... .......... .......... 70% 24.9M 13s
355150K .......... .......... .......... .......... .......... 70% 30.7M 13s
355200K .......... .......... .......... .......... .......... 70% 37.5M 13s
355250K .......... .......... .......... .......... .......... 70% 31.4M 13s
355300K .......... .......... .......... .......... .......... 70% 31.4M 13s
355350K .......... .......... .......... .......... .......... 70% 29.1M 13s
355400K .......... .......... .......... .......... .......... 70% 31.9M 13s
355450K .......... .......... .......... .......... .......... 70% 22.7M 13s
355500K .......... .......... .......... .......... .......... 70% 34.0M 13s
355550K .......... .......... .......... .......... .......... 70% 18.9M 13s
355600K .......... .......... .......... .......... .......... 70% 15.3M 13s
355650K .......... .......... .......... .......... .......... 70% 18.8M 13s
355700K .......... .......... .......... .......... .......... 70% 20.7M 13s
355750K .......... .......... .......... .......... .......... 70% 20.8M 13s
355800K .......... .......... .......... .......... .......... 70% 19.8M 13s
355850K .......... .......... .......... .......... .......... 70% 24.8M 13s
355900K .......... .......... .......... .......... .......... 70% 19.2M 13s
355950K .......... .......... .......... .......... .......... 70% 23.3M 13s
356000K .......... .......... .......... .......... .......... 70% 24.2M 13s
356050K .......... .......... .......... .......... .......... 70% 26.2M 13s
356100K .......... .......... .......... .......... .......... 70% 20.1M 13s
356150K .......... .......... .......... .......... .......... 70% 23.6M 13s
356200K .......... .......... .......... .......... .......... 70% 18.4M 13s
356250K .......... .......... .......... .......... .......... 70% 25.0M 13s
356300K .......... .......... .......... .......... .......... 70% 29.4M 13s
356350K .......... .......... .......... .......... .......... 70% 17.0M 13s
356400K .......... .......... .......... .......... .......... 70% 25.9M 13s
356450K .......... .......... .......... .......... .......... 70% 18.5M 13s
356500K .......... .......... .......... .......... .......... 70% 28.8M 12s
356550K .......... .......... .......... .......... .......... 70% 37.8M 12s
356600K .......... .......... .......... .......... .......... 70% 14.1M 12s
356650K .......... .......... .......... .......... .......... 70% 39.4M 12s
356700K .......... .......... .......... .......... .......... 70% 10.0M 12s
356750K .......... .......... .......... .......... .......... 70% 99.2M 12s
356800K .......... .......... .......... .......... .......... 70% 59.4M 12s
356850K .......... .......... .......... .......... .......... 70% 17.3M 12s
356900K .......... .......... .......... .......... .......... 70% 12.6M 12s
356950K .......... .......... .......... .......... .......... 70% 10.7M 12s
357000K .......... .......... .......... .......... .......... 70% 41.9M 12s
357050K .......... .......... .......... .......... .......... 70% 23.7M 12s
357100K .......... .......... .......... .......... .......... 70% 13.5M 12s
357150K .......... .......... .......... .......... .......... 70% 14.1M 12s
357200K .......... .......... .......... .......... .......... 70% 18.9M 12s
357250K .......... .......... .......... .......... .......... 70% 15.1M 12s
357300K .......... .......... .......... .......... .......... 70% 20.8M 12s
357350K .......... .......... .......... .......... .......... 70% 13.7M 12s
357400K .......... .......... .......... .......... .......... 70% 17.8M 12s
357450K .......... .......... .......... .......... .......... 70% 12.2M 12s
357500K .......... .......... .......... .......... .......... 70% 18.8M 12s
357550K .......... .......... .......... .......... .......... 70% 13.6M 12s
357600K .......... .......... .......... .......... .......... 70% 26.3M 12s
357650K .......... .......... .......... .......... .......... 70% 24.5M 12s
357700K .......... .......... .......... .......... .......... 70% 20.5M 12s
357750K .......... .......... .......... .......... .......... 70% 13.7M 12s
357800K .......... .......... .......... .......... .......... 70% 78.5M 12s
357850K .......... .......... .......... .......... .......... 70% 12.4M 12s
357900K .......... .......... .......... .......... .......... 70% 16.8M 12s
357950K .......... .......... .......... .......... .......... 70% 34.7M 12s
358000K .......... .......... .......... .......... .......... 70% 17.0M 12s
358050K .......... .......... .......... .......... .......... 70% 17.0M 12s
358100K .......... .......... .......... .......... .......... 70% 16.3M 12s
358150K .......... .......... .......... .......... .......... 70% 16.0M 12s
358200K .......... .......... .......... .......... .......... 70% 13.5M 12s
358250K .......... .......... .......... .......... .......... 70% 13.0M 12s
358300K .......... .......... .......... .......... .......... 71% 15.8M 12s
358350K .......... .......... .......... .......... .......... 71% 16.4M 12s
358400K .......... .......... .......... .......... .......... 71% 17.1M 12s
358450K .......... .......... .......... .......... .......... 71% 7.90M 12s
358500K .......... .......... .......... .......... .......... 71% 13.6M 12s
358550K .......... .......... .......... .......... .......... 71% 26.9M 12s
358600K .......... .......... .......... .......... .......... 71% 20.8M 12s
358650K .......... .......... .......... .......... .......... 71% 12.1M 12s
358700K .......... .......... .......... .......... .......... 71% 74.9M 12s
358750K .......... .......... .......... .......... .......... 71% 81.8M 12s
358800K .......... .......... .......... .......... .......... 71% 22.4M 12s
358850K .......... .......... .......... .......... .......... 71% 59.2M 12s
358900K .......... .......... .......... .......... .......... 71% 20.1M 12s
358950K .......... .......... .......... .......... .......... 71% 52.2M 12s
359000K .......... .......... .......... .......... .......... 71% 23.5M 12s
359050K .......... .......... .......... .......... .......... 71% 22.9M 12s
359100K .......... .......... .......... .......... .......... 71% 20.8M 12s
359150K .......... .......... .......... .......... .......... 71% 21.2M 12s
359200K .......... .......... .......... .......... .......... 71% 24.4M 12s
359250K .......... .......... .......... .......... .......... 71% 18.1M 12s
359300K .......... .......... .......... .......... .......... 71% 27.7M 12s
359350K .......... .......... .......... .......... .......... 71% 22.7M 12s
359400K .......... .......... .......... .......... .......... 71% 31.5M 12s
359450K .......... .......... .......... .......... .......... 71% 38.6M 12s
359500K .......... .......... .......... .......... .......... 71% 30.6M 12s
359550K .......... .......... .......... .......... .......... 71% 26.6M 12s
359600K .......... .......... .......... .......... .......... 71% 23.5M 12s
359650K .......... .......... .......... .......... .......... 71% 35.5M 12s
359700K .......... .......... .......... .......... .......... 71% 26.0M 12s
359750K .......... .......... .......... .......... .......... 71% 23.0M 12s
359800K .......... .......... .......... .......... .......... 71% 34.1M 12s
359850K .......... .......... .......... .......... .......... 71% 26.7M 12s
359900K .......... .......... .......... .......... .......... 71% 30.9M 12s
359950K .......... .......... .......... .......... .......... 71% 24.9M 12s
360000K .......... .......... .......... .......... .......... 71% 32.5M 12s
360050K .......... .......... .......... .......... .......... 71% 24.3M 12s
360100K .......... .......... .......... .......... .......... 71% 31.9M 12s
360150K .......... .......... .......... .......... .......... 71% 10.3M 12s
360200K .......... .......... .......... .......... .......... 71% 65.3M 12s
360250K .......... .......... .......... .......... .......... 71% 65.9M 12s
360300K .......... .......... .......... .......... .......... 71% 32.6M 12s
360350K .......... .......... .......... .......... .......... 71% 47.3M 12s
360400K .......... .......... .......... .......... .......... 71% 27.1M 12s
360450K .......... .......... .......... .......... .......... 71% 20.7M 12s
360500K .......... .......... .......... .......... .......... 71% 15.3M 12s
360550K .......... .......... .......... .......... .......... 71% 75.6M 12s
360600K .......... .......... .......... .......... .......... 71% 17.3M 12s
360650K .......... .......... .......... .......... .......... 71% 25.1M 12s
360700K .......... .......... .......... .......... .......... 71% 17.7M 12s
360750K .......... .......... .......... .......... .......... 71% 20.7M 12s
360800K .......... .......... .......... .......... .......... 71% 26.6M 12s
360850K .......... .......... .......... .......... .......... 71% 18.6M 12s
360900K .......... .......... .......... .......... .......... 71% 25.6M 12s
360950K .......... .......... .......... .......... .......... 71% 19.4M 12s
361000K .......... .......... .......... .......... .......... 71% 26.7M 12s
361050K .......... .......... .......... .......... .......... 71% 19.7M 12s
361100K .......... .......... .......... .......... .......... 71% 19.8M 12s
361150K .......... .......... .......... .......... .......... 71% 23.5M 12s
361200K .......... .......... .......... .......... .......... 71% 19.8M 12s
361250K .......... .......... .......... .......... .......... 71% 22.1M 12s
361300K .......... .......... .......... .......... .......... 71% 19.8M 12s
361350K .......... .......... .......... .......... .......... 71% 16.4M 12s
361400K .......... .......... .......... .......... .......... 71% 20.0M 12s
361450K .......... .......... .......... .......... .......... 71% 24.5M 12s
361500K .......... .......... .......... .......... .......... 71%  112M 12s
361550K .......... .......... .......... .......... .......... 71% 8.59M 12s
361600K .......... .......... .......... .......... .......... 71% 73.8M 12s
361650K .......... .......... .......... .......... .......... 71% 92.3M 12s
361700K .......... .......... .......... .......... .......... 71% 38.5M 12s
361750K .......... .......... .......... .......... .......... 71% 13.7M 12s
361800K .......... .......... .......... .......... .......... 71% 79.4M 12s
361850K .......... .......... .......... .......... .......... 71% 30.4M 12s
361900K .......... .......... .......... .......... .......... 71% 27.0M 12s
361950K .......... .......... .......... .......... .......... 71% 28.6M 12s
362000K .......... .......... .......... .......... .......... 71% 34.3M 12s
362050K .......... .......... .......... .......... .......... 71% 22.1M 12s
362100K .......... .......... .......... .......... .......... 71% 20.8M 12s
362150K .......... .......... .......... .......... .......... 71% 28.7M 12s
362200K .......... .......... .......... .......... .......... 71% 25.1M 12s
362250K .......... .......... .......... .......... .......... 71% 31.2M 12s
362300K .......... .......... .......... .......... .......... 71% 25.0M 12s
362350K .......... .......... .......... .......... .......... 71% 24.9M 12s
362400K .......... .......... .......... .......... .......... 71% 26.5M 12s
362450K .......... .......... .......... .......... .......... 71% 24.9M 12s
362500K .......... .......... .......... .......... .......... 71% 31.3M 12s
362550K .......... .......... .......... .......... .......... 71% 38.4M 12s
362600K .......... .......... .......... .......... .......... 71% 25.2M 12s
362650K .......... .......... .......... .......... .......... 71% 29.9M 12s
362700K .......... .......... .......... .......... .......... 71% 24.2M 12s
362750K .......... .......... .......... .......... .......... 71% 21.4M 12s
362800K .......... .......... .......... .......... .......... 71% 46.4M 12s
362850K .......... .......... .......... .......... .......... 71% 23.2M 12s
362900K .......... .......... .......... .......... .......... 71% 38.7M 12s
362950K .......... .......... .......... .......... .......... 71% 16.2M 12s
363000K .......... .......... .......... .......... .......... 71%  122M 12s
363050K .......... .......... .......... .......... .......... 71%  124M 12s
363100K .......... .......... .......... .......... .......... 71% 24.5M 12s
363150K .......... .......... .......... .......... .......... 71% 44.1M 12s
363200K .......... .......... .......... .......... .......... 71% 36.2M 12s
363250K .......... .......... .......... .......... .......... 71% 87.2M 12s
363300K .......... .......... .......... .......... .......... 71% 28.8M 12s
363350K .......... .......... .......... .......... .......... 72% 34.3M 12s
363400K .......... .......... .......... .......... .......... 72% 17.0M 12s
363450K .......... .......... .......... .......... .......... 72% 37.7M 12s
363500K .......... .......... .......... .......... .......... 72% 22.0M 12s
363550K .......... .......... .......... .......... .......... 72% 23.1M 12s
363600K .......... .......... .......... .......... .......... 72% 22.1M 12s
363650K .......... .......... .......... .......... .......... 72% 17.3M 12s
363700K .......... .......... .......... .......... .......... 72% 16.7M 12s
363750K .......... .......... .......... .......... .......... 72% 28.9M 12s
363800K .......... .......... .......... .......... .......... 72% 26.5M 12s
363850K .......... .......... .......... .......... .......... 72% 18.7M 12s
363900K .......... .......... .......... .......... .......... 72% 28.7M 12s
363950K .......... .......... .......... .......... .......... 72% 16.4M 12s
364000K .......... .......... .......... .......... .......... 72% 24.9M 12s
364050K .......... .......... .......... .......... .......... 72% 20.8M 12s
364100K .......... .......... .......... .......... .......... 72% 19.9M 12s
364150K .......... .......... .......... .......... .......... 72% 20.8M 12s
364200K .......... .......... .......... .......... .......... 72% 17.3M 12s
364250K .......... .......... .......... .......... .......... 72% 23.6M 12s
364300K .......... .......... .......... .......... .......... 72% 18.5M 12s
364350K .......... .......... .......... .......... .......... 72% 20.9M 12s
364400K .......... .......... .......... .......... .......... 72% 13.5M 12s
364450K .......... .......... .......... .......... .......... 72% 13.4M 12s
364500K .......... .......... .......... .......... .......... 72% 8.92M 12s
364550K .......... .......... .......... .......... .......... 72% 91.6M 12s
364600K .......... .......... .......... .......... .......... 72% 15.6M 12s
364650K .......... .......... .......... .......... .......... 72% 19.6M 12s
364700K .......... .......... .......... .......... .......... 72% 16.1M 12s
364750K .......... .......... .......... .......... .......... 72% 15.0M 12s
364800K .......... .......... .......... .......... .......... 72% 15.1M 12s
364850K .......... .......... .......... .......... .......... 72% 12.6M 12s
364900K .......... .......... .......... .......... .......... 72% 14.9M 12s
364950K .......... .......... .......... .......... .......... 72% 12.2M 12s
365000K .......... .......... .......... .......... .......... 72% 14.4M 12s
365050K .......... .......... .......... .......... .......... 72% 15.6M 12s
365100K .......... .......... .......... .......... .......... 72% 15.0M 12s
365150K .......... .......... .......... .......... .......... 72% 15.8M 12s
365200K .......... .......... .......... .......... .......... 72% 14.5M 12s
365250K .......... .......... .......... .......... .......... 72% 33.8M 12s
365300K .......... .......... .......... .......... .......... 72% 17.2M 12s
365350K .......... .......... .......... .......... .......... 72% 10.4M 12s
365400K .......... .......... .......... .......... .......... 72% 74.4M 12s
365450K .......... .......... .......... .......... .......... 72% 27.0M 12s
365500K .......... .......... .......... .......... .......... 72% 20.9M 12s
365550K .......... .......... .......... .......... .......... 72% 52.7M 12s
365600K .......... .......... .......... .......... .......... 72% 19.8M 12s
365650K .......... .......... .......... .......... .......... 72% 17.6M 12s
365700K .......... .......... .......... .......... .......... 72% 12.7M 12s
365750K .......... .......... .......... .......... .......... 72% 16.8M 12s
365800K .......... .......... .......... .......... .......... 72% 15.5M 12s
365850K .......... .......... .......... .......... .......... 72% 14.0M 12s
365900K .......... .......... .......... .......... .......... 72% 15.7M 12s
365950K .......... .......... .......... .......... .......... 72% 13.9M 12s
366000K .......... .......... .......... .......... .......... 72% 14.4M 12s
366050K .......... .......... .......... .......... .......... 72% 17.0M 12s
366100K .......... .......... .......... .......... .......... 72% 14.9M 12s
366150K .......... .......... .......... .......... .......... 72% 6.76M 12s
366200K .......... .......... .......... .......... .......... 72% 7.11M 12s
366250K .......... .......... .......... .......... .......... 72% 10.2M 12s
366300K .......... .......... .......... .......... .......... 72% 10.2M 12s
366350K .......... .......... .......... .......... .......... 72% 8.74M 12s
366400K .......... .......... .......... .......... .......... 72% 9.96M 12s
366450K .......... .......... .......... .......... .......... 72% 8.39M 12s
366500K .......... .......... .......... .......... .......... 72% 9.71M 12s
366550K .......... .......... .......... .......... .......... 72% 11.5M 12s
366600K .......... .......... .......... .......... .......... 72% 13.8M 12s
366650K .......... .......... .......... .......... .......... 72% 13.5M 12s
366700K .......... .......... .......... .......... .......... 72% 9.51M 12s
366750K .......... .......... .......... .......... .......... 72% 17.2M 11s
366800K .......... .......... .......... .......... .......... 72% 15.5M 11s
366850K .......... .......... .......... .......... .......... 72% 12.5M 11s
366900K .......... .......... .......... .......... .......... 72% 11.8M 11s
366950K .......... .......... .......... .......... .......... 72% 15.7M 11s
367000K .......... .......... .......... .......... .......... 72% 14.9M 11s
367050K .......... .......... .......... .......... .......... 72% 15.7M 11s
367100K .......... .......... .......... .......... .......... 72% 16.2M 11s
367150K .......... .......... .......... .......... .......... 72% 15.1M 11s
367200K .......... .......... .......... .......... .......... 72% 17.7M 11s
367250K .......... .......... .......... .......... .......... 72% 17.3M 11s
367300K .......... .......... .......... .......... .......... 72% 20.6M 11s
367350K .......... .......... .......... .......... .......... 72% 20.1M 11s
367400K .......... .......... .......... .......... .......... 72% 51.8M 11s
367450K .......... .......... .......... .......... .......... 72% 35.8M 11s
367500K .......... .......... .......... .......... .......... 72% 19.1M 11s
367550K .......... .......... .......... .......... .......... 72% 61.3M 11s
367600K .......... .......... .......... .......... .......... 72% 58.1M 11s
367650K .......... .......... .......... .......... .......... 72% 18.7M 11s
367700K .......... .......... .......... .......... .......... 72% 61.0M 11s
367750K .......... .......... .......... .......... .......... 72% 46.9M 11s
367800K .......... .......... .......... .......... .......... 72% 29.3M 11s
367850K .......... .......... .......... .......... .......... 72% 23.2M 11s
367900K .......... .......... .......... .......... .......... 72% 30.9M 11s
367950K .......... .......... .......... .......... .......... 72% 23.1M 11s
368000K .......... .......... .......... .......... .......... 72% 22.3M 11s
368050K .......... .......... .......... .......... .......... 72% 20.6M 11s
368100K .......... .......... .......... .......... .......... 72% 31.1M 11s
368150K .......... .......... .......... .......... .......... 72% 26.8M 11s
368200K .......... .......... .......... .......... .......... 72% 18.8M 11s
368250K .......... .......... .......... .......... .......... 72% 19.6M 11s
368300K .......... .......... .......... .......... .......... 72% 34.1M 11s
368350K .......... .......... .......... .......... .......... 72% 19.4M 11s
368400K .......... .......... .......... .......... .......... 73% 23.7M 11s
368450K .......... .......... .......... .......... .......... 73% 22.5M 11s
368500K .......... .......... .......... .......... .......... 73% 18.9M 11s
368550K .......... .......... .......... .......... .......... 73% 19.6M 11s
368600K .......... .......... .......... .......... .......... 73% 13.4M 11s
368650K .......... .......... .......... .......... .......... 73% 15.7M 11s
368700K .......... .......... .......... .......... .......... 73% 14.4M 11s
368750K .......... .......... .......... .......... .......... 73% 17.7M 11s
368800K .......... .......... .......... .......... .......... 73% 22.1M 11s
368850K .......... .......... .......... .......... .......... 73% 15.1M 11s
368900K .......... .......... .......... .......... .......... 73% 21.0M 11s
368950K .......... .......... .......... .......... .......... 73% 18.0M 11s
369000K .......... .......... .......... .......... .......... 73% 16.3M 11s
369050K .......... .......... .......... .......... .......... 73% 17.1M 11s
369100K .......... .......... .......... .......... .......... 73% 17.8M 11s
369150K .......... .......... .......... .......... .......... 73% 16.5M 11s
369200K .......... .......... .......... .......... .......... 73% 14.8M 11s
369250K .......... .......... .......... .......... .......... 73% 18.7M 11s
369300K .......... .......... .......... .......... .......... 73% 13.4M 11s
369350K .......... .......... .......... .......... .......... 73% 16.4M 11s
369400K .......... .......... .......... .......... .......... 73% 11.6M 11s
369450K .......... .......... .......... .......... .......... 73% 62.8M 11s
369500K .......... .......... .......... .......... .......... 73% 14.9M 11s
369550K .......... .......... .......... .......... .......... 73% 21.4M 11s
369600K .......... .......... .......... .......... .......... 73% 20.4M 11s
369650K .......... .......... .......... .......... .......... 73% 26.9M 11s
369700K .......... .......... .......... .......... .......... 73% 17.0M 11s
369750K .......... .......... .......... .......... .......... 73% 18.7M 11s
369800K .......... .......... .......... .......... .......... 73% 21.9M 11s
369850K .......... .......... .......... .......... .......... 73% 20.2M 11s
369900K .......... .......... .......... .......... .......... 73% 16.1M 11s
369950K .......... .......... .......... .......... .......... 73% 17.9M 11s
370000K .......... .......... .......... .......... .......... 73% 21.0M 11s
370050K .......... .......... .......... .......... .......... 73% 23.5M 11s
370100K .......... .......... .......... .......... .......... 73% 16.9M 11s
370150K .......... .......... .......... .......... .......... 73% 22.1M 11s
370200K .......... .......... .......... .......... .......... 73% 12.2M 11s
370250K .......... .......... .......... .......... .......... 73% 19.4M 11s
370300K .......... .......... .......... .......... .......... 73% 22.0M 11s
370350K .......... .......... .......... .......... .......... 73% 8.38M 11s
370400K .......... .......... .......... .......... .......... 73% 19.7M 11s
370450K .......... .......... .......... .......... .......... 73% 9.89M 11s
370500K .......... .......... .......... .......... .......... 73% 10.8M 11s
370550K .......... .......... .......... .......... .......... 73% 7.65M 11s
370600K .......... .......... .......... .......... .......... 73% 7.27M 11s
370650K .......... .......... .......... .......... .......... 73% 8.92M 11s
370700K .......... .......... .......... .......... .......... 73% 8.38M 11s
370750K .......... .......... .......... .......... .......... 73% 8.80M 11s
370800K .......... .......... .......... .......... .......... 73% 9.41M 11s
370850K .......... .......... .......... .......... .......... 73% 13.9M 11s
370900K .......... .......... .......... .......... .......... 73% 23.8M 11s
370950K .......... .......... .......... .......... .......... 73% 17.9M 11s
371000K .......... .......... .......... .......... .......... 73% 13.7M 11s
371050K .......... .......... .......... .......... .......... 73% 78.5M 11s
371100K .......... .......... .......... .......... .......... 73% 38.1M 11s
371150K .......... .......... .......... .......... .......... 73% 28.2M 11s
371200K .......... .......... .......... .......... .......... 73% 31.2M 11s
371250K .......... .......... .......... .......... .......... 73% 31.5M 11s
371300K .......... .......... .......... .......... .......... 73% 31.4M 11s
371350K .......... .......... .......... .......... .......... 73% 19.4M 11s
371400K .......... .......... .......... .......... .......... 73% 36.3M 11s
371450K .......... .......... .......... .......... .......... 73% 22.5M 11s
371500K .......... .......... .......... .......... .......... 73% 37.5M 11s
371550K .......... .......... .......... .......... .......... 73% 28.5M 11s
371600K .......... .......... .......... .......... .......... 73% 25.1M 11s
371650K .......... .......... .......... .......... .......... 73% 33.6M 11s
371700K .......... .......... .......... .......... .......... 73% 23.2M 11s
371750K .......... .......... .......... .......... .......... 73% 33.7M 11s
371800K .......... .......... .......... .......... .......... 73% 29.6M 11s
371850K .......... .......... .......... .......... .......... 73% 27.9M 11s
371900K .......... .......... .......... .......... .......... 73% 29.5M 11s
371950K .......... .......... .......... .......... .......... 73% 20.3M 11s
372000K .......... .......... .......... .......... .......... 73% 31.0M 11s
372050K .......... .......... .......... .......... .......... 73% 35.1M 11s
372100K .......... .......... .......... .......... .......... 73% 20.2M 11s
372150K .......... .......... .......... .......... .......... 73% 12.8M 11s
372200K .......... .......... .......... .......... .......... 73% 22.1M 11s
372250K .......... .......... .......... .......... .......... 73% 59.5M 11s
372300K .......... .......... .......... .......... .......... 73% 44.1M 11s
372350K .......... .......... .......... .......... .......... 73% 17.4M 11s
372400K .......... .......... .......... .......... .......... 73% 22.6M 11s
372450K .......... .......... .......... .......... .......... 73% 17.1M 11s
372500K .......... .......... .......... .......... .......... 73% 19.8M 11s
372550K .......... .......... .......... .......... .......... 73% 19.7M 11s
372600K .......... .......... .......... .......... .......... 73% 17.1M 11s
372650K .......... .......... .......... .......... .......... 73% 19.8M 11s
372700K .......... .......... .......... .......... .......... 73% 16.5M 11s
372750K .......... .......... .......... .......... .......... 73% 19.3M 11s
372800K .......... .......... .......... .......... .......... 73% 21.2M 11s
372850K .......... .......... .......... .......... .......... 73% 14.7M 11s
372900K .......... .......... .......... .......... .......... 73% 19.1M 11s
372950K .......... .......... .......... .......... .......... 73% 17.4M 11s
373000K .......... .......... .......... .......... .......... 73% 11.4M 11s
373050K .......... .......... .......... .......... .......... 73% 9.75M 11s
373100K .......... .......... .......... .......... .......... 73% 10.4M 11s
373150K .......... .......... .......... .......... .......... 73% 12.1M 11s
373200K .......... .......... .......... .......... .......... 73% 9.20M 11s
373250K .......... .......... .......... .......... .......... 73% 11.1M 11s
373300K .......... .......... .......... .......... .......... 73% 11.1M 11s
373350K .......... .......... .......... .......... .......... 73% 9.90M 11s
373400K .......... .......... .......... .......... .......... 73% 12.6M 11s
373450K .......... .......... .......... .......... .......... 74% 13.9M 11s
373500K .......... .......... .......... .......... .......... 74% 44.1M 11s
373550K .......... .......... .......... .......... .......... 74% 36.4M 11s
373600K .......... .......... .......... .......... .......... 74% 18.5M 11s
373650K .......... .......... .......... .......... .......... 74% 53.1M 11s
373700K .......... .......... .......... .......... .......... 74% 28.7M 11s
373750K .......... .......... .......... .......... .......... 74%  115M 11s
373800K .......... .......... .......... .......... .......... 74% 48.5M 11s
373850K .......... .......... .......... .......... .......... 74% 24.8M 11s
373900K .......... .......... .......... .......... .......... 74% 15.3M 11s
373950K .......... .......... .......... .......... .......... 74% 50.9M 11s
374000K .......... .......... .......... .......... .......... 74% 24.9M 11s
374050K .......... .......... .......... .......... .......... 74% 25.0M 11s
374100K .......... .......... .......... .......... .......... 74% 28.5M 11s
374150K .......... .......... .......... .......... .......... 74% 31.5M 11s
374200K .......... .......... .......... .......... .......... 74% 21.8M 11s
374250K .......... .......... .......... .......... .......... 74% 37.6M 11s
374300K .......... .......... .......... .......... .......... 74% 37.6M 11s
374350K .......... .......... .......... .......... .......... 74% 21.8M 11s
374400K .......... .......... .......... .......... .......... 74% 50.1M 11s
374450K .......... .......... .......... .......... .......... 74% 29.7M 11s
374500K .......... .......... .......... .......... .......... 74% 24.8M 11s
374550K .......... .......... .......... .......... .......... 74% 38.5M 11s
374600K .......... .......... .......... .......... .......... 74% 26.0M 11s
374650K .......... .......... .......... .......... .......... 74% 28.8M 11s
374700K .......... .......... .......... .......... .......... 74% 23.4M 11s
374750K .......... .......... .......... .......... .......... 74% 31.1M 11s
374800K .......... .......... .......... .......... .......... 74% 26.7M 11s
374850K .......... .......... .......... .......... .......... 74% 28.6M 11s
374900K .......... .......... .......... .......... .......... 74% 24.2M 11s
374950K .......... .......... .......... .......... .......... 74% 29.5M 11s
375000K .......... .......... .......... .......... .......... 74% 31.1M 11s
375050K .......... .......... .......... .......... .......... 74% 53.0M 11s
375100K .......... .......... .......... .......... .......... 74% 18.2M 11s
375150K .......... .......... .......... .......... .......... 74%  136M 11s
375200K .......... .......... .......... .......... .......... 74%  119M 11s
375250K .......... .......... .......... .......... .......... 74% 33.3M 11s
375300K .......... .......... .......... .......... .......... 74% 57.7M 11s
375350K .......... .......... .......... .......... .......... 74%  120M 11s
375400K .......... .......... .......... .......... .......... 74% 49.5M 11s
375450K .......... .......... .......... .......... .......... 74% 41.1M 11s
375500K .......... .......... .......... .......... .......... 74% 40.1M 11s
375550K .......... .......... .......... .......... .......... 74% 45.7M 11s
375600K .......... .......... .......... .......... .......... 74% 21.4M 11s
375650K .......... .......... .......... .......... .......... 74%  142M 11s
375700K .......... .......... .......... .......... .......... 74% 31.8M 11s
375750K .......... .......... .......... .......... .......... 74% 28.1M 11s
375800K .......... .......... .......... .......... .......... 74% 35.1M 11s
375850K .......... .......... .......... .......... .......... 74% 49.9M 11s
375900K .......... .......... .......... .......... .......... 74% 29.3M 11s
375950K .......... .......... .......... .......... .......... 74% 41.7M 11s
376000K .......... .......... .......... .......... .......... 74% 44.1M 11s
376050K .......... .......... .......... .......... .......... 74% 27.4M 11s
376100K .......... .......... .......... .......... .......... 74% 35.8M 11s
376150K .......... .......... .......... .......... .......... 74% 32.2M 11s
376200K .......... .......... .......... .......... .......... 74% 25.0M 11s
376250K .......... .......... .......... .......... .......... 74% 39.0M 11s
376300K .......... .......... .......... .......... .......... 74% 43.7M 11s
376350K .......... .......... .......... .......... .......... 74% 30.8M 11s
376400K .......... .......... .......... .......... .......... 74% 41.6M 11s
376450K .......... .......... .......... .......... .......... 74% 41.0M 11s
376500K .......... .......... .......... .......... .......... 74% 30.3M 11s
376550K .......... .......... .......... .......... .......... 74% 43.4M 11s
376600K .......... .......... .......... .......... .......... 74% 30.8M 11s
376650K .......... .......... .......... .......... .......... 74% 53.7M 11s
376700K .......... .......... .......... .......... .......... 74% 34.9M 11s
376750K .......... .......... .......... .......... .......... 74% 30.7M 11s
376800K .......... .......... .......... .......... .......... 74% 37.3M 11s
376850K .......... .......... .......... .......... .......... 74% 29.8M 11s
376900K .......... .......... .......... .......... .......... 74% 20.2M 11s
376950K .......... .......... .......... .......... .......... 74% 44.1M 11s
377000K .......... .......... .......... .......... .......... 74% 47.3M 11s
377050K .......... .......... .......... .......... .......... 74%  140M 11s
377100K .......... .......... .......... .......... .......... 74% 30.1M 11s
377150K .......... .......... .......... .......... .......... 74% 18.7M 10s
377200K .......... .......... .......... .......... .......... 74% 23.2M 10s
377250K .......... .......... .......... .......... .......... 74% 13.3M 10s
377300K .......... .......... .......... .......... .......... 74% 22.3M 10s
377350K .......... .......... .......... .......... .......... 74% 15.5M 10s
377400K .......... .......... .......... .......... .......... 74% 17.8M 10s
377450K .......... .......... .......... .......... .......... 74% 16.3M 10s
377500K .......... .......... .......... .......... .......... 74% 25.2M 10s
377550K .......... .......... .......... .......... .......... 74% 20.6M 10s
377600K .......... .......... .......... .......... .......... 74% 15.8M 10s
377650K .......... .......... .......... .......... .......... 74% 21.9M 10s
377700K .......... .......... .......... .......... .......... 74% 19.0M 10s
377750K .......... .......... .......... .......... .......... 74% 22.7M 10s
377800K .......... .......... .......... .......... .......... 74% 18.6M 10s
377850K .......... .......... .......... .......... .......... 74% 17.3M 10s
377900K .......... .......... .......... .......... .......... 74% 25.1M 10s
377950K .......... .......... .......... .......... .......... 74% 13.4M 10s
378000K .......... .......... .......... .......... .......... 74% 25.5M 10s
378050K .......... .......... .......... .......... .......... 74% 13.4M 10s
378100K .......... .......... .......... .......... .......... 74%  104M 10s
378150K .......... .......... .......... .......... .......... 74% 42.4M 10s
378200K .......... .......... .......... .......... .......... 74% 26.2M 10s
378250K .......... .......... .......... .......... .......... 74% 27.4M 10s
378300K .......... .......... .......... .......... .......... 74% 24.8M 10s
378350K .......... .......... .......... .......... .......... 74% 22.1M 10s
378400K .......... .......... .......... .......... .......... 74% 26.6M 10s
378450K .......... .......... .......... .......... .......... 74% 20.8M 10s
378500K .......... .......... .......... .......... .......... 75% 20.8M 10s
378550K .......... .......... .......... .......... .......... 75% 23.3M 10s
378600K .......... .......... .......... .......... .......... 75% 21.2M 10s
378650K .......... .......... .......... .......... .......... 75% 27.9M 10s
378700K .......... .......... .......... .......... .......... 75% 20.7M 10s
378750K .......... .......... .......... .......... .......... 75% 25.9M 10s
378800K .......... .......... .......... .......... .......... 75% 23.2M 10s
378850K .......... .......... .......... .......... .......... 75% 20.3M 10s
378900K .......... .......... .......... .......... .......... 75% 25.6M 10s
378950K .......... .......... .......... .......... .......... 75% 19.2M 10s
379000K .......... .......... .......... .......... .......... 75% 15.9M 10s
379050K .......... .......... .......... .......... .......... 75% 11.3M 10s
379100K .......... .......... .......... .......... .......... 75% 23.3M 10s
379150K .......... .......... .......... .......... .......... 75% 16.4M 10s
379200K .......... .......... .......... .......... .......... 75% 18.4M 10s
379250K .......... .......... .......... .......... .......... 75% 16.0M 10s
379300K .......... .......... .......... .......... .......... 75% 21.6M 10s
379350K .......... .......... .......... .......... .......... 75% 14.4M 10s
379400K .......... .......... .......... .......... .......... 75% 13.6M 10s
379450K .......... .......... .......... .......... .......... 75% 24.2M 10s
379500K .......... .......... .......... .......... .......... 75% 15.8M 10s
379550K .......... .......... .......... .......... .......... 75% 16.4M 10s
379600K .......... .......... .......... .......... .......... 75% 12.2M 10s
379650K .......... .......... .......... .......... .......... 75% 11.1M 10s
379700K .......... .......... .......... .......... .......... 75% 11.5M 10s
379750K .......... .......... .......... .......... .......... 75% 14.7M 10s
379800K .......... .......... .......... .......... .......... 75% 14.0M 10s
379850K .......... .......... .......... .......... .......... 75% 6.70M 10s
379900K .......... .......... .......... .......... .......... 75% 9.61M 10s
379950K .......... .......... .......... .......... .......... 75% 7.28M 10s
380000K .......... .......... .......... .......... .......... 75% 9.92M 10s
380050K .......... .......... .......... .......... .......... 75% 8.87M 10s
380100K .......... .......... .......... .......... .......... 75% 8.79M 10s
380150K .......... .......... .......... .......... .......... 75% 8.64M 10s
380200K .......... .......... .......... .......... .......... 75% 7.73M 10s
380250K .......... .......... .......... .......... .......... 75% 17.2M 10s
380300K .......... .......... .......... .......... .......... 75% 13.9M 10s
380350K .......... .......... .......... .......... .......... 75% 18.3M 10s
380400K .......... .......... .......... .......... .......... 75% 22.8M 10s
380450K .......... .......... .......... .......... .......... 75% 15.6M 10s
380500K .......... .......... .......... .......... .......... 75% 51.5M 10s
380550K .......... .......... .......... .......... .......... 75% 14.5M 10s
380600K .......... .......... .......... .......... .......... 75% 24.6M 10s
380650K .......... .......... .......... .......... .......... 75% 19.6M 10s
380700K .......... .......... .......... .......... .......... 75% 14.5M 10s
380750K .......... .......... .......... .......... .......... 75% 17.2M 10s
380800K .......... .......... .......... .......... .......... 75% 16.4M 10s
380850K .......... .......... .......... .......... .......... 75% 12.5M 10s
380900K .......... .......... .......... .......... .......... 75% 17.2M 10s
380950K .......... .......... .......... .......... .......... 75% 14.3M 10s
381000K .......... .......... .......... .......... .......... 75% 14.2M 10s
381050K .......... .......... .......... .......... .......... 75% 11.6M 10s
381100K .......... .......... .......... .......... .......... 75% 7.27M 10s
381150K .......... .......... .......... .......... .......... 75% 5.43M 10s
381200K .......... .......... .......... .......... .......... 75% 9.62M 10s
381250K .......... .......... .......... .......... .......... 75% 12.5M 10s
381300K .......... .......... .......... .......... .......... 75% 10.5M 10s
381350K .......... .......... .......... .......... .......... 75% 13.4M 10s
381400K .......... .......... .......... .......... .......... 75% 12.6M 10s
381450K .......... .......... .......... .......... .......... 75% 11.4M 10s
381500K .......... .......... .......... .......... .......... 75% 11.8M 10s
381550K .......... .......... .......... .......... .......... 75% 11.4M 10s
381600K .......... .......... .......... .......... .......... 75% 9.04M 10s
381650K .......... .......... .......... .......... .......... 75% 6.98M 10s
381700K .......... .......... .......... .......... .......... 75% 13.9M 10s
381750K .......... .......... .......... .......... .......... 75% 10.5M 10s
381800K .......... .......... .......... .......... .......... 75% 10.6M 10s
381850K .......... .......... .......... .......... .......... 75% 8.80M 10s
381900K .......... .......... .......... .......... .......... 75% 11.9M 10s
381950K .......... .......... .......... .......... .......... 75% 9.20M 10s
382000K .......... .......... .......... .......... .......... 75% 8.75M 10s
382050K .......... .......... .......... .......... .......... 75% 17.9M 10s
382100K .......... .......... .......... .......... .......... 75% 18.4M 10s
382150K .......... .......... .......... .......... .......... 75% 11.0M 10s
382200K .......... .......... .......... .......... .......... 75% 26.9M 10s
382250K .......... .......... .......... .......... .......... 75% 17.1M 10s
382300K .......... .......... .......... .......... .......... 75% 22.1M 10s
382350K .......... .......... .......... .......... .......... 75% 19.7M 10s
382400K .......... .......... .......... .......... .......... 75% 25.0M 10s
382450K .......... .......... .......... .......... .......... 75% 15.7M 10s
382500K .......... .......... .......... .......... .......... 75% 16.5M 10s
382550K .......... .......... .......... .......... .......... 75% 31.3M 10s
382600K .......... .......... .......... .......... .......... 75% 15.7M 10s
382650K .......... .......... .......... .......... .......... 75% 23.4M 10s
382700K .......... .......... .......... .......... .......... 75% 18.7M 10s
382750K .......... .......... .......... .......... .......... 75% 19.7M 10s
382800K .......... .......... .......... .......... .......... 75% 23.1M 10s
382850K .......... .......... .......... .......... .......... 75% 17.0M 10s
382900K .......... .......... .......... .......... .......... 75% 27.0M 10s
382950K .......... .......... .......... .......... .......... 75% 18.1M 10s
383000K .......... .......... .......... .......... .......... 75% 30.5M 10s
383050K .......... .......... .......... .......... .......... 75% 51.0M 10s
383100K .......... .......... .......... .......... .......... 75% 14.6M 10s
383150K .......... .......... .......... .......... .......... 75% 48.3M 10s
383200K .......... .......... .......... .......... .......... 75% 69.4M 10s
383250K .......... .......... .......... .......... .......... 75% 61.1M 10s
383300K .......... .......... .......... .......... .......... 75% 39.3M 10s
383350K .......... .......... .......... .......... .......... 75% 25.3M 10s
383400K .......... .......... .......... .......... .......... 75% 39.1M 10s
383450K .......... .......... .......... .......... .......... 75% 18.4M 10s
383500K .......... .......... .......... .......... .......... 75% 22.7M 10s
383550K .......... .......... .......... .......... .......... 76% 37.2M 10s
383600K .......... .......... .......... .......... .......... 76% 19.7M 10s
383650K .......... .......... .......... .......... .......... 76% 29.3M 10s
383700K .......... .......... .......... .......... .......... 76% 21.9M 10s
383750K .......... .......... .......... .......... .......... 76% 26.8M 10s
383800K .......... .......... .......... .......... .......... 76% 26.6M 10s
383850K .......... .......... .......... .......... .......... 76% 22.2M 10s
383900K .......... .......... .......... .......... .......... 76% 31.8M 10s
383950K .......... .......... .......... .......... .......... 76% 19.4M 10s
384000K .......... .......... .......... .......... .......... 76% 28.4M 10s
384050K .......... .......... .......... .......... .......... 76% 26.8M 10s
384100K .......... .......... .......... .......... .......... 76% 26.7M 10s
384150K .......... .......... .......... .......... .......... 76% 27.3M 10s
384200K .......... .......... .......... .......... .......... 76% 20.5M 10s
384250K .......... .......... .......... .......... .......... 76% 26.9M 10s
384300K .......... .......... .......... .......... .......... 76% 22.1M 10s
384350K .......... .......... .......... .......... .......... 76% 21.8M 10s
384400K .......... .......... .......... .......... .......... 76% 18.4M 10s
384450K .......... .......... .......... .......... .......... 76% 9.31M 10s
384500K .......... .......... .......... .......... .......... 76% 49.6M 10s
384550K .......... .......... .......... .......... .......... 76% 44.5M 10s
384600K .......... .......... .......... .......... .......... 76% 14.7M 10s
384650K .......... .......... .......... .......... .......... 76% 19.1M 10s
384700K .......... .......... .......... .......... .......... 76% 29.4M 10s
384750K .......... .......... .......... .......... .......... 76% 25.1M 10s
384800K .......... .......... .......... .......... .......... 76% 23.4M 10s
384850K .......... .......... .......... .......... .......... 76% 25.2M 10s
384900K .......... .......... .......... .......... .......... 76% 23.2M 10s
384950K .......... .......... .......... .......... .......... 76% 18.7M 10s
385000K .......... .......... .......... .......... .......... 76% 20.3M 10s
385050K .......... .......... .......... .......... .......... 76% 29.1M 10s
385100K .......... .......... .......... .......... .......... 76% 14.4M 10s
385150K .......... .......... .......... .......... .......... 76% 21.0M 10s
385200K .......... .......... .......... .......... .......... 76% 17.7M 10s
385250K .......... .......... .......... .......... .......... 76% 22.9M 10s
385300K .......... .......... .......... .......... .......... 76% 16.4M 10s
385350K .......... .......... .......... .......... .......... 76% 18.0M 10s
385400K .......... .......... .......... .......... .......... 76% 21.9M 10s
385450K .......... .......... .......... .......... .......... 76% 15.6M 10s
385500K .......... .......... .......... .......... .......... 76% 15.1M 10s
385550K .......... .......... .......... .......... .......... 76% 13.2M 10s
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385650K .......... .......... .......... .......... .......... 76% 20.9M 10s
385700K .......... .......... .......... .......... .......... 76% 12.9M 10s
385750K .......... .......... .......... .......... .......... 76% 18.8M 10s
385800K .......... .......... .......... .......... .......... 76% 12.1M 10s
385850K .......... .......... .......... .......... .......... 76% 17.0M 10s
385900K .......... .......... .......... .......... .......... 76% 16.9M 10s
385950K .......... .......... .......... .......... .......... 76% 16.9M 10s
386000K .......... .......... .......... .......... .......... 76% 18.0M 10s
386050K .......... .......... .......... .......... .......... 76% 16.2M 10s
386100K .......... .......... .......... .......... .......... 76% 9.47M 10s
386150K .......... .......... .......... .......... .......... 76% 12.3M 10s
386200K .......... .......... .......... .......... .......... 76% 8.78M 10s
386250K .......... .......... .......... .......... .......... 76% 15.8M 10s
386300K .......... .......... .......... .......... .......... 76% 11.4M 10s
386350K .......... .......... .......... .......... .......... 76% 9.91M 10s
386400K .......... .......... .......... .......... .......... 76% 11.1M 10s
386450K .......... .......... .......... .......... .......... 76% 9.70M 10s
386500K .......... .......... .......... .......... .......... 76% 10.8M 10s
386550K .......... .......... .......... .......... .......... 76% 10.9M 10s
386600K .......... .......... .......... .......... .......... 76% 8.44M 10s
386650K .......... .......... .......... .......... .......... 76% 13.7M 10s
386700K .......... .......... .......... .......... .......... 76% 13.9M 10s
386750K .......... .......... .......... .......... .......... 76% 11.9M 10s
386800K .......... .......... .......... .......... .......... 76% 12.1M 10s
386850K .......... .......... .......... .......... .......... 76% 9.18M 10s
386900K .......... .......... .......... .......... .......... 76% 12.5M 10s
386950K .......... .......... .......... .......... .......... 76% 10.2M 10s
387000K .......... .......... .......... .......... .......... 76% 12.1M 10s
387050K .......... .......... .......... .......... .......... 76% 12.6M 10s
387100K .......... .......... .......... .......... .......... 76% 10.5M 10s
387150K .......... .......... .......... .......... .......... 76% 21.4M 10s
387200K .......... .......... .......... .......... .......... 76% 33.1M 10s
387250K .......... .......... .......... .......... .......... 76% 19.4M 10s
387300K .......... .......... .......... .......... .......... 76% 35.2M 10s
387350K .......... .......... .......... .......... .......... 76% 45.5M 10s
387400K .......... .......... .......... .......... .......... 76% 37.9M 10s
387450K .......... .......... .......... .......... .......... 76% 22.9M 10s
387500K .......... .......... .......... .......... .......... 76% 23.7M 10s
387550K .......... .......... .......... .......... .......... 76% 31.2M 10s
387600K .......... .......... .......... .......... .......... 76% 26.4M 10s
387650K .......... .......... .......... .......... .......... 76% 25.2M 10s
387700K .......... .......... .......... .......... .......... 76% 26.7M 10s
387750K .......... .......... .......... .......... .......... 76% 28.9M 10s
387800K .......... .......... .......... .......... .......... 76% 37.2M 10s
387850K .......... .......... .......... .......... .......... 76% 26.4M 10s
387900K .......... .......... .......... .......... .......... 76% 28.8M 10s
387950K .......... .......... .......... .......... .......... 76% 23.3M 10s
388000K .......... .......... .......... .......... .......... 76% 42.2M 10s
388050K .......... .......... .......... .......... .......... 76% 26.0M 10s
388100K .......... .......... .......... .......... .......... 76% 28.6M 10s
388150K .......... .......... .......... .......... .......... 76% 32.3M 10s
388200K .......... .......... .......... .......... .......... 76% 30.0M 10s
388250K .......... .......... .......... .......... .......... 76% 33.8M 10s
388300K .......... .......... .......... .......... .......... 76% 31.4M 10s
388350K .......... .......... .......... .......... .......... 76% 23.4M 9s
388400K .......... .......... .......... .......... .......... 76% 20.8M 9s
388450K .......... .......... .......... .......... .......... 76% 22.3M 9s
388500K .......... .......... .......... .......... .......... 76% 15.6M 9s
388550K .......... .......... .......... .......... .......... 76%  107M 9s
388600K .......... .......... .......... .......... .......... 77% 15.0M 9s
388650K .......... .......... .......... .......... .......... 77% 82.2M 9s
388700K .......... .......... .......... .......... .......... 77% 13.8M 9s
388750K .......... .......... .......... .......... .......... 77% 39.0M 9s
388800K .......... .......... .......... .......... .......... 77% 16.3M 9s
388850K .......... .......... .......... .......... .......... 77% 17.2M 9s
388900K .......... .......... .......... .......... .......... 77% 18.7M 9s
388950K .......... .......... .......... .......... .......... 77% 17.1M 9s
389000K .......... .......... .......... .......... .......... 77% 19.0M 9s
389050K .......... .......... .......... .......... .......... 77% 30.8M 9s
389100K .......... .......... .......... .......... .......... 77% 15.0M 9s
389150K .......... .......... .......... .......... .......... 77% 28.7M 9s
389200K .......... .......... .......... .......... .......... 77% 19.0M 9s
389250K .......... .......... .......... .......... .......... 77% 18.6M 9s
389300K .......... .......... .......... .......... .......... 77% 23.5M 9s
389350K .......... .......... .......... .......... .......... 77% 18.8M 9s
389400K .......... .......... .......... .......... .......... 77% 18.1M 9s
389450K .......... .......... .......... .......... .......... 77% 9.46M 9s
389500K .......... .......... .......... .......... .......... 77% 10.5M 9s
389550K .......... .......... .......... .......... .......... 77% 25.2M 9s
389600K .......... .......... .......... .......... .......... 77% 21.8M 9s
389650K .......... .......... .......... .......... .......... 77% 25.0M 9s
389700K .......... .......... .......... .......... .......... 77% 18.8M 9s
389750K .......... .......... .......... .......... .......... 77% 19.9M 9s
389800K .......... .......... .......... .......... .......... 77% 24.8M 9s
389850K .......... .......... .......... .......... .......... 77% 20.8M 9s
389900K .......... .......... .......... .......... .......... 77% 22.0M 9s
389950K .......... .......... .......... .......... .......... 77% 17.8M 9s
390000K .......... .......... .......... .......... .......... 77% 20.7M 9s
390050K .......... .......... .......... .......... .......... 77% 19.8M 9s
390100K .......... .......... .......... .......... .......... 77% 23.5M 9s
390150K .......... .......... .......... .......... .......... 77% 19.6M 9s
390200K .......... .......... .......... .......... .......... 77% 19.7M 9s
390250K .......... .......... .......... .......... .......... 77% 19.6M 9s
390300K .......... .......... .......... .......... .......... 77% 14.3M 9s
390350K .......... .......... .......... .......... .......... 77% 12.5M 9s
390400K .......... .......... .......... .......... .......... 77% 15.3M 9s
390450K .......... .......... .......... .......... .......... 77% 12.3M 9s
390500K .......... .......... .......... .......... .......... 77% 17.0M 9s
390550K .......... .......... .......... .......... .......... 77% 13.4M 9s
390600K .......... .......... .......... .......... .......... 77% 11.2M 9s
390650K .......... .......... .......... .......... .......... 77% 14.4M 9s
390700K .......... .......... .......... .......... .......... 77% 8.20M 9s
390750K .......... .......... .......... .......... .......... 77% 13.4M 9s
390800K .......... .......... .......... .......... .......... 77% 14.5M 9s
390850K .......... .......... .......... .......... .......... 77% 8.21M 9s
390900K .......... .......... .......... .......... .......... 77% 17.8M 9s
390950K .......... .......... .......... .......... .......... 77% 10.4M 9s
391000K .......... .......... .......... .......... .......... 77% 13.4M 9s
391050K .......... .......... .......... .......... .......... 77% 17.9M 9s
391100K .......... .......... .......... .......... .......... 77% 15.6M 9s
391150K .......... .......... .......... .......... .......... 77% 16.2M 9s
391200K .......... .......... .......... .......... .......... 77% 14.5M 9s
391250K .......... .......... .......... .......... .......... 77% 15.0M 9s
391300K .......... .......... .......... .......... .......... 77% 16.3M 9s
391350K .......... .......... .......... .......... .......... 77% 14.5M 9s
391400K .......... .......... .......... .......... .......... 77% 18.0M 9s
391450K .......... .......... .......... .......... .......... 77% 21.4M 9s
391500K .......... .......... .......... .......... .......... 77% 12.1M 9s
391550K .......... .......... .......... .......... .......... 77% 20.9M 9s
391600K .......... .......... .......... .......... .......... 77% 27.1M 9s
391650K .......... .......... .......... .......... .......... 77% 19.6M 9s
391700K .......... .......... .......... .......... .......... 77% 17.5M 9s
391750K .......... .......... .......... .......... .......... 77% 22.1M 9s
391800K .......... .......... .......... .......... .......... 77% 19.3M 9s
391850K .......... .......... .......... .......... .......... 77% 21.9M 9s
391900K .......... .......... .......... .......... .......... 77% 25.0M 9s
391950K .......... .......... .......... .......... .......... 77% 18.1M 9s
392000K .......... .......... .......... .......... .......... 77% 18.9M 9s
392050K .......... .......... .......... .......... .......... 77% 19.5M 9s
392100K .......... .......... .......... .......... .......... 77% 18.9M 9s
392150K .......... .......... .......... .......... .......... 77% 19.7M 9s
392200K .......... .......... .......... .......... .......... 77% 17.1M 9s
392250K .......... .......... .......... .......... .......... 77% 21.9M 9s
392300K .......... .......... .......... .......... .......... 77% 34.3M 9s
392350K .......... .......... .......... .......... .......... 77% 12.6M 9s
392400K .......... .......... .......... .......... .......... 77% 78.1M 9s
392450K .......... .......... .......... .......... .......... 77% 25.8M 9s
392500K .......... .......... .......... .......... .......... 77% 24.8M 9s
392550K .......... .......... .......... .......... .......... 77% 75.7M 9s
392600K .......... .......... .......... .......... .......... 77% 22.6M 9s
392650K .......... .......... .......... .......... .......... 77% 25.6M 9s
392700K .......... .......... .......... .......... .......... 77% 17.8M 9s
392750K .......... .......... .......... .......... .......... 77% 20.7M 9s
392800K .......... .......... .......... .......... .......... 77% 19.0M 9s
392850K .......... .......... .......... .......... .......... 77% 18.8M 9s
392900K .......... .......... .......... .......... .......... 77% 17.7M 9s
392950K .......... .......... .......... .......... .......... 77% 18.7M 9s
393000K .......... .......... .......... .......... .......... 77% 19.7M 9s
393050K .......... .......... .......... .......... .......... 77% 23.6M 9s
393100K .......... .......... .......... .......... .......... 77% 13.6M 9s
393150K .......... .......... .......... .......... .......... 77% 16.5M 9s
393200K .......... .......... .......... .......... .......... 77% 19.1M 9s
393250K .......... .......... .......... .......... .......... 77% 23.3M 9s
393300K .......... .......... .......... .......... .......... 77% 20.3M 9s
393350K .......... .......... .......... .......... .......... 77% 21.8M 9s
393400K .......... .......... .......... .......... .......... 77% 32.6M 9s
393450K .......... .......... .......... .......... .......... 77% 23.4M 9s
393500K .......... .......... .......... .......... .......... 77% 9.05M 9s
393550K .......... .......... .......... .......... .......... 77% 81.8M 9s
393600K .......... .......... .......... .......... .......... 78% 65.5M 9s
393650K .......... .......... .......... .......... .......... 78% 21.9M 9s
393700K .......... .......... .......... .......... .......... 78% 71.5M 9s
393750K .......... .......... .......... .......... .......... 78% 22.5M 9s
393800K .......... .......... .......... .......... .......... 78% 26.7M 9s
393850K .......... .......... .......... .......... .......... 78% 18.9M 9s
393900K .......... .......... .......... .......... .......... 78% 20.8M 9s
393950K .......... .......... .......... .......... .......... 78% 19.6M 9s
394000K .......... .......... .......... .......... .......... 78% 20.7M 9s
394050K .......... .......... .......... .......... .......... 78% 22.3M 9s
394100K .......... .......... .......... .......... .......... 78% 18.0M 9s
394150K .......... .......... .......... .......... .......... 78% 22.6M 9s
394200K .......... .......... .......... .......... .......... 78% 18.9M 9s
394250K .......... .......... .......... .......... .......... 78% 20.7M 9s
394300K .......... .......... .......... .......... .......... 78% 26.9M 9s
394350K .......... .......... .......... .......... .......... 78% 17.0M 9s
394400K .......... .......... .......... .......... .......... 78% 25.0M 9s
394450K .......... .......... .......... .......... .......... 78% 15.6M 9s
394500K .......... .......... .......... .......... .......... 78% 30.2M 9s
394550K .......... .......... .......... .......... .......... 78% 29.8M 9s
394600K .......... .......... .......... .......... .......... 78% 17.3M 9s
394650K .......... .......... .......... .......... .......... 78% 29.4M 9s
394700K .......... .......... .......... .......... .......... 78% 25.2M 9s
394750K .......... .......... .......... .......... .......... 78% 14.9M 9s
394800K .......... .......... .......... .......... .......... 78% 35.1M 9s
394850K .......... .......... .......... .......... .......... 78% 82.6M 9s
394900K .......... .......... .......... .......... .......... 78% 16.6M 9s
394950K .......... .......... .......... .......... .......... 78% 33.9M 9s
395000K .......... .......... .......... .......... .......... 78% 93.0M 9s
395050K .......... .......... .......... .......... .......... 78% 21.5M 9s
395100K .......... .......... .......... .......... .......... 78% 22.6M 9s
395150K .......... .......... .......... .......... .......... 78% 21.8M 9s
395200K .......... .......... .......... .......... .......... 78% 23.1M 9s
395250K .......... .......... .......... .......... .......... 78% 22.3M 9s
395300K .......... .......... .......... .......... .......... 78% 17.4M 9s
395350K .......... .......... .......... .......... .......... 78% 17.7M 9s
395400K .......... .......... .......... .......... .......... 78% 18.8M 9s
395450K .......... .......... .......... .......... .......... 78% 19.4M 9s
395500K .......... .......... .......... .......... .......... 78% 18.9M 9s
395550K .......... .......... .......... .......... .......... 78% 18.6M 9s
395600K .......... .......... .......... .......... .......... 78% 18.5M 9s
395650K .......... .......... .......... .......... .......... 78% 20.7M 9s
395700K .......... .......... .......... .......... .......... 78% 12.6M 9s
395750K .......... .......... .......... .......... .......... 78% 12.2M 9s
395800K .......... .......... .......... .......... .......... 78% 14.3M 9s
395850K .......... .......... .......... .......... .......... 78% 11.0M 9s
395900K .......... .......... .......... .......... .......... 78% 10.5M 9s
395950K .......... .......... .......... .......... .......... 78% 10.3M 9s
396000K .......... .......... .......... .......... .......... 78% 11.1M 9s
396050K .......... .......... .......... .......... .......... 78% 14.7M 9s
396100K .......... .......... .......... .......... .......... 78% 9.71M 9s
396150K .......... .......... .......... .......... .......... 78% 12.1M 9s
396200K .......... .......... .......... .......... .......... 78% 21.8M 9s
396250K .......... .......... .......... .......... .......... 78% 19.3M 9s
396300K .......... .......... .......... .......... .......... 78% 94.4M 9s
396350K .......... .......... .......... .......... .......... 78% 37.8M 9s
396400K .......... .......... .......... .......... .......... 78% 29.3M 9s
396450K .......... .......... .......... .......... .......... 78% 21.8M 9s
396500K .......... .......... .......... .......... .......... 78% 23.4M 9s
396550K .......... .......... .......... .......... .......... 78% 26.6M 9s
396600K .......... .......... .......... .......... .......... 78% 28.8M 9s
396650K .......... .......... .......... .......... .......... 78% 31.1M 9s
396700K .......... .......... .......... .......... .......... 78% 28.9M 9s
396750K .......... .......... .......... .......... .......... 78% 23.6M 9s
396800K .......... .......... .......... .......... .......... 78% 42.6M 9s
396850K .......... .......... .......... .......... .......... 78% 24.9M 9s
396900K .......... .......... .......... .......... .......... 78% 21.6M 9s
396950K .......... .......... .......... .......... .......... 78% 25.8M 9s
397000K .......... .......... .......... .......... .......... 78% 28.6M 9s
397050K .......... .......... .......... .......... .......... 78% 25.0M 9s
397100K .......... .......... .......... .......... .......... 78% 26.7M 9s
397150K .......... .......... .......... .......... .......... 78% 31.1M 9s
397200K .......... .......... .......... .......... .......... 78% 31.3M 9s
397250K .......... .......... .......... .......... .......... 78% 31.1M 9s
397300K .......... .......... .......... .......... .......... 78% 28.7M 9s
397350K .......... .......... .......... .......... .......... 78% 56.7M 9s
397400K .......... .......... .......... .......... .......... 78% 49.5M 9s
397450K .......... .......... .......... .......... .......... 78% 68.5M 9s
397500K .......... .......... .......... .......... .......... 78% 10.9M 9s
397550K .......... .......... .......... .......... .......... 78%  101M 9s
397600K .......... .......... .......... .......... .......... 78% 84.2M 9s
397650K .......... .......... .......... .......... .......... 78%  104M 9s
397700K .......... .......... .......... .......... .......... 78% 84.8M 9s
397750K .......... .......... .......... .......... .......... 78% 28.8M 9s
397800K .......... .......... .......... .......... .......... 78% 89.8M 9s
397850K .......... .......... .......... .......... .......... 78% 38.6M 9s
397900K .......... .......... .......... .......... .......... 78% 68.3M 9s
397950K .......... .......... .......... .......... .......... 78% 86.1M 9s
398000K .......... .......... .......... .......... .......... 78% 48.7M 9s
398050K .......... .......... .......... .......... .......... 78% 41.6M 9s
398100K .......... .......... .......... .......... .......... 78% 24.9M 9s
398150K .......... .......... .......... .......... .......... 78% 62.3M 9s
398200K .......... .......... .......... .......... .......... 78% 40.2M 9s
398250K .......... .......... .......... .......... .......... 78% 35.5M 9s
398300K .......... .......... .......... .......... .......... 78% 37.1M 9s
398350K .......... .......... .......... .......... .......... 78% 30.9M 9s
398400K .......... .......... .......... .......... .......... 78% 37.6M 9s
398450K .......... .......... .......... .......... .......... 78% 38.1M 9s
398500K .......... .......... .......... .......... .......... 78% 40.7M 9s
398550K .......... .......... .......... .......... .......... 78% 40.4M 9s
398600K .......... .......... .......... .......... .......... 78% 29.7M 9s
398650K .......... .......... .......... .......... .......... 79% 46.6M 9s
398700K .......... .......... .......... .......... .......... 79% 41.2M 9s
398750K .......... .......... .......... .......... .......... 79% 49.3M 9s
398800K .......... .......... .......... .......... .......... 79% 29.9M 9s
398850K .......... .......... .......... .......... .......... 79% 37.4M 9s
398900K .......... .......... .......... .......... .......... 79% 49.9M 9s
398950K .......... .......... .......... .......... .......... 79% 36.9M 9s
399000K .......... .......... .......... .......... .......... 79% 47.0M 9s
399050K .......... .......... .......... .......... .......... 79% 31.4M 9s
399100K .......... .......... .......... .......... .......... 79% 29.6M 9s
399150K .......... .......... .......... .......... .......... 79% 37.4M 9s
399200K .......... .......... .......... .......... .......... 79% 26.6M 9s
399250K .......... .......... .......... .......... .......... 79% 28.7M 9s
399300K .......... .......... .......... .......... .......... 79% 12.4M 9s
399350K .......... .......... .......... .......... .......... 79% 16.8M 8s
399400K .......... .......... .......... .......... .......... 79% 16.7M 8s
399450K .......... .......... .......... .......... .......... 79% 15.9M 8s
399500K .......... .......... .......... .......... .......... 79% 25.2M 8s
399550K .......... .......... .......... .......... .......... 79% 19.1M 8s
399600K .......... .......... .......... .......... .......... 79% 15.6M 8s
399650K .......... .......... .......... .......... .......... 79% 20.0M 8s
399700K .......... .......... .......... .......... .......... 79% 19.7M 8s
399750K .......... .......... .......... .......... .......... 79% 20.9M 8s
399800K .......... .......... .......... .......... .......... 79% 18.9M 8s
399850K .......... .......... .......... .......... .......... 79% 17.8M 8s
399900K .......... .......... .......... .......... .......... 79% 22.9M 8s
399950K .......... .......... .......... .......... .......... 79% 20.1M 8s
400000K .......... .......... .......... .......... .......... 79% 13.3M 8s
400050K .......... .......... .......... .......... .......... 79% 13.9M 8s
400100K .......... .......... .......... .......... .......... 79% 13.0M 8s
400150K .......... .......... .......... .......... .......... 79% 19.6M 8s
400200K .......... .......... .......... .......... .......... 79% 20.9M 8s
400250K .......... .......... .......... .......... .......... 79% 21.5M 8s
400300K .......... .......... .......... .......... .......... 79% 19.7M 8s
400350K .......... .......... .......... .......... .......... 79% 17.8M 8s
400400K .......... .......... .......... .......... .......... 79% 15.1M 8s
400450K .......... .......... .......... .......... .......... 79% 14.4M 8s
400500K .......... .......... .......... .......... .......... 79% 24.9M 8s
400550K .......... .......... .......... .......... .......... 79% 16.3M 8s
400600K .......... .......... .......... .......... .......... 79% 18.8M 8s
400650K .......... .......... .......... .......... .......... 79% 19.0M 8s
400700K .......... .......... .......... .......... .......... 79% 16.8M 8s
400750K .......... .......... .......... .......... .......... 79% 17.8M 8s
400800K .......... .......... .......... .......... .......... 79% 17.7M 8s
400850K .......... .......... .......... .......... .......... 79% 19.5M 8s
400900K .......... .......... .......... .......... .......... 79% 18.7M 8s
400950K .......... .......... .......... .......... .......... 79% 27.3M 8s
401000K .......... .......... .......... .......... .......... 79% 11.2M 8s
401050K .......... .......... .......... .......... .......... 79% 86.1M 8s
401100K .......... .......... .......... .......... .......... 79% 32.9M 8s
401150K .......... .......... .......... .......... .......... 79% 17.1M 8s
401200K .......... .......... .......... .......... .......... 79% 22.9M 8s
401250K .......... .......... .......... .......... .......... 79% 40.3M 8s
401300K .......... .......... .......... .......... .......... 79% 21.4M 8s
401350K .......... .......... .......... .......... .......... 79% 19.7M 8s
401400K .......... .......... .......... .......... .......... 79% 20.5M 8s
401450K .......... .......... .......... .......... .......... 79% 21.2M 8s
401500K .......... .......... .......... .......... .......... 79% 26.6M 8s
401550K .......... .......... .......... .......... .......... 79% 27.1M 8s
401600K .......... .......... .......... .......... .......... 79% 21.5M 8s
401650K .......... .......... .......... .......... .......... 79% 23.8M 8s
401700K .......... .......... .......... .......... .......... 79% 26.9M 8s
401750K .......... .......... .......... .......... .......... 79% 26.1M 8s
401800K .......... .......... .......... .......... .......... 79% 21.9M 8s
401850K .......... .......... .......... .......... .......... 79% 24.8M 8s
401900K .......... .......... .......... .......... .......... 79% 18.9M 8s
401950K .......... .......... .......... .......... .......... 79% 17.2M 8s
402000K .......... .......... .......... .......... .......... 79% 37.7M 8s
402050K .......... .......... .......... .......... .......... 79% 20.7M 8s
402100K .......... .......... .......... .......... .......... 79% 17.1M 8s
402150K .......... .......... .......... .......... .......... 79% 37.6M 8s
402200K .......... .......... .......... .......... .......... 79% 34.3M 8s
402250K .......... .......... .......... .......... .......... 79% 33.7M 8s
402300K .......... .......... .......... .......... .......... 79% 37.3M 8s
402350K .......... .......... .......... .......... .......... 79% 61.7M 8s
402400K .......... .......... .......... .......... .......... 79% 18.7M 8s
402450K .......... .......... .......... .......... .......... 79% 84.8M 8s
402500K .......... .......... .......... .......... .......... 79% 48.1M 8s
402550K .......... .......... .......... .......... .......... 79% 23.5M 8s
402600K .......... .......... .......... .......... .......... 79% 15.0M 8s
402650K .......... .......... .......... .......... .......... 79% 18.0M 8s
402700K .......... .......... .......... .......... .......... 79% 27.2M 8s
402750K .......... .......... .......... .......... .......... 79% 22.2M 8s
402800K .......... .......... .......... .......... .......... 79% 17.1M 8s
402850K .......... .......... .......... .......... .......... 79% 16.9M 8s
402900K .......... .......... .......... .......... .......... 79% 21.9M 8s
402950K .......... .......... .......... .......... .......... 79% 19.8M 8s
403000K .......... .......... .......... .......... .......... 79% 23.6M 8s
403050K .......... .......... .......... .......... .......... 79% 20.5M 8s
403100K .......... .......... .......... .......... .......... 79% 16.4M 8s
403150K .......... .......... .......... .......... .......... 79% 15.3M 8s
403200K .......... .......... .......... .......... .......... 79% 23.4M 8s
403250K .......... .......... .......... .......... .......... 79% 17.0M 8s
403300K .......... .......... .......... .......... .......... 79% 25.3M 8s
403350K .......... .......... .......... .......... .......... 79% 11.9M 8s
403400K .......... .......... .......... .......... .......... 79% 17.7M 8s
403450K .......... .......... .......... .......... .......... 79% 14.5M 8s
403500K .......... .......... .......... .......... .......... 79% 18.8M 8s
403550K .......... .......... .......... .......... .......... 79% 15.0M 8s
403600K .......... .......... .......... .......... .......... 79% 17.1M 8s
403650K .......... .......... .......... .......... .......... 79% 22.1M 8s
403700K .......... .......... .......... .......... .......... 80% 21.1M 8s
403750K .......... .......... .......... .......... .......... 80% 24.6M 8s
403800K .......... .......... .......... .......... .......... 80% 26.8M 8s
403850K .......... .......... .......... .......... .......... 80% 16.7M 8s
403900K .......... .......... .......... .......... .......... 80% 23.0M 8s
403950K .......... .......... .......... .......... .......... 80% 12.5M 8s
404000K .......... .......... .......... .......... .......... 80% 53.6M 8s
404050K .......... .......... .......... .......... .......... 80% 28.9M 8s
404100K .......... .......... .......... .......... .......... 80% 14.9M 8s
404150K .......... .......... .......... .......... .......... 80% 46.0M 8s
404200K .......... .......... .......... .......... .......... 80% 22.0M 8s
404250K .......... .......... .......... .......... .......... 80% 23.9M 8s
404300K .......... .......... .......... .......... .......... 80% 22.9M 8s
404350K .......... .......... .......... .......... .......... 80% 18.7M 8s
404400K .......... .......... .......... .......... .......... 80% 24.0M 8s
404450K .......... .......... .......... .......... .......... 80% 23.3M 8s
404500K .......... .......... .......... .......... .......... 80% 28.3M 8s
404550K .......... .......... .......... .......... .......... 80% 23.3M 8s
404600K .......... .......... .......... .......... .......... 80% 17.9M 8s
404650K .......... .......... .......... .......... .......... 80% 31.6M 8s
404700K .......... .......... .......... .......... .......... 80% 20.9M 8s
404750K .......... .......... .......... .......... .......... 80% 20.6M 8s
404800K .......... .......... .......... .......... .......... 80% 26.6M 8s
404850K .......... .......... .......... .......... .......... 80% 17.9M 8s
404900K .......... .......... .......... .......... .......... 80% 17.1M 8s
404950K .......... .......... .......... .......... .......... 80% 17.8M 8s
405000K .......... .......... .......... .......... .......... 80% 28.2M 8s
405050K .......... .......... .......... .......... .......... 80% 33.4M 8s
405100K .......... .......... .......... .......... .......... 80% 19.9M 8s
405150K .......... .......... .......... .......... .......... 80% 74.0M 8s
405200K .......... .......... .......... .......... .......... 80% 26.4M 8s
405250K .......... .......... .......... .......... .......... 80% 32.3M 8s
405300K .......... .......... .......... .......... .......... 80% 29.8M 8s
405350K .......... .......... .......... .......... .......... 80% 26.1M 8s
405400K .......... .......... .......... .......... .......... 80% 27.0M 8s
405450K .......... .......... .......... .......... .......... 80% 30.1M 8s
405500K .......... .......... .......... .......... .......... 80% 29.6M 8s
405550K .......... .......... .......... .......... .......... 80% 31.3M 8s
405600K .......... .......... .......... .......... .......... 80% 19.4M 8s
405650K .......... .......... .......... .......... .......... 80% 37.2M 8s
405700K .......... .......... .......... .......... .......... 80% 21.2M 8s
405750K .......... .......... .......... .......... .......... 80% 42.6M 8s
405800K .......... .......... .......... .......... .......... 80% 33.9M 8s
405850K .......... .......... .......... .......... .......... 80% 25.2M 8s
405900K .......... .......... .......... .......... .......... 80% 26.2M 8s
405950K .......... .......... .......... .......... .......... 80% 28.6M 8s
406000K .......... .......... .......... .......... .......... 80% 29.9M 8s
406050K .......... .......... .......... .......... .......... 80% 29.3M 8s
406100K .......... .......... .......... .......... .......... 80% 31.3M 8s
406150K .......... .......... .......... .......... .......... 80% 28.1M 8s
406200K .......... .......... .......... .......... .......... 80% 24.9M 8s
406250K .......... .......... .......... .......... .......... 80% 60.5M 8s
406300K .......... .......... .......... .......... .......... 80% 9.90M 8s
406350K .......... .......... .......... .......... .......... 80% 96.1M 8s
406400K .......... .......... .......... .......... .......... 80%  109M 8s
406450K .......... .......... .......... .......... .......... 80% 69.5M 8s
406500K .......... .......... .......... .......... .......... 80% 33.6M 8s
406550K .......... .......... .......... .......... .......... 80% 20.7M 8s
406600K .......... .......... .......... .......... .......... 80% 61.5M 8s
406650K .......... .......... .......... .......... .......... 80% 32.6M 8s
406700K .......... .......... .......... .......... .......... 80% 22.6M 8s
406750K .......... .......... .......... .......... .......... 80% 22.7M 8s
406800K .......... .......... .......... .......... .......... 80% 35.5M 8s
406850K .......... .......... .......... .......... .......... 80% 23.6M 8s
406900K .......... .......... .......... .......... .......... 80% 26.6M 8s
406950K .......... .......... .......... .......... .......... 80% 21.0M 8s
407000K .......... .......... .......... .......... .......... 80% 25.4M 8s
407050K .......... .......... .......... .......... .......... 80% 25.8M 8s
407100K .......... .......... .......... .......... .......... 80% 24.9M 8s
407150K .......... .......... .......... .......... .......... 80% 24.3M 8s
407200K .......... .......... .......... .......... .......... 80% 22.7M 8s
407250K .......... .......... .......... .......... .......... 80% 31.0M 8s
407300K .......... .......... .......... .......... .......... 80% 26.9M 8s
407350K .......... .......... .......... .......... .......... 80% 20.8M 8s
407400K .......... .......... .......... .......... .......... 80% 26.7M 8s
407450K .......... .......... .......... .......... .......... 80% 24.4M 8s
407500K .......... .......... .......... .......... .......... 80% 12.2M 8s
407550K .......... .......... .......... .......... .......... 80% 55.5M 8s
407600K .......... .......... .......... .......... .......... 80% 9.83M 8s
407650K .......... .......... .......... .......... .......... 80% 21.7M 8s
407700K .......... .......... .......... .......... .......... 80% 11.3M 8s
407750K .......... .......... .......... .......... .......... 80% 14.3M 8s
407800K .......... .......... .......... .......... .......... 80% 14.6M 8s
407850K .......... .......... .......... .......... .......... 80% 11.6M 8s
407900K .......... .......... .......... .......... .......... 80% 13.5M 8s
407950K .......... .......... .......... .......... .......... 80% 11.0M 8s
408000K .......... .......... .......... .......... .......... 80% 14.1M 8s
408050K .......... .......... .......... .......... .......... 80% 15.4M 8s
408100K .......... .......... .......... .......... .......... 80% 10.4M 8s
408150K .......... .......... .......... .......... .......... 80% 18.2M 8s
408200K .......... .......... .......... .......... .......... 80% 8.63M 8s
408250K .......... .......... .......... .......... .......... 80% 15.4M 8s
408300K .......... .......... .......... .......... .......... 80% 19.1M 8s
408350K .......... .......... .......... .......... .......... 80% 9.30M 8s
408400K .......... .......... .......... .......... .......... 80% 12.6M 8s
408450K .......... .......... .......... .......... .......... 80% 10.7M 8s
408500K .......... .......... .......... .......... .......... 80% 12.6M 8s
408550K .......... .......... .......... .......... .......... 80% 14.1M 8s
408600K .......... .......... .......... .......... .......... 80% 10.4M 8s
408650K .......... .......... .......... .......... .......... 80% 13.0M 8s
408700K .......... .......... .......... .......... .......... 80% 12.1M 8s
408750K .......... .......... .......... .......... .......... 81% 9.94M 8s
408800K .......... .......... .......... .......... .......... 81% 12.2M 8s
408850K .......... .......... .......... .......... .......... 81% 22.0M 8s
408900K .......... .......... .......... .......... .......... 81% 27.2M 8s
408950K .......... .......... .......... .......... .......... 81% 11.5M 8s
409000K .......... .......... .......... .......... .......... 81% 81.0M 8s
409050K .......... .......... .......... .......... .......... 81% 34.0M 8s
409100K .......... .......... .......... .......... .......... 81% 19.6M 8s
409150K .......... .......... .......... .......... .......... 81% 18.0M 8s
409200K .......... .......... .......... .......... .......... 81% 16.9M 8s
409250K .......... .......... .......... .......... .......... 81% 24.8M 8s
409300K .......... .......... .......... .......... .......... 81% 25.9M 8s
409350K .......... .......... .......... .......... .......... 81% 16.7M 8s
409400K .......... .......... .......... .......... .......... 81% 23.4M 8s
409450K .......... .......... .......... .......... .......... 81% 18.6M 8s
409500K .......... .......... .......... .......... .......... 81% 20.7M 8s
409550K .......... .......... .......... .......... .......... 81% 4.15M 8s
409600K .......... .......... .......... .......... .......... 81%  108M 8s
409650K .......... .......... .......... .......... .......... 81%  167M 8s
409700K .......... .......... .......... .......... .......... 81%  168M 8s
409750K .......... .......... .......... .......... .......... 81%  470M 8s
409800K .......... .......... .......... .......... .......... 81% 51.8M 8s
409850K .......... .......... .......... .......... .......... 81% 17.8M 8s
409900K .......... .......... .......... .......... .......... 81% 20.1M 8s
409950K .......... .......... .......... .......... .......... 81% 9.94M 8s
410000K .......... .......... .......... .......... .......... 81% 17.4M 8s
410050K .......... .......... .......... .......... .......... 81% 23.1M 8s
410100K .......... .......... .......... .......... .......... 81% 9.83M 8s
410150K .......... .......... .......... .......... .......... 81% 16.4M 8s
410200K .......... .......... .......... .......... .......... 81% 14.0M 8s
410250K .......... .......... .......... .......... .......... 81% 12.7M 8s
410300K .......... .......... .......... .......... .......... 81% 11.8M 8s
410350K .......... .......... .......... .......... .......... 81% 11.1M 8s
410400K .......... .......... .......... .......... .......... 81% 18.0M 8s
410450K .......... .......... .......... .......... .......... 81% 10.4M 8s
410500K .......... .......... .......... .......... .......... 81% 14.4M 8s
410550K .......... .......... .......... .......... .......... 81% 15.6M 8s
410600K .......... .......... .......... .......... .......... 81% 15.3M 8s
410650K .......... .......... .......... .......... .......... 81% 11.2M 8s
410700K .......... .......... .......... .......... .......... 81% 74.9M 7s
410750K .......... .......... .......... .......... .......... 81% 17.9M 7s
410800K .......... .......... .......... .......... .......... 81% 21.3M 7s
410850K .......... .......... .......... .......... .......... 81% 17.5M 7s
410900K .......... .......... .......... .......... .......... 81% 23.6M 7s
410950K .......... .......... .......... .......... .......... 81% 13.4M 7s
411000K .......... .......... .......... .......... .......... 81% 25.0M 7s
411050K .......... .......... .......... .......... .......... 81% 22.4M 7s
411100K .......... .......... .......... .......... .......... 81% 19.1M 7s
411150K .......... .......... .......... .......... .......... 81% 23.5M 7s
411200K .......... .......... .......... .......... .......... 81% 17.6M 7s
411250K .......... .......... .......... .......... .......... 81% 20.7M 7s
411300K .......... .......... .......... .......... .......... 81% 18.6M 7s
411350K .......... .......... .......... .......... .......... 81% 22.9M 7s
411400K .......... .......... .......... .......... .......... 81% 18.8M 7s
411450K .......... .......... .......... .......... .......... 81% 21.4M 7s
411500K .......... .......... .......... .......... .......... 81% 21.5M 7s
411550K .......... .......... .......... .......... .......... 81% 28.8M 7s
411600K .......... .......... .......... .......... .......... 81% 30.8M 7s
411650K .......... .......... .......... .......... .......... 81% 53.7M 7s
411700K .......... .......... .......... .......... .......... 81% 62.0M 7s
411750K .......... .......... .......... .......... .......... 81% 31.3M 7s
411800K .......... .......... .......... .......... .......... 81% 41.9M 7s
411850K .......... .......... .......... .......... .......... 81% 14.6M 7s
411900K .......... .......... .......... .......... .......... 81% 90.6M 7s
411950K .......... .......... .......... .......... .......... 81% 72.9M 7s
412000K .......... .......... .......... .......... .......... 81% 19.5M 7s
412050K .......... .......... .......... .......... .......... 81% 96.7M 7s
412100K .......... .......... .......... .......... .......... 81% 17.3M 7s
412150K .......... .......... .......... .......... .......... 81% 67.8M 7s
412200K .......... .......... .......... .......... .......... 81% 23.1M 7s
412250K .......... .......... .......... .......... .......... 81% 27.1M 7s
412300K .......... .......... .......... .......... .......... 81% 30.9M 7s
412350K .......... .......... .......... .......... .......... 81% 27.4M 7s
412400K .......... .......... .......... .......... .......... 81% 27.8M 7s
412450K .......... .......... .......... .......... .......... 81% 31.2M 7s
412500K .......... .......... .......... .......... .......... 81% 21.9M 7s
412550K .......... .......... .......... .......... .......... 81% 29.1M 7s
412600K .......... .......... .......... .......... .......... 81% 17.0M 7s
412650K .......... .......... .......... .......... .......... 81% 61.8M 7s
412700K .......... .......... .......... .......... .......... 81% 20.0M 7s
412750K .......... .......... .......... .......... .......... 81% 23.1M 7s
412800K .......... .......... .......... .......... .......... 81% 28.7M 7s
412850K .......... .......... .......... .......... .......... 81% 26.7M 7s
412900K .......... .......... .......... .......... .......... 81% 27.1M 7s
412950K .......... .......... .......... .......... .......... 81% 22.7M 7s
413000K .......... .......... .......... .......... .......... 81% 22.2M 7s
413050K .......... .......... .......... .......... .......... 81% 31.6M 7s
413100K .......... .......... .......... .......... .......... 81% 15.5M 7s
413150K .......... .......... .......... .......... .......... 81% 11.8M 7s
413200K .......... .......... .......... .......... .......... 81% 13.4M 7s
413250K .......... .......... .......... .......... .......... 81% 12.4M 7s
413300K .......... .......... .......... .......... .......... 81% 11.2M 7s
413350K .......... .......... .......... .......... .......... 81% 11.0M 7s
413400K .......... .......... .......... .......... .......... 81% 10.5M 7s
413450K .......... .......... .......... .......... .......... 81% 8.57M 7s
413500K .......... .......... .......... .......... .......... 81% 11.5M 7s
413550K .......... .......... .......... .......... .......... 81% 12.1M 7s
413600K .......... .......... .......... .......... .......... 81% 5.27M 7s
413650K .......... .......... .......... .......... .......... 81% 18.1M 7s
413700K .......... .......... .......... .......... .......... 81% 7.46M 7s
413750K .......... .......... .......... .......... .......... 81% 12.1M 7s
413800K .......... .......... .......... .......... .......... 82% 11.8M 7s
413850K .......... .......... .......... .......... .......... 82% 10.7M 7s
413900K .......... .......... .......... .......... .......... 82% 8.66M 7s
413950K .......... .......... .......... .......... .......... 82% 20.7M 7s
414000K .......... .......... .......... .......... .......... 82% 12.2M 7s
414050K .......... .......... .......... .......... .......... 82% 12.1M 7s
414100K .......... .......... .......... .......... .......... 82% 10.2M 7s
414150K .......... .......... .......... .......... .......... 82% 20.3M 7s
414200K .......... .......... .......... .......... .......... 82% 11.0M 7s
414250K .......... .......... .......... .......... .......... 82% 68.1M 7s
414300K .......... .......... .......... .......... .......... 82% 10.4M 7s
414350K .......... .......... .......... .......... .......... 82% 23.5M 7s
414400K .......... .......... .......... .......... .......... 82% 16.8M 7s
414450K .......... .......... .......... .......... .......... 82% 13.0M 7s
414500K .......... .......... .......... .......... .......... 82% 16.4M 7s
414550K .......... .......... .......... .......... .......... 82% 19.0M 7s
414600K .......... .......... .......... .......... .......... 82% 15.5M 7s
414650K .......... .......... .......... .......... .......... 82% 15.8M 7s
414700K .......... .......... .......... .......... .......... 82% 14.4M 7s
414750K .......... .......... .......... .......... .......... 82% 15.4M 7s
414800K .......... .......... .......... .......... .......... 82% 19.2M 7s
414850K .......... .......... .......... .......... .......... 82% 13.8M 7s
414900K .......... .......... .......... .......... .......... 82% 22.2M 7s
414950K .......... .......... .......... .......... .......... 82% 20.2M 7s
415000K .......... .......... .......... .......... .......... 82% 35.0M 7s
415050K .......... .......... .......... .......... .......... 82% 21.9M 7s
415100K .......... .......... .......... .......... .......... 82% 22.5M 7s
415150K .......... .......... .......... .......... .......... 82% 7.70M 7s
415200K .......... .......... .......... .......... .......... 82% 68.1M 7s
415250K .......... .......... .......... .......... .......... 82% 82.3M 7s
415300K .......... .......... .......... .......... .......... 82% 37.0M 7s
415350K .......... .......... .......... .......... .......... 82% 19.9M 7s
415400K .......... .......... .......... .......... .......... 82% 18.7M 7s
415450K .......... .......... .......... .......... .......... 82% 22.0M 7s
415500K .......... .......... .......... .......... .......... 82% 20.8M 7s
415550K .......... .......... .......... .......... .......... 82% 18.7M 7s
415600K .......... .......... .......... .......... .......... 82% 17.8M 7s
415650K .......... .......... .......... .......... .......... 82% 18.7M 7s
415700K .......... .......... .......... .......... .......... 82% 16.4M 7s
415750K .......... .......... .......... .......... .......... 82% 21.1M 7s
415800K .......... .......... .......... .......... .......... 82% 21.5M 7s
415850K .......... .......... .......... .......... .......... 82% 18.1M 7s
415900K .......... .......... .......... .......... .......... 82% 21.4M 7s
415950K .......... .......... .......... .......... .......... 82% 16.7M 7s
416000K .......... .......... .......... .......... .......... 82% 12.2M 7s
416050K .......... .......... .......... .......... .......... 82% 9.23M 7s
416100K .......... .......... .......... .......... .......... 82% 30.8M 7s
416150K .......... .......... .......... .......... .......... 82% 23.9M 7s
416200K .......... .......... .......... .......... .......... 82% 17.8M 7s
416250K .......... .......... .......... .......... .......... 82% 19.5M 7s
416300K .......... .......... .......... .......... .......... 82% 22.2M 7s
416350K .......... .......... .......... .......... .......... 82% 15.6M 7s
416400K .......... .......... .......... .......... .......... 82% 17.8M 7s
416450K .......... .......... .......... .......... .......... 82% 15.5M 7s
416500K .......... .......... .......... .......... .......... 82% 16.3M 7s
416550K .......... .......... .......... .......... .......... 82% 18.6M 7s
416600K .......... .......... .......... .......... .......... 82% 15.0M 7s
416650K .......... .......... .......... .......... .......... 82% 15.1M 7s
416700K .......... .......... .......... .......... .......... 82% 15.0M 7s
416750K .......... .......... .......... .......... .......... 82% 15.6M 7s
416800K .......... .......... .......... .......... .......... 82% 15.7M 7s
416850K .......... .......... .......... .......... .......... 82% 18.0M 7s
416900K .......... .......... .......... .......... .......... 82% 26.3M 7s
416950K .......... .......... .......... .......... .......... 82% 9.72M 7s
417000K .......... .......... .......... .......... .......... 82% 75.0M 7s
417050K .......... .......... .......... .......... .......... 82% 9.90M 7s
417100K .......... .......... .......... .......... .......... 82% 42.1M 7s
417150K .......... .......... .......... .......... .......... 82% 19.7M 7s
417200K .......... .......... .......... .......... .......... 82% 16.6M 7s
417250K .......... .......... .......... .......... .......... 82% 20.5M 7s
417300K .......... .......... .......... .......... .......... 82% 12.2M 7s
417350K .......... .......... .......... .......... .......... 82% 19.4M 7s
417400K .......... .......... .......... .......... .......... 82% 19.8M 7s
417450K .......... .......... .......... .......... .......... 82% 16.4M 7s
417500K .......... .......... .......... .......... .......... 82% 22.2M 7s
417550K .......... .......... .......... .......... .......... 82% 20.9M 7s
417600K .......... .......... .......... .......... .......... 82% 16.8M 7s
417650K .......... .......... .......... .......... .......... 82% 19.7M 7s
417700K .......... .......... .......... .......... .......... 82% 20.7M 7s
417750K .......... .......... .......... .......... .......... 82% 17.1M 7s
417800K .......... .......... .......... .......... .......... 82% 17.1M 7s
417850K .......... .......... .......... .......... .......... 82% 17.1M 7s
417900K .......... .......... .......... .......... .......... 82% 10.5M 7s
417950K .......... .......... .......... .......... .......... 82% 17.0M 7s
418000K .......... .......... .......... .......... .......... 82% 15.1M 7s
418050K .......... .......... .......... .......... .......... 82% 9.48M 7s
418100K .......... .......... .......... .......... .......... 82% 8.15M 7s
418150K .......... .......... .......... .......... .......... 82% 10.9M 7s
418200K .......... .......... .......... .......... .......... 82% 8.38M 7s
418250K .......... .......... .......... .......... .......... 82% 11.9M 7s
418300K .......... .......... .......... .......... .......... 82% 12.8M 7s
418350K .......... .......... .......... .......... .......... 82% 9.71M 7s
418400K .......... .......... .......... .......... .......... 82% 12.1M 7s
418450K .......... .......... .......... .......... .......... 82% 23.4M 7s
418500K .......... .......... .......... .......... .......... 82% 31.4M 7s
418550K .......... .......... .......... .......... .......... 82% 34.1M 7s
418600K .......... .......... .......... .......... .......... 82% 23.5M 7s
418650K .......... .......... .......... .......... .......... 82% 23.4M 7s
418700K .......... .......... .......... .......... .......... 82% 26.1M 7s
418750K .......... .......... .......... .......... .......... 82% 31.3M 7s
418800K .......... .......... .......... .......... .......... 82% 17.1M 7s
418850K .......... .......... .......... .......... .......... 83% 28.9M 7s
418900K .......... .......... .......... .......... .......... 83% 18.7M 7s
418950K .......... .......... .......... .......... .......... 83% 23.5M 7s
419000K .......... .......... .......... .......... .......... 83% 24.8M 7s
419050K .......... .......... .......... .......... .......... 83% 29.3M 7s
419100K .......... .......... .......... .......... .......... 83% 16.4M 7s
419150K .......... .......... .......... .......... .......... 83% 24.7M 7s
419200K .......... .......... .......... .......... .......... 83% 17.2M 7s
419250K .......... .......... .......... .......... .......... 83% 12.0M 7s
419300K .......... .......... .......... .......... .......... 83% 20.7M 7s
419350K .......... .......... .......... .......... .......... 83% 19.9M 7s
419400K .......... .......... .......... .......... .......... 83% 16.1M 7s
419450K .......... .......... .......... .......... .......... 83% 12.1M 7s
419500K .......... .......... .......... .......... .......... 83% 17.7M 7s
419550K .......... .......... .......... .......... .......... 83% 19.7M 7s
419600K .......... .......... .......... .......... .......... 83% 17.2M 7s
419650K .......... .......... .......... .......... .......... 83% 16.7M 7s
419700K .......... .......... .......... .......... .......... 83% 16.2M 7s
419750K .......... .......... .......... .......... .......... 83% 13.4M 7s
419800K .......... .......... .......... .......... .......... 83% 18.7M 7s
419850K .......... .......... .......... .......... .......... 83% 13.9M 7s
419900K .......... .......... .......... .......... .......... 83% 17.7M 7s
419950K .......... .......... .......... .......... .......... 83% 15.1M 7s
420000K .......... .......... .......... .......... .......... 83% 16.3M 7s
420050K .......... .......... .......... .......... .......... 83% 18.2M 7s
420100K .......... .......... .......... .......... .......... 83% 8.57M 7s
420150K .......... .......... .......... .......... .......... 83% 11.2M 7s
420200K .......... .......... .......... .......... .......... 83% 12.9M 7s
420250K .......... .......... .......... .......... .......... 83% 13.0M 7s
420300K .......... .......... .......... .......... .......... 83% 18.8M 7s
420350K .......... .......... .......... .......... .......... 83% 14.4M 7s
420400K .......... .......... .......... .......... .......... 83% 41.5M 7s
420450K .......... .......... .......... .......... .......... 83% 13.7M 7s
420500K .......... .......... .......... .......... .......... 83% 25.6M 7s
420550K .......... .......... .......... .......... .......... 83% 12.6M 7s
420600K .......... .......... .......... .......... .......... 83% 11.4M 7s
420650K .......... .......... .......... .......... .......... 83% 13.2M 7s
420700K .......... .......... .......... .......... .......... 83% 14.1M 7s
420750K .......... .......... .......... .......... .......... 83% 13.1M 7s
420800K .......... .......... .......... .......... .......... 83% 15.6M 7s
420850K .......... .......... .......... .......... .......... 83% 10.0M 7s
420900K .......... .......... .......... .......... .......... 83% 15.1M 7s
420950K .......... .......... .......... .......... .......... 83% 6.03M 7s
421000K .......... .......... .......... .......... .......... 83% 10.5M 7s
421050K .......... .......... .......... .......... .......... 83% 61.4M 7s
421100K .......... .......... .......... .......... .......... 83% 17.4M 7s
421150K .......... .......... .......... .......... .......... 83% 21.9M 7s
421200K .......... .......... .......... .......... .......... 83% 14.0M 7s
421250K .......... .......... .......... .......... .......... 83% 25.3M 7s
421300K .......... .......... .......... .......... .......... 83% 17.0M 7s
421350K .......... .......... .......... .......... .......... 83% 17.2M 7s
421400K .......... .......... .......... .......... .......... 83% 21.7M 7s
421450K .......... .......... .......... .......... .......... 83% 18.9M 7s
421500K .......... .......... .......... .......... .......... 83% 24.8M 7s
421550K .......... .......... .......... .......... .......... 83% 19.6M 7s
421600K .......... .......... .......... .......... .......... 83% 21.5M 7s
421650K .......... .......... .......... .......... .......... 83% 30.9M 7s
421700K .......... .......... .......... .......... .......... 83% 19.2M 7s
421750K .......... .......... .......... .......... .......... 83% 22.5M 7s
421800K .......... .......... .......... .......... .......... 83% 20.9M 7s
421850K .......... .......... .......... .......... .......... 83% 21.6M 7s
421900K .......... .......... .......... .......... .......... 83% 31.0M 7s
421950K .......... .......... .......... .......... .......... 83% 19.7M 7s
422000K .......... .......... .......... .......... .......... 83% 33.2M 7s
422050K .......... .......... .......... .......... .......... 83% 83.5M 7s
422100K .......... .......... .......... .......... .......... 83% 21.4M 7s
422150K .......... .......... .......... .......... .......... 83% 29.6M 7s
422200K .......... .......... .......... .......... .......... 83% 40.9M 7s
422250K .......... .......... .......... .......... .......... 83% 17.9M 7s
422300K .......... .......... .......... .......... .......... 83% 18.9M 7s
422350K .......... .......... .......... .......... .......... 83% 14.8M 7s
422400K .......... .......... .......... .......... .......... 83% 18.7M 7s
422450K .......... .......... .......... .......... .......... 83% 16.3M 7s
422500K .......... .......... .......... .......... .......... 83% 17.8M 7s
422550K .......... .......... .......... .......... .......... 83% 18.8M 6s
422600K .......... .......... .......... .......... .......... 83% 16.4M 6s
422650K .......... .......... .......... .......... .......... 83% 19.8M 6s
422700K .......... .......... .......... .......... .......... 83% 16.8M 6s
422750K .......... .......... .......... .......... .......... 83% 18.7M 6s
422800K .......... .......... .......... .......... .......... 83% 15.7M 6s
422850K .......... .......... .......... .......... .......... 83% 19.8M 6s
422900K .......... .......... .......... .......... .......... 83% 31.0M 6s
422950K .......... .......... .......... .......... .......... 83% 11.0M 6s
423000K .......... .......... .......... .......... .......... 83% 55.0M 6s
423050K .......... .......... .......... .......... .......... 83% 12.5M 6s
423100K .......... .......... .......... .......... .......... 83% 28.8M 6s
423150K .......... .......... .......... .......... .......... 83% 13.0M 6s
423200K .......... .......... .......... .......... .......... 83% 11.8M 6s
423250K .......... .......... .......... .......... .......... 83% 16.3M 6s
423300K .......... .......... .......... .......... .......... 83% 13.9M 6s
423350K .......... .......... .......... .......... .......... 83% 12.9M 6s
423400K .......... .......... .......... .......... .......... 83% 13.9M 6s
423450K .......... .......... .......... .......... .......... 83% 12.2M 6s
423500K .......... .......... .......... .......... .......... 83% 14.8M 6s
423550K .......... .......... .......... .......... .......... 83% 14.1M 6s
423600K .......... .......... .......... .......... .......... 83% 18.3M 6s
423650K .......... .......... .......... .......... .......... 83% 24.1M 6s
423700K .......... .......... .......... .......... .......... 83% 8.18M 6s
423750K .......... .......... .......... .......... .......... 83% 81.4M 6s
423800K .......... .......... .......... .......... .......... 83% 14.7M 6s
423850K .......... .......... .......... .......... .......... 83% 15.8M 6s
423900K .......... .......... .......... .......... .......... 84% 40.5M 6s
423950K .......... .......... .......... .......... .......... 84% 21.8M 6s
424000K .......... .......... .......... .......... .......... 84% 23.6M 6s
424050K .......... .......... .......... .......... .......... 84% 27.2M 6s
424100K .......... .......... .......... .......... .......... 84% 20.6M 6s
424150K .......... .......... .......... .......... .......... 84% 24.8M 6s
424200K .......... .......... .......... .......... .......... 84% 18.8M 6s
424250K .......... .......... .......... .......... .......... 84% 30.8M 6s
424300K .......... .......... .......... .......... .......... 84% 26.4M 6s
424350K .......... .......... .......... .......... .......... 84% 18.7M 6s
424400K .......... .......... .......... .......... .......... 84% 26.7M 6s
424450K .......... .......... .......... .......... .......... 84% 24.8M 6s
424500K .......... .......... .......... .......... .......... 84% 26.7M 6s
424550K .......... .......... .......... .......... .......... 84% 25.0M 6s
424600K .......... .......... .......... .......... .......... 84% 22.2M 6s
424650K .......... .......... .......... .......... .......... 84% 28.9M 6s
424700K .......... .......... .......... .......... .......... 84% 20.7M 6s
424750K .......... .......... .......... .......... .......... 84% 33.4M 6s
424800K .......... .......... .......... .......... .......... 84% 40.1M 6s
424850K .......... .......... .......... .......... .......... 84% 41.7M 6s
424900K .......... .......... .......... .......... .......... 84% 16.2M 6s
424950K .......... .......... .......... .......... .......... 84% 22.5M 6s
425000K .......... .......... .......... .......... .......... 84%  108M 6s
425050K .......... .......... .......... .......... .......... 84% 63.2M 6s
425100K .......... .......... .......... .......... .......... 84% 27.3M 6s
425150K .......... .......... .......... .......... .......... 84% 49.8M 6s
425200K .......... .......... .......... .......... .......... 84% 27.4M 6s
425250K .......... .......... .......... .......... .......... 84% 61.7M 6s
425300K .......... .......... .......... .......... .......... 84% 41.8M 6s
425350K .......... .......... .......... .......... .......... 84% 29.3M 6s
425400K .......... .......... .......... .......... .......... 84% 36.9M 6s
425450K .......... .......... .......... .......... .......... 84% 28.9M 6s
425500K .......... .......... .......... .......... .......... 84% 34.9M 6s
425550K .......... .......... .......... .......... .......... 84% 32.6M 6s
425600K .......... .......... .......... .......... .......... 84% 35.5M 6s
425650K .......... .......... .......... .......... .......... 84% 30.4M 6s
425700K .......... .......... .......... .......... .......... 84% 33.1M 6s
425750K .......... .......... .......... .......... .......... 84% 34.1M 6s
425800K .......... .......... .......... .......... .......... 84% 43.6M 6s
425850K .......... .......... .......... .......... .......... 84% 30.3M 6s
425900K .......... .......... .......... .......... .......... 84% 43.2M 6s
425950K .......... .......... .......... .......... .......... 84% 28.8M 6s
426000K .......... .......... .......... .......... .......... 84% 44.1M 6s
426050K .......... .......... .......... .......... .......... 84% 30.0M 6s
426100K .......... .......... .......... .......... .......... 84% 29.6M 6s
426150K .......... .......... .......... .......... .......... 84% 37.5M 6s
426200K .......... .......... .......... .......... .......... 84% 32.0M 6s
426250K .......... .......... .......... .......... .......... 84% 39.1M 6s
426300K .......... .......... .......... .......... .......... 84% 37.5M 6s
426350K .......... .......... .......... .......... .......... 84% 31.5M 6s
426400K .......... .......... .......... .......... .......... 84% 39.2M 6s
426450K .......... .......... .......... .......... .......... 84% 29.9M 6s
426500K .......... .......... .......... .......... .......... 84% 57.5M 6s
426550K .......... .......... .......... .......... .......... 84% 49.9M 6s
426600K .......... .......... .......... .......... .......... 84% 13.7M 6s
426650K .......... .......... .......... .......... .......... 84%  127M 6s
426700K .......... .......... .......... .......... .......... 84%  146M 6s
426750K .......... .......... .......... .......... .......... 84% 26.4M 6s
426800K .......... .......... .......... .......... .......... 84% 20.4M 6s
426850K .......... .......... .......... .......... .......... 84%  135M 6s
426900K .......... .......... .......... .......... .......... 84%  157M 6s
426950K .......... .......... .......... .......... .......... 84%  145M 6s
427000K .......... .......... .......... .......... .......... 84%  138M 6s
427050K .......... .......... .......... .......... .......... 84% 35.1M 6s
427100K .......... .......... .......... .......... .......... 84% 31.3M 6s
427150K .......... .......... .......... .......... .......... 84% 32.7M 6s
427200K .......... .......... .......... .......... .......... 84% 37.3M 6s
427250K .......... .......... .......... .......... .......... 84% 38.6M 6s
427300K .......... .......... .......... .......... .......... 84% 19.4M 6s
427350K .......... .......... .......... .......... .......... 84%  161M 6s
427400K .......... .......... .......... .......... .......... 84% 32.0M 6s
427450K .......... .......... .......... .......... .......... 84% 25.1M 6s
427500K .......... .......... .......... .......... .......... 84% 46.2M 6s
427550K .......... .......... .......... .......... .......... 84% 25.1M 6s
427600K .......... .......... .......... .......... .......... 84% 31.3M 6s
427650K .......... .......... .......... .......... .......... 84% 31.1M 6s
427700K .......... .......... .......... .......... .......... 84% 26.6M 6s
427750K .......... .......... .......... .......... .......... 84% 46.9M 6s
427800K .......... .......... .......... .......... .......... 84% 30.8M 6s
427850K .......... .......... .......... .......... .......... 84% 34.1M 6s
427900K .......... .......... .......... .......... .......... 84% 37.4M 6s
427950K .......... .......... .......... .......... .......... 84% 24.8M 6s
428000K .......... .......... .......... .......... .......... 84% 37.9M 6s
428050K .......... .......... .......... .......... .......... 84% 34.6M 6s
428100K .......... .......... .......... .......... .......... 84% 27.7M 6s
428150K .......... .......... .......... .......... .......... 84% 29.2M 6s
428200K .......... .......... .......... .......... .......... 84% 23.6M 6s
428250K .......... .......... .......... .......... .......... 84% 15.4M 6s
428300K .......... .......... .......... .......... .......... 84% 9.48M 6s
428350K .......... .......... .......... .......... .......... 84% 39.6M 6s
428400K .......... .......... .......... .......... .......... 84% 26.7M 6s
428450K .......... .......... .......... .......... .......... 84% 23.1M 6s
428500K .......... .......... .......... .......... .......... 84% 26.9M 6s
428550K .......... .......... .......... .......... .......... 84% 22.9M 6s
428600K .......... .......... .......... .......... .......... 84% 22.1M 6s
428650K .......... .......... .......... .......... .......... 84% 23.9M 6s
428700K .......... .......... .......... .......... .......... 84% 15.7M 6s
428750K .......... .......... .......... .......... .......... 84% 33.6M 6s
428800K .......... .......... .......... .......... .......... 84% 20.9M 6s
428850K .......... .......... .......... .......... .......... 84% 17.8M 6s
428900K .......... .......... .......... .......... .......... 84% 23.3M 6s
428950K .......... .......... .......... .......... .......... 85% 22.0M 6s
429000K .......... .......... .......... .......... .......... 85% 21.0M 6s
429050K .......... .......... .......... .......... .......... 85% 26.7M 6s
429100K .......... .......... .......... .......... .......... 85% 21.8M 6s
429150K .......... .......... .......... .......... .......... 85% 22.1M 6s
429200K .......... .......... .......... .......... .......... 85% 16.8M 6s
429250K .......... .......... .......... .......... .......... 85%  117M 6s
429300K .......... .......... .......... .......... .......... 85% 68.4M 6s
429350K .......... .......... .......... .......... .......... 85% 58.4M 6s
429400K .......... .......... .......... .......... .......... 85% 16.7M 6s
429450K .......... .......... .......... .......... .......... 85% 32.7M 6s
429500K .......... .......... .......... .......... .......... 85% 49.4M 6s
429550K .......... .......... .......... .......... .......... 85% 69.4M 6s
429600K .......... .......... .......... .......... .......... 85% 21.3M 6s
429650K .......... .......... .......... .......... .......... 85% 24.2M 6s
429700K .......... .......... .......... .......... .......... 85% 36.8M 6s
429750K .......... .......... .......... .......... .......... 85% 25.1M 6s
429800K .......... .......... .......... .......... .......... 85% 39.2M 6s
429850K .......... .......... .......... .......... .......... 85% 25.8M 6s
429900K .......... .......... .......... .......... .......... 85% 31.1M 6s
429950K .......... .......... .......... .......... .......... 85% 17.8M 6s
430000K .......... .......... .......... .......... .......... 85% 37.0M 6s
430050K .......... .......... .......... .......... .......... 85% 22.1M 6s
430100K .......... .......... .......... .......... .......... 85% 16.4M 6s
430150K .......... .......... .......... .......... .......... 85% 26.6M 6s
430200K .......... .......... .......... .......... .......... 85% 23.4M 6s
430250K .......... .......... .......... .......... .......... 85% 19.0M 6s
430300K .......... .......... .......... .......... .......... 85% 33.3M 6s
430350K .......... .......... .......... .......... .......... 85% 16.4M 6s
430400K .......... .......... .......... .......... .......... 85% 23.6M 6s
430450K .......... .......... .......... .......... .......... 85% 18.8M 6s
430500K .......... .......... .......... .......... .......... 85% 12.5M 6s
430550K .......... .......... .......... .......... .......... 85% 8.80M 6s
430600K .......... .......... .......... .......... .......... 85% 16.2M 6s
430650K .......... .......... .......... .......... .......... 85% 15.7M 6s
430700K .......... .......... .......... .......... .......... 85% 9.04M 6s
430750K .......... .......... .......... .......... .......... 85% 15.7M 6s
430800K .......... .......... .......... .......... .......... 85% 13.0M 6s
430850K .......... .......... .......... .......... .......... 85% 11.4M 6s
430900K .......... .......... .......... .......... .......... 85% 12.1M 6s
430950K .......... .......... .......... .......... .......... 85% 11.1M 6s
431000K .......... .......... .......... .......... .......... 85% 12.5M 6s
431050K .......... .......... .......... .......... .......... 85% 8.84M 6s
431100K .......... .......... .......... .......... .......... 85% 13.6M 6s
431150K .......... .......... .......... .......... .......... 85% 31.1M 6s
431200K .......... .......... .......... .......... .......... 85% 12.5M 6s
431250K .......... .......... .......... .......... .......... 85% 84.0M 6s
431300K .......... .......... .......... .......... .......... 85% 29.4M 6s
431350K .......... .......... .......... .......... .......... 85% 29.3M 6s
431400K .......... .......... .......... .......... .......... 85% 15.7M 6s
431450K .......... .......... .......... .......... .......... 85% 21.8M 6s
431500K .......... .......... .......... .......... .......... 85% 20.0M 6s
431550K .......... .......... .......... .......... .......... 85% 19.7M 6s
431600K .......... .......... .......... .......... .......... 85% 17.1M 6s
431650K .......... .......... .......... .......... .......... 85% 22.2M 6s
431700K .......... .......... .......... .......... .......... 85% 16.9M 6s
431750K .......... .......... .......... .......... .......... 85% 22.3M 6s
431800K .......... .......... .......... .......... .......... 85% 21.7M 6s
431850K .......... .......... .......... .......... .......... 85% 17.1M 6s
431900K .......... .......... .......... .......... .......... 85% 22.3M 6s
431950K .......... .......... .......... .......... .......... 85% 19.5M 6s
432000K .......... .......... .......... .......... .......... 85% 20.4M 6s
432050K .......... .......... .......... .......... .......... 85% 20.2M 6s
432100K .......... .......... .......... .......... .......... 85% 13.4M 6s
432150K .......... .......... .......... .......... .......... 85% 21.4M 6s
432200K .......... .......... .......... .......... .......... 85% 8.52M 6s
432250K .......... .......... .......... .......... .......... 85% 25.3M 6s
432300K .......... .......... .......... .......... .......... 85% 42.8M 6s
432350K .......... .......... .......... .......... .......... 85% 16.2M 6s
432400K .......... .......... .......... .......... .......... 85% 23.8M 6s
432450K .......... .......... .......... .......... .......... 85% 14.2M 6s
432500K .......... .......... .......... .......... .......... 85% 19.5M 6s
432550K .......... .......... .......... .......... .......... 85% 17.9M 6s
432600K .......... .......... .......... .......... .......... 85% 16.3M 6s
432650K .......... .......... .......... .......... .......... 85% 23.3M 6s
432700K .......... .......... .......... .......... .......... 85% 16.3M 6s
432750K .......... .......... .......... .......... .......... 85% 17.1M 6s
432800K .......... .......... .......... .......... .......... 85% 14.9M 6s
432850K .......... .......... .......... .......... .......... 85% 13.5M 6s
432900K .......... .......... .......... .......... .......... 85% 17.0M 6s
432950K .......... .......... .......... .......... .......... 85% 12.5M 6s
433000K .......... .......... .......... .......... .......... 85% 16.5M 6s
433050K .......... .......... .......... .......... .......... 85% 13.8M 6s
433100K .......... .......... .......... .......... .......... 85% 12.5M 6s
433150K .......... .......... .......... .......... .......... 85% 8.38M 6s
433200K .......... .......... .......... .......... .......... 85% 9.04M 6s
433250K .......... .......... .......... .......... .......... 85% 12.5M 6s
433300K .......... .......... .......... .......... .......... 85% 12.1M 6s
433350K .......... .......... .......... .......... .......... 85% 13.9M 6s
433400K .......... .......... .......... .......... .......... 85% 12.9M 6s
433450K .......... .......... .......... .......... .......... 85% 11.9M 6s
433500K .......... .......... .......... .......... .......... 85% 14.2M 6s
433550K .......... .......... .......... .......... .......... 85% 12.5M 6s
433600K .......... .......... .......... .......... .......... 85% 13.0M 6s
433650K .......... .......... .......... .......... .......... 85% 13.5M 6s
433700K .......... .......... .......... .......... .......... 85% 9.48M 6s
433750K .......... .......... .......... .......... .......... 85% 11.2M 6s
433800K .......... .......... .......... .......... .......... 85% 11.3M 6s
433850K .......... .......... .......... .......... .......... 85% 13.9M 6s
433900K .......... .......... .......... .......... .......... 85% 13.5M 6s
433950K .......... .......... .......... .......... .......... 85% 13.3M 6s
434000K .......... .......... .......... .......... .......... 86% 14.5M 6s
434050K .......... .......... .......... .......... .......... 86% 15.5M 6s
434100K .......... .......... .......... .......... .......... 86% 12.2M 6s
434150K .......... .......... .......... .......... .......... 86% 11.4M 6s
434200K .......... .......... .......... .......... .......... 86% 12.9M 6s
434250K .......... .......... .......... .......... .......... 86% 14.0M 6s
434300K .......... .......... .......... .......... .......... 86% 19.8M 6s
434350K .......... .......... .......... .......... .......... 86% 13.8M 6s
434400K .......... .......... .......... .......... .......... 86% 23.1M 6s
434450K .......... .......... .......... .......... .......... 86% 25.6M 5s
434500K .......... .......... .......... .......... .......... 86% 27.9M 5s
434550K .......... .......... .......... .......... .......... 86% 13.4M 5s
434600K .......... .......... .......... .......... .......... 86% 16.3M 5s
434650K .......... .......... .......... .......... .......... 86% 31.2M 5s
434700K .......... .......... .......... .......... .......... 86% 11.4M 5s
434750K .......... .......... .......... .......... .......... 86% 13.9M 5s
434800K .......... .......... .......... .......... .......... 86% 15.7M 5s
434850K .......... .......... .......... .......... .......... 86% 11.0M 5s
434900K .......... .......... .......... .......... .......... 86% 15.7M 5s
434950K .......... .......... .......... .......... .......... 86% 11.7M 5s
435000K .......... .......... .......... .......... .......... 86% 13.0M 5s
435050K .......... .......... .......... .......... .......... 86% 13.9M 5s
435100K .......... .......... .......... .......... .......... 86% 13.5M 5s
435150K .......... .......... .......... .......... .......... 86% 13.4M 5s
435200K .......... .......... .......... .......... .......... 86% 18.7M 5s
435250K .......... .......... .......... .......... .......... 86% 25.5M 5s
435300K .......... .......... .......... .......... .......... 86% 33.4M 5s
435350K .......... .......... .......... .......... .......... 86% 14.5M 5s
435400K .......... .......... .......... .......... .......... 86% 28.9M 5s
435450K .......... .......... .......... .......... .......... 86% 21.5M 5s
435500K .......... .......... .......... .......... .......... 86% 18.3M 5s
435550K .......... .......... .......... .......... .......... 86% 22.2M 5s
435600K .......... .......... .......... .......... .......... 86% 14.3M 5s
435650K .......... .......... .......... .......... .......... 86% 23.5M 5s
435700K .......... .......... .......... .......... .......... 86% 15.1M 5s
435750K .......... .......... .......... .......... .......... 86% 21.6M 5s
435800K .......... .......... .......... .......... .......... 86% 17.9M 5s
435850K .......... .......... .......... .......... .......... 86% 16.2M 5s
435900K .......... .......... .......... .......... .......... 86% 16.9M 5s
435950K .......... .......... .......... .......... .......... 86% 18.0M 5s
436000K .......... .......... .......... .......... .......... 86% 19.5M 5s
436050K .......... .......... .......... .......... .......... 86% 16.2M 5s
436100K .......... .......... .......... .......... .......... 86% 17.9M 5s
436150K .......... .......... .......... .......... .......... 86% 12.3M 5s
436200K .......... .......... .......... .......... .......... 86% 66.9M 5s
436250K .......... .......... .......... .......... .......... 86% 13.5M 5s
436300K .......... .......... .......... .......... .......... 86% 20.0M 5s
436350K .......... .......... .......... .......... .......... 86% 15.9M 5s
436400K .......... .......... .......... .......... .......... 86% 12.4M 5s
436450K .......... .......... .......... .......... .......... 86% 12.5M 5s
436500K .......... .......... .......... .......... .......... 86% 15.7M 5s
436550K .......... .......... .......... .......... .......... 86% 15.0M 5s
436600K .......... .......... .......... .......... .......... 86% 12.9M 5s
436650K .......... .......... .......... .......... .......... 86% 17.0M 5s
436700K .......... .......... .......... .......... .......... 86% 13.0M 5s
436750K .......... .......... .......... .......... .......... 86% 14.5M 5s
436800K .......... .......... .......... .......... .......... 86% 17.9M 5s
436850K .......... .......... .......... .......... .......... 86% 17.1M 5s
436900K .......... .......... .......... .......... .......... 86% 43.2M 5s
436950K .......... .......... .......... .......... .......... 86% 36.2M 5s
437000K .......... .......... .......... .......... .......... 86% 53.7M 5s
437050K .......... .......... .......... .......... .......... 86% 65.1M 5s
437100K .......... .......... .......... .......... .......... 86% 25.1M 5s
437150K .......... .......... .......... .......... .......... 86% 56.5M 5s
437200K .......... .......... .......... .......... .......... 86% 68.4M 5s
437250K .......... .......... .......... .......... .......... 86% 79.3M 5s
437300K .......... .......... .......... .......... .......... 86% 82.8M 5s
437350K .......... .......... .......... .......... .......... 86% 58.2M 5s
437400K .......... .......... .......... .......... .......... 86% 51.2M 5s
437450K .......... .......... .......... .......... .......... 86% 51.4M 5s
437500K .......... .......... .......... .......... .......... 86% 50.8M 5s
437550K .......... .......... .......... .......... .......... 86% 62.9M 5s
437600K .......... .......... .......... .......... .......... 86% 36.1M 5s
437650K .......... .......... .......... .......... .......... 86% 45.1M 5s
437700K .......... .......... .......... .......... .......... 86% 22.1M 5s
437750K .......... .......... .......... .......... .......... 86% 75.5M 5s
437800K .......... .......... .......... .......... .......... 86% 40.3M 5s
437850K .......... .......... .......... .......... .......... 86% 20.8M 5s
437900K .......... .......... .......... .......... .......... 86% 56.8M 5s
437950K .......... .......... .......... .......... .......... 86% 21.9M 5s
438000K .......... .......... .......... .......... .......... 86% 25.4M 5s
438050K .......... .......... .......... .......... .......... 86% 28.5M 5s
438100K .......... .......... .......... .......... .......... 86% 24.6M 5s
438150K .......... .......... .......... .......... .......... 86% 53.2M 5s
438200K .......... .......... .......... .......... .......... 86% 26.2M 5s
438250K .......... .......... .......... .......... .......... 86% 33.8M 5s
438300K .......... .......... .......... .......... .......... 86% 37.2M 5s
438350K .......... .......... .......... .......... .......... 86% 27.9M 5s
438400K .......... .......... .......... .......... .......... 86% 42.0M 5s
438450K .......... .......... .......... .......... .......... 86% 18.9M 5s
438500K .......... .......... .......... .......... .......... 86%  105M 5s
438550K .......... .......... .......... .......... .......... 86% 33.5M 5s
438600K .......... .......... .......... .......... .......... 86% 26.8M 5s
438650K .......... .......... .......... .......... .......... 86% 33.7M 5s
438700K .......... .......... .......... .......... .......... 86% 33.8M 5s
438750K .......... .......... .......... .......... .......... 86% 24.4M 5s
438800K .......... .......... .......... .......... .......... 86% 28.5M 5s
438850K .......... .......... .......... .......... .......... 86% 16.7M 5s
438900K .......... .......... .......... .......... .......... 86% 22.2M 5s
438950K .......... .......... .......... .......... .......... 86% 13.8M 5s
439000K .......... .......... .......... .......... .......... 86% 16.0M 5s
439050K .......... .......... .......... .......... .......... 87% 12.3M 5s
439100K .......... .......... .......... .......... .......... 87% 12.1M 5s
439150K .......... .......... .......... .......... .......... 87% 15.6M 5s
439200K .......... .......... .......... .......... .......... 87% 12.1M 5s
439250K .......... .......... .......... .......... .......... 87% 15.1M 5s
439300K .......... .......... .......... .......... .......... 87% 17.1M 5s
439350K .......... .......... .......... .......... .......... 87% 11.7M 5s
439400K .......... .......... .......... .......... .......... 87% 16.2M 5s
439450K .......... .......... .......... .......... .......... 87% 14.3M 5s
439500K .......... .......... .......... .......... .......... 87% 15.8M 5s
439550K .......... .......... .......... .......... .......... 87% 12.5M 5s
439600K .......... .......... .......... .......... .......... 87% 7.78M 5s
439650K .......... .......... .......... .......... .......... 87% 14.0M 5s
439700K .......... .......... .......... .......... .......... 87% 29.8M 5s
439750K .......... .......... .......... .......... .......... 87% 16.3M 5s
439800K .......... .......... .......... .......... .......... 87% 20.1M 5s
439850K .......... .......... .......... .......... .......... 87% 15.4M 5s
439900K .......... .......... .......... .......... .......... 87% 18.7M 5s
439950K .......... .......... .......... .......... .......... 87% 18.9M 5s
440000K .......... .......... .......... .......... .......... 87% 20.4M 5s
440050K .......... .......... .......... .......... .......... 87% 18.8M 5s
440100K .......... .......... .......... .......... .......... 87% 15.6M 5s
440150K .......... .......... .......... .......... .......... 87% 17.1M 5s
440200K .......... .......... .......... .......... .......... 87% 19.0M 5s
440250K .......... .......... .......... .......... .......... 87% 20.5M 5s
440300K .......... .......... .......... .......... .......... 87% 17.9M 5s
440350K .......... .......... .......... .......... .......... 87% 19.8M 5s
440400K .......... .......... .......... .......... .......... 87% 30.8M 5s
440450K .......... .......... .......... .......... .......... 87% 73.4M 5s
440500K .......... .......... .......... .......... .......... 87% 45.2M 5s
440550K .......... .......... .......... .......... .......... 87% 15.7M 5s
440600K .......... .......... .......... .......... .......... 87% 42.3M 5s
440650K .......... .......... .......... .......... .......... 87% 43.0M 5s
440700K .......... .......... .......... .......... .......... 87% 28.7M 5s
440750K .......... .......... .......... .......... .......... 87% 35.2M 5s
440800K .......... .......... .......... .......... .......... 87% 21.1M 5s
440850K .......... .......... .......... .......... .......... 87% 23.2M 5s
440900K .......... .......... .......... .......... .......... 87% 23.4M 5s
440950K .......... .......... .......... .......... .......... 87% 22.3M 5s
441000K .......... .......... .......... .......... .......... 87% 24.5M 5s
441050K .......... .......... .......... .......... .......... 87% 23.9M 5s
441100K .......... .......... .......... .......... .......... 87% 25.5M 5s
441150K .......... .......... .......... .......... .......... 87% 30.0M 5s
441200K .......... .......... .......... .......... .......... 87% 17.8M 5s
441250K .......... .......... .......... .......... .......... 87% 16.3M 5s
441300K .......... .......... .......... .......... .......... 87% 22.2M 5s
441350K .......... .......... .......... .......... .......... 87% 18.5M 5s
441400K .......... .......... .......... .......... .......... 87% 20.8M 5s
441450K .......... .......... .......... .......... .......... 87% 14.5M 5s
441500K .......... .......... .......... .......... .......... 87% 18.9M 5s
441550K .......... .......... .......... .......... .......... 87% 6.39M 5s
441600K .......... .......... .......... .......... .......... 87% 12.2M 5s
441650K .......... .......... .......... .......... .......... 87% 9.39M 5s
441700K .......... .......... .......... .......... .......... 87% 8.91M 5s
441750K .......... .......... .......... .......... .......... 87% 9.04M 5s
441800K .......... .......... .......... .......... .......... 87% 10.2M 5s
441850K .......... .......... .......... .......... .......... 87% 9.82M 5s
441900K .......... .......... .......... .......... .......... 87% 9.21M 5s
441950K .......... .......... .......... .......... .......... 87% 13.0M 5s
442000K .......... .......... .......... .......... .......... 87% 9.21M 5s
442050K .......... .......... .......... .......... .......... 87% 38.1M 5s
442100K .......... .......... .......... .......... .......... 87% 19.7M 5s
442150K .......... .......... .......... .......... .......... 87% 18.7M 5s
442200K .......... .......... .......... .......... .......... 87% 13.0M 5s
442250K .......... .......... .......... .......... .......... 87% 16.3M 5s
442300K .......... .......... .......... .......... .......... 87% 14.4M 5s
442350K .......... .......... .......... .......... .......... 87% 13.0M 5s
442400K .......... .......... .......... .......... .......... 87% 13.5M 5s
442450K .......... .......... .......... .......... .......... 87% 9.15M 5s
442500K .......... .......... .......... .......... .......... 87% 13.5M 5s
442550K .......... .......... .......... .......... .......... 87% 12.8M 5s
442600K .......... .......... .......... .......... .......... 87% 10.0M 5s
442650K .......... .......... .......... .......... .......... 87% 7.80M 5s
442700K .......... .......... .......... .......... .......... 87% 11.8M 5s
442750K .......... .......... .......... .......... .......... 87% 17.2M 5s
442800K .......... .......... .......... .......... .......... 87% 11.1M 5s
442850K .......... .......... .......... .......... .......... 87% 10.1M 5s
442900K .......... .......... .......... .......... .......... 87% 13.9M 5s
442950K .......... .......... .......... .......... .......... 87% 12.1M 5s
443000K .......... .......... .......... .......... .......... 87% 17.1M 5s
443050K .......... .......... .......... .......... .......... 87% 14.4M 5s
443100K .......... .......... .......... .......... .......... 87% 13.9M 5s
443150K .......... .......... .......... .......... .......... 87% 12.1M 5s
443200K .......... .......... .......... .......... .......... 87% 9.95M 5s
443250K .......... .......... .......... .......... .......... 87% 7.16M 5s
443300K .......... .......... .......... .......... .......... 87% 13.3M 5s
443350K .......... .......... .......... .......... .......... 87% 8.26M 5s
443400K .......... .......... .......... .......... .......... 87% 9.00M 5s
443450K .......... .......... .......... .......... .......... 87% 7.82M 5s
443500K .......... .......... .......... .......... .......... 87% 9.06M 5s
443550K .......... .......... .......... .......... .......... 87% 6.92M 5s
443600K .......... .......... .......... .......... .......... 87% 4.48M 5s
443650K .......... .......... .......... .......... .......... 87% 6.75M 5s
443700K .......... .......... .......... .......... .......... 87% 5.90M 5s
443750K .......... .......... .......... .......... .......... 87% 7.01M 5s
443800K .......... .......... .......... .......... .......... 87% 6.33M 5s
443850K .......... .......... .......... .......... .......... 87% 10.5M 5s
443900K .......... .......... .......... .......... .......... 87% 10.5M 5s
443950K .......... .......... .......... .......... .......... 87% 22.9M 5s
444000K .......... .......... .......... .......... .......... 87% 9.02M 5s
444050K .......... .......... .......... .......... .......... 87% 21.5M 5s
444100K .......... .......... .......... .......... .......... 88% 11.7M 5s
444150K .......... .......... .......... .......... .......... 88% 15.0M 5s
444200K .......... .......... .......... .......... .......... 88% 13.9M 5s
444250K .......... .......... .......... .......... .......... 88% 15.2M 5s
444300K .......... .......... .......... .......... .......... 88% 12.9M 5s
444350K .......... .......... .......... .......... .......... 88% 14.0M 5s
444400K .......... .......... .......... .......... .......... 88% 13.1M 5s
444450K .......... .......... .......... .......... .......... 88% 11.7M 5s
444500K .......... .......... .......... .......... .......... 88% 13.5M 5s
444550K .......... .......... .......... .......... .......... 88% 33.9M 5s
444600K .......... .......... .......... .......... .......... 88% 16.7M 5s
444650K .......... .......... .......... .......... .......... 88% 47.0M 5s
444700K .......... .......... .......... .......... .......... 88% 79.3M 5s
444750K .......... .......... .......... .......... .......... 88% 17.0M 5s
444800K .......... .......... .......... .......... .......... 88% 53.8M 5s
444850K .......... .......... .......... .......... .......... 88% 19.5M 5s
444900K .......... .......... .......... .......... .......... 88% 22.0M 5s
444950K .......... .......... .......... .......... .......... 88% 15.6M 5s
445000K .......... .......... .......... .......... .......... 88% 25.5M 5s
445050K .......... .......... .......... .......... .......... 88% 21.7M 5s
445100K .......... .......... .......... .......... .......... 88% 15.2M 5s
445150K .......... .......... .......... .......... .......... 88% 21.6M 5s
445200K .......... .......... .......... .......... .......... 88% 15.0M 5s
445250K .......... .......... .......... .......... .......... 88% 11.4M 5s
445300K .......... .......... .......... .......... .......... 88% 24.9M 5s
445350K .......... .......... .......... .......... .......... 88% 8.61M 5s
445400K .......... .......... .......... .......... .......... 88% 23.7M 5s
445450K .......... .......... .......... .......... .......... 88% 14.5M 5s
445500K .......... .......... .......... .......... .......... 88% 11.7M 5s
445550K .......... .......... .......... .......... .......... 88% 15.6M 5s
445600K .......... .......... .......... .......... .......... 88% 12.7M 5s
445650K .......... .......... .......... .......... .......... 88% 13.7M 5s
445700K .......... .......... .......... .......... .......... 88% 13.0M 5s
445750K .......... .......... .......... .......... .......... 88% 17.1M 5s
445800K .......... .......... .......... .......... .......... 88% 10.8M 5s
445850K .......... .......... .......... .......... .......... 88% 7.26M 5s
445900K .......... .......... .......... .......... .......... 88% 15.2M 5s
445950K .......... .......... .......... .......... .......... 88% 10.7M 5s
446000K .......... .......... .......... .......... .......... 88% 13.4M 5s
446050K .......... .......... .......... .......... .......... 88% 17.2M 5s
446100K .......... .......... .......... .......... .......... 88% 12.4M 5s
446150K .......... .......... .......... .......... .......... 88% 13.9M 5s
446200K .......... .......... .......... .......... .......... 88% 13.2M 5s
446250K .......... .......... .......... .......... .......... 88% 14.9M 5s
446300K .......... .......... .......... .......... .......... 88% 45.0M 5s
446350K .......... .......... .......... .......... .......... 88% 42.1M 5s
446400K .......... .......... .......... .......... .......... 88% 60.7M 5s
446450K .......... .......... .......... .......... .......... 88% 18.4M 5s
446500K .......... .......... .......... .......... .......... 88% 60.6M 5s
446550K .......... .......... .......... .......... .......... 88% 79.9M 5s
446600K .......... .......... .......... .......... .......... 88% 73.8M 5s
446650K .......... .......... .......... .......... .......... 88% 7.55M 5s
446700K .......... .......... .......... .......... .......... 88% 63.2M 5s
446750K .......... .......... .......... .......... .......... 88% 75.6M 5s
446800K .......... .......... .......... .......... .......... 88% 79.8M 5s
446850K .......... .......... .......... .......... .......... 88% 72.2M 4s
446900K .......... .......... .......... .......... .......... 88% 81.9M 4s
446950K .......... .......... .......... .......... .......... 88% 71.0M 4s
447000K .......... .......... .......... .......... .......... 88% 43.5M 4s
447050K .......... .......... .......... .......... .......... 88% 34.1M 4s
447100K .......... .......... .......... .......... .......... 88% 30.7M 4s
447150K .......... .......... .......... .......... .......... 88% 36.9M 4s
447200K .......... .......... .......... .......... .......... 88% 25.7M 4s
447250K .......... .......... .......... .......... .......... 88% 36.4M 4s
447300K .......... .......... .......... .......... .......... 88% 46.6M 4s
447350K .......... .......... .......... .......... .......... 88% 34.0M 4s
447400K .......... .......... .......... .......... .......... 88% 38.1M 4s
447450K .......... .......... .......... .......... .......... 88% 30.2M 4s
447500K .......... .......... .......... .......... .......... 88% 32.3M 4s
447550K .......... .......... .......... .......... .......... 88% 45.5M 4s
447600K .......... .......... .......... .......... .......... 88% 29.3M 4s
447650K .......... .......... .......... .......... .......... 88% 50.5M 4s
447700K .......... .......... .......... .......... .......... 88% 34.9M 4s
447750K .......... .......... .......... .......... .......... 88% 30.3M 4s
447800K .......... .......... .......... .......... .......... 88% 46.4M 4s
447850K .......... .......... .......... .......... .......... 88% 23.4M 4s
447900K .......... .......... .......... .......... .......... 88% 34.9M 4s
447950K .......... .......... .......... .......... .......... 88% 15.4M 4s
448000K .......... .......... .......... .......... .......... 88% 93.0M 4s
448050K .......... .......... .......... .......... .......... 88% 12.9M 4s
448100K .......... .......... .......... .......... .......... 88% 19.3M 4s
448150K .......... .......... .......... .......... .......... 88% 97.9M 4s
448200K .......... .......... .......... .......... .......... 88% 30.0M 4s
448250K .......... .......... .......... .......... .......... 88%  106M 4s
448300K .......... .......... .......... .......... .......... 88% 46.4M 4s
448350K .......... .......... .......... .......... .......... 88% 21.9M 4s
448400K .......... .......... .......... .......... .......... 88% 34.2M 4s
448450K .......... .......... .......... .......... .......... 88% 29.0M 4s
448500K .......... .......... .......... .......... .......... 88% 31.7M 4s
448550K .......... .......... .......... .......... .......... 88% 31.8M 4s
448600K .......... .......... .......... .......... .......... 88% 25.8M 4s
448650K .......... .......... .......... .......... .......... 88% 28.9M 4s
448700K .......... .......... .......... .......... .......... 88% 26.7M 4s
448750K .......... .......... .......... .......... .......... 88% 28.7M 4s
448800K .......... .......... .......... .......... .......... 88% 34.1M 4s
448850K .......... .......... .......... .......... .......... 88% 24.8M 4s
448900K .......... .......... .......... .......... .......... 88% 29.9M 4s
448950K .......... .......... .......... .......... .......... 88% 25.9M 4s
449000K .......... .......... .......... .......... .......... 88% 27.8M 4s
449050K .......... .......... .......... .......... .......... 88% 27.8M 4s
449100K .......... .......... .......... .......... .......... 88% 31.1M 4s
449150K .......... .......... .......... .......... .......... 89% 34.0M 4s
449200K .......... .......... .......... .......... .......... 89% 23.2M 4s
449250K .......... .......... .......... .......... .......... 89% 27.1M 4s
449300K .......... .......... .......... .......... .......... 89% 12.2M 4s
449350K .......... .......... .......... .......... .......... 89% 28.7M 4s
449400K .......... .......... .......... .......... .......... 89%  137M 4s
449450K .......... .......... .......... .......... .......... 89% 20.2M 4s
449500K .......... .......... .......... .......... .......... 89% 27.5M 4s
449550K .......... .......... .......... .......... .......... 89% 28.8M 4s
449600K .......... .......... .......... .......... .......... 89% 21.0M 4s
449650K .......... .......... .......... .......... .......... 89% 33.2M 4s
449700K .......... .......... .......... .......... .......... 89% 25.3M 4s
449750K .......... .......... .......... .......... .......... 89% 28.6M 4s
449800K .......... .......... .......... .......... .......... 89% 30.8M 4s
449850K .......... .......... .......... .......... .......... 89% 26.8M 4s
449900K .......... .......... .......... .......... .......... 89% 33.0M 4s
449950K .......... .......... .......... .......... .......... 89% 27.0M 4s
450000K .......... .......... .......... .......... .......... 89% 26.8M 4s
450050K .......... .......... .......... .......... .......... 89% 32.7M 4s
450100K .......... .......... .......... .......... .......... 89% 29.9M 4s
450150K .......... .......... .......... .......... .......... 89% 29.0M 4s
450200K .......... .......... .......... .......... .......... 89% 24.8M 4s
450250K .......... .......... .......... .......... .......... 89% 31.5M 4s
450300K .......... .......... .......... .......... .......... 89% 26.6M 4s
450350K .......... .......... .......... .......... .......... 89% 26.0M 4s
450400K .......... .......... .......... .......... .......... 89% 37.0M 4s
450450K .......... .......... .......... .......... .......... 89% 22.0M 4s
450500K .......... .......... .......... .......... .......... 89% 25.1M 4s
450550K .......... .......... .......... .......... .......... 89% 41.5M 4s
450600K .......... .......... .......... .......... .......... 89% 25.1M 4s
450650K .......... .......... .......... .......... .......... 89% 12.0M 4s
450700K .......... .......... .......... .......... .......... 89% 83.3M 4s
450750K .......... .......... .......... .......... .......... 89%  109M 4s
450800K .......... .......... .......... .......... .......... 89% 19.3M 4s
450850K .......... .......... .......... .......... .......... 89% 42.3M 4s
450900K .......... .......... .......... .......... .......... 89% 22.3M 4s
450950K .......... .......... .......... .......... .......... 89% 20.6M 4s
451000K .......... .......... .......... .......... .......... 89% 22.2M 4s
451050K .......... .......... .......... .......... .......... 89% 22.0M 4s
451100K .......... .......... .......... .......... .......... 89% 18.7M 4s
451150K .......... .......... .......... .......... .......... 89% 25.1M 4s
451200K .......... .......... .......... .......... .......... 89% 19.7M 4s
451250K .......... .......... .......... .......... .......... 89% 24.9M 4s
451300K .......... .......... .......... .......... .......... 89% 28.6M 4s
451350K .......... .......... .......... .......... .......... 89% 23.6M 4s
451400K .......... .......... .......... .......... .......... 89% 21.9M 4s
451450K .......... .......... .......... .......... .......... 89% 19.5M 4s
451500K .......... .......... .......... .......... .......... 89% 28.7M 4s
451550K .......... .......... .......... .......... .......... 89% 26.8M 4s
451600K .......... .......... .......... .......... .......... 89% 23.6M 4s
451650K .......... .......... .......... .......... .......... 89% 19.4M 4s
451700K .......... .......... .......... .......... .......... 89% 22.2M 4s
451750K .......... .......... .......... .......... .......... 89% 33.7M 4s
451800K .......... .......... .......... .......... .......... 89% 54.9M 4s
451850K .......... .......... .......... .......... .......... 89% 24.8M 4s
451900K .......... .......... .......... .......... .......... 89% 17.7M 4s
451950K .......... .......... .......... .......... .......... 89% 29.0M 4s
452000K .......... .......... .......... .......... .......... 89% 19.3M 4s
452050K .......... .......... .......... .......... .......... 89%  106M 4s
452100K .......... .......... .......... .......... .......... 89% 84.3M 4s
452150K .......... .......... .......... .......... .......... 89%  111M 4s
452200K .......... .......... .......... .......... .......... 89% 20.5M 4s
452250K .......... .......... .......... .......... .......... 89%  106M 4s
452300K .......... .......... .......... .......... .......... 89% 29.1M 4s
452350K .......... .......... .......... .......... .......... 89% 26.8M 4s
452400K .......... .......... .......... .......... .......... 89% 25.6M 4s
452450K .......... .......... .......... .......... .......... 89% 25.8M 4s
452500K .......... .......... .......... .......... .......... 89% 39.1M 4s
452550K .......... .......... .......... .......... .......... 89% 27.7M 4s
452600K .......... .......... .......... .......... .......... 89% 30.0M 4s
452650K .......... .......... .......... .......... .......... 89% 14.2M 4s
452700K .......... .......... .......... .......... .......... 89% 31.6M 4s
452750K .......... .......... .......... .......... .......... 89% 16.9M 4s
452800K .......... .......... .......... .......... .......... 89% 17.0M 4s
452850K .......... .......... .......... .......... .......... 89% 13.4M 4s
452900K .......... .......... .......... .......... .......... 89% 18.7M 4s
452950K .......... .......... .......... .......... .......... 89% 14.0M 4s
453000K .......... .......... .......... .......... .......... 89% 18.0M 4s
453050K .......... .......... .......... .......... .......... 89% 7.57M 4s
453100K .......... .......... .......... .......... .......... 89% 7.69M 4s
453150K .......... .......... .......... .......... .......... 89% 7.52M 4s
453200K .......... .......... .......... .......... .......... 89% 9.74M 4s
453250K .......... .......... .......... .......... .......... 89% 12.2M 4s
453300K .......... .......... .......... .......... .......... 89% 11.0M 4s
453350K .......... .......... .......... .......... .......... 89% 11.5M 4s
453400K .......... .......... .......... .......... .......... 89% 10.9M 4s
453450K .......... .......... .......... .......... .......... 89% 20.4M 4s
453500K .......... .......... .......... .......... .......... 89% 22.6M 4s
453550K .......... .......... .......... .......... .......... 89% 72.6M 4s
453600K .......... .......... .......... .......... .......... 89% 20.4M 4s
453650K .......... .......... .......... .......... .......... 89% 41.2M 4s
453700K .......... .......... .......... .......... .......... 89% 61.0M 4s
453750K .......... .......... .......... .......... .......... 89% 44.3M 4s
453800K .......... .......... .......... .......... .......... 89% 28.3M 4s
453850K .......... .......... .......... .......... .......... 89% 38.1M 4s
453900K .......... .......... .......... .......... .......... 89% 41.0M 4s
453950K .......... .......... .......... .......... .......... 89% 23.3M 4s
454000K .......... .......... .......... .......... .......... 89% 34.0M 4s
454050K .......... .......... .......... .......... .......... 89% 17.8M 4s
454100K .......... .......... .......... .......... .......... 89% 37.2M 4s
454150K .......... .......... .......... .......... .......... 89% 30.9M 4s
454200K .......... .......... .......... .......... .......... 90% 20.8M 4s
454250K .......... .......... .......... .......... .......... 90% 27.6M 4s
454300K .......... .......... .......... .......... .......... 90% 28.1M 4s
454350K .......... .......... .......... .......... .......... 90% 25.0M 4s
454400K .......... .......... .......... .......... .......... 90% 22.5M 4s
454450K .......... .......... .......... .......... .......... 90% 18.3M 4s
454500K .......... .......... .......... .......... .......... 90% 37.8M 4s
454550K .......... .......... .......... .......... .......... 90% 26.3M 4s
454600K .......... .......... .......... .......... .......... 90% 17.3M 4s
454650K .......... .......... .......... .......... .......... 90% 15.0M 4s
454700K .......... .......... .......... .......... .......... 90% 7.17M 4s
454750K .......... .......... .......... .......... .......... 90% 15.9M 4s
454800K .......... .......... .......... .......... .......... 90% 16.1M 4s
454850K .......... .......... .......... .......... .......... 90% 13.1M 4s
454900K .......... .......... .......... .......... .......... 90% 14.0M 4s
454950K .......... .......... .......... .......... .......... 90% 13.9M 4s
455000K .......... .......... .......... .......... .......... 90% 15.1M 4s
455050K .......... .......... .......... .......... .......... 90% 12.6M 4s
455100K .......... .......... .......... .......... .......... 90% 12.2M 4s
455150K .......... .......... .......... .......... .......... 90% 17.5M 4s
455200K .......... .......... .......... .......... .......... 90% 15.8M 4s
455250K .......... .......... .......... .......... .......... 90% 16.5M 4s
455300K .......... .......... .......... .......... .......... 90% 14.9M 4s
455350K .......... .......... .......... .......... .......... 90% 6.33M 4s
455400K .......... .......... .......... .......... .......... 90% 11.4M 4s
455450K .......... .......... .......... .......... .......... 90% 9.94M 4s
455500K .......... .......... .......... .......... .......... 90% 13.0M 4s
455550K .......... .......... .......... .......... .......... 90% 12.6M 4s
455600K .......... .......... .......... .......... .......... 90% 26.6M 4s
455650K .......... .......... .......... .......... .......... 90% 19.2M 4s
455700K .......... .......... .......... .......... .......... 90% 36.0M 4s
455750K .......... .......... .......... .......... .......... 90% 27.4M 4s
455800K .......... .......... .......... .......... .......... 90% 28.3M 4s
455850K .......... .......... .......... .......... .......... 90% 18.0M 4s
455900K .......... .......... .......... .......... .......... 90% 21.8M 4s
455950K .......... .......... .......... .......... .......... 90% 15.2M 4s
456000K .......... .......... .......... .......... .......... 90% 22.3M 4s
456050K .......... .......... .......... .......... .......... 90% 17.4M 4s
456100K .......... .......... .......... .......... .......... 90% 18.8M 4s
456150K .......... .......... .......... .......... .......... 90% 21.1M 4s
456200K .......... .......... .......... .......... .......... 90% 14.5M 4s
456250K .......... .......... .......... .......... .......... 90% 24.8M 4s
456300K .......... .......... .......... .......... .......... 90% 19.1M 4s
456350K .......... .......... .......... .......... .......... 90% 14.9M 4s
456400K .......... .......... .......... .......... .......... 90% 17.0M 4s
456450K .......... .......... .......... .......... .......... 90% 19.1M 4s
456500K .......... .......... .......... .......... .......... 90% 30.1M 4s
456550K .......... .......... .......... .......... .......... 90% 23.3M 4s
456600K .......... .......... .......... .......... .......... 90% 16.5M 4s
456650K .......... .......... .......... .......... .......... 90% 86.4M 4s
456700K .......... .......... .......... .......... .......... 90% 20.8M 4s
456750K .......... .......... .......... .......... .......... 90% 18.7M 4s
456800K .......... .......... .......... .......... .......... 90% 15.4M 4s
456850K .......... .......... .......... .......... .......... 90% 25.0M 4s
456900K .......... .......... .......... .......... .......... 90% 23.4M 4s
456950K .......... .......... .......... .......... .......... 90% 13.6M 4s
457000K .......... .......... .......... .......... .......... 90% 18.0M 4s
457050K .......... .......... .......... .......... .......... 90% 20.0M 4s
457100K .......... .......... .......... .......... .......... 90% 14.5M 4s
457150K .......... .......... .......... .......... .......... 90% 19.7M 4s
457200K .......... .......... .......... .......... .......... 90% 17.0M 4s
457250K .......... .......... .......... .......... .......... 90% 18.9M 4s
457300K .......... .......... .......... .......... .......... 90% 15.7M 4s
457350K .......... .......... .......... .......... .......... 90% 17.3M 4s
457400K .......... .......... .......... .......... .......... 90% 16.9M 4s
457450K .......... .......... .......... .......... .......... 90% 8.87M 4s
457500K .......... .......... .......... .......... .......... 90% 10.2M 4s
457550K .......... .......... .......... .......... .......... 90% 9.55M 4s
457600K .......... .......... .......... .......... .......... 90% 9.24M 4s
457650K .......... .......... .......... .......... .......... 90% 9.47M 4s
457700K .......... .......... .......... .......... .......... 90% 8.24M 4s
457750K .......... .......... .......... .......... .......... 90% 8.12M 4s
457800K .......... .......... .......... .......... .......... 90% 10.0M 4s
457850K .......... .......... .......... .......... .......... 90% 7.31M 4s
457900K .......... .......... .......... .......... .......... 90% 8.67M 4s
457950K .......... .......... .......... .......... .......... 90% 22.4M 4s
458000K .......... .......... .......... .......... .......... 90% 41.3M 4s
458050K .......... .......... .......... .......... .......... 90% 49.1M 4s
458100K .......... .......... .......... .......... .......... 90% 48.3M 4s
458150K .......... .......... .......... .......... .......... 90% 13.1M 4s
458200K .......... .......... .......... .......... .......... 90% 40.7M 4s
458250K .......... .......... .......... .......... .......... 90% 79.7M 4s
458300K .......... .......... .......... .......... .......... 90% 16.7M 4s
458350K .......... .......... .......... .......... .......... 90% 14.1M 4s
458400K .......... .......... .......... .......... .......... 90% 15.2M 4s
458450K .......... .......... .......... .......... .......... 90% 16.4M 4s
458500K .......... .......... .......... .......... .......... 90% 14.0M 4s
458550K .......... .......... .......... .......... .......... 90% 26.8M 4s
458600K .......... .......... .......... .......... .......... 90% 15.2M 4s
458650K .......... .......... .......... .......... .......... 90% 17.2M 4s
458700K .......... .......... .......... .......... .......... 90% 14.1M 4s
458750K .......... .......... .......... .......... .......... 90% 14.4M 4s
458800K .......... .......... .......... .......... .......... 90% 16.6M 4s
458850K .......... .......... .......... .......... .......... 90% 8.83M 4s
458900K .......... .......... .......... .......... .......... 90% 12.6M 4s
458950K .......... .......... .......... .......... .......... 90% 9.90M 4s
459000K .......... .......... .......... .......... .......... 90% 13.6M 4s
459050K .......... .......... .......... .......... .......... 90% 14.6M 4s
459100K .......... .......... .......... .......... .......... 90% 21.9M 4s
459150K .......... .......... .......... .......... .......... 90% 16.6M 4s
459200K .......... .......... .......... .......... .......... 90% 10.7M 3s
459250K .......... .......... .......... .......... .......... 91% 15.0M 3s
459300K .......... .......... .......... .......... .......... 91% 15.3M 3s
459350K .......... .......... .......... .......... .......... 91% 11.8M 3s
459400K .......... .......... .......... .......... .......... 91% 16.6M 3s
459450K .......... .......... .......... .......... .......... 91% 16.5M 3s
459500K .......... .......... .......... .......... .......... 91% 13.2M 3s
459550K .......... .......... .......... .......... .......... 91% 11.7M 3s
459600K .......... .......... .......... .......... .......... 91% 7.57M 3s
459650K .......... .......... .......... .......... .......... 91% 97.3M 3s
459700K .......... .......... .......... .......... .......... 91% 13.3M 3s
459750K .......... .......... .......... .......... .......... 91% 20.7M 3s
459800K .......... .......... .......... .......... .......... 91% 17.8M 3s
459850K .......... .......... .......... .......... .......... 91% 15.8M 3s
459900K .......... .......... .......... .......... .......... 91% 15.0M 3s
459950K .......... .......... .......... .......... .......... 91% 17.2M 3s
460000K .......... .......... .......... .......... .......... 91% 19.8M 3s
460050K .......... .......... .......... .......... .......... 91% 14.9M 3s
460100K .......... .......... .......... .......... .......... 91% 15.6M 3s
460150K .......... .......... .......... .......... .......... 91% 19.2M 3s
460200K .......... .......... .......... .......... .......... 91% 17.0M 3s
460250K .......... .......... .......... .......... .......... 91% 14.9M 3s
460300K .......... .......... .......... .......... .......... 91% 23.2M 3s
460350K .......... .......... .......... .......... .......... 91% 29.6M 3s
460400K .......... .......... .......... .......... .......... 91% 81.8M 3s
460450K .......... .......... .......... .......... .......... 91% 54.3M 3s
460500K .......... .......... .......... .......... .......... 91% 43.7M 3s
460550K .......... .......... .......... .......... .......... 91% 16.1M 3s
460600K .......... .......... .......... .......... .......... 91% 56.4M 3s
460650K .......... .......... .......... .......... .......... 91% 93.0M 3s
460700K .......... .......... .......... .......... .......... 91% 69.9M 3s
460750K .......... .......... .......... .......... .......... 91% 43.9M 3s
460800K .......... .......... .......... .......... .......... 91% 33.6M 3s
460850K .......... .......... .......... .......... .......... 91% 41.1M 3s
460900K .......... .......... .......... .......... .......... 91% 33.5M 3s
460950K .......... .......... .......... .......... .......... 91% 17.3M 3s
461000K .......... .......... .......... .......... .......... 91% 17.9M 3s
461050K .......... .......... .......... .......... .......... 91% 20.9M 3s
461100K .......... .......... .......... .......... .......... 91% 15.6M 3s
461150K .......... .......... .......... .......... .......... 91% 20.3M 3s
461200K .......... .......... .......... .......... .......... 91% 13.7M 3s
461250K .......... .......... .......... .......... .......... 91% 18.1M 3s
461300K .......... .......... .......... .......... .......... 91% 17.0M 3s
461350K .......... .......... .......... .......... .......... 91% 21.6M 3s
461400K .......... .......... .......... .......... .......... 91% 17.4M 3s
461450K .......... .......... .......... .......... .......... 91% 22.0M 3s
461500K .......... .......... .......... .......... .......... 91% 15.2M 3s
461550K .......... .......... .......... .......... .......... 91% 25.4M 3s
461600K .......... .......... .......... .......... .......... 91% 10.5M 3s
461650K .......... .......... .......... .......... .......... 91% 85.8M 3s
461700K .......... .......... .......... .......... .......... 91% 71.3M 3s
461750K .......... .......... .......... .......... .......... 91% 15.2M 3s
461800K .......... .......... .......... .......... .......... 91% 80.8M 3s
461850K .......... .......... .......... .......... .......... 91% 17.6M 3s
461900K .......... .......... .......... .......... .......... 91% 26.7M 3s
461950K .......... .......... .......... .......... .......... 91% 20.9M 3s
462000K .......... .......... .......... .......... .......... 91% 20.9M 3s
462050K .......... .......... .......... .......... .......... 91% 34.2M 3s
462100K .......... .......... .......... .......... .......... 91% 19.3M 3s
462150K .......... .......... .......... .......... .......... 91% 25.2M 3s
462200K .......... .......... .......... .......... .......... 91% 24.0M 3s
462250K .......... .......... .......... .......... .......... 91% 30.0M 3s
462300K .......... .......... .......... .......... .......... 91% 22.3M 3s
462350K .......... .......... .......... .......... .......... 91% 19.5M 3s
462400K .......... .......... .......... .......... .......... 91% 27.4M 3s
462450K .......... .......... .......... .......... .......... 91% 18.6M 3s
462500K .......... .......... .......... .......... .......... 91% 21.8M 3s
462550K .......... .......... .......... .......... .......... 91% 31.9M 3s
462600K .......... .......... .......... .......... .......... 91% 21.5M 3s
462650K .......... .......... .......... .......... .......... 91% 21.2M 3s
462700K .......... .......... .......... .......... .......... 91% 25.0M 3s
462750K .......... .......... .......... .......... .......... 91% 37.5M 3s
462800K .......... .......... .......... .......... .......... 91% 13.8M 3s
462850K .......... .......... .......... .......... .......... 91% 23.3M 3s
462900K .......... .......... .......... .......... .......... 91% 95.6M 3s
462950K .......... .......... .......... .......... .......... 91% 25.4M 3s
463000K .......... .......... .......... .......... .......... 91% 36.8M 3s
463050K .......... .......... .......... .......... .......... 91% 27.4M 3s
463100K .......... .......... .......... .......... .......... 91% 26.2M 3s
463150K .......... .......... .......... .......... .......... 91% 19.9M 3s
463200K .......... .......... .......... .......... .......... 91% 41.2M 3s
463250K .......... .......... .......... .......... .......... 91% 25.0M 3s
463300K .......... .......... .......... .......... .......... 91% 18.9M 3s
463350K .......... .......... .......... .......... .......... 91% 22.4M 3s
463400K .......... .......... .......... .......... .......... 91% 17.8M 3s
463450K .......... .......... .......... .......... .......... 91% 21.0M 3s
463500K .......... .......... .......... .......... .......... 91% 17.2M 3s
463550K .......... .......... .......... .......... .......... 91% 17.8M 3s
463600K .......... .......... .......... .......... .......... 91% 18.0M 3s
463650K .......... .......... .......... .......... .......... 91% 18.7M 3s
463700K .......... .......... .......... .......... .......... 91% 20.8M 3s
463750K .......... .......... .......... .......... .......... 91% 19.8M 3s
463800K .......... .......... .......... .......... .......... 91% 18.1M 3s
463850K .......... .......... .......... .......... .......... 91% 18.8M 3s
463900K .......... .......... .......... .......... .......... 91% 23.8M 3s
463950K .......... .......... .......... .......... .......... 91% 11.7M 3s
464000K .......... .......... .......... .......... .......... 91% 83.3M 3s
464050K .......... .......... .......... .......... .......... 91% 80.3M 3s
464100K .......... .......... .......... .......... .......... 91% 12.0M 3s
464150K .......... .......... .......... .......... .......... 91% 80.6M 3s
464200K .......... .......... .......... .......... .......... 91% 35.7M 3s
464250K .......... .......... .......... .......... .......... 91% 31.1M 3s
464300K .......... .......... .......... .......... .......... 92% 27.0M 3s
464350K .......... .......... .......... .......... .......... 92% 22.0M 3s
464400K .......... .......... .......... .......... .......... 92% 34.3M 3s
464450K .......... .......... .......... .......... .......... 92% 13.4M 3s
464500K .......... .......... .......... .......... .......... 92% 81.8M 3s
464550K .......... .......... .......... .......... .......... 92% 29.9M 3s
464600K .......... .......... .......... .......... .......... 92% 22.0M 3s
464650K .......... .......... .......... .......... .......... 92% 25.0M 3s
464700K .......... .......... .......... .......... .......... 92% 23.8M 3s
464750K .......... .......... .......... .......... .......... 92% 26.7M 3s
464800K .......... .......... .......... .......... .......... 92% 29.0M 3s
464850K .......... .......... .......... .......... .......... 92% 21.9M 3s
464900K .......... .......... .......... .......... .......... 92% 42.8M 3s
464950K .......... .......... .......... .......... .......... 92% 23.0M 3s
465000K .......... .......... .......... .......... .......... 92% 28.7M 3s
465050K .......... .......... .......... .......... .......... 92% 25.0M 3s
465100K .......... .......... .......... .......... .......... 92% 21.8M 3s
465150K .......... .......... .......... .......... .......... 92% 25.5M 3s
465200K .......... .......... .......... .......... .......... 92% 11.0M 3s
465250K .......... .......... .......... .......... .......... 92% 77.5M 3s
465300K .......... .......... .......... .......... .......... 92% 26.6M 3s
465350K .......... .......... .......... .......... .......... 92% 16.9M 3s
465400K .......... .......... .......... .......... .......... 92% 17.2M 3s
465450K .......... .......... .......... .......... .......... 92% 10.8M 3s
465500K .......... .......... .......... .......... .......... 92% 8.78M 3s
465550K .......... .......... .......... .......... .......... 92% 23.5M 3s
465600K .......... .......... .......... .......... .......... 92% 11.8M 3s
465650K .......... .......... .......... .......... .......... 92% 14.0M 3s
465700K .......... .......... .......... .......... .......... 92% 11.9M 3s
465750K .......... .......... .......... .......... .......... 92% 14.5M 3s
465800K .......... .......... .......... .......... .......... 92% 14.4M 3s
465850K .......... .......... .......... .......... .......... 92% 7.76M 3s
465900K .......... .......... .......... .......... .......... 92% 12.0M 3s
465950K .......... .......... .......... .......... .......... 92% 9.85M 3s
466000K .......... .......... .......... .......... .......... 92% 9.28M 3s
466050K .......... .......... .......... .......... .......... 92% 10.8M 3s
466100K .......... .......... .......... .......... .......... 92% 9.04M 3s
466150K .......... .......... .......... .......... .......... 92% 11.5M 3s
466200K .......... .......... .......... .......... .......... 92% 8.47M 3s
466250K .......... .......... .......... .......... .......... 92% 12.2M 3s
466300K .......... .......... .......... .......... .......... 92% 26.7M 3s
466350K .......... .......... .......... .......... .......... 92% 8.34M 3s
466400K .......... .......... .......... .......... .......... 92% 29.7M 3s
466450K .......... .......... .......... .......... .......... 92% 14.2M 3s
466500K .......... .......... .......... .......... .......... 92% 20.8M 3s
466550K .......... .......... .......... .......... .......... 92% 15.0M 3s
466600K .......... .......... .......... .......... .......... 92% 17.8M 3s
466650K .......... .......... .......... .......... .......... 92% 18.0M 3s
466700K .......... .......... .......... .......... .......... 92% 15.1M 3s
466750K .......... .......... .......... .......... .......... 92% 13.9M 3s
466800K .......... .......... .......... .......... .......... 92% 23.7M 3s
466850K .......... .......... .......... .......... .......... 92% 19.9M 3s
466900K .......... .......... .......... .......... .......... 92% 14.3M 3s
466950K .......... .......... .......... .......... .......... 92% 18.9M 3s
467000K .......... .......... .......... .......... .......... 92% 20.6M 3s
467050K .......... .......... .......... .......... .......... 92% 17.0M 3s
467100K .......... .......... .......... .......... .......... 92% 24.9M 3s
467150K .......... .......... .......... .......... .......... 92% 10.9M 3s
467200K .......... .......... .......... .......... .......... 92% 40.2M 3s
467250K .......... .......... .......... .......... .......... 92% 83.8M 3s
467300K .......... .......... .......... .......... .......... 92% 15.8M 3s
467350K .......... .......... .......... .......... .......... 92% 25.2M 3s
467400K .......... .......... .......... .......... .......... 92% 28.0M 3s
467450K .......... .......... .......... .......... .......... 92% 12.2M 3s
467500K .......... .......... .......... .......... .......... 92% 18.2M 3s
467550K .......... .......... .......... .......... .......... 92% 13.3M 3s
467600K .......... .......... .......... .......... .......... 92% 12.1M 3s
467650K .......... .......... .......... .......... .......... 92% 17.7M 3s
467700K .......... .......... .......... .......... .......... 92% 12.5M 3s
467750K .......... .......... .......... .......... .......... 92% 18.0M 3s
467800K .......... .......... .......... .......... .......... 92% 13.5M 3s
467850K .......... .......... .......... .......... .......... 92% 11.4M 3s
467900K .......... .......... .......... .......... .......... 92% 13.0M 3s
467950K .......... .......... .......... .......... .......... 92% 7.70M 3s
468000K .......... .......... .......... .......... .......... 92% 83.0M 3s
468050K .......... .......... .......... .......... .......... 92% 16.5M 3s
468100K .......... .......... .......... .......... .......... 92% 12.6M 3s
468150K .......... .......... .......... .......... .......... 92% 16.4M 3s
468200K .......... .......... .......... .......... .......... 92% 9.64M 3s
468250K .......... .......... .......... .......... .......... 92% 12.2M 3s
468300K .......... .......... .......... .......... .......... 92% 12.2M 3s
468350K .......... .......... .......... .......... .......... 92% 13.6M 3s
468400K .......... .......... .......... .......... .......... 92% 13.1M 3s
468450K .......... .......... .......... .......... .......... 92% 12.2M 3s
468500K .......... .......... .......... .......... .......... 92% 13.4M 3s
468550K .......... .......... .......... .......... .......... 92% 11.6M 3s
468600K .......... .......... .......... .......... .......... 92% 9.63M 3s
468650K .......... .......... .......... .......... .......... 92% 11.3M 3s
468700K .......... .......... .......... .......... .......... 92% 26.2M 3s
468750K .......... .......... .......... .......... .......... 92% 23.9M 3s
468800K .......... .......... .......... .......... .......... 92% 15.9M 3s
468850K .......... .......... .......... .......... .......... 92% 12.0M 3s
468900K .......... .......... .......... .......... .......... 92% 18.2M 3s
468950K .......... .......... .......... .......... .......... 92% 14.0M 3s
469000K .......... .......... .......... .......... .......... 92% 14.6M 3s
469050K .......... .......... .......... .......... .......... 92% 13.8M 3s
469100K .......... .......... .......... .......... .......... 92% 11.1M 3s
469150K .......... .......... .......... .......... .......... 92% 18.0M 3s
469200K .......... .......... .......... .......... .......... 92% 13.4M 3s
469250K .......... .......... .......... .......... .......... 92% 15.3M 3s
469300K .......... .......... .......... .......... .......... 92% 18.1M 3s
469350K .......... .......... .......... .......... .......... 93% 7.09M 3s
469400K .......... .......... .......... .......... .......... 93% 86.3M 3s
469450K .......... .......... .......... .......... .......... 93% 39.2M 3s
469500K .......... .......... .......... .......... .......... 93% 42.1M 3s
469550K .......... .......... .......... .......... .......... 93% 21.2M 3s
469600K .......... .......... .......... .......... .......... 93% 20.8M 3s
469650K .......... .......... .......... .......... .......... 93% 20.1M 3s
469700K .......... .......... .......... .......... .......... 93% 19.7M 3s
469750K .......... .......... .......... .......... .......... 93% 17.3M 3s
469800K .......... .......... .......... .......... .......... 93% 18.7M 3s
469850K .......... .......... .......... .......... .......... 93% 18.2M 3s
469900K .......... .......... .......... .......... .......... 93% 17.9M 3s
469950K .......... .......... .......... .......... .......... 93% 16.6M 3s
470000K .......... .......... .......... .......... .......... 93% 16.7M 3s
470050K .......... .......... .......... .......... .......... 93% 24.2M 3s
470100K .......... .......... .......... .......... .......... 93% 20.7M 3s
470150K .......... .......... .......... .......... .......... 93% 18.2M 3s
470200K .......... .......... .......... .......... .......... 93% 15.8M 3s
470250K .......... .......... .......... .......... .......... 93% 34.1M 3s
470300K .......... .......... .......... .......... .......... 93% 38.5M 3s
470350K .......... .......... .......... .......... .......... 93% 10.0M 3s
470400K .......... .......... .......... .......... .......... 93% 79.1M 3s
470450K .......... .......... .......... .......... .......... 93% 68.7M 3s
470500K .......... .......... .......... .......... .......... 93% 38.0M 3s
470550K .......... .......... .......... .......... .......... 93% 37.5M 3s
470600K .......... .......... .......... .......... .......... 93% 37.4M 3s
470650K .......... .......... .......... .......... .......... 93% 24.7M 3s
470700K .......... .......... .......... .......... .......... 93% 23.9M 3s
470750K .......... .......... .......... .......... .......... 93% 24.3M 3s
470800K .......... .......... .......... .......... .......... 93% 23.3M 3s
470850K .......... .......... .......... .......... .......... 93% 40.4M 3s
470900K .......... .......... .......... .......... .......... 93% 20.2M 3s
470950K .......... .......... .......... .......... .......... 93% 23.8M 3s
471000K .......... .......... .......... .......... .......... 93% 28.7M 3s
471050K .......... .......... .......... .......... .......... 93% 31.9M 3s
471100K .......... .......... .......... .......... .......... 93% 25.9M 3s
471150K .......... .......... .......... .......... .......... 93% 27.0M 3s
471200K .......... .......... .......... .......... .......... 93% 22.1M 3s
471250K .......... .......... .......... .......... .......... 93% 35.1M 3s
471300K .......... .......... .......... .......... .......... 93% 23.5M 3s
471350K .......... .......... .......... .......... .......... 93% 26.4M 3s
471400K .......... .......... .......... .......... .......... 93% 31.8M 3s
471450K .......... .......... .......... .......... .......... 93% 21.0M 3s
471500K .......... .......... .......... .......... .......... 93% 21.9M 3s
471550K .......... .......... .......... .......... .......... 93% 26.5M 3s
471600K .......... .......... .......... .......... .......... 93% 22.8M 3s
471650K .......... .......... .......... .......... .......... 93% 11.3M 3s
471700K .......... .......... .......... .......... .......... 93% 43.1M 3s
471750K .......... .......... .......... .......... .......... 93% 40.1M 3s
471800K .......... .......... .......... .......... .......... 93% 33.5M 3s
471850K .......... .......... .......... .......... .......... 93% 16.3M 3s
471900K .......... .......... .......... .......... .......... 93% 34.2M 2s
471950K .......... .......... .......... .......... .......... 93% 17.0M 2s
472000K .......... .......... .......... .......... .......... 93% 17.9M 2s
472050K .......... .......... .......... .......... .......... 93% 17.4M 2s
472100K .......... .......... .......... .......... .......... 93% 17.1M 2s
472150K .......... .......... .......... .......... .......... 93% 19.2M 2s
472200K .......... .......... .......... .......... .......... 93% 17.3M 2s
472250K .......... .......... .......... .......... .......... 93% 18.3M 2s
472300K .......... .......... .......... .......... .......... 93% 16.7M 2s
472350K .......... .......... .......... .......... .......... 93% 18.8M 2s
472400K .......... .......... .......... .......... .......... 93% 16.4M 2s
472450K .......... .......... .......... .......... .......... 93% 17.5M 2s
472500K .......... .......... .......... .......... .......... 93% 21.7M 2s
472550K .......... .......... .......... .......... .......... 93% 21.0M 2s
472600K .......... .......... .......... .......... .......... 93% 8.74M 2s
472650K .......... .......... .......... .......... .......... 93% 95.0M 2s
472700K .......... .......... .......... .......... .......... 93% 31.4M 2s
472750K .......... .......... .......... .......... .......... 93% 29.1M 2s
472800K .......... .......... .......... .......... .......... 93% 21.4M 2s
472850K .......... .......... .......... .......... .......... 93% 22.1M 2s
472900K .......... .......... .......... .......... .......... 93% 20.9M 2s
472950K .......... .......... .......... .......... .......... 93% 19.0M 2s
473000K .......... .......... .......... .......... .......... 93% 23.4M 2s
473050K .......... .......... .......... .......... .......... 93% 20.9M 2s
473100K .......... .......... .......... .......... .......... 93% 22.3M 2s
473150K .......... .......... .......... .......... .......... 93% 22.9M 2s
473200K .......... .......... .......... .......... .......... 93% 23.9M 2s
473250K .......... .......... .......... .......... .......... 93% 21.4M 2s
473300K .......... .......... .......... .......... .......... 93% 25.0M 2s
473350K .......... .......... .......... .......... .......... 93% 19.5M 2s
473400K .......... .......... .......... .......... .......... 93% 28.0M 2s
473450K .......... .......... .......... .......... .......... 93% 15.3M 2s
473500K .......... .......... .......... .......... .......... 93% 27.7M 2s
473550K .......... .......... .......... .......... .......... 93% 27.3M 2s
473600K .......... .......... .......... .......... .......... 93% 16.7M 2s
473650K .......... .......... .......... .......... .......... 93% 10.7M 2s
473700K .......... .......... .......... .......... .......... 93% 64.8M 2s
473750K .......... .......... .......... .......... .......... 93% 19.9M 2s
473800K .......... .......... .......... .......... .......... 93% 15.8M 2s
473850K .......... .......... .......... .......... .......... 93% 42.4M 2s
473900K .......... .......... .......... .......... .......... 93% 15.6M 2s
473950K .......... .......... .......... .......... .......... 93% 14.0M 2s
474000K .......... .......... .......... .......... .......... 93% 15.1M 2s
474050K .......... .......... .......... .......... .......... 93% 13.6M 2s
474100K .......... .......... .......... .......... .......... 93% 11.0M 2s
474150K .......... .......... .......... .......... .......... 93% 15.1M 2s
474200K .......... .......... .......... .......... .......... 93% 14.7M 2s
474250K .......... .......... .......... .......... .......... 93% 17.1M 2s
474300K .......... .......... .......... .......... .......... 93% 11.7M 2s
474350K .......... .......... .......... .......... .......... 94% 13.4M 2s
474400K .......... .......... .......... .......... .......... 94% 25.5M 2s
474450K .......... .......... .......... .......... .......... 94% 11.2M 2s
474500K .......... .......... .......... .......... .......... 94% 84.9M 2s
474550K .......... .......... .......... .......... .......... 94% 25.8M 2s
474600K .......... .......... .......... .......... .......... 94% 16.6M 2s
474650K .......... .......... .......... .......... .......... 94% 26.0M 2s
474700K .......... .......... .......... .......... .......... 94% 16.3M 2s
474750K .......... .......... .......... .......... .......... 94% 22.0M 2s
474800K .......... .......... .......... .......... .......... 94% 16.2M 2s
474850K .......... .......... .......... .......... .......... 94% 18.0M 2s
474900K .......... .......... .......... .......... .......... 94% 22.2M 2s
474950K .......... .......... .......... .......... .......... 94% 13.5M 2s
475000K .......... .......... .......... .......... .......... 94% 26.8M 2s
475050K .......... .......... .......... .......... .......... 94% 22.5M 2s
475100K .......... .......... .......... .......... .......... 94% 17.4M 2s
475150K .......... .......... .......... .......... .......... 94% 16.4M 2s
475200K .......... .......... .......... .......... .......... 94% 23.0M 2s
475250K .......... .......... .......... .......... .......... 94% 16.5M 2s
475300K .......... .......... .......... .......... .......... 94% 20.9M 2s
475350K .......... .......... .......... .......... .......... 94% 13.8M 2s
475400K .......... .......... .......... .......... .......... 94% 28.5M 2s
475450K .......... .......... .......... .......... .......... 94% 25.6M 2s
475500K .......... .......... .......... .......... .......... 94% 23.3M 2s
475550K .......... .......... .......... .......... .......... 94% 39.6M 2s
475600K .......... .......... .......... .......... .......... 94% 24.4M 2s
475650K .......... .......... .......... .......... .......... 94% 20.6M 2s
475700K .......... .......... .......... .......... .......... 94% 20.9M 2s
475750K .......... .......... .......... .......... .......... 94% 19.7M 2s
475800K .......... .......... .......... .......... .......... 94% 23.5M 2s
475850K .......... .......... .......... .......... .......... 94% 23.8M 2s
475900K .......... .......... .......... .......... .......... 94% 24.9M 2s
475950K .......... .......... .......... .......... .......... 94% 21.1M 2s
476000K .......... .......... .......... .......... .......... 94% 31.8M 2s
476050K .......... .......... .......... .......... .......... 94% 23.2M 2s
476100K .......... .......... .......... .......... .......... 94% 23.6M 2s
476150K .......... .......... .......... .......... .......... 94% 31.6M 2s
476200K .......... .......... .......... .......... .......... 94% 22.0M 2s
476250K .......... .......... .......... .......... .......... 94% 14.5M 2s
476300K .......... .......... .......... .......... .......... 94% 29.1M 2s
476350K .......... .......... .......... .......... .......... 94% 18.5M 2s
476400K .......... .......... .......... .......... .......... 94% 17.1M 2s
476450K .......... .......... .......... .......... .......... 94% 22.2M 2s
476500K .......... .......... .......... .......... .......... 94% 18.5M 2s
476550K .......... .......... .......... .......... .......... 94% 18.6M 2s
476600K .......... .......... .......... .......... .......... 94% 14.3M 2s
476650K .......... .......... .......... .......... .......... 94% 19.6M 2s
476700K .......... .......... .......... .......... .......... 94% 7.02M 2s
476750K .......... .......... .......... .......... .......... 94% 11.8M 2s
476800K .......... .......... .......... .......... .......... 94% 11.4M 2s
476850K .......... .......... .......... .......... .......... 94% 11.4M 2s
476900K .......... .......... .......... .......... .......... 94% 11.8M 2s
476950K .......... .......... .......... .......... .......... 94% 9.95M 2s
477000K .......... .......... .......... .......... .......... 94% 14.5M 2s
477050K .......... .......... .......... .......... .......... 94% 11.1M 2s
477100K .......... .......... .......... .......... .......... 94% 9.44M 2s
477150K .......... .......... .......... .......... .......... 94% 9.53M 2s
477200K .......... .......... .......... .......... .......... 94% 15.0M 2s
477250K .......... .......... .......... .......... .......... 94% 45.5M 2s
477300K .......... .......... .......... .......... .......... 94% 14.4M 2s
477350K .......... .......... .......... .......... .......... 94% 13.4M 2s
477400K .......... .......... .......... .......... .......... 94% 20.1M 2s
477450K .......... .......... .......... .......... .......... 94% 14.2M 2s
477500K .......... .......... .......... .......... .......... 94% 17.0M 2s
477550K .......... .......... .......... .......... .......... 94% 14.4M 2s
477600K .......... .......... .......... .......... .......... 94% 16.5M 2s
477650K .......... .......... .......... .......... .......... 94% 18.4M 2s
477700K .......... .......... .......... .......... .......... 94% 14.8M 2s
477750K .......... .......... .......... .......... .......... 94% 18.1M 2s
477800K .......... .......... .......... .......... .......... 94% 17.3M 2s
477850K .......... .......... .......... .......... .......... 94% 16.0M 2s
477900K .......... .......... .......... .......... .......... 94% 16.9M 2s
477950K .......... .......... .......... .......... .......... 94% 14.9M 2s
478000K .......... .......... .......... .......... .......... 94% 93.0M 2s
478050K .......... .......... .......... .......... .......... 94% 25.5M 2s
478100K .......... .......... .......... .......... .......... 94% 11.5M 2s
478150K .......... .......... .......... .......... .......... 94% 42.9M 2s
478200K .......... .......... .......... .......... .......... 94% 26.0M 2s
478250K .......... .......... .......... .......... .......... 94% 24.3M 2s
478300K .......... .......... .......... .......... .......... 94% 22.7M 2s
478350K .......... .......... .......... .......... .......... 94% 17.2M 2s
478400K .......... .......... .......... .......... .......... 94% 21.9M 2s
478450K .......... .......... .......... .......... .......... 94% 17.2M 2s
478500K .......... .......... .......... .......... .......... 94% 18.9M 2s
478550K .......... .......... .......... .......... .......... 94% 17.0M 2s
478600K .......... .......... .......... .......... .......... 94% 17.2M 2s
478650K .......... .......... .......... .......... .......... 94% 25.5M 2s
478700K .......... .......... .......... .......... .......... 94% 15.6M 2s
478750K .......... .......... .......... .......... .......... 94% 19.5M 2s
478800K .......... .......... .......... .......... .......... 94% 19.6M 2s
478850K .......... .......... .......... .......... .......... 94% 18.9M 2s
478900K .......... .......... .......... .......... .......... 94% 18.0M 2s
478950K .......... .......... .......... .......... .......... 94% 10.2M 2s
479000K .......... .......... .......... .......... .......... 94% 79.0M 2s
479050K .......... .......... .......... .......... .......... 94% 36.7M 2s
479100K .......... .......... .......... .......... .......... 94% 12.4M 2s
479150K .......... .......... .......... .......... .......... 94% 61.7M 2s
479200K .......... .......... .......... .......... .......... 94% 20.9M 2s
479250K .......... .......... .......... .......... .......... 94% 17.0M 2s
479300K .......... .......... .......... .......... .......... 94% 22.1M 2s
479350K .......... .......... .......... .......... .......... 94% 16.4M 2s
479400K .......... .......... .......... .......... .......... 95% 17.1M 2s
479450K .......... .......... .......... .......... .......... 95% 6.34M 2s
479500K .......... .......... .......... .......... .......... 95% 80.3M 2s
479550K .......... .......... .......... .......... .......... 95% 71.9M 2s
479600K .......... .......... .......... .......... .......... 95% 57.2M 2s
479650K .......... .......... .......... .......... .......... 95% 18.0M 2s
479700K .......... .......... .......... .......... .......... 95% 19.8M 2s
479750K .......... .......... .......... .......... .......... 95% 16.6M 2s
479800K .......... .......... .......... .......... .......... 95% 23.4M 2s
479850K .......... .......... .......... .......... .......... 95% 17.1M 2s
479900K .......... .......... .......... .......... .......... 95% 27.0M 2s
479950K .......... .......... .......... .......... .......... 95% 7.48M 2s
480000K .......... .......... .......... .......... .......... 95% 29.2M 2s
480050K .......... .......... .......... .......... .......... 95% 21.9M 2s
480100K .......... .......... .......... .......... .......... 95% 28.8M 2s
480150K .......... .......... .......... .......... .......... 95% 18.1M 2s
480200K .......... .......... .......... .......... .......... 95% 16.9M 2s
480250K .......... .......... .......... .......... .......... 95% 18.1M 2s
480300K .......... .......... .......... .......... .......... 95% 29.6M 2s
480350K .......... .......... .......... .......... .......... 95% 19.3M 2s
480400K .......... .......... .......... .......... .......... 95% 28.1M 2s
480450K .......... .......... .......... .......... .......... 95% 18.6M 2s
480500K .......... .......... .......... .......... .......... 95% 27.9M 2s
480550K .......... .......... .......... .......... .......... 95% 22.8M 2s
480600K .......... .......... .......... .......... .......... 95% 17.1M 2s
480650K .......... .......... .......... .......... .......... 95% 25.4M 2s
480700K .......... .......... .......... .......... .......... 95% 15.0M 2s
480750K .......... .......... .......... .......... .......... 95% 37.3M 2s
480800K .......... .......... .......... .......... .......... 95% 26.5M 2s
480850K .......... .......... .......... .......... .......... 95% 25.4M 2s
480900K .......... .......... .......... .......... .......... 95% 38.2M 2s
480950K .......... .......... .......... .......... .......... 95% 20.2M 2s
481000K .......... .......... .......... .......... .......... 95% 36.3M 2s
481050K .......... .......... .......... .......... .......... 95% 83.6M 2s
481100K .......... .......... .......... .......... .......... 95% 44.4M 2s
481150K .......... .......... .......... .......... .......... 95% 73.6M 2s
481200K .......... .......... .......... .......... .......... 95% 71.5M 2s
481250K .......... .......... .......... .......... .......... 95% 76.2M 2s
481300K .......... .......... .......... .......... .......... 95% 78.8M 2s
481350K .......... .......... .......... .......... .......... 95% 73.1M 2s
481400K .......... .......... .......... .......... .......... 95% 48.2M 2s
481450K .......... .......... .......... .......... .......... 95% 54.8M 2s
481500K .......... .......... .......... .......... .......... 95% 51.1M 2s
481550K .......... .......... .......... .......... .......... 95% 41.2M 2s
481600K .......... .......... .......... .......... .......... 95% 47.5M 2s
481650K .......... .......... .......... .......... .......... 95% 41.2M 2s
481700K .......... .......... .......... .......... .......... 95% 42.5M 2s
481750K .......... .......... .......... .......... .......... 95% 57.2M 2s
481800K .......... .......... .......... .......... .......... 95% 54.4M 2s
481850K .......... .......... .......... .......... .......... 95% 37.2M 2s
481900K .......... .......... .......... .......... .......... 95% 41.6M 2s
481950K .......... .......... .......... .......... .......... 95% 53.7M 2s
482000K .......... .......... .......... .......... .......... 95% 50.2M 2s
482050K .......... .......... .......... .......... .......... 95% 43.7M 2s
482100K .......... .......... .......... .......... .......... 95% 46.2M 2s
482150K .......... .......... .......... .......... .......... 95% 73.9M 2s
482200K .......... .......... .......... .......... .......... 95% 43.7M 2s
482250K .......... .......... .......... .......... .......... 95% 45.9M 2s
482300K .......... .......... .......... .......... .......... 95% 49.8M 2s
482350K .......... .......... .......... .......... .......... 95% 47.4M 2s
482400K .......... .......... .......... .......... .......... 95% 45.5M 2s
482450K .......... .......... .......... .......... .......... 95% 46.7M 2s
482500K .......... .......... .......... .......... .......... 95% 37.0M 2s
482550K .......... .......... .......... .......... .......... 95% 53.7M 2s
482600K .......... .......... .......... .......... .......... 95% 39.7M 2s
482650K .......... .......... .......... .......... .......... 95% 55.9M 2s
482700K .......... .......... .......... .......... .......... 95% 47.0M 2s
482750K .......... .......... .......... .......... .......... 95% 38.6M 2s
482800K .......... .......... .......... .......... .......... 95% 50.6M 2s
482850K .......... .......... .......... .......... .......... 95% 31.1M 2s
482900K .......... .......... .......... .......... .......... 95% 40.4M 2s
482950K .......... .......... .......... .......... .......... 95% 13.8M 2s
483000K .......... .......... .......... .......... .......... 95%  142M 2s
483050K .......... .......... .......... .......... .......... 95% 52.3M 2s
483100K .......... .......... .......... .......... .......... 95% 35.1M 2s
483150K .......... .......... .......... .......... .......... 95% 48.5M 2s
483200K .......... .......... .......... .......... .......... 95% 37.0M 2s
483250K .......... .......... .......... .......... .......... 95% 28.8M 2s
483300K .......... .......... .......... .......... .......... 95% 26.5M 2s
483350K .......... .......... .......... .......... .......... 95% 20.3M 2s
483400K .......... .......... .......... .......... .......... 95% 44.1M 2s
483450K .......... .......... .......... .......... .......... 95% 17.7M 2s
483500K .......... .......... .......... .......... .......... 95% 22.0M 2s
483550K .......... .......... .......... .......... .......... 95% 23.9M 2s
483600K .......... .......... .......... .......... .......... 95% 18.1M 2s
483650K .......... .......... .......... .......... .......... 95% 22.1M 2s
483700K .......... .......... .......... .......... .......... 95% 19.0M 2s
483750K .......... .......... .......... .......... .......... 95% 23.5M 2s
483800K .......... .......... .......... .......... .......... 95% 21.4M 2s
483850K .......... .......... .......... .......... .......... 95% 22.7M 2s
483900K .......... .......... .......... .......... .......... 95% 24.0M 2s
483950K .......... .......... .......... .......... .......... 95% 21.9M 2s
484000K .......... .......... .......... .......... .......... 95% 20.7M 2s
484050K .......... .......... .......... .......... .......... 95% 24.5M 2s
484100K .......... .......... .......... .......... .......... 95% 7.91M 2s
484150K .......... .......... .......... .......... .......... 95% 99.9M 2s
484200K .......... .......... .......... .......... .......... 95% 24.4M 2s
484250K .......... .......... .......... .......... .......... 95% 23.5M 2s
484300K .......... .......... .......... .......... .......... 95% 20.8M 2s
484350K .......... .......... .......... .......... .......... 95% 15.8M 2s
484400K .......... .......... .......... .......... .......... 95% 24.0M 2s
484450K .......... .......... .......... .......... .......... 96% 21.4M 2s
484500K .......... .......... .......... .......... .......... 96% 19.0M 2s
484550K .......... .......... .......... .......... .......... 96% 24.8M 2s
484600K .......... .......... .......... .......... .......... 96% 19.6M 2s
484650K .......... .......... .......... .......... .......... 96% 20.1M 2s
484700K .......... .......... .......... .......... .......... 96% 24.3M 2s
484750K .......... .......... .......... .......... .......... 96% 22.2M 2s
484800K .......... .......... .......... .......... .......... 96% 21.3M 1s
484850K .......... .......... .......... .......... .......... 96% 18.5M 1s
484900K .......... .......... .......... .......... .......... 96% 20.0M 1s
484950K .......... .......... .......... .......... .......... 96% 24.0M 1s
485000K .......... .......... .......... .......... .......... 96% 44.4M 1s
485050K .......... .......... .......... .......... .......... 96% 34.7M 1s
485100K .......... .......... .......... .......... .......... 96% 41.4M 1s
485150K .......... .......... .......... .......... .......... 96% 86.1M 1s
485200K .......... .......... .......... .......... .......... 96% 14.1M 1s
485250K .......... .......... .......... .......... .......... 96%  109M 1s
485300K .......... .......... .......... .......... .......... 96% 26.8M 1s
485350K .......... .......... .......... .......... .......... 96% 61.3M 1s
485400K .......... .......... .......... .......... .......... 96% 34.4M 1s
485450K .......... .......... .......... .......... .......... 96% 62.0M 1s
485500K .......... .......... .......... .......... .......... 96% 24.8M 1s
485550K .......... .......... .......... .......... .......... 96% 27.9M 1s
485600K .......... .......... .......... .......... .......... 96% 26.3M 1s
485650K .......... .......... .......... .......... .......... 96% 30.5M 1s
485700K .......... .......... .......... .......... .......... 96% 22.1M 1s
485750K .......... .......... .......... .......... .......... 96% 34.4M 1s
485800K .......... .......... .......... .......... .......... 96% 26.4M 1s
485850K .......... .......... .......... .......... .......... 96% 23.5M 1s
485900K .......... .......... .......... .......... .......... 96% 37.3M 1s
485950K .......... .......... .......... .......... .......... 96% 20.8M 1s
486000K .......... .......... .......... .......... .......... 96% 32.1M 1s
486050K .......... .......... .......... .......... .......... 96% 30.2M 1s
486100K .......... .......... .......... .......... .......... 96% 23.5M 1s
486150K .......... .......... .......... .......... .......... 96% 34.6M 1s
486200K .......... .......... .......... .......... .......... 96% 21.9M 1s
486250K .......... .......... .......... .......... .......... 96% 34.4M 1s
486300K .......... .......... .......... .......... .......... 96% 26.7M 1s
486350K .......... .......... .......... .......... .......... 96% 29.5M 1s
486400K .......... .......... .......... .......... .......... 96% 22.8M 1s
486450K .......... .......... .......... .......... .......... 96% 36.5M 1s
486500K .......... .......... .......... .......... .......... 96% 13.1M 1s
486550K .......... .......... .......... .......... .......... 96% 27.7M 1s
486600K .......... .......... .......... .......... .......... 96% 93.5M 1s
486650K .......... .......... .......... .......... .......... 96% 37.4M 1s
486700K .......... .......... .......... .......... .......... 96% 34.8M 1s
486750K .......... .......... .......... .......... .......... 96% 27.2M 1s
486800K .......... .......... .......... .......... .......... 96% 29.1M 1s
486850K .......... .......... .......... .......... .......... 96% 21.7M 1s
486900K .......... .......... .......... .......... .......... 96% 22.0M 1s
486950K .......... .......... .......... .......... .......... 96% 16.4M 1s
487000K .......... .......... .......... .......... .......... 96% 19.6M 1s
487050K .......... .......... .......... .......... .......... 96% 18.7M 1s
487100K .......... .......... .......... .......... .......... 96% 14.5M 1s
487150K .......... .......... .......... .......... .......... 96% 25.2M 1s
487200K .......... .......... .......... .......... .......... 96% 15.6M 1s
487250K .......... .......... .......... .......... .......... 96% 27.0M 1s
487300K .......... .......... .......... .......... .......... 96% 18.7M 1s
487350K .......... .......... .......... .......... .......... 96% 14.4M 1s
487400K .......... .......... .......... .......... .......... 96% 17.2M 1s
487450K .......... .......... .......... .......... .......... 96% 19.8M 1s
487500K .......... .......... .......... .......... .......... 96% 19.1M 1s
487550K .......... .......... .......... .......... .......... 96% 21.8M 1s
487600K .......... .......... .......... .......... .......... 96% 11.4M 1s
487650K .......... .......... .......... .......... .......... 96% 51.4M 1s
487700K .......... .......... .......... .......... .......... 96% 22.8M 1s
487750K .......... .......... .......... .......... .......... 96% 33.0M 1s
487800K .......... .......... .......... .......... .......... 96% 20.5M 1s
487850K .......... .......... .......... .......... .......... 96% 20.6M 1s
487900K .......... .......... .......... .......... .......... 96% 21.1M 1s
487950K .......... .......... .......... .......... .......... 96% 21.4M 1s
488000K .......... .......... .......... .......... .......... 96% 22.7M 1s
488050K .......... .......... .......... .......... .......... 96% 24.8M 1s
488100K .......... .......... .......... .......... .......... 96% 22.1M 1s
488150K .......... .......... .......... .......... .......... 96% 25.1M 1s
488200K .......... .......... .......... .......... .......... 96% 22.3M 1s
488250K .......... .......... .......... .......... .......... 96% 22.6M 1s
488300K .......... .......... .......... .......... .......... 96% 22.8M 1s
488350K .......... .......... .......... .......... .......... 96% 13.7M 1s
488400K .......... .......... .......... .......... .......... 96% 24.0M 1s
488450K .......... .......... .......... .......... .......... 96% 13.5M 1s
488500K .......... .......... .......... .......... .......... 96% 10.4M 1s
488550K .......... .......... .......... .......... .......... 96% 7.67M 1s
488600K .......... .......... .......... .......... .......... 96% 8.40M 1s
488650K .......... .......... .......... .......... .......... 96% 15.1M 1s
488700K .......... .......... .......... .......... .......... 96% 7.44M 1s
488750K .......... .......... .......... .......... .......... 96% 12.5M 1s
488800K .......... .......... .......... .......... .......... 96% 9.80M 1s
488850K .......... .......... .......... .......... .......... 96% 10.2M 1s
488900K .......... .......... .......... .......... .......... 96% 11.1M 1s
488950K .......... .......... .......... .......... .......... 96% 10.3M 1s
489000K .......... .......... .......... .......... .......... 96% 12.5M 1s
489050K .......... .......... .......... .......... .......... 96% 15.3M 1s
489100K .......... .......... .......... .......... .......... 96% 7.85M 1s
489150K .......... .......... .......... .......... .......... 96% 15.8M 1s
489200K .......... .......... .......... .......... .......... 96% 9.61M 1s
489250K .......... .......... .......... .......... .......... 96% 14.0M 1s
489300K .......... .......... .......... .......... .......... 96% 7.32M 1s
489350K .......... .......... .......... .......... .......... 96% 7.11M 1s
489400K .......... .......... .......... .......... .......... 96% 8.43M 1s
489450K .......... .......... .......... .......... .......... 96% 15.6M 1s
489500K .......... .......... .......... .......... .......... 97% 19.0M 1s
489550K .......... .......... .......... .......... .......... 97% 17.8M 1s
489600K .......... .......... .......... .......... .......... 97% 18.9M 1s
489650K .......... .......... .......... .......... .......... 97% 18.7M 1s
489700K .......... .......... .......... .......... .......... 97% 12.9M 1s
489750K .......... .......... .......... .......... .......... 97% 22.9M 1s
489800K .......... .......... .......... .......... .......... 97% 17.7M 1s
489850K .......... .......... .......... .......... .......... 97% 12.2M 1s
489900K .......... .......... .......... .......... .......... 97% 19.7M 1s
489950K .......... .......... .......... .......... .......... 97% 18.0M 1s
490000K .......... .......... .......... .......... .......... 97% 13.2M 1s
490050K .......... .......... .......... .......... .......... 97% 5.76M 1s
490100K .......... .......... .......... .......... .......... 97% 71.9M 1s
490150K .......... .......... .......... .......... .......... 97% 90.8M 1s
490200K .......... .......... .......... .......... .......... 97% 28.7M 1s
490250K .......... .......... .......... .......... .......... 97% 18.7M 1s
490300K .......... .......... .......... .......... .......... 97% 22.0M 1s
490350K .......... .......... .......... .......... .......... 97% 15.7M 1s
490400K .......... .......... .......... .......... .......... 97% 23.2M 1s
490450K .......... .......... .......... .......... .......... 97% 14.5M 1s
490500K .......... .......... .......... .......... .......... 97% 25.1M 1s
490550K .......... .......... .......... .......... .......... 97% 16.4M 1s
490600K .......... .......... .......... .......... .......... 97% 15.0M 1s
490650K .......... .......... .......... .......... .......... 97% 18.9M 1s
490700K .......... .......... .......... .......... .......... 97% 16.4M 1s
490750K .......... .......... .......... .......... .......... 97% 22.4M 1s
490800K .......... .......... .......... .......... .......... 97% 17.5M 1s
490850K .......... .......... .......... .......... .......... 97% 15.4M 1s
490900K .......... .......... .......... .......... .......... 97% 21.1M 1s
490950K .......... .......... .......... .......... .......... 97% 66.9M 1s
491000K .......... .......... .......... .......... .......... 97% 12.8M 1s
491050K .......... .......... .......... .......... .......... 97% 79.1M 1s
491100K .......... .......... .......... .......... .......... 97% 12.8M 1s
491150K .......... .......... .......... .......... .......... 97%  110M 1s
491200K .......... .......... .......... .......... .......... 97% 97.3M 1s
491250K .......... .......... .......... .......... .......... 97% 71.6M 1s
491300K .......... .......... .......... .......... .......... 97% 16.0M 1s
491350K .......... .......... .......... .......... .......... 97% 51.0M 1s
491400K .......... .......... .......... .......... .......... 97% 26.7M 1s
491450K .......... .......... .......... .......... .......... 97% 23.7M 1s
491500K .......... .......... .......... .......... .......... 97% 25.4M 1s
491550K .......... .......... .......... .......... .......... 97% 24.5M 1s
491600K .......... .......... .......... .......... .......... 97% 18.7M 1s
491650K .......... .......... .......... .......... .......... 97% 31.7M 1s
491700K .......... .......... .......... .......... .......... 97% 23.2M 1s
491750K .......... .......... .......... .......... .......... 97% 25.2M 1s
491800K .......... .......... .......... .......... .......... 97% 27.8M 1s
491850K .......... .......... .......... .......... .......... 97% 17.7M 1s
491900K .......... .......... .......... .......... .......... 97% 31.1M 1s
491950K .......... .......... .......... .......... .......... 97% 23.9M 1s
492000K .......... .......... .......... .......... .......... 97% 26.6M 1s
492050K .......... .......... .......... .......... .......... 97% 23.1M 1s
492100K .......... .......... .......... .......... .......... 97% 15.8M 1s
492150K .......... .......... .......... .......... .......... 97% 17.1M 1s
492200K .......... .......... .......... .......... .......... 97% 12.3M 1s
492250K .......... .......... .......... .......... .......... 97% 27.8M 1s
492300K .......... .......... .......... .......... .......... 97% 29.6M 1s
492350K .......... .......... .......... .......... .......... 97% 30.2M 1s
492400K .......... .......... .......... .......... .......... 97% 19.3M 1s
492450K .......... .......... .......... .......... .......... 97% 18.0M 1s
492500K .......... .......... .......... .......... .......... 97% 20.0M 1s
492550K .......... .......... .......... .......... .......... 97% 18.1M 1s
492600K .......... .......... .......... .......... .......... 97% 18.0M 1s
492650K .......... .......... .......... .......... .......... 97% 22.1M 1s
492700K .......... .......... .......... .......... .......... 97% 18.9M 1s
492750K .......... .......... .......... .......... .......... 97% 19.6M 1s
492800K .......... .......... .......... .......... .......... 97% 20.8M 1s
492850K .......... .......... .......... .......... .......... 97% 17.4M 1s
492900K .......... .......... .......... .......... .......... 97% 20.9M 1s
492950K .......... .......... .......... .......... .......... 97% 19.5M 1s
493000K .......... .......... .......... .......... .......... 97% 22.6M 1s
493050K .......... .......... .......... .......... .......... 97% 26.7M 1s
493100K .......... .......... .......... .......... .......... 97% 26.9M 1s
493150K .......... .......... .......... .......... .......... 97% 17.1M 1s
493200K .......... .......... .......... .......... .......... 97% 27.9M 1s
493250K .......... .......... .......... .......... .......... 97% 95.4M 1s
493300K .......... .......... .......... .......... .......... 97% 16.8M 1s
493350K .......... .......... .......... .......... .......... 97% 87.2M 1s
493400K .......... .......... .......... .......... .......... 97% 18.4M 1s
493450K .......... .......... .......... .......... .......... 97% 33.8M 1s
493500K .......... .......... .......... .......... .......... 97% 25.9M 1s
493550K .......... .......... .......... .......... .......... 97% 21.8M 1s
493600K .......... .......... .......... .......... .......... 97% 19.8M 1s
493650K .......... .......... .......... .......... .......... 97% 27.5M 1s
493700K .......... .......... .......... .......... .......... 97% 21.6M 1s
493750K .......... .......... .......... .......... .......... 97% 23.5M 1s
493800K .......... .......... .......... .......... .......... 97% 23.6M 1s
493850K .......... .......... .......... .......... .......... 97% 27.6M 1s
493900K .......... .......... .......... .......... .......... 97% 20.4M 1s
493950K .......... .......... .......... .......... .......... 97% 19.6M 1s
494000K .......... .......... .......... .......... .......... 97% 27.8M 1s
494050K .......... .......... .......... .......... .......... 97% 19.8M 1s
494100K .......... .......... .......... .......... .......... 97% 19.1M 1s
494150K .......... .......... .......... .......... .......... 97% 46.6M 1s
494200K .......... .......... .......... .......... .......... 97% 18.8M 1s
494250K .......... .......... .......... .......... .......... 97% 25.0M 1s
494300K .......... .......... .......... .......... .......... 97% 17.2M 1s
494350K .......... .......... .......... .......... .......... 97% 10.8M 1s
494400K .......... .......... .......... .......... .......... 97% 37.8M 1s
494450K .......... .......... .......... .......... .......... 97% 21.2M 1s
494500K .......... .......... .......... .......... .......... 97% 70.2M 1s
494550K .......... .......... .......... .......... .......... 98% 24.7M 1s
494600K .......... .......... .......... .......... .......... 98% 18.9M 1s
494650K .......... .......... .......... .......... .......... 98% 21.2M 1s
494700K .......... .......... .......... .......... .......... 98% 17.1M 1s
494750K .......... .......... .......... .......... .......... 98% 17.8M 1s
494800K .......... .......... .......... .......... .......... 98% 21.9M 1s
494850K .......... .......... .......... .......... .......... 98% 16.5M 1s
494900K .......... .......... .......... .......... .......... 98% 14.6M 1s
494950K .......... .......... .......... .......... .......... 98% 28.8M 1s
495000K .......... .......... .......... .......... .......... 98% 20.9M 1s
495050K .......... .......... .......... .......... .......... 98% 17.8M 1s
495100K .......... .......... .......... .......... .......... 98% 17.1M 1s
495150K .......... .......... .......... .......... .......... 98% 15.0M 1s
495200K .......... .......... .......... .......... .......... 98% 11.4M 1s
495250K .......... .......... .......... .......... .......... 98% 11.0M 1s
495300K .......... .......... .......... .......... .......... 98% 11.7M 1s
495350K .......... .......... .......... .......... .......... 98% 9.24M 1s
495400K .......... .......... .......... .......... .......... 98% 11.8M 1s
495450K .......... .......... .......... .......... .......... 98% 7.79M 1s
495500K .......... .......... .......... .......... .......... 98% 15.2M 1s
495550K .......... .......... .......... .......... .......... 98% 11.1M 1s
495600K .......... .......... .......... .......... .......... 98% 10.1M 1s
495650K .......... .......... .......... .......... .......... 98% 18.9M 1s
495700K .......... .......... .......... .......... .......... 98% 10.4M 1s
495750K .......... .......... .......... .......... .......... 98% 88.5M 1s
495800K .......... .......... .......... .......... .......... 98% 14.5M 1s
495850K .......... .......... .......... .......... .......... 98% 42.6M 1s
495900K .......... .......... .......... .......... .......... 98% 19.9M 1s
495950K .......... .......... .......... .......... .......... 98% 18.5M 1s
496000K .......... .......... .......... .......... .......... 98% 21.0M 1s
496050K .......... .......... .......... .......... .......... 98% 17.8M 1s
496100K .......... .......... .......... .......... .......... 98% 15.7M 1s
496150K .......... .......... .......... .......... .......... 98% 22.3M 1s
496200K .......... .......... .......... .......... .......... 98% 15.7M 1s
496250K .......... .......... .......... .......... .......... 98% 21.0M 1s
496300K .......... .......... .......... .......... .......... 98% 19.7M 1s
496350K .......... .......... .......... .......... .......... 98% 15.7M 1s
496400K .......... .......... .......... .......... .......... 98% 17.1M 1s
496450K .......... .......... .......... .......... .......... 98% 15.2M 1s
496500K .......... .......... .......... .......... .......... 98% 18.7M 1s
496550K .......... .......... .......... .......... .......... 98% 27.2M 1s
496600K .......... .......... .......... .......... .......... 98% 15.6M 1s
496650K .......... .......... .......... .......... .......... 98% 15.7M 1s
496700K .......... .......... .......... .......... .......... 98% 21.8M 1s
496750K .......... .......... .......... .......... .......... 98% 38.0M 1s
496800K .......... .......... .......... .......... .......... 98% 16.2M 1s
496850K .......... .......... .......... .......... .......... 98% 19.8M 1s
496900K .......... .......... .......... .......... .......... 98% 19.5M 1s
496950K .......... .......... .......... .......... .......... 98% 17.2M 1s
497000K .......... .......... .......... .......... .......... 98% 13.3M 1s
497050K .......... .......... .......... .......... .......... 98% 23.5M 1s
497100K .......... .......... .......... .......... .......... 98% 17.8M 1s
497150K .......... .......... .......... .......... .......... 98% 18.2M 1s
497200K .......... .......... .......... .......... .......... 98% 17.0M 1s
497250K .......... .......... .......... .......... .......... 98% 19.0M 1s
497300K .......... .......... .......... .......... .......... 98% 19.2M 1s
497350K .......... .......... .......... .......... .......... 98% 22.5M 1s
497400K .......... .......... .......... .......... .......... 98% 25.2M 1s
497450K .......... .......... .......... .......... .......... 98% 11.3M 1s
497500K .......... .......... .......... .......... .......... 98% 74.3M 1s
497550K .......... .......... .......... .......... .......... 98% 70.0M 1s
497600K .......... .......... .......... .......... .......... 98% 26.9M 1s
497650K .......... .......... .......... .......... .......... 98% 78.8M 1s
497700K .......... .......... .......... .......... .......... 98% 26.7M 1s
497750K .......... .......... .......... .......... .......... 98% 35.3M 1s
497800K .......... .......... .......... .......... .......... 98% 17.8M 1s
497850K .......... .......... .......... .......... .......... 98% 31.7M 1s
497900K .......... .......... .......... .......... .......... 98% 34.3M 1s
497950K .......... .......... .......... .......... .......... 98% 18.8M 1s
498000K .......... .......... .......... .......... .......... 98% 37.7M 0s
498050K .......... .......... .......... .......... .......... 98% 25.4M 0s
498100K .......... .......... .......... .......... .......... 98% 25.0M 0s
498150K .......... .......... .......... .......... .......... 98% 30.7M 0s
498200K .......... .......... .......... .......... .......... 98% 22.5M 0s
498250K .......... .......... .......... .......... .......... 98% 24.7M 0s
498300K .......... .......... .......... .......... .......... 98% 22.9M 0s
498350K .......... .......... .......... .......... .......... 98% 24.4M 0s
498400K .......... .......... .......... .......... .......... 98% 25.6M 0s
498450K .......... .......... .......... .......... .......... 98% 18.9M 0s
498500K .......... .......... .......... .......... .......... 98% 25.0M 0s
498550K .......... .......... .......... .......... .......... 98% 33.8M 0s
498600K .......... .......... .......... .......... .......... 98% 21.3M 0s
498650K .......... .......... .......... .......... .......... 98% 23.8M 0s
498700K .......... .......... .......... .......... .......... 98% 25.6M 0s
498750K .......... .......... .......... .......... .......... 98% 22.7M 0s
498800K .......... .......... .......... .......... .......... 98% 89.3M 0s
498850K .......... .......... .......... .......... .......... 98% 14.0M 0s
498900K .......... .......... .......... .......... .......... 98% 81.9M 0s
498950K .......... .......... .......... .......... .......... 98% 71.3M 0s
499000K .......... .......... .......... .......... .......... 98% 25.0M 0s
499050K .......... .......... .......... .......... .......... 98% 83.9M 0s
499100K .......... .......... .......... .......... .......... 98% 50.4M 0s
499150K .......... .......... .......... .......... .......... 98% 41.5M 0s
499200K .......... .......... .......... .......... .......... 98% 39.4M 0s
499250K .......... .......... .......... .......... .......... 98% 33.5M 0s
499300K .......... .......... .......... .......... .......... 98% 40.6M 0s
499350K .......... .......... .......... .......... .......... 98% 36.7M 0s
499400K .......... .......... .......... .......... .......... 98% 34.1M 0s
499450K .......... .......... .......... .......... .......... 98% 49.5M 0s
499500K .......... .......... .......... .......... .......... 98% 43.8M 0s
499550K .......... .......... .......... .......... .......... 98% 41.7M 0s
499600K .......... .......... .......... .......... .......... 99% 42.0M 0s
499650K .......... .......... .......... .......... .......... 99% 34.4M 0s
499700K .......... .......... .......... .......... .......... 99% 37.1M 0s
499750K .......... .......... .......... .......... .......... 99% 47.0M 0s
499800K .......... .......... .......... .......... .......... 99% 49.4M 0s
499850K .......... .......... .......... .......... .......... 99% 44.2M 0s
499900K .......... .......... .......... .......... .......... 99% 44.1M 0s
499950K .......... .......... .......... .......... .......... 99% 39.0M 0s
500000K .......... .......... .......... .......... .......... 99% 46.7M 0s
500050K .......... .......... .......... .......... .......... 99% 45.0M 0s
500100K .......... .......... .......... .......... .......... 99% 41.4M 0s
500150K .......... .......... .......... .......... .......... 99% 43.3M 0s
500200K .......... .......... .......... .......... .......... 99% 34.0M 0s
500250K .......... .......... .......... .......... .......... 99% 58.8M 0s
500300K .......... .......... .......... .......... .......... 99% 56.3M 0s
500350K .......... .......... .......... .......... .......... 99% 36.9M 0s
500400K .......... .......... .......... .......... .......... 99% 41.5M 0s
500450K .......... .......... .......... .......... .......... 99% 53.7M 0s
500500K .......... .......... .......... .......... .......... 99% 37.4M 0s
500550K .......... .......... .......... .......... .......... 99% 46.8M 0s
500600K .......... .......... .......... .......... .......... 99% 45.4M 0s
500650K .......... .......... .......... .......... .......... 99% 38.5M 0s
500700K .......... .......... .......... .......... .......... 99% 76.1M 0s
500750K .......... .......... .......... .......... .......... 99% 13.7M 0s
500800K .......... .......... .......... .......... .......... 99% 35.7M 0s
500850K .......... .......... .......... .......... .......... 99%  311M 0s
500900K .......... .......... .......... .......... .......... 99%  359M 0s
500950K .......... .......... .......... .......... .......... 99% 26.1M 0s
501000K .......... .......... .......... .......... .......... 99% 63.2M 0s
501050K .......... .......... .......... .......... .......... 99% 30.3M 0s
501100K .......... .......... .......... .......... .......... 99%  144M 0s
501150K .......... .......... .......... .......... .......... 99%  163M 0s
501200K .......... .......... .......... .......... .......... 99% 83.6M 0s
501250K .......... .......... .......... .......... .......... 99% 87.5M 0s
501300K .......... .......... .......... .......... .......... 99% 38.9M 0s
501350K .......... .......... .......... .......... .......... 99% 38.3M 0s
501400K .......... .......... .......... .......... .......... 99% 43.1M 0s
501450K .......... .......... .......... .......... .......... 99% 30.2M 0s
501500K .......... .......... .......... .......... .......... 99% 61.7M 0s
501550K .......... .......... .......... .......... .......... 99% 53.2M 0s
501600K .......... .......... .......... .......... .......... 99% 34.8M 0s
501650K .......... .......... .......... .......... .......... 99% 47.4M 0s
501700K .......... .......... .......... .......... .......... 99% 34.2M 0s
501750K .......... .......... .......... .......... .......... 99% 42.2M 0s
501800K .......... .......... .......... .......... .......... 99% 61.4M 0s
501850K .......... .......... .......... .......... .......... 99% 35.0M 0s
501900K .......... .......... .......... .......... .......... 99% 47.6M 0s
501950K .......... .......... .......... .......... .......... 99% 38.0M 0s
502000K .......... .......... .......... .......... .......... 99% 42.2M 0s
502050K .......... .......... .......... .......... .......... 99% 54.1M 0s
502100K .......... .......... .......... .......... .......... 99% 37.7M 0s
502150K .......... .......... .......... .......... .......... 99% 47.2M 0s
502200K .......... .......... .......... .......... .......... 99% 42.3M 0s
502250K .......... .......... .......... .......... .......... 99% 40.7M 0s
502300K .......... .......... .......... .......... .......... 99% 39.0M 0s
502350K .......... .......... .......... .......... .......... 99% 42.0M 0s
502400K .......... .......... .......... .......... .......... 99% 54.4M 0s
502450K .......... .......... .......... .......... .......... 99% 37.4M 0s
502500K .......... .......... .......... .......... .......... 99% 41.9M 0s
502550K .......... .......... .......... .......... .......... 99% 40.8M 0s
502600K .......... .......... .......... .......... .......... 99% 27.8M 0s
502650K .......... .......... .......... .......... .......... 99% 47.4M 0s
502700K .......... .......... .......... .......... .......... 99% 37.5M 0s
502750K .......... .......... .......... .......... .......... 99% 53.5M 0s
502800K .......... .......... .......... .......... .......... 99% 43.1M 0s
502850K .......... .......... .......... .......... .......... 99% 11.7M 0s
502900K .......... .......... .......... .......... .......... 99%  425M 0s
502950K .......... .......... .......... .......... .......... 99% 68.4M 0s
503000K .......... .......... .......... .......... .......... 99%  448M 0s
503050K .......... .......... .......... .......... .......... 99% 31.7M 0s
503100K .......... .......... .......... .......... .......... 99% 54.6M 0s
503150K .......... .......... .......... .......... .......... 99% 30.1M 0s
503200K .......... .......... .......... .......... .......... 99% 42.8M 0s
503250K .......... .......... .......... .......... .......... 99% 27.6M 0s
503300K .......... .......... .......... .......... .......... 99% 67.4M 0s
503350K .......... .......... .......... .......... .......... 99% 22.2M 0s
503400K .......... .......... .......... .......... .......... 99% 41.6M 0s
503450K .......... .......... .......... .......... .......... 99% 27.2M 0s
503500K .......... .......... .......... .......... .......... 99% 31.4M 0s
503550K .......... .......... .......... .......... .......... 99% 34.0M 0s
503600K .......... .......... .......... .......... .......... 99% 21.4M 0s
503650K .......... .......... .......... .......... .......... 99% 33.8M 0s
503700K .......... .......... .......... .......... .......... 99% 23.8M 0s
503750K .......... .......... .......... .......... .......... 99% 26.9M 0s
503800K .......... .......... .......... .......... .......... 99% 26.7M 0s
503850K .......... .......... .......... .......... .......... 99% 22.6M 0s
503900K .......... .......... .......... .......... .......... 99% 34.1M 0s
503950K .......... .......... .......... .......... .......... 99% 24.6M 0s
504000K .......... .......... .......... .......... .......... 99% 24.8M 0s
504050K .......... .......... .......... .......... .......... 99% 20.8M 0s
504100K .......... .......... .......... .......... .......... 99% 25.7M 0s
504150K .......... .......... .......... .......... .......... 99% 40.2M 0s
504200K .......... .......... .......... .......... .......... 99% 21.7M 0s
504250K .......... .......... .......... .......... .......... 99% 37.7M 0s
504300K .......... .......... .......... .......... .......... 99% 31.1M 0s
504350K .......... .......... .......... .......... .......... 99% 10.1M 0s
504400K .......... .......... .......... .......... .......... 99%  142M 0s
504450K .......... .......... .......... .......... .......... 99% 49.0M 0s
504500K .......... .......... .......... .......... .......... 99% 24.3M 0s
504550K .......... .......... .......... .......... .......... 99% 40.6M 0s
504600K .......... .......... .......... .......... .......... 99% 44.3M 0s
504650K .......... .......... .......                         100% 56.6M=37s

2024-03-06 16:57:47 (13.1 MB/s) - ‘ESPbeta-macos-arm64.tgz’ saved [516790230/516790230]

+ 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-3.11.6/bin/idle3.11'
Patching '/Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/Python-3.11.6/bin/pyftsubset'
Patching '/Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/Python-3.11.6/bin/test_op4'
Patching '/Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/Python-3.11.6/bin/ttx'
Patching '/Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/Python-3.11.6/bin/wingproj'
Patching '/Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/Python-3.11.6/bin/test_op2'
Patching '/Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/Python-3.11.6/bin/pip3'
Patching '/Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/Python-3.11.6/bin/test_bdf'
Patching '/Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/Python-3.11.6/bin/aggregate_profile.pl'
Patching '/Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/Python-3.11.6/bin/imageio_remove_bin'
Patching '/Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/Python-3.11.6/bin/undill'
Patching '/Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/Python-3.11.6/bin/bdf'
Patching '/Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/Python-3.11.6/bin/run_om_test'
Patching '/Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/Python-3.11.6/bin/f90nml'
Patching '/Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/Python-3.11.6/bin/profile2mat.pl'
Patching '/Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/Python-3.11.6/bin/webview'
Patching '/Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/Python-3.11.6/bin/fonttools'
Patching '/Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/Python-3.11.6/bin/openmdao'
Patching '/Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/Python-3.11.6/bin/pyNastranGUI'
Patching '/Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/Python-3.11.6/bin/f2py'
Patching '/Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/Python-3.11.6/bin/pip'
Patching '/Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/Python-3.11.6/bin/pydoc3.11'
Patching '/Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/Python-3.11.6/bin/2to3-3.11'
Patching '/Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/Python-3.11.6/bin/imageio_download_bin'
Patching '/Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/Python-3.11.6/bin/pip3.11'
Patching '/Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/Python-3.11.6/bin/test_pynastrangui'
Patching '/Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/Python-3.11.6/bin/numba'
Patching '/Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/Python-3.11.6/bin/normalizer'
Patching '/Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/Python-3.11.6/bin/virtualenv'
Patching '/Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/Python-3.11.6/bin/reset_notebook'
Patching '/Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/Python-3.11.6/bin/get_gprof'
Patching '/Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/Python-3.11.6/bin/format_converter'
Patching '/Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/Python-3.11.6/bin/qtpy'
Patching '/Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/Python-3.11.6/bin/pyftmerge'
Patching '/Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/Python-3.11.6/bin/python3.11-config'
Patching '/Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/Python-3.11.6/bin/f06'
Patching '/Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/Python-3.11.6/bin/get_objgraph'
Patching '/Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/Python-3.11.6/lib/python3.11/config-3.11-darwin/Makefile'
Patching '/Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/Python-3.11.6/lib/python3.11/config-3.11-darwin/python-config.py'
Patching '/Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/Python-3.11.6/lib/pkgconfig/python-3.11-embed.pc'
Patching '/Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/Python-3.11.6/lib/pkgconfig/python-3.11.pc'
Patching '/Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/Python-3.11.6/lib/python3.11/_sysconfigdata__darwin_darwin.py'
Patching '/Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/Python-3.11.6/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-3.11.6/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-3.11.6/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-3.11.6/include/python3.11
++ PYTHONINC=/Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/Python-3.11.6/include/python3.11
++ export 'PYTHONLIB=-L/Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/Python-3.11.6/lib -lpython3.11'
++ PYTHONLIB='-L/Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/Python-3.11.6/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-3.11.6/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-3.11.6/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-3.11.6/bin/python
+ python --version
Python 3.11.6
+ 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	0m0.446s
user	0m0.134s
sys	0m0.027s
+ 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	0m0.240s
user	0m0.245s
sys	0m0.030s
+ 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	0m1.080s
user	0m1.712s
sys	0m0.662s
+ 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	0m0.273s
user	0m0.312s
sys	0m0.031s
+ 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	0m0.329s
user	0m0.464s
sys	0m0.054s
+ 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	0m0.311s
user	0m0.442s
sys	0m0.016s
+ 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	0m1.538s
user	0m2.997s
sys	0m0.353s
+ 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	0m11.452s
user	0m22.234s
sys	0m1.252s
+ 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	0m0.298s
user	0m0.366s
sys	0m0.011s
+ 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	0m12.520s
user	0m41.764s
sys	0m19.241s
+ 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	0m0.195s
user	0m0.208s
sys	0m0.023s
+ 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	0m0.369s
user	0m0.575s
sys	0m0.006s
+ 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	0m0.146s
user	0m0.159s
sys	0m0.005s
+ 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	0m0.250s
user	0m0.316s
sys	0m0.008s
+ set +x

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

+ cd /Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/EngSketchPad/pyESP/testEGADS
+ make test
python --version
Python 3.11.6
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 0.981s

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	0m3.076s
user	0m5.071s
sys	0m0.076s
++ set +x
=================================================
test_pyOCSM.py passed (as expected)
=================================================
+ cd /Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/EngSketchPad/pyESP/testCAPS
+ make test
python --version
Python 3.11.6
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 = 147
	Number of elements = 290
	Elemental Nodes = 0
	Elemental Rods  = 0
	Elemental Tria3 = 290
	Elemental Quad4 = 0
Combining multiple FEA meshes!
	Combined Number of nodal coordinates = 290
	Combined Number of elements = 572
	Combined Elemental Nodes = 0
	Combined Elemental Rods  = 0
	Combined Elemental Tria3 = 572
	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 7.512s

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 3.11.6
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 9.14.7
AFLR2    : Version Date   07/16/23 @ 01:42PM
AFLR2    : Compile OS     Darwin 22.6.0 arm64
AFLR2    : Compile Date   08/01/23 @ 11:39PM
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      =      1086      2174
AFLR2 IG : Nodes, Faces      =      1087      2176
AFLR2 IG : Nodes, Faces      =      1321      2644
AFLR2 IG : Nodes, Faces      =      1350      2702
AFLR2 IG : Nodes, Faces      =      1421      2844
AFLR2 IG : Nodes, Faces      =      1521      3044
AFLR2 IG : Nodes, Faces      =      1621      3244
AFLR2 IG : Nodes, Faces      =      1721      3444
AFLR2 IG : Nodes, Faces      =      1800      3602
AFLR2 IG : Nodes, Faces      =      1821      3644
AFLR2 IG : Nodes, Faces      =      1921      3844
AFLR2 IG : Nodes, Faces      =      2021      4044
AFLR2 IG : Nodes, Faces      =      2121      4244
AFLR2 IG : Nodes, Faces      =      2221      4444
AFLR2 IG : Nodes, Faces      =      2244      4490
AFLR2 IG : Nodes, Faces      =      2248      4490
AFLR2 IG : Nodes, Faces      =      2244      2244
 
AFLR2    : CPU Time          =     0.003   seconds
 
AFLR2 GG : FIELD GRID GENERATION
 
AFLR2 GG : Nodes, Faces      =      2244      2244
AFLR2 GG : Nodes, Faces      =      4284      6324
AFLR2 GG : Nodes, Faces      =      6145     10046
AFLR2 GG : Nodes, Faces      =      7886     13528
AFLR2 GG : Nodes, Faces      =      9454     16664
AFLR2 GG : Nodes, Faces      =     10741     19238
AFLR2 GG : Nodes, Faces      =     11943     21642
AFLR2 GG : Nodes, Faces      =     13066     23888
AFLR2 GG : Nodes, Faces      =     14097     25950
AFLR2 GG : Nodes, Faces      =     15067     27890
AFLR2 GG : Nodes, Faces      =     15974     29704
AFLR2 GG : Nodes, Faces      =     16822     31400
AFLR2 GG : Nodes, Faces      =     17616     32988
AFLR2 GG : Nodes, Faces      =     18347     34450
AFLR2 GG : Nodes, Faces      =     19005     35766
AFLR2 GG : Nodes, Faces      =     19620     36996
AFLR2 GG : Nodes, Faces      =     20189     38134
AFLR2 GG : Nodes, Faces      =     20718     39192
AFLR2 GG : Nodes, Faces      =     21211     40178
AFLR2 GG : Nodes, Faces      =     21668     41092
AFLR2 GG : Nodes, Faces      =     22096     41948
AFLR2 GG : Nodes, Faces      =     22480     42716
AFLR2 GG : Nodes, Faces      =     22835     43426
AFLR2 GG : Nodes, Faces      =     23135     44026
AFLR2 GG : Nodes, Faces      =     23375     44506
AFLR2 GG : Nodes, Faces      =     23584     44924
AFLR2 GG : Nodes, Faces      =     23776     45308
AFLR2 GG : Nodes, Faces      =     23937     45630
AFLR2 GG : Nodes, Faces      =     24040     45836
AFLR2 GG : Nodes, Faces      =     24141     46038
AFLR2 GG : Nodes, Faces      =     24236     46228
AFLR2 GG : Nodes, Faces      =     24313     46382
AFLR2 GG : Nodes, Faces      =     24371     46498
AFLR2 GG : Nodes, Faces      =     24418     46592
AFLR2 GG : Nodes, Faces      =     24438     46632
AFLR2 GG : Nodes, Faces      =     24445     46646
AFLR2 GG : Nodes, Faces      =     24446     46648
 
AFLR2    : CPU Time          =     0.033   seconds
 
AFLR2 QI : QUALITY IMPROVEMENT
 
AFLR2 QI : Nodes, Faces      =     24446     46648
 
AFLR2    : CPU Time          =     0.002   seconds
 
AFLR2    : DONE

Writing AFLR3 file ....
Finished writing AFLR3 file

Number of nodes = 24446
Number of elements = 48892
Number of tris = 46648
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      =       850      1702
AFLR2 IG : Nodes, Faces      =       851      1704
AFLR2 IG : Nodes, Faces      =       892      1786
AFLR2 IG : Nodes, Faces      =      1301      2604
AFLR2 IG : Nodes, Faces      =      1338      2678
AFLR2 IG : Nodes, Faces      =      1401      2804
AFLR2 IG : Nodes, Faces      =      1501      3004
AFLR2 IG : Nodes, Faces      =      1601      3204
AFLR2 IG : Nodes, Faces      =      1701      3404
AFLR2 IG : Nodes, Faces      =      1784      3570
AFLR2 IG : Nodes, Faces      =      1801      3604
AFLR2 IG : Nodes, Faces      =      1901      3804
AFLR2 IG : Nodes, Faces      =      2001      4004
AFLR2 IG : Nodes, Faces      =      2101      4204
AFLR2 IG : Nodes, Faces      =      2201      4404
AFLR2 IG : Nodes, Faces      =      2224      4450
AFLR2 IG : Nodes, Faces      =      2228      4450
AFLR2 IG : Nodes, Faces      =      2224      2224
 
AFLR2    : CPU Time          =     0.004   seconds
 
AFLR2 GG : FIELD GRID GENERATION
 
AFLR2 GG : Nodes, Faces      =      2224      2224
AFLR2 GG : Nodes, Faces      =      4125      6026
AFLR2 GG : Nodes, Faces      =      5678      9132
AFLR2 GG : Nodes, Faces      =      6935     11646
AFLR2 GG : Nodes, Faces      =      8014     13804
AFLR2 GG : Nodes, Faces      =      8951     15678
AFLR2 GG : Nodes, Faces      =      9771     17318
AFLR2 GG : Nodes, Faces      =     10475     18726
AFLR2 GG : Nodes, Faces      =     11059     19894
AFLR2 GG : Nodes, Faces      =     11570     20916
AFLR2 GG : Nodes, Faces      =     12009     21794
AFLR2 GG : Nodes, Faces      =     12391     22558
AFLR2 GG : Nodes, Faces      =     12726     23228
AFLR2 GG : Nodes, Faces      =     12997     23770
AFLR2 GG : Nodes, Faces      =     13221     24218
AFLR2 GG : Nodes, Faces      =     13414     24604
AFLR2 GG : Nodes, Faces      =     13547     24870
AFLR2 GG : Nodes, Faces      =     13643     25062
AFLR2 GG : Nodes, Faces      =     13711     25198
AFLR2 GG : Nodes, Faces      =     13758     25292
AFLR2 GG : Nodes, Faces      =     13790     25356
AFLR2 GG : Nodes, Faces      =     13806     25388
AFLR2 GG : Nodes, Faces      =     13809     25394
AFLR2 GG : Nodes, Faces      =     13810     25396
 
AFLR2    : CPU Time          =     0.018   seconds
 
AFLR2 QI : QUALITY IMPROVEMENT
 
AFLR2 QI : Nodes, Faces      =     13810     25396
 
AFLR2    : CPU Time          =     0.002   seconds
 
AFLR2    : DONE

Writing AFLR3 file ....
Finished writing AFLR3 file

Number of nodes = 13810
Number of elements = 27620
Number of tris = 25396
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 9.14.7
AFLR2    : Version Date   07/16/23 @ 01:42PM
AFLR2    : Compile OS     Darwin 22.6.0 arm64
AFLR2    : Compile Date   08/01/23 @ 11:39PM
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      =      1086      2174
AFLR2 IG : Nodes, Faces      =      1087      2176
AFLR2 IG : Nodes, Faces      =      1321      2644
AFLR2 IG : Nodes, Faces      =      1350      2702
AFLR2 IG : Nodes, Faces      =      1421      2844
AFLR2 IG : Nodes, Faces      =      1521      3044
AFLR2 IG : Nodes, Faces      =      1621      3244
AFLR2 IG : Nodes, Faces      =      1721      3444
AFLR2 IG : Nodes, Faces      =      1800      3602
AFLR2 IG : Nodes, Faces      =      1821      3644
AFLR2 IG : Nodes, Faces      =      1921      3844
AFLR2 IG : Nodes, Faces      =      2021      4044
AFLR2 IG : Nodes, Faces      =      2121      4244
AFLR2 IG : Nodes, Faces      =      2221      4444
AFLR2 IG : Nodes, Faces      =      2244      4490
AFLR2 IG : Nodes, Faces      =      2248      4490
AFLR2 IG : Nodes, Faces      =      2244      2244
 
AFLR2    : CPU Time          =     0.003   seconds
 
AFLR2 GG : FIELD GRID GENERATION
 
AFLR2 GG : Nodes, Faces      =      2244      2244
AFLR2 GG : Nodes, Faces      =      4284      6324
AFLR2 GG : Nodes, Faces      =      6145     10046
AFLR2 GG : Nodes, Faces      =      7886     13528
AFLR2 GG : Nodes, Faces      =      9454     16664
AFLR2 GG : Nodes, Faces      =     10741     19238
AFLR2 GG : Nodes, Faces      =     11943     21642
AFLR2 GG : Nodes, Faces      =     13066     23888
AFLR2 GG : Nodes, Faces      =     14097     25950
AFLR2 GG : Nodes, Faces      =     15067     27890
AFLR2 GG : Nodes, Faces      =     15974     29704
AFLR2 GG : Nodes, Faces      =     16822     31400
AFLR2 GG : Nodes, Faces      =     17616     32988
AFLR2 GG : Nodes, Faces      =     18347     34450
AFLR2 GG : Nodes, Faces      =     19005     35766
AFLR2 GG : Nodes, Faces      =     19620     36996
AFLR2 GG : Nodes, Faces      =     20189     38134
AFLR2 GG : Nodes, Faces      =     20718     39192
AFLR2 GG : Nodes, Faces      =     21211     40178
AFLR2 GG : Nodes, Faces      =     21668     41092
AFLR2 GG : Nodes, Faces      =     22096     41948
AFLR2 GG : Nodes, Faces      =     22480     42716
AFLR2 GG : Nodes, Faces      =     22835     43426
AFLR2 GG : Nodes, Faces      =     23135     44026
AFLR2 GG : Nodes, Faces      =     23375     44506
AFLR2 GG : Nodes, Faces      =     23584     44924
AFLR2 GG : Nodes, Faces      =     23776     45308
AFLR2 GG : Nodes, Faces      =     23937     45630
AFLR2 GG : Nodes, Faces      =     24040     45836
AFLR2 GG : Nodes, Faces      =     24141     46038
AFLR2 GG : Nodes, Faces      =     24236     46228
AFLR2 GG : Nodes, Faces      =     24313     46382
AFLR2 GG : Nodes, Faces      =     24371     46498
AFLR2 GG : Nodes, Faces      =     24418     46592
AFLR2 GG : Nodes, Faces      =     24438     46632
AFLR2 GG : Nodes, Faces      =     24445     46646
AFLR2 GG : Nodes, Faces      =     24446     46648
 
AFLR2    : CPU Time          =     0.033   seconds
 
AFLR2 QI : QUALITY IMPROVEMENT
 
AFLR2 QI : Nodes, Faces      =     24446     46648
 
AFLR2    : CPU Time          =     0.003   seconds
 
AFLR2    : DONE

Writing AFLR3 file ....
Finished writing AFLR3 file

Number of nodes = 24446
Number of elements = 48892
Number of tris = 46648
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 9.14.7
AFLR2    : Version Date   07/16/23 @ 01:42PM
AFLR2    : Compile OS     Darwin 22.6.0 arm64
AFLR2    : Compile Date   08/01/23 @ 11:39PM
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      =       850      1702
AFLR2 IG : Nodes, Faces      =       851      1704
AFLR2 IG : Nodes, Faces      =       892      1786
AFLR2 IG : Nodes, Faces      =      1301      2604
AFLR2 IG : Nodes, Faces      =      1338      2678
AFLR2 IG : Nodes, Faces      =      1401      2804
AFLR2 IG : Nodes, Faces      =      1501      3004
AFLR2 IG : Nodes, Faces      =      1601      3204
AFLR2 IG : Nodes, Faces      =      1701      3404
AFLR2 IG : Nodes, Faces      =      1784      3570
AFLR2 IG : Nodes, Faces      =      1801      3604
AFLR2 IG : Nodes, Faces      =      1901      3804
AFLR2 IG : Nodes, Faces      =      2001      4004
AFLR2 IG : Nodes, Faces      =      2101      4204
AFLR2 IG : Nodes, Faces      =      2201      4404
AFLR2 IG : Nodes, Faces      =      2224      4450
AFLR2 IG : Nodes, Faces      =      2228      4450
AFLR2 IG : Nodes, Faces      =      2224      2224
 
AFLR2    : CPU Time          =     0.004   seconds
 
AFLR2 GG : FIELD GRID GENERATION
 
AFLR2 GG : Nodes, Faces      =      2224      2224
AFLR2 GG : Nodes, Faces      =      4125      6026
AFLR2 GG : Nodes, Faces      =      5678      9132
AFLR2 GG : Nodes, Faces      =      6935     11646
AFLR2 GG : Nodes, Faces      =      8014     13804
AFLR2 GG : Nodes, Faces      =      8951     15678
AFLR2 GG : Nodes, Faces      =      9771     17318
AFLR2 GG : Nodes, Faces      =     10475     18726
AFLR2 GG : Nodes, Faces      =     11059     19894
AFLR2 GG : Nodes, Faces      =     11570     20916
AFLR2 GG : Nodes, Faces      =     12009     21794
AFLR2 GG : Nodes, Faces      =     12391     22558
AFLR2 GG : Nodes, Faces      =     12726     23228
AFLR2 GG : Nodes, Faces      =     12997     23770
AFLR2 GG : Nodes, Faces      =     13221     24218
AFLR2 GG : Nodes, Faces      =     13414     24604
AFLR2 GG : Nodes, Faces      =     13547     24870
AFLR2 GG : Nodes, Faces      =     13643     25062
AFLR2 GG : Nodes, Faces      =     13711     25198
AFLR2 GG : Nodes, Faces      =     13758     25292
AFLR2 GG : Nodes, Faces      =     13790     25356
AFLR2 GG : Nodes, Faces      =     13806     25388
AFLR2 GG : Nodes, Faces      =     13809     25394
AFLR2 GG : Nodes, Faces      =     13810     25396
 
AFLR2    : CPU Time          =     0.018   seconds
 
AFLR2 QI : QUALITY IMPROVEMENT
 
AFLR2 QI : Nodes, Faces      =     13810     25396
 
AFLR2    : CPU Time          =     0.001   seconds
 
AFLR2    : DONE

Writing AFLR3 file ....
Finished writing AFLR3 file

Number of nodes = 13810
Number of elements = 27620
Number of tris = 25396
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 9.14.7
AFLR2    : Version Date   07/16/23 @ 01:42PM
AFLR2    : Compile OS     Darwin 22.6.0 arm64
AFLR2    : Compile Date   08/01/23 @ 11:39PM
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      =      1086      2174
AFLR2 IG : Nodes, Faces      =      1087      2176
AFLR2 IG : Nodes, Faces      =      1321      2644
AFLR2 IG : Nodes, Faces      =      1350      2702
AFLR2 IG : Nodes, Faces      =      1421      2844
AFLR2 IG : Nodes, Faces      =      1521      3044
AFLR2 IG : Nodes, Faces      =      1621      3244
AFLR2 IG : Nodes, Faces      =      1721      3444
AFLR2 IG : Nodes, Faces      =      1800      3602
AFLR2 IG : Nodes, Faces      =      1821      3644
AFLR2 IG : Nodes, Faces      =      1921      3844
AFLR2 IG : Nodes, Faces      =      2021      4044
AFLR2 IG : Nodes, Faces      =      2121      4244
AFLR2 IG : Nodes, Faces      =      2221      4444
AFLR2 IG : Nodes, Faces      =      2244      4490
AFLR2 IG : Nodes, Faces      =      2248      4490
AFLR2 IG : Nodes, Faces      =      2244      2244
 
AFLR2    : CPU Time          =     0.003   seconds
 
AFLR2 GG : FIELD GRID GENERATION
 
AFLR2 GG : Nodes, Faces      =      2244      2244
AFLR2 GG : Nodes, Faces      =      4284      6324
AFLR2 GG : Nodes, Faces      =      6145     10046
AFLR2 GG : Nodes, Faces      =      7886     13528
AFLR2 GG : Nodes, Faces      =      9454     16664
AFLR2 GG : Nodes, Faces      =     10741     19238
AFLR2 GG : Nodes, Faces      =     11943     21642
AFLR2 GG : Nodes, Faces      =     13066     23888
AFLR2 GG : Nodes, Faces      =     14097     25950
AFLR2 GG : Nodes, Faces      =     15067     27890
AFLR2 GG : Nodes, Faces      =     15974     29704
AFLR2 GG : Nodes, Faces      =     16822     31400
AFLR2 GG : Nodes, Faces      =     17616     32988
AFLR2 GG : Nodes, Faces      =     18347     34450
AFLR2 GG : Nodes, Faces      =     19005     35766
AFLR2 GG : Nodes, Faces      =     19620     36996
AFLR2 GG : Nodes, Faces      =     20189     38134
AFLR2 GG : Nodes, Faces      =     20718     39192
AFLR2 GG : Nodes, Faces      =     21211     40178
AFLR2 GG : Nodes, Faces      =     21668     41092
AFLR2 GG : Nodes, Faces      =     22096     41948
AFLR2 GG : Nodes, Faces      =     22480     42716
AFLR2 GG : Nodes, Faces      =     22835     43426
AFLR2 GG : Nodes, Faces      =     23135     44026
AFLR2 GG : Nodes, Faces      =     23375     44506
AFLR2 GG : Nodes, Faces      =     23584     44924
AFLR2 GG : Nodes, Faces      =     23776     45308
AFLR2 GG : Nodes, Faces      =     23937     45630
AFLR2 GG : Nodes, Faces      =     24040     45836
AFLR2 GG : Nodes, Faces      =     24141     46038
AFLR2 GG : Nodes, Faces      =     24236     46228
AFLR2 GG : Nodes, Faces      =     24313     46382
AFLR2 GG : Nodes, Faces      =     24371     46498
AFLR2 GG : Nodes, Faces      =     24418     46592
AFLR2 GG : Nodes, Faces      =     24438     46632
AFLR2 GG : Nodes, Faces      =     24445     46646
AFLR2 GG : Nodes, Faces      =     24446     46648
 
AFLR2    : CPU Time          =     0.033   seconds
 
AFLR2 QI : QUALITY IMPROVEMENT
 
AFLR2 QI : Nodes, Faces      =     24446     46648
 
AFLR2    : CPU Time          =     0.003   seconds
 
AFLR2    : DONE

Writing AFLR3 file ....
Finished writing AFLR3 file

Number of nodes = 24446
Number of elements = 48892
Number of tris = 46648
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 9.14.7
AFLR2    : Version Date   07/16/23 @ 01:42PM
AFLR2    : Compile OS     Darwin 22.6.0 arm64
AFLR2    : Compile Date   08/01/23 @ 11:39PM
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      =        38        78
AFLR2 IG : Nodes, Faces      =        39        80
AFLR2 IG : Nodes, Faces      =        40        82
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      =       106       164
AFLR2 GG : Nodes, Faces      =       120       192
AFLR2 GG : Nodes, Faces      =       132       216
AFLR2 GG : Nodes, Faces      =       143       238
AFLR2 GG : Nodes, Faces      =       154       260
AFLR2 GG : Nodes, Faces      =       165       282
AFLR2 GG : Nodes, Faces      =       174       300
AFLR2 GG : Nodes, Faces      =       181       314
AFLR2 GG : Nodes, Faces      =       183       318
 
AFLR2    : CPU Time          =     0.000   seconds
 
AFLR2 QI : QUALITY IMPROVEMENT
 
AFLR2 QI : Nodes, Faces      =       183       318
 
AFLR2    : CPU Time          =     0.000   seconds
 
AFLR2    : DONE

Writing AFLR3 file ....
Finished writing AFLR3 file

Number of nodes = 183
Number of elements = 366
Number of tris = 318
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 9.14.7
AFLR2    : Version Date   07/16/23 @ 01:42PM
AFLR2    : Compile OS     Darwin 22.6.0 arm64
AFLR2    : Compile Date   08/01/23 @ 11:39PM
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 GG : Nodes, Faces      =       344       344
AFLR2 GG : Nodes, Faces      =       680      1016
AFLR2 GG : Nodes, Faces      =      1009      1674
AFLR2 GG : Nodes, Faces      =      1333      2322
AFLR2 GG : Nodes, Faces      =      1650      2956
AFLR2 GG : Nodes, Faces      =      1957      3570
AFLR2 GG : Nodes, Faces      =      2258      4172
AFLR2 GG : Nodes, Faces      =      2548      4752
AFLR2 GG : Nodes, Faces      =      2831      5318
AFLR2 GG : Nodes, Faces      =      3102      5860
AFLR2 GG : Nodes, Faces      =      3364      6384
AFLR2 GG : Nodes, Faces      =      3614      6884
AFLR2 GG : Nodes, Faces      =      3830      7316
AFLR2 GG : Nodes, Faces      =      4037      7730
AFLR2 GG : Nodes, Faces      =      4229      8114
AFLR2 GG : Nodes, Faces      =      4415      8486
AFLR2 GG : Nodes, Faces      =      4594      8844
AFLR2 GG : Nodes, Faces      =      4763      9182
AFLR2 GG : Nodes, Faces      =      4926      9508
AFLR2 GG : Nodes, Faces      =      5086      9828
AFLR2 GG : Nodes, Faces      =      5239     10134
AFLR2 GG : Nodes, Faces      =      5385     10426
AFLR2 GG : Nodes, Faces      =      5529     10714
AFLR2 GG : Nodes, Faces      =      5669     10994
AFLR2 GG : Nodes, Faces      =      5812     11280
AFLR2 GG : Nodes, Faces      =      5943     11542
AFLR2 GG : Nodes, Faces      =      6070     11796
AFLR2 GG : Nodes, Faces      =      6189     12034
AFLR2 GG : Nodes, Faces      =      6307     12270
AFLR2 GG : Nodes, Faces      =      6415     12486
AFLR2 GG : Nodes, Faces      =      6510     12676
AFLR2 GG : Nodes, Faces      =      6595     12846
AFLR2 GG : Nodes, Faces      =      6665     12986
AFLR2 GG : Nodes, Faces      =      6727     13110
AFLR2 GG : Nodes, Faces      =      6772     13200
AFLR2 GG : Nodes, Faces      =      6806     13268
AFLR2 GG : Nodes, Faces      =      6831     13318
AFLR2 GG : Nodes, Faces      =      6850     13356
AFLR2 GG : Nodes, Faces      =      6864     13384
AFLR2 GG : Nodes, Faces      =      6872     13400
AFLR2 GG : Nodes, Faces      =      6875     13406
AFLR2 GG : Nodes, Faces      =      6876     13408
 
AFLR2    : CPU Time          =     0.007   seconds
 
AFLR2 QI : QUALITY IMPROVEMENT
 
AFLR2 QI : Nodes, Faces      =      6876     13408
 
AFLR2    : CPU Time          =     0.001   seconds
 
AFLR2    : DONE

Writing AFLR3 file ....
Finished writing AFLR3 file

Number of nodes = 6876
Number of elements = 13752
Number of tris = 13408
Number of quad = 0

Writing TECPLOT file: pyCAPS_aflr2_Tri.dat ....
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      =       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

Writing TECPLOT file: pyCAPS_aflr2_Quad.dat ....
Finished writing TECPLOT file

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)!
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 9.14.7
AFLR2    : Version Date   07/16/23 @ 01:42PM
AFLR2    : Compile OS     Darwin 22.6.0 arm64
AFLR2    : Compile Date   08/01/23 @ 11:39PM
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

Writing TECPLOT file: pyCAPS_aflr2_Test.dat ....
Finished writing TECPLOT file

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)!
ok
test_Multiple_Mesh (test_aflr3.TestAFLR3.test_Multiple_Mesh) ... ERROR:: BAD STATUS = -276 from matsol (called from solveSketchOrig:61202)
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
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
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 9.14.7
AFLR2    : Version Date   07/16/23 @ 01:42PM
AFLR2    : Compile OS     Darwin 22.6.0 arm64
AFLR2    : Compile Date   08/01/23 @ 11:39PM
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 11.5.9
AFLR4    : Version Date   08/14/23 @ 12:27AM
AFLR4    : Compile OS     Darwin 22.6.0 arm64
AFLR4    : Compile Date   08/14/23 @ 12:31AM
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          = 1191
	Number of elements       = 6258
	Number of triangles      = 1332
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 4926
	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          = 6247
	Number of elements       = 34665
	Number of triangles      = 4438
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 30227
	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          = 13624
	Number of elements       = 76441
	Number of triangles      = 8142
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 68299
	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          = 42012
	Number of elements       = 238767
	Number of triangles      = 19898
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 218869
	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          = 4303
	Number of elements       = 23832
	Number of triangles      = 3020
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 20812
	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          = 11065
	Number of elements       = 61168
	Number of triangles      = 8630
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 52538
	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          = 10501
	Number of elements       = 58839
	Number of triangles      = 6368
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 52471
	Number of pyramids       = 0
	Number of prisms         = 0
	Number of hexahedrals    = 0

Writing AFLR3 file ....
Finished writing AFLR3 file


Writing AFLR3 file ....
Finished writing AFLR3 file


Writing AFLR3 file ....
Finished writing AFLR3 file


Writing AFLR3 file ....
Finished writing AFLR3 file


Writing AFLR3 file ....
Finished writing AFLR3 file


Writing AFLR3 file ....
Finished writing AFLR3 file


Writing AFLR3 file ....
Finished writing AFLR3 file

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          = 88943
	Number of elements       = 499970
	Number of triangles      = 51828
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 448142
	Number of pyramids       = 0
	Number of prisms         = 0
	Number of hexahedrals    = 0

Writing AFLR3 file ....
Finished writing AFLR3 file

ok
test_all (test_aflr3.TestAFLR3.test_all) ... ERROR:: BAD STATUS = -276 from matsol (called from solveSketchOrig:61202)
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
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
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 9.14.7
AFLR2    : Version Date   07/16/23 @ 01:42PM
AFLR2    : Compile OS     Darwin 22.6.0 arm64
AFLR2    : Compile Date   08/01/23 @ 11:39PM
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 11.5.9
AFLR4    : Version Date   08/14/23 @ 12:27AM
AFLR4    : Compile OS     Darwin 22.6.0 arm64
AFLR4    : Compile Date   08/14/23 @ 12:31AM
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          = 17719
	Number of elements       = 100939
	Number of triangles      = 8324
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 92615
	Number of pyramids       = 0
	Number of prisms         = 0
	Number of hexahedrals    = 0
No project name ("Proj_Name") provided - A volume mesh will not be written out
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          = 2560
	Number of elements       = 13640
	Number of triangles      = 2760
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 10880
	Number of pyramids       = 0
	Number of prisms         = 0
	Number of hexahedrals    = 0
No project name ("Proj_Name") provided - A volume mesh will not be written out
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          = 3643
	Number of elements       = 19753
	Number of triangles      = 3396
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 16357
	Number of pyramids       = 0
	Number of prisms         = 0
	Number of hexahedrals    = 0
No project name ("Proj_Name") provided - A volume mesh will not be written out
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          = 5497
	Number of elements       = 30553
	Number of triangles      = 3658
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 26895
	Number of pyramids       = 0
	Number of prisms         = 0
	Number of hexahedrals    = 0
No project name ("Proj_Name") provided - A volume mesh will not be written out
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          = 4709
	Number of elements       = 26067
	Number of triangles      = 3328
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 22739
	Number of pyramids       = 0
	Number of prisms         = 0
	Number of hexahedrals    = 0
No project name ("Proj_Name") provided - A volume mesh will not be written out
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          = 5505
	Number of elements       = 30555
	Number of triangles      = 3758
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 26797
	Number of pyramids       = 0
	Number of prisms         = 0
	Number of hexahedrals    = 0
No project name ("Proj_Name") provided - A volume mesh will not be written out
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          = 2258
	Number of elements       = 12120
	Number of triangles      = 2220
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 9900
	Number of pyramids       = 0
	Number of prisms         = 0
	Number of hexahedrals    = 0
No project name ("Proj_Name") provided - A volume mesh will not be written out
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          = 3320
	Number of elements       = 17943
	Number of triangles      = 3108
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 14835
	Number of pyramids       = 0
	Number of prisms         = 0
	Number of hexahedrals    = 0
No project name ("Proj_Name") provided - A volume mesh will not be written out
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          = 4387
	Number of elements       = 23813
	Number of triangles      = 3994
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 19819
	Number of pyramids       = 0
	Number of prisms         = 0
	Number of hexahedrals    = 0
No project name ("Proj_Name") provided - A volume mesh will not be written out
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          = 5459
	Number of elements       = 29714
	Number of triangles      = 4882
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 24832
	Number of pyramids       = 0
	Number of prisms         = 0
	Number of hexahedrals    = 0
No project name ("Proj_Name") provided - A volume mesh will not be written out
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          = 6538
	Number of elements       = 35638
	Number of triangles      = 5772
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 29866
	Number of pyramids       = 0
	Number of prisms         = 0
	Number of hexahedrals    = 0
No project name ("Proj_Name") provided - A volume mesh will not be written out
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          = 7610
	Number of elements       = 41543
	Number of triangles      = 6662
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 34881
	Number of pyramids       = 0
	Number of prisms         = 0
	Number of hexahedrals    = 0
No project name ("Proj_Name") provided - A volume mesh will not be written out
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          = 19842
	Number of elements       = 110111
	Number of triangles      = 15544
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 94567
	Number of pyramids       = 0
	Number of prisms         = 0
	Number of hexahedrals    = 0
No project name ("Proj_Name") provided - A volume mesh will not be written out
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          = 29703
	Number of elements       = 171754
	Number of triangles      = 7670
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 164084
	Number of pyramids       = 0
	Number of prisms         = 0
	Number of hexahedrals    = 0
No project name ("Proj_Name") provided - A volume mesh will not be written out
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          = 22531
	Number of elements       = 130381
	Number of triangles      = 6118
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 124263
	Number of pyramids       = 0
	Number of prisms         = 0
	Number of hexahedrals    = 0
No project name ("Proj_Name") provided - A volume mesh will not be written out
 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          = 29703
	Number of elements       = 171754
	Number of triangles      = 7670
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 164084
	Number of pyramids       = 0
	Number of prisms         = 0
	Number of hexahedrals    = 0
No project name ("Proj_Name") provided - A volume mesh will not be written out
 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          = 22531
	Number of elements       = 130381
	Number of triangles      = 6118
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 124263
	Number of pyramids       = 0
	Number of prisms         = 0
	Number of hexahedrals    = 0
No project name ("Proj_Name") provided - A volume mesh will not be written out
 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          = 29703
	Number of elements       = 171754
	Number of triangles      = 7670
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 164084
	Number of pyramids       = 0
	Number of prisms         = 0
	Number of hexahedrals    = 0

Writing TECPLOT file: test.dat ....
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          = 22531
	Number of elements       = 130381
	Number of triangles      = 6118
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 124263
	Number of pyramids       = 0
	Number of prisms         = 0
	Number of hexahedrals    = 0

Writing TECPLOT file: test.dat ....
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          = 29703
	Number of elements       = 171754
	Number of triangles      = 7670
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 164084
	Number of pyramids       = 0
	Number of prisms         = 0
	Number of hexahedrals    = 0

Writing TECPLOT file: test.dat ....
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          = 22531
	Number of elements       = 130381
	Number of triangles      = 6118
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 124263
	Number of pyramids       = 0
	Number of prisms         = 0
	Number of hexahedrals    = 0

Writing TECPLOT file: test.dat ....
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          = 4983
	Number of elements       = 27605
	Number of triangles      = 3464
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 24141
	Number of pyramids       = 0
	Number of prisms         = 0
	Number of hexahedrals    = 0
No project name ("Proj_Name") provided - A volume mesh will not be written out
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
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
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          = 6477
	Number of elements       = 36245
	Number of triangles      = 4050
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 32195
	Number of pyramids       = 0
	Number of prisms         = 0
	Number of hexahedrals    = 0
No project name ("Proj_Name") provided - A volume mesh will not be written out
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
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to 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
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          = 40466
	Number of elements       = 233749
	Number of triangles      = 12424
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 221325
	Number of pyramids       = 0
	Number of prisms         = 0
	Number of hexahedrals    = 0

Writing TECPLOT file: test.dat ....
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          = 44743
	Number of elements       = 259184
	Number of triangles      = 12406
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 246778
	Number of pyramids       = 0
	Number of prisms         = 0
	Number of hexahedrals    = 0

Writing TECPLOT file: test.dat ....
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          = 40466
	Number of elements       = 233731
	Number of triangles      = 12406
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 221325
	Number of pyramids       = 0
	Number of prisms         = 0
	Number of hexahedrals    = 0

Writing TECPLOT file: test.dat ....
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
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to 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 1 of face 1, unable to 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
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:61202)
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
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
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 capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = wall, index = 1
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 capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = wall, index = 1
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 capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = wall, index = 1
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
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:61202)
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:61202)
ERROR:: BAD STATUS = -276 from matsol (called from solveSketchOrig:61202)
 CAPS Info: Hit last success -- going live!
ERROR:: BAD STATUS = -276 from matsol (called from solveSketchOrig:61202)
 CAPS Info: Hit last success -- going live!
ERROR:: BAD STATUS = -276 from matsol (called from solveSketchOrig:61202)
 CAPS Info: Hit last success -- going live!
ERROR:: BAD STATUS = -276 from matsol (called from solveSketchOrig:61202)
 CAPS Info: Hit last success -- going live!
ERROR:: BAD STATUS = -276 from matsol (called from solveSketchOrig:61202)
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:61202)
 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:61202)
 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:61202)
 CAPS Info: Hit last success -- going live!
ERROR:: BAD STATUS = -276 from matsol (called from solveSketchOrig:61202)
 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:61202)
 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:61202)
ok
test_phase (test_aflr4.TestAFLR4.test_phase) ... ERROR:: BAD STATUS = -276 from matsol (called from solveSketchOrig:61202)
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:61202)
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
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
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
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 = 1
Number of node elements          = 1
Number of line 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 node elements          = 0
Number of line elements          = 0
Number of triangle elements      = 0
Number of quadrilateral elements = 44
----------------------------
Total number of nodes    = 47
Total number of elements = 45
Mapping Csys attributes ................
	Number of unique Csys attributes = 0

Getting FEA 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)
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to 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
Body 1 (of 1)
Number of nodes    = 25
Number of elements = 16
Number of node elements          = 0
Number of line elements          = 0
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
   (16:59:51) Running aero.csh on 2 core(s) in M0.5A1B0_DP1
   (16:59:52) aero.csh done
 o case M0.5A1B0_DP1, averaging data over 1 cycle(s)
 o Evaluating Cart3D functionals and/or gradients
   ATTENTION: using static geometry ../inputs/Components.i.tri
   (16:59:53) Running aero.csh on 2 core(s) in M0.5A1B0_DP1
   (16:59:54) aero.csh done
              Max memory allowed:       32 GB
              Flow hexes:               8744
              Estimated cutter memory:  0.000874 GB / DV
              Estimated xsensit memory: 0.016614 GB / DV
              Available threads:        2
              # DVs:                    1
   o Number of simultaneous cutter jobs:   1
   (16:59:55) Linearizing cut-cells
   (16:59:55) ... done
   o Number of simultaneous xsensit jobs:  1
   (16:59:55) Computing gradients
   (17:00:03) ... done
 o case M0.5A1B0_DP1, averaging data over 1 cycle(s)
 o Evaluating Cart3D functionals and/or gradients
   ATTENTION: using static geometry ../inputs/Components.i.tri
   (17:00:03) Running aero.csh on 2 core(s) in M0.5A1B0_DP1
   (17:00:04) 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
   (17:00:05) Running aero.csh on 2 core(s) in M0.5A1B0_DP1
   (17:00:06) aero.csh done
 o case M0.5A1B0_DP1, averaging data over 1 cycle(s)
 o Evaluating Cart3D functionals and/or gradients
   ATTENTION: using static geometry ../inputs/Components.i.tri
   (17:00:06) Running aero.csh on 2 core(s) in M0.5A1B0_DP1
   (17:00:08) 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
   (17:00:08) Linearizing cut-cells
   (17:00:08) ... done
   o Number of simultaneous xsensit jobs:  1
   (17:00:08) Computing gradients
   (17:00:16) ... 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
   (17:00:17) Running aero.csh on 2 core(s) in M0.5A1B0_DP1
   (17:00:18) 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
   (17:00:18) Running aero.csh on 2 core(s) in M0.5A1B0_DP1
   (17:00:19) 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
   (17:00:20) Running aero.csh on 2 core(s) in M0.5A1B0_DP1
   (17:00:20) 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
   (17:00:21) Linearizing cut-cells
   (17:00:21) ... done
   o Number of simultaneous xsensit jobs:  1
   (17:00:21) Computing gradients
   (17:00:25) ... 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
   (17:00:25) Running aero.csh on 2 core(s) in M0.5A1B0_DP1
   (17:00:26) 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
   (17:00:27) Running aero.csh on 2 core(s) in M0.5A1B0_DP1
   (17:00:28) 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
   (17:00:28) Running aero.csh on 2 core(s) in M0.5A1B0_DP1
   (17:00:29) 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
   (17:00:29) Linearizing cut-cells
   (17:00:29) ... done
   o Number of simultaneous xsensit jobs:  1
   (17:00:29) Computing gradients
   (17:00:33) ... 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
   (17:00:34) Running aero.csh on 2 core(s) in M0.5A1B0_DP1
   (17:00:35) 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
   (17:00:35) Running aero.csh on 2 core(s) in M0.5A1B0_DP1
   (17:00:36) 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
   (17:00:37) Running aero.csh on 2 core(s) in M0.5A1B0_DP1
   (17:00:37) 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
   (17:00:38) Linearizing cut-cells
   (17:00:38) ... done
   o Number of simultaneous xsensit jobs:  1
   (17:00:38) Computing gradients
   (17:00:42) ... 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
   (17:00:42) Running aero.csh on 2 core(s) in M0.5A1B0_DP1
   (17:00:43) 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
   (17:00:44) Running aero.csh on 2 core(s) in M0.5A1B0_DP1
   (17:00:45) 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
   (17:00:45) Running aero.csh on 2 core(s) in M0.5A1B0_DP1
   (17:00:46) 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
   (17:00:46) Linearizing cut-cells
   (17:00:46) ... done
   o Number of simultaneous xsensit jobs:  1
   (17:00:46) Computing gradients
   (17:00:50) ... 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
   (17:00:51) Running aero.csh on 2 core(s) in M0.5A1B0_DP1
   (17:00:52) 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
   (17:00:52) Running aero.csh on 2 core(s) in M0.5A1B0_DP1
   (17:00:53) 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
   (17:00:54) Running aero.csh on 2 core(s) in M0.5A1B0_DP1
   (17:00:54) aero.csh done
              Max memory allowed:       32 GB
              Flow hexes:               8744
              Estimated cutter memory:  0.000874 GB / DV
              Estimated xsensit memory: 0.016614 GB / DV
              Available threads:        2
              # DVs:                    1
   o Number of simultaneous cutter jobs:   1
   (17:00:55) Linearizing cut-cells
   (17:00:55) ... done
   o Number of simultaneous xsensit jobs:  1
   (17:00:55) Computing gradients
   (17:00:59) ... 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
   (17:00:59) Running aero.csh on 2 core(s) in M0.5A1B0_DP1
   (17:01:00) 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
   (17:01:01) Running aero.csh on 2 core(s) in M0.5A1B0_DP1
   (17:01:02) 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
   (17:01:02) Running aero.csh on 2 core(s) in M0.5A1B0_DP1
   (17:01:03) 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
   (17:01:03) Linearizing cut-cells
   (17:01:03) ... done
   o Number of simultaneous xsensit jobs:  1
   (17:01:03) Computing gradients
   (17:01:07) ... 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
   (17:01:08) Running aero.csh on 2 core(s) in M0.5A1B0_DP1
   (17:01:09) 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
   (17:01:10) Running aero.csh on 2 core(s) in M0.5A1B0_DP1
   (17:01:11) 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
   (17:01:11) Running aero.csh on 2 core(s) in M0.5A1B0_DP1
   (17:01:13) 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
   (17:01:13) Linearizing cut-cells
   (17:01:15) ... done
   o Number of simultaneous xsensit jobs:  2
   (17:01:15) Computing gradients
              Adjusted OMP_NUM_THREADS to 1 for xsensit
   (17:01:23) ... 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
   (17:01:24) Running aero.csh on 2 core(s) in M0.5A1B0_DP1
   (17:01:25) 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
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to 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
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:61202)
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!
 1717DB000 EGADS Info: Face #5 -> Edge #17 (9) Internally in Loop 7 4, sen = -1!
 1717DB000 EGADS Info: Face #5 -> Edge #17 (9) Internally in Loop 4 7, sen = 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
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
 1717DB000 EGADS Info: Face #3 -> Edge #9 (9) Internally in Loop 4 7, sen = -1!
 1717DB000 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_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:61202)
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:61202)
ERROR:: BAD STATUS = -276 from matsol (called from solveSketchOrig:61202)
 CAPS Info: Hit last success -- going live!
ERROR:: BAD STATUS = -276 from matsol (called from solveSketchOrig:61202)
 CAPS Info: Hit last success -- going live!
ERROR:: BAD STATUS = -276 from matsol (called from solveSketchOrig:61202)
 CAPS Info: Hit last success -- going live!
ERROR:: BAD STATUS = -276 from matsol (called from solveSketchOrig:61202)
 CAPS Info: Hit last success -- going live!
ERROR:: BAD STATUS = -276 from matsol (called from solveSketchOrig:61202)
 CAPS Info: Hit last success -- going live!
ERROR:: BAD STATUS = -276 from matsol (called from solveSketchOrig:61202)
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:61202)
 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:61202)
 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:61202)
 CAPS Info: Hit last success -- going live!
ERROR:: BAD STATUS = -276 from matsol (called from solveSketchOrig:61202)
 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:61202)
 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:61202)
 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:61202)
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:61202)
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:61202)
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
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_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
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
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    = 7802
Number of elements = 15600
Number of node elements          = 0
Number of line elements          = 0
Number of triangle elements      = 15600
Number of quadrilateral elements = 0
Body 2 (of 3)
Number of nodes    = 5906
Number of elements = 11808
Number of node elements          = 0
Number of line elements          = 0
Number of triangle elements      = 11808
Number of quadrilateral elements = 0
Body 3 (of 3)
Number of nodes    = 545
Number of elements = 1086
Number of node elements          = 0
Number of line elements          = 0
Number of triangle elements      = 1086
Number of quadrilateral elements = 0
----------------------------
Total number of nodes    = 14253
Total number of elements = 28494
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 - 14253, elements - 28494
Getting volume mesh

Generating volume mesh using TetGen.....

Tetgen input string = pYq1.500/0.000T1.00e-16A
Delaunizing vertices...
Delaunay seconds:  0.084979
Creating surface mesh ...
Surface mesh seconds:  0.011234
Recovering boundaries...
Boundary recovery seconds:  0.049414
Removing exterior tetrahedra ...
Spreading region attributes.
Exterior tets removal seconds:  0.016706
Recovering Delaunayness...
Delaunay recovery seconds:  0.030604
Refining mesh...
  18999 insertions, added 13806 points, 712098 tetrahedra in queue.
  6326 insertions, added 2564 points, 586841 tetrahedra in queue.
  8433 insertions, added 1779 points, 64950 tetrahedra in queue.
Refinement seconds:  0.963638
Smoothing vertices...
Mesh smoothing seconds:  0.810195
Improving mesh...
Mesh improvement seconds:  0.022766

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

Output seconds:  0.00389
Total running seconds:  1.99368

Statistics:

  Input points: 14253
  Input facets: 28494
  Input segments: 42741
  Input holes: 2
  Input regions: 0

  Mesh points: 33071
  Mesh tetrahedra: 159280
  Mesh faces: 332807
  Mesh faces on exterior boundary: 28494
  Mesh faces on input facets: 28494
  Mesh edges on input segments: 42741
  Steiner points inside domain: 18818

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    = 7802
Number of elements = 15600
Number of node elements          = 0
Number of line elements          = 0
Number of triangle elements      = 15600
Number of quadrilateral elements = 0
Body 2 (of 3)
Number of nodes    = 5906
Number of elements = 11808
Number of node elements          = 0
Number of line elements          = 0
Number of triangle elements      = 11808
Number of quadrilateral elements = 0
Body 3 (of 3)
Number of nodes    = 545
Number of elements = 1086
Number of node elements          = 0
Number of line elements          = 0
Number of triangle elements      = 1086
Number of quadrilateral elements = 0
----------------------------
Total number of nodes    = 14253
Total number of elements = 28494
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 - 14253, elements - 28494
Getting volume mesh

Generating volume mesh using TetGen.....

Tetgen input string = pYq1.500/0.000T1.00e-16A
Delaunizing vertices...
Delaunay seconds:  0.085286
Creating surface mesh ...
Surface mesh seconds:  0.011465
Recovering boundaries...
Boundary recovery seconds:  0.04969
Removing exterior tetrahedra ...
Spreading region attributes.
Exterior tets removal seconds:  0.016693
Recovering Delaunayness...
Delaunay recovery seconds:  0.030549
Refining mesh...
  18999 insertions, added 13806 points, 712098 tetrahedra in queue.
  6326 insertions, added 2564 points, 586841 tetrahedra in queue.
  8433 insertions, added 1779 points, 64950 tetrahedra in queue.
Refinement seconds:  0.959758
Smoothing vertices...
Mesh smoothing seconds:  0.812706
Improving mesh...
Mesh improvement seconds:  0.023077

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

Output seconds:  0.003929
Total running seconds:  1.99344

Statistics:

  Input points: 14253
  Input facets: 28494
  Input segments: 42741
  Input holes: 2
  Input regions: 0

  Mesh points: 33071
  Mesh tetrahedra: 159280
  Mesh faces: 332807
  Mesh faces on exterior boundary: 28494
  Mesh faces on input facets: 28494
  Mesh edges on input segments: 42741
  Steiner points inside domain: 18818

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 - 5100, elements - 10188
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 - 5100, elements - 10188
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 - 14253, elements - 28494
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_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 9.14.7
AFLR2    : Version Date   07/16/23 @ 01:42PM
AFLR2    : Compile OS     Darwin 22.6.0 arm64
AFLR2    : Compile Date   08/01/23 @ 11:39PM
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 11.5.9
AFLR4    : Version Date   08/14/23 @ 12:27AM
AFLR4    : Compile OS     Darwin 22.6.0 arm64
AFLR4    : Compile Date   08/14/23 @ 12:31AM
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          = 1017
	Number of elements       = 5484
	Number of triangles      = 918
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 4566
	Number of pyramids       = 0
	Number of prisms         = 0
	Number of hexahedrals    = 0
No project name ("Proj_Name") provided - A volume mesh will not be written out
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          = 320
	Number of elements       = 1559
	Number of triangles      = 496
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 1063
	Number of pyramids       = 0
	Number of prisms         = 0
	Number of hexahedrals    = 0
No project name ("Proj_Name") provided - A volume mesh will not be written out
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          = 951
	Number of elements       = 5079
	Number of triangles      = 874
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 4205
	Number of pyramids       = 0
	Number of prisms         = 0
	Number of hexahedrals    = 0
No project name ("Proj_Name") provided - A volume mesh will not be written out
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          = 17432
	Number of elements       = 100418
	Number of triangles      = 5240
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 95178
	Number of pyramids       = 0
	Number of prisms         = 0
	Number of hexahedrals    = 0
No project name ("Proj_Name") provided - A volume mesh will not be written out

Writing SU2 file ....
Finished writing SU2 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 (8.0.0) "

Writing SU2 file ....
Finished writing SU2 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 (8.0.0) "

Writing SU2 file ....
Finished writing SU2 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 (8.0.0) "
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          = 1017
	Number of elements       = 5484
	Number of triangles      = 918
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 4566
	Number of pyramids       = 0
	Number of prisms         = 0
	Number of hexahedrals    = 0
No project name ("Proj_Name") provided - A volume mesh will not be written out
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          = 393
	Number of elements       = 1929
	Number of triangles      = 612
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 1317
	Number of pyramids       = 0
	Number of prisms         = 0
	Number of hexahedrals    = 0
No project name ("Proj_Name") provided - A volume mesh will not be written out
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          = 304
	Number of elements       = 1461
	Number of triangles      = 468
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 993
	Number of pyramids       = 0
	Number of prisms         = 0
	Number of hexahedrals    = 0
No project name ("Proj_Name") provided - A volume mesh will not be written out
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 9.14.7
AFLR2    : Version Date   07/16/23 @ 01:42PM
AFLR2    : Compile OS     Darwin 22.6.0 arm64
AFLR2    : Compile Date   08/01/23 @ 11:39PM
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 11.5.9
AFLR4    : Version Date   08/14/23 @ 12:27AM
AFLR4    : Compile OS     Darwin 22.6.0 arm64
AFLR4    : Compile Date   08/14/23 @ 12:31AM
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 Sense   Edges
EGADS    :      1     Yes     1   1 4 -3 -2
EGADS    :      2     Yes     1   3 7 -6 -5
EGADS    :      3     Yes     1   6 9 -1 -8
EGADS    :      4     Yes     1   -4 -9 -7
EGADS    :      5     Yes     1   -10 2 11 -12
EGADS    :      6     Yes     1   -11 5 13 -14
EGADS    :      7     Yes     1   -13 8 10 -15
EGADS    :      8     Yes     1   12 14 15
EGADS    :      9     Yes     1   16 19 -18 -17
EGADS    :     10     Yes     1   18 22 -21 -20
EGADS    :     11     Yes     1   21 24 -16 -23
EGADS    :     12     Yes     1   -19 -24 -22
EGADS    :     13     Yes     1   -25 17 26 -27
EGADS    :     14     Yes     1   -26 20 28 -29
EGADS    :     15     Yes     1   -28 23 25 -30
EGADS    :     16     Yes     1   27 29 30
EGADS    :     17     Yes     1   -31 -32 33 34
EGADS    :     18     Yes     1   -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=     12406
AFLR43   : Nodes             =      6209
 
 
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 16.32.49
AFLR3    : Version Date   07/26/23 @ 12:32AM
AFLR3    : Compile OS     Darwin 22.6.0 arm64
AFLR3    : Compile Date   08/01/23 @ 11:39PM
AFLR3    : Copyright 1994-2021, D.L. Marcum
AFLR3    : ---------------------------------------
 
AFLR3 IC : INPUT SURFACE GRID CHECK
 
AFLR3 IC : Nodes, Elements   =      6209         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          =     0.008   seconds
 
AFLR3 IG : INITIAL VOLUME GRID GENERATION
 
AFLR3 IG : Nodes, Elements   =      6209         0
AFLR3 IG : Nodes, Elements   =         8        10
AFLR3 IG : Nodes, Elements   =      1244      7682
AFLR3 IG : Nodes, Elements   =      2488     16247
AFLR3 IG : Nodes, Elements   =      3732     24929
AFLR3 IG : Nodes, Elements   =      4976     33969
AFLR3 IG : Nodes, Elements   =      6216     42984
AFLR3 IG : Nodes, Elements   =      6216     42922
AFLR3 IG : Nodes, Elements   =      6216     42927
AFLR3 IG : Nodes, Elements   =      6216     42922
AFLR3 IG : Nodes, Elements   =      6216     42927
AFLR3 IG : Nodes, Elements   =      6216     42920
AFLR3 IG : Nodes, Elements   =      6216     42921
AFLR3 IG : Nodes, Elements   =      6209     25546
AFLR3 IG : Nodes, Elements   =      6209     25566
AFLR3 IG : Nodes, Elements   =      6209     20496
AFLR3 IG : Nodes, Elements   =      6209     18359
 
AFLR3    : CPU Time          =     0.105   seconds
 
AFLR3 GG : ISOTROPIC VOLUME GRID GENERATION
 
AFLR3 GG : Nodes, Elements   =      6209     18359
AFLR3 GG : Nodes, Elements   =      9074     27175
AFLR3 GG : Nodes, Elements   =      9074     39170
AFLR3 GG : Nodes, Elements   =      9074     36224
AFLR3 GG : Nodes, Elements   =      9074     34723
AFLR3 GG : Nodes, Elements   =     11644     42749
AFLR3 GG : Nodes, Elements   =     11644     54099
AFLR3 GG : Nodes, Elements   =     11644     50812
AFLR3 GG : Nodes, Elements   =     11644     49921
AFLR3 GG : Nodes, Elements   =     14441     58599
AFLR3 GG : Nodes, Elements   =     14441     70844
AFLR3 GG : Nodes, Elements   =     14441     67333
AFLR3 GG : Nodes, Elements   =     14441     66422
AFLR3 GG : Nodes, Elements   =     17481     75734
AFLR3 GG : Nodes, Elements   =     17481     88956
AFLR3 GG : Nodes, Elements   =     17481     85215
AFLR3 GG : Nodes, Elements   =     17481     84368
AFLR3 GG : Nodes, Elements   =     20614     93923
AFLR3 GG : Nodes, Elements   =     20614    107375
AFLR3 GG : Nodes, Elements   =     20614    103694
AFLR3 GG : Nodes, Elements   =     20614    102890
AFLR3 GG : Nodes, Elements   =     23924    112944
AFLR3 GG : Nodes, Elements   =     23924    127128
AFLR3 GG : Nodes, Elements   =     23924    123349
AFLR3 GG : Nodes, Elements   =     23924    122508
AFLR3 GG : Nodes, Elements   =     27322    132858
AFLR3 GG : Nodes, Elements   =     27322    147287
AFLR3 GG : Nodes, Elements   =     27322    143409
AFLR3 GG : Nodes, Elements   =     27322    142563
AFLR3 GG : Nodes, Elements   =     30785    153086
AFLR3 GG : Nodes, Elements   =     30785    167947
AFLR3 GG : Nodes, Elements   =     30785    163988
AFLR3 GG : Nodes, Elements   =     30785    163155
AFLR3 GG : Nodes, Elements   =     34330    173904
AFLR3 GG : Nodes, Elements   =     34330    188899
AFLR3 GG : Nodes, Elements   =     34330    184950
AFLR3 GG : Nodes, Elements   =     34330    184198
AFLR3 GG : Nodes, Elements   =     37875    194909
AFLR3 GG : Nodes, Elements   =     37875    209837
AFLR3 GG : Nodes, Elements   =     37875    205939
AFLR3 GG : Nodes, Elements   =     37875    205185
AFLR3 GG : Nodes, Elements   =     41383    215750
AFLR3 GG : Nodes, Elements   =     41383    230824
AFLR3 GG : Nodes, Elements   =     41383    226838
AFLR3 GG : Nodes, Elements   =     41383    226055
AFLR3 GG : Nodes, Elements   =     44758    236221
AFLR3 GG : Nodes, Elements   =     44758    250507
AFLR3 GG : Nodes, Elements   =     44758    246858
AFLR3 GG : Nodes, Elements   =     44758    246174
AFLR3 GG : Nodes, Elements   =     47993    255921
AFLR3 GG : Nodes, Elements   =     47993    269685
AFLR3 GG : Nodes, Elements   =     47993    266082
AFLR3 GG : Nodes, Elements   =     47993    265470
AFLR3 GG : Nodes, Elements   =     51138    274926
AFLR3 GG : Nodes, Elements   =     51138    288260
AFLR3 GG : Nodes, Elements   =     51138    284900
AFLR3 GG : Nodes, Elements   =     51138    284259
AFLR3 GG : Nodes, Elements   =     54127    293245
AFLR3 GG : Nodes, Elements   =     54127    305708
AFLR3 GG : Nodes, Elements   =     54127    302622
AFLR3 GG : Nodes, Elements   =     54127    302089
AFLR3 GG : Nodes, Elements   =     56876    310344
AFLR3 GG : Nodes, Elements   =     56876    321960
AFLR3 GG : Nodes, Elements   =     56876    319008
AFLR3 GG : Nodes, Elements   =     56876    318534
AFLR3 GG : Nodes, Elements   =     59490    326385
AFLR3 GG : Nodes, Elements   =     59490    337219
AFLR3 GG : Nodes, Elements   =     59490    334507
AFLR3 GG : Nodes, Elements   =     59490    334143
AFLR3 GG : Nodes, Elements   =     61763    340968
AFLR3 GG : Nodes, Elements   =     61763    350625
AFLR3 GG : Nodes, Elements   =     61763    348113
AFLR3 GG : Nodes, Elements   =     61763    347806
AFLR3 GG : Nodes, Elements   =     63781    353860
AFLR3 GG : Nodes, Elements   =     63781    362343
AFLR3 GG : Nodes, Elements   =     63781    360110
AFLR3 GG : Nodes, Elements   =     63781    359835
AFLR3 GG : Nodes, Elements   =     65434    364796
AFLR3 GG : Nodes, Elements   =     65434    371861
AFLR3 GG : Nodes, Elements   =     65434    369981
AFLR3 GG : Nodes, Elements   =     65434    369781
AFLR3 GG : Nodes, Elements   =     66679    373516
AFLR3 GG : Nodes, Elements   =     66679    378838
AFLR3 GG : Nodes, Elements   =     66679    377349
AFLR3 GG : Nodes, Elements   =     66679    377207
AFLR3 GG : Nodes, Elements   =     67556    379838
AFLR3 GG : Nodes, Elements   =     67556    383674
AFLR3 GG : Nodes, Elements   =     67556    382612
AFLR3 GG : Nodes, Elements   =     67556    382516
AFLR3 GG : Nodes, Elements   =     68132    384245
AFLR3 GG : Nodes, Elements   =     68132    386717
AFLR3 GG : Nodes, Elements   =     68132    386001
AFLR3 GG : Nodes, Elements   =     68132    385950
AFLR3 GG : Nodes, Elements   =     68454    386917
AFLR3 GG : Nodes, Elements   =     68454    388272
AFLR3 GG : Nodes, Elements   =     68454    387885
AFLR3 GG : Nodes, Elements   =     68454    387856
AFLR3 GG : Nodes, Elements   =     68603    388303
AFLR3 GG : Nodes, Elements   =     68603    388994
AFLR3 GG : Nodes, Elements   =     68603    388755
AFLR3 GG : Nodes, Elements   =     68603    388747
AFLR3 GG : Nodes, Elements   =     68663    388927
AFLR3 GG : Nodes, Elements   =     68663    389173
AFLR3 GG : Nodes, Elements   =     68663    389089
AFLR3 GG : Nodes, Elements   =     68663    389081
AFLR3 GG : Nodes, Elements   =     68678    389127
AFLR3 GG : Nodes, Elements   =     68678    389189
AFLR3 GG : Nodes, Elements   =     68678    389164
AFLR3 GG : Nodes, Elements   =     68678    389168
AFLR3 GG : Nodes, Elements   =     68680    389174
AFLR3 GG : Nodes, Elements   =     68680    389185
AFLR3 GG : Nodes, Elements   =     68680    389182
AFLR3 GG : Nodes, Elements   =     68701    389245
AFLR3 GG : Nodes, Elements   =     68701    389327
AFLR3 GG : Nodes, Elements   =     68701    389297
AFLR3 GG : Nodes, Elements   =     68701    389298
AFLR3 GG : Nodes, Elements   =     68710    389325
AFLR3 GG : Nodes, Elements   =     68710    389355
AFLR3 GG : Nodes, Elements   =     68710    389347
AFLR3 GG : Nodes, Elements   =     68715    389362
AFLR3 GG : Nodes, Elements   =     68715    389378
AFLR3 GG : Nodes, Elements   =     68715    389373
AFLR3 GG : Nodes, Elements   =     68715    389374
AFLR3 GG : Nodes, Elements   =     68716    389377
AFLR3 GG : Nodes, Elements   =     68716    389381
AFLR3 GG : Nodes, Elements   =     68716    389380
 
AFLR3    : CPU Time          =     1.856   seconds
 
AFLR3 QI : QUALITY IMPROVEMENT
 
AFLR3 QI : Nodes, Elements   =     68716    389380
AFLR3 QI : Nodes, Elements   =     67278    381216
AFLR3 QI : Nodes, Elements   =     67023    379752
AFLR3 QI : Nodes, Elements   =     67008    379668
AFLR3 QI : Nodes, Elements   =     67006    379656
AFLR3 QI : Nodes, Elements   =     67006    383317
AFLR3 QI : Nodes, Elements   =     67006    379427
AFLR3 QI : Nodes, Elements   =     67006    379059
AFLR3 QI : Nodes, Elements   =     67006    379440
AFLR3 QI : Nodes, Elements   =     67006    378845
AFLR3 QI : Nodes, Elements   =     67006    378651
AFLR3 QI : Nodes, Elements   =     67006    378930
AFLR3 QI : Nodes, Elements   =     67006    378627
AFLR3 QI : Nodes, Elements   =     67006    378531
AFLR3 QI : Nodes, Elements   =     67006    378787
AFLR3 QI : Nodes, Elements   =     67006    378530
AFLR3 QI : Nodes, Elements   =     67006    378477
AFLR3 QI : Nodes, Elements   =     67006    378727
AFLR3 QI : Nodes, Elements   =     67006    378484
AFLR3 QI : Nodes, Elements   =     67006    378447
AFLR3 QI : Nodes, Elements   =     67009    378461
AFLR3 QI : Nodes, Elements   =     67009    378706
AFLR3 QI : Nodes, Elements   =     67009    378476
AFLR3 QI : Nodes, Elements   =     67009    378460
AFLR3 QI : Nodes, Elements   =     67009    378698
AFLR3 QI : Nodes, Elements   =     67009    378474
AFLR3 QI : Nodes, Elements   =     67009    378437
 
AFLR3    : CPU Time          =     0.595   seconds
 
AFLR3 QRG: QUALITY GRID RE-GENERATION
 
AFLR3 QRG: Nodes, Elements   =     67009    378437
AFLR3 QRG: Nodes, Elements   =     67032    378558
AFLR3 QRG: Nodes, Elements   =     67031    378553
AFLR3 QRG: Nodes, Elements   =     67037    378584
AFLR3 QRG: Nodes, Elements   =     67046    378631
AFLR3 QRG: Nodes, Elements   =     67044    378622
 
AFLR3    : CPU Time          =     0.023   seconds
 
AFLR3    : DONE

UG3      : DIHEDRAL ANGLE CHECK

UG3      : No. Tet Elems     =    378622
UG3      : Min, Max Ang      =     1.144     173.8
UG3      : Average Angle     =      70.2
UG3      : No. Angle>160.0   =        55
UG3      : No. Angle>179.9   =         0

UG3      : VOL CHECK

UG3      : Total-Volume      =  2.11e+06

UG3      : No. Tet Elems     =    378622
UG3      : Min Vol           =  6.04e-10
UG3      : Average Vol       =      5.57
UG3      : Total-Tet-Vol     =  2.11e+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     =    378622
UG3      : Min, Max Q        =    0.0662         1
UG3      : Average Q         =      0.89
UG3      : No. Q<       0.1  =        20
UG3      : No. Q<      0.01  =         0

OVERALL  : CPU Time          =     2.766   seconds

UG3      : DIHEDRAL ANGLE CHECK

UG3      : No. Tet Elems     =    378622
UG3      : Min, Max Ang      =     1.144     173.8
UG3      : Average Angle     =      70.2
UG3      : No. Angle>160.0   =        55
UG3      : No. Angle>179.9   =         0

UG3      : VOL CHECK

UG3      : Total-Volume      =  2.11e+06

UG3      : No. Tet Elems     =    378622
UG3      : Min Vol           =  6.04e-10
UG3      : Average Vol       =      5.57
UG3      : Total-Tet-Vol     =  2.11e+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     =    378622
UG3      : Min, Max Q        =     0.171         1
UG3      : Average Q         =     0.853
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          = 67044
	Number of elements       = 391028
	Number of triangles      = 12406
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 378622
	Number of pyramids       = 0
	Number of prisms         = 0
	Number of hexahedrals    = 0
No project name ("Proj_Name") provided - A volume mesh will not be written out

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          = 67044
	Number of elements       = 391028
	Number of triangles      = 12406
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 378622
	Number of pyramids       = 0
	Number of prisms         = 0
	Number of hexahedrals    = 0
No project name ("Proj_Name") provided - A volume mesh will not be written out

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 (8.0.0) "
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 (8.0.0) "
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!
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          = 67044
	Number of elements       = 391028
	Number of triangles      = 12406
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 378622
	Number of pyramids       = 0
	Number of prisms         = 0
	Number of hexahedrals    = 0
No project name ("Proj_Name") provided - A volume mesh will not be written out

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 (8.0.0) "
 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 (8.0.0) "
 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          = 67044
	Number of elements       = 391028
	Number of triangles      = 12406
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 378622
	Number of pyramids       = 0
	Number of prisms         = 0
	Number of hexahedrals    = 0
No project name ("Proj_Name") provided - A volume mesh will not be written out

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 (8.0.0) "
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 (8.0.0) "
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 (8.0.0) "
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)
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to 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
Body 1 (of 1)
Number of nodes    = 25
Number of elements = 16
Number of node elements          = 0
Number of line elements          = 0
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)
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to 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
Body 1 (of 1)
Number of nodes    = 25
Number of elements = 16
Number of node elements          = 0
Number of line elements          = 0
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 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 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 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 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 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 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 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 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 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 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 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 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 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 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 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 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 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 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 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 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 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 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 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 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 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 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 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 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 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 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 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 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 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 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 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 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 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 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 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 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 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 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 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 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 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 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 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 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 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 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 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 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 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 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 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 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 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 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 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 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 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 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 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 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 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 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 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 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 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 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 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 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 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 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 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 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 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 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 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 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 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 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 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 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 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 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 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 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 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 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 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 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 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 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 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 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 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 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 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 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:61202)
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!
 1717DB000 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!
 1717DB000 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 node elements          = 0
Number of line elements          = 0
Number of triangle elements      = 192
Number of quadrilateral elements = 0
Body 2 (of 7)
Number of nodes    = 298
Number of elements = 592
Number of node elements          = 0
Number of line elements          = 0
Number of triangle elements      = 592
Number of quadrilateral elements = 0
Body 3 (of 7)
Number of nodes    = 488
Number of elements = 972
Number of node elements          = 0
Number of line elements          = 0
Number of triangle elements      = 972
Number of quadrilateral elements = 0
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Body 4 (of 7)
Number of nodes    = 2048
Number of elements = 4096
Number of node elements          = 0
Number of line elements          = 0
Number of triangle elements      = 4096
Number of quadrilateral elements = 0
Body 5 (of 7)
Number of nodes    = 152
Number of elements = 300
Number of node elements          = 0
Number of line elements          = 0
Number of triangle elements      = 300
Number of quadrilateral elements = 0
Body 6 (of 7)
Number of nodes    = 624
Number of elements = 1248
Number of node elements          = 0
Number of line elements          = 0
Number of triangle elements      = 1248
Number of quadrilateral elements = 0
Body 7 (of 7)
Number of nodes    = 489
Number of elements = 974
Number of node elements          = 0
Number of line elements          = 0
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 = pYq1.500/0.000T1.00e-16A
Delaunizing vertices...
Delaunay seconds:  0.001929
Creating surface mesh ...
Surface mesh seconds:  5e-05
Recovering boundaries...
Boundary recovery seconds:  0.000755
Removing exterior tetrahedra ...
Spreading region attributes.
Exterior tets removal seconds:  2.7e-05
Recovering Delaunayness...
Delaunay recovery seconds:  0.0007
Refining mesh...
Refinement seconds:  0.000594
Smoothing vertices...
Mesh smoothing seconds:  0.002418
Improving mesh...
Mesh improvement seconds:  0.000252

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

Output seconds:  1.7e-05
Total running seconds:  0.006762

Statistics:

  Input points: 98
  Input facets: 192
  Input segments: 288
  Input holes: 0
  Input regions: 0

  Mesh points: 100
  Mesh tetrahedra: 232
  Mesh faces: 560
  Mesh faces on exterior boundary: 192
  Mesh faces on input facets: 192
  Mesh edges on input segments: 288
  Steiner points inside domain: 2

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 = pYq1.500/0.000T1.00e-16A
Delaunizing vertices...
Delaunay seconds:  0.010752
Creating surface mesh ...
Surface mesh seconds:  0.00018
Recovering boundaries...
Boundary recovery seconds:  0.001579
Removing exterior tetrahedra ...
Spreading region attributes.
Exterior tets removal seconds:  0.000165
Recovering Delaunayness...
Delaunay recovery seconds:  0.003096
Refining mesh...
Refinement seconds:  0.013403
Smoothing vertices...
Mesh smoothing seconds:  0.016146
Improving mesh...
Mesh improvement seconds:  0.000323

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

Output seconds:  3.1e-05
Total running seconds:  0.045704

Statistics:

  Input points: 298
  Input facets: 592
  Input segments: 888
  Input holes: 0
  Input regions: 0

  Mesh points: 355
  Mesh tetrahedra: 1106
  Mesh faces: 2508
  Mesh faces on exterior boundary: 592
  Mesh faces on input facets: 592
  Mesh edges on input segments: 888
  Steiner points inside domain: 57

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 = pYq1.500/0.000T1.00e-16A
Delaunizing vertices...
Delaunay seconds:  0.044931
Creating surface mesh ...
Surface mesh seconds:  0.000237
Recovering boundaries...
Boundary recovery seconds:  0.004679
Removing exterior tetrahedra ...
Spreading region attributes.
Exterior tets removal seconds:  0.000327
Recovering Delaunayness...
Delaunay recovery seconds:  0.010319
Refining mesh...
  650 insertions, added 162 points, 7185 tetrahedra in queue.
  216 insertions, added 10 points, 5924 tetrahedra in queue.
  288 insertions, added 6 points, 2911 tetrahedra in queue.
  384 insertions, added 10 points, 126 tetrahedra in queue.
Refinement seconds:  0.108674
Smoothing vertices...
Mesh smoothing seconds:  0.037474
Improving mesh...
Mesh improvement seconds:  0.000443

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

Output seconds:  4.9e-05
Total running seconds:  0.207166

Statistics:

  Input points: 488
  Input facets: 972
  Input segments: 1458
  Input holes: 0
  Input regions: 0

  Mesh points: 687
  Mesh tetrahedra: 2744
  Mesh faces: 5974
  Mesh faces on exterior boundary: 972
  Mesh faces on input facets: 972
  Mesh edges on input segments: 1458
  Steiner points inside domain: 199

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 = pYq1.500/0.000T1.00e-16A
Delaunizing vertices...
Delaunay seconds:  0.324082
Creating surface mesh ...
Surface mesh seconds:  0.000991
Recovering boundaries...
Boundary recovery seconds:  0.004595
Removing exterior tetrahedra ...
Spreading region attributes.
Exterior tets removal seconds:  0.001207
Recovering Delaunayness...
Delaunay recovery seconds:  0.092607
Refining mesh...
Refinement seconds:  0.214905
Smoothing vertices...
Mesh smoothing seconds:  0.153941
Improving mesh...
Mesh improvement seconds:  0.001873

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

Output seconds:  0.000196
Total running seconds:  0.794465

Statistics:

  Input points: 2048
  Input facets: 4096
  Input segments: 6144
  Input holes: 0
  Input regions: 0

  Mesh points: 2901
  Mesh tetrahedra: 11307
  Mesh faces: 24662
  Mesh faces on exterior boundary: 4096
  Mesh faces on input facets: 4096
  Mesh edges on input segments: 6144
  Steiner points inside domain: 853

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 = pYq1.500/0.000T1.00e-16A
Delaunizing vertices...
Delaunay seconds:  0.000211
Creating surface mesh ...
Surface mesh seconds:  8.2e-05
Recovering boundaries...
Boundary recovery seconds:  0.000186
Removing exterior tetrahedra ...
Spreading region attributes.
Exterior tets removal seconds:  4.9e-05
Recovering Delaunayness...
Delaunay recovery seconds:  0.000275
Refining mesh...
Refinement seconds:  0.001556
Smoothing vertices...
Mesh smoothing seconds:  0.001366
Improving mesh...
Mesh improvement seconds:  9.3e-05

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

Output seconds:  2e-05
Total running seconds:  0.003859

Statistics:

  Input points: 152
  Input facets: 300
  Input segments: 450
  Input holes: 0
  Input regions: 0

  Mesh points: 193
  Mesh tetrahedra: 636
  Mesh faces: 1422
  Mesh faces on exterior boundary: 300
  Mesh faces on input facets: 300
  Mesh edges on input segments: 450
  Steiner points inside domain: 41

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 = pYq1.500/0.000T1.00e-16A
Delaunizing vertices...
Delaunay seconds:  0.038234
Creating surface mesh ...
Surface mesh seconds:  0.000288
Recovering boundaries...
Boundary recovery seconds:  0.003368
Removing exterior tetrahedra ...
Spreading region attributes.
Exterior tets removal seconds:  0.000375
Recovering Delaunayness...
Delaunay recovery seconds:  0.004972
Refining mesh...
  831 insertions, added 215 points, 6026 tetrahedra in queue.
  276 insertions, added 15 points, 1148 tetrahedra in queue.
Refinement seconds:  0.045688
Smoothing vertices...
Mesh smoothing seconds:  0.036682
Improving mesh...
Mesh improvement seconds:  0.000528

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

Output seconds:  6e-05
Total running seconds:  0.130233

Statistics:

  Input points: 624
  Input facets: 1248
  Input segments: 1872
  Input holes: 0
  Input regions: 0

  Mesh points: 854
  Mesh tetrahedra: 3220
  Mesh faces: 7064
  Mesh faces on exterior boundary: 1248
  Mesh faces on input facets: 1248
  Mesh edges on input segments: 1872
  Steiner points inside domain: 230

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 = pYq1.500/0.000T1.00e-16A
Delaunizing vertices...
Delaunay seconds:  0.033704
Creating surface mesh ...
Surface mesh seconds:  0.00025
Recovering boundaries...
Boundary recovery seconds:  0.002564
Removing exterior tetrahedra ...
Spreading region attributes.
Exterior tets removal seconds:  0.000228
Recovering Delaunayness...
Delaunay recovery seconds:  0.024781
Refining mesh...
Refinement seconds:  0.033269
Smoothing vertices...
Mesh smoothing seconds:  0.019102
Improving mesh...
Mesh improvement seconds:  0.000406

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

Output seconds:  5e-05
Total running seconds:  0.114392

Statistics:

  Input points: 489
  Input facets: 974
  Input segments: 1461
  Input holes: 0
  Input regions: 0

  Mesh points: 670
  Mesh tetrahedra: 2479
  Mesh faces: 5445
  Mesh faces on exterior boundary: 974
  Mesh faces on input facets: 974
  Mesh edges on input segments: 1461
  Steiner points inside domain: 181

Done meshing using TetGen!

Writing AFLR3 file ....
Finished writing AFLR3 file


Writing AFLR3 file ....
Finished writing AFLR3 file


Writing AFLR3 file ....
Finished writing AFLR3 file


Writing AFLR3 file ....
Finished writing AFLR3 file


Writing AFLR3 file ....
Finished writing AFLR3 file


Writing AFLR3 file ....
Finished writing AFLR3 file


Writing AFLR3 file ....
Finished writing AFLR3 file

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 = pYq1.500/0.000T1.00e-16A
Delaunizing vertices...
Delaunay seconds:  0.001942
Creating surface mesh ...
Surface mesh seconds:  4.5e-05
Recovering boundaries...
Boundary recovery seconds:  0.000765
Removing exterior tetrahedra ...
Spreading region attributes.
Exterior tets removal seconds:  2.8e-05
Recovering Delaunayness...
Delaunay recovery seconds:  0.0007
Refining mesh...
Refinement seconds:  0.001319
Smoothing vertices...
Mesh smoothing seconds:  0.002377
Improving mesh...
Mesh improvement seconds:  4.2e-05

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

Output seconds:  1.3e-05
Total running seconds:  0.007255

Statistics:

  Input points: 98
  Input facets: 192
  Input segments: 288
  Input holes: 0
  Input regions: 1

  Mesh points: 100
  Mesh tetrahedra: 232
  Mesh faces: 560
  Mesh faces on exterior boundary: 192
  Mesh faces on input facets: 192
  Mesh edges on input segments: 288
  Steiner points inside domain: 2


Generating volume mesh using TetGen.....

Tetgen input string = pYq1.500/0.000T1.00e-16A
Delaunizing vertices...
Delaunay seconds:  0.010456
Creating surface mesh ...
Surface mesh seconds:  0.000141
Recovering boundaries...
Boundary recovery seconds:  0.001556
Removing exterior tetrahedra ...
Warning:  The 1-th region point lies outside the convex hull.
Spreading region attributes.
Exterior tets removal seconds:  0.000158
Recovering Delaunayness...
Delaunay recovery seconds:  0.003052
Refining mesh...
Refinement seconds:  0.013356
Smoothing vertices...
Mesh smoothing seconds:  0.016144
Improving mesh...
Mesh improvement seconds:  0.000506

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

Output seconds:  3.3e-05
Total running seconds:  0.045429

Statistics:

  Input points: 298
  Input facets: 592
  Input segments: 888
  Input holes: 0
  Input regions: 2

  Mesh points: 355
  Mesh tetrahedra: 1106
  Mesh faces: 2508
  Mesh faces on exterior boundary: 592
  Mesh faces on input facets: 592
  Mesh edges on input segments: 888
  Steiner points inside domain: 57


Generating volume mesh using TetGen.....

Tetgen input string = pYq1.500/0.000T1.00e-16A
Delaunizing vertices...
Delaunay seconds:  0.04491
Creating surface mesh ...
Surface mesh seconds:  0.000223
Recovering boundaries...
Boundary recovery seconds:  0.004685
Removing exterior tetrahedra ...
Warning:  The 1-th region point lies outside the convex hull.
Warning:  The 2-th region point lies outside the convex hull.
Spreading region attributes.
Exterior tets removal seconds:  0.000336
Recovering Delaunayness...
Delaunay recovery seconds:  0.010333
Refining mesh...
  650 insertions, added 162 points, 7185 tetrahedra in queue.
  216 insertions, added 10 points, 5924 tetrahedra in queue.
  288 insertions, added 6 points, 2911 tetrahedra in queue.
  384 insertions, added 10 points, 126 tetrahedra in queue.
Refinement seconds:  0.108996
Smoothing vertices...
Mesh smoothing seconds:  0.03749
Improving mesh...
Mesh improvement seconds:  0.00044

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

Output seconds:  4.8e-05
Total running seconds:  0.207492

Statistics:

  Input points: 488
  Input facets: 972
  Input segments: 1458
  Input holes: 0
  Input regions: 3

  Mesh points: 687
  Mesh tetrahedra: 2744
  Mesh faces: 5974
  Mesh faces on exterior boundary: 972
  Mesh faces on input facets: 972
  Mesh edges on input segments: 1458
  Steiner points inside domain: 199


Generating volume mesh using TetGen.....

Tetgen input string = pYq1.500/0.000T1.00e-16A
Delaunizing vertices...
Delaunay seconds:  0.324135
Creating surface mesh ...
Surface mesh seconds:  0.001013
Recovering boundaries...
Boundary recovery seconds:  0.004601
Removing exterior tetrahedra ...
Warning:  The 1-th region point lies outside the convex hull.
Warning:  The 2-th region point lies outside the convex hull.
Warning:  The 3-th region point lies outside the convex hull.
Spreading region attributes.
Exterior tets removal seconds:  0.001221
Recovering Delaunayness...
Delaunay recovery seconds:  0.092517
Refining mesh...
Refinement seconds:  0.216591
Smoothing vertices...
Mesh smoothing seconds:  0.154021
Improving mesh...
Mesh improvement seconds:  0.001881

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

Output seconds:  0.000191
Total running seconds:  0.796242

Statistics:

  Input points: 2048
  Input facets: 4096
  Input segments: 6144
  Input holes: 0
  Input regions: 4

  Mesh points: 2901
  Mesh tetrahedra: 11307
  Mesh faces: 24662
  Mesh faces on exterior boundary: 4096
  Mesh faces on input facets: 4096
  Mesh edges on input segments: 6144
  Steiner points inside domain: 853


Generating volume mesh using TetGen.....

Tetgen input string = pYq1.500/0.000T1.00e-16A
Delaunizing vertices...
Delaunay seconds:  0.000216
Creating surface mesh ...
Surface mesh seconds:  9.1e-05
Recovering boundaries...
Boundary recovery seconds:  0.000191
Removing exterior tetrahedra ...
Warning:  The 1-th region point lies outside the convex hull.
Warning:  The 2-th region point lies outside the convex hull.
Warning:  The 3-th region point lies outside the convex hull.
Warning:  The 4-th region point lies outside the convex hull.
Spreading region attributes.
Exterior tets removal seconds:  5.4e-05
Recovering Delaunayness...
Delaunay recovery seconds:  0.000277
Refining mesh...
Refinement seconds:  0.001566
Smoothing vertices...
Mesh smoothing seconds:  0.00137
Improving mesh...
Mesh improvement seconds:  9.6e-05

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

Output seconds:  2e-05
Total running seconds:  0.003906

Statistics:

  Input points: 152
  Input facets: 300
  Input segments: 450
  Input holes: 0
  Input regions: 5

  Mesh points: 193
  Mesh tetrahedra: 636
  Mesh faces: 1422
  Mesh faces on exterior boundary: 300
  Mesh faces on input facets: 300
  Mesh edges on input segments: 450
  Steiner points inside domain: 41


Generating volume mesh using TetGen.....

Tetgen input string = pYq1.500/0.000T1.00e-16A
Delaunizing vertices...
Delaunay seconds:  0.038317
Creating surface mesh ...
Surface mesh seconds:  0.000317
Recovering boundaries...
Boundary recovery seconds:  0.003395
Removing exterior tetrahedra ...
Warning:  The 1-th region point lies outside the convex hull.
Warning:  The 2-th region point lies outside the convex hull.
Warning:  The 3-th region point lies outside the convex hull.
Warning:  The 4-th region point lies outside the convex hull.
Warning:  The 5-th region point lies outside the convex hull.
Spreading region attributes.
Exterior tets removal seconds:  0.00038
Recovering Delaunayness...
Delaunay recovery seconds:  0.004951
Refining mesh...
  831 insertions, added 215 points, 6026 tetrahedra in queue.
  276 insertions, added 15 points, 1148 tetrahedra in queue.
Refinement seconds:  0.045686
Smoothing vertices...
Mesh smoothing seconds:  0.036654
Improving mesh...
Mesh improvement seconds:  0.000526

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

Output seconds:  5.9e-05
Total running seconds:  0.130322

Statistics:

  Input points: 624
  Input facets: 1248
  Input segments: 1872
  Input holes: 0
  Input regions: 6

  Mesh points: 854
  Mesh tetrahedra: 3220
  Mesh faces: 7064
  Mesh faces on exterior boundary: 1248
  Mesh faces on input facets: 1248
  Mesh edges on input segments: 1872
  Steiner points inside domain: 230


Generating volume mesh using TetGen.....

Tetgen input string = pYq1.500/0.000T1.00e-16A
Delaunizing vertices...
Delaunay seconds:  0.033742
Creating surface mesh ...
Surface mesh seconds:  0.000227
Recovering boundaries...
Boundary recovery seconds:  0.002556
Removing exterior tetrahedra ...
Warning:  The 1-th region point lies outside the convex hull.
Warning:  The 2-th region point lies outside the convex hull.
Warning:  The 3-th region point lies outside the convex hull.
Warning:  The 4-th region point lies outside the convex hull.
Warning:  The 5-th region point lies outside the convex hull.
Warning:  The 6-th region point lies outside the convex hull.
Spreading region attributes.
Exterior tets removal seconds:  0.00024
Recovering Delaunayness...
Delaunay recovery seconds:  0.024761
Refining mesh...
Refinement seconds:  0.030203
Smoothing vertices...
Mesh smoothing seconds:  0.021362
Improving mesh...
Mesh improvement seconds:  0.000451

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

Output seconds:  5.9e-05
Total running seconds:  0.113626

Statistics:

  Input points: 489
  Input facets: 974
  Input segments: 1461
  Input holes: 0
  Input regions: 7

  Mesh points: 673
  Mesh tetrahedra: 2510
  Mesh faces: 5507
  Mesh faces on exterior boundary: 974
  Mesh faces on input facets: 974
  Mesh edges on input segments: 1461
  Steiner points inside domain: 184

Done meshing using TetGen!

Writing AFLR3 file ....
Finished writing AFLR3 file

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!

Writing TECPLOT file: test.dat ....
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

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 - 7137, elements - 14266
Getting volume mesh

Generating volume mesh using TetGen.....

Tetgen input string = pYq1.500/0.000QT1.00e-16A
Done meshing using TetGen!

Writing TECPLOT file: test.dat ....
Finished writing TECPLOT file

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 node elements          = 0
Number of line elements          = 0
Number of triangle elements      = 19158
Number of quadrilateral elements = 0
----------------------------
Total number of nodes    = 9583
Total number of elements = 19158

Writing TECPLOT file: test.dat ....
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 = pYq1.500/0.000QT1.00e-16A
Done meshing using TetGen!

Writing TECPLOT file: test.dat ....
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 TECPLOT file: test.dat ....
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

----------------------------------------------------------------------
Ran 137 tests in 325.193s

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,-4.178738547362e-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,-7.889656776594e-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	0m0.398s
user	0m0.251s
sys	0m0.069s
+ 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	0m1.201s
user	0m1.086s
sys	0m0.038s
+ 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	0m0.330s
user	0m0.152s
sys	0m0.023s
+ 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 9.14.7
AFLR2    : Version Date   07/16/23 @ 01:42PM
AFLR2    : Compile OS     Darwin 22.6.0 arm64
AFLR2    : Compile Date   08/01/23 @ 11:39PM
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      2159
AFLR2 QI : Nodes, Faces      =     18604     17104
AFLR2 QI : Nodes, Faces      =     18604     36367
AFLR2 QI : Nodes, Faces      =     18604      2159
AFLR2 QI : Nodes, Faces      =     18604     17104
AFLR2 QI : Nodes, Faces      =     18604      2159
AFLR2 QI : Nodes, Faces      =     18604     17104
 
AFLR2    : CPU Time          =     0.014   seconds
 
AFLR2    : DONE

Writing AFLR3 file ....
Finished writing AFLR3 file

Number of nodes = 18604
Number of elements = 20104
Number of tris = 2159
Number of quad = 17104

Writing TECPLOT file: AFLR2_Test.dat ....
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 =  2159
	Number of Hexahedral =  17104

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	0m0.755s
user	0m0.587s
sys	0m0.330s
+ 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 node elements          = 0
Number of line elements          = 0
Number of triangle elements      = 19142
Number of quadrilateral elements = 0
Body 2 (of 3)
Number of nodes    = 6160
Number of elements = 12316
Number of node elements          = 0
Number of line elements          = 0
Number of triangle elements      = 12316
Number of quadrilateral elements = 0
Body 3 (of 3)
Number of nodes    = 258
Number of elements = 512
Number of node elements          = 0
Number of line elements          = 0
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:  0.095898
Creating surface mesh ...
Surface mesh seconds:  0.013086
Recovering boundaries...
Boundary recovery seconds:  0.058786
Removing exterior tetrahedra ...
Spreading region attributes.
Exterior tets removal seconds:  0.018946
Recovering Delaunayness...
Delaunay recovery seconds:  0.036778
Refining mesh...
  21316 insertions, added 16866 points, 786217 tetrahedra in queue.
  7098 insertions, added 2814 points, 333350 tetrahedra in queue.
Refinement seconds:  0.721143
Smoothing vertices...
Mesh smoothing seconds:  0.925034
Improving mesh...
Mesh improvement seconds:  0.025669

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

Output seconds:  0.004438
Total running seconds:  1.89995

Statistics:

  Input points: 15991
  Input facets: 31970
  Input segments: 47955
  Input holes: 2
  Input regions: 0

  Mesh points: 36858
  Mesh tetrahedra: 177623
  Mesh faces: 371231
  Mesh faces on exterior boundary: 31970
  Mesh faces on input facets: 31970
  Mesh edges on input segments: 47955
  Steiner points inside domain: 20867

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	0m3.522s
user	0m3.964s
sys	0m0.108s
+ 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  -2.715465e-02   0.000000e+00   0.000000e+00 
 -2.715465e-02   0.000000e+00   0.000000e+00  -2.543571e-02 
  0.000000e+00   0.000000e+00   0.000000e+00   0.000000e+00 
  0.000000e+00  -2.543571e-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  -2.059198e-02   0.000000e+00 
 -2.059198e-02   0.000000e+00   0.000000e+00 
  0.000000e+00   0.000000e+00   0.000000e+00 


real	0m2.135s
user	0m3.837s
sys	0m0.037s
+ 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	0m0.320s
user	0m0.224s
sys	0m0.023s
+ 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	0m0.495s
user	0m0.402s
sys	0m0.022s
+ 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	0m0.299s
user	0m0.205s
sys	0m0.024s
+ 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-3.11.6/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   0.0006119078685800691
CYtot   -6.294248256212792e-15
CZtot   -0.3012861394881716
Cltot   -4.783257394769952e-14
Cmtot   -0.1945055953448142
Cntot   -2.33897052252666e-15
Cl'tot  -4.786610947920897e-14
Cn'tot  -1.50382076451035e-15
CLtot   0.3012509314146399
CDtot   0.00464635348821982
CDvis   0.0
CLff    0.3009503023516155
CYff    -7.721166100146254e-15
CDind   0.00464635348821982
CDff    0.00496896950089486
e       0.9669902146156001
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 =  [-0.004234137763147, -0.004494543653181, -0.003752887372721, -0.002739626801633, -0.001762021024329, -0.0007386538946455, 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, -0.003752887372441, -0.004494543653151, -0.00423413776453]

real	0m0.454s
user	0m0.584s
sys	0m0.174s
+ 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   -0.0412001563846227
CYtot   2.978622347381309e-11
CZtot   -1.125018848419552
Cltot   6.433305666344365e-11
Cmtot   -1.954741259599045
Cntot   -8.596041715790853e-12
Cl'tot  6.417323681353383e-11
Cn'tot  -9.717499149244883e-12
CLtot   1.124128460725282
CDtot   0.06082816759347054
CDvis   0.0
CLff    1.12310548217915
CYff    1.557646063320801e-11
CDind   0.06082816759347054
CDff    -0.2032105909613897
e       -0.3293014157959109

real	0m5.437s
user	0m5.658s
sys	0m4.997s
+ 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 = 0.002572533601550746
Cl = 0.2009337808873514
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 = 0.002586364230241773
Cl = 0.2015191856814839
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 = 0.002609799718816135
Cl = 0.202507529643331
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 = 0.002643444008424596
Cl = 0.2039185811658758
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 = 0.002688200920998178
Cl = 0.2057816377790573
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 = 0.002745342060015916
Cl = 0.2081373840559939
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 = 0.002816610334298742
Cl = 0.2110406736705551
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 = 0.002904376657734686
Cl = 0.2145646488015986
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 = 0.003011879793042714
Cl = 0.2188068842334934
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 = 0.003143602034586197
Cl = 0.2238987294815716
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 = 0.003305877285452323
Cl = 0.2300199286487145
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 = 0.003507917885472498
Cl = 0.2374223860296622
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 = 0.003763643677259927
Cl = 0.2464707142744897
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 = 0.004095167898227168
Cl = 0.2577158067747692
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 = 0.004540047408135285
Cl = 0.2720394012163574
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 = 0.005168237926851837
Cl = 0.2909701507463247
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 = 0.006128930715329106
Cl = 0.3174875485935573
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 = 0.007818359051271607
Cl = 0.3586078919918749
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 = 0.01186220444373959
Cl = 0.438263863524391
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 = 0.002572533601550746
Cl = 0.2009337808873514
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 = 0.002586364230241773
Cl = 0.2015191856814839
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 = 0.002609799718816135
Cl = 0.202507529643331
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 = 0.002643444008424596
Cl = 0.2039185811658758
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 = 0.002688200920998178
Cl = 0.2057816377790573
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 = 0.002745342060015916
Cl = 0.2081373840559939
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 = 0.002816610334298742
Cl = 0.2110406736705551
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 = 0.002904376657734686
Cl = 0.2145646488015986
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 = 0.003011879793042714
Cl = 0.2188068842334934
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 = 0.003143602034586197
Cl = 0.2238987294815716
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 = 0.003305877285452323
Cl = 0.2300199286487145
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 = 0.003507917885472498
Cl = 0.2374223860296622
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 = 0.003763643677259927
Cl = 0.2464707142744897
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 = 0.004095167898227168
Cl = 0.2577158067747692
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 = 0.004540047408135285
Cl = 0.2720394012163574
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 = 0.005168237926851837
Cl = 0.2909701507463247
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 = 0.006128930715329106
Cl = 0.3174875485935573
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 = 0.007818359051271607
Cl = 0.3586078919918749
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 = 0.01186220444373959
Cl = 0.438263863524391
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 = 0.002572533601550746
Cl = 0.2009337808873514
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 = 0.002586364230241773
Cl = 0.2015191856814839
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 = 0.002609799718816135
Cl = 0.202507529643331
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 = 0.002643444008424596
Cl = 0.2039185811658758
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 = 0.002688200920998178
Cl = 0.2057816377790573
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 = 0.002745342060015916
Cl = 0.2081373840559939
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 = 0.002816610334298742
Cl = 0.2110406736705551
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 = 0.002904376657734686
Cl = 0.2145646488015986
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 = 0.003011879793042714
Cl = 0.2188068842334934
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 = 0.003143602034586197
Cl = 0.2238987294815716
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 = 0.003305877285452323
Cl = 0.2300199286487145
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 = 0.003507917885472498
Cl = 0.2374223860296622
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 = 0.003763643677259927
Cl = 0.2464707142744897
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 = 0.004095167898227168
Cl = 0.2577158067747692
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 = 0.004540047408135285
Cl = 0.2720394012163574
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 = 0.005168237926851837
Cl = 0.2909701507463247
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 = 0.006128930715329106
Cl = 0.3174875485935573
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 = 0.007818359051271607
Cl = 0.3586078919918749
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 = 0.01186220444373959
Cl = 0.438263863524391
Cl[0] =  0.2009337808873514
Cd[0] =  0.002572533601550746

real	0m16.159s
user	0m8.265s
sys	0m7.810s
+ 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  -0.01911479917641004
CYtot  0.03828770401115552
CZtot  -0.6203123021537943
Cltot  0.05803020542928476
Cmtot  -0.3649415791575075
Cntot  -0.02051317548232544
Cl'tot 0.05766336287208541
Cn'tot -0.02152281795713262
CLtot  0.6198842263414324
CDtot  0.02993783031514589
CDvis  0.0
CLff   0.6192452092592857
CYff   0.03287079625844262
CDind  0.02993783031514589
CDff   0.02861019822657772
e      0.7130586920543268

real	0m0.538s
user	0m0.654s
sys	0m0.190s
+ 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	0m0.445s
user	0m0.582s
sys	0m0.169s
+ 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	0m12.603s
user	0m4.128s
sys	0m0.810s
+ 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	0m0.291s
user	0m0.375s
sys	0m0.068s
+ 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	0m0.371s
user	0m0.469s
sys	0m0.053s
+ 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	0m1.844s
user	0m2.064s
sys	0m0.083s
+ 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 =   7.5820667358140921E-003

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

real	0m13.703s
user	0m13.747s
sys	0m0.315s
+ 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	0m1.940s
user	0m2.178s
sys	0m0.068s
+ 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 node elements          = 0
Number of line elements          = 0
Number of triangle elements      = 0
Number of quadrilateral elements = 4001
Body 2 (of 4)
Number of nodes    = 1
Number of elements = 1
Number of node elements          = 1
Number of line elements          = 0
Number of triangle elements      = 0
Number of quadrilateral elements = 0
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Body 3 (of 4)
Number of nodes    = 76
Number of elements = 55
Number of node elements          = 0
Number of line elements          = 0
Number of triangle elements      = 0
Number of quadrilateral elements = 55
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to 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 4 (of 4)
Number of nodes    = 100
Number of elements = 73
Number of node elements          = 0
Number of line elements          = 0
Number of triangle elements      = 0
Number of quadrilateral elements = 73
----------------------------
Total number of nodes    = 3970
Total number of elements = 4130

Writing TECPLOT file: egadsTessMesh_Surf_0.dat ....
Finished writing TECPLOT file


Writing TECPLOT file: egadsTessMesh_Surf_1.dat ....
Finished writing TECPLOT file


Writing TECPLOT file: egadsTessMesh_Surf_2.dat ....
Finished writing TECPLOT file


Writing TECPLOT file: egadsTessMesh_Surf_3.dat ....
Finished writing TECPLOT file


real	0m3.240s
user	0m9.017s
sys	0m5.111s
+ 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 node elements          = 0
Number of line elements          = 0
Number of triangle elements      = 0
Number of quadrilateral elements = 600
	capsIgnore attribute found for face - 6!!
Body 2 (of 3)
Number of nodes    = 537
Number of elements = 535
Number of node elements          = 0
Number of line elements          = 0
Number of triangle elements      = 0
Number of quadrilateral elements = 535
Body 3 (of 3)
Number of nodes    = 1356
Number of elements = 1354
Number of node elements          = 0
Number of line elements          = 0
Number of triangle elements      = 0
Number of quadrilateral elements = 1354
----------------------------
Total number of nodes    = 2495
Total number of elements = 2489

Writing TECPLOT file: egadsTessMesh_Surf_0.dat ....
Finished writing TECPLOT file


Writing TECPLOT file: egadsTessMesh_Surf_1.dat ....
Finished writing TECPLOT file


Writing TECPLOT file: egadsTessMesh_Surf_2.dat ....
Finished writing TECPLOT file


real	0m2.072s
user	0m2.610s
sys	0m0.046s
+ 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    = 6316
Number of elements = 6314
Number of node elements          = 0
Number of line elements          = 0
Number of triangle elements      = 0
Number of quadrilateral elements = 6314
----------------------------
Total number of nodes    = 6316
Total number of elements = 6314

Writing TECPLOT file: egadsTessMesh.dat ....
Finished writing TECPLOT file


real	0m5.446s
user	0m8.447s
sys	0m0.119s
+ 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 (1.013232 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 (1.046939 0.962477)!
 EG_getSidepoint: LineSearch Failed (2.750998 0.986828)!
 EG_getSidepoint: LineSearch Failed (1.035340 0.957497)!
 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 (0.856445 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 node elements          = 0
Number of line elements          = 0
Number of triangle elements      = 0
Number of quadrilateral elements = 1496
----------------------------
Total number of nodes    = 1498
Total number of elements = 1496

Writing TECPLOT file: egadsTessMesh.dat ....
Finished writing TECPLOT file


real	0m1.803s
user	0m2.187s
sys	0m0.072s
+ 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 9.14.7
AFLR2    : Version Date   07/16/23 @ 01:42PM
AFLR2    : Compile OS     Darwin 22.6.0 arm64
AFLR2    : Compile Date   08/01/23 @ 11:39PM
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          =     0.010   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

Writing TECPLOT file: pyCAPS_AFLR2_Test.dat ....
Finished writing TECPLOT file

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)!

real	0m0.436s
user	0m0.689s
sys	0m0.348s
+ 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
AFLR4    : Proximity BG Surface Grid Generation Skipped
AFLR4    : No Modifications Required
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to 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

Writing TECPLOT file: pyCAPS_AFLR4_Test.dat ....
Finished writing TECPLOT file


real	0m1.007s
user	0m1.221s
sys	0m0.092s
+ 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: pyCAPS_AFLR4_Test.dat ....
Finished writing TECPLOT file


real	0m1.173s
user	0m1.376s
sys	0m0.254s
+ 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: pyCAPS_AFLR4_Missile_Test.dat ....
Finished writing TECPLOT file


real	0m3.197s
user	0m5.992s
sys	0m0.311s
+ 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: pyCAPS_AFLR4_1B2_Test.dat ....
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: pyCAPS_AFLR4_1B0_Test.dat ....
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: pyCAPS_AFLR4_1S2_Test.dat ....
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: pyCAPS_AFLR4_1S0_Test.dat ....
Finished writing TECPLOT file


real	0m4.398s
user	0m4.535s
sys	0m0.157s
+ 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
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to 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

Writing TECPLOT file: pyCAPS_AFLR4_AFLR3.dat ....
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 - 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 9.14.7
AFLR2    : Version Date   07/16/23 @ 01:42PM
AFLR2    : Compile OS     Darwin 22.6.0 arm64
AFLR2    : Compile Date   08/01/23 @ 11:39PM
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 11.5.9
AFLR4    : Version Date   08/14/23 @ 12:27AM
AFLR4    : Compile OS     Darwin 22.6.0 arm64
AFLR4    : Compile Date   08/14/23 @ 12:31AM
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          = 150594
	Number of elements       = 452252
	Number of triangles      = 14380
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 216820
	Number of pyramids       = 424
	Number of prisms         = 220628
	Number of hexahedrals    = 0

Writing TECPLOT file: pyCAPS_AFLR4_AFLR3_VolMesh.dat ....
Finished writing TECPLOT file


real	0m6.368s
user	0m6.472s
sys	0m0.186s
+ 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: pyCAPS_AFLR4_Test.dat ....
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 9.14.7
AFLR2    : Version Date   07/16/23 @ 01:42PM
AFLR2    : Compile OS     Darwin 22.6.0 arm64
AFLR2    : Compile Date   08/01/23 @ 11:39PM
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 11.5.9
AFLR4    : Version Date   08/14/23 @ 12:27AM
AFLR4    : Compile OS     Darwin 22.6.0 arm64
AFLR4    : Compile Date   08/14/23 @ 12:31AM
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          = 332429
	Number of elements       = 1065072
	Number of triangles      = 44190
	Number of quadrilatarals = 1613
	Number of tetrahedrals   = 569874
	Number of pyramids       = 327
	Number of prisms         = 449068
	Number of hexahedrals    = 0

Writing TECPLOT file: pyCAPS_AFLR3_VolMesh.dat ....
Finished writing TECPLOT file


real	0m13.710s
user	0m13.703s
sys	0m0.434s
+ 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: pyCAPS_AFLR4_QuadMesh_Test.dat ....
Finished writing TECPLOT file


real	0m3.602s
user	0m9.261s
sys	0m5.115s
+ 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: pyCAPS_AFLR4_Tetgen.dat ....
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 - 30088, elements - 60164
Getting volume mesh

Generating volume mesh using TetGen.....

Tetgen input string = pYq1.500/0.000QT1.00e-16A
Done meshing using TetGen!

Writing TECPLOT file: pyCAPS_AFLR4_Tetgen_VolMesh.dat ....
Finished writing TECPLOT file


real	0m5.413s
user	0m5.505s
sys	0m0.201s
+ 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 9.14.7
AFLR2    : Version Date   07/16/23 @ 01:42PM
AFLR2    : Compile OS     Darwin 22.6.0 arm64
AFLR2    : Compile Date   08/01/23 @ 11:39PM
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 11.5.9
AFLR4    : Version Date   08/14/23 @ 12:27AM
AFLR4    : Compile OS     Darwin 22.6.0 arm64
AFLR4    : Compile Date   08/14/23 @ 12:31AM
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 Sense   Edges
EGADS    :      1     Yes     1   -1 2 3 -4
EGADS    :      2     Yes     1   -5 6 7 -2
EGADS    :      3     Yes     1   8 5 9 -10
EGADS    :      4     Yes     1   10 11 -12 -13
EGADS    :      5     Yes     1   14 15 -16 -11
EGADS    :      6     Yes     1   1 -17 -14 -9
EGADS    :      7     Yes     1   -18 12 -19 -7
EGADS    :      8     Yes     1   16 20 -3 19
EGADS    :      9     Yes     1   13 18 -6 -8
EGADS    :     10     Yes     1   -15 17 4 -20
EGADS    :     11     Yes     1   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=       135       228         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=       133       220         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=       206       360         0
AFLR4    : Nodes, Trias,Quads=       193       334         0

AFLR4    : Generate optimal mesh on surface definition 7
AFLR2    : Nodes, Trias,Quads=       204       356         0
AFLR4    : Nodes, Trias,Quads=       193       334         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=      1245      2532       464

OVERALL  : CPU Time          =     0.047   seconds
Body 1 (of 1)
Number of nodes    = 1245
Number of elements = 2532
Number of node elements          = 0
Number of line elements          = 0
Number of triangle elements      = 2532
Number of quadrilateral elements = 0
----------------------------
Total number of nodes    = 1245
Total number of elements = 2532
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 2
	Name = box, index = 1
	Name = cut, index = 2
Number of surface: nodes - 1245, elements - 2532
Getting volume mesh

Generating volume mesh using TetGen.....

Tetgen input string = pYq1.500/0.000T1.00e-16A
Delaunizing vertices...
Delaunay seconds:  0.019257
Creating surface mesh ...
Surface mesh seconds:  0.000679
Recovering boundaries...
Boundary recovery seconds:  0.003887
Removing exterior tetrahedra ...
Spreading region attributes.
Exterior tets removal seconds:  0.000328
Recovering Delaunayness...
Delaunay recovery seconds:  0.010528
Refining mesh...
Refinement seconds:  0.006494
Smoothing vertices...
Mesh smoothing seconds:  0.022411
Improving mesh...
Mesh improvement seconds:  0.00076

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

Output seconds:  0.00014
Total running seconds:  0.06452

Statistics:

  Input points: 1245
  Input facets: 2532
  Input segments: 3774
  Input holes: 0
  Input regions: 2

  Mesh points: 1460
  Mesh tetrahedra: 5105
  Mesh faces: 11318
  Mesh faces on exterior boundary: 2216
  Mesh faces on input facets: 2532
  Mesh edges on input segments: 3774
  Steiner points inside domain: 215

Done meshing using TetGen!

Writing VTK file: volume.vtk....
Finished writing VTK file


real	0m0.396s
user	0m0.573s
sys	0m0.084s
+ 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 node elements          = 0
Number of line elements          = 0
Number of triangle elements      = 4468
Number of quadrilateral elements = 0
Body 2 (of 3)
Number of nodes    = 636
Number of elements = 1268
Number of node elements          = 0
Number of line elements          = 0
Number of triangle elements      = 1268
Number of quadrilateral elements = 0
Body 3 (of 3)
Number of nodes    = 258
Number of elements = 512
Number of node elements          = 0
Number of line elements          = 0
Number of triangle elements      = 512
Number of quadrilateral elements = 0
----------------------------
Total number of nodes    = 3130
Total number of elements = 6248

Writing TECPLOT file: egadsTessMesh_Surf_0.dat ....
Finished writing TECPLOT file


Writing TECPLOT file: egadsTessMesh_Surf_1.dat ....
Finished writing TECPLOT file


Writing TECPLOT file: egadsTessMesh_Surf_2.dat ....
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:  0.0132
Creating surface mesh ...
Surface mesh seconds:  0.001708
Recovering boundaries...
Boundary recovery seconds:  0.0387
Removing exterior tetrahedra ...
Spreading region attributes.
Exterior tets removal seconds:  0.002357
Suppressing Steiner points ...
Steiner suppression seconds:  7e-06
Recovering Delaunayness...
Delaunay recovery seconds:  0.004769
Refining mesh...
  4177 insertions, added 2144 points, 130054 tetrahedra in queue.
  1390 insertions, added 431 points, 133424 tetrahedra in queue.
  1853 insertions, added 429 points, 130659 tetrahedra in queue.
  2470 insertions, added 556 points, 115243 tetrahedra in queue.
  3293 insertions, added 486 points, 72303 tetrahedra in queue.
  4389 insertions, added 459 points, 4095 tetrahedra in queue.
Refinement seconds:  0.337445
Smoothing vertices...
Mesh smoothing seconds:  0.177375
Improving mesh...
Mesh improvement seconds:  0.006183
Jettisoning redundant points.

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

Output seconds:  0.000541
Total running seconds:  0.582438

Statistics:

  Input points: 3130
  Input facets: 6248
  Input segments: 9372
  Input holes: 2
  Input regions: 0

  Mesh points: 8153
  Mesh tetrahedra: 40225
  Mesh faces: 83575
  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: 5022

Done meshing using TetGen!
Volume mesher did not preserve surface elements - data transfer will NOT be possible.

Writing TECPLOT file: pyCAPS_Tetgen_Test.dat ....
	Binary output is not currently supported for Tecplot output
	..... switching to ASCII!
Finished writing TECPLOT file


real	0m1.274s
user	0m1.561s
sys	0m0.122s
+ 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 node elements          = 0
Number of line elements          = 0
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:  0.155171
Creating surface mesh ...
Surface mesh seconds:  0.004506
Recovering boundaries...
Boundary recovery seconds:  0.055039
Removing exterior tetrahedra ...
Spreading region attributes.
Exterior tets removal seconds:  0.003891
Recovering Delaunayness...
Delaunay recovery seconds:  0.033453
Refining mesh...
Refinement seconds:  0.133008
Smoothing vertices...
Mesh smoothing seconds:  0.146216
Improving mesh...
Mesh improvement seconds:  0.004714
Jettisoning redundant points.

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

Output seconds:  0.000955
Total running seconds:  0.537121

Statistics:

  Input points: 8995
  Input facets: 18112
  Input segments: 27104
  Input holes: 1
  Input regions: 0

  Mesh points: 7132
  Mesh tetrahedra: 27859
  Mesh faces: 60758
  Mesh faces on exterior boundary: 10080
  Mesh faces on input facets: 10080
  Mesh edges on input segments: 15120
  Steiner points inside domain: 2090

Done meshing using TetGen!
Volume mesher did not preserve surface elements - data transfer will NOT be possible.

Writing TECPLOT file: volume.dat ....
Finished writing TECPLOT file


real	0m1.187s
user	0m1.421s
sys	0m0.081s
+ 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 node elements          = 0
Number of line elements          = 0
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:  0.155525
Creating surface mesh ...
Surface mesh seconds:  0.004528
Recovering boundaries...
Boundary recovery seconds:  0.055564
Removing exterior tetrahedra ...
Spreading region attributes.
Exterior tets removal seconds:  0.002554
Recovering Delaunayness...
Delaunay recovery seconds:  0.068975
Refining mesh...
Refinement seconds:  0.263157
Smoothing vertices...
Mesh smoothing seconds:  0.302048
Improving mesh...
Mesh improvement seconds:  0.008834

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

Output seconds:  0.001267
Total running seconds:  0.862659

Statistics:

  Input points: 8995
  Input facets: 18112
  Input segments: 27104
  Input holes: 0
  Input regions: 2

  Mesh points: 13158
  Mesh tetrahedra: 55587
  Mesh faces: 119206
  Mesh faces on exterior boundary: 16064
  Mesh faces on input facets: 18112
  Mesh edges on input segments: 27104
  Steiner points inside domain: 4163

Done meshing using TetGen!

Writing TECPLOT file: volume.dat ....
Finished writing TECPLOT file


real	0m1.526s
user	0m1.758s
sys	0m0.083s
+ 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 be 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 - delaundoMesh.mesh
	Swapping y and z coordinates!

Writing TECPLOT file: delaundoMesh.dat ....
Finished writing TECPLOT file


real	0m0.391s
user	0m0.573s
sys	0m0.252s
+ 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 9.14.7
AFLR2    : Version Date   07/16/23 @ 01:42PM
AFLR2    : Compile OS     Darwin 22.6.0 arm64
AFLR2    : Compile Date   08/01/23 @ 11:39PM
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          =     0.003   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 be 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 (8.0.0) "


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.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|  2.0030e-02|   -0.385358|    2.453598|    1.625650|    5.369499|    0.360138|
|           0|           0|           1|  0.0000e+00|  0.0000e+00|  1.9722e-02|   -0.512634|    2.087781|    1.374671|    4.973554|    1.183036|
|           0|           0|           2|  0.0000e+00|  0.0000e+00|  1.9448e-02|   -0.792582|    1.733529|    1.142729|    4.657622|    3.896320|
|           0|           0|           3|  0.0000e+00|  0.0000e+00|  1.9316e-02|   -0.880738|    1.486539|    1.023158|    4.334759|   14.592265|
|           0|           0|           4|  0.0000e+00|  0.0000e+00|  1.9227e-02|   -0.987528|    1.351478|    0.932491|    4.191092|  111.166022|
|           0|           0|           5|  0.0000e+00|  0.0000e+00|  1.9166e-02|   -1.104038|    1.188715|    0.874764|    3.951825| -483.924340|
|           0|           0|           6|  0.0000e+00|  0.0000e+00|  1.9120e-02|   -1.178622|    1.124587|    0.844310|    3.820426|  127.331200|
|           0|           0|           7|  0.0000e+00|  0.0000e+00|  1.9092e-02|   -1.243517|    1.097463|    0.824869|    3.768858|   40.162273|
|           0|           0|           8|  0.0000e+00|  0.0000e+00|  1.9066e-02|   -1.287932|    1.075843|    0.810639|    3.733440|   25.154653|
|           0|           0|           9|  0.0000e+00|  0.0000e+00|  1.9047e-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	0m0.897s
user	0m0.952s
sys	0m0.450s
+ 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 9.14.7
AFLR2    : Version Date   07/16/23 @ 01:42PM
AFLR2    : Compile OS     Darwin 22.6.0 arm64
AFLR2    : Compile Date   08/01/23 @ 11:39PM
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

Writing TECPLOT file: pyCAPS_su2_aflr2.dat ....
Finished writing TECPLOT file

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 SU2 file ....
SU2 expects 2D meshes be 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 (8.0.0) "


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.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|  4.8362e-02|    0.071067|    2.739763|    1.616077|    5.599701|    0.055267|
|           0|           0|           1|  0.0000e+00|  0.0000e+00|  4.7201e-02|   -0.447576|    2.193837|    1.571349|    5.070382|    0.046028|
|           0|           0|           2|  0.0000e+00|  0.0000e+00|  4.6705e-02|   -0.561159|    2.074597|    1.490746|    4.953698|    0.033910|
|           0|           0|           3|  0.0000e+00|  0.0000e+00|  4.6428e-02|   -0.723326|    1.921155|    1.390756|    4.790278|    0.049695|
|           0|           0|           4|  0.0000e+00|  0.0000e+00|  4.6233e-02|   -0.876572|    1.825653|    1.275093|    4.637161|    0.133976|
|           0|           0|           5|  0.0000e+00|  0.0000e+00|  4.6100e-02|   -1.029177|    1.759196|    1.156078|    4.482282|    0.368542|
|           0|           0|           6|  0.0000e+00|  0.0000e+00|  4.6006e-02|   -1.215334|    1.704909|    1.114966|    4.286060|    0.974759|
|           0|           0|           7|  0.0000e+00|  0.0000e+00|  4.5943e-02|   -1.329970|    1.644937|    1.145030|    4.116982|    2.716332|
|           0|           0|           8|  0.0000e+00|  0.0000e+00|  4.5887e-02|   -1.270672|    1.570739|    1.155400|    4.139480|   16.569216|
|           0|           0|           9|  0.0000e+00|  0.0000e+00|  4.5835e-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	0m1.340s
user	0m1.418s
sys	0m0.562s
+ 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
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to 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

Writing TECPLOT file: AFLR4_Mesh.dat ....
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 9.14.7
AFLR2    : Version Date   07/16/23 @ 01:42PM
AFLR2    : Compile OS     Darwin 22.6.0 arm64
AFLR2    : Compile Date   08/01/23 @ 11:39PM
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 11.5.9
AFLR4    : Version Date   08/14/23 @ 12:27AM
AFLR4    : Compile OS     Darwin 22.6.0 arm64
AFLR4    : Compile Date   08/14/23 @ 12:31AM
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          = 38502
	Number of elements       = 221920
	Number of triangles      = 12446
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 209474
	Number of pyramids       = 0
	Number of prisms         = 0
	Number of hexahedrals    = 0

Writing TECPLOT file: AFLR3_Mesh.dat ....
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 (8.0.0) "


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_0.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.
38502 grid points.
209474 volume elements.
4 surface markers.
6594 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).
209474 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: 61.8683. Standard deviation K: 266.942.
Checking for periodicity.
Computing mesh quality statistics for the dual control volumes.
+--------------------------------------------------------------+
|           Mesh Quality Metric|        Minimum|        Maximum|
+--------------------------------------------------------------+
|    Orthogonality Angle (deg.)|        25.7373|        86.6783|
|     CV Face Area Aspect Ratio|        1.09466|        7304.38|
|           CV Sub-Volume Ratio|        1.04044|        69268.7|
+--------------------------------------------------------------+
Setting the multigrid structure.
+-------------------------------------------+
|  MG Level|       CVs|Aggl. Rate|       CFL|
+-------------------------------------------+
|         0|     38502|    1/1.00|        10|
|         1|      6385|    1/6.03|   8.24107|
|         2|      1003|    1/6.37|   6.66994|
+-------------------------------------------+
Finding max control volume width.
Semi-span length = 7.90569 m.
Wetted area = 118.038 m^2.
Area projection in the x-plane = 11.1422 m^2, y-plane = 4.96709 m^2, z-plane = 55.4183 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|  5.9888e-01|   -0.060087|    2.302216|    2.037805|    5.430808|    1.979346|
|           0|           0|           1|  0.0000e+00|  0.0000e+00|  5.9147e-01|   -0.010036|    2.482646|    2.186974|    5.492648|    2.690164|
|           0|           0|           2|  0.0000e+00|  0.0000e+00|  5.8601e-01|    0.015122|    2.560028|    2.424390|    5.513110|    4.144990|
|           0|           0|           3|  0.0000e+00|  0.0000e+00|  5.8305e-01|   -0.037042|    2.579202|    2.559777|    5.446956|    6.076344|
|           0|           0|           4|  0.0000e+00|  0.0000e+00|  5.8049e-01|   -0.081173|    2.578114|    2.616175|    5.391591|    7.699778|
|           0|           0|           5|  0.0000e+00|  0.0000e+00|  5.7810e-01|   -0.085972|    2.582416|    2.631873|    5.398797|    8.892926|
|           0|           0|           6|  0.0000e+00|  0.0000e+00|  5.7707e-01|   -0.096180|    2.574091|    2.638010|    5.401796|    9.787209|
|           0|           0|           7|  0.0000e+00|  0.0000e+00|  5.7646e-01|   -0.128924|    2.539338|    2.641609|    5.371412|   10.317352|
|           0|           0|           8|  0.0000e+00|  0.0000e+00|  5.7595e-01|   -0.184841|    2.469269|    2.632268|    5.306572|   10.430833|
|           0|           0|           9|  0.0000e+00|  0.0000e+00|  5.7551e-01|   -0.254301|    2.406660|    2.598073|    5.225779|   10.218562|

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

Maximum number of iterations reached (ITER = 10) before convergence.
+-----------------------------------------------------------------------+
|      Convergence Field     |     Value    |   Criterion  |  Converged |
+-----------------------------------------------------------------------+
|                    rms[Rho]|     -0.254301|          < -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 =  0.799154 Cd =  0.078206
Cmx =  0.000491 Cmy =  -0.204969 Cmz =  0.000591
Cx =  0.064247 Cy =  0.000689 Cz =  0.800398
Pressure Contribution
Cl_p =  0.799154 Cd_p =  0.078206
Cmx_p =  0.000491 Cmy_p =  -0.204969 Cmz_p =  0.000591
Cx_p =  0.064247 Cy_p =  0.000689 Cz_p =  0.800398
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	0m15.629s
user	0m15.502s
sys	0m0.405s
+ 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
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to 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

Writing TECPLOT file: pyCAPS_AFLR4_AFLR3.dat ....
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 9.14.7
AFLR2    : Version Date   07/16/23 @ 01:42PM
AFLR2    : Compile OS     Darwin 22.6.0 arm64
AFLR2    : Compile Date   08/01/23 @ 11:39PM
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 11.5.9
AFLR4    : Version Date   08/14/23 @ 12:27AM
AFLR4    : Compile OS     Darwin 22.6.0 arm64
AFLR4    : Compile Date   08/14/23 @ 12:31AM
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          = 55692
	Number of elements       = 322597
	Number of triangles      = 15872
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 306725
	Number of pyramids       = 0
	Number of prisms         = 0
	Number of hexahedrals    = 0

Writing TECPLOT file: pyCAPS_AFLR4_AFLR3_VolMesh.dat ....
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 (8.0.0) "


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_0.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.
55692 grid points.
306725 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).
306725 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: 58.8178. 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.)|        17.6334|        85.6893|
|     CV Face Area Aspect Ratio|        1.03551|        10026.2|
|           CV Sub-Volume Ratio|        1.03837|        55476.6|
+--------------------------------------------------------------+
Setting the multigrid structure.
+-------------------------------------------+
|  MG Level|       CVs|Aggl. Rate|       CFL|
+-------------------------------------------+
|         0|     55692|    1/1.00|        10|
|         1|      9209|    1/6.05|   8.23312|
|         2|      1415|    1/6.51|    6.6146|
+-------------------------------------------+
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|  9.1962e-01|   -0.456432|    1.874717|    1.658147|    5.034463|    0.751359|
|           0|           0|           1|  0.0000e+00|  0.0000e+00|  9.0591e-01|   -0.486415|    2.011739|    1.708650|    5.010503|    1.410135|
|           0|           0|           2|  0.0000e+00|  0.0000e+00|  8.9786e-01|   -0.426910|    2.085510|    1.930071|    5.059947|    3.183469|
|           0|           0|           3|  0.0000e+00|  0.0000e+00|  8.8482e-01|   -0.413221|    2.123390|    2.080595|    5.061524|    6.846574|
|           0|           0|           4|  0.0000e+00|  0.0000e+00|  8.8412e-01|   -0.415069|    2.144313|    2.168724|    5.045574|   12.481741|
|           0|           0|           5|  0.0000e+00|  0.0000e+00|  8.7929e-01|   -0.408728|    2.161839|    2.210835|    5.050178|   19.569122|
|           0|           0|           6|  0.0000e+00|  0.0000e+00|  8.7530e-01|   -0.400272|    2.162405|    2.231094|    5.064509|   27.279075|
|           0|           0|           7|  0.0000e+00|  0.0000e+00|  8.7163e-01|   -0.415420|    2.140420|    2.247896|    5.053374|   31.968213|
|           0|           0|           8|  0.0000e+00|  0.0000e+00|  8.6948e-01|   -0.459344|    2.092599|    2.258672|    5.008518|   30.523517|
|           0|           0|           9|  0.0000e+00|  0.0000e+00|  8.6713e-01|   -0.475584|    2.031862|    2.254220|    4.985969|   25.858195|

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

Maximum number of iterations reached (ITER = 10) before convergence.
+-----------------------------------------------------------------------+
|      Convergence Field     |     Value    |   Criterion  |  Converged |
+-----------------------------------------------------------------------+
|                    rms[Rho]|     -0.475584|          < -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 =  0.52098 Cd =  0.020148
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 (8.0.0) "


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_0.su2

---------------- Grid deformation parameters ( Zone 0 )  ----------------
Grid deformation using a linear elasticity method.


-------------------- Output Information ( Zone 0 ) ----------------------
Output mesh file name: aflr3_0.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.
55692 grid points.
306725 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).
306725 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 4.266421 seconds on 1 core.

----------------------- Write deformed grid files -----------------------
|SU2 mesh                           |aflr3_0.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_0.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.
55692 grid points.
306725 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).
306725 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.)|        17.5434|        84.9572|
|     CV Face Area Aspect Ratio|        1.03956|        11174.7|
|           CV Sub-Volume Ratio|        1.03737|        76809.1|
+--------------------------------------------------------------+
Setting the multigrid structure.
+-------------------------------------------+
|  MG Level|       CVs|Aggl. Rate|       CFL|
+-------------------------------------------+
|         0|     55692|    1/1.00|        10|
|         1|      9209|    1/6.05|   8.23312|
|         2|      1415|    1/6.51|    6.6146|
+-------------------------------------------+
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|  9.0233e-01|   -0.395911|    1.980314|    1.646923|    5.094985|    1.913176|
|           0|           0|           1|  0.0000e+00|  0.0000e+00|  8.7704e-01|   -0.263244|    2.226198|    1.949589|    5.238568|    2.547049|
|           0|           0|           2|  0.0000e+00|  0.0000e+00|  8.6689e-01|   -0.208348|    2.309357|    2.198185|    5.285085|    3.914397|
|           0|           0|           3|  0.0000e+00|  0.0000e+00|  8.6333e-01|   -0.234717|    2.345148|    2.348550|    5.245683|    5.879161|
|           0|           0|           4|  0.0000e+00|  0.0000e+00|  8.6804e-01|   -0.273135|    2.359089|    2.421633|    5.194487|    7.767865|
|           0|           0|           5|  0.0000e+00|  0.0000e+00|  8.6491e-01|   -0.284384|    2.368405|    2.446997|    5.189344|    9.270982|
|           0|           0|           6|  0.0000e+00|  0.0000e+00|  8.6383e-01|   -0.294753|    2.363090|    2.455733|    5.191507|   10.462882|
|           0|           0|           7|  0.0000e+00|  0.0000e+00|  8.6167e-01|   -0.319538|    2.340251|    2.466131|    5.173062|   11.320106|
|           0|           0|           8|  0.0000e+00|  0.0000e+00|  8.6000e-01|   -0.349768|    2.292885|    2.471955|    5.137977|   11.778124|
|           0|           0|           9|  0.0000e+00|  0.0000e+00|  8.5864e-01|   -0.372277|    2.234008|    2.463003|    5.106430|   11.856729|

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

Maximum number of iterations reached (ITER = 10) before convergence.
+-----------------------------------------------------------------------+
|      Convergence Field     |     Value    |   Criterion  |  Converged |
+-----------------------------------------------------------------------+
|                    rms[Rho]|     -0.372277|          < -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 =  0.883374 Cd =  0.074504

real	0m38.506s
user	0m37.036s
sys	0m1.395s
+ 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 be 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 - delaundoMesh.mesh
	Swapping y and z coordinates!

Writing TECPLOT file: delaundoMesh.dat ....
Finished writing TECPLOT file


Writing SU2 file ....
SU2 expects 2D meshes be 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 (8.0.0) "


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/delaundoMesh.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_delaundoMesh.dat.
Surface file name: surface_flow_delaundoMesh.
Volume file name: flow_delaundoMesh.
Restart file name: restart_flow_delaundoMesh.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|  3.4680e-02|   -1.163068|    1.073873|    1.341547|    4.312268|    0.062082|
|           0|           0|           1|  0.0000e+00|  0.0000e+00|  3.4305e-02|   -1.558471|    0.813117|    0.969484|    3.926501|    0.143132|
|           0|           0|           2|  0.0000e+00|  0.0000e+00|  3.4023e-02|   -1.599269|    0.950037|    1.012154|    3.879885|    0.386300|
|           0|           0|           3|  0.0000e+00|  0.0000e+00|  3.3681e-02|   -1.661284|    1.005970|    1.023067|    3.797319|    0.981260|
|           0|           0|           4|  0.0000e+00|  0.0000e+00|  3.3553e-02|   -1.658421|    1.009907|    0.965279|    3.792658|    2.399755|
|           0|           0|           5|  0.0000e+00|  0.0000e+00|  3.3408e-02|   -1.630602|    0.996801|    0.859556|    3.833204|    6.390579|
|           0|           0|           6|  0.0000e+00|  0.0000e+00|  3.3300e-02|   -1.628009|    1.002770|    0.822847|    3.846297|   27.872536|
|           0|           0|           7|  0.0000e+00|  0.0000e+00|  3.3232e-02|   -1.646113|    1.024424|    0.882502|    3.830202|  -48.293527|
|           0|           0|           8|  0.0000e+00|  0.0000e+00|  3.3176e-02|   -1.672152|    1.033657|    0.939200|    3.797228|  -22.113788|
|           0|           0|           9|  0.0000e+00|  0.0000e+00|  3.3128e-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_delaundoMesh.dat      |

Writing the forces breakdown file (forces_breakdown_delaundoMesh.dat).
|CSV file                           |surface_flow_delaundoMesh.csv      |

Writing the forces breakdown file (forces_breakdown_delaundoMesh.dat).
|Tecplot binary                     |flow_delaundoMesh.szplt            |

Writing the forces breakdown file (forces_breakdown_delaundoMesh.dat).
|Tecplot binary surface             |surface_flow_delaundoMesh.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_delaundoMesh.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	0m1.066s
user	0m1.181s
sys	0m0.473s
+ 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 node elements          = 0
Number of line elements          = 0
Number of triangle elements      = 4468
Number of quadrilateral elements = 0
Body 2 (of 3)
Number of nodes    = 636
Number of elements = 1268
Number of node elements          = 0
Number of line elements          = 0
Number of triangle elements      = 1268
Number of quadrilateral elements = 0
Body 3 (of 3)
Number of nodes    = 258
Number of elements = 512
Number of node elements          = 0
Number of line elements          = 0
Number of triangle elements      = 512
Number of quadrilateral elements = 0
----------------------------
Total number of nodes    = 3130
Total number of elements = 6248

Writing TECPLOT file: egadsTessMesh_Surf_0.dat ....
Finished writing TECPLOT file


Writing TECPLOT file: egadsTessMesh_Surf_1.dat ....
Finished writing TECPLOT file


Writing TECPLOT file: egadsTessMesh_Surf_2.dat ....
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:  0.013067
Creating surface mesh ...
Surface mesh seconds:  0.001821
Recovering boundaries...
Boundary recovery seconds:  0.033983
Removing exterior tetrahedra ...
Spreading region attributes.
Exterior tets removal seconds:  0.002314
Suppressing Steiner points ...
Steiner suppression seconds:  5e-06
Recovering Delaunayness...
Delaunay recovery seconds:  0.004602
Refining mesh...
  4180 insertions, added 2061 points, 130359 tetrahedra in queue.
  1391 insertions, added 425 points, 134059 tetrahedra in queue.
  1855 insertions, added 465 points, 131734 tetrahedra in queue.
  2472 insertions, added 531 points, 115562 tetrahedra in queue.
  3296 insertions, added 526 points, 67935 tetrahedra in queue.
  4393 insertions, added 433 points, 372 tetrahedra in queue.
  5856 insertions, added 571 points, 794 tetrahedra in queue.
Refinement seconds:  0.316072
Smoothing vertices...
Mesh smoothing seconds:  0.177336
Improving mesh...
Mesh improvement seconds:  0.005952
Jettisoning redundant points.

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

Output seconds:  0.000593
Total running seconds:  0.555875

Statistics:

  Input points: 3130
  Input facets: 6248
  Input segments: 9372
  Input holes: 2
  Input regions: 0

  Mesh points: 8154
  Mesh tetrahedra: 40351
  Mesh faces: 83827
  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: 5023

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 (8.0.0) "


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_0.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.
8154 grid points.
40351 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).
40351 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.)|        1.93303|        83.8522|
|     CV Face Area Aspect Ratio|        1.66492|        8220.52|
|           CV Sub-Volume Ratio|         1.0945|         249103|
+--------------------------------------------------------------+
Setting the multigrid structure.
+-------------------------------------------+
|  MG Level|       CVs|Aggl. Rate|       CFL|
+-------------------------------------------+
|         0|      8154|    1/1.00|        10|
|         1|      1365|    1/5.97|   8.26695|
|         2|       222|    1/6.15|   6.76877|
+-------------------------------------------+
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|  1.0691e-01|    0.616284|    3.048260|    2.091357|    6.107180|    1.815389|
|           0|           0|           1|  0.0000e+00|  0.0000e+00|  1.0582e-01|    0.741001|    3.258088|    2.952168|    6.243294|    2.156707|
|           0|           0|           2|  0.0000e+00|  0.0000e+00|  1.0518e-01|    0.650783|    3.322878|    3.201040|    6.147243|    3.157692|
|           0|           0|           3|  0.0000e+00|  0.0000e+00|  1.0483e-01|    0.569960|    3.293032|    3.250810|    6.036360|    4.529265|
|           0|           0|           4|  0.0000e+00|  0.0000e+00|  1.0460e-01|    0.533226|    3.191940|    3.195181|    5.994483|    5.686317|

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

Maximum number of iterations reached (ITER = 5) before convergence.
+-----------------------------------------------------------------------+
|      Convergence Field     |     Value    |   Criterion  |  Converged |
+-----------------------------------------------------------------------+
|                    rms[Rho]|      0.533226|         < -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 =  0.757437 Cd =  0.133203
Cmx =  -0.003663 Cmy =  -0.214942 Cmz =  0.000732
Cx =  0.119964 Cy =  0.000385 Cz =  0.759646

real	0m2.538s
user	0m2.685s
sys	0m0.248s
+ 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    = 3801
Number of elements = 7602
Number of node elements          = 0
Number of line elements          = 0
Number of triangle elements      = 7602
Number of quadrilateral elements = 0
Body 2 (of 2)
Number of nodes    = 5678
Number of elements = 11352
Number of node elements          = 0
Number of line elements          = 0
Number of triangle elements      = 11352
Number of quadrilateral elements = 0
----------------------------
Total number of nodes    = 9479
Total number of elements = 18954

Writing TECPLOT file: egadsTessMesh_Surf_0.dat ....
Finished writing TECPLOT file


Writing TECPLOT file: egadsTessMesh_Surf_1.dat ....
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 - 9479, elements - 18954
Getting volume mesh

Generating volume mesh using TetGen.....

Tetgen input string = pYq1.500/0.000T1.00e-16A
Delaunizing vertices...
Delaunay seconds:  0.031102
Creating surface mesh ...
Surface mesh seconds:  0.006203
Recovering boundaries...
Boundary recovery seconds:  0.075911
Removing exterior tetrahedra ...
Spreading region attributes.
Exterior tets removal seconds:  0.00528
Recovering Delaunayness...
Delaunay recovery seconds:  0.013312
Refining mesh...
  12636 insertions, added 5223 points, 13721 tetrahedra in queue.
Refinement seconds:  0.302593
Smoothing vertices...
Mesh smoothing seconds:  0.232095
Improving mesh...
Mesh improvement seconds:  0.009745
Jettisoning redundant points.

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

Output seconds:  0.001513
Total running seconds:  0.677948

Statistics:

  Input points: 9479
  Input facets: 18954
  Input segments: 28431
  Input holes: 1
  Input regions: 0

  Mesh points: 14887
  Mesh tetrahedra: 61377
  Mesh faces: 132231
  Mesh faces on exterior boundary: 18954
  Mesh faces on input facets: 18954
  Mesh edges on input segments: 28431
  Steiner points inside domain: 5408

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 (8.0.0) "


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_0.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.
14887 grid points.
61377 volume elements.
2 surface markers.
7602 boundary elements in index 0 (Marker = BC_1).
11352 boundary elements in index 1 (Marker = BC_2).
61377 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: 0.525135. Standard deviation K: 2.58749.
Checking for periodicity.
Computing mesh quality statistics for the dual control volumes.
+--------------------------------------------------------------+
|           Mesh Quality Metric|        Minimum|        Maximum|
+--------------------------------------------------------------+
|    Orthogonality Angle (deg.)|        5.16386|        84.6502|
|     CV Face Area Aspect Ratio|        1.64402|        2742.24|
|           CV Sub-Volume Ratio|              1|    1.84831e+06|
+--------------------------------------------------------------+
Setting the multigrid structure.
+-------------------------------------------+
|  MG Level|       CVs|Aggl. Rate|       CFL|
+-------------------------------------------+
|         0|     14887|    1/1.00|        10|
|         1|      2696|    1/5.52|    8.4865|
|         2|       504|    1/5.35|   7.27875|
+-------------------------------------------+
Finding max control volume width.
Semi-span length = 30 m.
Wetted area = 13592.9 m^2.
Area projection in the x-plane = 761.52 m^2, y-plane = 2060.65 m^2, z-plane = 5463.74 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|  2.0285e-01|    2.730964|    5.665275|    4.731423|    8.730439|   -0.395648|
|           0|           0|           1|  0.0000e+00|  0.0000e+00|  1.9674e-01|    3.174156|    6.235391|    5.715889|    9.174756|   -0.117154|
|           0|           0|           2|  0.0000e+00|  0.0000e+00|  1.9262e-01|    3.277847|    6.355257|    5.895285|    9.253987|   -0.024962|
|           0|           0|           3|  0.0000e+00|  0.0000e+00|  1.9106e-01|    3.266256|    6.318770|    5.740790|    9.221197|   -0.009379|
|           0|           0|           4|  0.0000e+00|  0.0000e+00|  1.9017e-01|    3.237301|    6.293206|    5.572048|    9.228342|   -0.028277|

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

Maximum number of iterations reached (ITER = 5) before convergence.
+-----------------------------------------------------------------------+
|      Convergence Field     |     Value    |   Criterion  |  Converged |
+-----------------------------------------------------------------------+
|                    rms[Rho]|        3.2373|         < -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 122 non-physical points in the solution.
Warning: 66 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 =  -3.304274 Cd =  116.853222
Cmx =  1.489219 Cmy =  8823.598105 Cmz =  124.696329
Cx =  116.866011 Cy =  1.290643 Cz =  2.815879

real	0m4.931s
user	0m6.543s
sys	0m0.875s
+ 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	0m8.419s
user	0m14.962s
sys	0m0.327s
+ 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
   (17:07:20) Running aero.csh on 2 core(s) in M0.5901A2B0_DP1
   (17:07:22) 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
   (17:07:22) Running aero.csh on 2 core(s) in M0.5901A2B0_DP1
   (17:07:24) 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
   (17:07:24) Linearizing cut-cells
   (17:07:24) ... done
   o Number of simultaneous xsensit jobs:  1
   (17:07:24) Computing gradients
   (17:07:28) ... 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
   (17:07:29) Running aero.csh on 2 core(s) in M0.5901A1.98427B0_DP1
   (17:07:30) 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
   (17:07:31) Running aero.csh on 2 core(s) in M0.5901A1.98427B0_DP1
   (17:07:33) 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
   (17:07:33) Linearizing cut-cells
   (17:07:33) ... done
   o Number of simultaneous xsensit jobs:  1
   (17:07:33) Computing gradients
   (17:07:37) ... 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
   (17:07:37) Running aero.csh on 2 core(s) in M0.5901A-0.0109917B0_DP1
   (17:07:39) 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
   (17:07:40) Running aero.csh on 2 core(s) in M0.5901A-0.0109917B0_DP1
   (17:07:41) 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
   (17:07:41) Linearizing cut-cells
   (17:07:41) ... done
   o Number of simultaneous xsensit jobs:  1
   (17:07:41) Computing gradients
   (17:07:46) ... 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
   (17:07:46) Running aero.csh on 2 core(s) in M0.5901A-0.0514929B0_DP1
   (17:07:48) 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
   (17:07:48) Running aero.csh on 2 core(s) in M0.5901A-0.0514929B0_DP1
   (17:07:50) 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
   (17:07:50) Linearizing cut-cells
   (17:07:50) ... done
   o Number of simultaneous xsensit jobs:  1
   (17:07:50) Computing gradients
   (17:07:54) ... 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
   (17:07:55) Running aero.csh on 2 core(s) in M0.5901A-0.0517603B0_DP1
   (17:07:56) 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
   (17:07:57) Running aero.csh on 2 core(s) in M0.5901A-0.0517603B0_DP1
   (17:07:59) 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
   (17:07:59) Linearizing cut-cells
   (17:07:59) ... done
   o Number of simultaneous xsensit jobs:  1
   (17:07:59) Computing gradients
   (17:08:03) ... 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	0m44.732s
user	0m30.269s
sys	0m4.678s
+ 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
   (17:08:05) Running aero.csh on 2 core(s) in M0.5901A0B0_DP1
   (17:08:12) 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
   (17:08:13) Running aero.csh on 2 core(s) in M0.5901A0B0_DP1
   (17:08:23) 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
   (17:08:24) Linearizing cut-cells
   (17:08:26) ... done
   o Number of simultaneous xsensit jobs:  1
   (17:08:26) Computing gradients
   (17:08:30) ... 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
   (17:08:31) Running aero.csh on 2 core(s) in M0.5901A0B0_DP1
   (17:08:38) 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
   (17:08:39) Running aero.csh on 2 core(s) in M0.5901A0B0_DP1
   (17:08:49) 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
   (17:08:50) Linearizing cut-cells
   (17:08:52) ... done
   o Number of simultaneous xsensit jobs:  1
   (17:08:52) Computing gradients
   (17:08:56) ... 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 [-6.51746917]
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
   (17:08:57) Running aero.csh on 2 core(s) in M0.5901A0B0_DP1
   (17:09:04) aero.csh done
 o case M0.5901A0B0_DP1, averaging data over 1 cycle(s)
>>> CL2 [0.00998116]  CL -0.099904
----------------------------------------
========================================
 o Evaluating Cart3D functionals and/or gradients
   ATTENTION: using static geometry ../inputs/Components.i.tri
   (17:09:05) Running aero.csh on 2 core(s) in M0.5901A0B0_DP1
   (17:09:16) 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
   (17:09:16) Linearizing cut-cells
   (17:09:18) ... done
   o Number of simultaneous xsensit jobs:  1
   (17:09:18) Computing gradients
   (17:09:22) ... done
 o case M0.5901A0B0_DP1, averaging data over 1 cycle(s)
>>> CL2_twist [[-0.003197]]
========================================
----------------------------------------
>>> twist [-0.14353734]
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
   (17:09:23) Running aero.csh on 2 core(s) in M0.5901A0B0_DP1
   (17:09:30) aero.csh done
 o case M0.5901A0B0_DP1, averaging data over 1 cycle(s)
>>> CL2 [6.66921728e-08]  CL -0.00023482
----------------------------------------
========================================
 o Evaluating Cart3D functionals and/or gradients
   ATTENTION: using static geometry ../inputs/Components.i.tri
   (17:09:31) Running aero.csh on 2 core(s) in M0.5901A0B0_DP1
   (17:09:41) 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
   (17:09:42) Linearizing cut-cells
   (17:09:44) ... done
   o Number of simultaneous xsensit jobs:  1
   (17:09:44) Computing gradients
   (17:09:48) ... done
 o case M0.5901A0B0_DP1, averaging data over 1 cycle(s)
>>> CL2_twist [[-8.5476956e-06]]
========================================

At iterate    2    f=  6.66922D-08    |proj g|=  8.54770D-06
----------------------------------------
>>> twist [-0.12674978]
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = Wing, index = 1
 Body size = 3.625744
 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
   (17:09:49) Running aero.csh on 2 core(s) in M0.5901A0B0_DP1
   (17:09:56) aero.csh done
 o case M0.5901A0B0_DP1, averaging data over 1 cycle(s)
>>> CL2 [5.57224144e-09]  CL 0.00010424
----------------------------------------
========================================
 o Evaluating Cart3D functionals and/or gradients
   ATTENTION: using static geometry ../inputs/Components.i.tri
   (17:09:57) Running aero.csh on 2 core(s) in M0.5901A0B0_DP1
   (17:10:07) 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
   (17:10:07) Linearizing cut-cells
   (17:10:09) ... done
   o Number of simultaneous xsensit jobs:  1
   (17:10:10) Computing gradients
   (17:10:14) ... done
 o case M0.5901A0B0_DP1, averaging data over 1 cycle(s)
>>> CL2_twist [[2.4723127e-06]]
========================================

At iterate    3    f=  5.57224D-09    |proj g|=  2.47231D-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   2.472D-06   5.572D-09
  F =   5.5722414353000007E-009

CONVERGENCE: REL_REDUCTION_OF_F_<=_FACTR*EPSMCH             
Optimization Complete
-----------------------------------
Optimized values: [-0.12674978]

real	2m10.705s
user	2m56.315s
sys	0m5.259s
+ 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: pyCAPS_AFLR4_AFLR3.dat ....
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 9.14.7
AFLR2    : Version Date   07/16/23 @ 01:42PM
AFLR2    : Compile OS     Darwin 22.6.0 arm64
AFLR2    : Compile Date   08/01/23 @ 11:39PM
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 11.5.9
AFLR4    : Version Date   08/14/23 @ 12:27AM
AFLR4    : Compile OS     Darwin 22.6.0 arm64
AFLR4    : Compile Date   08/14/23 @ 12:31AM
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          = 81189
	Number of elements       = 474220
	Number of triangles      = 15680
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 458540
	Number of pyramids       = 0
	Number of prisms         = 0
	Number of hexahedrals    = 0

Writing TECPLOT file: pyCAPS_AFLR4_AFLR3_VolMesh.dat ....
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	0m5.214s
user	0m5.194s
sys	0m0.310s
+ 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 node elements          = 0
Number of line elements          = 0
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      3.428666259746
Mass      5383.006027801
Centroid  [1.222256036872, 0.1634981473779, -4.406149178354e-11]
CG        [1.222256036872, 0.1634981473779, -4.406161310553e-11]
Ixx       22133.97306028
Iyy       23448.30046701
Izz       1389.213122561
Ixy       164.2055275652
Ixz       -7.483326592478e-06
Iyz       1.710428542532e-06
I         [22133.97306028, 23448.30046701, 1389.213122561, 164.2055275652, -7.483326592478e-06, 1.710428542532e-06]
II        [[22133.97306028, -164.2055275652, 7.483326592478e-06], [-164.2055275652, 23448.30046701, -1.710428542532e-06], [7.483326592478e-06, -1.710428542532e-06, 1389.213122561]]

real	0m3.352s
user	0m4.519s
sys	0m8.715s
+ 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	0m0.259s
user	0m0.316s
sys	0m0.067s
+ 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	0m0.403s
user	0m0.623s
sys	0m0.046s
+ 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	0m0.337s
user	0m0.494s
sys	0m0.045s
+ 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 = 368
	Number of elements = 527
	Elemental Nodes = 0
	Elemental Rods  = 0
	Elemental Tria3 = 194
	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 = 369
	Combined Number of elements = 528
	Combined Elemental Nodes = 1
	Combined Elemental Rods  = 0
	Combined Elemental Tria3 = 194
	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 369)
	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	0m6.222s
user	0m11.503s
sys	0m5.386s
+ 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	0m0.375s
user	0m0.513s
sys	0m0.098s
+ 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	0m0.473s
user	0m0.677s
sys	0m0.099s
+ status=0
+ set +x

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


=================================================
+ echo 'astros_CompositeWingFreq_PyTest.py test;'
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/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 = 402
	Number of elements = 763
	Elemental Nodes = 0
	Elemental Rods  = 0
	Elemental Tria3 = 763
	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) = 5.92088 (Hz)
Natural freq (Mode 2) = 29.77630 (Hz)
Natural freq (Mode 3) = 39.17100 (Hz)
Natural freq (Mode 4) = 77.68370 (Hz)
Natural freq (Mode 5) = 99.80360 (Hz)
Natural freq (Mode 6) = 145.83600 (Hz)
Natural freq (Mode 7) = 177.88500 (Hz)
Natural freq (Mode 8) = 237.90000 (Hz)
Natural freq (Mode 9) = 280.01500 (Hz)
Natural freq (Mode 10) = 305.57400 (Hz)
Reading Astros OUT file - extracting Eigen-Vectors!
	Number of Eigen-Vectors = 10
	Number of Grid Points = 402 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 = 402 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 = 402 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 = 402 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 = 402 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	0m16.375s
user	0m16.271s
sys	0m0.364s
+ 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	0m0.685s
user	0m0.806s
sys	0m0.182s
+ status=0
+ set +x

=================================================
CAPS verification (using pyCAPS) case astros_Flutter_15degree.py passed (as expected)
=================================================


=================================================
+ echo 'astros_MultipleLoadCase_PyTest.py test;'
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/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	0m0.561s
user	0m0.757s
sys	0m0.107s
+ 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 node elements          = 0
Number of line elements          = 0
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	0m8.247s
user	0m9.297s
sys	0m8.247s
+ 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	0m0.468s
user	0m0.672s
sys	0m0.100s
+ 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	0m0.463s
user	0m0.665s
sys	0m0.101s
+ 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	0m0.556s
user	0m0.755s
sys	0m0.105s
+ 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	0m0.478s
user	0m0.681s
sys	0m0.100s
+ 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	0m0.459s
user	0m0.664s
sys	0m0.097s
+ 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	0m0.665s
user	0m0.812s
sys	0m0.158s
+ 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 9.14.7
AFLR2    : Version Date   07/16/23 @ 01:42PM
AFLR2    : Compile OS     Darwin 22.6.0 arm64
AFLR2    : Compile Date   08/01/23 @ 11:39PM
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 11.5.9
AFLR4    : Version Date   08/14/23 @ 12:27AM
AFLR4    : Compile OS     Darwin 22.6.0 arm64
AFLR4    : Compile Date   08/14/23 @ 12:31AM
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 Sense   Edges
EGADS    :      1     Yes     1   1 2 -3 -4
EGADS    :      2     Yes     1   5 6 -7 -1
EGADS    :      3     Yes     1   -2 7 9 -8
EGADS    :      4     Yes     1   -10 -11
EGADS    :      5     Yes     1   -12 3 8 -13
EGADS    :      6     Yes     1   4 12 -14 -5
EGADS    :      7     Yes     1   -6 14 13 -9
EGADS    :      8     Yes     1   15 10 -17 -16
EGADS    :      9     Yes     1   17 11 -15 -18
EGADS    :     10     Yes     1   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=      1315      2496         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=      1298      2462         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=      9344     18684       928

AFLR4    : Curvature BG Surface Grid Generation

AFLR4    : Nodes, Faces      =      9344     18684

AFLR4    : Surface Grid Generation

AFLR4    : Generate optimal mesh on surface definition 1
AFLR2    : Nodes, Trias,Quads=      1336      2538         0
AFLR4    : Nodes, Trias,Quads=      1321      2508         0

AFLR4    : Generate optimal mesh on surface definition 2
AFLR2    : Nodes, Trias,Quads=      1340      2546         0
AFLR4    : Nodes, Trias,Quads=      1319      2504         0

AFLR4    : Generate optimal mesh on surface definition 3
AFLR2    : Nodes, Trias,Quads=      3812      7470         0
AFLR4    : Nodes, Trias,Quads=      2928      5702         0

AFLR4    : Generate optimal mesh on surface definition 4
AFLR2    : Nodes, Trias,Quads=      1337      2540         0
AFLR4    : Nodes, Trias,Quads=      1320      2506         0

AFLR4    : Generate optimal mesh on surface definition 5
AFLR2    : Nodes, Trias,Quads=      1338      2542         0
AFLR4    : Nodes, Trias,Quads=      1319      2504         0

AFLR4    : Generate optimal mesh on surface definition 6
AFLR2    : Nodes, Trias,Quads=      1340      2546         0
AFLR4    : Nodes, Trias,Quads=      1319      2504         0

AFLR4    : Generate optimal mesh on surface definition 7
AFLR2    : Nodes, Trias,Quads=       233       404         0
AFLR4    : Nodes, Trias,Quads=       210       358         0

AFLR4    : Generate optimal mesh on surface definition 8
AFLR2    : Nodes, Trias,Quads=       224       386         0
AFLR4    : Nodes, Trias,Quads=       196       330         0

AFLR4    : Generate optimal mesh on surface definition 9
AFLR2    : Nodes, Trias,Quads=        18        22         0
AFLR4    : Nodes, Trias,Quads=        12        10         0

DGEOM    : Add surface definitions to composite definition 0
DGEOM    : Glue composite surface definition 0
DGEOM    : Nodes,Faces,BEdges=      9465     18926       946

OVERALL  : CPU Time          =     0.137   seconds
Body 1 (of 1)
Number of nodes    = 9465
Number of elements = 18926
Number of node elements          = 0
Number of line elements          = 0
Number of triangle elements      = 18926
Number of quadrilateral elements = 0
----------------------------
Total number of nodes    = 9465
Total number of elements = 18926
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 9.14.7
AFLR2    : Version Date   07/16/23 @ 01:42PM
AFLR2    : Compile OS     Darwin 22.6.0 arm64
AFLR2    : Compile Date   08/01/23 @ 11:39PM
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 11.5.9
AFLR4    : Version Date   08/14/23 @ 12:27AM
AFLR4    : Compile OS     Darwin 22.6.0 arm64
AFLR4    : Compile Date   08/14/23 @ 12:31AM
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          = 58649
	Number of elements       = 337486
	Number of triangles      = 18926
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 318560
	Number of pyramids       = 0
	Number of prisms         = 0
	Number of hexahedrals    = 0
No project name ("Proj_Name") provided - A volume mesh will not be written out

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 (8.0.0) "


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_0.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.
58649 grid points.
318560 volume elements.
3 surface markers.
12526 boundary elements in index 0 (Marker = BC_1).
5702 boundary elements in index 1 (Marker = BC_2).
698 boundary elements in index 2 (Marker = BC_3).
318560 tetrahedra.
Setting point connectivity.
Renumbering points (Reverse Cuthill McKee Ordering).
Recomputing point connectivity.
Setting element connectivity.
Checking the numerical grid orientation.
All volume elements are correctly orientend.
All surface elements are correctly orientend.
Identifying edges and vertices.
Setting the control volume structure.
Volume of the computational grid: 63999.5.
Searching for the closest normal neighbors to the surfaces.
Storing a mapping from global to local point index.
Compute the surface curvature.
Max K: 83.4538. Mean K: 0.864574. Standard deviation K: 5.00994.
Checking for periodicity.
Computing mesh quality statistics for the dual control volumes.
+--------------------------------------------------------------+
|           Mesh Quality Metric|        Minimum|        Maximum|
+--------------------------------------------------------------+
|    Orthogonality Angle (deg.)|        54.7348|        86.5097|
|     CV Face Area Aspect Ratio|        1.06172|        21.5651|
|           CV Sub-Volume Ratio|              1|        8.56379|
+--------------------------------------------------------------+
Setting the multigrid structure.
+-------------------------------------------+
|  MG Level|       CVs|Aggl. Rate|       CFL|
+-------------------------------------------+
|         0|     58649|    1/1.00|        10|
|         1|      9982|    1/5.88|   8.31273|
|         2|      1772|    1/5.63|   7.00783|
+-------------------------------------------+
Finding max control volume width.
Semi-span length = 3.87298 m.
Wetted area = 9.2451 m^2.
Area projection in the x-plane = 0.651846 m^2, y-plane = 0.30478 m^2, z-plane = 4.4157 m^2.
Max. coordinate in the x-direction = 2.53651 m, y-direction = 3.87298 m, z-direction = 0.38 m.
Min. coordinate in the x-direction = 0 m, y-direction = -2.86329e-18 m, z-direction = -0.0467611 m.
Checking if Euler & 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|  9.6026e-01|   -1.350049|    0.930283|    0.592066|    4.119057|   -0.975174|
|           0|           0|           1|  0.0000e+00|  0.0000e+00|  9.5423e-01|   -1.745176|    0.769686|    0.421814|    3.710349|   -0.522367|
|           0|           0|           2|  0.0000e+00|  0.0000e+00|  9.5254e-01|   -1.753732|    0.584287|    0.243601|    3.703267|    1.886644|

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

Maximum number of iterations reached (ITER = 3) before convergence.
+-----------------------------------------------------------------------+
|      Convergence Field     |     Value    |   Criterion  |  Converged |
+-----------------------------------------------------------------------+
|                    rms[Rho]|      -1.75373|         < -14|          No|
+-----------------------------------------------------------------------+
-------------------------------------------------------------------------
+-----------------------------------------------------------------------+
|        File Writing Summary       |              Filename             |
+-----------------------------------------------------------------------+
|SU2 binary restart                 |restart_flow_aeroelasticSimple_Pressure_SA.dat|

Writing the forces breakdown file (forces_breakdown_aeroelasticSimple_Pressure_SA.dat).
|CSV file                           |surface_flow_aeroelasticSimple_Pressure_SA.csv|

Writing the forces breakdown file (forces_breakdown_aeroelasticSimple_Pressure_SA.dat).
|Tecplot binary                     |flow_aeroelasticSimple_Pressure_SA.szplt|

Writing the forces breakdown file (forces_breakdown_aeroelasticSimple_Pressure_SA.dat).
|Tecplot binary surface             |surface_flow_aeroelasticSimple_Pressure_SA.szplt|

Writing the forces breakdown file (forces_breakdown_aeroelasticSimple_Pressure_SA.dat).
+-----------------------------------------------------------------------+

--------------------------- Finalizing Solver ---------------------------
Deleted CNumerics container.
Deleted CIntegration container.
Deleted CSolver container.
Deleted CIteration container.
Deleted CInterface container.
Deleted CGeometry container.
Deleted CFreeFormDefBox class.
Deleted CSurfaceMovement class.
Deleted CVolumetricMovement class.
Deleted CConfig container.
Deleted nInst container.
Deleted COutput class.
-------------------------------------------------------------------------

------------------------- Exit Success (SU2_CFD) ------------------------


Running PostAnalysis ...... su2

Running ...... astros
Mapping Csys attributes ................
	Number of unique Csys attributes = 0

Getting FEA coordinate systems.......
	Number of coordinate systems - 0
	No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
	Number of unique capsConstraint attributes = 1
	Name = Rib_Root, index = 1
Mapping capsLoad attributes ................
	Number of unique capsLoad attributes = 1
	Name = Skin, index = 1
Mapping capsBound attributes ................
	Number of unique capsBound attributes = 3
	Name = Skin_Top, index = 1
	Name = Skin_Bottom, index = 2
	Name = Skin_Tip, index = 3
Mapping capsConnect attributes ................
	Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
	Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
	Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 2
	Name = Skin, index = 1
	Name = Rib_Root, index = 2
Setting FEA Data
	Mesh for body = 0
	Number of nodal coordinates = 180
	Number of elements = 194
	Elemental Nodes = 0
	Elemental Rods  = 0
	Elemental Tria3 = 32
	Elemental Quad4 = 162
Aero_Reference value is NULL - No aero reference parameters set

Getting FEA materials.......
	Number of materials - 1
	Material name - Madeupium
	Done getting FEA materials

Getting FEA properties.......
	Number of properties - 2
	Property name - Rib_Root
	Property name - Skin
	Done getting FEA properties
Updating mesh element types based on properties input

Getting FEA constraints.......
	Number of constraints - 1
	Constraint name - edgeConstraint
	No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement"
	Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults

Getting FEA loads.......
	Number of loads - 1
	Load name - pressureAero
	No "groupName" specified for Load tuple pressureAero, going to use load name
	Done getting FEA loads
Optimization Control tuple is NULL - Default optimization control is used

Getting FEA optimization control.......
Done getting FEA Optimization Control
Design_Variable tuple is NULL - No design variables applied
Design_Constraint tuple is NULL - No design constraints applied
Analysis tuple is NULL

Getting FEA analyses.......
	Number of analyses - 1
	Analysis name - Default
	Done getting FEA analyses
Reading SU2 AeroLoad File - surface_flow_aeroelasticSimple_Pressure_SA.csv
	Number of variables = 16
	Number of data points = 361
 CAPS Info: Bound 'Skin_Top' Normalized Integrated 'Pressure'
            Rank 0: src = 3.101438e+09, tgt = 3.101438e+09, diff = 1.877431e+02
Reading SU2 AeroLoad File - surface_flow_aeroelasticSimple_Pressure_SA.csv
	Number of variables = 16
	Number of data points = 361
 CAPS Info: Bound 'Skin_Bottom' Normalized Integrated 'Pressure'
            Rank 0: src = 3.018930e+09, tgt = 3.018930e+09, diff = 1.945207e+02
Reading SU2 AeroLoad File - surface_flow_aeroelasticSimple_Pressure_SA.csv
	Number of variables = 16
	Number of data points = 361
 CAPS Info: Bound 'Skin_Tip' Normalized Integrated 'Pressure'
            Rank 0: src = 4.374734e+07, tgt = 4.374734e+07, diff = 6.132574e-02
Extracting external pressure loads from data transfer....
	TransferName = Skin_Top
	Number of Elements = 81 (total = 81)
Extracting external pressure loads from data transfer....
	TransferName = Skin_Bottom
	Number of Elements = 81 (total = 162)
Extracting external pressure loads from data transfer....
	TransferName = Skin_Tip
	Number of Elements = 16 (total = 178)

Writing Astros grid and connectivity file (in free field format) ....
Finished writing Astros grid file

Writing subElement types (if any) - appending mesh file

Writing Astros instruction file....
	Writing analysis cards
	Writing load ADD cards
	Writing constraint cards--each subcase individually
	Writing load cards
	Writing material cards
	Writing property cards
Note: The following floating-point exceptions are signalling: IEEE_UNDERFLOW_FLAG

real	0m10.091s
user	0m10.610s
sys	0m0.889s
+ 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 9.14.7
AFLR2    : Version Date   07/16/23 @ 01:42PM
AFLR2    : Compile OS     Darwin 22.6.0 arm64
AFLR2    : Compile Date   08/01/23 @ 11:39PM
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 11.5.9
AFLR4    : Version Date   08/14/23 @ 12:27AM
AFLR4    : Compile OS     Darwin 22.6.0 arm64
AFLR4    : Compile Date   08/14/23 @ 12:31AM
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 Sense   Edges
EGADS    :      1     Yes     1   1 2 -3 -4
EGADS    :      2     Yes     1   5 6 -7 -1
EGADS    :      3     Yes     1   -2 7 9 -8
EGADS    :      4     Yes     1   -10 -11
EGADS    :      5     Yes     1   -12 3 8 -13
EGADS    :      6     Yes     1   4 12 -14 -5
EGADS    :      7     Yes     1   -6 14 13 -9
EGADS    :      8     Yes     1   15 10 -17 -16
EGADS    :      9     Yes     1   17 11 -15 -18
EGADS    :     10     Yes     1   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=      1315      2496         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=      1298      2462         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=      9344     18684       928

AFLR4    : Curvature BG Surface Grid Generation

AFLR4    : Nodes, Faces      =      9344     18684

AFLR4    : Surface Grid Generation

AFLR4    : Generate optimal mesh on surface definition 1
AFLR2    : Nodes, Trias,Quads=      1336      2538         0
AFLR4    : Nodes, Trias,Quads=      1321      2508         0

AFLR4    : Generate optimal mesh on surface definition 2
AFLR2    : Nodes, Trias,Quads=      1340      2546         0
AFLR4    : Nodes, Trias,Quads=      1319      2504         0

AFLR4    : Generate optimal mesh on surface definition 3
AFLR2    : Nodes, Trias,Quads=      3812      7470         0
AFLR4    : Nodes, Trias,Quads=      2928      5702         0

AFLR4    : Generate optimal mesh on surface definition 4
AFLR2    : Nodes, Trias,Quads=      1337      2540         0
AFLR4    : Nodes, Trias,Quads=      1320      2506         0

AFLR4    : Generate optimal mesh on surface definition 5
AFLR2    : Nodes, Trias,Quads=      1338      2542         0
AFLR4    : Nodes, Trias,Quads=      1319      2504         0

AFLR4    : Generate optimal mesh on surface definition 6
AFLR2    : Nodes, Trias,Quads=      1340      2546         0
AFLR4    : Nodes, Trias,Quads=      1319      2504         0

AFLR4    : Generate optimal mesh on surface definition 7
AFLR2    : Nodes, Trias,Quads=       233       404         0
AFLR4    : Nodes, Trias,Quads=       210       358         0

AFLR4    : Generate optimal mesh on surface definition 8
AFLR2    : Nodes, Trias,Quads=       224       386         0
AFLR4    : Nodes, Trias,Quads=       196       330         0

AFLR4    : Generate optimal mesh on surface definition 9
AFLR2    : Nodes, Trias,Quads=        18        22         0
AFLR4    : Nodes, Trias,Quads=        12        10         0

DGEOM    : Add surface definitions to composite definition 0
DGEOM    : Glue composite surface definition 0
DGEOM    : Nodes,Faces,BEdges=      9465     18926       946

OVERALL  : CPU Time          =     0.137   seconds
Body 1 (of 1)
Number of nodes    = 9465
Number of elements = 18926
Number of node elements          = 0
Number of line elements          = 0
Number of triangle elements      = 18926
Number of quadrilateral elements = 0
----------------------------
Total number of nodes    = 9465
Total number of elements = 18926
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 9.14.7
AFLR2    : Version Date   07/16/23 @ 01:42PM
AFLR2    : Compile OS     Darwin 22.6.0 arm64
AFLR2    : Compile Date   08/01/23 @ 11:39PM
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 11.5.9
AFLR4    : Version Date   08/14/23 @ 12:27AM
AFLR4    : Compile OS     Darwin 22.6.0 arm64
AFLR4    : Compile Date   08/14/23 @ 12:31AM
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          = 58649
	Number of elements       = 337486
	Number of triangles      = 18926
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 318560
	Number of pyramids       = 0
	Number of prisms         = 0
	Number of hexahedrals    = 0
No project name ("Proj_Name") provided - A volume mesh will not be written out

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 (8.0.0) "


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_0.su2

---------------- Grid deformation parameters ( Zone 0 )  ----------------
Grid deformation using a linear elasticity method.


-------------------- Output Information ( Zone 0 ) ----------------------
Output mesh file name: ../aflr3/aflr3_0.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.
58649 grid points.
318560 volume elements.
3 surface markers.
12526 boundary elements in index 0 (Marker = BC_1).
5702 boundary elements in index 1 (Marker = BC_2).
698 boundary elements in index 2 (Marker = BC_3).
318560 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 9.402171 seconds on 1 core.

----------------------- Write deformed grid files -----------------------
|SU2 mesh                           |../aflr3/aflr3_0.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_0.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.
58649 grid points.
318560 volume elements.
3 surface markers.
12526 boundary elements in index 0 (Marker = BC_1).
5702 boundary elements in index 1 (Marker = BC_2).
698 boundary elements in index 2 (Marker = BC_3).
318560 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 2 TETRAHEDRON volume elements.
There has been a re-orientation of 1 TRIANGLE surface elements.
Identifying edges and vertices.
Setting the control volume structure.
Volume of the computational grid: 63997.8.
Searching for the closest normal neighbors to the surfaces.
Storing a mapping from global to local point index.
Compute the surface curvature.
Max K: 83.9101. Mean K: 0.904589. Standard deviation K: 4.47748.
Checking for periodicity.
Computing mesh quality statistics for the dual control volumes.
+--------------------------------------------------------------+
|           Mesh Quality Metric|        Minimum|        Maximum|
+--------------------------------------------------------------+
|    Orthogonality Angle (deg.)|        37.6974|        86.4905|
|     CV Face Area Aspect Ratio|          1.068|        23.4392|
|           CV Sub-Volume Ratio|              1|        94.1303|
+--------------------------------------------------------------+
Setting the multigrid structure.
+-------------------------------------------+
|  MG Level|       CVs|Aggl. Rate|       CFL|
+-------------------------------------------+
|         0|     58649|    1/1.00|        10|
|         1|      9982|    1/5.88|   8.31273|
|         2|      1772|    1/5.63|   7.00783|
+-------------------------------------------+
Finding max control volume width.
Semi-span length = 3.89892 m.
Wetted area = 11.6364 m^2.
Area projection in the x-plane = 2.8893 m^2, y-plane = 1.28921 m^2, z-plane = 4.27235 m^2.
Max. coordinate in the x-direction = 2.53729 m, y-direction = 3.89892 m, z-direction = 0.526515 m.
Min. coordinate in the x-direction = 0.000170858 m, y-direction = -2.86329e-18 m, z-direction = -0.706552 m.
Checking if Euler & 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|  9.6165e-01|   -0.678896|    1.760803|    1.264301|    4.790210|    0.038456|
|           0|           0|           1|  0.0000e+00|  0.0000e+00|  9.5536e-01|   -1.122450|    1.498914|    1.120504|    4.348779|    0.006780|
|           0|           0|           2|  0.0000e+00|  0.0000e+00|  9.5065e-01|   -1.132662|    1.314462|    0.931988|    4.331991|    0.031135|

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

Maximum number of iterations reached (ITER = 3) before convergence.
+-----------------------------------------------------------------------+
|      Convergence Field     |     Value    |   Criterion  |  Converged |
+-----------------------------------------------------------------------+
|                    rms[Rho]|      -1.13266|         < -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	0m23.737s
user	0m23.360s
sys	0m1.677s
+ 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 9.14.7
AFLR2    : Version Date   07/16/23 @ 01:42PM
AFLR2    : Compile OS     Darwin 22.6.0 arm64
AFLR2    : Compile Date   08/01/23 @ 11:39PM
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 11.5.9
AFLR4    : Version Date   08/14/23 @ 12:27AM
AFLR4    : Compile OS     Darwin 22.6.0 arm64
AFLR4    : Compile Date   08/14/23 @ 12:31AM
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 Sense   Edges
EGADS    :      1     Yes     1   1 2 -3 -4
EGADS    :      2     Yes     1   5 6 -7 -1
EGADS    :      3     Yes     1   -2 7 9 -8
EGADS    :      4     Yes     1   -10 -11
EGADS    :      5     Yes     1   -12 3 8 -13
EGADS    :      6     Yes     1   4 12 -14 -5
EGADS    :      7     Yes     1   -6 14 13 -9
EGADS    :      8     Yes     1   15 10 -17 -16
EGADS    :      9     Yes     1   17 11 -15 -18
EGADS    :     10     Yes     1   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            = 3.22749
AFLR4    : BL Thickness                = 0
AFLR4    : Abs Min Surf Spacing        = 0.00806872
AFLR4    : Min Surf Spacing            = 0.322749
AFLR4    : Max Surf Spacing            = 2.42061
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=       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=       984      1890         0
AFLR4    : Nodes, Trias,Quads=       852      1626         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=        91       147         0
AFLR4    : Nodes, Trias,Quads=        72       109         0

AFLR4    : Generate optimal mesh on surface definition 8
AFLR2    : Nodes, Trias,Quads=        89       142         0
AFLR4    : Nodes, Trias,Quads=        70       104         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=      2648      5292       492

AFLR4    : Curvature BG Surface Grid Generation

AFLR4    : Nodes, Faces      =      2648      5292

AFLR4    : Surface Grid Generation

AFLR4    : Generate optimal mesh on surface definition 1
AFLR2    : Nodes, Trias,Quads=       385       700         0
AFLR4    : Nodes, Trias,Quads=       379       688         0

AFLR4    : Generate optimal mesh on surface definition 2
AFLR2    : Nodes, Trias,Quads=       382       694         0
AFLR4    : Nodes, Trias,Quads=       381       692         0

AFLR4    : Generate optimal mesh on surface definition 3
AFLR2    : Nodes, Trias,Quads=      1084      2088         0
AFLR4    : Nodes, Trias,Quads=      1012      1944         0

AFLR4    : Generate optimal mesh on surface definition 4
AFLR2    : Nodes, Trias,Quads=       381       692         0
AFLR4    : Nodes, Trias,Quads=       378       686         0

AFLR4    : Generate optimal mesh on surface definition 5
AFLR2    : Nodes, Trias,Quads=       383       696         0
AFLR4    : Nodes, Trias,Quads=       381       692         0

AFLR4    : Generate optimal mesh on surface definition 6
AFLR2    : Nodes, Trias,Quads=       383       696         0
AFLR4    : Nodes, Trias,Quads=       379       688         0

AFLR4    : Generate optimal mesh on surface definition 7
AFLR2    : Nodes, Trias,Quads=        99       160         0
AFLR4    : Nodes, Trias,Quads=        81       124         0

AFLR4    : Generate optimal mesh on surface definition 8
AFLR2    : Nodes, Trias,Quads=        96       154         0
AFLR4    : Nodes, Trias,Quads=        77       116         0

AFLR4    : Generate optimal mesh on surface definition 9
AFLR2    : Nodes, Trias,Quads=        11        12         0
AFLR4    : Nodes, Trias,Quads=         8         6         0

DGEOM    : Add surface definitions to composite definition 0
DGEOM    : Glue composite surface definition 0
DGEOM    : Nodes,Faces,BEdges=      2820      5636       500

OVERALL  : CPU Time          =     0.062   seconds
Body 1 (of 1)
Number of nodes    = 2820
Number of elements = 5636
Number of node elements          = 0
Number of line elements          = 0
Number of triangle elements      = 5636
Number of quadrilateral elements = 0
----------------------------
Total number of nodes    = 2820
Total number of elements = 5636
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 9.14.7
AFLR2    : Version Date   07/16/23 @ 01:42PM
AFLR2    : Compile OS     Darwin 22.6.0 arm64
AFLR2    : Compile Date   08/01/23 @ 11:39PM
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 11.5.9
AFLR4    : Version Date   08/14/23 @ 12:27AM
AFLR4    : Compile OS     Darwin 22.6.0 arm64
AFLR4    : Compile Date   08/14/23 @ 12:31AM
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          = 11908
	Number of elements       = 67561
	Number of triangles      = 5636
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 61925
	Number of pyramids       = 0
	Number of prisms         = 0
	Number of hexahedrals    = 0
No project name ("Proj_Name") provided - A volume mesh will not be written out

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 (8.0.0) "


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_0.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.
11908 grid points.
61925 volume elements.
3 surface markers.
3446 boundary elements in index 0 (Marker = BC_1).
1944 boundary elements in index 1 (Marker = BC_2).
246 boundary elements in index 2 (Marker = BC_3).
61925 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: 50.9602. Mean K: 0.841392. Standard deviation K: 3.91829.
Checking for periodicity.
Computing mesh quality statistics for the dual control volumes.
+--------------------------------------------------------------+
|           Mesh Quality Metric|        Minimum|        Maximum|
+--------------------------------------------------------------+
|    Orthogonality Angle (deg.)|        54.7347|        85.0322|
|     CV Face Area Aspect Ratio|        1.16344|        19.2647|
|           CV Sub-Volume Ratio|              1|        11.2523|
+--------------------------------------------------------------+
Setting the multigrid structure.
+-------------------------------------------+
|  MG Level|       CVs|Aggl. Rate|       CFL|
+-------------------------------------------+
|         0|     11908|    1/1.00|        10|
|         1|      2108|    1/5.65|   8.42239|
|         2|       441|    1/4.78|   7.49979|
+-------------------------------------------+
Finding max control volume width.
Semi-span length = 3.87298 m.
Wetted area = 8.34825 m^2.
Area projection in the x-plane = 0.587638 m^2, y-plane = 0.276904 m^2, z-plane = 3.94911 m^2.
Max. coordinate in the x-direction = 2.53651 m, y-direction = 3.87298 m, z-direction = 0.380417 m.
Min. coordinate in the x-direction = 0 m, y-direction = -2.85958e-18 m, z-direction = -0.0467006 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|  1.8327e-01|   -0.835779|    1.475337|    1.164402|    4.633327|   -1.069323|
|           0|           0|           1|  0.0000e+00|  0.0000e+00|  1.7823e-01|   -1.169523|    1.337951|    0.991972|    4.282357|   -0.707163|
|           0|           0|           2|  0.0000e+00|  0.0000e+00|  1.7862e-01|   -1.219552|    1.197742|    0.832257|    4.232440|    0.340563|

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

Maximum number of iterations reached (ITER = 3) before convergence.
+-----------------------------------------------------------------------+
|      Convergence Field     |     Value    |   Criterion  |  Converged |
+-----------------------------------------------------------------------+
|                    rms[Rho]|      -1.21955|         < -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 = 130
 CAPS Info: Bound 'Skin_Top' Normalized Integrated 'Pressure'
            Rank 0: src = 3.094239e+09, tgt = 3.094239e+09, diff = 1.697796e+02
Reading SU2 AeroLoad File - surface_flow_aeroelasticSimple_Iterative.csv
	Number of variables = 16
	Number of data points = 130
 CAPS Info: Bound 'Skin_Bottom' Normalized Integrated 'Pressure'
            Rank 0: src = 3.011585e+09, tgt = 3.011585e+09, diff = 1.847555e+02
Reading SU2 AeroLoad File - surface_flow_aeroelasticSimple_Iterative.csv
	Number of variables = 16
	Number of data points = 130
 CAPS Info: Bound 'Skin_Tip' Normalized Integrated 'Pressure'
            Rank 0: src = 4.097986e+07, tgt = 4.097986e+07, diff = 3.341614e-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 (8.0.0) "


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_0.su2

---------------- Grid deformation parameters ( Zone 0 )  ----------------
Grid deformation using a linear elasticity method.


-------------------- Output Information ( Zone 0 ) ----------------------
Output mesh file name: ../aflr3/aflr3_0.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.
11908 grid points.
61925 volume elements.
3 surface markers.
3446 boundary elements in index 0 (Marker = BC_1).
1944 boundary elements in index 1 (Marker = BC_2).
246 boundary elements in index 2 (Marker = BC_3).
61925 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 0.671151 seconds on 1 core.

----------------------- Write deformed grid files -----------------------
|SU2 mesh                           |../aflr3/aflr3_0.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_0.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.
11908 grid points.
61925 volume elements.
3 surface markers.
3446 boundary elements in index 0 (Marker = BC_1).
1944 boundary elements in index 1 (Marker = BC_2).
246 boundary elements in index 2 (Marker = BC_3).
61925 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 1103 TETRAHEDRON volume elements.
There has been a re-orientation of 64 TRIANGLE surface elements.
Identifying edges and vertices.
Setting the control volume structure.
Volume of the computational grid: 64440.8.
Searching for the closest normal neighbors to the surfaces.
Storing a mapping from global to local point index.
Compute the surface curvature.
Max K: 25.9358. Mean K: 0.573224. Standard deviation K: 1.86381.
Checking for periodicity.
Computing mesh quality statistics for the dual control volumes.
+--------------------------------------------------------------+
|           Mesh Quality Metric|        Minimum|        Maximum|
+--------------------------------------------------------------+
|    Orthogonality Angle (deg.)|       0.568085|        85.2217|
|     CV Face Area Aspect Ratio|        1.23147|        204.176|
|           CV Sub-Volume Ratio|              1|         197161|
+--------------------------------------------------------------+
Setting the multigrid structure.
+-------------------------------------------+
|  MG Level|       CVs|Aggl. Rate|       CFL|
+-------------------------------------------+
|         0|     11908|    1/1.00|        10|
|         1|      2088|     1/5.7|   8.39567|
|         2|       424|    1/4.92|   7.40216|
+-------------------------------------------+
Finding max control volume width.
Semi-span length = 5.04689 m.
Wetted area = 174.995 m^2.
Area projection in the x-plane = 66.7106 m^2, y-plane = 38.0858 m^2, z-plane = 6.30894 m^2.
Max. coordinate in the x-direction = 2.8362 m, y-direction = 5.04689 m, z-direction = 7.00377 m.
Min. coordinate in the x-direction = -0.81093 m, y-direction = -0.0123551 m, z-direction = -19.8631 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|  1.8908e-01|    1.720014|    4.670347|    4.852889|    7.189119|    0.036087|
|           0|           0|           1|  0.0000e+00|  0.0000e+00|  1.9128e-01|    2.050374|    4.610643|    4.787622|    7.486479|   -0.011983|
|           0|           0|           2|  0.0000e+00|  0.0000e+00|  1.9180e-01|    2.230285|    4.776975|    4.799901|    7.661578|   -0.064284|

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

Maximum number of iterations reached (ITER = 3) before convergence.
+-----------------------------------------------------------------------+
|      Convergence Field     |     Value    |   Criterion  |  Converged |
+-----------------------------------------------------------------------+
|                    rms[Rho]|       2.23028|         < -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 28 non-physical points in the solution.
Warning: 9 reconstructed states for upwinding are non-physical.

--------------------------- Finalizing Solver ---------------------------
Deleted CNumerics container.
Deleted CIntegration container.
Deleted CSolver container.
Deleted CIteration container.
Deleted CInterface container.
Deleted CGeometry container.
Deleted CFreeFormDefBox class.
Deleted CSurfaceMovement class.
Deleted CVolumetricMovement class.
Deleted CConfig container.
Deleted nInst container.
Deleted COutput class.
-------------------------------------------------------------------------

------------------------- Exit Success (SU2_CFD) ------------------------


Running PostAnalysis ...... su2

Running PreAnalysis ...... su2
Reading SU2 AeroLoad File - surface_flow_aeroelasticSimple_Iterative.csv
	Number of variables = 16
	Number of data points = 130
 CAPS Info: Bound 'Skin_Top' Normalized Integrated 'Pressure'
            Rank 0: src = 1.528910e+09, tgt = 1.528911e+09, diff = 3.948348e+02
Reading SU2 AeroLoad File - surface_flow_aeroelasticSimple_Iterative.csv
	Number of variables = 16
	Number of data points = 130
 CAPS Info: Bound 'Skin_Bottom' Normalized Integrated 'Pressure'
            Rank 0: src = 1.417409e+09, tgt = 1.417409e+09, diff = 1.691035e+02
Reading SU2 AeroLoad File - surface_flow_aeroelasticSimple_Iterative.csv
	Number of variables = 16
	Number of data points = 130
 CAPS Info: Bound 'Skin_Tip' Normalized Integrated 'Pressure'
            Rank 0: src = 2.450056e+07, tgt = 2.450056e+07, diff = 2.537084e-01
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 (8.0.0) "


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_0.su2

---------------- Grid deformation parameters ( Zone 0 )  ----------------
Grid deformation using a linear elasticity method.


-------------------- Output Information ( Zone 0 ) ----------------------
Output mesh file name: ../aflr3/aflr3_0.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.
11908 grid points.
61925 volume elements.
3 surface markers.
3446 boundary elements in index 0 (Marker = BC_1).
1944 boundary elements in index 1 (Marker = BC_2).
246 boundary elements in index 2 (Marker = BC_3).
61925 tetrahedra.

----------------------- Preprocessing computations ----------------------
Setting local point connectivity.
Checking the numerical grid orientation of the interior elements.
There has been a re-orientation of 1103 TETRAHEDRON volume elements.
There has been a re-orientation of 64 TRIANGLE surface elements.
Identify edges and vertices.
Setting the bound control volume structure.
Volume of the computational grid: 64440.8.
  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 1.620206 seconds on 1 core.

----------------------- Write deformed grid files -----------------------
|SU2 mesh                           |../aflr3/aflr3_0.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_0.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.
11908 grid points.
61925 volume elements.
3 surface markers.
3446 boundary elements in index 0 (Marker = BC_1).
1944 boundary elements in index 1 (Marker = BC_2).
246 boundary elements in index 2 (Marker = BC_3).
61925 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 32493 TETRAHEDRON volume elements.
There has been a re-orientation of 1656 TRIANGLE surface elements.
Identifying edges and vertices.
Setting the control volume structure.
Volume of the computational grid: 768397.
Searching for the closest normal neighbors to the surfaces.
Storing a mapping from global to local point index.
Compute the surface curvature.
Max K: 68.4801. Mean K: 1.48855. Standard deviation K: 5.3251.
Checking for periodicity.
Computing mesh quality statistics for the dual control volumes.
+--------------------------------------------------------------+
|           Mesh Quality Metric|        Minimum|        Maximum|
+--------------------------------------------------------------+
|    Orthogonality Angle (deg.)|       0.789304|        81.2248|
|     CV Face Area Aspect Ratio|        1.70696|        1443.72|
|           CV Sub-Volume Ratio|              1|        68046.3|
+--------------------------------------------------------------+
Setting the multigrid structure.
+-------------------------------------------+
|  MG Level|       CVs|Aggl. Rate|       CFL|
+-------------------------------------------+
|         0|     11908|    1/1.00|        10|
|         1|      2098|    1/5.68|   8.40905|
|         2|       430|    1/4.88|   7.43691|
+-------------------------------------------+
Finding max control volume width.
Semi-span length = 22.756 m.
Wetted area = 1816.34 m^2.
Area projection in the x-plane = 945.548 m^2, y-plane = 256.811 m^2, z-plane = 29.1949 m^2.
Max. coordinate in the x-direction = 2.09844 m, y-direction = 22.756 m, z-direction = 0.155398 m.
Min. coordinate in the x-direction = -3.70658 m, y-direction = -2.85958e-18 m, z-direction = -238.685 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|  1.8298e-01|    3.643452|    6.607905|    6.649404|    9.112558|   -0.075438|
|           0|           0|           1|  0.0000e+00|  0.0000e+00|  1.8918e-01|    3.973473|    6.567229|    6.628976|    9.388960|   -0.091461|
|           0|           0|           2|  0.0000e+00|  0.0000e+00|  1.9081e-01|    4.045356|    6.641283|    6.646420|    9.458361|   -0.084590|

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

Maximum number of iterations reached (ITER = 3) before convergence.
+-----------------------------------------------------------------------+
|      Convergence Field     |     Value    |   Criterion  |  Converged |
+-----------------------------------------------------------------------+
|                    rms[Rho]|       4.04536|         < -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 303 non-physical points in the solution.
Warning: 6 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 = 130
 CAPS Info: Bound 'Skin_Top' Normalized Integrated 'Pressure'
            Rank 0: src = 2.115109e+09, tgt = 2.115108e+09, diff = 6.871555e+02
Reading SU2 AeroLoad File - surface_flow_aeroelasticSimple_Iterative.csv
	Number of variables = 16
	Number of data points = 130
 CAPS Info: Bound 'Skin_Bottom' Normalized Integrated 'Pressure'
            Rank 0: src = 2.093310e+09, tgt = 2.093310e+09, diff = 2.820739e+01
Reading SU2 AeroLoad File - surface_flow_aeroelasticSimple_Iterative.csv
	Number of variables = 16
	Number of data points = 130
 CAPS Info: Bound 'Skin_Tip' Normalized Integrated 'Pressure'
            Rank 0: src = 1.865993e+07, tgt = 1.865993e+07, diff = 1.753187e-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 (8.0.0) "


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_0.su2

---------------- Grid deformation parameters ( Zone 0 )  ----------------
Grid deformation using a linear elasticity method.


-------------------- Output Information ( Zone 0 ) ----------------------
Output mesh file name: ../aflr3/aflr3_0.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.
11908 grid points.
61925 volume elements.
3 surface markers.
3446 boundary elements in index 0 (Marker = BC_1).
1944 boundary elements in index 1 (Marker = BC_2).
246 boundary elements in index 2 (Marker = BC_3).
61925 tetrahedra.

----------------------- Preprocessing computations ----------------------
Setting local point connectivity.
Checking the numerical grid orientation of the interior elements.
There has been a re-orientation of 32493 TETRAHEDRON volume elements.
There has been a re-orientation of 1656 TRIANGLE surface elements.
Identify edges and vertices.
Setting the bound control volume structure.
Volume of the computational grid: 768397.
  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 24.960697 seconds on 1 core.

----------------------- Write deformed grid files -----------------------
|SU2 mesh                           |../aflr3/aflr3_0.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_0.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.
11908 grid points.
61925 volume elements.
3 surface markers.
3446 boundary elements in index 0 (Marker = BC_1).
1944 boundary elements in index 1 (Marker = BC_2).
246 boundary elements in index 2 (Marker = BC_3).
61925 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 19828 TETRAHEDRON volume elements.
There has been a re-orientation of 2837 TRIANGLE surface elements.
Identifying edges and vertices.
Setting the control volume structure.
Volume of the computational grid: 7.14074e+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: 72.7515. Mean K: 0.679573. Standard deviation K: 2.34024.
Checking for periodicity.
Computing mesh quality statistics for the dual control volumes.
+--------------------------------------------------------------+
|           Mesh Quality Metric|        Minimum|        Maximum|
+--------------------------------------------------------------+
|    Orthogonality Angle (deg.)|       0.909038|        82.6277|
|     CV Face Area Aspect Ratio|         1.1202|         6742.5|
|           CV Sub-Volume Ratio|              1|    8.12104e+06|
+--------------------------------------------------------------+
Setting the multigrid structure.
+-------------------------------------------+
|  MG Level|       CVs|Aggl. Rate|       CFL|
+-------------------------------------------+
|         0|     11908|    1/1.00|        10|
|         1|      2108|    1/5.65|   8.42239|
|         2|       421|    1/5.01|   7.38466|
+-------------------------------------------+
Finding max control volume width.
Semi-span length = 32.1598 m.
Wetted area = 5665.54 m^2.
Area projection in the x-plane = 3299.69 m^2, y-plane = 704.462 m^2, z-plane = 28.5975 m^2.
Max. coordinate in the x-direction = 9.70414 m, y-direction = 32.1598 m, z-direction = 1.54253 m.
Min. coordinate in the x-direction = -0.0131842 m, y-direction = -0.141473 m, z-direction = -418.415 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|  1.8218e-01|    5.498950|    8.465771|    8.452556|   10.968056|   -0.037521|
|           0|           0|           1|  0.0000e+00|  0.0000e+00|  1.8849e-01|    6.017813|    8.605945|    8.542315|   11.446029|   -0.078958|
|           0|           0|           2|  0.0000e+00|  0.0000e+00|  1.9023e-01|    6.205320|    8.836920|    8.594849|   11.634731|   -0.063121|

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

Maximum number of iterations reached (ITER = 3) before convergence.
+-----------------------------------------------------------------------+
|      Convergence Field     |     Value    |   Criterion  |  Converged |
+-----------------------------------------------------------------------+
|                    rms[Rho]|       6.20532|         < -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 521 non-physical points in the solution.
Warning: 59 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 =  309.986638
Cd =  -4910.998774

real	0m38.717s
user	0m37.893s
sys	0m1.769s
+ 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 9.14.7
AFLR2    : Version Date   07/16/23 @ 01:42PM
AFLR2    : Compile OS     Darwin 22.6.0 arm64
AFLR2    : Compile Date   08/01/23 @ 11:39PM
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 11.5.9
AFLR4    : Version Date   08/14/23 @ 12:27AM
AFLR4    : Compile OS     Darwin 22.6.0 arm64
AFLR4    : Compile Date   08/14/23 @ 12:31AM
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 Sense   Edges
EGADS    :      1     Yes     1   1 2 -3 -4
EGADS    :      2     Yes     1   5 6 -7 -1
EGADS    :      3     Yes     1   -2 7 9 -8
EGADS    :      4     Yes     1   -10 -11
EGADS    :      5     Yes     1   -12 3 8 -13
EGADS    :      6     Yes     1   4 12 -14 -5
EGADS    :      7     Yes     1   -6 14 13 -9
EGADS    :      8     Yes     1   15 10 -17 -16
EGADS    :      9     Yes     1   17 11 -15 -18
EGADS    :     10     Yes     1   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            = 3.22749
AFLR4    : BL Thickness                = 0
AFLR4    : Abs Min Surf Spacing        = 0.00806872
AFLR4    : Min Surf Spacing            = 0.322749
AFLR4    : Max Surf Spacing            = 2.42061
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=       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=       984      1890         0
AFLR4    : Nodes, Trias,Quads=       852      1626         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=        91       147         0
AFLR4    : Nodes, Trias,Quads=        72       109         0

AFLR4    : Generate optimal mesh on surface definition 8
AFLR2    : Nodes, Trias,Quads=        89       142         0
AFLR4    : Nodes, Trias,Quads=        70       104         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=      2648      5292       492

AFLR4    : Curvature BG Surface Grid Generation

AFLR4    : Nodes, Faces      =      2648      5292

AFLR4    : Surface Grid Generation

AFLR4    : Generate optimal mesh on surface definition 1
AFLR2    : Nodes, Trias,Quads=       385       700         0
AFLR4    : Nodes, Trias,Quads=       379       688         0

AFLR4    : Generate optimal mesh on surface definition 2
AFLR2    : Nodes, Trias,Quads=       382       694         0
AFLR4    : Nodes, Trias,Quads=       381       692         0

AFLR4    : Generate optimal mesh on surface definition 3
AFLR2    : Nodes, Trias,Quads=      1084      2088         0
AFLR4    : Nodes, Trias,Quads=      1012      1944         0

AFLR4    : Generate optimal mesh on surface definition 4
AFLR2    : Nodes, Trias,Quads=       381       692         0
AFLR4    : Nodes, Trias,Quads=       378       686         0

AFLR4    : Generate optimal mesh on surface definition 5
AFLR2    : Nodes, Trias,Quads=       383       696         0
AFLR4    : Nodes, Trias,Quads=       381       692         0

AFLR4    : Generate optimal mesh on surface definition 6
AFLR2    : Nodes, Trias,Quads=       383       696         0
AFLR4    : Nodes, Trias,Quads=       379       688         0

AFLR4    : Generate optimal mesh on surface definition 7
AFLR2    : Nodes, Trias,Quads=        99       160         0
AFLR4    : Nodes, Trias,Quads=        81       124         0

AFLR4    : Generate optimal mesh on surface definition 8
AFLR2    : Nodes, Trias,Quads=        96       154         0
AFLR4    : Nodes, Trias,Quads=        77       116         0

AFLR4    : Generate optimal mesh on surface definition 9
AFLR2    : Nodes, Trias,Quads=        11        12         0
AFLR4    : Nodes, Trias,Quads=         8         6         0

DGEOM    : Add surface definitions to composite definition 0
DGEOM    : Glue composite surface definition 0
DGEOM    : Nodes,Faces,BEdges=      2820      5636       500

OVERALL  : CPU Time          =     0.062   seconds
Body 1 (of 1)
Number of nodes    = 2820
Number of elements = 5636
Number of node elements          = 0
Number of line elements          = 0
Number of triangle elements      = 5636
Number of quadrilateral elements = 0
----------------------------
Total number of nodes    = 2820
Total number of elements = 5636
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 9.14.7
AFLR2    : Version Date   07/16/23 @ 01:42PM
AFLR2    : Compile OS     Darwin 22.6.0 arm64
AFLR2    : Compile Date   08/01/23 @ 11:39PM
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 11.5.9
AFLR4    : Version Date   08/14/23 @ 12:27AM
AFLR4    : Compile OS     Darwin 22.6.0 arm64
AFLR4    : Compile Date   08/14/23 @ 12:31AM
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          = 11908
	Number of elements       = 67561
	Number of triangles      = 5636
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 61925
	Number of pyramids       = 0
	Number of prisms         = 0
	Number of hexahedrals    = 0
No project name ("Proj_Name") provided - A volume mesh will not be written out

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 (8.0.0) "


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_0.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.
11908 grid points.
61925 volume elements.
3 surface markers.
3446 boundary elements in index 0 (Marker = BC_1).
1944 boundary elements in index 1 (Marker = BC_2).
246 boundary elements in index 2 (Marker = BC_3).
61925 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: 50.9602. Mean K: 0.841392. Standard deviation K: 3.91829.
Checking for periodicity.
Computing mesh quality statistics for the dual control volumes.
+--------------------------------------------------------------+
|           Mesh Quality Metric|        Minimum|        Maximum|
+--------------------------------------------------------------+
|    Orthogonality Angle (deg.)|        54.7347|        85.0322|
|     CV Face Area Aspect Ratio|        1.16344|        19.2647|
|           CV Sub-Volume Ratio|              1|        11.2523|
+--------------------------------------------------------------+
Setting the multigrid structure.
+-------------------------------------------+
|  MG Level|       CVs|Aggl. Rate|       CFL|
+-------------------------------------------+
|         0|     11908|    1/1.00|        10|
|         1|      2108|    1/5.65|   8.42239|
|         2|       441|    1/4.78|   7.49979|
+-------------------------------------------+
Finding max control volume width.
Semi-span length = 3.87298 m.
Wetted area = 8.34825 m^2.
Area projection in the x-plane = 0.587638 m^2, y-plane = 0.276904 m^2, z-plane = 3.94911 m^2.
Max. coordinate in the x-direction = 2.53651 m, y-direction = 3.87298 m, z-direction = 0.380417 m.
Min. coordinate in the x-direction = 0 m, y-direction = -2.85958e-18 m, z-direction = -0.0467006 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|  1.7747e-01|   -0.835779|    1.475337|    1.164402|    4.633327|   -1.069323|
|           0|           0|           1|  0.0000e+00|  0.0000e+00|  1.7521e-01|   -1.169523|    1.337951|    0.991972|    4.282357|   -0.707163|
|           0|           0|           2|  0.0000e+00|  0.0000e+00|  1.7659e-01|   -1.219552|    1.197742|    0.832257|    4.232440|    0.340563|

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

Maximum number of iterations reached (ITER = 3) before convergence.
+-----------------------------------------------------------------------+
|      Convergence Field     |     Value    |   Criterion  |  Converged |
+-----------------------------------------------------------------------+
|                    rms[Rho]|      -1.21955|         < -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 = 130
 CAPS Info: Bound 'Skin_Top' Normalized Integrated 'Pressure'
            Rank 0: src = 3.094239e+09, tgt = 3.094240e+09, diff = 9.801585e+01
Reading SU2 AeroLoad File - surface_flow_aeroelastic_Iterative.csv
	Number of variables = 16
	Number of data points = 130
 CAPS Info: Bound 'Skin_Bottom' Normalized Integrated 'Pressure'
            Rank 0: src = 3.011585e+09, tgt = 3.011585e+09, diff = 6.390332e+01
Reading SU2 AeroLoad File - surface_flow_aeroelastic_Iterative.csv
	Number of variables = 16
	Number of data points = 130
 CAPS Info: Bound 'Skin_Tip' Normalized Integrated 'Pressure'
            Rank 0: src = 4.097986e+07, tgt = 4.097985e+07, diff = 3.286700e+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 (8.0.0) "


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_0.su2

---------------- Grid deformation parameters ( Zone 0 )  ----------------
Grid deformation using a linear elasticity method.


-------------------- Output Information ( Zone 0 ) ----------------------
Output mesh file name: ../aflr3/aflr3_0.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.
11908 grid points.
61925 volume elements.
3 surface markers.
3446 boundary elements in index 0 (Marker = BC_1).
1944 boundary elements in index 1 (Marker = BC_2).
246 boundary elements in index 2 (Marker = BC_3).
61925 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 0.681336 seconds on 1 core.

----------------------- Write deformed grid files -----------------------
|SU2 mesh                           |../aflr3/aflr3_0.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_0.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.
11908 grid points.
61925 volume elements.
3 surface markers.
3446 boundary elements in index 0 (Marker = BC_1).
1944 boundary elements in index 1 (Marker = BC_2).
246 boundary elements in index 2 (Marker = BC_3).
61925 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 25539 TETRAHEDRON volume elements.
There has been a re-orientation of 1443 TRIANGLE surface elements.
Identifying edges and vertices.
Setting the control volume structure.
Volume of the computational grid: 433151.
Searching for the closest normal neighbors to the surfaces.
Storing a mapping from global to local point index.
Compute the surface curvature.
Max K: 174.848. Mean K: 1.81464. Standard deviation K: 9.67786.
Checking for periodicity.
Computing mesh quality statistics for the dual control volumes.
+--------------------------------------------------------------+
|           Mesh Quality Metric|        Minimum|        Maximum|
+--------------------------------------------------------------+
|    Orthogonality Angle (deg.)|        1.02474|        82.8568|
|     CV Face Area Aspect Ratio|        1.27915|        746.178|
|           CV Sub-Volume Ratio|              1|        27636.8|
+--------------------------------------------------------------+
Setting the multigrid structure.
+-------------------------------------------+
|  MG Level|       CVs|Aggl. Rate|       CFL|
+-------------------------------------------+
|         0|     11908|    1/1.00|        10|
|         1|      2100|    1/5.67|   8.41172|
|         2|       419|    1/5.01|   7.37294|
+-------------------------------------------+
Finding max control volume width.
Semi-span length = 24.2419 m.
Wetted area = 3029.92 m^2.
Area projection in the x-plane = 535.45 m^2, y-plane = 986.125 m^2, z-plane = 108.557 m^2.
Max. coordinate in the x-direction = 4.83758 m, y-direction = 24.2419 m, z-direction = 26.8693 m.
Min. coordinate in the x-direction = -13.0716 m, y-direction = -0.915654 m, z-direction = -247.285 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|  1.8102e-01|    3.556322|    6.521883|    6.735668|    9.025428|   -0.363276|
|           0|           0|           1|  0.0000e+00|  0.0000e+00|  1.8790e-01|    3.775224|    6.384952|    6.551528|    9.224250|   -0.392841|
|           0|           0|           2|  0.0000e+00|  0.0000e+00|  1.8972e-01|    4.025558|    6.414910|    6.646520|    9.411271|   -0.249156|

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

Maximum number of iterations reached (ITER = 3) before convergence.
+-----------------------------------------------------------------------+
|      Convergence Field     |     Value    |   Criterion  |  Converged |
+-----------------------------------------------------------------------+
|                    rms[Rho]|       4.02556|         < -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 186 non-physical points in the solution.
Warning: 6 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 = 130
 CAPS Info: Bound 'Skin_Top' Normalized Integrated 'Pressure'
            Rank 0: src = 1.410187e+09, tgt = 1.410186e+09, diff = 3.602318e+02
Reading SU2 AeroLoad File - surface_flow_aeroelastic_Iterative.csv
	Number of variables = 16
	Number of data points = 130
 CAPS Info: Bound 'Skin_Bottom' Normalized Integrated 'Pressure'
            Rank 0: src = 8.591697e+08, tgt = 8.591703e+08, diff = 5.944963e+02
Reading SU2 AeroLoad File - surface_flow_aeroelastic_Iterative.csv
	Number of variables = 16
	Number of data points = 130
 CAPS Info: Bound 'Skin_Tip' Normalized Integrated 'Pressure'
            Rank 0: src = 8.125293e+06, tgt = 8.125314e+06, diff = 2.059804e+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 (8.0.0) "


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_0.su2

---------------- Grid deformation parameters ( Zone 0 )  ----------------
Grid deformation using a linear elasticity method.


-------------------- Output Information ( Zone 0 ) ----------------------
Output mesh file name: ../aflr3/aflr3_0.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.
11908 grid points.
61925 volume elements.
3 surface markers.
3446 boundary elements in index 0 (Marker = BC_1).
1944 boundary elements in index 1 (Marker = BC_2).
246 boundary elements in index 2 (Marker = BC_3).
61925 tetrahedra.

----------------------- Preprocessing computations ----------------------
Setting local point connectivity.
Checking the numerical grid orientation of the interior elements.
There has been a re-orientation of 25539 TETRAHEDRON volume elements.
There has been a re-orientation of 1443 TRIANGLE surface elements.
Identify edges and vertices.
Setting the bound control volume structure.
Volume of the computational grid: 433151.
  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 24.918696 seconds on 1 core.

----------------------- Write deformed grid files -----------------------
|SU2 mesh                           |../aflr3/aflr3_0.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_0.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.
11908 grid points.
61925 volume elements.
3 surface markers.
3446 boundary elements in index 0 (Marker = BC_1).
1944 boundary elements in index 1 (Marker = BC_2).
246 boundary elements in index 2 (Marker = BC_3).
61925 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 38328 TETRAHEDRON volume elements.
There has been a re-orientation of 1598 TRIANGLE surface elements.
Identifying edges and vertices.
Setting the control volume structure.
Volume of the computational grid: 7.42434e+11.
Searching for the closest normal neighbors to the surfaces.
Storing a mapping from global to local point index.
Compute the surface curvature.
Max K: 12.2371. Mean K: 0.221668. Standard deviation K: 0.773141.
Checking for periodicity.
Computing mesh quality statistics for the dual control volumes.
+--------------------------------------------------------------+
|           Mesh Quality Metric|        Minimum|        Maximum|
+--------------------------------------------------------------+
|    Orthogonality Angle (deg.)|       0.285943|        81.3626|
|     CV Face Area Aspect Ratio|        1.45886|         417020|
|           CV Sub-Volume Ratio|              1|    3.17763e+07|
+--------------------------------------------------------------+
Setting the multigrid structure.
+-------------------------------------------+
|  MG Level|       CVs|Aggl. Rate|       CFL|
+-------------------------------------------+
|         0|     11908|    1/1.00|        10|
|         1|      2110|    1/5.64|   8.42505|
|         2|       433|    1/4.87|   7.45416|
+-------------------------------------------+
Finding max control volume width.
Semi-span length = 19.7694 m.
Wetted area = 1.74808e+06 m^2.
Area projection in the x-plane = 338696 m^2, y-plane = 594656 m^2, z-plane = 40453.6 m^2.
Max. coordinate in the x-direction = 62.4212 m, y-direction = 19.7694 m, z-direction = 8016.54 m.
Min. coordinate in the x-direction = -42.5817 m, y-direction = -590.328 m, z-direction = -0.229846 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|  1.8823e-01|    7.454779|   10.421451|   10.456663|   12.923885|   -0.033773|
|           0|           0|           1|  0.0000e+00|  0.0000e+00|  1.9171e-01|    8.012761|   10.668752|   10.464329|   13.576159|   -0.033620|
|           0|           0|           2|  0.0000e+00|  0.0000e+00|  1.9283e-01|    8.111493|   10.617099|   10.585648|   13.504448|   -0.033451|

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

Maximum number of iterations reached (ITER = 3) before convergence.
+-----------------------------------------------------------------------+
|      Convergence Field     |     Value    |   Criterion  |  Converged |
+-----------------------------------------------------------------------+
|                    rms[Rho]|       8.11149|         < -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 502 non-physical points in the solution.
Warning: 50 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 = 130
 CAPS Info: Bound 'Skin_Top' Normalized Integrated 'Pressure'
            Rank 0: src = 1.517138e+09, tgt = 1.517138e+09, diff = 4.692427e+02
Reading SU2 AeroLoad File - surface_flow_aeroelastic_Iterative.csv
	Number of variables = 16
	Number of data points = 130
 CAPS Info: Bound 'Skin_Bottom' Normalized Integrated 'Pressure'
            Rank 0: src = 1.539054e+09, tgt = 1.539053e+09, diff = 2.540065e+02
Reading SU2 AeroLoad File - surface_flow_aeroelastic_Iterative.csv
	Number of variables = 16
	Number of data points = 130
 CAPS Info: Bound 'Skin_Tip' Normalized Integrated 'Pressure'
            Rank 0: src = 2.579027e+07, tgt = 2.579021e+07, diff = 5.582233e+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 (8.0.0) "


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_0.su2

---------------- Grid deformation parameters ( Zone 0 )  ----------------
Grid deformation using a linear elasticity method.


-------------------- Output Information ( Zone 0 ) ----------------------
Output mesh file name: ../aflr3/aflr3_0.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.
11908 grid points.
61925 volume elements.
3 surface markers.
3446 boundary elements in index 0 (Marker = BC_1).
1944 boundary elements in index 1 (Marker = BC_2).
246 boundary elements in index 2 (Marker = BC_3).
61925 tetrahedra.

----------------------- Preprocessing computations ----------------------
Setting local point connectivity.
Checking the numerical grid orientation of the interior elements.
There has been a re-orientation of 38328 TETRAHEDRON volume elements.
There has been a re-orientation of 1598 TRIANGLE surface elements.
Identify edges and vertices.
Setting the bound control volume structure.
Volume of the computational grid: 7.42434e+11.
  Info: Ignoring the following volume output fields/groups:
  SOLUTION
Volume output fields: COORDINATES
  Info: Ignoring the following screen output fields:
  RMS_DENSITY, RMS_MOMENTUM-X, RMS_MOMENTUM-Y, RMS_ENERGY, EFFICIENCY
Screen output fields: TIME_ITER, OUTER_ITER, INNER_ITER, CUR_TIME, TIME_STEP, WALL_TIME
  Info: Ignoring the following history output groups:
  RMS_RES, AERO_COEFF
History output group(s): ITER, TIME_DOMAIN, WALL_TIME
Warning: No (valid) fields chosen for convergence monitoring. Convergence monitoring inactive.
Warning: No (valid) fields chosen for time convergence monitoring. Time convergence monitoring inactive.

--------------------- Surface grid deformation (ZONE 0) -----------------
Performing the deformation of the surface grid.
Updating the surface coordinates from the input file.

------------------- Volumetric grid deformation (ZONE 0) ----------------
Performing the deformation of the volumetric grid.

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


Completed in 24.902843 seconds on 1 core.

----------------------- Write deformed grid files -----------------------
|SU2 mesh                           |../aflr3/aflr3_0.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_0.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.
11908 grid points.
61925 volume elements.
3 surface markers.
3446 boundary elements in index 0 (Marker = BC_1).
1944 boundary elements in index 1 (Marker = BC_2).
246 boundary elements in index 2 (Marker = BC_3).
61925 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 33081 TETRAHEDRON volume elements.
There has been a re-orientation of 2988 TRIANGLE surface elements.
Identifying edges and vertices.
Setting the control volume structure.
Volume of the computational grid: 5.8158e+15.
Searching for the closest normal neighbors to the surfaces.
Storing a mapping from global to local point index.
Compute the surface curvature.
Max K: 11.3037. Mean K: 0.182876. Standard deviation K: 0.782659.
Checking for periodicity.
Computing mesh quality statistics for the dual control volumes.
+--------------------------------------------------------------+
|           Mesh Quality Metric|        Minimum|        Maximum|
+--------------------------------------------------------------+
|    Orthogonality Angle (deg.)|       0.766697|         82.092|
|     CV Face Area Aspect Ratio|        1.79727|     8.3847e+08|
|           CV Sub-Volume Ratio|              1|    3.69912e+09|
+--------------------------------------------------------------+
Setting the multigrid structure.
+-------------------------------------------+
|  MG Level|       CVs|Aggl. Rate|       CFL|
+-------------------------------------------+
|         0|     11908|    1/1.00|        10|
|         1|      2100|    1/5.67|   8.41172|
|         2|       424|    1/4.95|   7.40216|
+-------------------------------------------+
Finding max control volume width.
Semi-span length = 404.148 m.
Wetted area = 1.0396e+06 m^2.
Area projection in the x-plane = 153335 m^2, y-plane = 367670 m^2, z-plane = 16927.4 m^2.
Max. coordinate in the x-direction = 70.0988 m, y-direction = 404.148 m, z-direction = 4.72929 m.
Min. coordinate in the x-direction = -16.5462 m, y-direction = -10.1271 m, z-direction = -5698.95 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|  1.8053e-01|   10.044140|   13.010996|   13.056978|   15.513246|   -0.018041|
|           0|           0|           1|  0.0000e+00|  0.0000e+00|  1.8755e-01|   10.667977|   13.092077|   13.232395|   16.099153|   -0.020224|
|           0|           0|           2|  0.0000e+00|  0.0000e+00|  1.8952e-01|   10.680255|   13.183304|   13.214584|   16.066809|   -0.020200|

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

Maximum number of iterations reached (ITER = 3) before convergence.
+-----------------------------------------------------------------------+
|      Convergence Field     |     Value    |   Criterion  |  Converged |
+-----------------------------------------------------------------------+
|                    rms[Rho]|       10.6803|         < -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 491 non-physical points in the solution.
Warning: 36 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	1m22.933s
user	1m26.830s
sys	0m8.101s
+ 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 9.14.7
AFLR2    : Version Date   07/16/23 @ 01:42PM
AFLR2    : Compile OS     Darwin 22.6.0 arm64
AFLR2    : Compile Date   08/01/23 @ 11:39PM
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 11.5.9
AFLR4    : Version Date   08/14/23 @ 12:27AM
AFLR4    : Compile OS     Darwin 22.6.0 arm64
AFLR4    : Compile Date   08/14/23 @ 12:31AM
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 Sense   Edges
EGADS    :      1     Yes     1   1 2 -3 -4
EGADS    :      2     Yes     1   5 6 -7 -1
EGADS    :      3     Yes     1   -2 7 9 -8
EGADS    :      4     Yes     1   -10 -11
EGADS    :      5     Yes     1   -12 3 8 -13
EGADS    :      6     Yes     1   4 12 -14 -5
EGADS    :      7     Yes     1   -6 14 13 -9
EGADS    :      8     Yes     1   15 10 -17 -16
EGADS    :      9     Yes     1   17 11 -15 -18
EGADS    :     10     Yes     1   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=      1315      2496         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=      1298      2462         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=      9344     18684       928

AFLR4    : Curvature BG Surface Grid Generation

AFLR4    : Nodes, Faces      =      9344     18684

AFLR4    : Surface Grid Generation

AFLR4    : Generate optimal mesh on surface definition 1
AFLR2    : Nodes, Trias,Quads=      1336      2538         0
AFLR4    : Nodes, Trias,Quads=      1321      2508         0

AFLR4    : Generate optimal mesh on surface definition 2
AFLR2    : Nodes, Trias,Quads=      1340      2546         0
AFLR4    : Nodes, Trias,Quads=      1319      2504         0

AFLR4    : Generate optimal mesh on surface definition 3
AFLR2    : Nodes, Trias,Quads=      3812      7470         0
AFLR4    : Nodes, Trias,Quads=      2928      5702         0

AFLR4    : Generate optimal mesh on surface definition 4
AFLR2    : Nodes, Trias,Quads=      1337      2540         0
AFLR4    : Nodes, Trias,Quads=      1320      2506         0

AFLR4    : Generate optimal mesh on surface definition 5
AFLR2    : Nodes, Trias,Quads=      1338      2542         0
AFLR4    : Nodes, Trias,Quads=      1319      2504         0

AFLR4    : Generate optimal mesh on surface definition 6
AFLR2    : Nodes, Trias,Quads=      1340      2546         0
AFLR4    : Nodes, Trias,Quads=      1319      2504         0

AFLR4    : Generate optimal mesh on surface definition 7
AFLR2    : Nodes, Trias,Quads=       233       404         0
AFLR4    : Nodes, Trias,Quads=       210       358         0

AFLR4    : Generate optimal mesh on surface definition 8
AFLR2    : Nodes, Trias,Quads=       224       386         0
AFLR4    : Nodes, Trias,Quads=       196       330         0

AFLR4    : Generate optimal mesh on surface definition 9
AFLR2    : Nodes, Trias,Quads=        18        22         0
AFLR4    : Nodes, Trias,Quads=        12        10         0

DGEOM    : Add surface definitions to composite definition 0
DGEOM    : Glue composite surface definition 0
DGEOM    : Nodes,Faces,BEdges=      9465     18926       946

OVERALL  : CPU Time          =     0.137   seconds
Body 1 (of 1)
Number of nodes    = 9465
Number of elements = 18926
Number of node elements          = 0
Number of line elements          = 0
Number of triangle elements      = 18926
Number of quadrilateral elements = 0
----------------------------
Total number of nodes    = 9465
Total number of elements = 18926
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 9.14.7
AFLR2    : Version Date   07/16/23 @ 01:42PM
AFLR2    : Compile OS     Darwin 22.6.0 arm64
AFLR2    : Compile Date   08/01/23 @ 11:39PM
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 11.5.9
AFLR4    : Version Date   08/14/23 @ 12:27AM
AFLR4    : Compile OS     Darwin 22.6.0 arm64
AFLR4    : Compile Date   08/14/23 @ 12:31AM
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          = 58649
	Number of elements       = 337486
	Number of triangles      = 18926
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 318560
	Number of pyramids       = 0
	Number of prisms         = 0
	Number of hexahedrals    = 0
No project name ("Proj_Name") provided - A volume mesh will not be written out

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_0.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.
58649 grid points.
318560 volume elements.
3 surface markers.
12526 boundary elements in index 0 (Marker = BC_1).
5702 boundary elements in index 1 (Marker = BC_2).
698 boundary elements in index 2 (Marker = BC_3).
318560 tetrahedra.
Setting point connectivity.
Renumbering points (Reverse Cuthill McKee Ordering).
Recomputing point connectivity.
Setting element connectivity.
Checking the numerical grid orientation.
All volume elements are correctly orientend.
All surface elements are correctly orientend.
Identifying edges and vertices.
Setting the control volume structure.
Volume of the computational grid: 63999.5.
Searching for the closest normal neighbors to the surfaces.
Storing a mapping from global to local point index.
Compute the surface curvature.
Max K: 83.4538. Mean K: 0.864574. Standard deviation K: 5.00994.
Checking for periodicity.
Computing mesh quality statistics for the dual control volumes.
+--------------------------------------------------------------+
|           Mesh Quality Metric|        Minimum|        Maximum|
+--------------------------------------------------------------+
|    Orthogonality Angle (deg.)|        54.7348|        86.5097|
|     CV Face Area Aspect Ratio|        1.06172|        21.5651|
|           CV Sub-Volume Ratio|              1|        8.56379|
+--------------------------------------------------------------+
Setting the multigrid structure.
+-------------------------------------------+
|  MG Level|       CVs|Aggl. Rate|       CFL|
+-------------------------------------------+
|         0|     58649|    1/1.00|        10|
|         1|      9982|    1/5.88|   8.31273|
|         2|      1772|    1/5.63|   7.00783|
+-------------------------------------------+
Finding max control volume width.
Semi-span length = 3.87298 m.
Wetted area = 9.2451 m^2.
Area projection in the x-plane = 0.651846 m^2, y-plane = 0.30478 m^2, z-plane = 4.4157 m^2.
Max. coordinate in the x-direction = 2.53651 m, y-direction = 3.87298 m, z-direction = 0.38 m.
Min. coordinate in the x-direction = 0 m, y-direction = -2.86329e-18 m, z-direction = -0.0467611 m.
Checking if Euler & 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|  9.6245e-01|   -1.350049|    0.930283|    0.592066|    4.119057|   -0.975174|
|           0|           0|           1|  0.0000e+00|  0.0000e+00|  9.5266e-01|   -1.745176|    0.769686|    0.421814|    3.710349|   -0.522367|
|           0|           0|           2|  0.0000e+00|  0.0000e+00|  9.4898e-01|   -1.753732|    0.584287|    0.243601|    3.703267|    1.886644|

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

Maximum number of iterations reached (ITER = 3) before convergence.
+-----------------------------------------------------------------------+
|      Convergence Field     |     Value    |   Criterion  |  Converged |
+-----------------------------------------------------------------------+
|                    rms[Rho]|      -1.75373|         < -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 node elements          = 0
Number of line elements          = 0
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 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 capsGroup attributes ................
	Number of unique capsGroup attributes = 2
	Name = Skin, index = 1
	Name = Rib_Root, index = 2
Setting FEA Data
	Mesh for body = 0
	Number of nodal coordinates = 12
	Number of elements = 12
	Elemental Nodes = 0
	Elemental Rods  = 0
	Elemental Tria3 = 4
	Elemental Quad4 = 8
Reading SU2 AeroLoad File - surface_flow_aeroelasticSimple_Temperature_SM.csv
	Number of variables = 16
	Number of data points = 361
 CAPS Info: Bound 'Skin_Top' Normalized Integrated 'Temperature'
            Rank 0: src = 1.497300e+03, tgt = 1.497300e+03, diff = 1.045589e-05
Mapping Csys attributes ................
	Number of unique Csys attributes = 0

Getting FEA 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 capsGroup attributes ................
	Number of unique capsGroup attributes = 2
	Name = Skin, index = 1
	Name = Rib_Root, index = 2
Setting FEA Data
	Mesh for body = 0
	Number of nodal coordinates = 12
	Number of elements = 12
	Elemental Nodes = 0
	Elemental Rods  = 0
	Elemental Tria3 = 4
	Elemental Quad4 = 8
Reading SU2 AeroLoad File - surface_flow_aeroelasticSimple_Temperature_SM.csv
	Number of variables = 16
	Number of data points = 361
 CAPS Info: Bound 'Skin_Bottom' Normalized Integrated 'Temperature'
            Rank 0: src = 1.453584e+03, tgt = 1.453584e+03, diff = 9.270707e-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 capsGroup attributes ................
	Number of unique capsGroup attributes = 2
	Name = Skin, index = 1
	Name = Rib_Root, index = 2
Setting FEA Data
	Mesh for body = 0
	Number of nodal coordinates = 12
	Number of elements = 12
	Elemental Nodes = 0
	Elemental Rods  = 0
	Elemental Tria3 = 4
	Elemental Quad4 = 8
Reading SU2 AeroLoad File - surface_flow_aeroelasticSimple_Temperature_SM.csv
	Number of variables = 16
	Number of data points = 361
 CAPS Info: Bound 'Skin_Tip' Normalized Integrated 'Temperature'
            Rank 0: src = 2.098482e+01, tgt = 2.098482e+01, diff = 5.684342e-14
Extracting external thermal loads from data transfer....
	TransferName = Skin_Top
	Number of Nodes = 9 (total = 9)
Extracting external thermal loads from data transfer....
	TransferName = Skin_Bottom
	Number of Nodes = 9 (total = 18)
Extracting external thermal loads from data transfer....
	TransferName = Skin_Tip
	Number of Nodes = 4 (total = 16)

Writing Nastran grid and connectivity file (in free field format) ....
Finished writing Nastran grid file

Writing subElement types (if any) - appending mesh file

Writing TACS instruction file....
	Writing analysis cards
	Writing load ADD cards
	Writing constraint ADD cards
	Writing load cards
	Writing constraint cards
	Writing material cards
	Writing property cards

Running PostAnalysis ...... tacs

real	0m10.600s
user	0m10.889s
sys	0m0.886s
+ 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	0m1.904s
user	0m1.134s
sys	0m0.111s
+ 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	0m0.706s
user	0m0.986s
sys	0m0.055s
+ 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	0m0.687s
user	0m0.967s
sys	0m0.054s
+ 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	0m0.593s
user	0m0.876s
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	0m4.669s
user	0m4.935s
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	0m18.706s
user	0m18.932s
sys	0m0.082s
+ 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	0m0.856s
user	0m1.113s
sys	0m0.081s
+ 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	0m3.117s
user	0m2.307s
sys	0m1.068s
+ 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 0.1685 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 0.7149 seconds
Got sol from cvxopt at 0.7238 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 1.2684 seconds
Starting iteration 1 at 1.2833 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 1.2871 seconds
Got sol from cvxopt at 1.2938 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 1.8340 seconds
Starting iteration 2 at 1.8513 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 1.8552 seconds
Got sol from cvxopt at 1.8620 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 2.4052 seconds
Starting iteration 3 at 2.4227 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 2.4267 seconds
Got sol from cvxopt at 2.4334 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 2.9739 seconds
Starting iteration 4 at 2.9916 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 2.9954 seconds
Got sol from cvxopt at 3.0022 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 3.5536 seconds
Starting iteration 5 at 3.5711 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 3.5750 seconds
Got sol from cvxopt at 3.5819 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 4.1302 seconds
Starting iteration 6 at 4.1478 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 4.1517 seconds
Got sol from cvxopt at 4.1584 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 4.6968 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	0m5.529s
user	0m3.895s
sys	0m1.857s
+ 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	0m4.822s
user	0m5.039s
sys	0m0.117s
+ 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	3m23.742s
user	3m20.086s
sys	0m3.611s
+ 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	10m54.287s
user	10m41.884s
sys	0m11.542s
+ 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	3m36.402s
user	3m32.847s
sys	0m3.493s
+ 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 46488
-rw-r--r--  1 jenkins  staff   1.2M Dec 20 15:00 ASTRO.D01
-rw-r--r--  1 jenkins  staff   277K Dec 20 15:00 ASTRO.IDX
-rwxr-xr-x  1 jenkins  staff   130K Dec 20 15:01 ESPxddm
-rwxr-xr-x  1 jenkins  staff   212K Feb 28 10:02 Slugs
-rwxr-xr-x  1 jenkins  staff    86K Feb 28 10:02 TestFit
-rwxr-xr-x  1 jenkins  staff   1.6M Dec 20 15:00 avl
-rwxr-xr-x  1 jenkins  staff    51K Feb 28 10:02 cart3dTest
-rwxr-xr-x  1 jenkins  staff    51K Mar  6 10:45 egads2cart
-rwxr-xr-x  1 jenkins  staff   403K Dec 20 15:00 friction
-rwxr-xr-x  1 jenkins  staff    10M Dec 20 15:00 mastros.exe
-rwxr-xr-x  1 jenkins  staff   749K Dec 20 15:00 mses
-rwxr-xr-x  1 jenkins  staff   1.4M Dec 20 15:00 mset
-rwxr-xr-x  1 jenkins  staff    51K Feb 28 10:02 phaseUtil
-rw-r--r--  1 jenkins  staff   1.6K Mar  6 16:58 pod.egads
-rw-r--r--  1 jenkins  staff     0B Mar  6 16:58 port7681.jrnl
-rwxr-xr-x  1 jenkins  staff   1.2M Dec 20 15:00 pplot
-rwxr-xr-x  1 jenkins  staff   1.1M Dec 20 15:00 pxplot
-rwxr-xr-x  1 jenkins  staff    68K Feb 28 10:02 sensCSM
-rwxr-xr-x  1 jenkins  staff   192K Feb 28 10:02 serveCSM
-rwxr-xr-x  1 jenkins  staff   176K Feb 28 10:02 serveESP
-rwxr-xr-x  1 jenkins  staff    52K Feb 28 10:02 vCurvature
-rwxr-xr-x  1 jenkins  staff    51K Feb 28 10:02 vGeom
-rwxr-xr-x  1 jenkins  staff    53K Feb 28 10:02 vTess
-rwxr-xr-x  1 jenkins  staff   1.7M Mar  6 10:45 vTesstatic
-rw-r--r--  1 jenkins  staff   195K Mar  6 16:58 wingMultiModel.bdf
-rwxr-xr-x  1 jenkins  staff   1.7M Dec 20 15:00 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	0m4.272s
user	0m4.317s
sys	0m0.214s
++ 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	0m3.844s
user	0m4.816s
sys	0m0.019s
++ 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	0m12.053s
user	0m19.177s
sys	0m0.036s
++ 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	0m12.011s
user	0m19.101s
sys	0m0.033s
++ 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 #66'.
[Checks API] No suitable checks publisher found.
[WS-CLEANUP] Deleting project workspace...
[WS-CLEANUP] Deferred wipeout is used...
[WS-CLEANUP] done
Finished: SUCCESS