Started by upstream project "ESP_Beta" build number 713
originally caused by:
 Started by remote host 18.18.33.14
Running as SYSTEM
[EnvInject] - Loading node environment variables.
Building remotely on viggen in workspace /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64
[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_Beta/7.8/DARWIN_ARM64
Cleaning local Directory .
Checking out svn+ssh://acdl.mit.edu/home/svnroot/OpenCSM/trunk/Jenkins at revision '2024-05-02T23:57:55.551 -0400' --quiet
Using sole credentials 3614a4cf-01de-4393-97de-73734b7dd5a2 in realm ‘svn+ssh://acdl.mit.edu’
Using sole credentials 3614a4cf-01de-4393-97de-73734b7dd5a2 in realm ‘svn+ssh://acdl.mit.edu’
At revision 2483

Checking out a fresh workspace because /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/JenkinsESP doesn't exist
Cleaning local Directory JenkinsESP
Checking out svn+ssh://acdl.mit.edu/home/svnroot/JenkinsESP at revision '2024-05-02T23:57:55.551 -0400' --quiet
Using sole credentials 3614a4cf-01de-4393-97de-73734b7dd5a2 in realm ‘svn+ssh://acdl.mit.edu’
Using sole credentials 3614a4cf-01de-4393-97de-73734b7dd5a2 in realm ‘svn+ssh://acdl.mit.edu’
At revision 860

No changes for svn+ssh://acdl.mit.edu/home/svnroot/OpenCSM/trunk/Jenkins since the previous build
Using sole credentials 3614a4cf-01de-4393-97de-73734b7dd5a2 in realm ‘svn+ssh://acdl.mit.edu’
Using sole credentials 3614a4cf-01de-4393-97de-73734b7dd5a2 in realm ‘svn+ssh://acdl.mit.edu’
[GitCheckoutListener] SCM 'hudson.scm.SubversionSCM' is not of type GitSCM
Run condition [Execution node ] enabling prebuild for step [Execute shell]
Run condition [Execution node ] enabling prebuild for step [Execute shell]
Run condition [Execution node ] enabling prebuild for step [Execute Windows batch command]
[Execution node] check if [viggen] is in [[macys, macys_VM, reynolds, reynolds-centOS7, reynolds-centOS8, reynolds-ubuntu18]]
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]
[DARWIN_ARM64] $ /bin/bash -ex /var/folders/l7/7s0m18td3fxg_w_dxpkj1d600000gp/T/jenkins16596977926862066438.sh
+ arch -arch arm64 /bin/bash -ex /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/JenkinsESP/ESP_Beta.sh
+ source /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/JenkinsESP/ESP_Env.sh
++ export OCCTREF=7.8
++ OCCTREF=7.8
++ AFLR_VERSION=11.5.14
++ SU2_VERSION=8.0.0
++ TETGEN_VERSION=1.6.0
++ VSP_VERSION=3.38.0
++ export PYTHON_VERSION=3.11.9
++ PYTHON_VERSION=3.11.9
++ export EFCOMP=gfortran
++ EFCOMP=gfortran
++ [[ viggen == \r\e\y\n\o\l\d\s ]]
++ [[ DARWIN_ARM64 == *\.\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
++ [[ DARWIN_ARM64 == \D\A\R\W\I\N\6\4\.\g\c\c ]]
++ export ESP_BLOC=/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/ESP/DARWIN_ARM64
++ ESP_BLOC=/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/ESP/DARWIN_ARM64
++ export ESP_ROOT=/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/ESP/DARWIN_ARM64
++ ESP_ROOT=/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/ESP/DARWIN_ARM64
++ export JULIA_DEPOT_PATH=/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/ESP/DARWIN_ARM64/julia
++ JULIA_DEPOT_PATH=/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/ESP/DARWIN_ARM64/julia
++ export AWAVE=awavemod.f
++ AWAVE=awavemod.f
++ export RLM_CONNECT_TIMEOUT=350
++ RLM_CONNECT_TIMEOUT=350
++ [[ 7.8 != '' ]]
++ [[ '' != '' ]]
++ [[ viggen == *\r\e\y\n\o\l\d\s* ]]
++ [[ viggen == *\m\a\c\y\s* ]]
++ [[ viggen == *\v\i\g\g\e\n* ]]
++ export EMPnumProc=2
++ EMPnumProc=2
++ export OMP_NUM_THREADS=2
++ OMP_NUM_THREADS=2
++ source /Users/jenkins/.bash_profile
++++ /opt/homebrew/bin/brew shellenv
+++ eval 'export HOMEBREW_PREFIX="/opt/homebrew";
export HOMEBREW_CELLAR="/opt/homebrew/Cellar";
export HOMEBREW_REPOSITORY="/opt/homebrew";
export PATH="/opt/homebrew/bin:/opt/homebrew/sbin${PATH+:$PATH}";
export MANPATH="/opt/homebrew/share/man${MANPATH+:$MANPATH}:";
export INFOPATH="/opt/homebrew/share/info:${INFOPATH:-}";'
++++ export HOMEBREW_PREFIX=/opt/homebrew
++++ HOMEBREW_PREFIX=/opt/homebrew
++++ export HOMEBREW_CELLAR=/opt/homebrew/Cellar
++++ HOMEBREW_CELLAR=/opt/homebrew/Cellar
++++ export HOMEBREW_REPOSITORY=/opt/homebrew
++++ HOMEBREW_REPOSITORY=/opt/homebrew
++++ export PATH=/opt/homebrew/bin:/opt/homebrew/sbin:/opt/intel/oneapi/dev-utilities/2021.5.0/bin:/usr/bin:/bin:/usr/sbin:/sbin
++++ PATH=/opt/homebrew/bin:/opt/homebrew/sbin:/opt/intel/oneapi/dev-utilities/2021.5.0/bin:/usr/bin:/bin:/usr/sbin:/sbin
++++ export MANPATH=/opt/homebrew/share/man:
++++ MANPATH=/opt/homebrew/share/man:
++++ export INFOPATH=/opt/homebrew/share/info:
++++ INFOPATH=/opt/homebrew/share/info:
+++ [[ -r /opt/homebrew/etc/profile.d/bash_completion.sh ]]
+++ . /opt/homebrew/etc/profile.d/bash_completion.sh
++++ '[' -z '3.2.57(1)-release' -o -z '' -o -n '' ']'
++++ return
+++ export NETCDF_PATH=/opt/homebrew
+++ NETCDF_PATH=/opt/homebrew
++ [[ viggen == *\m\a\c\y\s* ]]
++ export PATH=/opt/homebrew/bin:/opt/homebrew/sbin:/opt/intel/oneapi/dev-utilities/2021.5.0/bin:/usr/bin:/bin:/usr/sbin:/sbin:/opt/homebrew/bin/
++ PATH=/opt/homebrew/bin:/opt/homebrew/sbin:/opt/intel/oneapi/dev-utilities/2021.5.0/bin:/usr/bin:/bin:/usr/sbin:/sbin:/opt/homebrew/bin/
++ [[ viggen == \m\a\c\y\s ]]
++ export CASARCH=.
++ CASARCH=.
++ '[' '!' -z '' ']'
+++ ls -d /Users/jenkins/util/ESP/OpenCASCADE-7.8.0
++ export CASROOT=/Users/jenkins/util/ESP/OpenCASCADE-7.8.0
++ CASROOT=/Users/jenkins/util/ESP/OpenCASCADE-7.8.0
++ export UDUNITS2_XML_PATH=/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/ESP/udunits/udunits2.xml
++ UDUNITS2_XML_PATH=/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/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_Beta/7.8/DARWIN_ARM64/ESP/DARWIN_ARM64/lib:/Users/jenkins/util/ESP/OpenCASCADE-7.8.0/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_Beta/7.8/DARWIN_ARM64/ESP/DARWIN_ARM64/lib:/Users/jenkins/util/ESP/OpenCASCADE-7.8.0/lib:/opt/intel/oneapi/tbb/2021.5.0/env/../lib:/opt/intel/oneapi/mkl/2022.0.0/lib
++ export AFLR=/Users/jenkins/util/AFLR/aflr_lib_11.5.14
++ AFLR=/Users/jenkins/util/AFLR/aflr_lib_11.5.14
++ [[ viggen == *\m\a\c\y\s* ]]
++ export AFLR_ARCH=MacOSX-arm64
++ AFLR_ARCH=MacOSX-arm64
++ export ASTROS_ROOT=/Users/jenkins/util/astros/Astros/Darwin-64bit
++ ASTROS_ROOT=/Users/jenkins/util/astros/Astros/Darwin-64bit
++ export PATH=/Users/jenkins/util/astros/Astros/Darwin-64bit:/opt/homebrew/bin:/opt/homebrew/sbin:/opt/intel/oneapi/dev-utilities/2021.5.0/bin:/usr/bin:/bin:/usr/sbin:/sbin:/opt/homebrew/bin/
++ PATH=/Users/jenkins/util/astros/Astros/Darwin-64bit:/opt/homebrew/bin:/opt/homebrew/sbin:/opt/intel/oneapi/dev-utilities/2021.5.0/bin:/usr/bin:/bin:/usr/sbin:/sbin:/opt/homebrew/bin/
++ export CART3D=/Users/jenkins/util/cart3d/cart3d_v1.5.9_OSX64_ICC--22.11.16
++ CART3D=/Users/jenkins/util/cart3d/cart3d_v1.5.9_OSX64_ICC--22.11.16
++ export CART3D_ARCH=OSX64_ICC
++ CART3D_ARCH=OSX64_ICC
++ export PATH=/Users/jenkins/util/cart3d/cart3d_v1.5.9_OSX64_ICC--22.11.16/bin/OSX64_ICC/:/Users/jenkins/util/astros/Astros/Darwin-64bit:/opt/homebrew/bin:/opt/homebrew/sbin:/opt/intel/oneapi/dev-utilities/2021.5.0/bin:/usr/bin:/bin:/usr/sbin:/sbin:/opt/homebrew/bin/
++ PATH=/Users/jenkins/util/cart3d/cart3d_v1.5.9_OSX64_ICC--22.11.16/bin/OSX64_ICC/:/Users/jenkins/util/astros/Astros/Darwin-64bit:/opt/homebrew/bin:/opt/homebrew/sbin:/opt/intel/oneapi/dev-utilities/2021.5.0/bin:/usr/bin:/bin:/usr/sbin:/sbin:/opt/homebrew/bin/
++ export PATH=/Users/jenkins/util/cart3d/cart3d_v1.5.9_OSX64_ICC--22.11.16/bin:/Users/jenkins/util/cart3d/cart3d_v1.5.9_OSX64_ICC--22.11.16/bin/OSX64_ICC/:/Users/jenkins/util/astros/Astros/Darwin-64bit:/opt/homebrew/bin:/opt/homebrew/sbin:/opt/intel/oneapi/dev-utilities/2021.5.0/bin:/usr/bin:/bin:/usr/sbin:/sbin:/opt/homebrew/bin/
++ PATH=/Users/jenkins/util/cart3d/cart3d_v1.5.9_OSX64_ICC--22.11.16/bin:/Users/jenkins/util/cart3d/cart3d_v1.5.9_OSX64_ICC--22.11.16/bin/OSX64_ICC/:/Users/jenkins/util/astros/Astros/Darwin-64bit:/opt/homebrew/bin:/opt/homebrew/sbin:/opt/intel/oneapi/dev-utilities/2021.5.0/bin:/usr/bin:/bin:/usr/sbin:/sbin:/opt/homebrew/bin/
++ export PATH=/Users/jenkins/util/delaundo/delaundo/src:/Users/jenkins/util/cart3d/cart3d_v1.5.9_OSX64_ICC--22.11.16/bin:/Users/jenkins/util/cart3d/cart3d_v1.5.9_OSX64_ICC--22.11.16/bin/OSX64_ICC/:/Users/jenkins/util/astros/Astros/Darwin-64bit:/opt/homebrew/bin:/opt/homebrew/sbin:/opt/intel/oneapi/dev-utilities/2021.5.0/bin:/usr/bin:/bin:/usr/sbin:/sbin:/opt/homebrew/bin/
++ PATH=/Users/jenkins/util/delaundo/delaundo/src:/Users/jenkins/util/cart3d/cart3d_v1.5.9_OSX64_ICC--22.11.16/bin:/Users/jenkins/util/cart3d/cart3d_v1.5.9_OSX64_ICC--22.11.16/bin/OSX64_ICC/:/Users/jenkins/util/astros/Astros/Darwin-64bit:/opt/homebrew/bin:/opt/homebrew/sbin:/opt/intel/oneapi/dev-utilities/2021.5.0/bin:/usr/bin:/bin:/usr/sbin:/sbin:/opt/homebrew/bin/
++ export VSP3_ROOT=/Users/jenkins/util/OpenVSP/OpenVSP-3.38.0-MacOS
++ VSP3_ROOT=/Users/jenkins/util/OpenVSP/OpenVSP-3.38.0-MacOS
++ export PATH=/Users/jenkins/util/refine/build_parallel/install/bin:/Users/jenkins/util/delaundo/delaundo/src:/Users/jenkins/util/cart3d/cart3d_v1.5.9_OSX64_ICC--22.11.16/bin:/Users/jenkins/util/cart3d/cart3d_v1.5.9_OSX64_ICC--22.11.16/bin/OSX64_ICC/:/Users/jenkins/util/astros/Astros/Darwin-64bit:/opt/homebrew/bin:/opt/homebrew/sbin:/opt/intel/oneapi/dev-utilities/2021.5.0/bin:/usr/bin:/bin:/usr/sbin:/sbin:/opt/homebrew/bin/
++ PATH=/Users/jenkins/util/refine/build_parallel/install/bin:/Users/jenkins/util/delaundo/delaundo/src:/Users/jenkins/util/cart3d/cart3d_v1.5.9_OSX64_ICC--22.11.16/bin:/Users/jenkins/util/cart3d/cart3d_v1.5.9_OSX64_ICC--22.11.16/bin/OSX64_ICC/:/Users/jenkins/util/astros/Astros/Darwin-64bit:/opt/homebrew/bin:/opt/homebrew/sbin:/opt/intel/oneapi/dev-utilities/2021.5.0/bin:/usr/bin:/bin:/usr/sbin:/sbin:/opt/homebrew/bin/
++ [[ viggen == \m\a\c\y\s ]]
++ [[ viggen == \v\i\g\g\e\n ]]
++ export SEACAS=/Users/jenkins/util/sandialabs/seacas
++ SEACAS=/Users/jenkins/util/sandialabs/seacas
++ [[ viggen == \v\i\g\g\e\n ]]
++ export NETCDFINC=/opt/homebrew/include
++ NETCDFINC=/opt/homebrew/include
++ export SU2_HOME=/Users/jenkins/util/SU2/SU2-v8.0.0
++ SU2_HOME=/Users/jenkins/util/SU2/SU2-v8.0.0
++ export SU2_RUN=/Users/jenkins/util/SU2/SU2-v8.0.0/bin
++ SU2_RUN=/Users/jenkins/util/SU2/SU2-v8.0.0/bin
++ export PATH=/Users/jenkins/util/refine/build_parallel/install/bin:/Users/jenkins/util/delaundo/delaundo/src:/Users/jenkins/util/cart3d/cart3d_v1.5.9_OSX64_ICC--22.11.16/bin:/Users/jenkins/util/cart3d/cart3d_v1.5.9_OSX64_ICC--22.11.16/bin/OSX64_ICC/:/Users/jenkins/util/astros/Astros/Darwin-64bit:/opt/homebrew/bin:/opt/homebrew/sbin:/opt/intel/oneapi/dev-utilities/2021.5.0/bin:/usr/bin:/bin:/usr/sbin:/sbin:/opt/homebrew/bin/:/Users/jenkins/util/SU2/SU2-v8.0.0/bin
++ PATH=/Users/jenkins/util/refine/build_parallel/install/bin:/Users/jenkins/util/delaundo/delaundo/src:/Users/jenkins/util/cart3d/cart3d_v1.5.9_OSX64_ICC--22.11.16/bin:/Users/jenkins/util/cart3d/cart3d_v1.5.9_OSX64_ICC--22.11.16/bin/OSX64_ICC/:/Users/jenkins/util/astros/Astros/Darwin-64bit:/opt/homebrew/bin:/opt/homebrew/sbin:/opt/intel/oneapi/dev-utilities/2021.5.0/bin:/usr/bin:/bin:/usr/sbin:/sbin:/opt/homebrew/bin/:/Users/jenkins/util/SU2/SU2-v8.0.0/bin
++ export PYTHONPATH=:/Users/jenkins/util/SU2/SU2-v8.0.0/bin
++ PYTHONPATH=:/Users/jenkins/util/SU2/SU2-v8.0.0/bin
++ export TETGEN=/Users/jenkins/util/tetgen/tetgen1.6.0
++ TETGEN=/Users/jenkins/util/tetgen/tetgen1.6.0
++ export PATH=/Users/jenkins/util/tsfoil:/Users/jenkins/util/refine/build_parallel/install/bin:/Users/jenkins/util/delaundo/delaundo/src:/Users/jenkins/util/cart3d/cart3d_v1.5.9_OSX64_ICC--22.11.16/bin:/Users/jenkins/util/cart3d/cart3d_v1.5.9_OSX64_ICC--22.11.16/bin/OSX64_ICC/:/Users/jenkins/util/astros/Astros/Darwin-64bit:/opt/homebrew/bin:/opt/homebrew/sbin:/opt/intel/oneapi/dev-utilities/2021.5.0/bin:/usr/bin:/bin:/usr/sbin:/sbin:/opt/homebrew/bin/:/Users/jenkins/util/SU2/SU2-v8.0.0/bin
++ PATH=/Users/jenkins/util/tsfoil:/Users/jenkins/util/refine/build_parallel/install/bin:/Users/jenkins/util/delaundo/delaundo/src:/Users/jenkins/util/cart3d/cart3d_v1.5.9_OSX64_ICC--22.11.16/bin:/Users/jenkins/util/cart3d/cart3d_v1.5.9_OSX64_ICC--22.11.16/bin/OSX64_ICC/:/Users/jenkins/util/astros/Astros/Darwin-64bit:/opt/homebrew/bin:/opt/homebrew/sbin:/opt/intel/oneapi/dev-utilities/2021.5.0/bin:/usr/bin:/bin:/usr/sbin:/sbin:/opt/homebrew/bin/:/Users/jenkins/util/SU2/SU2-v8.0.0/bin
++ '[' -d /Users/jenkins/util/cart3d/cart3d_v1.5.9_OSX64_ICC--22.11.16 ']'
+++ perl -I/Users/jenkins/util/cart3d/cart3d_v1.5.9_OSX64_ICC--22.11.16/lib/perl/lib/perl5 -Mlocal::lib=/Users/jenkins/util/cart3d/cart3d_v1.5.9_OSX64_ICC--22.11.16/lib/perl
++ eval 'PATH="/Users/jenkins/util/cart3d/cart3d_v1.5.9_OSX64_ICC--22.11.16/lib/perl/bin${PATH:+:${PATH}}"; export PATH;
PERL5LIB="/Users/jenkins/util/cart3d/cart3d_v1.5.9_OSX64_ICC--22.11.16/lib/perl/lib/perl5${PERL5LIB:+:${PERL5LIB}}"; export PERL5LIB;
PERL_LOCAL_LIB_ROOT="/Users/jenkins/util/cart3d/cart3d_v1.5.9_OSX64_ICC--22.11.16/lib/perl${PERL_LOCAL_LIB_ROOT:+:${PERL_LOCAL_LIB_ROOT}}"; export PERL_LOCAL_LIB_ROOT;
PERL_MB_OPT="--install_base \"/Users/jenkins/util/cart3d/cart3d_v1.5.9_OSX64_ICC--22.11.16/lib/perl\""; export PERL_MB_OPT;
PERL_MM_OPT="INSTALL_BASE=/Users/jenkins/util/cart3d/cart3d_v1.5.9_OSX64_ICC--22.11.16/lib/perl"; export PERL_MM_OPT;'
+++ PATH=/Users/jenkins/util/cart3d/cart3d_v1.5.9_OSX64_ICC--22.11.16/lib/perl/bin:/Users/jenkins/util/tsfoil:/Users/jenkins/util/refine/build_parallel/install/bin:/Users/jenkins/util/delaundo/delaundo/src:/Users/jenkins/util/cart3d/cart3d_v1.5.9_OSX64_ICC--22.11.16/bin:/Users/jenkins/util/cart3d/cart3d_v1.5.9_OSX64_ICC--22.11.16/bin/OSX64_ICC/:/Users/jenkins/util/astros/Astros/Darwin-64bit:/opt/homebrew/bin:/opt/homebrew/sbin:/opt/intel/oneapi/dev-utilities/2021.5.0/bin:/usr/bin:/bin:/usr/sbin:/sbin:/opt/homebrew/bin/:/Users/jenkins/util/SU2/SU2-v8.0.0/bin
+++ export PATH
+++ PERL5LIB=/Users/jenkins/util/cart3d/cart3d_v1.5.9_OSX64_ICC--22.11.16/lib/perl/lib/perl5
+++ export PERL5LIB
+++ PERL_LOCAL_LIB_ROOT=/Users/jenkins/util/cart3d/cart3d_v1.5.9_OSX64_ICC--22.11.16/lib/perl
+++ export PERL_LOCAL_LIB_ROOT
+++ PERL_MB_OPT='--install_base "/Users/jenkins/util/cart3d/cart3d_v1.5.9_OSX64_ICC--22.11.16/lib/perl"'
+++ export PERL_MB_OPT
+++ PERL_MM_OPT=INSTALL_BASE=/Users/jenkins/util/cart3d/cart3d_v1.5.9_OSX64_ICC--22.11.16/lib/perl
+++ export PERL_MM_OPT
++ export PATH=/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/ESP/DARWIN_ARM64/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_Beta/7.8/DARWIN_ARM64/ESP/DARWIN_ARM64/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_Beta/7.8/DARWIN_ARM64/ESP/DARWIN_ARM64/test:/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/ESP/DARWIN_ARM64/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_Beta/7.8/DARWIN_ARM64/ESP/DARWIN_ARM64/test:/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/ESP/DARWIN_ARM64/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_Beta/7.8/DARWIN_ARM64/EGADS/trunk/pyEGADS::/Users/jenkins/util/SU2/SU2-v8.0.0/bin
++ PYTHONPATH=/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EGADS/trunk/pyEGADS::/Users/jenkins/util/SU2/SU2-v8.0.0/bin
++ export PYTHONPATH=/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/OpenCSM/trunk/pyOCSM:/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EGADS/trunk/pyEGADS::/Users/jenkins/util/SU2/SU2-v8.0.0/bin
++ PYTHONPATH=/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/OpenCSM/trunk/pyOCSM:/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EGADS/trunk/pyEGADS::/Users/jenkins/util/SU2/SU2-v8.0.0/bin
++ export PYTHONPATH=/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/CAPS/pyCAPS:/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/OpenCSM/trunk/pyOCSM:/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EGADS/trunk/pyEGADS::/Users/jenkins/util/SU2/SU2-v8.0.0/bin
++ PYTHONPATH=/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/CAPS/pyCAPS:/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/OpenCSM/trunk/pyOCSM:/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/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_Beta/7.8/DARWIN_ARM64/ESP/DARWIN_ARM64/bin
++ rm -f /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/ESP/DARWIN_ARM64/bin/python
++ rm -f /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/ESP/DARWIN_ARM64/bin/python-config
++ rm -f /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/ESP/DARWIN_ARM64/bin/virtualenv
++ rm -f '/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/ESP/DARWIN_ARM64/bin/analyze-*'
++ rm -f '/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/ESP/DARWIN_ARM64/bin/intercept-*'
++ [[ viggen == \m\a\c\y\s ]]
++ [[ viggen == \v\i\g\g\e\n ]]
++ ln -s /Users/jenkins/util/ESP/Python/ESP_Python-3.11.9/bin/python3 /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/ESP/DARWIN_ARM64/bin/python
++ ln -s /Users/jenkins/util/ESP/Python/ESP_Python-3.11.9/bin/python3-config /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/ESP/DARWIN_ARM64/bin/python-config
++ ln -s /Users/jenkins/util/ESP/Python/ESP_Python-3.11.9/bin/virtualenv /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/ESP/DARWIN_ARM64/bin/virtualenv
+++ ls /Users/jenkins/util/ESP/Python/ESP_Python-3.11.9/bin/analyze-build /Users/jenkins/util/ESP/Python/ESP_Python-3.11.9/bin/analyze-c++ /Users/jenkins/util/ESP/Python/ESP_Python-3.11.9/bin/analyze-cc /Users/jenkins/util/ESP/Python/ESP_Python-3.11.9/bin/intercept-build /Users/jenkins/util/ESP/Python/ESP_Python-3.11.9/bin/intercept-c++ /Users/jenkins/util/ESP/Python/ESP_Python-3.11.9/bin/intercept-cc
++ for i in '`ls /Users/jenkins/util/ESP/Python/ESP_Python-${PYTHON_VERSION}/bin/analyze-* /Users/jenkins/util/ESP/Python/ESP_Python-${PYTHON_VERSION}/bin/intercept-*`'
+++ basename /Users/jenkins/util/ESP/Python/ESP_Python-3.11.9/bin/analyze-build
+++ basename /Users/jenkins/util/ESP/Python/ESP_Python-3.11.9/bin/analyze-build
++ ln -s /Users/jenkins/util/ESP/Python/ESP_Python-3.11.9/bin/analyze-build /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/ESP/DARWIN_ARM64/bin/analyze-build
++ for i in '`ls /Users/jenkins/util/ESP/Python/ESP_Python-${PYTHON_VERSION}/bin/analyze-* /Users/jenkins/util/ESP/Python/ESP_Python-${PYTHON_VERSION}/bin/intercept-*`'
+++ basename /Users/jenkins/util/ESP/Python/ESP_Python-3.11.9/bin/analyze-c++
+++ basename /Users/jenkins/util/ESP/Python/ESP_Python-3.11.9/bin/analyze-c++
++ ln -s /Users/jenkins/util/ESP/Python/ESP_Python-3.11.9/bin/analyze-c++ /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/ESP/DARWIN_ARM64/bin/analyze-c++
++ for i in '`ls /Users/jenkins/util/ESP/Python/ESP_Python-${PYTHON_VERSION}/bin/analyze-* /Users/jenkins/util/ESP/Python/ESP_Python-${PYTHON_VERSION}/bin/intercept-*`'
+++ basename /Users/jenkins/util/ESP/Python/ESP_Python-3.11.9/bin/analyze-cc
+++ basename /Users/jenkins/util/ESP/Python/ESP_Python-3.11.9/bin/analyze-cc
++ ln -s /Users/jenkins/util/ESP/Python/ESP_Python-3.11.9/bin/analyze-cc /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/ESP/DARWIN_ARM64/bin/analyze-cc
++ for i in '`ls /Users/jenkins/util/ESP/Python/ESP_Python-${PYTHON_VERSION}/bin/analyze-* /Users/jenkins/util/ESP/Python/ESP_Python-${PYTHON_VERSION}/bin/intercept-*`'
+++ basename /Users/jenkins/util/ESP/Python/ESP_Python-3.11.9/bin/intercept-build
+++ basename /Users/jenkins/util/ESP/Python/ESP_Python-3.11.9/bin/intercept-build
++ ln -s /Users/jenkins/util/ESP/Python/ESP_Python-3.11.9/bin/intercept-build /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/ESP/DARWIN_ARM64/bin/intercept-build
++ for i in '`ls /Users/jenkins/util/ESP/Python/ESP_Python-${PYTHON_VERSION}/bin/analyze-* /Users/jenkins/util/ESP/Python/ESP_Python-${PYTHON_VERSION}/bin/intercept-*`'
+++ basename /Users/jenkins/util/ESP/Python/ESP_Python-3.11.9/bin/intercept-c++
+++ basename /Users/jenkins/util/ESP/Python/ESP_Python-3.11.9/bin/intercept-c++
++ ln -s /Users/jenkins/util/ESP/Python/ESP_Python-3.11.9/bin/intercept-c++ /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/ESP/DARWIN_ARM64/bin/intercept-c++
++ for i in '`ls /Users/jenkins/util/ESP/Python/ESP_Python-${PYTHON_VERSION}/bin/analyze-* /Users/jenkins/util/ESP/Python/ESP_Python-${PYTHON_VERSION}/bin/intercept-*`'
+++ basename /Users/jenkins/util/ESP/Python/ESP_Python-3.11.9/bin/intercept-cc
+++ basename /Users/jenkins/util/ESP/Python/ESP_Python-3.11.9/bin/intercept-cc
++ ln -s /Users/jenkins/util/ESP/Python/ESP_Python-3.11.9/bin/intercept-cc /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/ESP/DARWIN_ARM64/bin/intercept-cc
+++ python-config --includes
++ export 'PYTHONINC=. -I/Users/jenkins/util/ESP/Python/ESP_Python-3.11.9/include/python3.11 -I/Users/jenkins/util/ESP/Python/ESP_Python-3.11.9/include/python3.11'
++ PYTHONINC='. -I/Users/jenkins/util/ESP/Python/ESP_Python-3.11.9/include/python3.11 -I/Users/jenkins/util/ESP/Python/ESP_Python-3.11.9/include/python3.11'
+++ python-config --help
++ [[ Usage: /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/ESP/DARWIN_ARM64/bin/python-config [--prefix|--exec-prefix|--includes|--libs|--cflags|--ldflags|--extension-suffix|--help|--abiflags|--configdir|--embed] == *\e\m\b\e\d* ]]
+++ python-config --ldflags --embed
++ export 'PYTHONLIB=-L/Users/jenkins/util/ESP/Python/ESP_Python-3.11.9/lib -lpython3.11 -ldl -framework CoreFoundation'
++ PYTHONLIB='-L/Users/jenkins/util/ESP/Python/ESP_Python-3.11.9/lib -lpython3.11 -ldl -framework CoreFoundation'
++ [[ viggen == \m\a\c\y\s ]]
++ [[ viggen == \v\i\g\g\e\n ]]
++ export 'PYTHONLIB=-L/Users/jenkins/util/ESP/Python/ESP_Python-3.11.9/lib -lpython3.11 -ldl -framework CoreFoundation -Wl,-w'
++ PYTHONLIB='-L/Users/jenkins/util/ESP/Python/ESP_Python-3.11.9/lib -lpython3.11 -ldl -framework CoreFoundation -Wl,-w'
++ export PYTHONUNBUFFERED=true
++ PYTHONUNBUFFERED=true
++ export PYTHONFAULTHANDLER=true
++ PYTHONFAULTHANDLER=true
++ python --version
Python 3.11.9
++ [[ DARWIN_ARM64 == \D\A\R\W\I\N\6\4\.\g\c\c ]]
++ export CSMDATA=/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/OpenCSM/trunk/data
++ CSMDATA=/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/OpenCSM/trunk/data
+ virtualenv /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/ESP_venv
created virtual environment CPython3.11.9.final.0-64 in 330ms
  creator CPython3Posix(dest=/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/ESP_venv, clear=False, no_vcs_ignore=False, global=False)
  seeder FromAppData(download=False, pip=bundle, setuptools=bundle, wheel=bundle, via=copy, app_data_dir=/Users/jenkins/Library/Application Support/virtualenv)
    added seed packages: pip==24.0, setuptools==69.2.0, wheel==0.43.0
  activators BashActivator,CShellActivator,FishActivator,NushellActivator,PowerShellActivator,PythonActivator
+ . /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/ESP_venv/bin/activate
++ '[' /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/ESP_venv/bin/activate = /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/JenkinsESP/ESP_Beta.sh ']'
++ deactivate nondestructive
++ unset -f pydoc
++ '[' -z '' ']'
++ '[' -z '' ']'
++ hash -r
++ '[' -z '' ']'
++ unset VIRTUAL_ENV
++ unset VIRTUAL_ENV_PROMPT
++ '[' '!' nondestructive = nondestructive ']'
++ VIRTUAL_ENV=/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/ESP_venv
++ '[' darwin23 = cygwin ']'
++ '[' darwin23 = msys ']'
++ export VIRTUAL_ENV
++ _OLD_VIRTUAL_PATH=/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/ESP/DARWIN_ARM64/test:/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/ESP/DARWIN_ARM64/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_Beta/7.8/DARWIN_ARM64/ESP_venv/bin:/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/ESP/DARWIN_ARM64/test:/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/ESP/DARWIN_ARM64/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
++ '[' x '!=' x ']'
+++ basename /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/ESP_venv
++ VIRTUAL_ENV_PROMPT=ESP_venv
++ export VIRTUAL_ENV_PROMPT
++ '[' -z '' ']'
++ '[' -z '' ']'
++ _OLD_VIRTUAL_PS1=
++ PS1='(ESP_venv) '
++ export PS1
++ alias pydoc
++ true
++ hash -r
+ pip_install pip
+ /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/ESP_venv/bin/python -m pip install --only-binary all --upgrade pip
Requirement already satisfied: pip in ./ESP_venv/lib/python3.11/site-packages (24.0)
+ pip_install f90nml
+ /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/ESP_venv/bin/python -m pip install --only-binary all --upgrade f90nml
Collecting f90nml
  Using cached f90nml-1.4.4-py2.py3-none-any.whl.metadata (6.0 kB)
Using cached f90nml-1.4.4-py2.py3-none-any.whl (32 kB)
Installing collected packages: f90nml
Successfully installed f90nml-1.4.4
+ pip_install numpy
+ /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/ESP_venv/bin/python -m pip install --only-binary all --upgrade numpy
Collecting numpy
  Using cached numpy-1.26.4-cp311-cp311-macosx_11_0_arm64.whl.metadata (114 kB)
Using cached numpy-1.26.4-cp311-cp311-macosx_11_0_arm64.whl (14.0 MB)
Installing collected packages: numpy
Successfully installed numpy-1.26.4
+ pip_install openmdao
+ /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/ESP_venv/bin/python -m pip install --only-binary all --upgrade openmdao
Collecting openmdao
  Using cached openmdao-3.31.1-py3-none-any.whl
Collecting networkx>=2.0 (from openmdao)
  Using cached networkx-3.3-py3-none-any.whl.metadata (5.1 kB)
Requirement already satisfied: numpy in ./ESP_venv/lib/python3.11/site-packages (from openmdao) (1.26.4)
Collecting scipy (from openmdao)
  Using cached scipy-1.13.0-cp311-cp311-macosx_12_0_arm64.whl.metadata (60 kB)
Collecting requests (from openmdao)
  Using cached requests-2.31.0-py3-none-any.whl.metadata (4.6 kB)
Collecting packaging (from openmdao)
  Using cached packaging-24.0-py3-none-any.whl.metadata (3.2 kB)
Collecting charset-normalizer<4,>=2 (from requests->openmdao)
  Using cached charset_normalizer-3.3.2-cp311-cp311-macosx_11_0_arm64.whl.metadata (33 kB)
Collecting idna<4,>=2.5 (from requests->openmdao)
  Using cached idna-3.7-py3-none-any.whl.metadata (9.9 kB)
Collecting urllib3<3,>=1.21.1 (from requests->openmdao)
  Using cached urllib3-2.2.1-py3-none-any.whl.metadata (6.4 kB)
Collecting certifi>=2017.4.17 (from requests->openmdao)
  Using cached certifi-2024.2.2-py3-none-any.whl.metadata (2.2 kB)
Using cached networkx-3.3-py3-none-any.whl (1.7 MB)
Using cached packaging-24.0-py3-none-any.whl (53 kB)
Using cached requests-2.31.0-py3-none-any.whl (62 kB)
Using cached scipy-1.13.0-cp311-cp311-macosx_12_0_arm64.whl (30.3 MB)
Using cached certifi-2024.2.2-py3-none-any.whl (163 kB)
Using cached charset_normalizer-3.3.2-cp311-cp311-macosx_11_0_arm64.whl (118 kB)
Using cached idna-3.7-py3-none-any.whl (66 kB)
Using cached urllib3-2.2.1-py3-none-any.whl (121 kB)
Installing collected packages: urllib3, scipy, packaging, networkx, idna, charset-normalizer, certifi, requests, openmdao
Successfully installed certifi-2024.2.2 charset-normalizer-3.3.2 idna-3.7 networkx-3.3 openmdao-3.31.1 packaging-24.0 requests-2.31.0 scipy-1.13.0 urllib3-2.2.1
+ [[ viggen == *\v\i\g\g\e\n* ]]
+ export CVXOPT_BLAS_LIB_DIR=/Users/acdl/workspace/ESP/Python/lapack-3.10.1/build/lib
+ CVXOPT_BLAS_LIB_DIR=/Users/acdl/workspace/ESP/Python/lapack-3.10.1/build/lib
+ export CVXOPT_SUITESPARSE_SRC_DIR=/Users/acdl/workspace/ESP/Python/SuiteSparse-5.12.0
+ CVXOPT_SUITESPARSE_SRC_DIR=/Users/acdl/workspace/ESP/Python/SuiteSparse-5.12.0
+ GCC_MAJOR=11
+ export 'CVXOPT_BLAS_EXTRA_LINK_ARGS=/opt/homebrew/opt/gcc/lib/gcc/11/libgfortran.a;/opt/homebrew/opt/gcc/lib/gcc/11/libquadmath.a;/opt/homebrew/opt/gcc/lib/gcc/11/gcc/aarch64-apple-darwin21/11/libgcc.a'
+ CVXOPT_BLAS_EXTRA_LINK_ARGS='/opt/homebrew/opt/gcc/lib/gcc/11/libgfortran.a;/opt/homebrew/opt/gcc/lib/gcc/11/libquadmath.a;/opt/homebrew/opt/gcc/lib/gcc/11/gcc/aarch64-apple-darwin21/11/libgcc.a'
+ pip_install cvxopt
+ /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/ESP_venv/bin/python -m pip install --only-binary all --upgrade cvxopt
Collecting cvxopt
  Using cached cvxopt-1.3.2-cp311-cp311-macosx_11_0_arm64.whl.metadata (1.3 kB)
Using cached cvxopt-1.3.2-cp311-cp311-macosx_11_0_arm64.whl (11.1 MB)
Installing collected packages: cvxopt
Successfully installed cvxopt-1.3.2
+ pip_install dill
+ /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/ESP_venv/bin/python -m pip install --only-binary all --upgrade dill
Collecting dill
  Using cached dill-0.3.8-py3-none-any.whl.metadata (10 kB)
Using cached dill-0.3.8-py3-none-any.whl (116 kB)
Installing collected packages: dill
Successfully installed dill-0.3.8
+ pip_install packaging
+ /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/ESP_venv/bin/python -m pip install --only-binary all --upgrade packaging
Requirement already satisfied: packaging in ./ESP_venv/lib/python3.11/site-packages (24.0)
+ pip_install matplotlib
+ /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/ESP_venv/bin/python -m pip install --only-binary all --upgrade matplotlib
Collecting matplotlib
  Using cached matplotlib-3.8.4-cp311-cp311-macosx_11_0_arm64.whl.metadata (5.8 kB)
Collecting contourpy>=1.0.1 (from matplotlib)
  Using cached contourpy-1.2.1-cp311-cp311-macosx_11_0_arm64.whl.metadata (5.8 kB)
Collecting cycler>=0.10 (from matplotlib)
  Using cached cycler-0.12.1-py3-none-any.whl.metadata (3.8 kB)
Collecting fonttools>=4.22.0 (from matplotlib)
  Using cached fonttools-4.51.0-cp311-cp311-macosx_10_9_universal2.whl.metadata (159 kB)
Collecting kiwisolver>=1.3.1 (from matplotlib)
  Using cached kiwisolver-1.4.5-cp311-cp311-macosx_11_0_arm64.whl.metadata (6.4 kB)
Requirement already satisfied: numpy>=1.21 in ./ESP_venv/lib/python3.11/site-packages (from matplotlib) (1.26.4)
Requirement already satisfied: packaging>=20.0 in ./ESP_venv/lib/python3.11/site-packages (from matplotlib) (24.0)
Collecting pillow>=8 (from matplotlib)
  Using cached pillow-10.3.0-cp311-cp311-macosx_11_0_arm64.whl.metadata (9.2 kB)
Collecting pyparsing>=2.3.1 (from matplotlib)
  Using cached pyparsing-3.1.2-py3-none-any.whl.metadata (5.1 kB)
Collecting python-dateutil>=2.7 (from matplotlib)
  Using cached python_dateutil-2.9.0.post0-py2.py3-none-any.whl.metadata (8.4 kB)
Collecting six>=1.5 (from python-dateutil>=2.7->matplotlib)
  Using cached six-1.16.0-py2.py3-none-any.whl.metadata (1.8 kB)
Using cached matplotlib-3.8.4-cp311-cp311-macosx_11_0_arm64.whl (7.5 MB)
Using cached contourpy-1.2.1-cp311-cp311-macosx_11_0_arm64.whl (245 kB)
Using cached cycler-0.12.1-py3-none-any.whl (8.3 kB)
Using cached fonttools-4.51.0-cp311-cp311-macosx_10_9_universal2.whl (2.8 MB)
Using cached kiwisolver-1.4.5-cp311-cp311-macosx_11_0_arm64.whl (66 kB)
Using cached pillow-10.3.0-cp311-cp311-macosx_11_0_arm64.whl (3.4 MB)
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Using cached six-1.16.0-py2.py3-none-any.whl (11 kB)
Installing collected packages: six, pyparsing, pillow, kiwisolver, fonttools, cycler, contourpy, python-dateutil, matplotlib
Successfully installed contourpy-1.2.1 cycler-0.12.1 fonttools-4.51.0 kiwisolver-1.4.5 matplotlib-3.8.4 pillow-10.3.0 pyparsing-3.1.2 python-dateutil-2.9.0.post0 six-1.16.0
+ pip_install scipy
+ /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/ESP_venv/bin/python -m pip install --only-binary all --upgrade scipy
Requirement already satisfied: scipy in ./ESP_venv/lib/python3.11/site-packages (1.13.0)
Requirement already satisfied: numpy<2.3,>=1.22.4 in ./ESP_venv/lib/python3.11/site-packages (from scipy) (1.26.4)
+ unset PYTHONINC
+ unset PYTHONLIB
+ unset UDUNITS2_XML_PATH
+ unset ESP_BLOC
+ unset ESP_ROOT
+ unset ESP_ARCH
+ unset AWAVE
+ unset AFLR
+ unset AFLR_ARCH
+ wget --tries=3 https://acdl.mit.edu/ESP/archive/ESPbeta.tgz
--2024-05-03 00:16:00--  https://acdl.mit.edu/ESP/archive/ESPbeta.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: 268501958 (256M) [application/x-gzip]
Saving to: ‘ESPbeta.tgz’

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 12200K .......... .......... .......... .......... ..........  4% 27.6M 4s
 12250K .......... .......... .......... .......... ..........  4%  270M 4s
 12300K .......... .......... .......... .......... ..........  4%  384M 4s
 12350K .......... .......... .......... .......... ..........  4%  319M 4s
 12400K .......... .......... .......... .......... ..........  4%  351M 4s
 12450K .......... .......... .......... .......... ..........  4% 76.5M 4s
 12500K .......... .......... .......... .......... ..........  4% 98.6M 4s
 12550K .......... .......... .......... .......... ..........  4%  121M 4s
 12600K .......... .......... .......... .......... ..........  4% 79.0M 4s
 12650K .......... .......... .......... .......... ..........  4%  113M 4s
 12700K .......... .......... .......... .......... ..........  4% 79.9M 4s
 12750K .......... .......... .......... .......... ..........  4% 86.0M 4s
 12800K .......... .......... .......... .......... ..........  4%  109M 4s
 12850K .......... .......... .......... .......... ..........  4% 75.6M 4s
 12900K .......... .......... .......... .......... ..........  4%  124M 4s
 12950K .......... .......... .......... .......... ..........  4% 75.5M 4s
 13000K .......... .......... .......... .......... ..........  4% 98.2M 4s
 13050K .......... .......... .......... .......... ..........  4% 95.9M 4s
 13100K .......... .......... .......... .......... ..........  5% 93.5M 4s
 13150K .......... .......... .......... .......... ..........  5% 94.3M 4s
 13200K .......... .......... .......... .......... ..........  5% 94.8M 4s
 13250K .......... .......... .......... .......... ..........  5% 94.6M 4s
 13300K .......... .......... .......... .......... ..........  5% 93.9M 4s
 13350K .......... .......... .......... .......... ..........  5% 94.1M 4s
 13400K .......... .......... .......... .......... ..........  5% 95.7M 4s
 13450K .......... .......... .......... .......... ..........  5% 94.1M 4s
 13500K .......... .......... .......... .......... ..........  5% 93.9M 4s
 13550K .......... .......... .......... .......... ..........  5% 91.8M 4s
 13600K .......... .......... .......... .......... ..........  5% 94.4M 4s
 13650K .......... .......... .......... .......... ..........  5% 95.9M 4s
 13700K .......... .......... .......... .......... ..........  5% 77.3M 4s
 13750K .......... .......... .......... .......... ..........  5%  120M 4s
 13800K .......... .......... .......... .......... ..........  5% 78.1M 4s
 13850K .......... .......... .......... .......... ..........  5%  110M 4s
 13900K .......... .......... .......... .......... ..........  5%  105M 4s
 13950K .......... .......... .......... .......... ..........  5% 73.5M 4s
 14000K .......... .......... .......... .......... ..........  5% 97.1M 4s
 14050K .......... .......... .......... .......... ..........  5% 95.7M 4s
 14100K .......... .......... .......... .......... ..........  5% 94.1M 4s
 14150K .......... .......... .......... .......... ..........  5% 74.9M 4s
 14200K .......... .......... .......... .......... ..........  5% 94.1M 4s
 14250K .......... .......... .......... .......... ..........  5% 94.4M 4s
 14300K .......... .......... .......... .......... ..........  5%  125M 4s
 14350K .......... .......... .......... .......... ..........  5% 75.7M 4s
 14400K .......... .......... .......... .......... ..........  5%  119M 4s
 14450K .......... .......... .......... .......... ..........  5% 64.5M 4s
 14500K .......... .......... .......... .......... ..........  5%  117M 4s
 14550K .......... .......... .......... .......... ..........  5% 94.4M 4s
 14600K .......... .......... .......... .......... ..........  5% 91.6M 4s
 14650K .......... .......... .......... .......... ..........  5%  101M 4s
 14700K .......... .......... .......... .......... ..........  5% 89.3M 4s
 14750K .......... .......... .......... .......... ..........  5% 94.3M 4s
 14800K .......... .......... .......... .......... ..........  5% 94.1M 4s
 14850K .......... .......... .......... .......... ..........  5% 95.6M 4s
 14900K .......... .......... .......... .......... ..........  5% 77.9M 4s
 14950K .......... .......... .......... .......... ..........  5% 89.6M 4s
 15000K .......... .......... .......... .......... ..........  5% 97.7M 4s
 15050K .......... .......... .......... .......... ..........  5% 95.6M 4s
 15100K .......... .......... .......... .......... ..........  5% 89.9M 4s
 15150K .......... .......... .......... .......... ..........  5% 78.3M 4s
 15200K .......... .......... .......... .......... ..........  5% 93.2M 4s
 15250K .......... .......... .......... .......... ..........  5% 94.6M 4s
 15300K .......... .......... .......... .......... ..........  5% 94.3M 4s
 15350K .......... .......... .......... .......... ..........  5% 94.3M 4s
 15400K .......... .......... .......... .......... ..........  5% 88.9M 4s
 15450K .......... .......... .......... .......... ..........  5% 79.4M 4s
 15500K .......... .......... .......... .......... ..........  5%  125M 4s
 15550K .......... .......... .......... .......... ..........  5%  115M 4s
 15600K .......... .......... .......... .......... ..........  5% 98.8M 4s
 15650K .......... .......... .......... .......... ..........  5% 99.6M 4s
 15700K .......... .......... .......... .......... ..........  6% 92.8M 4s
 15750K .......... .......... .......... .......... ..........  6% 26.6M 4s
 15800K .......... .......... .......... .......... ..........  6%  326M 4s
 15850K .......... .......... .......... .......... ..........  6%  286M 4s
 15900K .......... .......... .......... .......... ..........  6% 29.0M 4s
 15950K .......... .......... .......... .......... ..........  6%  301M 4s
 16000K .......... .......... .......... .......... ..........  6%  362M 4s
 16050K .......... .......... .......... .......... ..........  6%  379M 4s
 16100K .......... .......... .......... .......... ..........  6%  268M 3s
 16150K .......... .......... .......... .......... ..........  6%  309M 3s
 16200K .......... .......... .......... .......... ..........  6%  107M 3s
 16250K .......... .......... .......... .......... ..........  6% 90.4M 3s
 16300K .......... .......... .......... .......... ..........  6% 99.9M 3s
 16350K .......... .......... .......... .......... ..........  6% 43.2M 3s
 16400K .......... .......... .......... .......... ..........  6% 70.8M 3s
 16450K .......... .......... .......... .......... ..........  6% 94.6M 3s
 16500K .......... .......... .......... .......... ..........  6% 93.0M 3s
 16550K .......... .......... .......... .......... ..........  6% 91.8M 3s
 16600K .......... .......... .......... .......... ..........  6% 45.6M 3s
 16650K .......... .......... .......... .......... ..........  6%  121M 3s
 16700K .......... .......... .......... .......... ..........  6% 48.0M 3s
 16750K .......... .......... .......... .......... ..........  6% 87.3M 3s
 16800K .......... .......... .......... .......... ..........  6% 65.5M 3s
 16850K .......... .......... .......... .......... ..........  6% 64.8M 3s
 16900K .......... .......... .......... .......... ..........  6%  124M 3s
 16950K .......... .......... .......... .......... ..........  6% 65.5M 3s
 17000K .......... .......... .......... .......... ..........  6%  115M 3s
 17050K .......... .......... .......... .......... ..........  6% 88.8M 3s
 17100K .......... .......... .......... .......... ..........  6% 92.7M 3s
 17150K .......... .......... .......... .......... ..........  6% 98.6M 3s
 17200K .......... .......... .......... .......... ..........  6% 64.2M 3s
 17250K .......... .......... .......... .......... ..........  6%  104M 3s
 17300K .......... .......... .......... .......... ..........  6% 69.7M 3s
 17350K .......... .......... .......... .......... ..........  6% 94.3M 3s
 17400K .......... .......... .......... .......... ..........  6% 93.4M 3s
 17450K .......... .......... .......... .......... ..........  6% 63.5M 3s
 17500K .......... .......... .......... .......... ..........  6%  118M 3s
 17550K .......... .......... .......... .......... ..........  6% 95.2M 3s
 17600K .......... .......... .......... .......... ..........  6% 65.1M 3s
 17650K .......... .......... .......... .......... ..........  6%  170M 3s
 17700K .......... .......... .......... .......... ..........  6% 63.3M 3s
 17750K .......... .......... .......... .......... ..........  6% 99.0M 3s
 17800K .......... .......... .......... .......... ..........  6% 74.1M 3s
 17850K .......... .......... .......... .......... ..........  6% 89.6M 3s
 17900K .......... .......... .......... .......... ..........  6% 72.9M 3s
 17950K .......... .......... .......... .......... ..........  6% 80.6M 3s
 18000K .......... .......... .......... .......... ..........  6% 94.4M 3s
 18050K .......... .......... .......... .......... ..........  6% 75.9M 3s
 18100K .......... .......... .......... .......... ..........  6% 86.4M 3s
 18150K .......... .......... .......... .......... ..........  6%  103M 3s
 18200K .......... .......... .......... .......... ..........  6% 90.9M 3s
 18250K .......... .......... .......... .......... ..........  6% 64.8M 3s
 18300K .......... .......... .......... .......... ..........  6%  174M 3s
 18350K .......... .......... .......... .......... ..........  7% 55.6M 3s
 18400K .......... .......... .......... .......... ..........  7%  179M 3s
 18450K .......... .......... .......... .......... ..........  7% 65.3M 3s
 18500K .......... .......... .......... .......... ..........  7% 94.3M 3s
 18550K .......... .......... .......... .......... ..........  7% 93.9M 3s
 18600K .......... .......... .......... .......... ..........  7% 90.3M 3s
 18650K .......... .......... .......... .......... ..........  7% 75.6M 3s
 18700K .......... .......... .......... .......... ..........  7% 95.2M 3s
 18750K .......... .......... .......... .......... ..........  7% 63.5M 3s
 18800K .......... .......... .......... .......... ..........  7%  107M 3s
 18850K .......... .......... .......... .......... ..........  7% 81.7M 3s
 18900K .......... .......... .......... .......... ..........  7% 65.3M 3s
 18950K .......... .......... .......... .......... ..........  7% 94.6M 3s
 19000K .......... .......... .......... .......... ..........  7%  118M 3s
 19050K .......... .......... .......... .......... ..........  7% 97.9M 3s
 19100K .......... .......... .......... .......... ..........  7% 95.9M 3s
 19150K .......... .......... .......... .......... ..........  7%  120M 3s
 19200K .......... .......... .......... .......... ..........  7% 90.8M 3s
 19250K .......... .......... .......... .......... ..........  7%  102M 3s
 19300K .......... .......... .......... .......... ..........  7%  121M 3s
 19350K .......... .......... .......... .......... ..........  7% 25.1M 3s
 19400K .......... .......... .......... .......... ..........  7%  102M 3s
 19450K .......... .......... .......... .......... ..........  7%  112M 3s
 19500K .......... .......... .......... .......... ..........  7%  128M 3s
 19550K .......... .......... .......... .......... ..........  7%  127M 3s
 19600K .......... .......... .......... .......... ..........  7%  109M 3s
 19650K .......... .......... .......... .......... ..........  7%  132M 3s
 19700K .......... .......... .......... .......... ..........  7%  109M 3s
 19750K .......... .......... .......... .......... ..........  7%  128M 3s
 19800K .......... .......... .......... .......... ..........  7%  142M 3s
 19850K .......... .......... .......... .......... ..........  7%  330M 3s
 19900K .......... .......... .......... .......... ..........  7%  339M 3s
 19950K .......... .......... .......... .......... ..........  7% 71.5M 3s
 20000K .......... .......... .......... .......... ..........  7% 76.7M 3s
 20050K .......... .......... .......... .......... ..........  7% 75.5M 3s
 20100K .......... .......... .......... .......... ..........  7% 63.3M 3s
 20150K .......... .......... .......... .......... ..........  7% 73.4M 3s
 20200K .......... .......... .......... .......... ..........  7% 55.7M 3s
 20250K .......... .......... .......... .......... ..........  7% 73.2M 3s
 20300K .......... .......... .......... .......... ..........  7% 55.5M 3s
 20350K .......... .......... .......... .......... ..........  7% 62.5M 3s
 20400K .......... .......... .......... .......... ..........  7% 94.8M 3s
 20450K .......... .......... .......... .......... ..........  7% 75.6M 3s
 20500K .......... .......... .......... .......... ..........  7% 62.9M 3s
 20550K .......... .......... .......... .......... ..........  7% 87.8M 3s
 20600K .......... .......... .......... .......... ..........  7% 48.6M 3s
 20650K .......... .......... .......... .......... ..........  7% 91.1M 3s
 20700K .......... .......... .......... .......... ..........  7% 65.5M 3s
 20750K .......... .......... .......... .......... ..........  7% 62.0M 3s
 20800K .......... .......... .......... .......... ..........  7% 53.4M 3s
 20850K .......... .......... .......... .......... ..........  7% 64.6M 3s
 20900K .......... .......... .......... .......... ..........  7%  127M 3s
 20950K .......... .......... .......... .......... ..........  8% 54.7M 3s
 21000K .......... .......... .......... .......... ..........  8% 71.9M 3s
 21050K .......... .......... .......... .......... ..........  8% 55.7M 3s
 21100K .......... .......... .......... .......... ..........  8% 73.6M 3s
 21150K .......... .......... .......... .......... ..........  8% 99.0M 3s
 21200K .......... .......... .......... .......... ..........  8% 63.5M 3s
 21250K .......... .......... .......... .......... ..........  8% 76.3M 3s
 21300K .......... .......... .......... .......... ..........  8% 90.3M 3s
 21350K .......... .......... .......... .......... ..........  8% 50.9M 3s
 21400K .......... .......... .......... .......... ..........  8% 51.1M 3s
 21450K .......... .......... .......... .......... ..........  8% 62.4M 3s
 21500K .......... .......... .......... .......... ..........  8% 52.4M 3s
 21550K .......... .......... .......... .......... ..........  8% 62.3M 3s
 21600K .......... .......... .......... .......... ..........  8%  112M 3s
 21650K .......... .......... .......... .......... ..........  8% 51.0M 3s
 21700K .......... .......... .......... .......... ..........  8% 63.1M 3s
 21750K .......... .......... .......... .......... ..........  8%  119M 3s
 21800K .......... .......... .......... .......... ..........  8% 53.8M 3s
 21850K .......... .......... .......... .......... ..........  8% 90.8M 3s
 21900K .......... .......... .......... .......... ..........  8% 57.8M 3s
 21950K .......... .......... .......... .......... ..........  8% 62.1M 3s
 22000K .......... .......... .......... .......... ..........  8% 77.8M 3s
 22050K .......... .......... .......... .......... ..........  8% 76.3M 3s
 22100K .......... .......... .......... .......... ..........  8% 63.2M 3s
 22150K .......... .......... .......... .......... ..........  8% 76.2M 3s
 22200K .......... .......... .......... .......... ..........  8% 54.0M 3s
 22250K .......... .......... .......... .......... ..........  8% 95.4M 3s
 22300K .......... .......... .......... .......... ..........  8% 75.7M 3s
 22350K .......... .......... .......... .......... ..........  8% 91.8M 3s
 22400K .......... .......... .......... .......... ..........  8% 97.9M 3s
 22450K .......... .......... .......... .......... ..........  8% 95.7M 3s
 22500K .......... .......... .......... .......... ..........  8%  120M 3s
 22550K .......... .......... .......... .......... ..........  8% 17.0M 3s
 22600K .......... .......... .......... .......... ..........  8% 27.7M 3s
 22650K .......... .......... .......... .......... ..........  8%  379M 3s
 22700K .......... .......... .......... .......... ..........  8%  337M 3s
 22750K .......... .......... .......... .......... ..........  8%  111M 3s
 22800K .......... .......... .......... .......... ..........  8%  404M 3s
 22850K .......... .......... .......... .......... ..........  8%  356M 3s
 22900K .......... .......... .......... .......... ..........  8%  421M 3s
 22950K .......... .......... .......... .......... ..........  8%  376M 3s
 23000K .......... .......... .......... .......... ..........  8%  391M 3s
 23050K .......... .......... .......... .......... ..........  8%  421M 3s
 23100K .......... .......... .......... .......... ..........  8% 30.4M 3s
 23150K .......... .......... .......... .......... ..........  8%  131M 3s
 23200K .......... .......... .......... .......... ..........  8% 54.9M 3s
 23250K .......... .......... .......... .......... ..........  8%  354M 3s
 23300K .......... .......... .......... .......... ..........  8%  417M 3s
 23350K .......... .......... .......... .......... ..........  8% 75.5M 3s
 23400K .......... .......... .......... .......... ..........  8%  135M 3s
 23450K .......... .......... .......... .......... ..........  8%  123M 3s
 23500K .......... .......... .......... .......... ..........  8%  138M 3s
 23550K .......... .......... .......... .......... ..........  9%  143M 3s
 23600K .......... .......... .......... .......... ..........  9%  119M 3s
 23650K .......... .......... .......... .......... ..........  9%  146M 3s
 23700K .......... .......... .......... .......... ..........  9%  115M 3s
 23750K .......... .......... .......... .......... ..........  9%  143M 3s
 23800K .......... .......... .......... .......... ..........  9%  149M 3s
 23850K .......... .......... .......... .......... ..........  9%  121M 3s
 23900K .......... .......... .......... .......... ..........  9% 83.6M 3s
 23950K .......... .......... .......... .......... ..........  9% 66.0M 3s
 24000K .......... .......... .......... .......... ..........  9% 90.8M 3s
 24050K .......... .......... .......... .......... ..........  9% 52.7M 3s
 24100K .......... .......... .......... .......... ..........  9% 93.7M 3s
 24150K .......... .......... .......... .......... ..........  9% 86.7M 3s
 24200K .......... .......... .......... .......... ..........  9% 47.9M 3s
 24250K .......... .......... .......... .......... ..........  9% 17.9M 3s
 24300K .......... .......... .......... .......... ..........  9%  286M 3s
 24350K .......... .......... .......... .......... ..........  9% 50.4M 3s
 24400K .......... .......... .......... .......... ..........  9% 19.6M 3s
 24450K .......... .......... .......... .......... ..........  9%  344M 3s
 24500K .......... .......... .......... .......... ..........  9% 38.2M 3s
 24550K .......... .......... .......... .......... ..........  9% 67.0M 3s
 24600K .......... .......... .......... .......... ..........  9% 35.8M 3s
 24650K .......... .......... .......... .......... ..........  9% 79.4M 3s
 24700K .......... .......... .......... .......... ..........  9% 58.5M 3s
 24750K .......... .......... .......... .......... ..........  9% 77.5M 3s
 24800K .......... .......... .......... .......... ..........  9%  130M 3s
 24850K .......... .......... .......... .......... ..........  9% 24.8M 3s
 24900K .......... .......... .......... .......... ..........  9% 26.9M 3s
 24950K .......... .......... .......... .......... ..........  9%  270M 3s
 25000K .......... .......... .......... .......... ..........  9% 38.7M 3s
 25050K .......... .......... .......... .......... ..........  9%  138M 3s
 25100K .......... .......... .......... .......... ..........  9% 12.4M 3s
 25150K .......... .......... .......... .......... ..........  9%  145M 3s
 25200K .......... .......... .......... .......... ..........  9% 35.9M 3s
 25250K .......... .......... .......... .......... ..........  9%  121M 3s
 25300K .......... .......... .......... .......... ..........  9% 73.3M 3s
 25350K .......... .......... .......... .......... ..........  9% 88.6M 3s
 25400K .......... .......... .......... .......... ..........  9%  136M 3s
 25450K .......... .......... .......... .......... ..........  9% 18.7M 3s
 25500K .......... .......... .......... .......... ..........  9%  294M 3s
 25550K .......... .......... .......... .......... ..........  9%  379M 3s
 25600K .......... .......... .......... .......... ..........  9% 52.6M 3s
 25650K .......... .......... .......... .......... ..........  9% 76.9M 3s
 25700K .......... .......... .......... .......... ..........  9% 37.2M 3s
 25750K .......... .......... .......... .......... ..........  9%  417M 3s
 25800K .......... .......... .......... .......... ..........  9% 22.0M 3s
 25850K .......... .......... .......... .......... ..........  9%  227M 3s
 25900K .......... .......... .......... .......... ..........  9%  307M 3s
 25950K .......... .......... .......... .......... ..........  9% 30.3M 3s
 26000K .......... .......... .......... .......... ..........  9%  400M 3s
 26050K .......... .......... .......... .......... ..........  9% 16.8M 3s
 26100K .......... .......... .......... .......... ..........  9%  323M 3s
 26150K .......... .......... .......... .......... ..........  9%  425M 3s
 26200K .......... .......... .......... .......... .......... 10% 38.6M 3s
 26250K .......... .......... .......... .......... .......... 10%  147M 3s
 26300K .......... .......... .......... .......... .......... 10% 94.4M 3s
 26350K .......... .......... .......... .......... .......... 10% 77.1M 3s
 26400K .......... .......... .......... .......... .......... 10% 81.0M 3s
 26450K .......... .......... .......... .......... .......... 10%  132M 3s
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 27350K .......... .......... .......... .......... .......... 10% 42.5M 3s
 27400K .......... .......... .......... .......... .......... 10% 80.3M 3s
 27450K .......... .......... .......... .......... .......... 10%  132M 3s
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 28400K .......... .......... .......... .......... .......... 10% 91.6M 3s
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 29350K .......... .......... .......... .......... .......... 11% 81.5M 3s
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 29750K .......... .......... .......... .......... .......... 11% 12.4M 3s
 29800K .......... .......... .......... .......... .......... 11%  110M 3s
 29850K .......... .......... .......... .......... .......... 11% 40.5M 3s
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 29950K .......... .......... .......... .......... .......... 11% 96.3M 3s
 30000K .......... .......... .......... .......... .......... 11%  102M 3s
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 30100K .......... .......... .......... .......... .......... 11% 67.0M 3s
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 30350K .......... .......... .......... .......... .......... 11% 34.4M 3s
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 30650K .......... .......... .......... .......... .......... 11%  376M 3s
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 30750K .......... .......... .......... .......... .......... 11%  379M 3s
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 30950K .......... .......... .......... .......... .......... 11% 94.6M 3s
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 31100K .......... .......... .......... .......... .......... 11% 90.1M 3s
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 31950K .......... .......... .......... .......... .......... 12% 75.8M 3s
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 32050K .......... .......... .......... .......... .......... 12% 76.2M 3s
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 32150K .......... .......... .......... .......... .......... 12%  105M 3s
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 32250K .......... .......... .......... .......... .......... 12% 78.6M 3s
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 33350K .......... .......... .......... .......... .......... 12% 78.0M 3s
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 33450K .......... .......... .......... .......... .......... 12% 75.9M 3s
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 34100K .......... .......... .......... .......... .......... 13% 67.3M 3s
 34150K .......... .......... .......... .......... .......... 13%  119M 3s
 34200K .......... .......... .......... .......... .......... 13% 51.1M 3s
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 37100K .......... .......... .......... .......... .......... 14% 94.3M 3s
 37150K .......... .......... .......... .......... .......... 14% 75.6M 3s
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 40000K .......... .......... .......... .......... .......... 15% 90.1M 3s
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 40950K .......... .......... .......... .......... .......... 15% 64.6M 3s
 41000K .......... .......... .......... .......... .......... 15% 69.4M 3s
 41050K .......... .......... .......... .......... .......... 15% 81.5M 3s
 41100K .......... .......... .......... .......... .......... 15%  118M 3s
 41150K .......... .......... .......... .......... .......... 15% 65.4M 3s
 41200K .......... .......... .......... .......... .......... 15% 74.9M 3s
 41250K .......... .......... .......... .......... .......... 15% 73.0M 3s
 41300K .......... .......... .......... .......... .......... 15% 97.9M 3s
 41350K .......... .......... .......... .......... .......... 15% 54.3M 3s
 41400K .......... .......... .......... .......... .......... 15%  168M 3s
 41450K .......... .......... .......... .......... .......... 15% 62.0M 3s
 41500K .......... .......... .......... .......... .......... 15% 66.7M 3s
 41550K .......... .......... .......... .......... .......... 15% 95.4M 3s
 41600K .......... .......... .......... .......... .......... 15% 73.0M 3s
 41650K .......... .......... .......... .......... .......... 15% 55.7M 3s
 41700K .......... .......... .......... .......... .......... 15% 28.7M 3s
 41750K .......... .......... .......... .......... .......... 15%  135M 3s
 41800K .......... .......... .......... .......... .......... 15% 40.4M 3s
 41850K .......... .......... .......... .......... .......... 15% 97.1M 3s
 41900K .......... .......... .......... .......... .......... 15% 46.3M 3s
 41950K .......... .......... .......... .......... .......... 16% 99.6M 3s
 42000K .......... .......... .......... .......... .......... 16% 98.0M 3s
 42050K .......... .......... .......... .......... .......... 16%  117M 3s
 42100K .......... .......... .......... .......... .......... 16% 86.6M 3s
 42150K .......... .......... .......... .......... .......... 16% 81.1M 3s
 42200K .......... .......... .......... .......... .......... 16%  124M 3s
 42250K .......... .......... .......... .......... .......... 16%  116M 3s
 42300K .......... .......... .......... .......... .......... 16% 80.7M 3s
 42350K .......... .......... .......... .......... .......... 16% 96.9M 3s
 42400K .......... .......... .......... .......... .......... 16%  103M 3s
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 42500K .......... .......... .......... .......... .......... 16%  120M 3s
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 42600K .......... .......... .......... .......... .......... 16% 91.4M 3s
 42650K .......... .......... .......... .......... .......... 16%  100M 3s
 42700K .......... .......... .......... .......... .......... 16% 87.5M 3s
 42750K .......... .......... .......... .......... .......... 16%  114M 3s
 42800K .......... .......... .......... .......... .......... 16%  138M 3s
 42850K .......... .......... .......... .......... .......... 16% 97.1M 3s
 42900K .......... .......... .......... .......... .......... 16% 85.1M 3s
 42950K .......... .......... .......... .......... .......... 16% 73.9M 3s
 43000K .......... .......... .......... .......... .......... 16%  144M 3s
 43050K .......... .......... .......... .......... .......... 16% 85.4M 3s
 43100K .......... .......... .......... .......... .......... 16%  135M 3s
 43150K .......... .......... .......... .......... .......... 16%  105M 3s
 43200K .......... .......... .......... .......... .......... 16% 88.1M 3s
 43250K .......... .......... .......... .......... .......... 16%  132M 3s
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 43350K .......... .......... .......... .......... .......... 16% 92.3M 3s
 43400K .......... .......... .......... .......... .......... 16%  106M 3s
 43450K .......... .......... .......... .......... .......... 16% 78.5M 3s
 43500K .......... .......... .......... .......... .......... 16%  131M 3s
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 43650K .......... .......... .......... .......... .......... 16% 32.9M 3s
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 43950K .......... .......... .......... .......... .......... 16% 70.7M 3s
 44000K .......... .......... .......... .......... .......... 16%  150M 3s
 44050K .......... .......... .......... .......... .......... 16%  112M 3s
 44100K .......... .......... .......... .......... .......... 16% 69.7M 3s
 44150K .......... .......... .......... .......... .......... 16%  154M 3s
 44200K .......... .......... .......... .......... .......... 16% 49.1M 3s
 44250K .......... .......... .......... .......... .......... 16%  117M 3s
 44300K .......... .......... .......... .......... .......... 16% 25.0M 3s
 44350K .......... .......... .......... .......... .......... 16% 19.3M 3s
 44400K .......... .......... .......... .......... .......... 16% 17.6M 3s
 44450K .......... .......... .......... .......... .......... 16%  120M 3s
 44500K .......... .......... .......... .......... .......... 16% 42.4M 3s
 44550K .......... .......... .......... .......... .......... 17%  141M 3s
 44600K .......... .......... .......... .......... .......... 17% 87.5M 3s
 44650K .......... .......... .......... .......... .......... 17% 57.0M 3s
 44700K .......... .......... .......... .......... .......... 17%  131M 3s
 44750K .......... .......... .......... .......... .......... 17% 48.0M 3s
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 44850K .......... .......... .......... .......... .......... 17% 71.0M 3s
 44900K .......... .......... .......... .......... .......... 17% 87.5M 3s
 44950K .......... .......... .......... .......... .......... 17%  132M 3s
 45000K .......... .......... .......... .......... .......... 17% 43.5M 3s
 45050K .......... .......... .......... .......... .......... 17% 35.2M 3s
 45100K .......... .......... .......... .......... .......... 17%  351M 3s
 45150K .......... .......... .......... .......... .......... 17% 44.0M 3s
 45200K .......... .......... .......... .......... .......... 17% 68.8M 3s
 45250K .......... .......... .......... .......... .......... 17%  414M 3s
 45300K .......... .......... .......... .......... .......... 17% 8.65M 3s
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 45400K .......... .......... .......... .......... .......... 17% 45.7M 3s
 45450K .......... .......... .......... .......... .......... 17% 68.4M 3s
 45500K .......... .......... .......... .......... .......... 17%  128M 3s
 45550K .......... .......... .......... .......... .......... 17%  151M 3s
 45600K .......... .......... .......... .......... .......... 17% 16.0M 3s
 45650K .......... .......... .......... .......... .......... 17%  150M 3s
 45700K .......... .......... .......... .......... .......... 17% 37.7M 3s
 45750K .......... .......... .......... .......... .......... 17% 88.9M 3s
 45800K .......... .......... .......... .......... .......... 17%  150M 3s
 45850K .......... .......... .......... .......... .......... 17% 38.5M 3s
 45900K .......... .......... .......... .......... .......... 17%  414M 3s
 45950K .......... .......... .......... .......... .......... 17% 79.9M 3s
 46000K .......... .......... .......... .......... .......... 17%  131M 3s
 46050K .......... .......... .......... .......... .......... 17%  143M 3s
 46100K .......... .......... .......... .......... .......... 17% 46.9M 3s
 46150K .......... .......... .......... .......... .......... 17% 36.4M 3s
 46200K .......... .......... .......... .......... .......... 17%  111M 3s
 46250K .......... .......... .......... .......... .......... 17%  123M 3s
 46300K .......... .......... .......... .......... .......... 17% 21.6M 3s
 46350K .......... .......... .......... .......... .......... 17%  122M 3s
 46400K .......... .......... .......... .......... .......... 17%  149M 3s
 46450K .......... .......... .......... .......... .......... 17% 42.9M 3s
 46500K .......... .......... .......... .......... .......... 17%  106M 3s
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 46600K .......... .......... .......... .......... .......... 17% 54.6M 3s
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 46700K .......... .......... .......... .......... .......... 17%  130M 3s
 46750K .......... .......... .......... .......... .......... 17% 43.6M 3s
 46800K .......... .......... .......... .......... .......... 17%  106M 3s
 46850K .......... .......... .......... .......... .......... 17%  121M 3s
 46900K .......... .......... .......... .......... .......... 17% 67.1M 3s
 46950K .......... .......... .......... .......... .......... 17% 29.5M 3s
 47000K .......... .......... .......... .......... .......... 17%  364M 3s
 47050K .......... .......... .......... .......... .......... 17% 31.3M 3s
 47100K .......... .......... .......... .......... .......... 17%  341M 3s
 47150K .......... .......... .......... .......... .......... 18%  407M 3s
 47200K .......... .......... .......... .......... .......... 18% 19.6M 3s
 47250K .......... .......... .......... .......... .......... 18%  143M 3s
 47300K .......... .......... .......... .......... .......... 18%  154M 3s
 47350K .......... .......... .......... .......... .......... 18% 15.9M 3s
 47400K .......... .......... .......... .......... .......... 18%  143M 3s
 47450K .......... .......... .......... .......... .......... 18%  132M 3s
 47500K .......... .......... .......... .......... .......... 18% 36.2M 3s
 47550K .......... .......... .......... .......... .......... 18%  149M 3s
 47600K .......... .......... .......... .......... .......... 18%  129M 3s
 47650K .......... .......... .......... .......... .......... 18% 72.3M 3s
 47700K .......... .......... .......... .......... .......... 18% 95.2M 3s
 47750K .......... .......... .......... .......... .......... 18%  102M 3s
 47800K .......... .......... .......... .......... .......... 18% 78.4M 3s
 47850K .......... .......... .......... .......... .......... 18%  111M 3s
 47900K .......... .......... .......... .......... .......... 18%  140M 3s
 47950K .......... .......... .......... .......... .......... 18% 68.6M 3s
 48000K .......... .......... .......... .......... .......... 18%  144M 3s
 48050K .......... .......... .......... .......... .......... 18% 95.7M 3s
 48100K .......... .......... .......... .......... .......... 18% 79.8M 3s
 48150K .......... .......... .......... .......... .......... 18%  128M 3s
 48200K .......... .......... .......... .......... .......... 18% 37.0M 3s
 48250K .......... .......... .......... .......... .......... 18%  379M 3s
 48300K .......... .......... .......... .......... .......... 18%  444M 3s
 48350K .......... .......... .......... .......... .......... 18% 47.2M 3s
 48400K .......... .......... .......... .......... .......... 18%  138M 3s
 48450K .......... .......... .......... .......... .......... 18%  114M 3s
 48500K .......... .......... .......... .......... .......... 18% 37.5M 3s
 48550K .......... .......... .......... .......... .......... 18%  414M 3s
 48600K .......... .......... .......... .......... .......... 18%  373M 3s
 48650K .......... .......... .......... .......... .......... 18% 38.1M 3s
 48700K .......... .......... .......... .......... .......... 18%  207M 3s
 48750K .......... .......... .......... .......... .......... 18%  107M 3s
 48800K .......... .......... .......... .......... .......... 18% 53.8M 3s
 48850K .......... .......... .......... .......... .......... 18% 62.0M 3s
 48900K .......... .......... .......... .......... .......... 18%  381M 3s
 48950K .......... .......... .......... .......... .......... 18% 18.5M 3s
 49000K .......... .......... .......... .......... .......... 18%  146M 3s
 49050K .......... .......... .......... .......... .......... 18%  150M 3s
 49100K .......... .......... .......... .......... .......... 18% 22.4M 3s
 49150K .......... .......... .......... .......... .......... 18% 51.5M 3s
 49200K .......... .......... .......... .......... .......... 18% 23.0M 3s
 49250K .......... .......... .......... .......... .......... 18%  121M 3s
 49300K .......... .......... .......... .......... .......... 18%  417M 3s
 49350K .......... .......... .......... .......... .......... 18% 13.9M 3s
 49400K .......... .......... .......... .......... .......... 18%  341M 3s
 49450K .......... .......... .......... .......... .......... 18%  321M 3s
 49500K .......... .......... .......... .......... .......... 18% 10.3M 3s
 49550K .......... .......... .......... .......... .......... 18%  139M 3s
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 49650K .......... .......... .......... .......... .......... 18% 45.8M 3s
 49700K .......... .......... .......... .......... .......... 18% 69.8M 3s
 49750K .......... .......... .......... .......... .......... 18%  133M 3s
 49800K .......... .......... .......... .......... .......... 19%  148M 3s
 49850K .......... .......... .......... .......... .......... 19% 36.6M 3s
 49900K .......... .......... .......... .......... .......... 19%  143M 3s
 49950K .......... .......... .......... .......... .......... 19%  102M 3s
 50000K .......... .......... .......... .......... .......... 19% 82.3M 3s
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 50100K .......... .......... .......... .......... .......... 19% 75.8M 3s
 50150K .......... .......... .......... .......... .......... 19%  126M 3s
 50200K .......... .......... .......... .......... .......... 19% 26.0M 3s
 50250K .......... .......... .......... .......... .......... 19%  137M 3s
 50300K .......... .......... .......... .......... .......... 19%  143M 3s
 50350K .......... .......... .......... .......... .......... 19% 24.6M 3s
 50400K .......... .......... .......... .......... .......... 19%  121M 3s
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 50550K .......... .......... .......... .......... .......... 19% 15.1M 3s
 50600K .......... .......... .......... .......... .......... 19%  124M 3s
 50650K .......... .......... .......... .......... .......... 19%  148M 3s
 50700K .......... .......... .......... .......... .......... 19% 32.7M 3s
 50750K .......... .......... .......... .......... .......... 19%  145M 3s
 50800K .......... .......... .......... .......... .......... 19%  153M 3s
 50850K .......... .......... .......... .......... .......... 19% 24.8M 3s
 50900K .......... .......... .......... .......... .......... 19%  132M 3s
 50950K .......... .......... .......... .......... .......... 19%  112M 3s
 51000K .......... .......... .......... .......... .......... 19% 41.8M 3s
 51050K .......... .......... .......... .......... .......... 19%  131M 3s
 51100K .......... .......... .......... .......... .......... 19% 76.7M 3s
 51150K .......... .......... .......... .......... .......... 19%  151M 3s
 51200K .......... .......... .......... .......... .......... 19% 68.1M 3s
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 51350K .......... .......... .......... .......... .......... 19% 47.7M 3s
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 51500K .......... .......... .......... .......... .......... 19%  143M 3s
 51550K .......... .......... .......... .......... .......... 19%  150M 3s
 51600K .......... .......... .......... .......... .......... 19% 32.2M 3s
 51650K .......... .......... .......... .......... .......... 19%  379M 3s
 51700K .......... .......... .......... .......... .......... 19% 78.6M 3s
 51750K .......... .......... .......... .......... .......... 19% 73.3M 3s
 51800K .......... .......... .......... .......... .......... 19%  440M 3s
 51850K .......... .......... .......... .......... .......... 19% 86.7M 3s
 51900K .......... .......... .......... .......... .......... 19% 85.1M 3s
 51950K .......... .......... .......... .......... .......... 19%  124M 3s
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 52100K .......... .......... .......... .......... .......... 19% 77.0M 3s
 52150K .......... .......... .......... .......... .......... 19% 95.4M 3s
 52200K .......... .......... .......... .......... .......... 19% 64.8M 3s
 52250K .......... .......... .......... .......... .......... 19%  132M 3s
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 52350K .......... .......... .......... .......... .......... 19% 91.8M 3s
 52400K .......... .......... .......... .......... .......... 20% 49.7M 3s
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 52600K .......... .......... .......... .......... .......... 20% 36.7M 3s
 52650K .......... .......... .......... .......... .......... 20%  421M 3s
 52700K .......... .......... .......... .......... .......... 20% 10.6M 3s
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 52900K .......... .......... .......... .......... .......... 20% 41.0M 3s
 52950K .......... .......... .......... .......... .......... 20% 96.3M 3s
 53000K .......... .......... .......... .......... .......... 20%  104M 3s
 53050K .......... .......... .......... .......... .......... 20% 96.5M 3s
 53100K .......... .......... .......... .......... .......... 20%  102M 3s
 53150K .......... .......... .......... .......... .......... 20% 83.2M 3s
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 53250K .......... .......... .......... .......... .......... 20%  131M 3s
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 53450K .......... .......... .......... .......... .......... 20% 90.1M 3s
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 53600K .......... .......... .......... .......... .......... 20% 88.0M 3s
 53650K .......... .......... .......... .......... .......... 20% 74.8M 3s
 53700K .......... .......... .......... .......... .......... 20% 94.1M 3s
 53750K .......... .......... .......... .......... .......... 20%  166M 3s
 53800K .......... .......... .......... .......... .......... 20% 27.2M 3s
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 53900K .......... .......... .......... .......... .......... 20% 10.4M 3s
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 54000K .......... .......... .......... .......... .......... 20% 38.3M 3s
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 54150K .......... .......... .......... .......... .......... 20%  436M 3s
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 54450K .......... .......... .......... .......... .......... 20% 83.3M 3s
 54500K .......... .......... .......... .......... .......... 20% 97.9M 3s
 54550K .......... .......... .......... .......... .......... 20% 98.2M 3s
 54600K .......... .......... .......... .......... .......... 20% 59.0M 3s
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 54750K .......... .......... .......... .......... .......... 20% 17.8M 3s
 54800K .......... .......... .......... .......... .......... 20%  199M 3s
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 55100K .......... .......... .......... .......... .......... 21% 29.3M 3s
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 55350K .......... .......... .......... .......... .......... 21% 86.7M 3s
 55400K .......... .......... .......... .......... .......... 21%  109M 3s
 55450K .......... .......... .......... .......... .......... 21% 69.1M 3s
 55500K .......... .......... .......... .......... .......... 21%  149M 3s
 55550K .......... .......... .......... .......... .......... 21% 82.8M 3s
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 55700K .......... .......... .......... .......... .......... 21% 68.2M 3s
 55750K .......... .......... .......... .......... .......... 21%  144M 3s
 55800K .......... .......... .......... .......... .......... 21%  106M 3s
 55850K .......... .......... .......... .......... .......... 21% 93.0M 3s
 55900K .......... .......... .......... .......... .......... 21%  138M 3s
 55950K .......... .......... .......... .......... .......... 21% 68.2M 3s
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 57150K .......... .......... .......... .......... .......... 21% 51.5M 3s
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 57900K .......... .......... .......... .......... .......... 22% 96.1M 3s
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 58400K .......... .......... .......... .......... .......... 22% 96.7M 3s
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 60300K .......... .......... .......... .......... .......... 23% 69.1M 3s
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 62800K .......... .......... .......... .......... .......... 23% 45.3M 3s
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 62900K .......... .......... .......... .......... .......... 24% 88.0M 3s
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 67250K .......... .......... .......... .......... .......... 25%  121M 3s
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 68150K .......... .......... .......... .......... .......... 26% 78.0M 3s
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 68850K .......... .......... .......... .......... .......... 26% 94.3M 3s
 68900K .......... .......... .......... .......... .......... 26% 98.0M 3s
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 69500K .......... .......... .......... .......... .......... 26% 92.1M 3s
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 70200K .......... .......... .......... .......... .......... 26% 75.1M 3s
 70250K .......... .......... .......... .......... .......... 26% 76.5M 3s
 70300K .......... .......... .......... .......... .......... 26% 90.9M 3s
 70350K .......... .......... .......... .......... .......... 26% 55.2M 3s
 70400K .......... .......... .......... .......... .......... 26% 75.5M 3s
 70450K .......... .......... .......... .......... .......... 26%  122M 3s
 70500K .......... .......... .......... .......... .......... 26% 61.9M 3s
 70550K .......... .......... .......... .......... .......... 26% 76.2M 3s
 70600K .......... .......... .......... .......... .......... 26% 64.2M 3s
 70650K .......... .......... .......... .......... .......... 26%  120M 3s
 70700K .......... .......... .......... .......... .......... 26% 63.3M 3s
 70750K .......... .......... .......... .......... .......... 27% 75.6M 3s
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 70850K .......... .......... .......... .......... .......... 27% 55.9M 3s
 70900K .......... .......... .......... .......... .......... 27%  127M 3s
 70950K .......... .......... .......... .......... .......... 27% 63.4M 3s
 71000K .......... .......... .......... .......... .......... 27% 72.9M 3s
 71050K .......... .......... .......... .......... .......... 27% 78.8M 3s
 71100K .......... .......... .......... .......... .......... 27% 63.5M 3s
 71150K .......... .......... .......... .......... .......... 27%  120M 3s
 71200K .......... .......... .......... .......... .......... 27% 76.4M 3s
 71250K .......... .......... .......... .......... .......... 27% 54.1M 3s
 71300K .......... .......... .......... .......... .......... 27% 94.1M 3s
 71350K .......... .......... .......... .......... .......... 27% 47.9M 3s
 71400K .......... .......... .......... .......... .......... 27% 94.6M 3s
 71450K .......... .......... .......... .......... .......... 27% 62.2M 3s
 71500K .......... .......... .......... .......... .......... 27% 73.4M 3s
 71550K .......... .......... .......... .......... .......... 27% 56.1M 3s
 71600K .......... .......... .......... .......... .......... 27%  117M 3s
 71650K .......... .......... .......... .......... .......... 27% 76.5M 3s
 71700K .......... .......... .......... .......... .......... 27% 62.4M 3s
 71750K .......... .......... .......... .......... .......... 27% 96.1M 3s
 71800K .......... .......... .......... .......... .......... 27% 65.1M 3s
 71850K .......... .......... .......... .......... .......... 27% 88.9M 3s
 71900K .......... .......... .......... .......... .......... 27% 65.5M 3s
 71950K .......... .......... .......... .......... .......... 27% 72.8M 3s
 72000K .......... .......... .......... .......... .......... 27% 77.8M 3s
 72050K .......... .......... .......... .......... .......... 27% 85.4M 3s
 72100K .......... .......... .......... .......... .......... 27% 54.4M 3s
 72150K .......... .......... .......... .......... .......... 27% 98.6M 3s
 72200K .......... .......... .......... .......... .......... 27% 58.3M 3s
 72250K .......... .......... .......... .......... .......... 27% 86.4M 3s
 72300K .......... .......... .......... .......... .......... 27% 62.7M 3s
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 72400K .......... .......... .......... .......... .......... 27% 42.7M 3s
 72450K .......... .......... .......... .......... .......... 27%  118M 3s
 72500K .......... .......... .......... .......... .......... 27% 79.4M 3s
 72550K .......... .......... .......... .......... .......... 27%  156M 3s
 72600K .......... .......... .......... .......... .......... 27% 96.5M 3s
 72650K .......... .......... .......... .......... .......... 27% 97.3M 3s
 72700K .......... .......... .......... .......... .......... 27% 92.5M 3s
 72750K .......... .......... .......... .......... .......... 27%  101M 3s
 72800K .......... .......... .......... .......... .......... 27% 27.7M 3s
 72850K .......... .......... .......... .......... .......... 27%  131M 3s
 72900K .......... .......... .......... .......... .......... 27%  291M 3s
 72950K .......... .......... .......... .......... .......... 27%  273M 3s
 73000K .......... .......... .......... .......... .......... 27%  229M 3s
 73050K .......... .......... .......... .......... .......... 27% 54.6M 3s
 73100K .......... .......... .......... .......... .......... 27%  174M 3s
 73150K .......... .......... .......... .......... .......... 27%  391M 3s
 73200K .......... .......... .......... .......... .......... 27%  134M 3s
 73250K .......... .......... .......... .......... .......... 27% 78.5M 3s
 73300K .......... .......... .......... .......... .......... 27% 74.9M 3s
 73350K .......... .......... .......... .......... .......... 27% 63.8M 3s
 73400K .......... .......... .......... .......... .......... 28%  124M 3s
 73450K .......... .......... .......... .......... .......... 28% 61.1M 3s
 73500K .......... .......... .......... .......... .......... 28% 98.6M 3s
 73550K .......... .......... .......... .......... .......... 28% 88.5M 3s
 73600K .......... .......... .......... .......... .......... 28% 65.5M 3s
 73650K .......... .......... .......... .......... .......... 28% 94.3M 3s
 73700K .......... .......... .......... .......... .......... 28% 48.8M 3s
 73750K .......... .......... .......... .......... .......... 28% 59.9M 3s
 73800K .......... .......... .......... .......... .......... 28%  119M 3s
 73850K .......... .......... .......... .......... .......... 28% 63.6M 3s
 73900K .......... .......... .......... .......... .......... 28% 95.4M 3s
 73950K .......... .......... .......... .......... .......... 28% 62.2M 3s
 74000K .......... .......... .......... .......... .......... 28% 91.8M 3s
 74050K .......... .......... .......... .......... .......... 28% 98.6M 3s
 74100K .......... .......... .......... .......... .......... 28% 61.7M 3s
 74150K .......... .......... .......... .......... .......... 28% 76.3M 3s
 74200K .......... .......... .......... .......... .......... 28% 93.7M 3s
 74250K .......... .......... .......... .......... .......... 28% 64.8M 3s
 74300K .......... .......... .......... .......... .......... 28%  119M 3s
 74350K .......... .......... .......... .......... .......... 28% 63.4M 3s
 74400K .......... .......... .......... .......... .......... 28% 96.9M 3s
 74450K .......... .......... .......... .......... .......... 28% 63.4M 3s
 74500K .......... .......... .......... .......... .......... 28% 75.2M 3s
 74550K .......... .......... .......... .......... .......... 28%  180M 3s
 74600K .......... .......... .......... .......... .......... 28% 60.7M 3s
 74650K .......... .......... .......... .......... .......... 28%  105M 3s
 74700K .......... .......... .......... .......... .......... 28% 63.2M 3s
 74750K .......... .......... .......... .......... .......... 28% 75.8M 3s
 74800K .......... .......... .......... .......... .......... 28% 92.1M 3s
 74850K .......... .......... .......... .......... .......... 28% 62.6M 3s
 74900K .......... .......... .......... .......... .......... 28%  119M 3s
 74950K .......... .......... .......... .......... .......... 28% 62.4M 3s
 75000K .......... .......... .......... .......... .......... 28% 64.6M 3s
 75050K .......... .......... .......... .......... .......... 28%  115M 3s
 75100K .......... .......... .......... .......... .......... 28% 62.8M 3s
 75150K .......... .......... .......... .......... .......... 28% 94.8M 3s
 75200K .......... .......... .......... .......... .......... 28% 57.0M 3s
 75250K .......... .......... .......... .......... .......... 28% 96.3M 3s
 75300K .......... .......... .......... .......... .......... 28% 68.2M 3s
 75350K .......... .......... .......... .......... .......... 28% 75.7M 3s
 75400K .......... .......... .......... .......... .......... 28% 93.2M 3s
 75450K .......... .......... .......... .......... .......... 28% 62.0M 3s
 75500K .......... .......... .......... .......... .......... 28% 75.2M 3s
 75550K .......... .......... .......... .......... .......... 28%  101M 3s
 75600K .......... .......... .......... .......... .......... 28% 61.3M 3s
 75650K .......... .......... .......... .......... .......... 28% 77.9M 3s
 75700K .......... .......... .......... .......... .......... 28% 73.2M 3s
 75750K .......... .......... .......... .......... .......... 28% 97.7M 3s
 75800K .......... .......... .......... .......... .......... 28% 75.0M 3s
 75850K .......... .......... .......... .......... .......... 28% 73.3M 3s
 75900K .......... .......... .......... .......... .......... 28% 94.6M 3s
 75950K .......... .......... .......... .......... .......... 28% 77.3M 3s
 76000K .......... .......... .......... .......... .......... 29%  122M 3s
 76050K .......... .......... .......... .......... .......... 29% 97.1M 3s
 76100K .......... .......... .......... .......... .......... 29%  121M 3s
 76150K .......... .......... .......... .......... .......... 29% 97.7M 3s
 76200K .......... .......... .......... .......... .......... 29% 93.9M 3s
 76250K .......... .......... .......... .......... .......... 29%  117M 3s
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 76350K .......... .......... .......... .......... .......... 29% 19.9M 3s
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 76800K .......... .......... .......... .......... .......... 29%  125M 3s
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 76900K .......... .......... .......... .......... .......... 29% 59.3M 3s
 76950K .......... .......... .......... .......... .......... 29%  173M 3s
 77000K .......... .......... .......... .......... .......... 29% 97.3M 3s
 77050K .......... .......... .......... .......... .......... 29%  479M 3s
 77100K .......... .......... .......... .......... .......... 29%  330M 2s
 77150K .......... .......... .......... .......... .......... 29%  102M 2s
 77200K .......... .......... .......... .......... .......... 29% 63.7M 2s
 77250K .......... .......... .......... .......... .......... 29% 73.1M 2s
 77300K .......... .......... .......... .......... .......... 29% 30.9M 2s
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 77400K .......... .......... .......... .......... .......... 29%  121M 2s
 77450K .......... .......... .......... .......... .......... 29% 63.7M 2s
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 77600K .......... .......... .......... .......... .......... 29% 63.5M 2s
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 77700K .......... .......... .......... .......... .......... 29% 61.7M 2s
 77750K .......... .......... .......... .......... .......... 29% 78.1M 2s
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 77850K .......... .......... .......... .......... .......... 29% 63.7M 2s
 77900K .......... .......... .......... .......... .......... 29% 89.3M 2s
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 78000K .......... .......... .......... .......... .......... 29% 75.7M 2s
 78050K .......... .......... .......... .......... .......... 29% 93.2M 2s
 78100K .......... .......... .......... .......... .......... 29% 76.3M 2s
 78150K .......... .......... .......... .......... .......... 29% 75.0M 2s
 78200K .......... .......... .......... .......... .......... 29% 65.4M 2s
 78250K .......... .......... .......... .......... .......... 29%  121M 2s
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 78400K .......... .......... .......... .......... .......... 29% 40.6M 2s
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 78700K .......... .......... .......... .......... .......... 30% 57.5M 2s
 78750K .......... .......... .......... .......... .......... 30% 27.1M 2s
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 78900K .......... .......... .......... .......... .......... 30% 32.8M 2s
 78950K .......... .......... .......... .......... .......... 30%  191M 2s
 79000K .......... .......... .......... .......... .......... 30% 28.9M 2s
 79050K .......... .......... .......... .......... .......... 30% 23.9M 2s
 79100K .......... .......... .......... .......... .......... 30%  425M 2s
 79150K .......... .......... .......... .......... .......... 30% 14.1M 3s
 79200K .......... .......... .......... .......... .......... 30% 93.9M 2s
 79250K .......... .......... .......... .......... .......... 30% 30.7M 3s
 79300K .......... .......... .......... .......... .......... 30%  519M 2s
 79350K .......... .......... .......... .......... .......... 30% 39.4M 2s
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 79450K .......... .......... .......... .......... .......... 30% 98.2M 2s
 79500K .......... .......... .......... .......... .......... 30% 49.2M 2s
 79550K .......... .......... .......... .......... .......... 30% 90.9M 2s
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 80000K .......... .......... .......... .......... .......... 30% 19.7M 2s
 80050K .......... .......... .......... .......... .......... 30%  186M 2s
 80100K .......... .......... .......... .......... .......... 30% 22.1M 2s
 80150K .......... .......... .......... .......... .......... 30%  470M 2s
 80200K .......... .......... .......... .......... .......... 30% 33.0M 2s
 80250K .......... .......... .......... .......... .......... 30%  341M 2s
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 80500K .......... .......... .......... .......... .......... 30% 62.7M 2s
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 80800K .......... .......... .......... .......... .......... 30% 87.0M 2s
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 80900K .......... .......... .......... .......... .......... 30% 79.3M 2s
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 81000K .......... .......... .......... .......... .......... 30% 52.0M 2s
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 81200K .......... .......... .......... .......... .......... 30%  328M 2s
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 81450K .......... .......... .......... .......... .......... 31% 97.9M 2s
 81500K .......... .......... .......... .......... .......... 31%  170M 2s
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 81600K .......... .......... .......... .......... .......... 31% 97.5M 2s
 81650K .......... .......... .......... .......... .......... 31% 64.8M 2s
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 81800K .......... .......... .......... .......... .......... 31%  111M 2s
 81850K .......... .......... .......... .......... .......... 31% 85.7M 2s
 81900K .......... .......... .......... .......... .......... 31% 61.3M 2s
 81950K .......... .......... .......... .......... .......... 31% 60.0M 2s
 82000K .......... .......... .......... .......... .......... 31% 93.9M 2s
 82050K .......... .......... .......... .......... .......... 31%  117M 2s
 82100K .......... .......... .......... .......... .......... 31% 28.6M 2s
 82150K .......... .......... .......... .......... .......... 31%  370M 2s
 82200K .......... .......... .......... .......... .......... 31% 28.3M 2s
 82250K .......... .......... .......... .......... .......... 31%  456M 2s
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 82350K .......... .......... .......... .......... .......... 31% 42.0M 2s
 82400K .......... .......... .......... .......... .......... 31% 93.5M 2s
 82450K .......... .......... .......... .......... .......... 31% 98.6M 2s
 82500K .......... .......... .......... .......... .......... 31% 34.7M 2s
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 82600K .......... .......... .......... .......... .......... 31% 31.9M 2s
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 82700K .......... .......... .......... .......... .......... 31%  135M 2s
 82750K .......... .......... .......... .......... .......... 31% 43.4M 2s
 82800K .......... .......... .......... .......... .......... 31% 16.2M 2s
 82850K .......... .......... .......... .......... .......... 31%  159M 2s
 82900K .......... .......... .......... .......... .......... 31% 31.8M 2s
 82950K .......... .......... .......... .......... .......... 31%  452M 2s
 83000K .......... .......... .......... .......... .......... 31%  183M 2s
 83050K .......... .......... .......... .......... .......... 31% 31.7M 2s
 83100K .......... .......... .......... .......... .......... 31%  440M 2s
 83150K .......... .......... .......... .......... .......... 31% 18.6M 2s
 83200K .......... .......... .......... .......... .......... 31%  156M 2s
 83250K .......... .......... .......... .......... .......... 31%  192M 2s
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 83400K .......... .......... .......... .......... .......... 31% 59.8M 2s
 83450K .......... .......... .......... .......... .......... 31% 87.5M 2s
 83500K .......... .......... .......... .......... .......... 31%  135M 2s
 83550K .......... .......... .......... .......... .......... 31% 75.6M 2s
 83600K .......... .......... .......... .......... .......... 31%  111M 2s
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 83700K .......... .......... .......... .......... .......... 31% 95.4M 2s
 83750K .......... .......... .......... .......... .......... 31% 87.8M 2s
 83800K .......... .......... .......... .......... .......... 31%  117M 2s
 83850K .......... .......... .......... .......... .......... 31% 69.8M 2s
 83900K .......... .......... .......... .......... .......... 32% 96.5M 2s
 83950K .......... .......... .......... .......... .......... 32% 84.8M 2s
 84000K .......... .......... .......... .......... .......... 32% 93.2M 2s
 84050K .......... .......... .......... .......... .......... 32%  130M 2s
 84100K .......... .......... .......... .......... .......... 32% 90.3M 2s
 84150K .......... .......... .......... .......... .......... 32%  127M 2s
 84200K .......... .......... .......... .......... .......... 32% 21.3M 2s
 84250K .......... .......... .......... .......... .......... 32%  332M 2s
 84300K .......... .......... .......... .......... .......... 32% 19.8M 2s
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 84550K .......... .......... .......... .......... .......... 32%  531M 2s
 84600K .......... .......... .......... .......... .......... 32% 39.6M 2s
 84650K .......... .......... .......... .......... .......... 32%  108M 2s
 84700K .......... .......... .......... .......... .......... 32% 89.8M 2s
 84750K .......... .......... .......... .......... .......... 32%  108M 2s
 84800K .......... .......... .......... .......... .......... 32%  106M 2s
 84850K .......... .......... .......... .......... .......... 32%  108M 2s
 84900K .......... .......... .......... .......... .......... 32%  108M 2s
 84950K .......... .......... .......... .......... .......... 32% 93.7M 2s
 85000K .......... .......... .......... .......... .......... 32% 98.8M 2s
 85050K .......... .......... .......... .......... .......... 32%  104M 2s
 85100K .......... .......... .......... .......... .......... 32% 62.9M 2s
 85150K .......... .......... .......... .......... .......... 32%  136M 2s
 85200K .......... .......... .......... .......... .......... 32%  108M 2s
 85250K .......... .......... .......... .......... .......... 32%  124M 2s
 85300K .......... .......... .......... .......... .......... 32% 95.9M 2s
 85350K .......... .......... .......... .......... .......... 32%  110M 2s
 85400K .......... .......... .......... .......... .......... 32% 87.8M 2s
 85450K .......... .......... .......... .......... .......... 32%  101M 2s
 85500K .......... .......... .......... .......... .......... 32% 36.3M 2s
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 85650K .......... .......... .......... .......... .......... 32% 40.3M 2s
 85700K .......... .......... .......... .......... .......... 32% 13.0M 2s
 85750K .......... .......... .......... .......... .......... 32%  164M 2s
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 85850K .......... .......... .......... .......... .......... 32% 37.7M 2s
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 85950K .......... .......... .......... .......... .......... 32% 68.8M 2s
 86000K .......... .......... .......... .......... .......... 32%  138M 2s
 86050K .......... .......... .......... .......... .......... 32% 98.2M 2s
 86100K .......... .......... .......... .......... .......... 32% 93.2M 2s
 86150K .......... .......... .......... .......... .......... 32%  120M 2s
 86200K .......... .......... .......... .......... .......... 32% 93.5M 2s
 86250K .......... .......... .......... .......... .......... 32%  124M 2s
 86300K .......... .......... .......... .......... .......... 32% 91.8M 2s
 86350K .......... .......... .......... .......... .......... 32% 95.9M 2s
 86400K .......... .......... .......... .......... .......... 32%  120M 2s
 86450K .......... .......... .......... .......... .......... 32% 75.4M 2s
 86500K .......... .......... .......... .......... .......... 33%  131M 2s
 86550K .......... .......... .......... .......... .......... 33%  120M 2s
 86600K .......... .......... .......... .......... .......... 33% 91.8M 2s
 86650K .......... .......... .......... .......... .......... 33% 28.4M 2s
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 87000K .......... .......... .......... .......... .......... 33% 97.1M 2s
 87050K .......... .......... .......... .......... .......... 33%  119M 2s
 87100K .......... .......... .......... .......... .......... 33% 64.6M 2s
 87150K .......... .......... .......... .......... .......... 33%  149M 2s
 87200K .......... .......... .......... .......... .......... 33% 67.5M 2s
 87250K .......... .......... .......... .......... .......... 33%  121M 2s
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 87350K .......... .......... .......... .......... .......... 33% 75.6M 2s
 87400K .......... .......... .......... .......... .......... 33%  124M 2s
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 87700K .......... .......... .......... .......... .......... 33% 62.4M 2s
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 87900K .......... .......... .......... .......... .......... 33% 83.9M 2s
 87950K .......... .......... .......... .......... .......... 33% 63.0M 2s
 88000K .......... .......... .......... .......... .......... 33%  126M 2s
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 88100K .......... .......... .......... .......... .......... 33% 92.3M 2s
 88150K .......... .......... .......... .......... .......... 33% 94.3M 2s
 88200K .......... .......... .......... .......... .......... 33% 96.1M 2s
 88250K .......... .......... .......... .......... .......... 33% 94.4M 2s
 88300K .......... .......... .......... .......... .......... 33% 97.3M 2s
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 88450K .......... .......... .......... .......... .......... 33% 88.0M 2s
 88500K .......... .......... .......... .......... .......... 33%  103M 2s
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 88650K .......... .......... .......... .......... .......... 33%  125M 2s
 88700K .......... .......... .......... .......... .......... 33% 76.7M 2s
 88750K .......... .......... .......... .......... .......... 33%  120M 2s
 88800K .......... .......... .......... .......... .......... 33% 77.1M 2s
 88850K .......... .......... .......... .......... .......... 33%  120M 2s
 88900K .......... .......... .......... .......... .......... 33% 76.5M 2s
 88950K .......... .......... .......... .......... .......... 33% 93.4M 2s
 89000K .......... .......... .......... .......... .......... 33% 90.9M 2s
 89050K .......... .......... .......... .......... .......... 33% 97.5M 2s
 89100K .......... .......... .......... .......... .......... 33% 92.3M 2s
 89150K .......... .......... .......... .......... .......... 34% 94.1M 2s
 89200K .......... .......... .......... .......... .......... 34% 89.6M 2s
 89250K .......... .......... .......... .......... .......... 34% 79.5M 2s
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 89550K .......... .......... .......... .......... .......... 34%  120M 2s
 89600K .......... .......... .......... .......... .......... 34% 76.7M 2s
 89650K .......... .......... .......... .......... .......... 34%  121M 2s
 89700K .......... .......... .......... .......... .......... 34% 77.0M 2s
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 90000K .......... .......... .......... .......... .......... 34%  122M 2s
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 90100K .......... .......... .......... .......... .......... 34% 81.1M 2s
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 90900K .......... .......... .......... .......... .......... 34% 75.9M 2s
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 91600K .......... .......... .......... .......... .......... 34% 69.6M 2s
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 91700K .......... .......... .......... .......... .......... 34% 27.4M 2s
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 92050K .......... .......... .......... .......... .......... 35% 86.6M 2s
 92100K .......... .......... .......... .......... .......... 35% 94.3M 2s
 92150K .......... .......... .......... .......... .......... 35%  121M 2s
 92200K .......... .......... .......... .......... .......... 35% 65.2M 2s
 92250K .......... .......... .......... .......... .......... 35% 69.2M 2s
 92300K .......... .......... .......... .......... .......... 35%  188M 2s
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 92400K .......... .......... .......... .......... .......... 35% 97.9M 2s
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 92500K .......... .......... .......... .......... .......... 35%  117M 2s
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 92600K .......... .......... .......... .......... .......... 35% 94.1M 2s
 92650K .......... .......... .......... .......... .......... 35%  121M 2s
 92700K .......... .......... .......... .......... .......... 35% 77.8M 2s
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 92800K .......... .......... .......... .......... .......... 35% 93.7M 2s
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 92900K .......... .......... .......... .......... .......... 35% 97.5M 2s
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 93000K .......... .......... .......... .......... .......... 35%  119M 2s
 93050K .......... .......... .......... .......... .......... 35% 78.1M 2s
 93100K .......... .......... .......... .......... .......... 35%  121M 2s
 93150K .......... .......... .......... .......... .......... 35% 76.4M 2s
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 93250K .......... .......... .......... .......... .......... 35% 94.4M 2s
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 93600K .......... .......... .......... .......... .......... 35% 75.1M 2s
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 93850K .......... .......... .......... .......... .......... 35% 75.7M 2s
 93900K .......... .......... .......... .......... .......... 35%  127M 2s
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 94000K .......... .......... .......... .......... .......... 35% 77.8M 2s
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 94100K .......... .......... .......... .......... .......... 35% 74.0M 2s
 94150K .......... .......... .......... .......... .......... 35% 98.6M 2s
 94200K .......... .......... .......... .......... .......... 35% 86.7M 2s
 94250K .......... .......... .......... .......... .......... 35% 80.8M 2s
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 94350K .......... .......... .......... .......... .......... 36% 94.3M 2s
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 94950K .......... .......... .......... .......... .......... 36% 75.4M 2s
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 95150K .......... .......... .......... .......... .......... 36% 94.4M 2s
 95200K .......... .......... .......... .......... .......... 36% 93.5M 2s
 95250K .......... .......... .......... .......... .......... 36%  121M 2s
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 96050K .......... .......... .......... .......... .......... 36% 27.6M 2s
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 97000K .......... .......... .......... .......... .......... 37% 62.0M 2s
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 97100K .......... .......... .......... .......... .......... 37% 48.2M 2s
 97150K .......... .......... .......... .......... .......... 37% 63.7M 2s
 97200K .......... .......... .......... .......... .......... 37% 62.8M 2s
 97250K .......... .......... .......... .......... .......... 37% 54.2M 2s
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 97600K .......... .......... .......... .......... .......... 37% 53.8M 2s
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 97800K .......... .......... .......... .......... .......... 37%  112M 2s
 97850K .......... .......... .......... .......... .......... 37% 39.2M 2s
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 98000K .......... .......... .......... .......... .......... 37% 64.1M 2s
 98050K .......... .......... .......... .......... .......... 37% 78.0M 2s
 98100K .......... .......... .......... .......... .......... 37% 69.3M 2s
 98150K .......... .......... .......... .......... .......... 37%  101M 2s
 98200K .......... .......... .......... .......... .......... 37% 94.3M 2s
 98250K .......... .......... .......... .......... .......... 37% 97.5M 2s
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 98350K .......... .......... .......... .......... .......... 37%  119M 2s
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 98450K .......... .......... .......... .......... .......... 37% 94.3M 2s
 98500K .......... .......... .......... .......... .......... 37%  126M 2s
 98550K .......... .......... .......... .......... .......... 37% 95.9M 2s
 98600K .......... .......... .......... .......... .......... 37% 23.0M 2s
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 98900K .......... .......... .......... .......... .......... 37%  119M 2s
 98950K .......... .......... .......... .......... .......... 37%  263M 2s
 99000K .......... .......... .......... .......... .......... 37%  404M 2s
 99050K .......... .......... .......... .......... .......... 37%  234M 2s
 99100K .......... .......... .......... .......... .......... 37% 95.0M 2s
 99150K .......... .......... .......... .......... .......... 37% 91.6M 2s
 99200K .......... .......... .......... .......... .......... 37% 93.7M 2s
 99250K .......... .......... .......... .......... .......... 37% 99.9M 2s
 99300K .......... .......... .......... .......... .......... 37% 94.6M 2s
 99350K .......... .......... .......... .......... .......... 37% 93.9M 2s
 99400K .......... .......... .......... .......... .......... 37% 75.6M 2s
 99450K .......... .......... .......... .......... .......... 37% 94.4M 2s
 99500K .......... .......... .......... .......... .......... 37% 94.6M 2s
 99550K .......... .......... .......... .......... .......... 37%  121M 2s
 99600K .......... .......... .......... .......... .......... 38% 77.3M 2s
 99650K .......... .......... .......... .......... .......... 38%  120M 2s
 99700K .......... .......... .......... .......... .......... 38% 93.4M 2s
 99750K .......... .......... .......... .......... .......... 38% 95.7M 2s
 99800K .......... .......... .......... .......... .......... 38% 97.5M 2s
 99850K .......... .......... .......... .......... .......... 38% 91.6M 2s
 99900K .......... .......... .......... .......... .......... 38% 97.3M 2s
 99950K .......... .......... .......... .......... .......... 38% 92.1M 2s
100000K .......... .......... .......... .......... .......... 38% 97.7M 2s
100050K .......... .......... .......... .......... .......... 38% 94.4M 2s
100100K .......... .......... .......... .......... .......... 38% 93.9M 2s
100150K .......... .......... .......... .......... .......... 38% 93.4M 2s
100200K .......... .......... .......... .......... .......... 38% 95.0M 2s
100250K .......... .......... .......... .......... .......... 38% 92.5M 2s
100300K .......... .......... .......... .......... .......... 38% 95.2M 2s
100350K .......... .......... .......... .......... .......... 38% 91.6M 2s
100400K .......... .......... .......... .......... .......... 38%  127M 2s
100450K .......... .......... .......... .......... .......... 38% 76.2M 2s
100500K .......... .......... .......... .......... .......... 38%  120M 2s
100550K .......... .......... .......... .......... .......... 38% 97.7M 2s
100600K .......... .......... .......... .......... .......... 38% 90.3M 2s
100650K .......... .......... .......... .......... .......... 38% 95.4M 2s
100700K .......... .......... .......... .......... .......... 38% 91.1M 2s
100750K .......... .......... .......... .......... .......... 38% 99.2M 2s
100800K .......... .......... .......... .......... .......... 38% 97.9M 2s
100850K .......... .......... .......... .......... .......... 38% 91.1M 2s
100900K .......... .......... .......... .......... .......... 38% 97.7M 2s
100950K .......... .......... .......... .......... .......... 38% 94.8M 2s
101000K .......... .......... .......... .......... .......... 38% 94.6M 2s
101050K .......... .......... .......... .......... .......... 38%  120M 2s
101100K .......... .......... .......... .......... .......... 38% 76.5M 2s
101150K .......... .......... .......... .......... .......... 38%  119M 2s
101200K .......... .......... .......... .......... .......... 38% 78.3M 2s
101250K .......... .......... .......... .......... .......... 38% 91.1M 2s
101300K .......... .......... .......... .......... .......... 38%  123M 2s
101350K .......... .......... .......... .......... .......... 38% 98.4M 2s
101400K .......... .......... .......... .......... .......... 38% 92.8M 2s
101450K .......... .......... .......... .......... .......... 38% 82.5M 2s
101500K .......... .......... .......... .......... .......... 38%  101M 2s
101550K .......... .......... .......... .......... .......... 38% 85.4M 2s
101600K .......... .......... .......... .......... .......... 38%  103M 2s
101650K .......... .......... .......... .......... .......... 38% 79.9M 2s
101700K .......... .......... .......... .......... .......... 38% 94.6M 2s
101750K .......... .......... .......... .......... .......... 38% 94.3M 2s
101800K .......... .......... .......... .......... .......... 38%  119M 2s
101850K .......... .......... .......... .......... .......... 38% 77.3M 2s
101900K .......... .......... .......... .......... .......... 38% 94.3M 2s
101950K .......... .......... .......... .......... .......... 38% 95.2M 2s
102000K .......... .......... .......... .......... .......... 38% 95.0M 2s
102050K .......... .......... .......... .......... .......... 38%  119M 2s
102100K .......... .......... .......... .......... .......... 38% 94.8M 2s
102150K .......... .......... .......... .......... .......... 38% 95.2M 2s
102200K .......... .......... .......... .......... .......... 38% 77.3M 2s
102250K .......... .......... .......... .......... .......... 39%  123M 2s
102300K .......... .......... .......... .......... .......... 39% 94.3M 2s
102350K .......... .......... .......... .......... .......... 39% 92.7M 2s
102400K .......... .......... .......... .......... .......... 39% 96.7M 2s
102450K .......... .......... .......... .......... .......... 39% 91.4M 2s
102500K .......... .......... .......... .......... .......... 39%  125M 2s
102550K .......... .......... .......... .......... .......... 39% 98.8M 2s
102600K .......... .......... .......... .......... .......... 39% 94.1M 2s
102650K .......... .......... .......... .......... .......... 39%  120M 2s
102700K .......... .......... .......... .......... .......... 39% 93.4M 2s
102750K .......... .......... .......... .......... .......... 39% 19.9M 2s
102800K .......... .......... .......... .......... .......... 39%  474M 2s
102850K .......... .......... .......... .......... .......... 39%  400M 2s
102900K .......... .......... .......... .......... .......... 39%  483M 2s
102950K .......... .......... .......... .......... .......... 39%  113M 2s
103000K .......... .......... .......... .......... .......... 39%  519M 2s
103050K .......... .......... .......... .......... .......... 39% 41.0M 2s
103100K .......... .......... .......... .......... .......... 39%  131M 2s
103150K .......... .......... .......... .......... .......... 39%  174M 2s
103200K .......... .......... .......... .......... .......... 39%  151M 2s
103250K .......... .......... .......... .......... .......... 39%  183M 2s
103300K .......... .......... .......... .......... .......... 39%  175M 2s
103350K .......... .......... .......... .......... .......... 39%  148M 2s
103400K .......... .......... .......... .......... .......... 39%  124M 2s
103450K .......... .......... .......... .......... .......... 39% 92.7M 2s
103500K .......... .......... .......... .......... .......... 39% 76.8M 2s
103550K .......... .......... .......... .......... .......... 39%  126M 2s
103600K .......... .......... .......... .......... .......... 39% 75.2M 2s
103650K .......... .......... .......... .......... .......... 39%  120M 2s
103700K .......... .......... .......... .......... .......... 39% 77.4M 2s
103750K .......... .......... .......... .......... .......... 39%  120M 2s
103800K .......... .......... .......... .......... .......... 39% 94.8M 2s
103850K .......... .......... .......... .......... .......... 39% 93.4M 2s
103900K .......... .......... .......... .......... .......... 39% 96.1M 2s
103950K .......... .......... .......... .......... .......... 39% 92.8M 2s
104000K .......... .......... .......... .......... .......... 39% 95.0M 2s
104050K .......... .......... .......... .......... .......... 39% 95.0M 2s
104100K .......... .......... .......... .......... .......... 39% 98.0M 2s
104150K .......... .......... .......... .......... .......... 39% 92.8M 2s
104200K .......... .......... .......... .......... .......... 39% 93.5M 2s
104250K .......... .......... .......... .......... .......... 39% 96.3M 2s
104300K .......... .......... .......... .......... .......... 39% 94.4M 2s
104350K .......... .......... .......... .......... .......... 39% 94.6M 2s
104400K .......... .......... .......... .......... .......... 39%  119M 2s
104450K .......... .......... .......... .......... .......... 39% 77.8M 2s
104500K .......... .......... .......... .......... .......... 39% 95.4M 2s
104550K .......... .......... .......... .......... .......... 39%  120M 2s
104600K .......... .......... .......... .......... .......... 39% 77.9M 2s
104650K .......... .......... .......... .......... .......... 39%  120M 2s
104700K .......... .......... .......... .......... .......... 39% 77.0M 2s
104750K .......... .......... .......... .......... .......... 39% 94.8M 2s
104800K .......... .......... .......... .......... .......... 39%  125M 2s
104850K .......... .......... .......... .......... .......... 40% 90.1M 2s
104900K .......... .......... .......... .......... .......... 40% 99.6M 2s
104950K .......... .......... .......... .......... .......... 40% 91.3M 2s
105000K .......... .......... .......... .......... .......... 40% 95.0M 2s
105050K .......... .......... .......... .......... .......... 40% 97.5M 2s
105100K .......... .......... .......... .......... .......... 40% 94.8M 2s
105150K .......... .......... .......... .......... .......... 40% 79.4M 2s
105200K .......... .......... .......... .......... .......... 40%  124M 2s
105250K .......... .......... .......... .......... .......... 40% 79.5M 2s
105300K .......... .......... .......... .......... .......... 40%  123M 2s
105350K .......... .......... .......... .......... .......... 40% 77.5M 2s
105400K .......... .......... .......... .......... .......... 40%  119M 2s
105450K .......... .......... .......... .......... .......... 40% 77.3M 2s
105500K .......... .......... .......... .......... .......... 40% 95.4M 2s
105550K .......... .......... .......... .......... .......... 40%  126M 2s
105600K .......... .......... .......... .......... .......... 40% 91.4M 2s
105650K .......... .......... .......... .......... .......... 40% 96.7M 2s
105700K .......... .......... .......... .......... .......... 40% 75.1M 2s
105750K .......... .......... .......... .......... .......... 40%  127M 2s
105800K .......... .......... .......... .......... .......... 40% 94.3M 2s
105850K .......... .......... .......... .......... .......... 40% 93.9M 2s
105900K .......... .......... .......... .......... .......... 40% 95.0M 2s
105950K .......... .......... .......... .......... .......... 40% 92.7M 2s
106000K .......... .......... .......... .......... .......... 40% 97.5M 2s
106050K .......... .......... .......... .......... .......... 40%  119M 2s
106100K .......... .......... .......... .......... .......... 40% 78.5M 2s
106150K .......... .......... .......... .......... .......... 40%  119M 2s
106200K .......... .......... .......... .......... .......... 40% 77.8M 2s
106250K .......... .......... .......... .......... .......... 40%  120M 2s
106300K .......... .......... .......... .......... .......... 40% 98.4M 2s
106350K .......... .......... .......... .......... .......... 40% 91.4M 2s
106400K .......... .......... .......... .......... .......... 40% 94.8M 2s
106450K .......... .......... .......... .......... .......... 40% 47.9M 2s
106500K .......... .......... .......... .......... .......... 40%  488M 2s
106550K .......... .......... .......... .......... .......... 40% 61.3M 2s
106600K .......... .......... .......... .......... .......... 40%  120M 2s
106650K .......... .......... .......... .......... .......... 40% 97.3M 2s
106700K .......... .......... .......... .......... .......... 40% 93.4M 2s
106750K .......... .......... .......... .......... .......... 40% 92.3M 2s
106800K .......... .......... .......... .......... .......... 40%  122M 2s
106850K .......... .......... .......... .......... .......... 40% 71.6M 2s
106900K .......... .......... .......... .......... .......... 40%  168M 2s
106950K .......... .......... .......... .......... .......... 40% 69.1M 2s
107000K .......... .......... .......... .......... .......... 40%  121M 2s
107050K .......... .......... .......... .......... .......... 40%  126M 2s
107100K .......... .......... .......... .......... .......... 40% 95.2M 2s
107150K .......... .......... .......... .......... .......... 40% 97.7M 2s
107200K .......... .......... .......... .......... .......... 40%  119M 2s
107250K .......... .......... .......... .......... .......... 40% 96.7M 2s
107300K .......... .......... .......... .......... .......... 40%  122M 2s
107350K .......... .......... .......... .......... .......... 40% 17.3M 2s
107400K .......... .......... .......... .......... .......... 40%  461M 2s
107450K .......... .......... .......... .......... .......... 40%  440M 2s
107500K .......... .......... .......... .......... .......... 41%  180M 2s
107550K .......... .......... .......... .......... .......... 41%  514M 2s
107600K .......... .......... .......... .......... .......... 41%  456M 2s
107650K .......... .......... .......... .......... .......... 41% 67.3M 2s
107700K .......... .......... .......... .......... .......... 41% 84.3M 2s
107750K .......... .......... .......... .......... .......... 41%  243M 2s
107800K .......... .......... .......... .......... .......... 41%  452M 2s
107850K .......... .......... .......... .......... .......... 41%  241M 2s
107900K .......... .......... .......... .......... .......... 41%  119M 2s
107950K .......... .......... .......... .......... .......... 41% 75.5M 2s
108000K .......... .......... .......... .......... .......... 41% 78.0M 2s
108050K .......... .......... .......... .......... .......... 41%  125M 2s
108100K .......... .......... .......... .......... .......... 41% 90.8M 2s
108150K .......... .......... .......... .......... .......... 41% 94.3M 2s
108200K .......... .......... .......... .......... .......... 41% 76.9M 2s
108250K .......... .......... .......... .......... .......... 41%  102M 2s
108300K .......... .......... .......... .......... .......... 41% 87.2M 2s
108350K .......... .......... .......... .......... .......... 41% 75.9M 2s
108400K .......... .......... .......... .......... .......... 41% 92.7M 2s
108450K .......... .......... .......... .......... .......... 41% 75.5M 2s
108500K .......... .......... .......... .......... .......... 41%  126M 2s
108550K .......... .......... .......... .......... .......... 41% 92.0M 2s
108600K .......... .......... .......... .......... .......... 41% 78.1M 2s
108650K .......... .......... .......... .......... .......... 41%  120M 2s
108700K .......... .......... .......... .......... .......... 41% 77.4M 2s
108750K .......... .......... .......... .......... .......... 41%  123M 2s
108800K .......... .......... .......... .......... .......... 41% 92.0M 2s
108850K .......... .......... .......... .......... .......... 41% 78.6M 2s
108900K .......... .......... .......... .......... .......... 41% 90.9M 2s
108950K .......... .......... .......... .......... .......... 41% 91.8M 2s
109000K .......... .......... .......... .......... .......... 41% 98.0M 2s
109050K .......... .......... .......... .......... .......... 41% 93.9M 2s
109100K .......... .......... .......... .......... .......... 41% 91.4M 2s
109150K .......... .......... .......... .......... .......... 41% 98.0M 2s
109200K .......... .......... .......... .......... .......... 41% 81.5M 2s
109250K .......... .......... .......... .......... .......... 41%  107M 2s
109300K .......... .......... .......... .......... .......... 41% 93.0M 2s
109350K .......... .......... .......... .......... .......... 41% 86.9M 2s
109400K .......... .......... .......... .......... .......... 41%  103M 2s
109450K .......... .......... .......... .......... .......... 41% 93.4M 2s
109500K .......... .......... .......... .......... .......... 41% 75.4M 2s
109550K .......... .......... .......... .......... .......... 41%  127M 2s
109600K .......... .......... .......... .......... .......... 41% 69.7M 2s
109650K .......... .......... .......... .......... .......... 41%  137M 2s
109700K .......... .......... .......... .......... .......... 41% 63.9M 2s
109750K .......... .......... .......... .......... .......... 41%  121M 2s
109800K .......... .......... .......... .......... .......... 41% 93.7M 2s
109850K .......... .......... .......... .......... .......... 41% 75.8M 2s
109900K .......... .......... .......... .......... .......... 41%  122M 2s
109950K .......... .......... .......... .......... .......... 41% 76.2M 2s
110000K .......... .......... .......... .......... .......... 41% 96.9M 2s
110050K .......... .......... .......... .......... .......... 41% 94.6M 2s
110100K .......... .......... .......... .......... .......... 42% 94.4M 2s
110150K .......... .......... .......... .......... .......... 42% 73.3M 2s
110200K .......... .......... .......... .......... .......... 42% 96.9M 2s
110250K .......... .......... .......... .......... .......... 42% 94.8M 2s
110300K .......... .......... .......... .......... .......... 42% 94.1M 2s
110350K .......... .......... .......... .......... .......... 42% 95.2M 2s
110400K .......... .......... .......... .......... .......... 42%  121M 2s
110450K .......... .......... .......... .......... .......... 42% 63.1M 2s
110500K .......... .......... .......... .......... .......... 42%  121M 2s
110550K .......... .......... .......... .......... .......... 42%  104M 2s
110600K .......... .......... .......... .......... .......... 42% 88.0M 2s
110650K .......... .......... .......... .......... .......... 42% 73.0M 2s
110700K .......... .......... .......... .......... .......... 42% 99.9M 2s
110750K .......... .......... .......... .......... .......... 42%  119M 2s
110800K .......... .......... .......... .......... .......... 42% 79.5M 2s
110850K .......... .......... .......... .......... .......... 42% 93.2M 2s
110900K .......... .......... .......... .......... .......... 42% 77.8M 2s
110950K .......... .......... .......... .......... .......... 42%  119M 2s
111000K .......... .......... .......... .......... .......... 42%  121M 2s
111050K .......... .......... .......... .......... .......... 42% 88.0M 2s
111100K .......... .......... .......... .......... .......... 42%  105M 2s
111150K .......... .......... .......... .......... .......... 42% 93.9M 2s
111200K .......... .......... .......... .......... .......... 42% 95.2M 2s
111250K .......... .......... .......... .......... .......... 42%  102M 2s
111300K .......... .......... .......... .......... .......... 42%  114M 2s
111350K .......... .......... .......... .......... .......... 42% 79.4M 2s
111400K .......... .......... .......... .......... .......... 42%  128M 2s
111450K .......... .......... .......... .......... .......... 42%  110M 2s
111500K .......... .......... .......... .......... .......... 42% 95.0M 2s
111550K .......... .......... .......... .......... .......... 42% 19.9M 2s
111600K .......... .......... .......... .......... .......... 42%  421M 2s
111650K .......... .......... .......... .......... .......... 42%  479M 2s
111700K .......... .......... .......... .......... .......... 42% 43.4M 2s
111750K .......... .......... .......... .......... .......... 42%  165M 2s
111800K .......... .......... .......... .......... .......... 42%  174M 2s
111850K .......... .......... .......... .......... .......... 42%  151M 2s
111900K .......... .......... .......... .......... .......... 42%  176M 2s
111950K .......... .......... .......... .......... .......... 42%  156M 2s
112000K .......... .......... .......... .......... .......... 42%  289M 2s
112050K .......... .......... .......... .......... .......... 42%  397M 2s
112100K .......... .......... .......... .......... .......... 42%  286M 2s
112150K .......... .......... .......... .......... .......... 42% 93.7M 2s
112200K .......... .......... .......... .......... .......... 42%  122M 2s
112250K .......... .......... .......... .......... .......... 42% 77.4M 2s
112300K .......... .......... .......... .......... .......... 42% 94.4M 2s
112350K .......... .......... .......... .......... .......... 42% 39.4M 2s
112400K .......... .......... .......... .......... .......... 42%  456M 2s
112450K .......... .......... .......... .......... .......... 42% 55.4M 2s
112500K .......... .......... .......... .......... .......... 42%  134M 2s
112550K .......... .......... .......... .......... .......... 42% 93.9M 2s
112600K .......... .......... .......... .......... .......... 42% 93.0M 2s
112650K .......... .......... .......... .......... .......... 42%  118M 2s
112700K .......... .......... .......... .......... .......... 43% 77.9M 2s
112750K .......... .......... .......... .......... .......... 43% 72.1M 2s
112800K .......... .......... .......... .......... .......... 43%  124M 2s
112850K .......... .......... .......... .......... .......... 43% 71.0M 2s
112900K .......... .......... .......... .......... .......... 43%  138M 2s
112950K .......... .......... .......... .......... .......... 43% 54.6M 2s
113000K .......... .......... .......... .......... .......... 43% 55.2M 2s
113050K .......... .......... .......... .......... .......... 43% 52.8M 2s
113100K .......... .......... .......... .......... .......... 43%  126M 2s
113150K .......... .......... .......... .......... .......... 43% 94.8M 2s
113200K .......... .......... .......... .......... .......... 43% 90.8M 2s
113250K .......... .......... .......... .......... .......... 43% 98.6M 2s
113300K .......... .......... .......... .......... .......... 43%  125M 2s
113350K .......... .......... .......... .......... .......... 43% 91.8M 2s
113400K .......... .......... .......... .......... .......... 43%  126M 2s
113450K .......... .......... .......... .......... .......... 43% 95.2M 2s
113500K .......... .......... .......... .......... .......... 43% 77.3M 2s
113550K .......... .......... .......... .......... .......... 43%  120M 2s
113600K .......... .......... .......... .......... .......... 43% 94.3M 2s
113650K .......... .......... .......... .......... .......... 43% 91.4M 2s
113700K .......... .......... .......... .......... .......... 43% 94.6M 2s
113750K .......... .......... .......... .......... .......... 43% 77.3M 2s
113800K .......... .......... .......... .......... .......... 43%  116M 2s
113850K .......... .......... .......... .......... .......... 43% 73.5M 2s
113900K .......... .......... .......... .......... .......... 43%  134M 2s
113950K .......... .......... .......... .......... .......... 43% 71.8M 2s
114000K .......... .......... .......... .......... .......... 43%  104M 2s
114050K .......... .......... .......... .......... .......... 43% 87.0M 2s
114100K .......... .......... .......... .......... .......... 43% 85.2M 2s
114150K .......... .......... .......... .......... .......... 43% 85.8M 2s
114200K .......... .......... .......... .......... .......... 43% 94.8M 2s
114250K .......... .......... .......... .......... .......... 43% 96.5M 2s
114300K .......... .......... .......... .......... .......... 43% 94.3M 2s
114350K .......... .......... .......... .......... .......... 43% 94.6M 2s
114400K .......... .......... .......... .......... .......... 43% 75.5M 2s
114450K .......... .......... .......... .......... .......... 43%  119M 2s
114500K .......... .......... .......... .......... .......... 43% 77.1M 2s
114550K .......... .......... .......... .......... .......... 43%  125M 2s
114600K .......... .......... .......... .......... .......... 43% 75.7M 2s
114650K .......... .......... .......... .......... .......... 43% 71.9M 2s
114700K .......... .......... .......... .......... .......... 43%  192M 2s
114750K .......... .......... .......... .......... .......... 43% 74.2M 2s
114800K .......... .......... .......... .......... .......... 43%  124M 2s
114850K .......... .......... .......... .......... .......... 43% 94.4M 2s
114900K .......... .......... .......... .......... .......... 43% 96.9M 2s
114950K .......... .......... .......... .......... .......... 43% 91.3M 2s
115000K .......... .......... .......... .......... .......... 43% 96.5M 2s
115050K .......... .......... .......... .......... .......... 43% 92.7M 2s
115100K .......... .......... .......... .......... .......... 43% 94.3M 2s
115150K .......... .......... .......... .......... .......... 43% 95.0M 2s
115200K .......... .......... .......... .......... .......... 43% 91.3M 2s
115250K .......... .......... .......... .......... .......... 43% 99.2M 2s
115300K .......... .......... .......... .......... .......... 43% 94.6M 2s
115350K .......... .......... .......... .......... .......... 44%  120M 2s
115400K .......... .......... .......... .......... .......... 44% 97.5M 2s
115450K .......... .......... .......... .......... .......... 44% 93.4M 2s
115500K .......... .......... .......... .......... .......... 44% 21.4M 2s
115550K .......... .......... .......... .......... .......... 44%  268M 2s
115600K .......... .......... .......... .......... .......... 44%  440M 2s
115650K .......... .......... .......... .......... .......... 44%  503M 2s
115700K .......... .......... .......... .......... .......... 44% 97.9M 2s
115750K .......... .......... .......... .......... .......... 44%  525M 2s
115800K .......... .......... .......... .......... .......... 44% 52.3M 2s
115850K .......... .......... .......... .......... .......... 44%  117M 2s
115900K .......... .......... .......... .......... .......... 44%  106M 2s
115950K .......... .......... .......... .......... .......... 44%  303M 2s
116000K .......... .......... .......... .......... .......... 44% 75.9M 2s
116050K .......... .......... .......... .......... .......... 44%  421M 2s
116100K .......... .......... .......... .......... .......... 44%  400M 2s
116150K .......... .......... .......... .......... .......... 44% 97.1M 2s
116200K .......... .......... .......... .......... .......... 44% 61.9M 2s
116250K .......... .......... .......... .......... .......... 44% 65.5M 2s
116300K .......... .......... .......... .......... .......... 44% 63.2M 2s
116350K .......... .......... .......... .......... .......... 44% 61.8M 2s
116400K .......... .......... .......... .......... .......... 44%  126M 2s
116450K .......... .......... .......... .......... .......... 44% 54.7M 2s
116500K .......... .......... .......... .......... .......... 44% 61.7M 2s
116550K .......... .......... .......... .......... .......... 44% 64.4M 2s
116600K .......... .......... .......... .......... .......... 44% 95.2M 2s
116650K .......... .......... .......... .......... .......... 44% 94.3M 2s
116700K .......... .......... .......... .......... .......... 44% 61.2M 2s
116750K .......... .......... .......... .......... .......... 44% 73.8M 2s
116800K .......... .......... .......... .......... .......... 44% 54.6M 2s
116850K .......... .......... .......... .......... .......... 44% 89.4M 2s
116900K .......... .......... .......... .......... .......... 44% 65.3M 2s
116950K .......... .......... .......... .......... .......... 44% 48.6M 2s
117000K .......... .......... .......... .......... .......... 44% 54.1M 2s
117050K .......... .......... .......... .......... .......... 44%  124M 2s
117100K .......... .......... .......... .......... .......... 44% 55.1M 2s
117150K .......... .......... .......... .......... .......... 44% 69.7M 2s
117200K .......... .......... .......... .......... .......... 44% 79.5M 2s
117250K .......... .......... .......... .......... .......... 44% 90.3M 2s
117300K .......... .......... .......... .......... .......... 44% 63.4M 2s
117350K .......... .......... .......... .......... .......... 44% 77.1M 2s
117400K .......... .......... .......... .......... .......... 44% 75.2M 2s
117450K .......... .......... .......... .......... .......... 44% 54.3M 2s
117500K .......... .......... .......... .......... .......... 44% 63.2M 2s
117550K .......... .......... .......... .......... .......... 44%  122M 2s
117600K .......... .......... .......... .......... .......... 44% 63.0M 2s
117650K .......... .......... .......... .......... .......... 44% 76.3M 2s
117700K .......... .......... .......... .......... .......... 44% 55.0M 2s
117750K .......... .......... .......... .......... .......... 44%  128M 2s
117800K .......... .......... .......... .......... .......... 44% 74.8M 2s
117850K .......... .......... .......... .......... .......... 44% 92.1M 2s
117900K .......... .......... .......... .......... .......... 44% 76.2M 2s
117950K .......... .......... .......... .......... .......... 45% 75.6M 2s
118000K .......... .......... .......... .......... .......... 45% 64.7M 2s
118050K .......... .......... .......... .......... .......... 45% 50.4M 2s
118100K .......... .......... .......... .......... .......... 45% 72.7M 2s
118150K .......... .......... .......... .......... .......... 45% 64.7M 2s
118200K .......... .......... .......... .......... .......... 45% 61.4M 2s
118250K .......... .......... .......... .......... .......... 45% 65.5M 2s
118300K .......... .......... .......... .......... .......... 45% 72.6M 2s
118350K .......... .......... .......... .......... .......... 45% 54.9M 2s
118400K .......... .......... .......... .......... .......... 45% 93.2M 2s
118450K .......... .......... .......... .......... .......... 45% 63.5M 2s
118500K .......... .......... .......... .......... .......... 45% 53.6M 2s
118550K .......... .......... .......... .......... .......... 45% 92.7M 2s
118600K .......... .......... .......... .......... .......... 45% 61.0M 2s
118650K .......... .......... .......... .......... .......... 45% 79.3M 2s
118700K .......... .......... .......... .......... .......... 45% 90.9M 2s
118750K .......... .......... .......... .......... .......... 45%  135M 2s
118800K .......... .......... .......... .......... .......... 45% 96.9M 2s
118850K .......... .......... .......... .......... .......... 45% 94.8M 2s
118900K .......... .......... .......... .......... .......... 45%  123M 2s
118950K .......... .......... .......... .......... .......... 45% 64.0M 2s
119000K .......... .......... .......... .......... .......... 45% 28.2M 2s
119050K .......... .......... .......... .......... .......... 45%  394M 2s
119100K .......... .......... .......... .......... .......... 45%  440M 2s
119150K .......... .......... .......... .......... .......... 45%  421M 2s
119200K .......... .......... .......... .......... .......... 45%  119M 2s
119250K .......... .......... .......... .......... .......... 45% 57.6M 2s
119300K .......... .......... .......... .......... .......... 45%  514M 2s
119350K .......... .......... .......... .......... .......... 45%  140M 2s
119400K .......... .......... .......... .......... .......... 45% 92.5M 2s
119450K .......... .......... .......... .......... .......... 45%  121M 2s
119500K .......... .......... .......... .......... .......... 45% 99.2M 2s
119550K .......... .......... .......... .......... .......... 45%  120M 2s
119600K .......... .......... .......... .......... .......... 45% 93.7M 2s
119650K .......... .......... .......... .......... .......... 45%  126M 2s
119700K .......... .......... .......... .......... .......... 45% 94.6M 2s
119750K .......... .......... .......... .......... .......... 45% 21.1M 2s
119800K .......... .......... .......... .......... .......... 45%  309M 2s
119850K .......... .......... .......... .......... .......... 45%  268M 2s
119900K .......... .......... .......... .......... .......... 45%  519M 2s
119950K .......... .......... .......... .......... .......... 45% 56.4M 2s
120000K .......... .......... .......... .......... .......... 45%  509M 2s
120050K .......... .......... .......... .......... .......... 45% 53.1M 2s
120100K .......... .......... .......... .......... .......... 45% 45.8M 2s
120150K .......... .......... .......... .......... .......... 45%  249M 2s
120200K .......... .......... .......... .......... .......... 45%  349M 2s
120250K .......... .......... .......... .......... .......... 45%  381M 2s
120300K .......... .......... .......... .......... .......... 45%  124M 2s
120350K .......... .......... .......... .......... .......... 45%  136M 2s
120400K .......... .......... .......... .......... .......... 45%  148M 2s
120450K .......... .......... .......... .......... .......... 45% 75.9M 2s
120500K .......... .......... .......... .......... .......... 45%  514M 2s
120550K .......... .......... .......... .......... .......... 45%  305M 2s
120600K .......... .......... .......... .......... .......... 46% 91.1M 2s
120650K .......... .......... .......... .......... .......... 46% 55.3M 2s
120700K .......... .......... .......... .......... .......... 46% 54.2M 2s
120750K .......... .......... .......... .......... .......... 46% 63.3M 2s
120800K .......... .......... .......... .......... .......... 46% 75.4M 2s
120850K .......... .......... .......... .......... .......... 46% 63.3M 2s
120900K .......... .......... .......... .......... .......... 46% 93.7M 2s
120950K .......... .......... .......... .......... .......... 46% 63.7M 2s
121000K .......... .......... .......... .......... .......... 46% 77.8M 2s
121050K .......... .......... .......... .......... .......... 46% 73.8M 2s
121100K .......... .......... .......... .......... .......... 46% 65.0M 2s
121150K .......... .......... .......... .......... .......... 46% 90.1M 2s
121200K .......... .......... .......... .......... .......... 46% 55.6M 2s
121250K .......... .......... .......... .......... .......... 46% 90.3M 2s
121300K .......... .......... .......... .......... .......... 46% 65.5M 2s
121350K .......... .......... .......... .......... .......... 46% 75.9M 2s
121400K .......... .......... .......... .......... .......... 46% 74.3M 2s
121450K .......... .......... .......... .......... .......... 46% 55.0M 2s
121500K .......... .......... .......... .......... .......... 46% 88.1M 2s
121550K .......... .......... .......... .......... .......... 46% 67.2M 2s
121600K .......... .......... .......... .......... .......... 46% 76.2M 2s
121650K .......... .......... .......... .......... .......... 46% 94.4M 2s
121700K .......... .......... .......... .......... .......... 46% 46.8M 2s
121750K .......... .......... .......... .......... .......... 46% 64.9M 2s
121800K .......... .......... .......... .......... .......... 46% 95.4M 2s
121850K .......... .......... .......... .......... .......... 46% 63.2M 2s
121900K .......... .......... .......... .......... .......... 46% 73.1M 2s
121950K .......... .......... .......... .......... .......... 46% 55.3M 2s
122000K .......... .......... .......... .......... .......... 46% 61.5M 2s
122050K .......... .......... .......... .......... .......... 46% 97.5M 2s
122100K .......... .......... .......... .......... .......... 46% 59.4M 2s
122150K .......... .......... .......... .......... .......... 46% 78.0M 2s
122200K .......... .......... .......... .......... .......... 46% 62.4M 2s
122250K .......... .......... .......... .......... .......... 46% 54.4M 2s
122300K .......... .......... .......... .......... .......... 46%  126M 2s
122350K .......... .......... .......... .......... .......... 46% 62.9M 2s
122400K .......... .......... .......... .......... .......... 46% 63.0M 2s
122450K .......... .......... .......... .......... .......... 46% 62.9M 2s
122500K .......... .......... .......... .......... .......... 46% 64.4M 2s
122550K .......... .......... .......... .......... .......... 46% 73.9M 2s
122600K .......... .......... .......... .......... .......... 46% 58.6M 2s
122650K .......... .......... .......... .......... .......... 46%  101M 2s
122700K .......... .......... .......... .......... .......... 46% 63.2M 2s
122750K .......... .......... .......... .......... .......... 46% 63.2M 2s
122800K .......... .......... .......... .......... .......... 46% 96.1M 2s
122850K .......... .......... .......... .......... .......... 46% 24.5M 2s
122900K .......... .......... .......... .......... .......... 46% 58.4M 2s
122950K .......... .......... .......... .......... .......... 46%  122M 2s
123000K .......... .......... .......... .......... .......... 46% 66.3M 2s
123050K .......... .......... .......... .......... .......... 46% 63.2M 2s
123100K .......... .......... .......... .......... .......... 46%  123M 2s
123150K .......... .......... .......... .......... .......... 46% 77.1M 2s
123200K .......... .......... .......... .......... .......... 47% 94.1M 2s
123250K .......... .......... .......... .......... .......... 47%  122M 2s
123300K .......... .......... .......... .......... .......... 47% 95.2M 2s
123350K .......... .......... .......... .......... .......... 47% 92.7M 2s
123400K .......... .......... .......... .......... .......... 47%  125M 2s
123450K .......... .......... .......... .......... .......... 47% 93.7M 2s
123500K .......... .......... .......... .......... .......... 47% 21.1M 2s
123550K .......... .......... .......... .......... .......... 47%  493M 2s
123600K .......... .......... .......... .......... .......... 47%  351M 2s
123650K .......... .......... .......... .......... .......... 47%  514M 2s
123700K .......... .......... .......... .......... .......... 47%  391M 2s
123750K .......... .......... .......... .......... .......... 47% 38.2M 2s
123800K .......... .......... .......... .......... .......... 47%  498M 2s
123850K .......... .......... .......... .......... .......... 47%  116M 2s
123900K .......... .......... .......... .......... .......... 47%  267M 2s
123950K .......... .......... .......... .......... .......... 47%  444M 2s
124000K .......... .......... .......... .......... .......... 47% 40.1M 2s
124050K .......... .......... .......... .......... .......... 47%  161M 2s
124100K .......... .......... .......... .......... .......... 47%  142M 2s
124150K .......... .......... .......... .......... .......... 47%  173M 2s
124200K .......... .......... .......... .......... .......... 47%  174M 2s
124250K .......... .......... .......... .......... .......... 47% 93.5M 2s
124300K .......... .......... .......... .......... .......... 47% 96.7M 2s
124350K .......... .......... .......... .......... .......... 47% 64.2M 2s
124400K .......... .......... .......... .......... .......... 47% 93.2M 2s
124450K .......... .......... .......... .......... .......... 47% 72.2M 2s
124500K .......... .......... .......... .......... .......... 47% 96.3M 2s
124550K .......... .......... .......... .......... .......... 47% 76.7M 2s
124600K .......... .......... .......... .......... .......... 47% 64.2M 2s
124650K .......... .......... .......... .......... .......... 47% 91.1M 2s
124700K .......... .......... .......... .......... .......... 47% 63.8M 2s
124750K .......... .......... .......... .......... .......... 47%  126M 2s
124800K .......... .......... .......... .......... .......... 47% 72.0M 2s
124850K .......... .......... .......... .......... .......... 47% 64.7M 2s
124900K .......... .......... .......... .......... .......... 47%  117M 2s
124950K .......... .......... .......... .......... .......... 47% 70.6M 2s
125000K .......... .......... .......... .......... .......... 47% 98.2M 2s
125050K .......... .......... .......... .......... .......... 47% 77.8M 2s
125100K .......... .......... .......... .......... .......... 47% 40.9M 2s
125150K .......... .......... .......... .......... .......... 47%  126M 2s
125200K .......... .......... .......... .......... .......... 47% 62.9M 2s
125250K .......... .......... .......... .......... .......... 47% 91.8M 2s
125300K .......... .......... .......... .......... .......... 47% 93.2M 2s
125350K .......... .......... .......... .......... .......... 47% 75.1M 2s
125400K .......... .......... .......... .......... .......... 47% 75.6M 2s
125450K .......... .......... .......... .......... .......... 47% 78.8M 2s
125500K .......... .......... .......... .......... .......... 47% 98.0M 2s
125550K .......... .......... .......... .......... .......... 47% 77.0M 2s
125600K .......... .......... .......... .......... .......... 47% 93.7M 2s
125650K .......... .......... .......... .......... .......... 47% 75.9M 2s
125700K .......... .......... .......... .......... .......... 47% 72.9M 2s
125750K .......... .......... .......... .......... .......... 47% 78.3M 2s
125800K .......... .......... .......... .......... .......... 47% 74.8M 2s
125850K .......... .......... .......... .......... .......... 48% 94.6M 2s
125900K .......... .......... .......... .......... .......... 48% 76.3M 2s
125950K .......... .......... .......... .......... .......... 48% 75.1M 2s
126000K .......... .......... .......... .......... .......... 48% 74.1M 2s
126050K .......... .......... .......... .......... .......... 48% 97.3M 2s
126100K .......... .......... .......... .......... .......... 48% 75.2M 2s
126150K .......... .......... .......... .......... .......... 48% 75.1M 2s
126200K .......... .......... .......... .......... .......... 48% 74.5M 2s
126250K .......... .......... .......... .......... .......... 48% 90.8M 2s
126300K .......... .......... .......... .......... .......... 48% 76.1M 2s
126350K .......... .......... .......... .......... .......... 48% 64.9M 2s
126400K .......... .......... .......... .......... .......... 48%  117M 2s
126450K .......... .......... .......... .......... .......... 48% 75.6M 2s
126500K .......... .......... .......... .......... .......... 48% 76.8M 2s
126550K .......... .......... .......... .......... .......... 48% 94.3M 2s
126600K .......... .......... .......... .......... .......... 48% 73.6M 2s
126650K .......... .......... .......... .......... .......... 48% 77.1M 2s
126700K .......... .......... .......... .......... .......... 48% 71.6M 2s
126750K .......... .......... .......... .......... .......... 48% 79.4M 2s
126800K .......... .......... .......... .......... .......... 48% 92.3M 2s
126850K .......... .......... .......... .......... .......... 48% 76.1M 2s
126900K .......... .......... .......... .......... .......... 48% 75.1M 2s
126950K .......... .......... .......... .......... .......... 48%  121M 2s
127000K .......... .......... .......... .......... .......... 48% 98.4M 2s
127050K .......... .......... .......... .......... .......... 48%  121M 2s
127100K .......... .......... .......... .......... .......... 48% 98.4M 2s
127150K .......... .......... .......... .......... .......... 48%  115M 2s
127200K .......... .......... .......... .......... .......... 48% 96.3M 2s
127250K .......... .......... .......... .......... .......... 48% 98.2M 2s
127300K .......... .......... .......... .......... .......... 48%  122M 2s
127350K .......... .......... .......... .......... .......... 48% 24.1M 2s
127400K .......... .......... .......... .......... .......... 48%  465M 2s
127450K .......... .......... .......... .......... .......... 48%  425M 2s
127500K .......... .......... .......... .......... .......... 48%  514M 2s
127550K .......... .......... .......... .......... .......... 48%  525M 2s
127600K .......... .......... .......... .......... .......... 48% 33.6M 2s
127650K .......... .......... .......... .......... .......... 48%  239M 2s
127700K .......... .......... .......... .......... .......... 48%  461M 2s
127750K .......... .......... .......... .......... .......... 48%  561M 2s
127800K .......... .......... .......... .......... .......... 48%  118M 2s
127850K .......... .......... .......... .......... .......... 48% 77.8M 2s
127900K .......... .......... .......... .......... .......... 48% 71.2M 2s
127950K .......... .......... .......... .......... .......... 48%  102M 2s
128000K .......... .......... .......... .......... .......... 48% 93.2M 2s
128050K .......... .......... .......... .......... .......... 48%  119M 2s
128100K .......... .......... .......... .......... .......... 48% 61.1M 2s
128150K .......... .......... .......... .......... .......... 48% 78.9M 2s
128200K .......... .......... .......... .......... .......... 48% 92.8M 2s
128250K .......... .......... .......... .......... .......... 48% 91.6M 2s
128300K .......... .......... .......... .......... .......... 48% 94.6M 2s
128350K .......... .......... .......... .......... .......... 48% 61.2M 2s
128400K .......... .......... .......... .......... .......... 48% 94.1M 2s
128450K .......... .......... .......... .......... .......... 49% 82.6M 2s
128500K .......... .......... .......... .......... .......... 49% 94.8M 2s
128550K .......... .......... .......... .......... .......... 49% 92.3M 2s
128600K .......... .......... .......... .......... .......... 49% 76.9M 2s
128650K .......... .......... .......... .......... .......... 49%  125M 2s
128700K .......... .......... .......... .......... .......... 49% 63.2M 2s
128750K .......... .......... .......... .......... .......... 49% 91.1M 2s
128800K .......... .......... .......... .......... .......... 49% 77.5M 2s
128850K .......... .......... .......... .......... .......... 49% 73.4M 2s
128900K .......... .......... .......... .......... .......... 49% 97.9M 2s
128950K .......... .......... .......... .......... .......... 49% 73.6M 2s
129000K .......... .......... .......... .......... .......... 49% 77.5M 2s
129050K .......... .......... .......... .......... .......... 49% 76.1M 2s
129100K .......... .......... .......... .......... .......... 49% 75.6M 2s
129150K .......... .......... .......... .......... .......... 49%  119M 2s
129200K .......... .......... .......... .......... .......... 49% 64.2M 2s
129250K .......... .......... .......... .......... .......... 49% 75.5M 2s
129300K .......... .......... .......... .......... .......... 49% 91.3M 2s
129350K .......... .......... .......... .......... .......... 49% 64.4M 2s
129400K .......... .......... .......... .......... .......... 49%  126M 2s
129450K .......... .......... .......... .......... .......... 49% 73.5M 2s
129500K .......... .......... .......... .......... .......... 49% 88.1M 2s
129550K .......... .......... .......... .......... .......... 49% 80.7M 2s
129600K .......... .......... .......... .......... .......... 49% 88.0M 2s
129650K .......... .......... .......... .......... .......... 49% 78.5M 2s
129700K .......... .......... .......... .......... .......... 49% 75.7M 2s
129750K .......... .......... .......... .......... .......... 49% 90.4M 2s
129800K .......... .......... .......... .......... .......... 49% 77.8M 2s
129850K .......... .......... .......... .......... .......... 49% 93.9M 2s
129900K .......... .......... .......... .......... .......... 49% 75.9M 2s
129950K .......... .......... .......... .......... .......... 49% 75.9M 2s
130000K .......... .......... .......... .......... .......... 49% 74.1M 2s
130050K .......... .......... .......... .......... .......... 49%  120M 2s
130100K .......... .......... .......... .......... .......... 49% 64.9M 2s
130150K .......... .......... .......... .......... .......... 49% 92.1M 2s
130200K .......... .......... .......... .......... .......... 49% 63.8M 2s
130250K .......... .......... .......... .......... .......... 49% 76.5M 2s
130300K .......... .......... .......... .......... .......... 49%  124M 2s
130350K .......... .......... .......... .......... .......... 49% 74.4M 2s
130400K .......... .......... .......... .......... .......... 49% 75.7M 2s
130450K .......... .......... .......... .......... .......... 49% 63.6M 2s
130500K .......... .......... .......... .......... .......... 49% 96.9M 2s
130550K .......... .......... .......... .......... .......... 49% 92.0M 2s
130600K .......... .......... .......... .......... .......... 49% 59.3M 2s
130650K .......... .......... .......... .......... .......... 49%  112M 2s
130700K .......... .......... .......... .......... .......... 49% 46.9M 2s
130750K .......... .......... .......... .......... .......... 49%  159M 2s
130800K .......... .......... .......... .......... .......... 49% 63.2M 2s
130850K .......... .......... .......... .......... .......... 49% 90.6M 2s
130900K .......... .......... .......... .......... .......... 49%  128M 2s
130950K .......... .......... .......... .......... .......... 49% 97.1M 2s
131000K .......... .......... .......... .......... .......... 49%  117M 2s
131050K .......... .......... .......... .......... .......... 49% 55.5M 2s
131100K .......... .......... .......... .......... .......... 50%  163M 2s
131150K .......... .......... .......... .......... .......... 50% 35.7M 2s
131200K .......... .......... .......... .......... .......... 50%  148M 2s
131250K .......... .......... .......... .......... .......... 50% 19.6M 2s
131300K .......... .......... .......... .......... .......... 50%  184M 2s
131350K .......... .......... .......... .......... .......... 50%  161M 2s
131400K .......... .......... .......... .......... .......... 50%  189M 2s
131450K .......... .......... .......... .......... .......... 50% 31.4M 2s
131500K .......... .......... .......... .......... .......... 50%  187M 2s
131550K .......... .......... .......... .......... .......... 50% 57.0M 2s
131600K .......... .......... .......... .......... .......... 50% 47.5M 2s
131650K .......... .......... .......... .......... .......... 50%  470M 2s
131700K .......... .......... .......... .......... .......... 50%  474M 2s
131750K .......... .......... .......... .......... .......... 50%  102M 2s
131800K .......... .......... .......... .......... .......... 50% 69.8M 2s
131850K .......... .......... .......... .......... .......... 50%  151M 2s
131900K .......... .......... .......... .......... .......... 50%  136M 2s
131950K .......... .......... .......... .......... .......... 50% 79.8M 2s
132000K .......... .......... .......... .......... .......... 50% 86.6M 2s
132050K .......... .......... .......... .......... .......... 50%  109M 2s
132100K .......... .......... .......... .......... .......... 50% 80.7M 2s
132150K .......... .......... .......... .......... .......... 50%  194M 2s
132200K .......... .......... .......... .......... .......... 50%  103M 2s
132250K .......... .......... .......... .......... .......... 50% 80.2M 2s
132300K .......... .......... .......... .......... .......... 50%  108M 2s
132350K .......... .......... .......... .......... .......... 50%  119M 2s
132400K .......... .......... .......... .......... .......... 50% 82.5M 2s
132450K .......... .......... .......... .......... .......... 50% 86.3M 2s
132500K .......... .......... .......... .......... .......... 50%  138M 2s
132550K .......... .......... .......... .......... .......... 50%  126M 2s
132600K .......... .......... .......... .......... .......... 50% 97.7M 2s
132650K .......... .......... .......... .......... .......... 50%  116M 2s
132700K .......... .......... .......... .......... .......... 50%  116M 2s
132750K .......... .......... .......... .......... .......... 50% 22.9M 2s
132800K .......... .......... .......... .......... .......... 50%  452M 2s
132850K .......... .......... .......... .......... .......... 50%  417M 2s
132900K .......... .......... .......... .......... .......... 50% 28.2M 2s
132950K .......... .......... .......... .......... .......... 50%  124M 2s
133000K .......... .......... .......... .......... .......... 50%  180M 2s
133050K .......... .......... .......... .......... .......... 50%  196M 2s
133100K .......... .......... .......... .......... .......... 50% 16.5M 2s
133150K .......... .......... .......... .......... .......... 50%  474M 2s
133200K .......... .......... .......... .......... .......... 50%  421M 2s
133250K .......... .......... .......... .......... .......... 50%  525M 2s
133300K .......... .......... .......... .......... .......... 50% 38.1M 2s
133350K .......... .......... .......... .......... .......... 50%  140M 2s
133400K .......... .......... .......... .......... .......... 50%  141M 2s
133450K .......... .......... .......... .......... .......... 50% 64.7M 2s
133500K .......... .......... .......... .......... .......... 50%  191M 2s
133550K .......... .......... .......... .......... .......... 50%  101M 2s
133600K .......... .......... .......... .......... .......... 50% 78.3M 2s
133650K .......... .......... .......... .......... .......... 50%  176M 2s
133700K .......... .......... .......... .......... .......... 51%  109M 2s
133750K .......... .......... .......... .......... .......... 51% 88.1M 2s
133800K .......... .......... .......... .......... .......... 51%  182M 2s
133850K .......... .......... .......... .......... .......... 51%  107M 2s
133900K .......... .......... .......... .......... .......... 51%  104M 2s
133950K .......... .......... .......... .......... .......... 51% 97.1M 2s
134000K .......... .......... .......... .......... .......... 51%  105M 2s
134050K .......... .......... .......... .......... .......... 51% 84.3M 2s
134100K .......... .......... .......... .......... .......... 51%  164M 2s
134150K .......... .......... .......... .......... .......... 51% 19.5M 2s
134200K .......... .......... .......... .......... .......... 51%  388M 2s
134250K .......... .......... .......... .......... .......... 51%  525M 2s
134300K .......... .......... .......... .......... .......... 51%  519M 2s
134350K .......... .......... .......... .......... .......... 51% 41.6M 2s
134400K .......... .......... .......... .......... .......... 51% 18.5M 2s
134450K .......... .......... .......... .......... .......... 51% 46.2M 2s
134500K .......... .......... .......... .......... .......... 51%  341M 2s
134550K .......... .......... .......... .......... .......... 51%  483M 2s
134600K .......... .......... .......... .......... .......... 51% 39.2M 2s
134650K .......... .......... .......... .......... .......... 51%  128M 2s
134700K .......... .......... .......... .......... .......... 51%  101M 2s
134750K .......... .......... .......... .......... .......... 51%  103M 2s
134800K .......... .......... .......... .......... .......... 51%  132M 2s
134850K .......... .......... .......... .......... .......... 51%  102M 2s
134900K .......... .......... .......... .......... .......... 51% 99.4M 2s
134950K .......... .......... .......... .......... .......... 51% 39.3M 2s
135000K .......... .......... .......... .......... .......... 51%  180M 2s
135050K .......... .......... .......... .......... .......... 51%  193M 2s
135100K .......... .......... .......... .......... .......... 51% 43.2M 2s
135150K .......... .......... .......... .......... .......... 51%  123M 2s
135200K .......... .......... .......... .......... .......... 51% 86.3M 2s
135250K .......... .......... .......... .......... .......... 51%  125M 2s
135300K .......... .......... .......... .......... .......... 51%  109M 2s
135350K .......... .......... .......... .......... .......... 51% 60.0M 2s
135400K .......... .......... .......... .......... .......... 51%  421M 2s
135450K .......... .......... .......... .......... .......... 51% 15.3M 2s
135500K .......... .......... .......... .......... .......... 51%  493M 2s
135550K .......... .......... .......... .......... .......... 51%  514M 2s
135600K .......... .......... .......... .......... .......... 51% 44.3M 2s
135650K .......... .......... .......... .......... .......... 51% 72.9M 2s
135700K .......... .......... .......... .......... .......... 51%  425M 2s
135750K .......... .......... .......... .......... .......... 51%  105M 2s
135800K .......... .......... .......... .......... .......... 51% 29.4M 2s
135850K .......... .......... .......... .......... .......... 51%  425M 2s
135900K .......... .......... .......... .......... .......... 51% 17.4M 2s
135950K .......... .......... .......... .......... .......... 51%  432M 2s
136000K .......... .......... .......... .......... .......... 51%  176M 2s
136050K .......... .......... .......... .......... .......... 51%  531M 2s
136100K .......... .......... .......... .......... .......... 51% 20.5M 2s
136150K .......... .......... .......... .......... .......... 51%  549M 2s
136200K .......... .......... .......... .......... .......... 51%  493M 2s
136250K .......... .......... .......... .......... .......... 51% 46.9M 2s
136300K .......... .......... .......... .......... .......... 52%  162M 2s
136350K .......... .......... .......... .......... .......... 52% 82.1M 2s
136400K .......... .......... .......... .......... .......... 52%  184M 2s
136450K .......... .......... .......... .......... .......... 52% 86.9M 2s
136500K .......... .......... .......... .......... .......... 52% 25.8M 2s
136550K .......... .......... .......... .......... .......... 52%  509M 2s
136600K .......... .......... .......... .......... .......... 52% 38.9M 2s
136650K .......... .......... .......... .......... .......... 52%  189M 2s
136700K .......... .......... .......... .......... .......... 52% 41.6M 2s
136750K .......... .......... .......... .......... .......... 52%  184M 2s
136800K .......... .......... .......... .......... .......... 52%  191M 2s
136850K .......... .......... .......... .......... .......... 52% 27.8M 2s
136900K .......... .......... .......... .......... .......... 52%  498M 2s
136950K .......... .......... .......... .......... .......... 52%  483M 2s
137000K .......... .......... .......... .......... .......... 52%  201M 2s
137050K .......... .......... .......... .......... .......... 52% 70.6M 2s
137100K .......... .......... .......... .......... .......... 52% 80.0M 2s
137150K .......... .......... .......... .......... .......... 52%  116M 2s
137200K .......... .......... .......... .......... .......... 52%  115M 2s
137250K .......... .......... .......... .......... .......... 52%  113M 2s
137300K .......... .......... .......... .......... .......... 52%  113M 2s
137350K .......... .......... .......... .......... .......... 52% 16.7M 2s
137400K .......... .......... .......... .......... .......... 52%  388M 2s
137450K .......... .......... .......... .......... .......... 52%  432M 2s
137500K .......... .......... .......... .......... .......... 52% 20.5M 2s
137550K .......... .......... .......... .......... .......... 52%  410M 2s
137600K .......... .......... .......... .......... .......... 52%  436M 2s
137650K .......... .......... .......... .......... .......... 52%  514M 2s
137700K .......... .......... .......... .......... .......... 52% 27.2M 2s
137750K .......... .......... .......... .......... .......... 52%  483M 2s
137800K .......... .......... .......... .......... .......... 52%  561M 2s
137850K .......... .......... .......... .......... .......... 52% 41.2M 2s
137900K .......... .......... .......... .......... .......... 52%  186M 2s
137950K .......... .......... .......... .......... .......... 52%  149M 2s
138000K .......... .......... .......... .......... .......... 52% 13.1M 2s
138050K .......... .......... .......... .......... .......... 52%  452M 2s
138100K .......... .......... .......... .......... .......... 52%  319M 2s
138150K .......... .......... .......... .......... .......... 52%  498M 2s
138200K .......... .......... .......... .......... .......... 52% 43.4M 2s
138250K .......... .......... .......... .......... .......... 52%  103M 2s
138300K .......... .......... .......... .......... .......... 52%  109M 2s
138350K .......... .......... .......... .......... .......... 52%  102M 2s
138400K .......... .......... .......... .......... .......... 52% 97.9M 2s
138450K .......... .......... .......... .......... .......... 52%  121M 2s
138500K .......... .......... .......... .......... .......... 52%  151M 2s
138550K .......... .......... .......... .......... .......... 52% 93.2M 2s
138600K .......... .......... .......... .......... .......... 52% 86.3M 2s
138650K .......... .......... .......... .......... .......... 52%  168M 2s
138700K .......... .......... .......... .......... .......... 52% 94.6M 2s
138750K .......... .......... .......... .......... .......... 52%  108M 2s
138800K .......... .......... .......... .......... .......... 52%  139M 2s
138850K .......... .......... .......... .......... .......... 52% 92.1M 2s
138900K .......... .......... .......... .......... .......... 52% 81.2M 2s
138950K .......... .......... .......... .......... .......... 53%  101M 2s
139000K .......... .......... .......... .......... .......... 53%  189M 2s
139050K .......... .......... .......... .......... .......... 53%  137M 2s
139100K .......... .......... .......... .......... .......... 53% 17.8M 2s
139150K .......... .......... .......... .......... .......... 53%  202M 2s
139200K .......... .......... .......... .......... .......... 53%  184M 2s
139250K .......... .......... .......... .......... .......... 53% 14.9M 2s
139300K .......... .......... .......... .......... .......... 53%  440M 2s
139350K .......... .......... .......... .......... .......... 53%  452M 2s
139400K .......... .......... .......... .......... .......... 53% 29.8M 2s
139450K .......... .......... .......... .......... .......... 53%  117M 2s
139500K .......... .......... .......... .......... .......... 53%  199M 2s
139550K .......... .......... .......... .......... .......... 53%  417M 2s
139600K .......... .......... .......... .......... .......... 53% 32.0M 2s
139650K .......... .......... .......... .......... .......... 53%  190M 2s
139700K .......... .......... .......... .......... .......... 53%  164M 2s
139750K .......... .......... .......... .......... .......... 53% 46.3M 2s
139800K .......... .......... .......... .......... .......... 53%  167M 2s
139850K .......... .......... .......... .......... .......... 53%  108M 2s
139900K .......... .......... .......... .......... .......... 53%  192M 2s
139950K .......... .......... .......... .......... .......... 53% 69.5M 2s
140000K .......... .......... .......... .......... .......... 53%  184M 2s
140050K .......... .......... .......... .......... .......... 53%  147M 2s
140100K .......... .......... .......... .......... .......... 53% 86.7M 2s
140150K .......... .......... .......... .......... .......... 53% 72.6M 2s
140200K .......... .......... .......... .......... .......... 53%  148M 2s
140250K .......... .......... .......... .......... .......... 53% 49.7M 2s
140300K .......... .......... .......... .......... .......... 53%  225M 2s
140350K .......... .......... .......... .......... .......... 53%  140M 2s
140400K .......... .......... .......... .......... .......... 53%  127M 2s
140450K .......... .......... .......... .......... .......... 53% 53.8M 2s
140500K .......... .......... .......... .......... .......... 53%  127M 2s
140550K .......... .......... .......... .......... .......... 53%  119M 2s
140600K .......... .......... .......... .......... .......... 53% 94.8M 2s
140650K .......... .......... .......... .......... .......... 53% 97.9M 2s
140700K .......... .......... .......... .......... .......... 53% 94.1M 2s
140750K .......... .......... .......... .......... .......... 53%  121M 2s
140800K .......... .......... .......... .......... .......... 53% 24.1M 2s
140850K .......... .......... .......... .......... .......... 53%  323M 2s
140900K .......... .......... .......... .......... .......... 53%  404M 2s
140950K .......... .......... .......... .......... .......... 53%  109M 2s
141000K .......... .......... .......... .......... .......... 53%  440M 2s
141050K .......... .......... .......... .......... .......... 53% 50.1M 2s
141100K .......... .......... .......... .......... .......... 53%  207M 2s
141150K .......... .......... .......... .......... .......... 53%  176M 2s
141200K .......... .......... .......... .......... .......... 53%  448M 2s
141250K .......... .......... .......... .......... .......... 53%  105M 2s
141300K .......... .......... .......... .......... .......... 53% 78.8M 2s
141350K .......... .......... .......... .......... .......... 53% 77.8M 2s
141400K .......... .......... .......... .......... .......... 53% 93.7M 2s
141450K .......... .......... .......... .......... .......... 53% 63.7M 2s
141500K .......... .......... .......... .......... .......... 53% 95.0M 2s
141550K .......... .......... .......... .......... .......... 54% 75.0M 2s
141600K .......... .......... .......... .......... .......... 54% 76.1M 2s
141650K .......... .......... .......... .......... .......... 54%  122M 2s
141700K .......... .......... .......... .......... .......... 54% 64.2M 2s
141750K .......... .......... .......... .......... .......... 54% 92.7M 2s
141800K .......... .......... .......... .......... .......... 54% 95.2M 2s
141850K .......... .......... .......... .......... .......... 54% 55.4M 2s
141900K .......... .......... .......... .......... .......... 54%  126M 2s
141950K .......... .......... .......... .......... .......... 54% 75.2M 2s
142000K .......... .......... .......... .......... .......... 54% 54.2M 2s
142050K .......... .......... .......... .......... .......... 54%  130M 2s
142100K .......... .......... .......... .......... .......... 54% 75.8M 2s
142150K .......... .......... .......... .......... .......... 54% 94.1M 2s
142200K .......... .......... .......... .......... .......... 54% 75.9M 2s
142250K .......... .......... .......... .......... .......... 54%  121M 2s
142300K .......... .......... .......... .......... .......... 54% 77.6M 2s
142350K .......... .......... .......... .......... .......... 54% 92.3M 2s
142400K .......... .......... .......... .......... .......... 54% 77.8M 2s
142450K .......... .......... .......... .......... .......... 54% 31.8M 2s
142500K .......... .......... .......... .......... .......... 54%  465M 2s
142550K .......... .......... .......... .......... .......... 54% 41.7M 2s
142600K .......... .......... .......... .......... .......... 54%  133M 2s
142650K .......... .......... .......... .......... .......... 54% 45.0M 2s
142700K .......... .......... .......... .......... .......... 54% 93.0M 2s
142750K .......... .......... .......... .......... .......... 54% 70.7M 2s
142800K .......... .......... .......... .......... .......... 54%  127M 2s
142850K .......... .......... .......... .......... .......... 54% 74.5M 2s
142900K .......... .......... .......... .......... .......... 54%  102M 2s
142950K .......... .......... .......... .......... .......... 54% 75.2M 2s
143000K .......... .......... .......... .......... .......... 54% 75.5M 2s
143050K .......... .......... .......... .......... .......... 54%  110M 2s
143100K .......... .......... .......... .......... .......... 54% 57.2M 2s
143150K .......... .......... .......... .......... .......... 54%  121M 2s
143200K .......... .......... .......... .......... .......... 54% 64.5M 2s
143250K .......... .......... .......... .......... .......... 54% 94.3M 2s
143300K .......... .......... .......... .......... .......... 54% 90.4M 2s
143350K .......... .......... .......... .......... .......... 54% 77.6M 2s
143400K .......... .......... .......... .......... .......... 54% 92.0M 2s
143450K .......... .......... .......... .......... .......... 54% 78.3M 2s
143500K .......... .......... .......... .......... .......... 54% 89.9M 2s
143550K .......... .......... .......... .......... .......... 54%  135M 2s
143600K .......... .......... .......... .......... .......... 54% 73.4M 2s
143650K .......... .......... .......... .......... .......... 54% 95.2M 2s
143700K .......... .......... .......... .......... .......... 54% 64.8M 2s
143750K .......... .......... .......... .......... .......... 54%  121M 2s
143800K .......... .......... .......... .......... .......... 54% 94.4M 2s
143850K .......... .......... .......... .......... .......... 54% 63.1M 2s
143900K .......... .......... .......... .......... .......... 54% 95.2M 2s
143950K .......... .......... .......... .......... .......... 54% 76.1M 2s
144000K .......... .......... .......... .......... .......... 54%  125M 2s
144050K .......... .......... .......... .......... .......... 54% 91.8M 2s
144100K .......... .......... .......... .......... .......... 54% 78.5M 2s
144150K .......... .......... .......... .......... .......... 54% 76.5M 2s
144200K .......... .......... .......... .......... .......... 55% 91.3M 2s
144250K .......... .......... .......... .......... .......... 55%  126M 2s
144300K .......... .......... .......... .......... .......... 55% 71.4M 2s
144350K .......... .......... .......... .......... .......... 55%  101M 2s
144400K .......... .......... .......... .......... .......... 55%  122M 2s
144450K .......... .......... .......... .......... .......... 55% 78.1M 2s
144500K .......... .......... .......... .......... .......... 55%  121M 2s
144550K .......... .......... .......... .......... .......... 55% 98.0M 2s
144600K .......... .......... .......... .......... .......... 55% 30.6M 2s
144650K .......... .......... .......... .......... .......... 55%  188M 2s
144700K .......... .......... .......... .......... .......... 55%  364M 2s
144750K .......... .......... .......... .......... .......... 55% 47.8M 2s
144800K .......... .......... .......... .......... .......... 55%  185M 2s
144850K .......... .......... .......... .......... .......... 55%  170M 2s
144900K .......... .......... .......... .......... .......... 55%  493M 2s
144950K .......... .......... .......... .......... .......... 55%  206M 2s
145000K .......... .......... .......... .......... .......... 55%  120M 2s
145050K .......... .......... .......... .......... .......... 55% 94.6M 2s
145100K .......... .......... .......... .......... .......... 55% 64.5M 2s
145150K .......... .......... .......... .......... .......... 55%  121M 2s
145200K .......... .......... .......... .......... .......... 55% 75.4M 2s
145250K .......... .......... .......... .......... .......... 55% 75.4M 2s
145300K .......... .......... .......... .......... .......... 55% 76.3M 2s
145350K .......... .......... .......... .......... .......... 55% 75.8M 1s
145400K .......... .......... .......... .......... .......... 55% 95.9M 1s
145450K .......... .......... .......... .......... .......... 55% 74.7M 1s
145500K .......... .......... .......... .......... .......... 55% 75.6M 1s
145550K .......... .......... .......... .......... .......... 55% 76.5M 1s
145600K .......... .......... .......... .......... .......... 55% 72.6M 1s
145650K .......... .......... .......... .......... .......... 55%  101M 1s
145700K .......... .......... .......... .......... .......... 55% 60.4M 1s
145750K .......... .......... .......... .......... .......... 55%  119M 1s
145800K .......... .......... .......... .......... .......... 55% 93.7M 1s
145850K .......... .......... .......... .......... .......... 55% 64.2M 1s
145900K .......... .......... .......... .......... .......... 55% 92.5M 1s
145950K .......... .......... .......... .......... .......... 55% 73.3M 1s
146000K .......... .......... .......... .......... .......... 55% 93.5M 1s
146050K .......... .......... .......... .......... .......... 55% 76.8M 1s
146100K .......... .......... .......... .......... .......... 55% 73.1M 1s
146150K .......... .......... .......... .......... .......... 55% 98.6M 1s
146200K .......... .......... .......... .......... .......... 55% 95.2M 1s
146250K .......... .......... .......... .......... .......... 55% 87.7M 1s
146300K .......... .......... .......... .......... .......... 55% 66.0M 1s
146350K .......... .......... .......... .......... .......... 55% 87.3M 1s
146400K .......... .......... .......... .......... .......... 55%  104M 1s
146450K .......... .......... .......... .......... .......... 55% 75.9M 1s
146500K .......... .......... .......... .......... .......... 55% 93.4M 1s
146550K .......... .......... .......... .......... .......... 55%  121M 1s
146600K .......... .......... .......... .......... .......... 55% 55.0M 1s
146650K .......... .......... .......... .......... .......... 55%  174M 1s
146700K .......... .......... .......... .......... .......... 55% 64.8M 1s
146750K .......... .......... .......... .......... .......... 55% 93.5M 1s
146800K .......... .......... .......... .......... .......... 56%  124M 1s
146850K .......... .......... .......... .......... .......... 56% 73.9M 1s
146900K .......... .......... .......... .......... .......... 56% 94.8M 1s
146950K .......... .......... .......... .......... .......... 56% 77.8M 1s
147000K .......... .......... .......... .......... .......... 56% 75.0M 1s
147050K .......... .......... .......... .......... .......... 56%  105M 1s
147100K .......... .......... .......... .......... .......... 56%  105M 1s
147150K .......... .......... .......... .......... .......... 56% 72.0M 1s
147200K .......... .......... .......... .......... .......... 56% 78.8M 1s
147250K .......... .......... .......... .......... .......... 56% 92.3M 1s
147300K .......... .......... .......... .......... .......... 56%  100M 1s
147350K .......... .......... .......... .......... .......... 56% 73.2M 1s
147400K .......... .......... .......... .......... .......... 56% 80.4M 1s
147450K .......... .......... .......... .......... .......... 56% 61.2M 1s
147500K .......... .......... .......... .......... .......... 56% 60.2M 1s
147550K .......... .......... .......... .......... .......... 56%  135M 1s
147600K .......... .......... .......... .......... .......... 56% 54.0M 1s
147650K .......... .......... .......... .......... .......... 56%  125M 1s
147700K .......... .......... .......... .......... .......... 56% 92.8M 1s
147750K .......... .......... .......... .......... .......... 56% 94.4M 1s
147800K .......... .......... .......... .......... .......... 56%  121M 1s
147850K .......... .......... .......... .......... .......... 56% 78.3M 1s
147900K .......... .......... .......... .......... .......... 56%  126M 1s
147950K .......... .......... .......... .......... .......... 56% 94.6M 1s
148000K .......... .......... .......... .......... .......... 56%  121M 1s
148050K .......... .......... .......... .......... .......... 56% 98.2M 1s
148100K .......... .......... .......... .......... .......... 56% 95.4M 1s
148150K .......... .......... .......... .......... .......... 56% 31.0M 1s
148200K .......... .......... .......... .......... .......... 56%  165M 1s
148250K .......... .......... .......... .......... .......... 56%  388M 1s
148300K .......... .......... .......... .......... .......... 56% 60.8M 1s
148350K .......... .......... .......... .......... .......... 56%  135M 1s
148400K .......... .......... .......... .......... .......... 56% 78.3M 1s
148450K .......... .......... .......... .......... .......... 56%  407M 1s
148500K .......... .......... .......... .......... .......... 56%  519M 1s
148550K .......... .......... .......... .......... .......... 56%  157M 1s
148600K .......... .......... .......... .......... .......... 56%  119M 1s
148650K .......... .......... .......... .......... .......... 56% 77.1M 1s
148700K .......... .......... .......... .......... .......... 56% 80.6M 1s
148750K .......... .......... .......... .......... .......... 56% 86.9M 1s
148800K .......... .......... .......... .......... .......... 56% 94.1M 1s
148850K .......... .......... .......... .......... .......... 56% 91.4M 1s
148900K .......... .......... .......... .......... .......... 56% 91.4M 1s
148950K .......... .......... .......... .......... .......... 56% 96.5M 1s
149000K .......... .......... .......... .......... .......... 56% 75.9M 1s
149050K .......... .......... .......... .......... .......... 56% 96.3M 1s
149100K .......... .......... .......... .......... .......... 56% 75.6M 1s
149150K .......... .......... .......... .......... .......... 56%  108M 1s
149200K .......... .......... .......... .......... .......... 56% 80.4M 1s
149250K .......... .......... .......... .......... .......... 56% 97.5M 1s
149300K .......... .......... .......... .......... .......... 56% 95.4M 1s
149350K .......... .......... .......... .......... .......... 56% 75.2M 1s
149400K .......... .......... .......... .......... .......... 56%  120M 1s
149450K .......... .......... .......... .......... .......... 57% 77.8M 1s
149500K .......... .......... .......... .......... .......... 57%  120M 1s
149550K .......... .......... .......... .......... .......... 57% 98.4M 1s
149600K .......... .......... .......... .......... .......... 57% 91.3M 1s
149650K .......... .......... .......... .......... .......... 57% 95.4M 1s
149700K .......... .......... .......... .......... .......... 57% 74.9M 1s
149750K .......... .......... .......... .......... .......... 57% 98.8M 1s
149800K .......... .......... .......... .......... .......... 57% 94.1M 1s
149850K .......... .......... .......... .......... .......... 57% 57.0M 1s
149900K .......... .......... .......... .......... .......... 57%  106M 1s
149950K .......... .......... .......... .......... .......... 57% 75.8M 1s
150000K .......... .......... .......... .......... .......... 57% 76.5M 1s
150050K .......... .......... .......... .......... .......... 57% 92.8M 1s
150100K .......... .......... .......... .......... .......... 57% 92.1M 1s
150150K .......... .......... .......... .......... .......... 57% 75.6M 1s
150200K .......... .......... .......... .......... .......... 57%  125M 1s
150250K .......... .......... .......... .......... .......... 57% 64.0M 1s
150300K .......... .......... .......... .......... .......... 57%  118M 1s
150350K .......... .......... .......... .......... .......... 57% 90.9M 1s
150400K .......... .......... .......... .......... .......... 57% 83.3M 1s
150450K .......... .......... .......... .......... .......... 57% 83.5M 1s
150500K .......... .......... .......... .......... .......... 57% 96.3M 1s
150550K .......... .......... .......... .......... .......... 57% 91.3M 1s
150600K .......... .......... .......... .......... .......... 57% 95.7M 1s
150650K .......... .......... .......... .......... .......... 57% 73.8M 1s
150700K .......... .......... .......... .......... .......... 57% 97.3M 1s
150750K .......... .......... .......... .......... .......... 57% 77.5M 1s
150800K .......... .......... .......... .......... .......... 57%  120M 1s
150850K .......... .......... .......... .......... .......... 57% 75.4M 1s
150900K .......... .......... .......... .......... .......... 57%  123M 1s
150950K .......... .......... .......... .......... .......... 57% 65.5M 1s
151000K .......... .......... .......... .......... .......... 57%  121M 1s
151050K .......... .......... .......... .......... .......... 57% 76.9M 1s
151100K .......... .......... .......... .......... .......... 57%  123M 1s
151150K .......... .......... .......... .......... .......... 57% 77.0M 1s
151200K .......... .......... .......... .......... .......... 57% 93.2M 1s
151250K .......... .......... .......... .......... .......... 57% 94.4M 1s
151300K .......... .......... .......... .......... .......... 57%  126M 1s
151350K .......... .......... .......... .......... .......... 57% 93.4M 1s
151400K .......... .......... .......... .......... .......... 57%  120M 1s
151450K .......... .......... .......... .......... .......... 57% 75.9M 1s
151500K .......... .......... .......... .......... .......... 57% 72.0M 1s
151550K .......... .......... .......... .......... .......... 57% 86.1M 1s
151600K .......... .......... .......... .......... .......... 57% 88.8M 1s
151650K .......... .......... .......... .......... .......... 57% 73.6M 1s
151700K .......... .......... .......... .......... .......... 57% 77.5M 1s
151750K .......... .......... .......... .......... .......... 57%  100M 1s
151800K .......... .......... .......... .......... .......... 57% 97.3M 1s
151850K .......... .......... .......... .......... .......... 57% 69.5M 1s
151900K .......... .......... .......... .......... .......... 57%  132M 1s
151950K .......... .......... .......... .......... .......... 57% 73.8M 1s
152000K .......... .......... .......... .......... .......... 57% 96.3M 1s
152050K .......... .......... .......... .......... .......... 58%  179M 1s
152100K .......... .......... .......... .......... .......... 58% 40.8M 1s
152150K .......... .......... .......... .......... .......... 58%  110M 1s
152200K .......... .......... .......... .......... .......... 58%  109M 1s
152250K .......... .......... .......... .......... .......... 58%  105M 1s
152300K .......... .......... .......... .......... .......... 58%  153M 1s
152350K .......... .......... .......... .......... .......... 58% 77.3M 1s
152400K .......... .......... .......... .......... .......... 58% 85.2M 1s
152450K .......... .......... .......... .......... .......... 58% 15.5M 1s
152500K .......... .......... .......... .......... .......... 58%  483M 1s
152550K .......... .......... .......... .......... .......... 58%  503M 1s
152600K .......... .......... .......... .......... .......... 58% 23.1M 1s
152650K .......... .......... .......... .......... .......... 58%  404M 1s
152700K .......... .......... .......... .......... .......... 58%  456M 1s
152750K .......... .......... .......... .......... .......... 58%  136M 1s
152800K .......... .......... .......... .......... .......... 58% 43.2M 1s
152850K .......... .......... .......... .......... .......... 58% 82.3M 1s
152900K .......... .......... .......... .......... .......... 58%  125M 1s
152950K .......... .......... .......... .......... .......... 58%  152M 1s
153000K .......... .......... .......... .......... .......... 58% 94.1M 1s
153050K .......... .......... .......... .......... .......... 58%  119M 1s
153100K .......... .......... .......... .......... .......... 58% 71.1M 1s
153150K .......... .......... .......... .......... .......... 58%  169M 1s
153200K .......... .......... .......... .......... .......... 58%  114M 1s
153250K .......... .......... .......... .......... .......... 58%  121M 1s
153300K .......... .......... .......... .......... .......... 58% 82.3M 1s
153350K .......... .......... .......... .......... .......... 58%  113M 1s
153400K .......... .......... .......... .......... .......... 58%  121M 1s
153450K .......... .......... .......... .......... .......... 58% 84.2M 1s
153500K .......... .......... .......... .......... .......... 58%  141M 1s
153550K .......... .......... .......... .......... .......... 58% 22.0M 1s
153600K .......... .......... .......... .......... .......... 58%  367M 1s
153650K .......... .......... .......... .......... .......... 58%  425M 1s
153700K .......... .......... .......... .......... .......... 58%  149M 1s
153750K .......... .......... .......... .......... .......... 58%  337M 1s
153800K .......... .......... .......... .......... .......... 58%  483M 1s
153850K .......... .......... .......... .......... .......... 58%  233M 1s
153900K .......... .......... .......... .......... .......... 58% 97.9M 1s
153950K .......... .......... .......... .......... .......... 58% 91.6M 1s
154000K .......... .......... .......... .......... .......... 58% 95.7M 1s
154050K .......... .......... .......... .......... .......... 58% 79.0M 1s
154100K .......... .......... .......... .......... .......... 58% 80.6M 1s
154150K .......... .......... .......... .......... .......... 58%  182M 1s
154200K .......... .......... .......... .......... .......... 58% 70.5M 1s
154250K .......... .......... .......... .......... .......... 58%  104M 1s
154300K .......... .......... .......... .......... .......... 58%  139M 1s
154350K .......... .......... .......... .......... .......... 58% 71.7M 1s
154400K .......... .......... .......... .......... .......... 58% 73.1M 1s
154450K .......... .......... .......... .......... .......... 58%  206M 1s
154500K .......... .......... .......... .......... .......... 58% 54.9M 1s
154550K .......... .......... .......... .......... .......... 58%  156M 1s
154600K .......... .......... .......... .......... .......... 58% 81.8M 1s
154650K .......... .......... .......... .......... .......... 58% 74.5M 1s
154700K .......... .......... .......... .......... .......... 59% 91.1M 1s
154750K .......... .......... .......... .......... .......... 59%  106M 1s
154800K .......... .......... .......... .......... .......... 59%  112M 1s
154850K .......... .......... .......... .......... .......... 59%  106M 1s
154900K .......... .......... .......... .......... .......... 59% 61.7M 1s
154950K .......... .......... .......... .......... .......... 59% 89.1M 1s
155000K .......... .......... .......... .......... .......... 59%  109M 1s
155050K .......... .......... .......... .......... .......... 59%  110M 1s
155100K .......... .......... .......... .......... .......... 59% 77.1M 1s
155150K .......... .......... .......... .......... .......... 59%  102M 1s
155200K .......... .......... .......... .......... .......... 59% 68.6M 1s
155250K .......... .......... .......... .......... .......... 59%  201M 1s
155300K .......... .......... .......... .......... .......... 59% 67.9M 1s
155350K .......... .......... .......... .......... .......... 59% 96.1M 1s
155400K .......... .......... .......... .......... .......... 59% 73.5M 1s
155450K .......... .......... .......... .......... .......... 59%  126M 1s
155500K .......... .......... .......... .......... .......... 59% 71.0M 1s
155550K .......... .......... .......... .......... .......... 59%  136M 1s
155600K .......... .......... .......... .......... .......... 59% 50.6M 1s
155650K .......... .......... .......... .......... .......... 59%  391M 1s
155700K .......... .......... .......... .......... .......... 59% 48.4M 1s
155750K .......... .......... .......... .......... .......... 59% 26.3M 1s
155800K .......... .......... .......... .......... .......... 59%  179M 1s
155850K .......... .......... .......... .......... .......... 59% 41.1M 1s
155900K .......... .......... .......... .......... .......... 59% 98.2M 1s
155950K .......... .......... .......... .......... .......... 59% 62.3M 1s
156000K .......... .......... .......... .......... .......... 59% 97.3M 1s
156050K .......... .......... .......... .......... .......... 59%  109M 1s
156100K .......... .......... .......... .......... .......... 59% 78.1M 1s
156150K .......... .......... .......... .......... .......... 59% 91.1M 1s
156200K .......... .......... .......... .......... .......... 59% 54.4M 1s
156250K .......... .......... .......... .......... .......... 59%  105M 1s
156300K .......... .......... .......... .......... .......... 59%  150M 1s
156350K .......... .......... .......... .......... .......... 59% 60.2M 1s
156400K .......... .......... .......... .......... .......... 59%  111M 1s
156450K .......... .......... .......... .......... .......... 59% 89.3M 1s
156500K .......... .......... .......... .......... .......... 59% 98.0M 1s
156550K .......... .......... .......... .......... .......... 59%  106M 1s
156600K .......... .......... .......... .......... .......... 59% 79.4M 1s
156650K .......... .......... .......... .......... .......... 59%  123M 1s
156700K .......... .......... .......... .......... .......... 59% 69.5M 1s
156750K .......... .......... .......... .......... .......... 59%  121M 1s
156800K .......... .......... .......... .......... .......... 59%  126M 1s
156850K .......... .......... .......... .......... .......... 59% 35.6M 1s
156900K .......... .......... .......... .......... .......... 59%  432M 1s
156950K .......... .......... .......... .......... .......... 59%  483M 1s
157000K .......... .......... .......... .......... .......... 59% 23.4M 1s
157050K .......... .......... .......... .......... .......... 59%  187M 1s
157100K .......... .......... .......... .......... .......... 59%  168M 1s
157150K .......... .......... .......... .......... .......... 59% 48.7M 1s
157200K .......... .......... .......... .......... .......... 59% 78.3M 1s
157250K .......... .......... .......... .......... .......... 59%  166M 1s
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157350K .......... .......... .......... .......... .......... 60% 47.4M 1s
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157650K .......... .......... .......... .......... .......... 60% 91.6M 1s
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157900K .......... .......... .......... .......... .......... 60% 17.6M 1s
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158000K .......... .......... .......... .......... .......... 60%  186M 1s
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158100K .......... .......... .......... .......... .......... 60% 36.6M 1s
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158250K .......... .......... .......... .......... .......... 60% 93.2M 1s
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158900K .......... .......... .......... .......... .......... 60% 26.2M 1s
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159000K .......... .......... .......... .......... .......... 60%  525M 1s
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159100K .......... .......... .......... .......... .......... 60% 41.7M 1s
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159250K .......... .......... .......... .......... .......... 60%  317M 1s
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159350K .......... .......... .......... .......... .......... 60% 62.9M 1s
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159900K .......... .......... .......... .......... .......... 61% 95.9M 1s
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162150K .......... .......... .......... .......... .......... 61%  537M 1s
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167000K .......... .......... .......... .......... .......... 63% 87.0M 1s
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170000K .......... .......... .......... .......... .......... 64% 88.0M 1s
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170700K .......... .......... .......... .......... .......... 65%  388M 1s
170750K .......... .......... .......... .......... .......... 65% 19.7M 1s
170800K .......... .......... .......... .......... .......... 65%  182M 1s
170850K .......... .......... .......... .......... .......... 65%  161M 1s
170900K .......... .......... .......... .......... .......... 65% 39.9M 1s
170950K .......... .......... .......... .......... .......... 65%  145M 1s
171000K .......... .......... .......... .......... .......... 65%  104M 1s
171050K .......... .......... .......... .......... .......... 65%  117M 1s
171100K .......... .......... .......... .......... .......... 65% 92.8M 1s
171150K .......... .......... .......... .......... .......... 65% 86.7M 1s
171200K .......... .......... .......... .......... .......... 65% 44.3M 1s
171250K .......... .......... .......... .......... .......... 65% 46.0M 1s
171300K .......... .......... .......... .......... .......... 65%  125M 1s
171350K .......... .......... .......... .......... .......... 65% 95.7M 1s
171400K .......... .......... .......... .......... .......... 65% 93.5M 1s
171450K .......... .......... .......... .......... .......... 65% 95.9M 1s
171500K .......... .......... .......... .......... .......... 65% 18.9M 1s
171550K .......... .......... .......... .......... .......... 65%  301M 1s
171600K .......... .......... .......... .......... .......... 65%  364M 1s
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171700K .......... .......... .......... .......... .......... 65%  407M 1s
171750K .......... .......... .......... .......... .......... 65% 94.3M 1s
171800K .......... .......... .......... .......... .......... 65%  150M 1s
171850K .......... .......... .......... .......... .......... 65% 84.0M 1s
171900K .......... .......... .......... .......... .......... 65%  531M 1s
171950K .......... .......... .......... .......... .......... 65% 78.5M 1s
172000K .......... .......... .......... .......... .......... 65% 28.7M 1s
172050K .......... .......... .......... .......... .......... 65%  428M 1s
172100K .......... .......... .......... .......... .......... 65% 55.1M 1s
172150K .......... .......... .......... .......... .......... 65% 63.3M 1s
172200K .......... .......... .......... .......... .......... 65% 47.5M 1s
172250K .......... .......... .......... .......... .......... 65%  176M 1s
172300K .......... .......... .......... .......... .......... 65% 53.9M 1s
172350K .......... .......... .......... .......... .......... 65% 56.1M 1s
172400K .......... .......... .......... .......... .......... 65% 62.2M 1s
172450K .......... .......... .......... .......... .......... 65% 63.4M 1s
172500K .......... .......... .......... .......... .......... 65% 77.6M 1s
172550K .......... .......... .......... .......... .......... 65% 63.0M 1s
172600K .......... .......... .......... .......... .......... 65% 62.3M 1s
172650K .......... .......... .......... .......... .......... 65% 25.2M 1s
172700K .......... .......... .......... .......... .......... 65% 42.6M 1s
172750K .......... .......... .......... .......... .......... 65% 60.4M 1s
172800K .......... .......... .......... .......... .......... 65% 65.5M 1s
172850K .......... .......... .......... .......... .......... 65% 36.8M 1s
172900K .......... .......... .......... .......... .......... 65%  214M 1s
172950K .......... .......... .......... .......... .......... 65% 54.9M 1s
173000K .......... .......... .......... .......... .......... 65% 53.8M 1s
173050K .......... .......... .......... .......... .......... 66% 63.7M 1s
173100K .......... .......... .......... .......... .......... 66% 54.3M 1s
173150K .......... .......... .......... .......... .......... 66% 75.0M 1s
173200K .......... .......... .......... .......... .......... 66% 47.0M 1s
173250K .......... .......... .......... .......... .......... 66% 52.8M 1s
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173400K .......... .......... .......... .......... .......... 66% 61.4M 1s
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173550K .......... .......... .......... .......... .......... 66% 75.6M 1s
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173700K .......... .......... .......... .......... .......... 66% 63.7M 1s
173750K .......... .......... .......... .......... .......... 66% 75.7M 1s
173800K .......... .......... .......... .......... .......... 66% 73.8M 1s
173850K .......... .......... .......... .......... .......... 66% 55.8M 1s
173900K .......... .......... .......... .......... .......... 66% 42.0M 1s
173950K .......... .......... .......... .......... .......... 66% 92.8M 1s
174000K .......... .......... .......... .......... .......... 66% 54.4M 1s
174050K .......... .......... .......... .......... .......... 66% 88.3M 1s
174100K .......... .......... .......... .......... .......... 66% 55.0M 1s
174150K .......... .......... .......... .......... .......... 66% 75.1M 1s
174200K .......... .......... .......... .......... .......... 66% 78.6M 1s
174250K .......... .......... .......... .......... .......... 66%  121M 1s
174300K .......... .......... .......... .......... .......... 66% 97.5M 1s
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174400K .......... .......... .......... .......... .......... 66%  127M 1s
174450K .......... .......... .......... .......... .......... 66% 19.2M 1s
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174700K .......... .......... .......... .......... .......... 66% 51.5M 1s
174750K .......... .......... .......... .......... .......... 66% 88.3M 1s
174800K .......... .......... .......... .......... .......... 66% 42.1M 1s
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174900K .......... .......... .......... .......... .......... 66%  498M 1s
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175000K .......... .......... .......... .......... .......... 66%  388M 1s
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175100K .......... .......... .......... .......... .......... 66% 34.1M 1s
175150K .......... .......... .......... .......... .......... 66%  425M 1s
175200K .......... .......... .......... .......... .......... 66%  180M 1s
175250K .......... .......... .......... .......... .......... 66% 73.6M 1s
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175400K .......... .......... .......... .......... .......... 66% 65.1M 1s
175450K .......... .......... .......... .......... .......... 66% 62.5M 1s
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175550K .......... .......... .......... .......... .......... 66% 76.5M 1s
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175750K .......... .......... .......... .......... .......... 67% 63.0M 1s
175800K .......... .......... .......... .......... .......... 67% 92.7M 1s
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175900K .......... .......... .......... .......... .......... 67% 61.0M 1s
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176000K .......... .......... .......... .......... .......... 67% 60.7M 1s
176050K .......... .......... .......... .......... .......... 67% 99.6M 1s
176100K .......... .......... .......... .......... .......... 67% 52.2M 1s
176150K .......... .......... .......... .......... .......... 67% 49.0M 1s
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176250K .......... .......... .......... .......... .......... 67% 54.0M 1s
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176500K .......... .......... .......... .......... .......... 67%  121M 1s
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177000K .......... .......... .......... .......... .......... 67% 82.6M 1s
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177250K .......... .......... .......... .......... .......... 67% 54.7M 1s
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177850K .......... .......... .......... .......... .......... 67% 22.2M 1s
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178100K .......... .......... .......... .......... .......... 67%  425M 1s
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182150K .......... .......... .......... .......... .......... 69% 92.0M 1s
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183000K .......... .......... .......... .......... .......... 69%  195M 1s
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183100K .......... .......... .......... .......... .......... 69% 78.1M 1s
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183700K .......... .......... .......... .......... .......... 70% 15.5M 1s
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183900K .......... .......... .......... .......... .......... 70% 36.4M 1s
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184150K .......... .......... .......... .......... .......... 70% 91.4M 1s
184200K .......... .......... .......... .......... .......... 70%  128M 1s
184250K .......... .......... .......... .......... .......... 70% 96.3M 1s
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184350K .......... .......... .......... .......... .......... 70% 86.9M 1s
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184750K .......... .......... .......... .......... .......... 70% 32.6M 1s
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185000K .......... .......... .......... .......... .......... 70%  195M 1s
185050K .......... .......... .......... .......... .......... 70%  194M 1s
185100K .......... .......... .......... .......... .......... 70% 76.8M 1s
185150K .......... .......... .......... .......... .......... 70% 88.6M 1s
185200K .......... .......... .......... .......... .......... 70% 54.5M 1s
185250K .......... .......... .......... .......... .......... 70%  531M 1s
185300K .......... .......... .......... .......... .......... 70% 18.8M 1s
185350K .......... .......... .......... .......... .......... 70%  159M 1s
185400K .......... .......... .......... .......... .......... 70% 36.1M 1s
185450K .......... .......... .......... .......... .......... 70%  130M 1s
185500K .......... .......... .......... .......... .......... 70%  104M 1s
185550K .......... .......... .......... .......... .......... 70%  142M 1s
185600K .......... .......... .......... .......... .......... 70% 71.6M 1s
185650K .......... .......... .......... .......... .......... 70%  100M 1s
185700K .......... .......... .......... .......... .......... 70%  139M 1s
185750K .......... .......... .......... .......... .......... 70%  102M 1s
185800K .......... .......... .......... .......... .......... 70%  100M 1s
185850K .......... .......... .......... .......... .......... 70% 92.3M 1s
185900K .......... .......... .......... .......... .......... 70%  108M 1s
185950K .......... .......... .......... .......... .......... 70% 89.3M 1s
186000K .......... .......... .......... .......... .......... 70%  141M 1s
186050K .......... .......... .......... .......... .......... 70%  104M 1s
186100K .......... .......... .......... .......... .......... 70% 84.0M 1s
186150K .......... .......... .......... .......... .......... 71%  175M 1s
186200K .......... .......... .......... .......... .......... 71% 21.1M 1s
186250K .......... .......... .......... .......... .......... 71%  186M 1s
186300K .......... .......... .......... .......... .......... 71% 12.1M 1s
186350K .......... .......... .......... .......... .......... 71%  153M 1s
186400K .......... .......... .......... .......... .......... 71% 43.7M 1s
186450K .......... .......... .......... .......... .......... 71%  108M 1s
186500K .......... .......... .......... .......... .......... 71%  108M 1s
186550K .......... .......... .......... .......... .......... 71% 64.9M 1s
186600K .......... .......... .......... .......... .......... 71% 92.3M 1s
186650K .......... .......... .......... .......... .......... 71%  126M 1s
186700K .......... .......... .......... .......... .......... 71% 75.6M 1s
186750K .......... .......... .......... .......... .......... 71%  137M 1s
186800K .......... .......... .......... .......... .......... 71% 85.4M 1s
186850K .......... .......... .......... .......... .......... 71% 94.3M 1s
186900K .......... .......... .......... .......... .......... 71% 99.4M 1s
186950K .......... .......... .......... .......... .......... 71% 66.0M 1s
187000K .......... .......... .......... .......... .......... 71%  178M 1s
187050K .......... .......... .......... .......... .......... 71% 79.4M 1s
187100K .......... .......... .......... .......... .......... 71% 20.2M 1s
187150K .......... .......... .......... .......... .......... 71%  503M 1s
187200K .......... .......... .......... .......... .......... 71% 31.8M 1s
187250K .......... .......... .......... .......... .......... 71%  525M 1s
187300K .......... .......... .......... .......... .......... 71% 10.9M 1s
187350K .......... .......... .......... .......... .......... 71%  332M 1s
187400K .......... .......... .......... .......... .......... 71%  514M 1s
187450K .......... .......... .......... .......... .......... 71% 32.4M 1s
187500K .......... .......... .......... .......... .......... 71%  537M 1s
187550K .......... .......... .......... .......... .......... 71%  156M 1s
187600K .......... .......... .......... .......... .......... 71% 53.5M 1s
187650K .......... .......... .......... .......... .......... 71%  178M 1s
187700K .......... .......... .......... .......... .......... 71% 86.6M 1s
187750K .......... .......... .......... .......... .......... 71%  106M 1s
187800K .......... .......... .......... .......... .......... 71%  115M 1s
187850K .......... .......... .......... .......... .......... 71% 61.3M 1s
187900K .......... .......... .......... .......... .......... 71%  192M 1s
187950K .......... .......... .......... .......... .......... 71% 91.6M 1s
188000K .......... .......... .......... .......... .......... 71% 69.8M 1s
188050K .......... .......... .......... .......... .......... 71%  171M 1s
188100K .......... .......... .......... .......... .......... 71% 82.5M 1s
188150K .......... .......... .......... .......... .......... 71% 98.2M 1s
188200K .......... .......... .......... .......... .......... 71% 91.1M 1s
188250K .......... .......... .......... .......... .......... 71%  126M 1s
188300K .......... .......... .......... .......... .......... 71%  135M 1s
188350K .......... .......... .......... .......... .......... 71% 35.7M 1s
188400K .......... .......... .......... .......... .......... 71% 11.2M 1s
188450K .......... .......... .......... .......... .......... 71% 35.4M 1s
188500K .......... .......... .......... .......... .......... 71%  164M 1s
188550K .......... .......... .......... .......... .......... 71%  169M 1s
188600K .......... .......... .......... .......... .......... 71% 74.3M 1s
188650K .......... .......... .......... .......... .......... 71% 51.5M 1s
188700K .......... .......... .......... .......... .......... 71%  151M 1s
188750K .......... .......... .......... .......... .......... 72%  196M 1s
188800K .......... .......... .......... .......... .......... 72% 44.9M 1s
188850K .......... .......... .......... .......... .......... 72% 85.4M 1s
188900K .......... .......... .......... .......... .......... 72%  176M 1s
188950K .......... .......... .......... .......... .......... 72% 58.5M 1s
189000K .......... .......... .......... .......... .......... 72%  175M 1s
189050K .......... .......... .......... .......... .......... 72% 97.3M 1s
189100K .......... .......... .......... .......... .......... 72% 75.6M 1s
189150K .......... .......... .......... .......... .......... 72%  113M 1s
189200K .......... .......... .......... .......... .......... 72% 87.5M 1s
189250K .......... .......... .......... .......... .......... 72%  129M 1s
189300K .......... .......... .......... .......... .......... 72% 70.7M 1s
189350K .......... .......... .......... .......... .......... 72% 81.8M 1s
189400K .......... .......... .......... .......... .......... 72% 32.6M 1s
189450K .......... .......... .......... .......... .......... 72%  159M 1s
189500K .......... .......... .......... .......... .......... 72%  191M 1s
189550K .......... .......... .......... .......... .......... 72% 20.1M 1s
189600K .......... .......... .......... .......... .......... 72%  159M 1s
189650K .......... .......... .......... .......... .......... 72% 42.3M 1s
189700K .......... .......... .......... .......... .......... 72% 24.3M 1s
189750K .......... .......... .......... .......... .......... 72%  488M 1s
189800K .......... .......... .......... .......... .......... 72%  509M 1s
189850K .......... .......... .......... .......... .......... 72% 25.1M 1s
189900K .......... .......... .......... .......... .......... 72%  184M 1s
189950K .......... .......... .......... .......... .......... 72%  162M 1s
190000K .......... .......... .......... .......... .......... 72% 44.9M 1s
190050K .......... .......... .......... .......... .......... 72%  114M 1s
190100K .......... .......... .......... .......... .......... 72% 95.2M 1s
190150K .......... .......... .......... .......... .......... 72%  120M 1s
190200K .......... .......... .......... .......... .......... 72% 93.9M 1s
190250K .......... .......... .......... .......... .......... 72%  108M 1s
190300K .......... .......... .......... .......... .......... 72% 73.8M 1s
190350K .......... .......... .......... .......... .......... 72%  162M 1s
190400K .......... .......... .......... .......... .......... 72% 85.7M 1s
190450K .......... .......... .......... .......... .......... 72%  100M 1s
190500K .......... .......... .......... .......... .......... 72%  120M 1s
190550K .......... .......... .......... .......... .......... 72% 10.9M 1s
190600K .......... .......... .......... .......... .......... 72%  153M 1s
190650K .......... .......... .......... .......... .......... 72%  184M 1s
190700K .......... .......... .......... .......... .......... 72% 15.8M 1s
190750K .......... .......... .......... .......... .......... 72%  432M 1s
190800K .......... .......... .......... .......... .......... 72%  514M 1s
190850K .......... .......... .......... .......... .......... 72% 48.8M 1s
190900K .......... .......... .......... .......... .......... 72%  154M 1s
190950K .......... .......... .......... .......... .......... 72% 72.8M 1s
191000K .......... .......... .......... .......... .......... 72%  128M 1s
191050K .......... .......... .......... .......... .......... 72% 11.3M 1s
191100K .......... .......... .......... .......... .......... 72%  404M 1s
191150K .......... .......... .......... .......... .......... 72%  525M 1s
191200K .......... .......... .......... .......... .......... 72% 45.9M 1s
191250K .......... .......... .......... .......... .......... 72%  120M 1s
191300K .......... .......... .......... .......... .......... 72% 17.9M 1s
191350K .......... .......... .......... .......... .......... 72%  105M 1s
191400K .......... .......... .......... .......... .......... 73%  474M 1s
191450K .......... .......... .......... .......... .......... 73% 35.8M 1s
191500K .......... .......... .......... .......... .......... 73%  152M 1s
191550K .......... .......... .......... .......... .......... 73% 12.6M 1s
191600K .......... .......... .......... .......... .......... 73%  150M 1s
191650K .......... .......... .......... .......... .......... 73%  192M 1s
191700K .......... .......... .......... .......... .......... 73% 40.3M 1s
191750K .......... .......... .......... .......... .......... 73%  190M 1s
191800K .......... .......... .......... .......... .......... 73% 95.0M 1s
191850K .......... .......... .......... .......... .......... 73%  125M 1s
191900K .......... .......... .......... .......... .......... 73% 69.2M 1s
191950K .......... .......... .......... .......... .......... 73%  163M 1s
192000K .......... .......... .......... .......... .......... 73%  115M 1s
192050K .......... .......... .......... .......... .......... 73%  119M 1s
192100K .......... .......... .......... .......... .......... 73% 80.7M 1s
192150K .......... .......... .......... .......... .......... 73% 30.2M 1s
192200K .......... .......... .......... .......... .......... 73%  164M 1s
192250K .......... .......... .......... .......... .......... 73%  195M 1s
192300K .......... .......... .......... .......... .......... 73% 11.8M 1s
192350K .......... .......... .......... .......... .......... 73%  291M 1s
192400K .......... .......... .......... .......... .......... 73%  493M 1s
192450K .......... .......... .......... .......... .......... 73% 30.4M 1s
192500K .......... .......... .......... .......... .......... 73%  367M 1s
192550K .......... .......... .......... .......... .......... 73%  440M 1s
192600K .......... .......... .......... .......... .......... 73% 47.4M 1s
192650K .......... .......... .......... .......... .......... 73%  179M 1s
192700K .......... .......... .......... .......... .......... 73%  165M 1s
192750K .......... .......... .......... .......... .......... 73% 59.8M 1s
192800K .......... .......... .......... .......... .......... 73% 92.7M 1s
192850K .......... .......... .......... .......... .......... 73% 57.0M 1s
192900K .......... .......... .......... .......... .......... 73%  187M 1s
192950K .......... .......... .......... .......... .......... 73% 63.0M 1s
193000K .......... .......... .......... .......... .......... 73% 99.0M 1s
193050K .......... .......... .......... .......... .......... 73%  143M 1s
193100K .......... .......... .......... .......... .......... 73%  105M 1s
193150K .......... .......... .......... .......... .......... 73%  110M 1s
193200K .......... .......... .......... .......... .......... 73% 8.35M 1s
193250K .......... .......... .......... .......... .......... 73%  417M 1s
193300K .......... .......... .......... .......... .......... 73%  479M 1s
193350K .......... .......... .......... .......... .......... 73%  421M 1s
193400K .......... .......... .......... .......... .......... 73% 23.3M 1s
193450K .......... .......... .......... .......... .......... 73%  157M 1s
193500K .......... .......... .......... .......... .......... 73%  174M 1s
193550K .......... .......... .......... .......... .......... 73% 11.9M 1s
193600K .......... .......... .......... .......... .......... 73%  407M 1s
193650K .......... .......... .......... .......... .......... 73%  531M 1s
193700K .......... .......... .......... .......... .......... 73% 38.6M 1s
193750K .......... .......... .......... .......... .......... 73% 79.5M 1s
193800K .......... .......... .......... .......... .......... 73%  268M 1s
193850K .......... .......... .......... .......... .......... 73% 60.4M 1s
193900K .......... .......... .......... .......... .......... 73%  179M 1s
193950K .......... .......... .......... .......... .......... 73% 15.5M 1s
194000K .......... .......... .......... .......... .......... 74%  367M 1s
194050K .......... .......... .......... .......... .......... 74%  503M 1s
194100K .......... .......... .......... .......... .......... 74%  432M 1s
194150K .......... .......... .......... .......... .......... 74% 7.20M 1s
194200K .......... .......... .......... .......... .......... 74%  151M 1s
194250K .......... .......... .......... .......... .......... 74%  178M 1s
194300K .......... .......... .......... .......... .......... 74%  187M 1s
194350K .......... .......... .......... .......... .......... 74% 26.3M 1s
194400K .......... .......... .......... .......... .......... 74%  488M 1s
194450K .......... .......... .......... .......... .......... 74%  187M 1s
194500K .......... .......... .......... .......... .......... 74%  113M 1s
194550K .......... .......... .......... .......... .......... 74%  115M 1s
194600K .......... .......... .......... .......... .......... 74% 92.3M 1s
194650K .......... .......... .......... .......... .......... 74%  110M 1s
194700K .......... .......... .......... .......... .......... 74% 94.8M 1s
194750K .......... .......... .......... .......... .......... 74% 99.0M 1s
194800K .......... .......... .......... .......... .......... 74%  187M 1s
194850K .......... .......... .......... .......... .......... 74% 90.6M 1s
194900K .......... .......... .......... .......... .......... 74%  143M 1s
194950K .......... .......... .......... .......... .......... 74% 68.2M 1s
195000K .......... .......... .......... .......... .......... 74% 27.9M 1s
195050K .......... .......... .......... .......... .......... 74%  498M 1s
195100K .......... .......... .......... .......... .......... 74%  376M 1s
195150K .......... .......... .......... .......... .......... 74%  525M 1s
195200K .......... .......... .......... .......... .......... 74% 39.4M 1s
195250K .......... .......... .......... .......... .......... 74% 27.0M 1s
195300K .......... .......... .......... .......... .......... 74%  188M 1s
195350K .......... .......... .......... .......... .......... 74%  162M 1s
195400K .......... .......... .......... .......... .......... 74% 15.3M 1s
195450K .......... .......... .......... .......... .......... 74%  126M 1s
195500K .......... .......... .......... .......... .......... 74%  184M 1s
195550K .......... .......... .......... .......... .......... 74%  191M 1s
195600K .......... .......... .......... .......... .......... 74% 30.4M 1s
195650K .......... .......... .......... .......... .......... 74%  346M 1s
195700K .......... .......... .......... .......... .......... 74%  136M 1s
195750K .......... .......... .......... .......... .......... 74% 96.9M 1s
195800K .......... .......... .......... .......... .......... 74% 85.8M 1s
195850K .......... .......... .......... .......... .......... 74%  129M 1s
195900K .......... .......... .......... .......... .......... 74%  116M 1s
195950K .......... .......... .......... .......... .......... 74% 97.7M 1s
196000K .......... .......... .......... .......... .......... 74% 94.8M 1s
196050K .......... .......... .......... .......... .......... 74%  135M 1s
196100K .......... .......... .......... .......... .......... 74% 94.1M 1s
196150K .......... .......... .......... .......... .......... 74%  122M 1s
196200K .......... .......... .......... .......... .......... 74% 74.1M 1s
196250K .......... .......... .......... .......... .......... 74% 84.5M 1s
196300K .......... .......... .......... .......... .......... 74%  125M 1s
196350K .......... .......... .......... .......... .......... 74%  140M 1s
196400K .......... .......... .......... .......... .......... 74% 73.9M 1s
196450K .......... .......... .......... .......... .......... 74%  156M 1s
196500K .......... .......... .......... .......... .......... 74% 89.3M 1s
196550K .......... .......... .......... .......... .......... 74%  136M 1s
196600K .......... .......... .......... .......... .......... 74% 48.8M 1s
196650K .......... .......... .......... .......... .......... 75%  168M 1s
196700K .......... .......... .......... .......... .......... 75%  145M 1s
196750K .......... .......... .......... .......... .......... 75% 73.8M 1s
196800K .......... .......... .......... .......... .......... 75% 93.2M 1s
196850K .......... .......... .......... .......... .......... 75% 94.6M 1s
196900K .......... .......... .......... .......... .......... 75%  120M 1s
196950K .......... .......... .......... .......... .......... 75% 30.0M 1s
197000K .......... .......... .......... .......... .......... 75%  346M 1s
197050K .......... .......... .......... .......... .......... 75% 78.3M 1s
197100K .......... .......... .......... .......... .......... 75%  250M 1s
197150K .......... .......... .......... .......... .......... 75% 59.5M 1s
197200K .......... .......... .......... .......... .......... 75%  239M 1s
197250K .......... .......... .......... .......... .......... 75%  156M 1s
197300K .......... .......... .......... .......... .......... 75% 88.9M 1s
197350K .......... .......... .......... .......... .......... 75%  328M 1s
197400K .......... .......... .......... .......... .......... 75%  163M 1s
197450K .......... .......... .......... .......... .......... 75% 48.8M 1s
197500K .......... .......... .......... .......... .......... 75% 74.5M 1s
197550K .......... .......... .......... .......... .......... 75% 75.2M 1s
197600K .......... .......... .......... .......... .......... 75% 54.7M 1s
197650K .......... .......... .......... .......... .......... 75% 63.2M 1s
197700K .......... .......... .......... .......... .......... 75% 62.0M 1s
197750K .......... .......... .......... .......... .......... 75% 57.6M 1s
197800K .......... .......... .......... .......... .......... 75% 36.5M 1s
197850K .......... .......... .......... .......... .......... 75% 52.1M 1s
197900K .......... .......... .......... .......... .......... 75%  104M 1s
197950K .......... .......... .......... .......... .......... 75% 45.2M 1s
198000K .......... .......... .......... .......... .......... 75% 31.7M 1s
198050K .......... .......... .......... .......... .......... 75% 40.9M 1s
198100K .......... .......... .......... .......... .......... 75% 50.9M 1s
198150K .......... .......... .......... .......... .......... 75% 92.8M 1s
198200K .......... .......... .......... .......... .......... 75% 52.6M 1s
198250K .......... .......... .......... .......... .......... 75% 65.2M 1s
198300K .......... .......... .......... .......... .......... 75% 69.0M 1s
198350K .......... .......... .......... .......... .......... 75% 50.4M 1s
198400K .......... .......... .......... .......... .......... 75% 64.3M 1s
198450K .......... .......... .......... .......... .......... 75% 61.9M 1s
198500K .......... .......... .......... .......... .......... 75% 47.0M 1s
198550K .......... .......... .......... .......... .......... 75% 56.3M 1s
198600K .......... .......... .......... .......... .......... 75% 45.5M 1s
198650K .......... .......... .......... .......... .......... 75% 63.0M 1s
198700K .......... .......... .......... .......... .......... 75% 55.5M 1s
198750K .......... .......... .......... .......... .......... 75% 63.4M 1s
198800K .......... .......... .......... .......... .......... 75% 94.1M 1s
198850K .......... .......... .......... .......... .......... 75% 54.2M 1s
198900K .......... .......... .......... .......... .......... 75% 61.0M 1s
198950K .......... .......... .......... .......... .......... 75% 48.7M 1s
199000K .......... .......... .......... .......... .......... 75%  123M 1s
199050K .......... .......... .......... .......... .......... 75% 63.5M 1s
199100K .......... .......... .......... .......... .......... 75% 53.0M 1s
199150K .......... .......... .......... .......... .......... 75% 55.3M 1s
199200K .......... .......... .......... .......... .......... 75% 91.4M 1s
199250K .......... .......... .......... .......... .......... 76% 63.8M 1s
199300K .......... .......... .......... .......... .......... 76% 54.9M 1s
199350K .......... .......... .......... .......... .......... 76% 63.6M 1s
199400K .......... .......... .......... .......... .......... 76% 75.1M 1s
199450K .......... .......... .......... .......... .......... 76% 74.2M 1s
199500K .......... .......... .......... .......... .......... 76% 72.4M 1s
199550K .......... .......... .......... .......... .......... 76% 81.4M 1s
199600K .......... .......... .......... .......... .......... 76% 92.0M 1s
199650K .......... .......... .......... .......... .......... 76%  130M 1s
199700K .......... .......... .......... .......... .......... 76% 94.8M 1s
199750K .......... .......... .......... .......... .......... 76% 94.3M 1s
199800K .......... .......... .......... .......... .......... 76%  114M 1s
199850K .......... .......... .......... .......... .......... 76%  101M 1s
199900K .......... .......... .......... .......... .......... 76%  123M 1s
199950K .......... .......... .......... .......... .......... 76% 12.0M 1s
200000K .......... .......... .......... .......... .......... 76%  407M 1s
200050K .......... .......... .......... .......... .......... 76%  488M 1s
200100K .......... .......... .......... .......... .......... 76%  407M 1s
200150K .......... .......... .......... .......... .......... 76%  525M 1s
200200K .......... .......... .......... .......... .......... 76%  362M 1s
200250K .......... .......... .......... .......... .......... 76%  192M 1s
200300K .......... .......... .......... .......... .......... 76%  187M 1s
200350K .......... .......... .......... .......... .......... 76% 82.3M 1s
200400K .......... .......... .......... .......... .......... 76%  284M 1s
200450K .......... .......... .......... .......... .......... 76%  214M 1s
200500K .......... .......... .......... .......... .......... 76% 98.0M 1s
200550K .......... .......... .......... .......... .......... 76%  204M 1s
200600K .......... .......... .......... .......... .......... 76% 57.0M 1s
200650K .......... .......... .......... .......... .......... 76%  388M 1s
200700K .......... .......... .......... .......... .......... 76%  101M 1s
200750K .......... .......... .......... .......... .......... 76%  493M 1s
200800K .......... .......... .......... .......... .......... 76%  274M 1s
200850K .......... .......... .......... .......... .......... 76% 47.0M 1s
200900K .......... .......... .......... .......... .......... 76%  161M 1s
200950K .......... .......... .......... .......... .......... 76% 82.2M 1s
201000K .......... .......... .......... .......... .......... 76% 80.6M 1s
201050K .......... .......... .......... .......... .......... 76% 92.1M 1s
201100K .......... .......... .......... .......... .......... 76% 75.5M 1s
201150K .......... .......... .......... .......... .......... 76% 77.6M 1s
201200K .......... .......... .......... .......... .......... 76% 76.1M 1s
201250K .......... .......... .......... .......... .......... 76% 75.0M 1s
201300K .......... .......... .......... .......... .......... 76% 94.8M 1s
201350K .......... .......... .......... .......... .......... 76% 74.8M 1s
201400K .......... .......... .......... .......... .......... 76% 93.0M 1s
201450K .......... .......... .......... .......... .......... 76% 64.5M 1s
201500K .......... .......... .......... .......... .......... 76% 90.9M 1s
201550K .......... .......... .......... .......... .......... 76% 95.2M 1s
201600K .......... .......... .......... .......... .......... 76% 75.9M 1s
201650K .......... .......... .......... .......... .......... 76% 78.6M 1s
201700K .......... .......... .......... .......... .......... 76% 73.3M 1s
201750K .......... .......... .......... .......... .......... 76% 77.5M 1s
201800K .......... .......... .......... .......... .......... 76% 95.2M 1s
201850K .......... .......... .......... .......... .......... 76% 74.7M 1s
201900K .......... .......... .......... .......... .......... 77% 73.2M 1s
201950K .......... .......... .......... .......... .......... 77% 75.5M 1s
202000K .......... .......... .......... .......... .......... 77% 75.0M 1s
202050K .......... .......... .......... .......... .......... 77% 94.8M 1s
202100K .......... .......... .......... .......... .......... 77% 62.9M 1s
202150K .......... .......... .......... .......... .......... 77% 76.7M 1s
202200K .......... .......... .......... .......... .......... 77% 74.5M 1s
202250K .......... .......... .......... .......... .......... 77% 94.6M 1s
202300K .......... .......... .......... .......... .......... 77%  116M 1s
202350K .......... .......... .......... .......... .......... 77% 79.0M 1s
202400K .......... .......... .......... .......... .......... 77% 79.0M 1s
202450K .......... .......... .......... .......... .......... 77% 93.9M 1s
202500K .......... .......... .......... .......... .......... 77% 92.7M 1s
202550K .......... .......... .......... .......... .......... 77% 97.1M 1s
202600K .......... .......... .......... .......... .......... 77% 73.4M 1s
202650K .......... .......... .......... .......... .......... 77% 93.7M 1s
202700K .......... .......... .......... .......... .......... 77% 77.0M 1s
202750K .......... .......... .......... .......... .......... 77% 97.1M 1s
202800K .......... .......... .......... .......... .......... 77%  123M 1s
202850K .......... .......... .......... .......... .......... 77% 63.5M 1s
202900K .......... .......... .......... .......... .......... 77% 97.3M 1s
202950K .......... .......... .......... .......... .......... 77% 90.4M 1s
203000K .......... .......... .......... .......... .......... 77% 98.0M 1s
203050K .......... .......... .......... .......... .......... 77% 75.9M 1s
203100K .......... .......... .......... .......... .......... 77% 95.2M 1s
203150K .......... .......... .......... .......... .......... 77% 93.2M 1s
203200K .......... .......... .......... .......... .......... 77% 73.2M 1s
203250K .......... .......... .......... .......... .......... 77% 94.6M 1s
203300K .......... .......... .......... .......... .......... 77% 78.5M 1s
203350K .......... .......... .......... .......... .......... 77% 73.3M 1s
203400K .......... .......... .......... .......... .......... 77% 95.4M 1s
203450K .......... .......... .......... .......... .......... 77% 75.1M 1s
203500K .......... .......... .......... .......... .......... 77% 77.9M 1s
203550K .......... .......... .......... .......... .......... 77% 94.6M 1s
203600K .......... .......... .......... .......... .......... 77% 70.6M 1s
203650K .......... .......... .......... .......... .......... 77% 80.0M 1s
203700K .......... .......... .......... .......... .......... 77% 72.0M 1s
203750K .......... .......... .......... .......... .......... 77%  126M 1s
203800K .......... .......... .......... .......... .......... 77% 73.6M 1s
203850K .......... .......... .......... .......... .......... 77% 77.6M 1s
203900K .......... .......... .......... .......... .......... 77%  126M 1s
203950K .......... .......... .......... .......... .......... 77% 93.0M 1s
204000K .......... .......... .......... .......... .......... 77% 97.7M 1s
204050K .......... .......... .......... .......... .......... 77% 31.6M 1s
204100K .......... .......... .......... .......... .......... 77%  229M 1s
204150K .......... .......... .......... .......... .......... 77% 66.0M 1s
204200K .......... .......... .......... .......... .......... 77%  194M 1s
204250K .......... .......... .......... .......... .......... 77% 75.5M 1s
204300K .......... .......... .......... .......... .......... 77%  164M 1s
204350K .......... .......... .......... .......... .......... 77%  404M 1s
204400K .......... .......... .......... .......... .......... 77% 78.8M 1s
204450K .......... .......... .......... .......... .......... 77% 76.7M 1s
204500K .......... .......... .......... .......... .......... 78% 95.0M 1s
204550K .......... .......... .......... .......... .......... 78%  115M 1s
204600K .......... .......... .......... .......... .......... 78% 66.4M 1s
204650K .......... .......... .......... .......... .......... 78% 76.3M 1s
204700K .......... .......... .......... .......... .......... 78% 87.7M 1s
204750K .......... .......... .......... .......... .......... 78% 74.2M 1s
204800K .......... .......... .......... .......... .......... 78% 95.9M 1s
204850K .......... .......... .......... .......... .......... 78% 46.9M 1s
204900K .......... .......... .......... .......... .......... 78% 64.8M 1s
204950K .......... .......... .......... .......... .......... 78%  127M 1s
205000K .......... .......... .......... .......... .......... 78% 75.4M 1s
205050K .......... .......... .......... .......... .......... 78% 62.7M 1s
205100K .......... .......... .......... .......... .......... 78% 51.9M 1s
205150K .......... .......... .......... .......... .......... 78%  100M 1s
205200K .......... .......... .......... .......... .......... 78% 73.9M 1s
205250K .......... .......... .......... .......... .......... 78%  133M 1s
205300K .......... .......... .......... .......... .......... 78% 69.1M 1s
205350K .......... .......... .......... .......... .......... 78% 67.9M 1s
205400K .......... .......... .......... .......... .......... 78%  107M 1s
205450K .......... .......... .......... .......... .......... 78% 50.8M 1s
205500K .......... .......... .......... .......... .......... 78%  131M 1s
205550K .......... .......... .......... .......... .......... 78% 70.3M 1s
205600K .......... .......... .......... .......... .......... 78% 78.8M 1s
205650K .......... .......... .......... .......... .......... 78% 74.9M 1s
205700K .......... .......... .......... .......... .......... 78% 78.0M 1s
205750K .......... .......... .......... .......... .......... 78%  121M 1s
205800K .......... .......... .......... .......... .......... 78% 75.1M 1s
205850K .......... .......... .......... .......... .......... 78% 77.6M 1s
205900K .......... .......... .......... .......... .......... 78%  126M 1s
205950K .......... .......... .......... .......... .......... 78% 72.7M 1s
206000K .......... .......... .......... .......... .......... 78% 97.9M 1s
206050K .......... .......... .......... .......... .......... 78% 92.1M 1s
206100K .......... .......... .......... .......... .......... 78% 75.9M 1s
206150K .......... .......... .......... .......... .......... 78% 63.0M 1s
206200K .......... .......... .......... .......... .......... 78%  117M 1s
206250K .......... .......... .......... .......... .......... 78% 65.3M 1s
206300K .......... .......... .......... .......... .......... 78%  126M 1s
206350K .......... .......... .......... .......... .......... 78% 63.3M 1s
206400K .......... .......... .......... .......... .......... 78%  125M 1s
206450K .......... .......... .......... .......... .......... 78% 62.8M 1s
206500K .......... .......... .......... .......... .......... 78%  122M 1s
206550K .......... .......... .......... .......... .......... 78% 76.8M 1s
206600K .......... .......... .......... .......... .......... 78% 54.0M 1s
206650K .......... .......... .......... .......... .......... 78%  106M 1s
206700K .......... .......... .......... .......... .......... 78% 40.3M 1s
206750K .......... .......... .......... .......... .......... 78% 90.3M 1s
206800K .......... .......... .......... .......... .......... 78% 73.3M 1s
206850K .......... .......... .......... .......... .......... 78% 72.7M 1s
206900K .......... .......... .......... .......... .......... 78% 64.0M 1s
206950K .......... .......... .......... .......... .......... 78% 87.0M 1s
207000K .......... .......... .......... .......... .......... 78% 62.0M 1s
207050K .......... .......... .......... .......... .......... 78% 31.2M 1s
207100K .......... .......... .......... .......... .......... 79%  158M 1s
207150K .......... .......... .......... .......... .......... 79% 16.7M 1s
207200K .......... .......... .......... .......... .......... 79%  150M 1s
207250K .......... .......... .......... .......... .......... 79%  190M 1s
207300K .......... .......... .......... .......... .......... 79% 40.0M 1s
207350K .......... .......... .......... .......... .......... 79% 24.4M 1s
207400K .......... .......... .......... .......... .......... 79%  179M 1s
207450K .......... .......... .......... .......... .......... 79%  164M 1s
207500K .......... .......... .......... .......... .......... 79% 40.9M 1s
207550K .......... .......... .......... .......... .......... 79%  155M 1s
207600K .......... .......... .......... .......... .......... 79% 78.6M 1s
207650K .......... .......... .......... .......... .......... 79% 92.8M 1s
207700K .......... .......... .......... .......... .......... 79%  135M 1s
207750K .......... .......... .......... .......... .......... 79% 58.2M 1s
207800K .......... .......... .......... .......... .......... 79%  125M 1s
207850K .......... .......... .......... .......... .......... 79% 93.2M 1s
207900K .......... .......... .......... .......... .......... 79% 87.5M 1s
207950K .......... .......... .......... .......... .......... 79%  105M 1s
208000K .......... .......... .......... .......... .......... 79% 87.0M 1s
208050K .......... .......... .......... .......... .......... 79% 91.8M 1s
208100K .......... .......... .......... .......... .......... 79%  121M 1s
208150K .......... .......... .......... .......... .......... 79%  155M 1s
208200K .......... .......... .......... .......... .......... 79% 71.7M 1s
208250K .......... .......... .......... .......... .......... 79%  142M 1s
208300K .......... .......... .......... .......... .......... 79% 81.4M 1s
208350K .......... .......... .......... .......... .......... 79% 97.3M 1s
208400K .......... .......... .......... .......... .......... 79% 94.6M 1s
208450K .......... .......... .......... .......... .......... 79% 71.1M 1s
208500K .......... .......... .......... .......... .......... 79%  127M 1s
208550K .......... .......... .......... .......... .......... 79% 34.1M 1s
208600K .......... .......... .......... .......... .......... 79%  162M 1s
208650K .......... .......... .......... .......... .......... 79% 27.6M 1s
208700K .......... .......... .......... .......... .......... 79%  153M 1s
208750K .......... .......... .......... .......... .......... 79% 43.5M 1s
208800K .......... .......... .......... .......... .......... 79%  147M 1s
208850K .......... .......... .......... .......... .......... 79% 90.3M 1s
208900K .......... .......... .......... .......... .......... 79%  102M 1s
208950K .......... .......... .......... .......... .......... 79% 77.9M 1s
209000K .......... .......... .......... .......... .......... 79%  159M 1s
209050K .......... .......... .......... .......... .......... 79%  118M 1s
209100K .......... .......... .......... .......... .......... 79% 61.6M 1s
209150K .......... .......... .......... .......... .......... 79%  105M 1s
209200K .......... .......... .......... .......... .......... 79%  104M 1s
209250K .......... .......... .......... .......... .......... 79% 99.9M 1s
209300K .......... .......... .......... .......... .......... 79%  134M 1s
209350K .......... .......... .......... .......... .......... 79% 54.7M 1s
209400K .......... .......... .......... .......... .......... 79% 95.9M 1s
209450K .......... .......... .......... .......... .......... 79%  150M 1s
209500K .......... .......... .......... .......... .......... 79% 88.9M 1s
209550K .......... .......... .......... .......... .......... 79%  102M 1s
209600K .......... .......... .......... .......... .......... 79%  130M 1s
209650K .......... .......... .......... .......... .......... 79% 92.7M 1s
209700K .......... .......... .......... .......... .......... 79% 97.1M 1s
209750K .......... .......... .......... .......... .......... 80%  115M 1s
209800K .......... .......... .......... .......... .......... 80% 74.8M 1s
209850K .......... .......... .......... .......... .......... 80% 45.6M 1s
209900K .......... .......... .......... .......... .......... 80%  186M 1s
209950K .......... .......... .......... .......... .......... 80% 44.2M 1s
210000K .......... .......... .......... .......... .......... 80%  298M 1s
210050K .......... .......... .......... .......... .......... 80%  144M 1s
210100K .......... .......... .......... .......... .......... 80% 73.4M 1s
210150K .......... .......... .......... .......... .......... 80%  120M 1s
210200K .......... .......... .......... .......... .......... 80%  102M 1s
210250K .......... .......... .......... .......... .......... 80% 97.9M 1s
210300K .......... .......... .......... .......... .......... 80% 73.5M 1s
210350K .......... .......... .......... .......... .......... 80%  154M 1s
210400K .......... .......... .......... .......... .......... 80% 54.6M 1s
210450K .......... .......... .......... .......... .......... 80% 83.5M 1s
210500K .......... .......... .......... .......... .......... 80%  118M 1s
210550K .......... .......... .......... .......... .......... 80% 63.6M 1s
210600K .......... .......... .......... .......... .......... 80% 77.4M 1s
210650K .......... .......... .......... .......... .......... 80% 93.4M 1s
210700K .......... .......... .......... .......... .......... 80%  120M 1s
210750K .......... .......... .......... .......... .......... 80% 77.0M 1s
210800K .......... .......... .......... .......... .......... 80%  102M 1s
210850K .......... .......... .......... .......... .......... 80% 52.8M 1s
210900K .......... .......... .......... .......... .......... 80%  376M 1s
210950K .......... .......... .......... .......... .......... 80%  116M 1s
211000K .......... .......... .......... .......... .......... 80% 68.2M 1s
211050K .......... .......... .......... .......... .......... 80% 90.6M 1s
211100K .......... .......... .......... .......... .......... 80%  113M 1s
211150K .......... .......... .......... .......... .......... 80%  120M 1s
211200K .......... .......... .......... .......... .......... 80% 67.3M 1s
211250K .......... .......... .......... .......... .......... 80%  284M 1s
211300K .......... .......... .......... .......... .......... 80% 57.4M 1s
211350K .......... .......... .......... .......... .......... 80%  114M 1s
211400K .......... .......... .......... .......... .......... 80% 17.9M 1s
211450K .......... .......... .......... .......... .......... 80%  139M 1s
211500K .......... .......... .......... .......... .......... 80%  182M 1s
211550K .......... .......... .......... .......... .......... 80% 33.7M 1s
211600K .......... .......... .......... .......... .......... 80%  131M 1s
211650K .......... .......... .......... .......... .......... 80%  149M 1s
211700K .......... .......... .......... .......... .......... 80% 47.5M 1s
211750K .......... .......... .......... .......... .......... 80%  103M 1s
211800K .......... .......... .......... .......... .......... 80%  121M 1s
211850K .......... .......... .......... .......... .......... 80% 92.8M 1s
211900K .......... .......... .......... .......... .......... 80%  105M 1s
211950K .......... .......... .......... .......... .......... 80% 53.1M 1s
212000K .......... .......... .......... .......... .......... 80% 77.0M 1s
212050K .......... .......... .......... .......... .......... 80%  142M 1s
212100K .......... .......... .......... .......... .......... 80% 69.4M 1s
212150K .......... .......... .......... .......... .......... 80%  110M 1s
212200K .......... .......... .......... .......... .......... 80% 93.7M 1s
212250K .......... .......... .......... .......... .......... 80% 66.2M 1s
212300K .......... .......... .......... .......... .......... 80%  172M 1s
212350K .......... .......... .......... .......... .......... 81% 94.4M 1s
212400K .......... .......... .......... .......... .......... 81% 86.7M 1s
212450K .......... .......... .......... .......... .......... 81%  105M 1s
212500K .......... .......... .......... .......... .......... 81% 66.0M 1s
212550K .......... .......... .......... .......... .......... 81%  182M 1s
212600K .......... .......... .......... .......... .......... 81% 32.8M 1s
212650K .......... .......... .......... .......... .......... 81%  509M 1s
212700K .......... .......... .......... .......... .......... 81%  436M 1s
212750K .......... .......... .......... .......... .......... 81% 46.9M 1s
212800K .......... .......... .......... .......... .......... 81%  133M 1s
212850K .......... .......... .......... .......... .......... 81% 80.6M 1s
212900K .......... .......... .......... .......... .......... 81%  157M 1s
212950K .......... .......... .......... .......... .......... 81% 49.8M 1s
213000K .......... .......... .......... .......... .......... 81%  184M 1s
213050K .......... .......... .......... .......... .......... 81%  189M 1s
213100K .......... .......... .......... .......... .......... 81% 59.6M 1s
213150K .......... .......... .......... .......... .......... 81%  121M 1s
213200K .......... .......... .......... .......... .......... 81% 93.4M 1s
213250K .......... .......... .......... .......... .......... 81% 98.8M 1s
213300K .......... .......... .......... .......... .......... 81%  115M 1s
213350K .......... .......... .......... .......... .......... 81% 95.7M 1s
213400K .......... .......... .......... .......... .......... 81%  109M 1s
213450K .......... .......... .......... .......... .......... 81%  100M 1s
213500K .......... .......... .......... .......... .......... 81% 92.8M 1s
213550K .......... .......... .......... .......... .......... 81%  129M 1s
213600K .......... .......... .......... .......... .......... 81%  126M 1s
213650K .......... .......... .......... .......... .......... 81% 78.1M 1s
213700K .......... .......... .......... .......... .......... 81%  115M 1s
213750K .......... .......... .......... .......... .......... 81% 82.1M 1s
213800K .......... .......... .......... .......... .......... 81%  160M 1s
213850K .......... .......... .......... .......... .......... 81% 91.6M 1s
213900K .......... .......... .......... .......... .......... 81%  133M 1s
213950K .......... .......... .......... .......... .......... 81% 67.3M 1s
214000K .......... .......... .......... .......... .......... 81%  181M 1s
214050K .......... .......... .......... .......... .......... 81%  110M 1s
214100K .......... .......... .......... .......... .......... 81% 92.3M 1s
214150K .......... .......... .......... .......... .......... 81% 91.4M 1s
214200K .......... .......... .......... .......... .......... 81% 88.8M 1s
214250K .......... .......... .......... .......... .......... 81%  121M 1s
214300K .......... .......... .......... .......... .......... 81% 88.3M 1s
214350K .......... .......... .......... .......... .......... 81% 88.9M 1s
214400K .......... .......... .......... .......... .......... 81% 95.0M 1s
214450K .......... .......... .......... .......... .......... 81% 86.1M 1s
214500K .......... .......... .......... .......... .......... 81%  134M 1s
214550K .......... .......... .......... .......... .......... 81%  126M 1s
214600K .......... .......... .......... .......... .......... 81% 97.7M 1s
214650K .......... .......... .......... .......... .......... 81%  131M 1s
214700K .......... .......... .......... .......... .......... 81% 89.1M 1s
214750K .......... .......... .......... .......... .......... 81%  120M 1s
214800K .......... .......... .......... .......... .......... 81% 62.7M 1s
214850K .......... .......... .......... .......... .......... 81%  148M 1s
214900K .......... .......... .......... .......... .......... 81% 68.9M 1s
214950K .......... .......... .......... .......... .......... 81% 40.0M 1s
215000K .......... .......... .......... .......... .......... 82%  456M 1s
215050K .......... .......... .......... .......... .......... 82%  239M 1s
215100K .......... .......... .......... .......... .......... 82% 69.9M 1s
215150K .......... .......... .......... .......... .......... 82%  139M 1s
215200K .......... .......... .......... .......... .......... 82% 90.6M 1s
215250K .......... .......... .......... .......... .......... 82% 65.7M 1s
215300K .......... .......... .......... .......... .......... 82%  161M 1s
215350K .......... .......... .......... .......... .......... 82%  118M 1s
215400K .......... .......... .......... .......... .......... 82% 73.9M 1s
215450K .......... .......... .......... .......... .......... 82%  126M 1s
215500K .......... .......... .......... .......... .......... 82%  134M 1s
215550K .......... .......... .......... .......... .......... 82% 86.9M 1s
215600K .......... .......... .......... .......... .......... 82% 99.0M 1s
215650K .......... .......... .......... .......... .......... 82%  121M 1s
215700K .......... .......... .......... .......... .......... 82% 76.9M 1s
215750K .......... .......... .......... .......... .......... 82%  133M 1s
215800K .......... .......... .......... .......... .......... 82%  107M 1s
215850K .......... .......... .......... .......... .......... 82%  105M 1s
215900K .......... .......... .......... .......... .......... 82%  116M 1s
215950K .......... .......... .......... .......... .......... 82% 70.2M 1s
216000K .......... .......... .......... .......... .......... 82%  125M 1s
216050K .......... .......... .......... .......... .......... 82% 76.9M 1s
216100K .......... .......... .......... .......... .......... 82% 84.3M 1s
216150K .......... .......... .......... .......... .......... 82% 86.0M 1s
216200K .......... .......... .......... .......... .......... 82%  296M 1s
216250K .......... .......... .......... .......... .......... 82% 66.2M 1s
216300K .......... .......... .......... .......... .......... 82%  126M 1s
216350K .......... .......... .......... .......... .......... 82% 94.1M 1s
216400K .......... .......... .......... .......... .......... 82% 77.0M 1s
216450K .......... .......... .......... .......... .......... 82%  110M 1s
216500K .......... .......... .......... .......... .......... 82%  147M 1s
216550K .......... .......... .......... .......... .......... 82%  118M 1s
216600K .......... .......... .......... .......... .......... 82% 52.1M 1s
216650K .......... .......... .......... .......... .......... 82%  436M 1s
216700K .......... .......... .......... .......... .......... 82% 72.3M 1s
216750K .......... .......... .......... .......... .......... 82%  184M 1s
216800K .......... .......... .......... .......... .......... 82% 63.0M 1s
216850K .......... .......... .......... .......... .......... 82% 67.8M 1s
216900K .......... .......... .......... .......... .......... 82%  178M 1s
216950K .......... .......... .......... .......... .......... 82% 83.9M 1s
217000K .......... .......... .......... .......... .......... 82%  134M 1s
217050K .......... .......... .......... .......... .......... 82% 93.0M 1s
217100K .......... .......... .......... .......... .......... 82% 93.7M 1s
217150K .......... .......... .......... .......... .......... 82%  115M 1s
217200K .......... .......... .......... .......... .......... 82%  105M 1s
217250K .......... .......... .......... .......... .......... 82%  118M 1s
217300K .......... .......... .......... .......... .......... 82% 83.5M 1s
217350K .......... .......... .......... .......... .......... 82% 55.2M 1s
217400K .......... .......... .......... .......... .......... 82%  465M 1s
217450K .......... .......... .......... .......... .......... 82% 34.1M 1s
217500K .......... .......... .......... .......... .......... 82%  158M 1s
217550K .......... .......... .......... .......... .......... 82%  180M 1s
217600K .......... .......... .......... .......... .......... 83% 43.5M 1s
217650K .......... .......... .......... .......... .......... 83%  146M 1s
217700K .......... .......... .......... .......... .......... 83% 96.7M 1s
217750K .......... .......... .......... .......... .......... 83%  119M 1s
217800K .......... .......... .......... .......... .......... 83%  127M 1s
217850K .......... .......... .......... .......... .......... 83% 93.9M 1s
217900K .......... .......... .......... .......... .......... 83% 99.4M 1s
217950K .......... .......... .......... .......... .......... 83% 93.2M 1s
218000K .......... .......... .......... .......... .......... 83%  113M 1s
218050K .......... .......... .......... .......... .......... 83% 17.4M 1s
218100K .......... .......... .......... .......... .......... 83%  139M 1s
218150K .......... .......... .......... .......... .......... 83%  146M 1s
218200K .......... .......... .......... .......... .......... 83%  171M 1s
218250K .......... .......... .......... .......... .......... 83%  397M 1s
218300K .......... .......... .......... .......... .......... 83%  452M 1s
218350K .......... .......... .......... .......... .......... 83%  261M 1s
218400K .......... .......... .......... .......... .......... 83%  440M 1s
218450K .......... .......... .......... .......... .......... 83%  432M 1s
218500K .......... .......... .......... .......... .......... 83%  133M 1s
218550K .......... .......... .......... .......... .......... 83% 75.8M 1s
218600K .......... .......... .......... .......... .......... 83% 75.7M 1s
218650K .......... .......... .......... .......... .......... 83% 62.9M 1s
218700K .......... .......... .......... .......... .......... 83% 75.1M 1s
218750K .......... .......... .......... .......... .......... 83%  120M 1s
218800K .......... .......... .......... .......... .......... 83% 64.8M 1s
218850K .......... .......... .......... .......... .......... 83% 90.9M 1s
218900K .......... .......... .......... .......... .......... 83% 75.1M 1s
218950K .......... .......... .......... .......... .......... 83% 77.8M 1s
219000K .......... .......... .......... .......... .......... 83% 75.5M 1s
219050K .......... .......... .......... .......... .......... 83% 64.2M 1s
219100K .......... .......... .......... .......... .......... 83% 93.5M 1s
219150K .......... .......... .......... .......... .......... 83% 79.8M 1s
219200K .......... .......... .......... .......... .......... 83% 90.9M 1s
219250K .......... .......... .......... .......... .......... 83% 75.0M 1s
219300K .......... .......... .......... .......... .......... 83% 76.4M 1s
219350K .......... .......... .......... .......... .......... 83% 63.2M 1s
219400K .......... .......... .......... .......... .......... 83% 54.8M 1s
219450K .......... .......... .......... .......... .......... 83% 83.8M 1s
219500K .......... .......... .......... .......... .......... 83% 81.0M 1s
219550K .......... .......... .......... .......... .......... 83% 71.2M 1s
219600K .......... .......... .......... .......... .......... 83% 66.3M 1s
219650K .......... .......... .......... .......... .......... 83%  117M 1s
219700K .......... .......... .......... .......... .......... 83% 63.4M 1s
219750K .......... .......... .......... .......... .......... 83% 78.1M 1s
219800K .......... .......... .......... .......... .......... 83% 95.0M 1s
219850K .......... .......... .......... .......... .......... 83% 73.8M 1s
219900K .......... .......... .......... .......... .......... 83% 93.7M 1s
219950K .......... .......... .......... .......... .......... 83% 64.4M 1s
220000K .......... .......... .......... .......... .......... 83% 75.1M 1s
220050K .......... .......... .......... .......... .......... 83% 94.8M 1s
220100K .......... .......... .......... .......... .......... 83% 66.2M 1s
220150K .......... .......... .......... .......... .......... 83% 89.6M 1s
220200K .......... .......... .......... .......... .......... 83% 57.3M 1s
220250K .......... .......... .......... .......... .......... 84% 49.9M 1s
220300K .......... .......... .......... .......... .......... 84% 96.1M 1s
220350K .......... .......... .......... .......... .......... 84% 53.5M 1s
220400K .......... .......... .......... .......... .......... 84%  121M 1s
220450K .......... .......... .......... .......... .......... 84% 65.4M 1s
220500K .......... .......... .......... .......... .......... 84%  120M 1s
220550K .......... .......... .......... .......... .......... 84% 75.2M 1s
220600K .......... .......... .......... .......... .......... 84% 64.9M 1s
220650K .......... .......... .......... .......... .......... 84% 95.4M 1s
220700K .......... .......... .......... .......... .......... 84% 74.1M 1s
220750K .......... .......... .......... .......... .......... 84% 75.1M 1s
220800K .......... .......... .......... .......... .......... 84% 97.9M 1s
220850K .......... .......... .......... .......... .......... 84% 62.2M 1s
220900K .......... .......... .......... .......... .......... 84% 73.3M 1s
220950K .......... .......... .......... .......... .......... 84% 97.1M 1s
221000K .......... .......... .......... .......... .......... 84% 76.2M 1s
221050K .......... .......... .......... .......... .......... 84% 75.1M 1s
221100K .......... .......... .......... .......... .......... 84% 73.6M 1s
221150K .......... .......... .......... .......... .......... 84% 6.14M 1s
221200K .......... .......... .......... .......... .......... 84%  388M 1s
221250K .......... .......... .......... .......... .......... 84% 43.2M 1s
221300K .......... .......... .......... .......... .......... 84%  135M 1s
221350K .......... .......... .......... .......... .......... 84% 93.5M 1s
221400K .......... .......... .......... .......... .......... 84% 98.4M 1s
221450K .......... .......... .......... .......... .......... 84% 61.6M 1s
221500K .......... .......... .......... .......... .......... 84%  112M 1s
221550K .......... .......... .......... .......... .......... 84%  474M 1s
221600K .......... .......... .......... .......... .......... 84% 76.3M 1s
221650K .......... .......... .......... .......... .......... 84% 98.6M 1s
221700K .......... .......... .......... .......... .......... 84%  121M 1s
221750K .......... .......... .......... .......... .......... 84%  117M 1s
221800K .......... .......... .......... .......... .......... 84%  134M 1s
221850K .......... .......... .......... .......... .......... 84% 71.5M 1s
221900K .......... .......... .......... .......... .......... 84%  135M 1s
221950K .......... .......... .......... .......... .......... 84% 87.2M 1s
222000K .......... .......... .......... .......... .......... 84% 96.1M 1s
222050K .......... .......... .......... .......... .......... 84%  115M 1s
222100K .......... .......... .......... .......... .......... 84%  105M 1s
222150K .......... .......... .......... .......... .......... 84% 74.4M 1s
222200K .......... .......... .......... .......... .......... 84%  119M 1s
222250K .......... .......... .......... .......... .......... 84% 96.3M 1s
222300K .......... .......... .......... .......... .......... 84%  119M 1s
222350K .......... .......... .......... .......... .......... 84% 93.9M 1s
222400K .......... .......... .......... .......... .......... 84%  113M 1s
222450K .......... .......... .......... .......... .......... 84% 82.2M 1s
222500K .......... .......... .......... .......... .......... 84%  115M 1s
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222600K .......... .......... .......... .......... .......... 84%  193M 1s
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222700K .......... .......... .......... .......... .......... 84% 98.2M 1s
222750K .......... .......... .......... .......... .......... 84%  126M 1s
222800K .......... .......... .......... .......... .......... 84% 89.4M 1s
222850K .......... .......... .......... .......... .......... 85%  122M 1s
222900K .......... .......... .......... .......... .......... 85% 77.6M 1s
222950K .......... .......... .......... .......... .......... 85% 64.6M 1s
223000K .......... .......... .......... .......... .......... 85% 93.9M 1s
223050K .......... .......... .......... .......... .......... 85%  178M 1s
223100K .......... .......... .......... .......... .......... 85% 78.5M 1s
223150K .......... .......... .......... .......... .......... 85%  119M 1s
223200K .......... .......... .......... .......... .......... 85% 94.6M 1s
223250K .......... .......... .......... .......... .......... 85% 99.2M 1s
223300K .......... .......... .......... .......... .......... 85%  119M 1s
223350K .......... .......... .......... .......... .......... 85% 90.9M 1s
223400K .......... .......... .......... .......... .......... 85% 97.5M 1s
223450K .......... .......... .......... .......... .......... 85% 91.8M 0s
223500K .......... .......... .......... .......... .......... 85%  104M 0s
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223600K .......... .......... .......... .......... .......... 85% 81.9M 0s
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223700K .......... .......... .......... .......... .......... 85% 74.8M 0s
223750K .......... .......... .......... .......... .......... 85%  138M 0s
223800K .......... .......... .......... .......... .......... 85%  120M 0s
223850K .......... .......... .......... .......... .......... 85% 94.6M 0s
223900K .......... .......... .......... .......... .......... 85% 86.9M 0s
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224000K .......... .......... .......... .......... .......... 85%  122M 0s
224050K .......... .......... .......... .......... .......... 85% 97.3M 0s
224100K .......... .......... .......... .......... .......... 85% 69.0M 0s
224150K .......... .......... .......... .......... .......... 85%  225M 0s
224200K .......... .......... .......... .......... .......... 85% 94.8M 0s
224250K .......... .......... .......... .......... .......... 85% 98.4M 0s
224300K .......... .......... .......... .......... .......... 85%  103M 0s
224350K .......... .......... .......... .......... .......... 85% 50.8M 0s
224400K .......... .......... .......... .......... .......... 85%  126M 0s
224450K .......... .......... .......... .......... .......... 85% 93.2M 0s
224500K .......... .......... .......... .......... .......... 85%  123M 0s
224550K .......... .......... .......... .......... .......... 85% 97.9M 0s
224600K .......... .......... .......... .......... .......... 85%  109M 0s
224650K .......... .......... .......... .......... .......... 85%  101M 0s
224700K .......... .......... .......... .......... .......... 85% 65.2M 0s
224750K .......... .......... .......... .......... .......... 85%  121M 0s
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224850K .......... .......... .......... .......... .......... 85% 93.9M 0s
224900K .......... .......... .......... .......... .......... 85% 75.1M 0s
224950K .......... .......... .......... .......... .......... 85%  115M 0s
225000K .......... .......... .......... .......... .......... 85% 80.3M 0s
225050K .......... .......... .......... .......... .......... 85%  119M 0s
225100K .......... .......... .......... .......... .......... 85% 93.7M 0s
225150K .......... .......... .......... .......... .......... 85%  101M 0s
225200K .......... .......... .......... .......... .......... 85% 93.7M 0s
225250K .......... .......... .......... .......... .......... 85%  118M 0s
225300K .......... .......... .......... .......... .......... 85%  128M 0s
225350K .......... .......... .......... .......... .......... 85% 27.8M 0s
225400K .......... .......... .......... .......... .......... 85%  163M 0s
225450K .......... .......... .......... .......... .......... 86% 32.1M 0s
225500K .......... .......... .......... .......... .......... 86%  444M 0s
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225600K .......... .......... .......... .......... .......... 86%  440M 0s
225650K .......... .......... .......... .......... .......... 86% 80.6M 0s
225700K .......... .......... .......... .......... .......... 86% 74.9M 0s
225750K .......... .......... .......... .......... .......... 86% 95.0M 0s
225800K .......... .......... .......... .......... .......... 86% 90.8M 0s
225850K .......... .......... .......... .......... .......... 86% 80.0M 0s
225900K .......... .......... .......... .......... .......... 86% 75.2M 0s
225950K .......... .......... .......... .......... .......... 86% 74.3M 0s
226000K .......... .......... .......... .......... .......... 86% 77.8M 0s
226050K .......... .......... .......... .......... .......... 86%  124M 0s
226100K .......... .......... .......... .......... .......... 86% 63.3M 0s
226150K .......... .......... .......... .......... .......... 86%  127M 0s
226200K .......... .......... .......... .......... .......... 86% 76.2M 0s
226250K .......... .......... .......... .......... .......... 86%  119M 0s
226300K .......... .......... .......... .......... .......... 86% 97.3M 0s
226350K .......... .......... .......... .......... .......... 86% 93.4M 0s
226400K .......... .......... .......... .......... .......... 86% 75.6M 0s
226450K .......... .......... .......... .......... .......... 86% 76.9M 0s
226500K .......... .......... .......... .......... .......... 86%  114M 0s
226550K .......... .......... .......... .......... .......... 86% 93.5M 0s
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226650K .......... .......... .......... .......... .......... 86% 56.7M 0s
226700K .......... .......... .......... .......... .......... 86%  115M 0s
226750K .......... .......... .......... .......... .......... 86% 64.2M 0s
226800K .......... .......... .......... .......... .......... 86%  159M 0s
226850K .......... .......... .......... .......... .......... 86% 67.7M 0s
226900K .......... .......... .......... .......... .......... 86% 89.3M 0s
226950K .......... .......... .......... .......... .......... 86% 69.7M 0s
227000K .......... .......... .......... .......... .......... 86% 94.3M 0s
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227100K .......... .......... .......... .......... .......... 86% 68.8M 0s
227150K .......... .......... .......... .......... .......... 86%  102M 0s
227200K .......... .......... .......... .......... .......... 86% 74.9M 0s
227250K .......... .......... .......... .......... .......... 86% 97.9M 0s
227300K .......... .......... .......... .......... .......... 86% 90.3M 0s
227350K .......... .......... .......... .......... .......... 86% 63.6M 0s
227400K .......... .......... .......... .......... .......... 86% 93.9M 0s
227450K .......... .......... .......... .......... .......... 86% 93.4M 0s
227500K .......... .......... .......... .......... .......... 86% 94.6M 0s
227550K .......... .......... .......... .......... .......... 86% 71.7M 0s
227600K .......... .......... .......... .......... .......... 86% 80.6M 0s
227650K .......... .......... .......... .......... .......... 86% 89.1M 0s
227700K .......... .......... .......... .......... .......... 86% 79.1M 0s
227750K .......... .......... .......... .......... .......... 86%  120M 0s
227800K .......... .......... .......... .......... .......... 86% 95.9M 0s
227850K .......... .......... .......... .......... .......... 86% 94.8M 0s
227900K .......... .......... .......... .......... .......... 86% 74.5M 0s
227950K .......... .......... .......... .......... .......... 86%  127M 0s
228000K .......... .......... .......... .......... .......... 86% 76.1M 0s
228050K .......... .......... .......... .......... .......... 86% 95.2M 0s
228100K .......... .......... .......... .......... .......... 87% 68.6M 0s
228150K .......... .......... .......... .......... .......... 87% 72.0M 0s
228200K .......... .......... .......... .......... .......... 87% 75.4M 0s
228250K .......... .......... .......... .......... .......... 87%  108M 0s
228300K .......... .......... .......... .......... .......... 87% 57.3M 0s
228350K .......... .......... .......... .......... .......... 87% 97.7M 0s
228400K .......... .......... .......... .......... .......... 87% 83.8M 0s
228450K .......... .......... .......... .......... .......... 87% 82.6M 0s
228500K .......... .......... .......... .......... .......... 87% 81.1M 0s
228550K .......... .......... .......... .......... .......... 87% 57.6M 0s
228600K .......... .......... .......... .......... .......... 87% 57.7M 0s
228650K .......... .......... .......... .......... .......... 87%  112M 0s
228700K .......... .......... .......... .......... .......... 87% 29.5M 0s
228750K .......... .......... .......... .......... .......... 87%  174M 0s
228800K .......... .......... .......... .......... .......... 87% 12.5M 0s
228850K .......... .......... .......... .......... .......... 87%  222M 0s
228900K .......... .......... .......... .......... .......... 87%  158M 0s
228950K .......... .......... .......... .......... .......... 87% 13.2M 0s
229000K .......... .......... .......... .......... .......... 87%  509M 0s
229050K .......... .......... .......... .......... .......... 87%  531M 0s
229100K .......... .......... .......... .......... .......... 87% 39.4M 0s
229150K .......... .......... .......... .......... .......... 87%  122M 0s
229200K .......... .......... .......... .......... .......... 87% 85.7M 0s
229250K .......... .......... .......... .......... .......... 87%  100M 0s
229300K .......... .......... .......... .......... .......... 87%  101M 0s
229350K .......... .......... .......... .......... .......... 87% 95.6M 0s
229400K .......... .......... .......... .......... .......... 87% 79.9M 0s
229450K .......... .......... .......... .......... .......... 87% 98.0M 0s
229500K .......... .......... .......... .......... .......... 87% 24.2M 0s
229550K .......... .......... .......... .......... .......... 87%  189M 0s
229600K .......... .......... .......... .......... .......... 87%  167M 0s
229650K .......... .......... .......... .......... .......... 87% 11.9M 0s
229700K .......... .......... .......... .......... .......... 87% 29.6M 0s
229750K .......... .......... .......... .......... .......... 87% 36.8M 0s
229800K .......... .......... .......... .......... .......... 87%  309M 0s
229850K .......... .......... .......... .......... .......... 87% 74.3M 0s
229900K .......... .......... .......... .......... .......... 87%  118M 0s
229950K .......... .......... .......... .......... .......... 87%  112M 0s
230000K .......... .......... .......... .......... .......... 87%  123M 0s
230050K .......... .......... .......... .......... .......... 87%  105M 0s
230100K .......... .......... .......... .......... .......... 87%  104M 0s
230150K .......... .......... .......... .......... .......... 87% 81.4M 0s
230200K .......... .......... .......... .......... .......... 87% 88.3M 0s
230250K .......... .......... .......... .......... .......... 87%  107M 0s
230300K .......... .......... .......... .......... .......... 87%  117M 0s
230350K .......... .......... .......... .......... .......... 87% 99.4M 0s
230400K .......... .......... .......... .......... .......... 87%  138M 0s
230450K .......... .......... .......... .......... .......... 87% 60.9M 0s
230500K .......... .......... .......... .......... .......... 87%  133M 0s
230550K .......... .......... .......... .......... .......... 87%  126M 0s
230600K .......... .......... .......... .......... .......... 87% 79.0M 0s
230650K .......... .......... .......... .......... .......... 87%  124M 0s
230700K .......... .......... .......... .......... .......... 88% 91.4M 0s
230750K .......... .......... .......... .......... .......... 88%  120M 0s
230800K .......... .......... .......... .......... .......... 88% 93.0M 0s
230850K .......... .......... .......... .......... .......... 88% 45.0M 0s
230900K .......... .......... .......... .......... .......... 88%  182M 0s
230950K .......... .......... .......... .......... .......... 88% 14.7M 0s
231000K .......... .......... .......... .......... .......... 88%  341M 0s
231050K .......... .......... .......... .......... .......... 88%  514M 0s
231100K .......... .......... .......... .......... .......... 88% 34.9M 0s
231150K .......... .......... .......... .......... .......... 88%  493M 0s
231200K .......... .......... .......... .......... .......... 88% 77.5M 0s
231250K .......... .......... .......... .......... .......... 88% 98.0M 0s
231300K .......... .......... .......... .......... .......... 88%  104M 0s
231350K .......... .......... .......... .......... .......... 88% 93.7M 0s
231400K .......... .......... .......... .......... .......... 88% 57.4M 0s
231450K .......... .......... .......... .......... .......... 88% 72.1M 0s
231500K .......... .......... .......... .......... .......... 88%  173M 0s
231550K .......... .......... .......... .......... .......... 88% 66.4M 0s
231600K .......... .......... .......... .......... .......... 88%  102M 0s
231650K .......... .......... .......... .......... .......... 88% 87.2M 0s
231700K .......... .......... .......... .......... .......... 88%  137M 0s
231750K .......... .......... .......... .......... .......... 88% 97.5M 0s
231800K .......... .......... .......... .......... .......... 88%  103M 0s
231850K .......... .......... .......... .......... .......... 88% 84.2M 0s
231900K .......... .......... .......... .......... .......... 88%  108M 0s
231950K .......... .......... .......... .......... .......... 88%  102M 0s
232000K .......... .......... .......... .......... .......... 88%  113M 0s
232050K .......... .......... .......... .......... .......... 88% 51.8M 0s
232100K .......... .......... .......... .......... .......... 88%  163M 0s
232150K .......... .......... .......... .......... .......... 88%  195M 0s
232200K .......... .......... .......... .......... .......... 88% 23.1M 0s
232250K .......... .......... .......... .......... .......... 88%  189M 0s
232300K .......... .......... .......... .......... .......... 88% 31.1M 0s
232350K .......... .......... .......... .......... .......... 88%  210M 0s
232400K .......... .......... .......... .......... .......... 88% 56.7M 0s
232450K .......... .......... .......... .......... .......... 88% 40.0M 0s
232500K .......... .......... .......... .......... .......... 88%  114M 0s
232550K .......... .......... .......... .......... .......... 88%  208M 0s
232600K .......... .......... .......... .......... .......... 88% 59.1M 0s
232650K .......... .......... .......... .......... .......... 88% 31.8M 0s
232700K .......... .......... .......... .......... .......... 88%  407M 0s
232750K .......... .......... .......... .......... .......... 88%  261M 0s
232800K .......... .......... .......... .......... .......... 88% 44.9M 0s
232850K .......... .......... .......... .......... .......... 88% 70.3M 0s
232900K .......... .......... .......... .......... .......... 88%  428M 0s
232950K .......... .......... .......... .......... .......... 88% 75.4M 0s
233000K .......... .......... .......... .......... .......... 88%  128M 0s
233050K .......... .......... .......... .......... .......... 88% 79.0M 0s
233100K .......... .......... .......... .......... .......... 88%  102M 0s
233150K .......... .......... .......... .......... .......... 88%  132M 0s
233200K .......... .......... .......... .......... .......... 88%  103M 0s
233250K .......... .......... .......... .......... .......... 88% 82.1M 0s
233300K .......... .......... .......... .......... .......... 88%  146M 0s
233350K .......... .......... .......... .......... .......... 89% 26.2M 0s
233400K .......... .......... .......... .......... .......... 89%  187M 0s
233450K .......... .......... .......... .......... .......... 89% 18.1M 0s
233500K .......... .......... .......... .......... .......... 89%  330M 0s
233550K .......... .......... .......... .......... .......... 89%  474M 0s
233600K .......... .......... .......... .......... .......... 89% 22.5M 0s
233650K .......... .......... .......... .......... .......... 89% 36.9M 0s
233700K .......... .......... .......... .......... .......... 89%  432M 0s
233750K .......... .......... .......... .......... .......... 89% 42.6M 0s
233800K .......... .......... .......... .......... .......... 89%  186M 0s
233850K .......... .......... .......... .......... .......... 89%  108M 0s
233900K .......... .......... .......... .......... .......... 89% 74.1M 0s
233950K .......... .......... .......... .......... .......... 89%  100M 0s
234000K .......... .......... .......... .......... .......... 89%  136M 0s
234050K .......... .......... .......... .......... .......... 89% 83.8M 0s
234100K .......... .......... .......... .......... .......... 89%  122M 0s
234150K .......... .......... .......... .......... .......... 89% 71.1M 0s
234200K .......... .......... .......... .......... .......... 89%  103M 0s
234250K .......... .......... .......... .......... .......... 89% 91.6M 0s
234300K .......... .......... .......... .......... .......... 89%  120M 0s
234350K .......... .......... .......... .......... .......... 89% 95.7M 0s
234400K .......... .......... .......... .......... .......... 89%  103M 0s
234450K .......... .......... .......... .......... .......... 89% 96.5M 0s
234500K .......... .......... .......... .......... .......... 89% 32.6M 0s
234550K .......... .......... .......... .......... .......... 89%  166M 0s
234600K .......... .......... .......... .......... .......... 89%  156M 0s
234650K .......... .......... .......... .......... .......... 89% 18.5M 0s
234700K .......... .......... .......... .......... .......... 89%  417M 0s
234750K .......... .......... .......... .......... .......... 89%  514M 0s
234800K .......... .......... .......... .......... .......... 89% 25.2M 0s
234850K .......... .......... .......... .......... .......... 89%  156M 0s
234900K .......... .......... .......... .......... .......... 89% 29.3M 0s
234950K .......... .......... .......... .......... .......... 89%  319M 0s
235000K .......... .......... .......... .......... .......... 89%  531M 0s
235050K .......... .......... .......... .......... .......... 89% 54.1M 0s
235100K .......... .......... .......... .......... .......... 89% 97.9M 0s
235150K .......... .......... .......... .......... .......... 89% 98.8M 0s
235200K .......... .......... .......... .......... .......... 89%  106M 0s
235250K .......... .......... .......... .......... .......... 89%  138M 0s
235300K .......... .......... .......... .......... .......... 89%  119M 0s
235350K .......... .......... .......... .......... .......... 89% 95.2M 0s
235400K .......... .......... .......... .......... .......... 89% 93.0M 0s
235450K .......... .......... .......... .......... .......... 89% 71.0M 0s
235500K .......... .......... .......... .......... .......... 89%  110M 0s
235550K .......... .......... .......... .......... .......... 89%  101M 0s
235600K .......... .......... .......... .......... .......... 89%  100M 0s
235650K .......... .......... .......... .......... .......... 89%  105M 0s
235700K .......... .......... .......... .......... .......... 89%  105M 0s
235750K .......... .......... .......... .......... .......... 89% 66.3M 0s
235800K .......... .......... .......... .......... .......... 89% 36.9M 0s
235850K .......... .......... .......... .......... .......... 89%  461M 0s
235900K .......... .......... .......... .......... .......... 89% 17.9M 0s
235950K .......... .......... .......... .......... .......... 90%  129M 0s
236000K .......... .......... .......... .......... .......... 90%  187M 0s
236050K .......... .......... .......... .......... .......... 90% 40.9M 0s
236100K .......... .......... .......... .......... .......... 90% 63.8M 0s
236150K .......... .......... .......... .......... .......... 90%  178M 0s
236200K .......... .......... .......... .......... .......... 90%  134M 0s
236250K .......... .......... .......... .......... .......... 90% 42.5M 0s
236300K .......... .......... .......... .......... .......... 90%  142M 0s
236350K .......... .......... .......... .......... .......... 90% 95.2M 0s
236400K .......... .......... .......... .......... .......... 90%  110M 0s
236450K .......... .......... .......... .......... .......... 90% 89.6M 0s
236500K .......... .......... .......... .......... .......... 90%  175M 0s
236550K .......... .......... .......... .......... .......... 90%  103M 0s
236600K .......... .......... .......... .......... .......... 90% 85.2M 0s
236650K .......... .......... .......... .......... .......... 90%  112M 0s
236700K .......... .......... .......... .......... .......... 90% 65.7M 0s
236750K .......... .......... .......... .......... .......... 90%  125M 0s
236800K .......... .......... .......... .......... .......... 90%  114M 0s
236850K .......... .......... .......... .......... .......... 90% 92.1M 0s
236900K .......... .......... .......... .......... .......... 90% 93.0M 0s
236950K .......... .......... .......... .......... .......... 90%  152M 0s
237000K .......... .......... .......... .......... .......... 90% 63.0M 0s
237050K .......... .......... .......... .......... .......... 90%  150M 0s
237100K .......... .......... .......... .......... .......... 90% 65.7M 0s
237150K .......... .......... .......... .......... .......... 90% 68.8M 0s
237200K .......... .......... .......... .......... .......... 90%  135M 0s
237250K .......... .......... .......... .......... .......... 90% 89.8M 0s
237300K .......... .......... .......... .......... .......... 90% 57.4M 0s
237350K .......... .......... .......... .......... .......... 90% 95.6M 0s
237400K .......... .......... .......... .......... .......... 90%  125M 0s
237450K .......... .......... .......... .......... .......... 90% 92.0M 0s
237500K .......... .......... .......... .......... .......... 90% 97.5M 0s
237550K .......... .......... .......... .......... .......... 90% 52.3M 0s
237600K .......... .......... .......... .......... .......... 90%  332M 0s
237650K .......... .......... .......... .......... .......... 90%  140M 0s
237700K .......... .......... .......... .......... .......... 90% 73.4M 0s
237750K .......... .......... .......... .......... .......... 90% 97.7M 0s
237800K .......... .......... .......... .......... .......... 90%  123M 0s
237850K .......... .......... .......... .......... .......... 90% 92.0M 0s
237900K .......... .......... .......... .......... .......... 90%  124M 0s
237950K .......... .......... .......... .......... .......... 90% 74.3M 0s
238000K .......... .......... .......... .......... .......... 90% 32.1M 0s
238050K .......... .......... .......... .......... .......... 90%  152M 0s
238100K .......... .......... .......... .......... .......... 90%  397M 0s
238150K .......... .......... .......... .......... .......... 90% 89.8M 0s
238200K .......... .......... .......... .......... .......... 90% 92.8M 0s
238250K .......... .......... .......... .......... .......... 90%  493M 0s
238300K .......... .......... .......... .......... .......... 90%  448M 0s
238350K .......... .......... .......... .......... .......... 90% 63.0M 0s
238400K .......... .......... .......... .......... .......... 90% 73.6M 0s
238450K .......... .......... .......... .......... .......... 90% 79.0M 0s
238500K .......... .......... .......... .......... .......... 90% 94.4M 0s
238550K .......... .......... .......... .......... .......... 90% 92.5M 0s
238600K .......... .......... .......... .......... .......... 91% 74.0M 0s
238650K .......... .......... .......... .......... .......... 91% 76.8M 0s
238700K .......... .......... .......... .......... .......... 91% 53.7M 0s
238750K .......... .......... .......... .......... .......... 91%  134M 0s
238800K .......... .......... .......... .......... .......... 91% 63.1M 0s
238850K .......... .......... .......... .......... .......... 91% 75.7M 0s
238900K .......... .......... .......... .......... .......... 91% 88.5M 0s
238950K .......... .......... .......... .......... .......... 91% 56.3M 0s
239000K .......... .......... .......... .......... .......... 91%  114M 0s
239050K .......... .......... .......... .......... .......... 91% 66.4M 0s
239100K .......... .......... .......... .......... .......... 91% 63.0M 0s
239150K .......... .......... .......... .......... .......... 91%  120M 0s
239200K .......... .......... .......... .......... .......... 91% 61.6M 0s
239250K .......... .......... .......... .......... .......... 91% 78.0M 0s
239300K .......... .......... .......... .......... .......... 91% 94.4M 0s
239350K .......... .......... .......... .......... .......... 91% 74.0M 0s
239400K .......... .......... .......... .......... .......... 91% 72.3M 0s
239450K .......... .......... .......... .......... .......... 91% 57.0M 0s
239500K .......... .......... .......... .......... .......... 91% 93.2M 0s
239550K .......... .......... .......... .......... .......... 91% 71.7M 0s
239600K .......... .......... .......... .......... .......... 91% 76.8M 0s
239650K .......... .......... .......... .......... .......... 91% 76.8M 0s
239700K .......... .......... .......... .......... .......... 91% 77.0M 0s
239750K .......... .......... .......... .......... .......... 91% 92.5M 0s
239800K .......... .......... .......... .......... .......... 91% 64.8M 0s
239850K .......... .......... .......... .......... .......... 91% 94.3M 0s
239900K .......... .......... .......... .......... .......... 91% 63.6M 0s
239950K .......... .......... .......... .......... .......... 91% 75.7M 0s
240000K .......... .......... .......... .......... .......... 91% 75.5M 0s
240050K .......... .......... .......... .......... .......... 91% 74.8M 0s
240100K .......... .......... .......... .......... .......... 91% 62.7M 0s
240150K .......... .......... .......... .......... .......... 91%  118M 0s
240200K .......... .......... .......... .......... .......... 91% 55.6M 0s
240250K .......... .......... .......... .......... .......... 91% 63.1M 0s
240300K .......... .......... .......... .......... .......... 91% 76.7M 0s
240350K .......... .......... .......... .......... .......... 91% 62.8M 0s
240400K .......... .......... .......... .......... .......... 91% 92.3M 0s
240450K .......... .......... .......... .......... .......... 91% 62.8M 0s
240500K .......... .......... .......... .......... .......... 91% 76.4M 0s
240550K .......... .......... .......... .......... .......... 91% 76.4M 0s
240600K .......... .......... .......... .......... .......... 91% 73.9M 0s
240650K .......... .......... .......... .......... .......... 91% 82.9M 0s
240700K .......... .......... .......... .......... .......... 91% 57.6M 0s
240750K .......... .......... .......... .......... .......... 91% 64.8M 0s
240800K .......... .......... .......... .......... .......... 91%  125M 0s
240850K .......... .......... .......... .......... .......... 91% 62.8M 0s
240900K .......... .......... .......... .......... .......... 91% 76.2M 0s
240950K .......... .......... .......... .......... .......... 91% 73.0M 0s
241000K .......... .......... .......... .......... .......... 91% 93.5M 0s
241050K .......... .......... .......... .......... .......... 91% 93.2M 0s
241100K .......... .......... .......... .......... .......... 91% 98.0M 0s
241150K .......... .......... .......... .......... .......... 91% 94.4M 0s
241200K .......... .......... .......... .......... .......... 92% 95.7M 0s
241250K .......... .......... .......... .......... .......... 92%  119M 0s
241300K .......... .......... .......... .......... .......... 92% 22.1M 0s
241350K .......... .......... .......... .......... .......... 92%  113M 0s
241400K .......... .......... .......... .......... .......... 92%  160M 0s
241450K .......... .......... .......... .......... .......... 92%  139M 0s
241500K .......... .......... .......... .......... .......... 92%  274M 0s
241550K .......... .......... .......... .......... .......... 92%  456M 0s
241600K .......... .......... .......... .......... .......... 92% 31.4M 0s
241650K .......... .......... .......... .......... .......... 92%  448M 0s
241700K .......... .......... .......... .......... .......... 92%  356M 0s
241750K .......... .......... .......... .......... .......... 92%  444M 0s
241800K .......... .......... .......... .......... .......... 92%  452M 0s
241850K .......... .......... .......... .......... .......... 92%  224M 0s
241900K .......... .......... .......... .......... .......... 92% 94.3M 0s
241950K .......... .......... .......... .......... .......... 92% 53.4M 0s
242000K .......... .......... .......... .......... .......... 92% 64.2M 0s
242050K .......... .......... .......... .......... .......... 92% 93.5M 0s
242100K .......... .......... .......... .......... .......... 92% 63.4M 0s
242150K .......... .......... .......... .......... .......... 92% 74.7M 0s
242200K .......... .......... .......... .......... .......... 92% 54.6M 0s
242250K .......... .......... .......... .......... .......... 92%  120M 0s
242300K .......... .......... .......... .......... .......... 92% 53.2M 0s
242350K .......... .......... .......... .......... .......... 92% 78.8M 0s
242400K .......... .......... .......... .......... .......... 92% 66.6M 0s
242450K .......... .......... .......... .......... .......... 92% 70.2M 0s
242500K .......... .......... .......... .......... .......... 92% 27.2M 0s
242550K .......... .......... .......... .......... .......... 92% 47.3M 0s
242600K .......... .......... .......... .......... .......... 92% 94.3M 0s
242650K .......... .......... .......... .......... .......... 92% 73.0M 0s
242700K .......... .......... .......... .......... .......... 92% 64.5M 0s
242750K .......... .......... .......... .......... .......... 92% 92.8M 0s
242800K .......... .......... .......... .......... .......... 92% 64.5M 0s
242850K .......... .......... .......... .......... .......... 92% 62.4M 0s
242900K .......... .......... .......... .......... .......... 92% 65.0M 0s
242950K .......... .......... .......... .......... .......... 92% 94.3M 0s
243000K .......... .......... .......... .......... .......... 92% 71.3M 0s
243050K .......... .......... .......... .......... .......... 92% 63.8M 0s
243100K .......... .......... .......... .......... .......... 92% 41.3M 0s
243150K .......... .......... .......... .......... .......... 92% 44.5M 0s
243200K .......... .......... .......... .......... .......... 92% 54.1M 0s
243250K .......... .......... .......... .......... .......... 92%  126M 0s
243300K .......... .......... .......... .......... .......... 92% 61.0M 0s
243350K .......... .......... .......... .......... .......... 92% 61.0M 0s
243400K .......... .......... .......... .......... .......... 92% 59.3M 0s
243450K .......... .......... .......... .......... .......... 92% 40.2M 0s
243500K .......... .......... .......... .......... .......... 92%  157M 0s
243550K .......... .......... .......... .......... .......... 92% 66.0M 0s
243600K .......... .......... .......... .......... .......... 92% 63.3M 0s
243650K .......... .......... .......... .......... .......... 92% 72.2M 0s
243700K .......... .......... .......... .......... .......... 92% 78.3M 0s
243750K .......... .......... .......... .......... .......... 92% 74.5M 0s
243800K .......... .......... .......... .......... .......... 92% 65.3M 0s
243850K .......... .......... .......... .......... .......... 93% 70.7M 0s
243900K .......... .......... .......... .......... .......... 93% 57.0M 0s
243950K .......... .......... .......... .......... .......... 93%  113M 0s
244000K .......... .......... .......... .......... .......... 93% 55.6M 0s
244050K .......... .......... .......... .......... .......... 93% 78.0M 0s
244100K .......... .......... .......... .......... .......... 93% 62.2M 0s
244150K .......... .......... .......... .......... .......... 93% 63.5M 0s
244200K .......... .......... .......... .......... .......... 93% 85.2M 0s
244250K .......... .......... .......... .......... .......... 93% 66.4M 0s
244300K .......... .......... .......... .......... .......... 93%  128M 0s
244350K .......... .......... .......... .......... .......... 93% 94.3M 0s
244400K .......... .......... .......... .......... .......... 93%  110M 0s
244450K .......... .......... .......... .......... .......... 93% 81.4M 0s
244500K .......... .......... .......... .......... .......... 93% 98.4M 0s
244550K .......... .......... .......... .......... .......... 93%  156M 0s
244600K .......... .......... .......... .......... .......... 93% 77.4M 0s
244650K .......... .......... .......... .......... .......... 93% 28.5M 0s
244700K .......... .......... .......... .......... .......... 93%  313M 0s
244750K .......... .......... .......... .......... .......... 93%  119M 0s
244800K .......... .......... .......... .......... .......... 93%  367M 0s
244850K .......... .......... .......... .......... .......... 93%  421M 0s
244900K .......... .......... .......... .......... .......... 93% 33.7M 0s
244950K .......... .......... .......... .......... .......... 93%  229M 0s
245000K .......... .......... .......... .......... .......... 93%  124M 0s
245050K .......... .......... .......... .......... .......... 93%  165M 0s
245100K .......... .......... .......... .......... .......... 93%  140M 0s
245150K .......... .......... .......... .......... .......... 93%  167M 0s
245200K .......... .......... .......... .......... .......... 93%  111M 0s
245250K .......... .......... .......... .......... .......... 93% 90.3M 0s
245300K .......... .......... .......... .......... .......... 93% 95.9M 0s
245350K .......... .......... .......... .......... .......... 93% 78.0M 0s
245400K .......... .......... .......... .......... .......... 93% 91.1M 0s
245450K .......... .......... .......... .......... .......... 93% 75.0M 0s
245500K .......... .......... .......... .......... .......... 93% 76.3M 0s
245550K .......... .......... .......... .......... .......... 93% 76.9M 0s
245600K .......... .......... .......... .......... .......... 93% 93.7M 0s
245650K .......... .......... .......... .......... .......... 93% 75.7M 0s
245700K .......... .......... .......... .......... .......... 93% 72.6M 0s
245750K .......... .......... .......... .......... .......... 93% 78.0M 0s
245800K .......... .......... .......... .......... .......... 93% 75.9M 0s
245850K .......... .......... .......... .......... .......... 93% 92.0M 0s
245900K .......... .......... .......... .......... .......... 93% 92.3M 0s
245950K .......... .......... .......... .......... .......... 93% 64.2M 0s
246000K .......... .......... .......... .......... .......... 93% 75.0M 0s
246050K .......... .......... .......... .......... .......... 93% 87.2M 0s
246100K .......... .......... .......... .......... .......... 93% 97.5M 0s
246150K .......... .......... .......... .......... .......... 93% 75.7M 0s
246200K .......... .......... .......... .......... .......... 93% 64.3M 0s
246250K .......... .......... .......... .......... .......... 93% 72.1M 0s
246300K .......... .......... .......... .......... .......... 93%  143M 0s
246350K .......... .......... .......... .......... .......... 93% 35.3M 0s
246400K .......... .......... .......... .......... .......... 93% 43.8M 0s
246450K .......... .......... .......... .......... .......... 94% 95.9M 0s
246500K .......... .......... .......... .......... .......... 94% 94.6M 0s
246550K .......... .......... .......... .......... .......... 94% 91.3M 0s
246600K .......... .......... .......... .......... .......... 94% 78.8M 0s
246650K .......... .......... .......... .......... .......... 94%  114M 0s
246700K .......... .......... .......... .......... .......... 94% 77.5M 0s
246750K .......... .......... .......... .......... .......... 94% 77.0M 0s
246800K .......... .......... .......... .......... .......... 94% 94.6M 0s
246850K .......... .......... .......... .......... .......... 94% 91.1M 0s
246900K .......... .......... .......... .......... .......... 94% 76.4M 0s
246950K .......... .......... .......... .......... .......... 94% 64.3M 0s
247000K .......... .......... .......... .......... .......... 94%  174M 0s
247050K .......... .......... .......... .......... .......... 94% 76.9M 0s
247100K .......... .......... .......... .......... .......... 94% 89.8M 0s
247150K .......... .......... .......... .......... .......... 94% 62.3M 0s
247200K .......... .......... .......... .......... .......... 94% 78.9M 0s
247250K .......... .......... .......... .......... .......... 94% 77.6M 0s
247300K .......... .......... .......... .......... .......... 94% 82.2M 0s
247350K .......... .......... .......... .......... .......... 94% 84.9M 0s
247400K .......... .......... .......... .......... .......... 94% 75.4M 0s
247450K .......... .......... .......... .......... .......... 94% 58.9M 0s
247500K .......... .......... .......... .......... .......... 94%  130M 0s
247550K .......... .......... .......... .......... .......... 94% 69.4M 0s
247600K .......... .......... .......... .......... .......... 94% 69.2M 0s
247650K .......... .......... .......... .......... .......... 94% 77.4M 0s
247700K .......... .......... .......... .......... .......... 94% 71.1M 0s
247750K .......... .......... .......... .......... .......... 94%  105M 0s
247800K .......... .......... .......... .......... .......... 94% 39.1M 0s
247850K .......... .......... .......... .......... .......... 94% 10.2M 0s
247900K .......... .......... .......... .......... .......... 94%  440M 0s
247950K .......... .......... .......... .......... .......... 94% 19.8M 0s
248000K .......... .......... .......... .......... .......... 94%  309M 0s
248050K .......... .......... .......... .......... .......... 94% 39.6M 0s
248100K .......... .......... .......... .......... .......... 94%  452M 0s
248150K .......... .......... .......... .......... .......... 94%  123M 0s
248200K .......... .......... .......... .......... .......... 94% 79.5M 0s
248250K .......... .......... .......... .......... .......... 94%  141M 0s
248300K .......... .......... .......... .......... .......... 94%  107M 0s
248350K .......... .......... .......... .......... .......... 94% 93.7M 0s
248400K .......... .......... .......... .......... .......... 94% 83.2M 0s
248450K .......... .......... .......... .......... .......... 94%  143M 0s
248500K .......... .......... .......... .......... .......... 94% 20.8M 0s
248550K .......... .......... .......... .......... .......... 94%  164M 0s
248600K .......... .......... .......... .......... .......... 94%  168M 0s
248650K .......... .......... .......... .......... .......... 94% 28.5M 0s
248700K .......... .......... .......... .......... .......... 94%  448M 0s
248750K .......... .......... .......... .......... .......... 94%  474M 0s
248800K .......... .......... .......... .......... .......... 94% 21.4M 0s
248850K .......... .......... .......... .......... .......... 94%  373M 0s
248900K .......... .......... .......... .......... .......... 94%  404M 0s
248950K .......... .......... .......... .......... .......... 94% 27.6M 0s
249000K .......... .......... .......... .......... .......... 94%  503M 0s
249050K .......... .......... .......... .......... .......... 95%  555M 0s
249100K .......... .......... .......... .......... .......... 95% 20.7M 0s
249150K .......... .......... .......... .......... .......... 95%  503M 0s
249200K .......... .......... .......... .......... .......... 95%  465M 0s
249250K .......... .......... .......... .......... .......... 95% 46.2M 0s
249300K .......... .......... .......... .......... .......... 95%  112M 0s
249350K .......... .......... .......... .......... .......... 95%  145M 0s
249400K .......... .......... .......... .......... .......... 95% 78.8M 0s
249450K .......... .......... .......... .......... .......... 95% 94.3M 0s
249500K .......... .......... .......... .......... .......... 95%  118M 0s
249550K .......... .......... .......... .......... .......... 95%  102M 0s
249600K .......... .......... .......... .......... .......... 95% 74.8M 0s
249650K .......... .......... .......... .......... .......... 95%  134M 0s
249700K .......... .......... .......... .......... .......... 95%  139M 0s
249750K .......... .......... .......... .......... .......... 95% 92.5M 0s
249800K .......... .......... .......... .......... .......... 95%  131M 0s
249850K .......... .......... .......... .......... .......... 95% 79.1M 0s
249900K .......... .......... .......... .......... .......... 95% 79.0M 0s
249950K .......... .......... .......... .......... .......... 95%  190M 0s
250000K .......... .......... .......... .......... .......... 95%  145M 0s
250050K .......... .......... .......... .......... .......... 95%  107M 0s
250100K .......... .......... .......... .......... .......... 95% 8.90M 0s
250150K .......... .......... .......... .......... .......... 95%  303M 0s
250200K .......... .......... .......... .......... .......... 95%  414M 0s
250250K .......... .......... .......... .......... .......... 95% 29.9M 0s
250300K .......... .......... .......... .......... .......... 95%  126M 0s
250350K .......... .......... .......... .......... .......... 95%  161M 0s
250400K .......... .......... .......... .......... .......... 95% 43.9M 0s
250450K .......... .......... .......... .......... .......... 95%  107M 0s
250500K .......... .......... .......... .......... .......... 95%  114M 0s
250550K .......... .......... .......... .......... .......... 95%  126M 0s
250600K .......... .......... .......... .......... .......... 95% 53.8M 0s
250650K .......... .......... .......... .......... .......... 95%  174M 0s
250700K .......... .......... .......... .......... .......... 95%  152M 0s
250750K .......... .......... .......... .......... .......... 95% 43.1M 0s
250800K .......... .......... .......... .......... .......... 95%  115M 0s
250850K .......... .......... .......... .......... .......... 95%  105M 0s
250900K .......... .......... .......... .......... .......... 95% 93.7M 0s
250950K .......... .......... .......... .......... .......... 95% 95.2M 0s
251000K .......... .......... .......... .......... .......... 95%  110M 0s
251050K .......... .......... .......... .......... .......... 95% 66.1M 0s
251100K .......... .......... .......... .......... .......... 95%  397M 0s
251150K .......... .......... .......... .......... .......... 95%  106M 0s
251200K .......... .......... .......... .......... .......... 95% 22.8M 0s
251250K .......... .......... .......... .......... .......... 95%  452M 0s
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251350K .......... .......... .......... .......... .......... 95% 39.2M 0s
251400K .......... .......... .......... .......... .......... 95%  181M 0s
251450K .......... .......... .......... .......... .......... 95% 51.0M 0s
251500K .......... .......... .......... .......... .......... 95%  131M 0s
251550K .......... .......... .......... .......... .......... 95%  191M 0s
251600K .......... .......... .......... .......... .......... 95% 16.4M 0s
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251750K .......... .......... .......... .......... .......... 96% 41.6M 0s
251800K .......... .......... .......... .......... .......... 96%  123M 0s
251850K .......... .......... .......... .......... .......... 96% 95.4M 0s
251900K .......... .......... .......... .......... .......... 96%  103M 0s
251950K .......... .......... .......... .......... .......... 96% 80.6M 0s
252000K .......... .......... .......... .......... .......... 96%  163M 0s
252050K .......... .......... .......... .......... .......... 96%  115M 0s
252100K .......... .......... .......... .......... .......... 96% 98.0M 0s
252150K .......... .......... .......... .......... .......... 96%  110M 0s
252200K .......... .......... .......... .......... .......... 96% 89.8M 0s
252250K .......... .......... .......... .......... .......... 96%  142M 0s
252300K .......... .......... .......... .......... .......... 96% 82.1M 0s
252350K .......... .......... .......... .......... .......... 96%  103M 0s
252400K .......... .......... .......... .......... .......... 96% 85.1M 0s
252450K .......... .......... .......... .......... .......... 96% 9.99M 0s
252500K .......... .......... .......... .......... .......... 96%  346M 0s
252550K .......... .......... .......... .......... .......... 96%  483M 0s
252600K .......... .......... .......... .......... .......... 96% 22.9M 0s
252650K .......... .......... .......... .......... .......... 96%  344M 0s
252700K .......... .......... .......... .......... .......... 96%  448M 0s
252750K .......... .......... .......... .......... .......... 96% 51.9M 0s
252800K .......... .......... .......... .......... .......... 96%  102M 0s
252850K .......... .......... .......... .......... .......... 96%  158M 0s
252900K .......... .......... .......... .......... .......... 96% 98.6M 0s
252950K .......... .......... .......... .......... .......... 96% 77.1M 0s
253000K .......... .......... .......... .......... .......... 96%  101M 0s
253050K .......... .......... .......... .......... .......... 96%  191M 0s
253100K .......... .......... .......... .......... .......... 96% 72.2M 0s
253150K .......... .......... .......... .......... .......... 96%  167M 0s
253200K .......... .......... .......... .......... .......... 96% 79.9M 0s
253250K .......... .......... .......... .......... .......... 96% 25.8M 0s
253300K .......... .......... .......... .......... .......... 96%  525M 0s
253350K .......... .......... .......... .......... .......... 96% 49.2M 0s
253400K .......... .......... .......... .......... .......... 96% 58.4M 0s
253450K .......... .......... .......... .......... .......... 96%  461M 0s
253500K .......... .......... .......... .......... .......... 96% 26.0M 0s
253550K .......... .......... .......... .......... .......... 96%  400M 0s
253600K .......... .......... .......... .......... .......... 96%  452M 0s
253650K .......... .......... .......... .......... .......... 96% 37.5M 0s
253700K .......... .......... .......... .......... .......... 96%  132M 0s
253750K .......... .......... .......... .......... .......... 96%  230M 0s
253800K .......... .......... .......... .......... .......... 96% 44.8M 0s
253850K .......... .......... .......... .......... .......... 96% 89.3M 0s
253900K .......... .......... .......... .......... .......... 96% 90.9M 0s
253950K .......... .......... .......... .......... .......... 96% 8.22M 0s
254000K .......... .......... .......... .......... .......... 96%  177M 0s
254050K .......... .......... .......... .......... .......... 96% 40.9M 0s
254100K .......... .......... .......... .......... .......... 96% 95.9M 0s
254150K .......... .......... .......... .......... .......... 96%  417M 0s
254200K .......... .......... .......... .......... .......... 96% 22.1M 0s
254250K .......... .......... .......... .......... .......... 96%  146M 0s
254300K .......... .......... .......... .......... .......... 97%  185M 0s
254350K .......... .......... .......... .......... .......... 97% 9.77M 0s
254400K .......... .......... .......... .......... .......... 97%  417M 0s
254450K .......... .......... .......... .......... .......... 97%  414M 0s
254500K .......... .......... .......... .......... .......... 97% 31.3M 0s
254550K .......... .......... .......... .......... .......... 97%  483M 0s
254600K .......... .......... .......... .......... .......... 97%  421M 0s
254650K .......... .......... .......... .......... .......... 97% 31.1M 0s
254700K .......... .......... .......... .......... .......... 97%  145M 0s
254750K .......... .......... .......... .......... .......... 97%  191M 0s
254800K .......... .......... .......... .......... .......... 97% 42.9M 0s
254850K .......... .......... .......... .......... .......... 97%  133M 0s
254900K .......... .......... .......... .......... .......... 97%  140M 0s
254950K .......... .......... .......... .......... .......... 97% 61.0M 0s
255000K .......... .......... .......... .......... .......... 97%  417M 0s
255050K .......... .......... .......... .......... .......... 97% 97.7M 0s
255100K .......... .......... .......... .......... .......... 97% 77.1M 0s
255150K .......... .......... .......... .......... .......... 97%  121M 0s
255200K .......... .......... .......... .......... .......... 97% 75.7M 0s
255250K .......... .......... .......... .......... .......... 97%  155M 0s
255300K .......... .......... .......... .......... .......... 97% 70.4M 0s
255350K .......... .......... .......... .......... .......... 97%  117M 0s
255400K .......... .......... .......... .......... .......... 97%  190M 0s
255450K .......... .......... .......... .......... .......... 97% 39.1M 0s
255500K .......... .......... .......... .......... .......... 97%  349M 0s
255550K .......... .......... .......... .......... .......... 97%  142M 0s
255600K .......... .......... .......... .......... .......... 97% 76.9M 0s
255650K .......... .......... .......... .......... .......... 97%  124M 0s
255700K .......... .......... .......... .......... .......... 97% 94.8M 0s
255750K .......... .......... .......... .......... .......... 97%  116M 0s
255800K .......... .......... .......... .......... .......... 97%  101M 0s
255850K .......... .......... .......... .......... .......... 97% 93.9M 0s
255900K .......... .......... .......... .......... .......... 97%  120M 0s
255950K .......... .......... .......... .......... .......... 97% 28.1M 0s
256000K .......... .......... .......... .......... .......... 97%  291M 0s
256050K .......... .......... .......... .......... .......... 97%  143M 0s
256100K .......... .......... .......... .......... .......... 97%  351M 0s
256150K .......... .......... .......... .......... .......... 97%  400M 0s
256200K .......... .......... .......... .......... .......... 97%  161M 0s
256250K .......... .......... .......... .......... .......... 97% 90.6M 0s
256300K .......... .......... .......... .......... .......... 97% 97.7M 0s
256350K .......... .......... .......... .......... .......... 97% 92.3M 0s
256400K .......... .......... .......... .......... .......... 97% 96.9M 0s
256450K .......... .......... .......... .......... .......... 97% 87.5M 0s
256500K .......... .......... .......... .......... .......... 97%  101M 0s
256550K .......... .......... .......... .......... .......... 97% 92.5M 0s
256600K .......... .......... .......... .......... .......... 97% 94.1M 0s
256650K .......... .......... .......... .......... .......... 97% 76.9M 0s
256700K .......... .......... .......... .......... .......... 97% 93.2M 0s
256750K .......... .......... .......... .......... .......... 97%  121M 0s
256800K .......... .......... .......... .......... .......... 97% 92.7M 0s
256850K .......... .......... .......... .......... .......... 97% 76.4M 0s
256900K .......... .......... .......... .......... .......... 97%  126M 0s
256950K .......... .......... .......... .......... .......... 98% 89.3M 0s
257000K .......... .......... .......... .......... .......... 98% 95.2M 0s
257050K .......... .......... .......... .......... .......... 98% 94.8M 0s
257100K .......... .......... .......... .......... .......... 98% 83.6M 0s
257150K .......... .......... .......... .......... .......... 98%  148M 0s
257200K .......... .......... .......... .......... .......... 98% 54.1M 0s
257250K .......... .......... .......... .......... .......... 98%  123M 0s
257300K .......... .......... .......... .......... .......... 98% 76.8M 0s
257350K .......... .......... .......... .......... .......... 98% 69.0M 0s
257400K .......... .......... .......... .......... .......... 98%  159M 0s
257450K .......... .......... .......... .......... .......... 98% 54.0M 0s
257500K .......... .......... .......... .......... .......... 98%  126M 0s
257550K .......... .......... .......... .......... .......... 98%  119M 0s
257600K .......... .......... .......... .......... .......... 98% 78.4M 0s
257650K .......... .......... .......... .......... .......... 98%  119M 0s
257700K .......... .......... .......... .......... .......... 98% 93.9M 0s
257750K .......... .......... .......... .......... .......... 98% 94.1M 0s
257800K .......... .......... .......... .......... .......... 98% 97.3M 0s
257850K .......... .......... .......... .......... .......... 98% 91.4M 0s
257900K .......... .......... .......... .......... .......... 98% 97.5M 0s
257950K .......... .......... .......... .......... .......... 98% 90.4M 0s
258000K .......... .......... .......... .......... .......... 98% 97.5M 0s
258050K .......... .......... .......... .......... .......... 98% 94.1M 0s
258100K .......... .......... .......... .......... .......... 98% 93.2M 0s
258150K .......... .......... .......... .......... .......... 98% 93.0M 0s
258200K .......... .......... .......... .......... .......... 98% 94.3M 0s
258250K .......... .......... .......... .......... .......... 98% 93.0M 0s
258300K .......... .......... .......... .......... .......... 98%  120M 0s
258350K .......... .......... .......... .......... .......... 98% 73.0M 0s
258400K .......... .......... .......... .......... .......... 98%  133M 0s
258450K .......... .......... .......... .......... .......... 98% 63.8M 0s
258500K .......... .......... .......... .......... .......... 98% 93.7M 0s
258550K .......... .......... .......... .......... .......... 98%  125M 0s
258600K .......... .......... .......... .......... .......... 98% 79.3M 0s
258650K .......... .......... .......... .......... .......... 98% 99.2M 0s
258700K .......... .......... .......... .......... .......... 98% 81.2M 0s
258750K .......... .......... .......... .......... .......... 98%  121M 0s
258800K .......... .......... .......... .......... .......... 98% 94.4M 0s
258850K .......... .......... .......... .......... .......... 98% 95.6M 0s
258900K .......... .......... .......... .......... .......... 98% 95.2M 0s
258950K .......... .......... .......... .......... .......... 98% 91.8M 0s
259000K .......... .......... .......... .......... .......... 98% 98.0M 0s
259050K .......... .......... .......... .......... .......... 98%  126M 0s
259100K .......... .......... .......... .......... .......... 98% 94.8M 0s
259150K .......... .......... .......... .......... .......... 98% 95.0M 0s
259200K .......... .......... .......... .......... .......... 98% 95.4M 0s
259250K .......... .......... .......... .......... .......... 98% 75.7M 0s
259300K .......... .......... .......... .......... .......... 98%  122M 0s
259350K .......... .......... .......... .......... .......... 98% 96.5M 0s
259400K .......... .......... .......... .......... .......... 98% 91.6M 0s
259450K .......... .......... .......... .......... .......... 98% 92.1M 0s
259500K .......... .......... .......... .......... .......... 98% 97.9M 0s
259550K .......... .......... .......... .......... .......... 99%  121M 0s
259600K .......... .......... .......... .......... .......... 99% 93.9M 0s
259650K .......... .......... .......... .......... .......... 99% 97.3M 0s
259700K .......... .......... .......... .......... .......... 99% 94.3M 0s
259750K .......... .......... .......... .......... .......... 99%  121M 0s
259800K .......... .......... .......... .......... .......... 99% 97.5M 0s
259850K .......... .......... .......... .......... .......... 99% 93.5M 0s
259900K .......... .......... .......... .......... .......... 99%  118M 0s
259950K .......... .......... .......... .......... .......... 99% 27.3M 0s
260000K .......... .......... .......... .......... .......... 99%  503M 0s
260050K .......... .......... .......... .......... .......... 99%  537M 0s
260100K .......... .......... .......... .......... .......... 99% 47.5M 0s
260150K .......... .......... .......... .......... .......... 99%  525M 0s
260200K .......... .......... .......... .......... .......... 99%  103M 0s
260250K .......... .......... .......... .......... .......... 99%  483M 0s
260300K .......... .......... .......... .......... .......... 99%  253M 0s
260350K .......... .......... .......... .......... .......... 99% 64.0M 0s
260400K .......... .......... .......... .......... .......... 99%  125M 0s
260450K .......... .......... .......... .......... .......... 99% 93.5M 0s
260500K .......... .......... .......... .......... .......... 99% 75.6M 0s
260550K .......... .......... .......... .......... .......... 99% 95.0M 0s
260600K .......... .......... .......... .......... .......... 99% 73.6M 0s
260650K .......... .......... .......... .......... .......... 99% 97.3M 0s
260700K .......... .......... .......... .......... .......... 99% 91.8M 0s
260750K .......... .......... .......... .......... .......... 99% 77.9M 0s
260800K .......... .......... .......... .......... .......... 99%  119M 0s
260850K .......... .......... .......... .......... .......... 99% 98.2M 0s
260900K .......... .......... .......... .......... .......... 99% 87.5M 0s
260950K .......... .......... .......... .......... .......... 99% 80.8M 0s
261000K .......... .......... .......... .......... .......... 99%  121M 0s
261050K .......... .......... .......... .......... .......... 99% 97.1M 0s
261100K .......... .......... .......... .......... .......... 99% 74.9M 0s
261150K .......... .......... .......... .......... .......... 99%  123M 0s
261200K .......... .......... .......... .......... .......... 99% 78.0M 0s
261250K .......... .......... .......... .......... .......... 99%  116M 0s
261300K .......... .......... .......... .......... .......... 99% 99.6M 0s
261350K .......... .......... .......... .......... .......... 99% 90.6M 0s
261400K .......... .......... .......... .......... .......... 99% 98.0M 0s
261450K .......... .......... .......... .......... .......... 99% 92.1M 0s
261500K .......... .......... .......... .......... .......... 99% 97.3M 0s
261550K .......... .......... .......... .......... .......... 99% 95.4M 0s
261600K .......... .......... .......... .......... .......... 99% 62.8M 0s
261650K .......... .......... .......... .......... .......... 99%  123M 0s
261700K .......... .......... .......... .......... .......... 99% 73.8M 0s
261750K .......... .......... .......... .......... .......... 99% 98.2M 0s
261800K .......... .......... .......... .......... .......... 99%  125M 0s
261850K .......... .......... .......... .......... .......... 99% 95.0M 0s
261900K .......... .......... .......... .......... .......... 99% 91.3M 0s
261950K .......... .......... .......... .......... .......... 99% 96.9M 0s
262000K .......... .......... .......... .......... .......... 99% 92.3M 0s
262050K .......... .......... .......... .......... .......... 99% 77.4M 0s
262100K .......... .......... .......... .......... .......... 99% 73.5M 0s
262150K .......... .......... .......... .......... .......... 99% 97.7M 0s
262200K ........                                              100%  380M=3.4s

2024-05-03 00:16:04 (75.8 MB/s) - ‘ESPbeta.tgz’ saved [268501958/268501958]

+ tar -xf ESPbeta.tgz
+ rm -rf EngSketchPad/data/Slugs
+ python --version
Python 3.11.9
+ [[ '' == *\.\i\f\o\r\t ]]
+ cd /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/config/
+ ./makeEnv

ESP runtime AutoConfigurator

CASROOT = /Users/jenkins/util/ESP/OpenCASCADE-7.8.0  with contents:
bin
include
lib
share


Info: Python exec /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/ESP_venv/bin/python found!
Info: Python header /Users/jenkins/util/ESP/Python/ESP_Python-3.11.9/include/python3.11/Python.h found!
Info: Python library /Users/jenkins/util/ESP/Python/ESP_Python-3.11.9/lib/libpython3.11.dylib found!

ESP_ARCH = DARWIN_ARM64
ESP_ROOT = /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad
EFCOMP   = gfortran

CARCH    = DARWIN_ARM64
CASROOT  = /Users/jenkins/util/ESP/OpenCASCADE-7.8.0
CASARCH  = .
CASREV   = 7.8

PYTHONINC= /Users/jenkins/util/ESP/Python/ESP_Python-3.11.9/include/python3.11
PYTHONLIB= -L/Users/jenkins/util/ESP/Python/ESP_Python-3.11.9/lib -lpython3.11

+ source /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/ESPenv.sh
++ export ESP_ARCH=DARWIN_ARM64
++ ESP_ARCH=DARWIN_ARM64
++ export ESP_ROOT=/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad
++ ESP_ROOT=/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad
++ export CASROOT=/Users/jenkins/util/ESP/OpenCASCADE-7.8.0
++ CASROOT=/Users/jenkins/util/ESP/OpenCASCADE-7.8.0
++ export CASARCH=.
++ CASARCH=.
++ export CASREV=7.8
++ CASREV=7.8
++ export PATH=/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/bin:/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/ESP_venv/bin:/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/ESP/DARWIN_ARM64/test:/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/ESP/DARWIN_ARM64/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_Beta/7.8/DARWIN_ARM64/EngSketchPad/bin:/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/ESP_venv/bin:/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/ESP/DARWIN_ARM64/test:/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/ESP/DARWIN_ARM64/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/util/ESP/Python/ESP_Python-3.11.9/include/python3.11
++ PYTHONINC=/Users/jenkins/util/ESP/Python/ESP_Python-3.11.9/include/python3.11
++ export 'PYTHONLIB=-L/Users/jenkins/util/ESP/Python/ESP_Python-3.11.9/lib -lpython3.11'
++ PYTHONLIB='-L/Users/jenkins/util/ESP/Python/ESP_Python-3.11.9/lib -lpython3.11'
++ export PYTHONPATH=/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/pyESP:/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/CAPS/pyCAPS:/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/OpenCSM/trunk/pyOCSM:/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EGADS/trunk/pyEGADS::/Users/jenkins/util/SU2/SU2-v8.0.0/bin
++ PYTHONPATH=/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/pyESP:/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/CAPS/pyCAPS:/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/OpenCSM/trunk/pyOCSM:/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EGADS/trunk/pyEGADS::/Users/jenkins/util/SU2/SU2-v8.0.0/bin
++ export EFCOMP=gfortran
++ EFCOMP=gfortran
++ export AFLR_ARCH=MacOSX-arm64
++ AFLR_ARCH=MacOSX-arm64
++ export UDUNITS2_XML_PATH=/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/src/CAPS/udunits/udunits2.xml
++ UDUNITS2_XML_PATH=/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/src/CAPS/udunits/udunits2.xml
++ export CAPS_GLYPH=
++ CAPS_GLYPH=
++ export TETGEN=/Users/jenkins/util/tetgen/tetgen1.6.0
++ TETGEN=/Users/jenkins/util/tetgen/tetgen1.6.0
++ export 'SLUGS_START=open -a /Applications/Safari.app /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/SLUGS/Slugs.html'
++ SLUGS_START='open -a /Applications/Safari.app /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/SLUGS/Slugs.html'
++ export 'ESP_START=open -a /Applications/Safari.app;sleep 1;open -a /Applications/Safari.app /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/ESP/ESP.html'
++ ESP_START='open -a /Applications/Safari.app;sleep 1;open -a /Applications/Safari.app /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/ESP/ESP.html'
++ export 'WV_START=open -a /Applications/Safari.app /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/wvClient/wv.html'
++ WV_START='open -a /Applications/Safari.app /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/wvClient/wv.html'
+ cd /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/src
+ make
(cd EGADS/src; make)
touch /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/include/DARWIN_ARM64
rm /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/include/DARWIN_ARM64
cp -p ../include/DARWIN_ARM64 /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/include/DARWIN_ARM64
touch /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/include/STANALYZER.make
rm /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/include/STANALYZER.make
cp -p ../include/STANALYZER.make /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/include/STANALYZER.make
touch /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/include/egads.h
rm /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/include/egads.h
cp -p ../include/egads.h /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/include/egads.h
touch /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/include/egads_dot.h
rm /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/include/egads_dot.h
cp -p ../include/egads_dot.h /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/include/egads_dot.h
touch /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/include/egads.inc
rm /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/include/egads.inc
cp -p ../include/egads.inc /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/include/egads.inc
touch /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/include/egadsErrors.h
rm /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/include/egadsErrors.h
cp -p ../include/egadsErrors.h /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/include/egadsErrors.h
touch /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/include/egadsTypes.h
rm /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/include/egadsTypes.h
cp -p ../include/egadsTypes.h /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/include/egadsTypes.h
touch /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/include/emp.h
rm /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/include/emp.h
cp -p ../include/emp.h /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/include/emp.h
touch /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/include/prm.h
rm /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/include/prm.h
cp -p ../include/prm.h /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/include/prm.h
touch /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/include/wsserver.h
rm /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/include/wsserver.h
cp -p ../include/wsserver.h /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/include/wsserver.h
touch /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/include/wsserver.inc
rm /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/include/wsserver.inc
cp -p ../include/wsserver.inc /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/include/wsserver.inc
touch /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/include/wsss.h
rm /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/include/wsss.h
cp -p ../include/wsss.h /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/include/wsss.h
touch /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/include/egadsTris.h
rm /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/include/egadsTris.h
cp -p egadsTris.h /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/include/egadsTris.h
touch /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/include/egadsSplineFit.h
rm /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/include/egadsSplineFit.h
cp -p egadsSplineFit.h /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/include/egadsSplineFit.h
touch /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/include/egadsSplineVels.h
rm /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/include/egadsSplineVels.h
cp -p egadsSplineVels.h /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/include/egadsSplineVels.h
touch /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/include/egadsf90.inc
rm /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/include/egadsf90.inc
cp -p ../include/egadsf90.inc /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/include/egadsf90.inc
mkdir -p /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/include/Surreal
cp Surreal/SurrealD.h /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/include/Surreal/SurrealD.h
mkdir -p /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/include/Surreal
cp Surreal/SurrealD_Lazy.h /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/include/Surreal/SurrealD_Lazy.h
mkdir -p /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/include/Surreal
cp Surreal/SurrealD_Trad.h /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/include/Surreal/SurrealD_Trad.h
mkdir -p /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/include/Surreal
cp Surreal/SurrealS.h /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/include/Surreal/SurrealS.h
mkdir -p /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/include/Surreal
cp Surreal/SurrealS_Lazy.h /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/include/Surreal/SurrealS_Lazy.h
mkdir -p /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/include/Surreal
cp Surreal/SurrealS_Trad.h /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/include/Surreal/SurrealS_Trad.h
mkdir -p /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/include/Surreal
cp Surreal/always_inline.h /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/include/Surreal/always_inline.h
clang++ -g -target arm64-apple-darwin  -c -O -fPIC -DOCC_CONVERT_SIGNALS -DNDEBUG -DNo_Exception -D_OCC64 -Wall -Wno-write-strings -Wno-dangling-else -Wno-unused-result -std=c++11 -ffp-model=strict -DREVISION=7.8  -IOCC -I/Users/jenkins/util/ESP/OpenCASCADE-7.8.0/inc -I/Users/jenkins/util/ESP/OpenCASCADE-7.8.0/include/opencascade -I/Users/jenkins/util/ESP/OpenCASCADE-7.8.0 -I../include \
		-I. egadsGeom.cpp -o ./egadsGeom.o
clang++ -g -target arm64-apple-darwin  -c -O -fPIC -DOCC_CONVERT_SIGNALS -DNDEBUG -DNo_Exception -D_OCC64 -Wall -Wno-write-strings -Wno-dangling-else -Wno-unused-result -std=c++11 -ffp-model=strict -DREVISION=7.8  -IOCC -I/Users/jenkins/util/ESP/OpenCASCADE-7.8.0/inc -I/Users/jenkins/util/ESP/OpenCASCADE-7.8.0/include/opencascade -I/Users/jenkins/util/ESP/OpenCASCADE-7.8.0 -I../include \
		-I. egadsHLevel.cpp -o ./egadsHLevel.o
clang++ -g -target arm64-apple-darwin  -c -O -fPIC -DOCC_CONVERT_SIGNALS -DNDEBUG -DNo_Exception -D_OCC64 -Wall -Wno-write-strings -Wno-dangling-else -Wno-unused-result -std=c++11 -ffp-model=strict -DREVISION=7.8  -IOCC -I/Users/jenkins/util/ESP/OpenCASCADE-7.8.0/inc -I/Users/jenkins/util/ESP/OpenCASCADE-7.8.0/include/opencascade -I/Users/jenkins/util/ESP/OpenCASCADE-7.8.0 -I../include \
		-I. egadsTopo.cpp -o ./egadsTopo.o
clang++ -g -target arm64-apple-darwin  -c -O -fPIC -DOCC_CONVERT_SIGNALS -DNDEBUG -DNo_Exception -D_OCC64 -Wall -Wno-write-strings -Wno-dangling-else -Wno-unused-result -std=c++11 -ffp-model=strict -DREVISION=7.8  -IOCC -I/Users/jenkins/util/ESP/OpenCASCADE-7.8.0/inc -I/Users/jenkins/util/ESP/OpenCASCADE-7.8.0/include/opencascade -I/Users/jenkins/util/ESP/OpenCASCADE-7.8.0 -I../include \
		-I. egadsCopy.cpp -o ./egadsCopy.o
clang++ -g -target arm64-apple-darwin  -c -O -fPIC -DOCC_CONVERT_SIGNALS -DNDEBUG -DNo_Exception -D_OCC64 -Wall -Wno-write-strings -Wno-dangling-else -Wno-unused-result -std=c++11 -ffp-model=strict -DREVISION=7.8  -IOCC -I/Users/jenkins/util/ESP/OpenCASCADE-7.8.0/inc -I/Users/jenkins/util/ESP/OpenCASCADE-7.8.0/include/opencascade -I/Users/jenkins/util/ESP/OpenCASCADE-7.8.0 -I../include \
		-I. egadsSpline.cpp -o ./egadsSpline.o
clang++ -g -target arm64-apple-darwin  -c -O -fPIC -DOCC_CONVERT_SIGNALS -DNDEBUG -DNo_Exception -D_OCC64 -Wall -Wno-write-strings -Wno-dangling-else -Wno-unused-result -std=c++11 -ffp-model=strict -DREVISION=7.8  -IOCC -I/Users/jenkins/util/ESP/OpenCASCADE-7.8.0/inc -I/Users/jenkins/util/ESP/OpenCASCADE-7.8.0/include/opencascade -I/Users/jenkins/util/ESP/OpenCASCADE-7.8.0 -I../include \
		-I. egadsIO.cpp -o ./egadsIO.o
clang++ -g -target arm64-apple-darwin  -c -O -fPIC -DOCC_CONVERT_SIGNALS -DNDEBUG -DNo_Exception -D_OCC64 -Wall -Wno-write-strings -Wno-dangling-else -Wno-unused-result -std=c++11 -ffp-model=strict -DREVISION=7.8  -IOCC -I/Users/jenkins/util/ESP/OpenCASCADE-7.8.0/inc -I/Users/jenkins/util/ESP/OpenCASCADE-7.8.0/include/opencascade -I/Users/jenkins/util/ESP/OpenCASCADE-7.8.0 -I../include \
		-I. egadsSplineFit.cpp -o ./egadsSplineFit.o
clang++ -g -target arm64-apple-darwin  -c -O -fPIC -DOCC_CONVERT_SIGNALS -DNDEBUG -DNo_Exception -D_OCC64 -Wall -Wno-write-strings -Wno-dangling-else -Wno-unused-result -std=c++11 -ffp-model=strict -DREVISION=7.8  -IOCC -I/Users/jenkins/util/ESP/OpenCASCADE-7.8.0/inc -I/Users/jenkins/util/ESP/OpenCASCADE-7.8.0/include/opencascade -I/Users/jenkins/util/ESP/OpenCASCADE-7.8.0 -I../include \
		-I. egadsSkinning.cpp -o ./egadsSkinning.o
clang++ -g -target arm64-apple-darwin  -c -O -fPIC -DOCC_CONVERT_SIGNALS -DNDEBUG -DNo_Exception -D_OCC64 -Wall -Wno-write-strings -Wno-dangling-else -Wno-unused-result -std=c++11 -ffp-model=strict -DREVISION=7.8  -IOCC -I/Users/jenkins/util/ESP/OpenCASCADE-7.8.0/inc -I/Users/jenkins/util/ESP/OpenCASCADE-7.8.0/include/opencascade -I/Users/jenkins/util/ESP/OpenCASCADE-7.8.0 -I../include \
		-I. egadsTessSens.cpp -o ./egadsTessSens.o
clang++ -g -target arm64-apple-darwin  -c -O -fPIC -DOCC_CONVERT_SIGNALS -DNDEBUG -DNo_Exception -D_OCC64 -Wall -Wno-write-strings -Wno-dangling-else -Wno-unused-result -std=c++11 -ffp-model=strict -DREVISION=7.8  -IOCC -I/Users/jenkins/util/ESP/OpenCASCADE-7.8.0/inc -I/Users/jenkins/util/ESP/OpenCASCADE-7.8.0/include/opencascade -I/Users/jenkins/util/ESP/OpenCASCADE-7.8.0 OCC/BRepLib_FuseEdges.cpp -o ./BRepLib_FuseEdges.o
clang -g -target arm64-apple-darwin  -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8  -I../include -I../util \
		-I../util/uvmap egadsBase.c -o ./egadsBase.o
clang -g -target arm64-apple-darwin  -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8  -I../include -I../util \
		-I../util/uvmap egadsMemory.c -o ./egadsMemory.o
clang -g -target arm64-apple-darwin  -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8  -I../include -I../util \
		-I../util/uvmap egadsAttrs.c -o ./egadsAttrs.o
clang -g -target arm64-apple-darwin  -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8  -I../include -I../util \
		-I../util/uvmap egadsTess.c -o ./egadsTess.o
clang -g -target arm64-apple-darwin  -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8  -I../include -I../util \
		-I../util/uvmap egadsTessInp.c -o ./egadsTessInp.o
clang -g -target arm64-apple-darwin  -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8  -I../include -I../util \
		-I../util/uvmap egadsTris.c -o ./egadsTris.o
clang -g -target arm64-apple-darwin  -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8  -I../include -I../util \
		-I../util/uvmap egadsQuads.c -o ./egadsQuads.o
clang -g -target arm64-apple-darwin  -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8  -I../include -I../util \
		-I../util/uvmap egadsFit.c -o ./egadsFit.o
clang -g -target arm64-apple-darwin  -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8  -I../include -I../util \
		-I../util/uvmap egadsRobust.c -o ./egadsRobust.o
clang -g -target arm64-apple-darwin  -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8  -I../include -I../util \
		-I../util/uvmap egadsSBO.c -o ./egadsSBO.o
clang -g -target arm64-apple-darwin  -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8  -I../include -I../util \
		-I../util/uvmap prmCfit.c -o ./prmCfit.o
clang -g -target arm64-apple-darwin  -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8  -I../include -I../util \
		-I../util/uvmap prmGrid.c -o ./prmGrid.o
clang -g -target arm64-apple-darwin  -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8  -I../include -I../util \
		-I../util/uvmap prmUV.c -o ./prmUV.o
clang -g -target arm64-apple-darwin  -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8  -I../include -I../util \
		-I../util/uvmap egadsExport.c -o ./egadsExport.o
clang -g -target arm64-apple-darwin  -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8  -I../include -I../util \
		-I../util/uvmap egadsEffect.c -o ./egadsEffect.o
clang -g -target arm64-apple-darwin  -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8  -I../include -I../util \
		-I../util/uvmap egadsSolids.c -o ./egadsSolids.o
clang -g -target arm64-apple-darwin  -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I../include ../util/emp.c \
		-o ./emp.o
clang++ -g -target arm64-apple-darwin  -x c++ -c -O -fPIC -DOCC_CONVERT_SIGNALS -DNDEBUG -DNo_Exception -D_OCC64 -Wall -Wno-write-strings -Wno-dangling-else -Wno-unused-result -std=c++11 -ffp-model=strict -DREVISION=7.8 -IOCC -I/Users/jenkins/util/ESP/OpenCASCADE-7.8.0/inc -I/Users/jenkins/util/ESP/OpenCASCADE-7.8.0/include/opencascade -I/Users/jenkins/util/ESP/OpenCASCADE-7.8.0 -I. -I../include \
		../util/evaluate.c -o ./evaluate.o
clang++ -g -target arm64-apple-darwin  -x c++ -c -O -fPIC -DOCC_CONVERT_SIGNALS -DNDEBUG -DNo_Exception -D_OCC64 -Wall -Wno-write-strings -Wno-dangling-else -Wno-unused-result -std=c++11 -ffp-model=strict -DREVISION=7.8 -I/Users/jenkins/util/ESP/OpenCASCADE-7.8.0/inc -I/Users/jenkins/util/ESP/OpenCASCADE-7.8.0/include/opencascade -I/Users/jenkins/util/ESP/OpenCASCADE-7.8.0 -I. -I../include \
		../util/rational.c -o ./rational.o
clang -g -target arm64-apple-darwin  -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/util/ESP/OpenCASCADE-7.8.0/inc -I/Users/jenkins/util/ESP/OpenCASCADE-7.8.0/include/opencascade -I/Users/jenkins/util/ESP/OpenCASCADE-7.8.0 -I../include -I../util \
		../util/regQuads.c -o ./regQuads.o
clang++ -g -target arm64-apple-darwin  -o ./SurrealD1 -O -std=c++11 -I. ../util/SurrealD1_btest.cpp
./SurrealD1

SurrealD1_test_suite Complete!

clang++ -g -target arm64-apple-darwin  -o ./SurrealD4 -O -std=c++11 -I. ../util/SurrealD4_btest.cpp
./SurrealD4

SurrealD4_test_suite Complete!

clang++ -g -target arm64-apple-darwin  -o ./SurrealS1 -O -std=c++11 -I. ../util/SurrealS1_btest.cpp
./SurrealS1

SurrealS1_test_suite Complete!

clang++ -g -target arm64-apple-darwin  -o ./SurrealS4 -O -std=c++11 -I. ../util/SurrealS4_btest.cpp
./SurrealS4

SurrealS4_test_suite Complete!

/Library/Developer/CommandLineTools/usr/bin/make -C ../util
clang -g -target arm64-apple-darwin  -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 uvmap/main/uvmap.c -Iuvmap \
		-o ./uvmap.o
clang -g -target arm64-apple-darwin  -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I. uvmap/EG_uvmapFindUV.c -o ./EG_uvmapFindUV.o
clang -g -target arm64-apple-darwin  -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I. uvmap/EG_uvmapGen.c -o ./EG_uvmapGen.o
clang -g -target arm64-apple-darwin  -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I. uvmap/EG_uvmapStructFree.c -o ./EG_uvmapStructFree.o
clang -g -target arm64-apple-darwin  -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I. uvmap/EG_uvmapTest.c -o ./EG_uvmapTest.o
clang -g -target arm64-apple-darwin  -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I. uvmap/EG_uvmap_Read.c -o ./EG_uvmap_Read.o
clang -g -target arm64-apple-darwin  -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I. uvmap/EG_uvmap_Write.c -o ./EG_uvmap_Write.o
clang -g -target arm64-apple-darwin  -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I. uvmap/uvmap_add.c -o ./uvmap_add.o
clang -g -target arm64-apple-darwin  -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I. uvmap/uvmap_bnd_adj.c -o ./uvmap_bnd_adj.o
clang -g -target arm64-apple-darwin  -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I. uvmap/uvmap_chk_area_uv.c -o ./uvmap_chk_area_uv.o
clang -g -target arm64-apple-darwin  -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I. uvmap/uvmap_chk_edge_ratio.c -o ./uvmap_chk_edge_ratio.o
clang -g -target arm64-apple-darwin  -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I. uvmap/uvmap_cpu_message.c -o ./uvmap_cpu_message.o
clang -g -target arm64-apple-darwin  -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I. uvmap/uvmap_find_uv.c -o ./uvmap_find_uv.o
clang -g -target arm64-apple-darwin  -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I. uvmap/uvmap_from_egads.c -o ./uvmap_from_egads.o
clang -g -target arm64-apple-darwin  -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I. uvmap/uvmap_gen.c -o ./uvmap_gen.o
clang -g -target arm64-apple-darwin  -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I. uvmap/uvmap_gen_uv.c -o ./uvmap_gen_uv.o
clang -g -target arm64-apple-darwin  -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I. uvmap/uvmap_ibeibe.c -o ./uvmap_ibeibe.o
clang -g -target arm64-apple-darwin  -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I. uvmap/uvmap_ibfibf.c -o ./uvmap_ibfibf.o
clang -g -target arm64-apple-darwin  -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I. uvmap/uvmap_ibfin.c -o ./uvmap_ibfin.o
clang -g -target arm64-apple-darwin  -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I. uvmap/uvmap_iccibe.c -o ./uvmap_iccibe.o
clang -g -target arm64-apple-darwin  -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I. uvmap/uvmap_iccin.c -o ./uvmap_iccin.o
clang -g -target arm64-apple-darwin  -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I. uvmap/uvmap_idibe.c -o ./uvmap_idibe.o
clang -g -target arm64-apple-darwin  -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I. uvmap/uvmap_inibe.c -o ./uvmap_inibe.o
clang -g -target arm64-apple-darwin  -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I. uvmap/uvmap_inl_uv_bnd.c -o ./uvmap_inl_uv_bnd.o
clang -g -target arm64-apple-darwin  -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I. uvmap/uvmap_malloc.c -o ./uvmap_malloc.o
clang -g -target arm64-apple-darwin  -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I. uvmap/uvmap_mben_disc.c -o ./uvmap_mben_disc.o
clang -g -target arm64-apple-darwin  -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I. uvmap/uvmap_message.c -o ./uvmap_message.o
clang -g -target arm64-apple-darwin  -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I. uvmap/uvmap_norm_uv.c -o ./uvmap_norm_uv.o
clang -g -target arm64-apple-darwin  -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I. uvmap/uvmap_read.c -o ./uvmap_read.o
clang -g -target arm64-apple-darwin  -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I. uvmap/uvmap_solve.c -o ./uvmap_solve.o
clang -g -target arm64-apple-darwin  -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I. uvmap/uvmap_struct_tasks.c -o ./uvmap_struct_tasks.o
clang -g -target arm64-apple-darwin  -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I. uvmap/uvmap_test.c -o ./uvmap_test.o
clang -g -target arm64-apple-darwin  -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I. uvmap/uvmap_to_egads.c -o ./uvmap_to_egads.o
clang -g -target arm64-apple-darwin  -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I. uvmap/uvmap_version.c -o ./uvmap_version.o
clang -g -target arm64-apple-darwin  -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I. uvmap/uvmap_write.c -o ./uvmap_write.o
clang -g -target arm64-apple-darwin  -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 egadsUVmap.c -Iuvmap \
		-o ./egadsUVmap.o
touch /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib/libuvmap.a
rm /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib/libuvmap.a
(cd .; ar rs /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib/libuvmap.a ./egadsUVmap.o EG_uvmapFindUV.o EG_uvmapGen.o EG_uvmapStructFree.o EG_uvmapTest.o EG_uvmap_Read.o EG_uvmap_Write.o uvmap_add.o uvmap_bnd_adj.o uvmap_chk_area_uv.o uvmap_chk_edge_ratio.o uvmap_cpu_message.o uvmap_find_uv.o uvmap_from_egads.o uvmap_gen.o uvmap_gen_uv.o uvmap_ibeibe.o uvmap_ibfibf.o uvmap_ibfin.o uvmap_iccibe.o uvmap_iccin.o uvmap_idibe.o uvmap_inibe.o uvmap_inl_uv_bnd.o uvmap_malloc.o uvmap_mben_disc.o uvmap_message.o uvmap_norm_uv.o uvmap_read.o uvmap_solve.o uvmap_struct_tasks.o uvmap_test.o uvmap_to_egads.o uvmap_version.o uvmap_write.o;  )
ar: creating archive /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib/libuvmap.a
clang -g -target arm64-apple-darwin  -o ./uvmap.exe ./uvmap.o \
		-L/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib -luvmap -rpath /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.8.0/./lib -lm
touch /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib/libegads.dylib
rm /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib/libegads.dylib
(cd .; clang -g -target arm64-apple-darwin  -dynamiclib -o /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib/libegads.dylib egadsGeom.o egadsHLevel.o egadsTopo.o egadsCopy.o egadsSpline.o egadsIO.o   egadsSplineFit.o egadsSkinning.o egadsTessSens.o  BRepLib_FuseEdges.o  \
		egadsBase.o egadsMemory.o egadsAttrs.o  egadsTess.o   egadsTessInp.o egadsTris.o egadsQuads.o  egadsFit.o    egadsRobust.o egadsSBO.o prmCfit.o   prmGrid.o     prmUV.o       egadsExport.o egadsEffect.o egadsSolids.o emp.o evaluate.o rational.o regQuads.o \
		-rpath /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.8.0/./lib -L/Users/jenkins/util/ESP/OpenCASCADE-7.8.0/./lib -L/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib -luvmap -lTKBool -lTKernel -lTKFeat -lTKBO -lTKGeomAlgo -lTKMath -lTKOffset -lTKPrim -lTKTopAlgo -lTKBRep -lTKG2d -lTKG3d -lTKGeomBase -lTKShHealing -lTKDESTEP -lTKDEIGES -lTKXSBase -lTKFillet -lc++ \
		-install_name '@rpath/libegads.dylib' \
		-compatibility_version 7.8 \
		-current_version 1.0.25 )
touch /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib/libegadstatic.a
rm /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib/libegadstatic.a
cp /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib/libuvmap.a /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib/libegadstatic.a
(cd .; \
		ar rs /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib/libegadstatic.a egadsBase.o egadsMemory.o egadsAttrs.o  egadsTess.o   egadsTessInp.o egadsTris.o egadsQuads.o  egadsFit.o    egadsRobust.o egadsSBO.o prmCfit.o   prmGrid.o     prmUV.o       egadsExport.o egadsEffect.o egadsSolids.o egadsGeom.o egadsHLevel.o egadsTopo.o egadsCopy.o egadsSpline.o egadsIO.o   egadsSplineFit.o egadsSkinning.o egadsTessSens.o  BRepLib_FuseEdges.o  emp.o \
		evaluate.o rational.o regQuads.o;  )
clang -g -target arm64-apple-darwin  -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8  -I../include fgadsBase.c -o ./fgadsBase.o
clang -g -target arm64-apple-darwin  -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8  -I../include fgadsMemory.c -o ./fgadsMemory.o
clang -g -target arm64-apple-darwin  -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8  -I../include fgadsAttrs.c -o ./fgadsAttrs.o
clang -g -target arm64-apple-darwin  -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8  -I../include fgadsTess.c -o ./fgadsTess.o
clang -g -target arm64-apple-darwin  -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8  -I../include fgadsHLevel.c -o ./fgadsHLevel.o
clang -g -target arm64-apple-darwin  -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8  -I../include fgadsGeom.c -o ./fgadsGeom.o
clang -g -target arm64-apple-darwin  -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8  -I../include fgadsTopo.c -o ./fgadsTopo.o
touch /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib/libfgads.a
rm /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib/libfgads.a
(cd .; ar rs /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib/libfgads.a fgadsBase.o fgadsMemory.o fgadsAttrs.o  fgadsTess.o   fgadsHLevel.o fgadsGeom.o fgadsTopo.o;  )
ar: creating archive /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib/libfgads.a
touch /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib/libemp.a
rm /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib/libemp.a
(cd .; ar rs /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib/libemp.a emp.o;  )
ar: creating archive /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib/libemp.a
 *** EGADS Build Complete! ***
(cd EGADS/lite; make)
clang -g -target arm64-apple-darwin  -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I../include -I. -I../src -I../util/uvmap \
		liteBase.c -o ./liteBase.o
clang -g -target arm64-apple-darwin  -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I../include -I. -I../src -I../util/uvmap \
		liteMemory.c -o ./liteMemory.o
clang -g -target arm64-apple-darwin  -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I../include -I. -I../src -I../util/uvmap \
		liteGeom.c -o ./liteGeom.o
clang -g -target arm64-apple-darwin  -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I../include -I. -I../src -I../util/uvmap \
		liteTopo.c -o ./liteTopo.o
clang -g -target arm64-apple-darwin  -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I../include -I. -I../src -I../util/uvmap \
		liteAttrs.c -o ./liteAttrs.o
clang -g -target arm64-apple-darwin  -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I../include -I. -I../src -I../util/uvmap \
		liteImport.c -o ./liteImport.o
clang -g -target arm64-apple-darwin  -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I../include -I. -I../src -I../util/uvmap \
		liteString.c -o ./liteString.o
clang -g -target arm64-apple-darwin  -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -DLITE -I../include -I. -I../src \
                ../src/egadsTess.c -o ./liteTess.o
clang -g -target arm64-apple-darwin  -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -DLITE -I../include -I. -I../src \
                ../src/egadsTris.c -o ./liteTris.o
clang -g -target arm64-apple-darwin  -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I../include -I. -I../src \
                ../src/egadsQuads.c -o ./liteQuads.o
clang -g -target arm64-apple-darwin  -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -DLITE -I../include -I. -I../src \
                -I../util ../src/egadsTessInp.c -o ./liteTessInp.o
clang -g -target arm64-apple-darwin  -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 ../src/egadsRobust.c \
		-o ./egadsRobust.o
clang -g -target arm64-apple-darwin  -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -DDARWIN_ARM64 -I../include ../util/emp.c \
		-o ./emp.o
clang -g -target arm64-apple-darwin  -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -DLITE -I../include -I. -I../src \
		../util/evaluate.c -o ./evaLite.o
clang -g -target arm64-apple-darwin  -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -DLITE ../util/rational.c \
		-o ./ratLite.o
clang -g -target arm64-apple-darwin  -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -DLITE -I../include -I../util \
		../util/regQuads.c -o ./liteRegQuads.o
clang -g -target arm64-apple-darwin  -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -DLITE -I../include -I. -I../src \
                ../src/egadsEffect.c -o ./liteEffect.o
clang -g -target arm64-apple-darwin  -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -DLITE -I../include -I. -I../src \
                -I../util/uvmap liteUVmap.c -o ./liteUVmap.o
touch /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib/libegadslite.dylib
rm /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib/libegadslite.dylib
(cd .; clang -g -target arm64-apple-darwin  -dynamiclib -o /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib/libegadslite.dylib \
                liteBase.o liteMemory.o liteGeom.o liteTopo.o liteAttrs.o liteImport.o liteString.o liteTess.o liteTris.o liteQuads.o liteTessInp.o \
		egadsRobust.o emp.o evaLite.o ratLite.o liteRegQuads.o \
		liteEffect.o liteUVmap.o \
		-install_name '@rpath/libegadslite.dylib' \
                -current_version 1.0.25 )
touch /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib/libegadslitestatic.a
rm /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib/libegadslitestatic.a
(cd .; ar rs /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib/libegadslitestatic.a liteBase.o liteMemory.o liteGeom.o liteTopo.o liteAttrs.o liteImport.o liteString.o \
                liteTess.o liteTris.o liteQuads.o liteTessInp.o egadsRobust.o \
		emp.o evaLite.o ratLite.o liteRegQuads.o liteEffect.o \
		liteUVmap.o ;  )
ar: creating archive /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib/libegadslitestatic.a
(cd wvServer; make)
clang++ -g -target arm64-apple-darwin  -c -O -fPIC -DOCC_CONVERT_SIGNALS -DNDEBUG -DNo_Exception -D_OCC64 -Wall -Wno-write-strings -Wno-dangling-else -Wno-unused-result -std=c++11 -ffp-model=strict map.cpp -o ./map.o
clang -g -target arm64-apple-darwin  -c -O -Wall -Wno-dangling-else -Wno-unused-result -DLWS_NO_FORK -I/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/include base64-decode.c -o ./base64-decode.o
clang -g -target arm64-apple-darwin  -c -O -Wall -Wno-dangling-else -Wno-unused-result -DLWS_NO_FORK -I/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/include handshake.c -o ./handshake.o
clang -g -target arm64-apple-darwin  -c -O -Wall -Wno-dangling-else -Wno-unused-result -DLWS_NO_FORK -I/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/include client-handshake.c -o ./client-handshake.o
clang -g -target arm64-apple-darwin  -c -O -Wall -Wno-dangling-else -Wno-unused-result -DLWS_NO_FORK -I/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/include libwebsockets.c -o ./libwebsockets.o
clang -g -target arm64-apple-darwin  -c -O -Wall -Wno-dangling-else -Wno-unused-result -DLWS_NO_FORK -I/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/include extension-deflate-stream.c -o ./extension-deflate-stream.o
clang -g -target arm64-apple-darwin  -c -O -Wall -Wno-dangling-else -Wno-unused-result -DLWS_NO_FORK -I/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/include md5.c -o ./md5.o
clang -g -target arm64-apple-darwin  -c -O -Wall -Wno-dangling-else -Wno-unused-result -DLWS_NO_FORK -I/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/include extension-x-google-mux.c -o ./extension-x-google-mux.o
clang -g -target arm64-apple-darwin  -c -O -Wall -Wno-dangling-else -Wno-unused-result -DLWS_NO_FORK -I/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/include parsers.c -o ./parsers.o
clang -g -target arm64-apple-darwin  -c -O -Wall -Wno-dangling-else -Wno-unused-result -DLWS_NO_FORK -I/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/include extension.c -o ./extension.o
clang -g -target arm64-apple-darwin  -c -O -Wall -Wno-dangling-else -Wno-unused-result -DLWS_NO_FORK -I/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/include sha-1.c -o ./sha-1.o
clang -g -target arm64-apple-darwin  -c -O -Wall -Wno-dangling-else -Wno-unused-result -DLWS_NO_FORK -I/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/include server.c -o ./server.o
clang -g -target arm64-apple-darwin  -c -O -Wall -Wno-dangling-else -Wno-unused-result -DLWS_NO_FORK -I/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/include wv.c -o ./wv.o
clang -g -target arm64-apple-darwin  -c -O -Wall -Wno-dangling-else -Wno-unused-result -DLWS_NO_FORK -I/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/include browserMessage.c -o ./browserMessage.o
clang -g -target arm64-apple-darwin  -c -O -Wall -Wno-dangling-else -Wno-unused-result -DLWS_NO_FORK -I/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/include fwv.c -o ./fwv.o
touch /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib/libwsserver.a
rm /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib/libwsserver.a
(cd .; ar rs /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib/libwsserver.a map.o base64-decode.o handshake.o client-handshake.o libwebsockets.o extension-deflate-stream.o md5.o extension-x-google-mux.o parsers.o extension.o sha-1.o server.o wv.o browserMessage.o \
		./fwv.o;  )
ar: creating archive /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib/libwsserver.a
clang -g -target arm64-apple-darwin  -c -O -Wall -Wno-dangling-else -Wno-unused-result -DLWS_NO_FORK -DSTANDALONE server.c \
		-I/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/include -I. -o ./servertest.o
clang++ -g -target arm64-apple-darwin  -o ./server ./servertest.o /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib/libwsserver.a  \
		-lpthread -lz -lm
touch /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib/libwsserver.dylib
rm /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib/libwsserver.dylib
(cd .; clang++ -g -target arm64-apple-darwin  -dynamiclib -o /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib/libwsserver.dylib \
		base64-decode.o handshake.o client-handshake.o libwebsockets.o extension-deflate-stream.o md5.o extension-x-google-mux.o parsers.o extension.o sha-1.o server.o wv.o browserMessage.o map.o -lz \
		-install_name '@rpath/libwsserver.dylib' \
		-compatibility_version 7.8 \
		-current_version 1.0.25 )
(cd EGADS/examples; make -f egads2cart.make)
clang -g -target arm64-apple-darwin  -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/include egads2cart.c \
		-o ./egads2cart.o
clang++ -g -target arm64-apple-darwin  -o /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/bin/egads2cart ./egads2cart.o -L/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib -legads \
		-rpath /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.8.0/./lib -lm
(cd EGADS/examples; make -f vCurvature.make)
clang -g -target arm64-apple-darwin  -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/include vCurvature.c -o ./vCurvature.o
clang++ -g -target arm64-apple-darwin  -o /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/bin/vCurvature ./vCurvature.o \
		-L/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib -lwsserver -legads -rpath /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.8.0/./lib
(cd EGADS/examples; make -f vGeom.make)
clang -g -target arm64-apple-darwin  -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/include vGeom.c -o ./vGeom.o
clang++ -g -target arm64-apple-darwin  -o /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/bin/vGeom ./vGeom.o -L/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib -lwsserver -legads \
		-rpath /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.8.0/./lib
(cd EGADS/examples; make -f vTess.make)
clang -g -target arm64-apple-darwin  -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/include vTess.c -o ./vTess.o
clang -g -target arm64-apple-darwin  -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/include ../util/retessFaces.c \
		-o ./retessFaces.o
clang++ -g -target arm64-apple-darwin  -o /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/bin/vTesstatic ./vTess.o ./retessFaces.o \
		-L/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib -lwsserver -legadstatic -L/Users/jenkins/util/ESP/OpenCASCADE-7.8.0/./lib -L/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib -lTKBool -lTKernel -lTKFeat -lTKBO -lTKGeomAlgo -lTKMath -lTKOffset -lTKPrim -lTKTopAlgo -lTKBRep -lTKG2d -lTKG3d -lTKGeomBase -lTKShHealing -lTKDESTEP -lTKDEIGES -lTKXSBase -lTKFillet \
		-lpthread -lz -rpath /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.8.0/./lib -lm
clang++ -g -target arm64-apple-darwin  -o /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/bin/vTess ./vTess.o ./retessFaces.o \
		-L/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib -lwsserver -legads -rpath /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.8.0/./lib
(cd OpenCSM; make)
clang -g -target arm64-apple-darwin  -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/include -I. serveCSM.c -o ./serveCSM.o
clang -g -target arm64-apple-darwin  -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/include -I. OpenCSM.c -o ./OpenCSM.o
clang -g -target arm64-apple-darwin  -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/include -I. udp.c -o ./udp.o
clang -g -target arm64-apple-darwin  -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/include -I. tim.c -o ./tim.o
touch /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib/libocsm.dylib
rm /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib/libocsm.dylib
clang -g -target arm64-apple-darwin  -dynamiclib -o /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib/libocsm.dylib ./OpenCSM.o ./udp.o ./tim.o -L/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib -legads -lwsserver -ldl -rpath /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.8.0/./lib -install_name '@rpath/libocsm.dylib' -compatibility_version 1.0.25 -current_version 1.0.25
clang++ -g -target arm64-apple-darwin  -o /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/bin/serveCSM ./serveCSM.o -L/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib -locsm -lwsserver -legads -ldl -rpath /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.8.0/./lib
clang -g -target arm64-apple-darwin  -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/include -I. serveESP.c -o ./serveESP.o
clang++ -g -target arm64-apple-darwin  -o /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/bin/serveESP ./serveESP.o -L/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib -locsm -lwsserver -legads -ldl -rpath /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.8.0/./lib
clang -g -target arm64-apple-darwin  -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/include -I. sensCSM.c -o ./sensCSM.o
clang -g -target arm64-apple-darwin  -o /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/bin/sensCSM ./sensCSM.o -L/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib -locsm -legads -rpath /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.8.0/./lib -lm
clang -g -target arm64-apple-darwin  -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/include -I. udpBezier.c -o ./udpBezier.o
touch /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib/bezier.so
rm /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib/bezier.so
clang -g -target arm64-apple-darwin  -bundle -o /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib/bezier.so ./udpBezier.o -L/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib -locsm -legads -lm
clang -g -target arm64-apple-darwin  -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/include -I. udpBiconvex.c -o ./udpBiconvex.o
touch /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib/biconvex.so
rm /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib/biconvex.so
clang -g -target arm64-apple-darwin  -bundle -o /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib/biconvex.so ./udpBiconvex.o -L/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib -locsm -legads -lm
clang -g -target arm64-apple-darwin  -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/include -I. udpBox.c -o ./udpBox.o
touch /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib/box.so
rm /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib/box.so
clang -g -target arm64-apple-darwin  -bundle -o /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib/box.so ./udpBox.o -L/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib -locsm -legads -lm
clang -g -target arm64-apple-darwin  -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/include -I. udpBspline.c -o ./udpBspline.o
touch /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib/bspline.so
rm /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib/bspline.so
clang -g -target arm64-apple-darwin  -bundle -o /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib/bspline.so ./udpBspline.o -L/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib -locsm -legads -lm
clang -g -target arm64-apple-darwin  -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/include -I. udfCatmull.c -o ./udfCatmull.o
touch /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib/catmull.so
rm /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib/catmull.so
clang -g -target arm64-apple-darwin  -bundle -o /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib/catmull.so ./udfCatmull.o -L/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib -locsm -legads -lm
clang -g -target arm64-apple-darwin  -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/include -I. udfCompare.c -o ./udfCompare.o
touch /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib/compare.so
rm /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib/compare.so
clang -g -target arm64-apple-darwin  -bundle -o /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib/compare.so ./udfCompare.o -L/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib -locsm -legads -lm
clang -g -target arm64-apple-darwin  -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/include -I. udfCreateBEM.c -o ./udfCreateBEM.o
touch /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib/createBEM.so
rm /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib/createBEM.so
clang -g -target arm64-apple-darwin  -bundle -o /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib/createBEM.so ./udfCreateBEM.o -L/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib -locsm -legads -lm
clang -g -target arm64-apple-darwin  -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/include -I. udfCreatePoly.c -o ./udfCreatePoly.o
touch /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib/createPoly.so
rm /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib/createPoly.so
clang -g -target arm64-apple-darwin  -bundle -o /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib/createPoly.so ./udfCreatePoly.o -L/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib -locsm -legads -lm
clang -g -target arm64-apple-darwin  -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/include -I. udpCsm.c -o ./udpCsm.o
touch /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib/csm.so
rm /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib/csm.so
clang -g -target arm64-apple-darwin  -bundle -o /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib/csm.so ./udpCsm.o -L/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib -locsm -legads -lm
clang -g -target arm64-apple-darwin  -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/include -I. udfDeform.c -o ./udfDeform.o
touch /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib/deform.so
rm /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib/deform.so
clang -g -target arm64-apple-darwin  -bundle -o /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib/deform.so ./udfDeform.o -L/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib -locsm -legads -lm
clang -g -target arm64-apple-darwin  -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/include -I. udfDroop.c -o ./udfDroop.o
touch /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib/droop.so
rm /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib/droop.so
clang -g -target arm64-apple-darwin  -bundle -o /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib/droop.so ./udfDroop.o -L/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib -locsm -legads -lm
clang -g -target arm64-apple-darwin  -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/include -I. udfDumpPmtrs.c -o ./udfDumpPmtrs.o
touch /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib/dumpPmtrs.so
rm /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib/dumpPmtrs.so
clang -g -target arm64-apple-darwin  -bundle -o /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib/dumpPmtrs.so ./udfDumpPmtrs.o -L/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib -locsm -legads -lm
clang -g -target arm64-apple-darwin  -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/include -I. udfEditAttr.c -o ./udfEditAttr.o
touch /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib/editAttr.so
rm /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib/editAttr.so
clang -g -target arm64-apple-darwin  -bundle -o /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib/editAttr.so ./udfEditAttr.o -L/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib -locsm -legads -lm
clang -g -target arm64-apple-darwin  -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/include -I. udpEllipse.c -o ./udpEllipse.o
touch /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib/ellipse.so
rm /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib/ellipse.so
clang -g -target arm64-apple-darwin  -bundle -o /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib/ellipse.so ./udpEllipse.o -L/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib -locsm -legads -lm
clang -g -target arm64-apple-darwin  -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/include -I. udpEqn2body.c -o ./udpEqn2body.o
touch /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib/eqn2body.so
rm /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib/eqn2body.so
clang -g -target arm64-apple-darwin  -bundle -o /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib/eqn2body.so ./udpEqn2body.o -L/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib -locsm -legads -lm
clang -g -target arm64-apple-darwin  -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/include -I. udpFitcurve.c -o ./udpFitcurve.o
touch /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib/fitcurve.so
rm /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib/fitcurve.so
clang -g -target arm64-apple-darwin  -bundle -o /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib/fitcurve.so ./udpFitcurve.o -L/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib -locsm -legads -lm
clang -g -target arm64-apple-darwin  -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/include -I. udfFlend.c -o ./udfFlend.o
touch /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib/flend.so
rm /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib/flend.so
clang -g -target arm64-apple-darwin  -bundle -o /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib/flend.so ./udfFlend.o -L/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib -locsm -legads -lm
clang -g -target arm64-apple-darwin  -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/include -I. udpFreeform.c -o ./udpFreeform.o
touch /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib/freeform.so
rm /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib/freeform.so
clang -g -target arm64-apple-darwin  -bundle -o /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib/freeform.so ./udpFreeform.o -L/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib -locsm -legads -lm
clang -g -target arm64-apple-darwin  -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/include -I. udfGanged.c -o ./udfGanged.o
touch /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib/ganged.so
rm /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib/ganged.so
clang -g -target arm64-apple-darwin  -bundle -o /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib/ganged.so ./udfGanged.o -L/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib -locsm -legads -lm
clang -g -target arm64-apple-darwin  -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/include -I. udfGuide.c -o ./udfGuide.o
touch /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib/guide.so
rm /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib/guide.so
clang -g -target arm64-apple-darwin  -bundle -o /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib/guide.so ./udfGuide.o -L/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib -locsm -legads -lm
clang -g -target arm64-apple-darwin  -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/include -I. udpHex.c -o ./udpHex.o
touch /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib/hex.so
rm /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib/hex.so
clang -g -target arm64-apple-darwin  -bundle -o /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib/hex.so ./udpHex.o -L/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib -locsm -legads -lm
clang -g -target arm64-apple-darwin  -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/include -I. udpImport.c -o ./udpImport.o
touch /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib/import.so
rm /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib/import.so
clang -g -target arm64-apple-darwin  -bundle -o /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib/import.so ./udpImport.o -L/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib -locsm -legads -lm
clang -g -target arm64-apple-darwin  -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/include -I. udpKulfan.c -o ./udpKulfan.o
touch /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib/kulfan.so
rm /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib/kulfan.so
clang -g -target arm64-apple-darwin  -bundle -o /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib/kulfan.so ./udpKulfan.o -L/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib -locsm -legads -lm
clang -g -target arm64-apple-darwin  -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/include -I. udfLinalg.c -o ./udfLinalg.o
touch /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib/linalg.so
rm /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib/linalg.so
clang -g -target arm64-apple-darwin  -bundle -o /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib/linalg.so ./udfLinalg.o -L/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib -locsm -legads -lm
clang -g -target arm64-apple-darwin  -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/include -I. udfMatchBodys.c -o ./udfMatchBodys.o
touch /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib/matchBodys.so
rm /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib/matchBodys.so
clang -g -target arm64-apple-darwin  -bundle -o /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib/matchBodys.so ./udfMatchBodys.o -L/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib -locsm -legads -lm
clang -g -target arm64-apple-darwin  -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/include -I. udfMechanism.c -o ./udfMechanism.o
touch /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib/mechanism.so
rm /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib/mechanism.so
clang -g -target arm64-apple-darwin  -bundle -o /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib/mechanism.so ./udfMechanism.o -L/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib -locsm -legads -lm
clang -g -target arm64-apple-darwin  -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/include -I. udpNaca.c -o ./udpNaca.o
touch /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib/naca.so
rm /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib/naca.so
clang -g -target arm64-apple-darwin  -bundle -o /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib/naca.so ./udpNaca.o -L/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib -locsm -legads -lm
clang -g -target arm64-apple-darwin  -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/include -I. udfNaca6mc.c -o ./udfNaca6mc.o
touch /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib/naca6mc.so
rm /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib/naca6mc.so
clang -g -target arm64-apple-darwin  -bundle -o /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib/naca6mc.so ./udfNaca6mc.o -L/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib -locsm -legads -lm
clang -g -target arm64-apple-darwin  -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/include -I. udfNacelle.c -o ./udfNacelle.o
touch /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib/nacelle.so
rm /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib/nacelle.so
clang -g -target arm64-apple-darwin  -bundle -o /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib/nacelle.so ./udfNacelle.o -L/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib -locsm -legads -lm
clang -g -target arm64-apple-darwin  -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/include -I. udpNurbbody.c -o ./udpNurbbody.o
touch /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib/nurbbody.so
rm /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib/nurbbody.so
clang -g -target arm64-apple-darwin  -bundle -o /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib/nurbbody.so ./udpNurbbody.o -L/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib -locsm -legads -lm
clang -g -target arm64-apple-darwin  -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/include -I. udfNuscale.c -o ./udfNuscale.o
touch /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib/nuscale.so
rm /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib/nuscale.so
clang -g -target arm64-apple-darwin  -bundle -o /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib/nuscale.so ./udfNuscale.o -L/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib -locsm -legads -lm
clang -g -target arm64-apple-darwin  -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/include -I. udfOffset.c -o ./udfOffset.o
touch /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib/offset.so
rm /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib/offset.so
clang -g -target arm64-apple-darwin  -bundle -o /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib/offset.so ./udfOffset.o -L/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib -locsm -legads -lm
clang -g -target arm64-apple-darwin  -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/include -I. udpParabaloid.c -o ./udpParabaloid.o
touch /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib/parabaloid.so
rm /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib/parabaloid.so
clang -g -target arm64-apple-darwin  -bundle -o /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib/parabaloid.so ./udpParabaloid.o -L/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib -locsm -legads -lm
clang++ -g -target arm64-apple-darwin  -c -O -fPIC -DOCC_CONVERT_SIGNALS -DNDEBUG -DNo_Exception -D_OCC64 -Wall -Wno-write-strings -Wno-dangling-else -Wno-unused-result -std=c++11 -ffp-model=strict -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/include -I. udpParsec.cpp -o ./udpParsec.o
touch /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib/parsec.so
rm /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib/parsec.so
clang++ -g -target arm64-apple-darwin  -bundle -o /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib/parsec.so ./udpParsec.o -L/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib -locsm -legads -lm
clang -g -target arm64-apple-darwin  -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/include -I. udpPod.c -o ./udpPod.o
touch /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib/pod.so
rm /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib/pod.so
clang -g -target arm64-apple-darwin  -bundle -o /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib/pod.so ./udpPod.o -L/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib -locsm -legads -lm
clang -g -target arm64-apple-darwin  -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/include -I. udpPoly.c -o ./udpPoly.o
touch /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib/poly.so
rm /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib/poly.so
clang -g -target arm64-apple-darwin  -bundle -o /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib/poly.so ./udpPoly.o -L/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib -locsm -legads -lm
clang -g -target arm64-apple-darwin  -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/include -I. udfPrintBbox.c -o ./udfPrintBbox.o
touch /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib/printBbox.so
rm /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib/printBbox.so
clang -g -target arm64-apple-darwin  -bundle -o /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib/printBbox.so ./udfPrintBbox.o -L/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib -locsm -legads -lm
clang -g -target arm64-apple-darwin  -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/include -I. udfPrintBrep.c -o ./udfPrintBrep.o
touch /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib/printBrep.so
rm /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib/printBrep.so
clang -g -target arm64-apple-darwin  -bundle -o /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib/printBrep.so ./udfPrintBrep.o -L/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib -locsm -legads -lm
clang -g -target arm64-apple-darwin  -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/include -I. udfPrintEgo.c -o ./udfPrintEgo.o
touch /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib/printEgo.so
rm /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib/printEgo.so
clang -g -target arm64-apple-darwin  -bundle -o /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib/printEgo.so ./udfPrintEgo.o -L/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib -locsm -legads -lm
clang -g -target arm64-apple-darwin  -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/include -I. udpProp.c -o ./udpProp.o
touch /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib/prop.so
rm /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib/prop.so
clang -g -target arm64-apple-darwin  -bundle -o /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib/prop.so ./udpProp.o -L/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib -locsm -legads -lm
clang -g -target arm64-apple-darwin  -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/include -I. udpRadwaf.c -o ./udpRadwaf.o
touch /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib/radwaf.so
rm /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib/radwaf.so
clang -g -target arm64-apple-darwin  -bundle -o /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib/radwaf.so ./udpRadwaf.o -L/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib -locsm -legads -lm
clang -g -target arm64-apple-darwin  -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/include -I. udpSample.c -o ./udpSample.o
touch /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib/sample.so
rm /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib/sample.so
clang -g -target arm64-apple-darwin  -bundle -o /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib/sample.so ./udpSample.o -L/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib -locsm -legads -lm
clang -g -target arm64-apple-darwin  -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/include -I. udpSew.c -o ./udpSew.o
touch /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib/sew.so
rm /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib/sew.so
clang -g -target arm64-apple-darwin  -bundle -o /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib/sew.so ./udpSew.o -L/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib -locsm -legads -lm
clang -g -target arm64-apple-darwin  -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/include -I. udfShadow.c -o ./udfShadow.o
touch /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib/shadow.so
rm /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib/shadow.so
clang -g -target arm64-apple-darwin  -bundle -o /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib/shadow.so ./udfShadow.o -L/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib -locsm -legads -lm
clang -g -target arm64-apple-darwin  -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/include -I. udfSlices.c -o ./udfSlices.o
touch /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib/slices.so
rm /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib/slices.so
clang -g -target arm64-apple-darwin  -bundle -o /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib/slices.so ./udfSlices.o -L/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib -locsm -legads -lm
clang -g -target arm64-apple-darwin  -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/include -I. udpStag.c -o ./udpStag.o
touch /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib/stag.so
rm /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib/stag.so
clang -g -target arm64-apple-darwin  -bundle -o /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib/stag.so ./udpStag.o -L/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib -locsm -legads -lm
clang -g -target arm64-apple-darwin  -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/include -I. udfStiffener.c -o ./udfStiffener.o
touch /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib/stiffener.so
rm /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib/stiffener.so
clang -g -target arm64-apple-darwin  -bundle -o /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib/stiffener.so ./udfStiffener.o -L/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib -locsm -legads -lm
clang -g -target arm64-apple-darwin  -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/include -I. udpSupell.c -o ./udpSupell.o
touch /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib/supell.so
rm /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib/supell.so
clang -g -target arm64-apple-darwin  -bundle -o /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib/supell.so ./udpSupell.o -L/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib -locsm -legads -lm
clang -g -target arm64-apple-darwin  -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/include -I. udfTester1.c -o ./udfTester1.o
touch /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib/tester1.so
rm /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib/tester1.so
clang -g -target arm64-apple-darwin  -bundle -o /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib/tester1.so ./udfTester1.o -L/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib -locsm -legads -lm
clang -g -target arm64-apple-darwin  -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/include -I. udpTester2.c -o ./udpTester2.o
touch /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib/tester2.so
rm /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib/tester2.so
clang -g -target arm64-apple-darwin  -bundle -o /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib/tester2.so ./udpTester2.o -L/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib -locsm -legads -lm
clang -g -target arm64-apple-darwin  -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/include -I. udpVsp3.c -o ./udpVsp3.o
touch /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib/vsp3.so
rm /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib/vsp3.so
clang -g -target arm64-apple-darwin  -bundle -o /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib/vsp3.so ./udpVsp3.o -L/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib -locsm -legads -lm
clang -g -target arm64-apple-darwin  -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/include -I. udpWaffle.c -o ./udpWaffle.o
touch /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib/waffle.so
rm /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib/waffle.so
clang -g -target arm64-apple-darwin  -bundle -o /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib/waffle.so ./udpWaffle.o -L/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib -locsm -legads -lm
clang -g -target arm64-apple-darwin  -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/include -I. udpWarp.c -o ./udpWarp.o
touch /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib/warp.so
rm /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib/warp.so
clang -g -target arm64-apple-darwin  -bundle -o /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib/warp.so ./udpWarp.o -L/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib -locsm -legads -lm
clang -g -target arm64-apple-darwin  -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/include -I. eggPDT2.c -o ./eggPDT2.o
touch /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib/PDT2.so
rm /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib/PDT2.so
clang -g -target arm64-apple-darwin  -bundle -o /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib/PDT2.so ./eggPDT2.o -L/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib -legads -lm
clang -g -target arm64-apple-darwin  -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/include -I. udpNaca456.c -o ./udpNaca456.o
gfortran -g  -c -O -frecursive -fcray-pointer naca456.f90 -o ./naca456.o -J .
touch /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib/naca456.so
rm /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib/naca456.so
gfortran -g  -bundle -o /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib/naca456.so ./udpNaca456.o ./naca456.o -L/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib -locsm -legads -lm -static-libgfortran -static-libgcc -Wl,-w
clang -g -target arm64-apple-darwin  -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/include -I. timEreped.c -o ./timEreped.o
touch /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib/ereped.so
rm /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib/ereped.so
clang++ -g -target arm64-apple-darwin  -bundle -o /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib/ereped.so ./timEreped.o -L/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib -locsm -lwsserver -legads -ldl -lm
clang -g -target arm64-apple-darwin  -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/include -I. timMitten.c -o ./timMitten.o
touch /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib/mitten.so
rm /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib/mitten.so
clang++ -g -target arm64-apple-darwin  -bundle -o /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib/mitten.so ./timMitten.o -L/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib -locsm -lwsserver -legads -ldl -rpath /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.8.0/./lib
clang -g -target arm64-apple-darwin  -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/include -I. timPlotter.c -o ./timPlotter.o
touch /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib/plotter.so
rm /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib/plotter.so
clang++ -g -target arm64-apple-darwin  -bundle -o /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib/plotter.so ./timPlotter.o -L/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib -locsm -lwsserver -legads -ldl -rpath /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.8.0/./lib
clang -g -target arm64-apple-darwin  -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/include -I. timPlugs.c -o ./timPlugs.o
touch /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib/plugs.so
rm /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib/plugs.so
clang++ -g -target arm64-apple-darwin  -bundle -o /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib/plugs.so ./timPlugs.o -L/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib -locsm -lwsserver -legads -ldl -rpath /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.8.0/./lib
clang -g -target arm64-apple-darwin  -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/include -I. timSlugs.c -o ./timSlugs.o
touch /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib/slugs.so
rm /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib/slugs.so
clang++ -g -target arm64-apple-darwin  -bundle -o /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib/slugs.so ./timSlugs.o -L/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib -locsm -lwsserver -legads -ldl -lm
clang -g -target arm64-apple-darwin  -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/include -I. timVspSetup.c -o ./timVspSetup.o
touch /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib/vspSetup.so
rm /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib/vspSetup.so
clang++ -g -target arm64-apple-darwin  -bundle -o /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib/vspSetup.so ./timVspSetup.o -L/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib -locsm -lwsserver -legads -ldl -lm
touch /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/include/OpenCSM.h
rm /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/include/OpenCSM.h
cp -p OpenCSM.h /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/include/OpenCSM.h
touch /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/include/common.h
rm /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/include/common.h
cp -p common.h /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/include/common.h
touch /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/include/udp.h
rm /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/include/udp.h
cp -p udp.h /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/include/udp.h
touch /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/include/esp.h
rm /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/include/esp.h
cp -p esp.h /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/include/esp.h
touch /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/include/tim.h
rm /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/include/tim.h
cp -p tim.h /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/include/tim.h
touch /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/include/egg.h
rm /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/include/egg.h
cp -p egg.h /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/include/egg.h
touch /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/include/udpUtilities.h
rm /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/include/udpUtilities.h
cp -p udpUtilities.h /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/include/udpUtilities.h
touch /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/include/udpUtilities.c
rm /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/include/udpUtilities.c
cp -p udpUtilities.c /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/include/udpUtilities.c
(cd Slugs; make)
clang -g -target arm64-apple-darwin  -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/include -I. Slugs.c -o ./Slugs.o
clang -g -target arm64-apple-darwin  -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/include -I. Fitter.c \
		-o ./Fitter.o
clang -g -target arm64-apple-darwin  -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/include -I. RedBlackTree.c \
		-o ./RedBlackTree.o
clang -g -target arm64-apple-darwin  -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/include -I. Tessellate.c \
		-o ./Tessellate.o
clang++ -g -target arm64-apple-darwin  -o /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/bin/Slugs ./Slugs.o ./Fitter.o ./RedBlackTree.o \
		./Tessellate.o -rpath /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.8.0/./lib -L/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib -lwsserver -legads \
		-lpthread -lz -lm
clang -g -target arm64-apple-darwin  -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/include -I. TestFit.c -o ./TestFit.o
clang++ -g -target arm64-apple-darwin  -o /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/bin/TestFit ./TestFit.o ./Fitter.o -rpath /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.8.0/./lib -L/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib -legads \
		-lpthread -lz -lm
(cd CAPS; make)
/bin/cp Cart3D/M1_CLANG/libc3dio.a /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib/libc3dio.a
/bin/cp Cart3D/M1_CLANG/libCart3D.a /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib/libCart3D.a
/bin/cp Executables/DARWIN_ARM64/avl /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/bin/avl
/bin/cp Executables/DARWIN_ARM64/pplot /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/bin/pplot
/bin/cp Executables/DARWIN_ARM64/pxplot /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/bin/pxplot
/bin/cp Executables/DARWIN_ARM64/xfoil /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/bin/xfoil
/bin/cp Executables/DARWIN_ARM64/mastros.exe /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/bin/mastros.exe
/bin/cp Executables/DARWIN_ARM64/ASTRO.D01 /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/bin/ASTRO.D01
/bin/cp Executables/DARWIN_ARM64/ASTRO.IDX /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/bin/ASTRO.IDX
/bin/cp Executables/DARWIN_ARM64/mses /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/bin/mses
/bin/cp Executables/DARWIN_ARM64/mset /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/bin/mset
/bin/cp udunits/include/*.h /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/include
/bin/cp udunits/DARWIN_ARM64/libudunits2.0.dylib /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib
/bin/ln -sf libudunits2.0.dylib /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib/libudunits2.dylib
/bin/cp Libraries/DARWIN_ARM64/aflr2AIM.so /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib/aflr2AIM.so
/bin/cp Libraries/DARWIN_ARM64/aflr3AIM.so /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib/aflr3AIM.so
/bin/cp Libraries/DARWIN_ARM64/aflr4AIM.so /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib/aflr4AIM.so
(cd CAPS/src; make)
touch /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/include/caps.h
rm /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/include/caps.h
cp -p ../include/caps.h /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/include/caps.h
touch /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/include/capsErrors.h
rm /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/include/capsErrors.h
cp -p ../include/capsErrors.h /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/include/capsErrors.h
touch /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/include/capsTypes.h
rm /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/include/capsTypes.h
cp -p ../include/capsTypes.h /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/include/capsTypes.h
touch /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/include/aimUtil.h
rm /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/include/aimUtil.h
cp -p ../include/aimUtil.h /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/include/aimUtil.h
touch /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/include/aimMesh.h
rm /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/include/aimMesh.h
cp -p ../include/aimMesh.h /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/include/aimMesh.h
clang -g -target arm64-apple-darwin  -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/include -I../include \
		-I/usr/include/udunits2 aimUtil.c -o ./aimUtil.o
clang -g -target arm64-apple-darwin  -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I../include -I/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/include \
		-I/usr/include/udunits2 aimTransferUtil.c \
		-o ./aimTransferUtil.o
clang -g -target arm64-apple-darwin  -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/include -I../include \
		aimMesh.c -o ./aimMesh.o
touch /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib/libaimUtil.a
rm /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib/libaimUtil.a
ar -rs /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib/libaimUtil.a ./aimUtil.o ./aimMesh.o \
		./aimTransferUtil.o 
ar: creating archive /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib/libaimUtil.a
clang -g -target arm64-apple-darwin  -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I../include -I/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/include -I. \
		-I/usr/include/udunits2 capsBase.c -o ./capsBase.o
clang -g -target arm64-apple-darwin  -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I../include -I/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/include -I. \
		-I/usr/include/udunits2 capsAnalysis.c -o ./capsAnalysis.o
clang -g -target arm64-apple-darwin  -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I../include -I/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/include -I. \
		-I/usr/include/udunits2 capsApprox.c -o ./capsApprox.o
clang -g -target arm64-apple-darwin  -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I../include -I/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/include -I. \
		-I/usr/include/udunits2 capsAttr.c -o ./capsAttr.o
clang -g -target arm64-apple-darwin  -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I../include -I/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/include -I. \
		-I/usr/include/udunits2 capsAIM.c -o ./capsAIM.o
clang -g -target arm64-apple-darwin  -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I../include -I/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/include -I. \
		-I/usr/include/udunits2 capsBound.c -o ./capsBound.o
clang -g -target arm64-apple-darwin  -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I../include -I/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/include -I. \
		-I/usr/include/udunits2 capsProblem.c -o ./capsProblem.o
clang -g -target arm64-apple-darwin  -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I../include -I/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/include -I. \
		-I/usr/include/udunits2 capsValue.c -o ./capsValue.o
clang -g -target arm64-apple-darwin  -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I../include -I/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/include -I. \
		-I/usr/include/udunits2 capsUnits.c -o ./capsUnits.o
clang -g -target arm64-apple-darwin  -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I../include -I/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/include -I. \
		-I/usr/include/udunits2 conjGrad.c -o ./conjGrad.o
clang -g -target arm64-apple-darwin  -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I../include -I/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/include -I. \
		-I/usr/include/udunits2 capsFunIDs.c -o ./capsFunIDs.o
clang -g -target arm64-apple-darwin  -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I../include -I/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/include -I. \
		-I/usr/include/udunits2 capsChkInpt.c -o ./capsChkInpt.o
clang -g -target arm64-apple-darwin  -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I../include -I/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/include -I. \
		-I/usr/include/udunits2 printObject.c -o ./printObject.o
touch /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib/libcaps.dylib
rm /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib/libcaps.dylib
(cd .; clang -g -target arm64-apple-darwin  -dynamiclib -o /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib/libcaps.dylib capsBase.o   capsAnalysis.o capsApprox.o capsAttr.o  capsAIM.o capsBound.o  capsProblem.o  capsValue.o  capsUnits.o conjGrad.o capsFunIDs.o capsChkInpt.o  printObject.o \
			-rpath /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.8.0/./lib -L/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib -ludunits2 -locsm -legads -ldl \
			-install_name '@rpath/libcaps.dylib' \
			-compatibility_version 1.0.25 \
			-current_version 1.0.25 )
touch /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib/libcapsstatic.a
rm /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib/libcapsstatic.a
(cd .; ar -rs /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib/libcapsstatic.a capsBase.o   capsAnalysis.o capsApprox.o capsAttr.o  capsAIM.o capsBound.o  capsProblem.o  capsValue.o  capsUnits.o conjGrad.o capsFunIDs.o capsChkInpt.o  printObject.o )
ar: creating archive /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib/libcapsstatic.a
clang -g -target arm64-apple-darwin  -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I../include -I/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/include testingAIM.c \
		-o ./testingAIM.o
rm /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib/testingAIM.so
rm: /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib/testingAIM.so: No such file or directory
make[1]: [/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib/testingAIM.so] Error 1 (ignored)
clang -g -target arm64-apple-darwin  -bundle -o /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib/testingAIM.so ./testingAIM.o \
		-L/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib -laimUtil -legads -locsm -ludunits2 -ldl -rpath /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.8.0/./lib -lm
clang -g -target arm64-apple-darwin  -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I../include -I/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/include testingWriter.c \
		-o ./testingWriter.o
rm /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib/testingWriter.so
rm: /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib/testingWriter.so: No such file or directory
make[1]: [/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib/testingWriter.so] Error 1 (ignored)
clang -g -target arm64-apple-darwin  -bundle -o /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib/testingWriter.so ./testingWriter.o \
		-L/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib -laimUtil -ldl -rpath /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.8.0/./lib -lm
clang -g -target arm64-apple-darwin  -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I../include -I/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/include phaseUtil.c \
		-o ./phaseUtil.o
clang -g -target arm64-apple-darwin  -o /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/bin/phaseUtil ./phaseUtil.o \
	-L/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib -lcaps -ludunits2 -locsm -legads -ldl -rpath /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.8.0/./lib -lm
(cd ../CAPSexamples; make)
(make -C cCAPS -f aeroelastic_SU2.make)
clang -g -target arm64-apple-darwin  -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/include aeroelasticSimple_Iterative_SU2_and_MystranTest.c -o ./aeroelasticSimple_Iterative_SU2_and_MystranTest.o
clang -g -target arm64-apple-darwin  -o ./aeroelasticSimple_Iterative_SU2_and_MystranTest ./aeroelasticSimple_Iterative_SU2_and_MystranTest.o -L/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib -lcaps -locsm -legads \
		-ludunits2 -rpath /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.8.0/./lib -lm -ldl
(make -C cCAPS -f avlTest.make)
clang -g -target arm64-apple-darwin  -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/include avlTest.c -o ./avlTest.o
clang -g -target arm64-apple-darwin  -o ./avlTest ./avlTest.o -L/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib -lcaps -legads -locsm \
		-ludunits2 -rpath /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.8.0/./lib -lm -ldl
(make -C cCAPS -f awaveTest.make)
clang -g -target arm64-apple-darwin  -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/include awaveTest.c -o ./awaveTest.o
clang -g -target arm64-apple-darwin  -o ./awaveTest ./awaveTest.o -L/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib -lcaps -legads -locsm \
		-ludunits2 -rpath /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.8.0/./lib -lm -ldl
(make -C cCAPS -f frictionTest.make)
clang -g -target arm64-apple-darwin  -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/include frictionTest.c -o ./frictionTest.o
clang -g -target arm64-apple-darwin  -o ./frictionTest ./frictionTest.o -L/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib -lcaps -locsm -legads \
		-ludunits2 -rpath /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.8.0/./lib -lm -ldl
(make -C cCAPS -f fun3d.make)
clang -g -target arm64-apple-darwin  -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/include fun3dAFLR2Test.c -o ./fun3dAFLR2Test.o
clang -g -target arm64-apple-darwin  -o ./fun3dAFLR2Test ./fun3dAFLR2Test.o \
	-L/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib -lcaps -locsm -legads -ludunits2 -rpath /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.8.0/./lib -lm -ldl
clang -g -target arm64-apple-darwin  -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/include fun3dTetgenTest.c -o ./fun3dTetgenTest.o
clang -g -target arm64-apple-darwin  -o ./fun3dTetgenTest ./fun3dTetgenTest.o \
	-L/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib -lcaps -locsm -legads -ludunits2 -rpath /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.8.0/./lib -lm -ldl
clang -g -target arm64-apple-darwin  -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/include aeroelasticTest.c -o ./aeroelasticTest.o
clang -g -target arm64-apple-darwin  -o ./aeroelasticTest ./aeroelasticTest.o \
	-L/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib -lcaps -locsm -legads -ludunits2 -rpath /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.8.0/./lib -lm -ldl
(make -C cCAPS -f hsm.make)
clang -g -target arm64-apple-darwin  -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/include hsmTest.c -o ./hsmTest.o   
clang -g -target arm64-apple-darwin  -o ./hsmTest ./hsmTest.o \
		-L/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib -lcaps -locsm -legads -ludunits2 -rpath /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.8.0/./lib -lm -ldl
clang -g -target arm64-apple-darwin  -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/include hsmSimplePlateTest.c -o ./hsmSimplePlateTest.o  
clang -g -target arm64-apple-darwin  -o ./hsmSimplePlateTest ./hsmSimplePlateTest.o \
		-L/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib -lcaps -locsm -legads -ludunits2 -rpath /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.8.0/./lib -lm -ldl
clang -g -target arm64-apple-darwin  -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/include hsmCantileverPlateTest.c -o ./hsmCantileverPlateTest.o  
clang -g -target arm64-apple-darwin  -o ./hsmCantileverPlateTest ./hsmCantileverPlateTest.o \
		-L/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib -lcaps -locsm -legads -ludunits2 -rpath /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.8.0/./lib -lm -ldl
clang -g -target arm64-apple-darwin  -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/include hsmJoinedPlateTest.c -o ./hsmJoinedPlateTest.o  
clang -g -target arm64-apple-darwin  -o ./hsmJoinedPlateTest ./hsmJoinedPlateTest.o \
		-L/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib -lcaps -locsm -legads -ludunits2 -rpath /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.8.0/./lib -lm -ldl
(make -C cCAPS -f interferenceTest.make)
clang -g -target arm64-apple-darwin  -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/include interferenceTest.c \
		-o ./interferenceTest.o   
clang -g -target arm64-apple-darwin  -o ./interferenceTest ./interferenceTest.o \
		-L/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib -lcaps -locsm -legads -ludunits2 -rpath /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.8.0/./lib -lm -ldl
(make -C cCAPS -f msesTest.make)
clang -g -target arm64-apple-darwin  -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/include msesTest.c -o ./msesTest.o
clang -g -target arm64-apple-darwin  -o ./msesTest ./msesTest.o -L/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib -lcaps -legads -locsm \
		-ludunits2 -rpath /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.8.0/./lib -lm -ldl
(make -C cCAPS -f mystran.make)
clang -g -target arm64-apple-darwin  -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/include mystranTest.c -o ./mystranTest.o   
clang -g -target arm64-apple-darwin  -o ./mystranTest ./mystranTest.o \
		-L/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib -lcaps -locsm -legads -ludunits2 -rpath /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.8.0/./lib -lm -ldl
(make -C cCAPS -f pointwiseTest.make)
clang -g -target arm64-apple-darwin  -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/include pointwiseTest.c -o ./pointwiseTest.o
clang -g -target arm64-apple-darwin  -o ./pointwiseTest ./pointwiseTest.o -L/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib -lcaps -locsm -legads \
		-ludunits2 -rpath /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.8.0/./lib -lm -ldl
(cd CAPS/aim; make)
/Library/Developer/CommandLineTools/usr/bin/make -C utils
clang -g -target arm64-apple-darwin  -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I../include -I/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/include -I. -DHAVE_PYTHON -I/Users/jenkins/util/ESP/Python/ESP_Python-3.11.9/include/python3.11 -Icython attrUtils.c -o ./attrUtils.o
clang -g -target arm64-apple-darwin  -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I../include -I/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/include -I. -DHAVE_PYTHON -I/Users/jenkins/util/ESP/Python/ESP_Python-3.11.9/include/python3.11 -Icython meshUtils.c -o ./meshUtils.o
clang -g -target arm64-apple-darwin  -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I../include -I/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/include -I. -DHAVE_PYTHON -I/Users/jenkins/util/ESP/Python/ESP_Python-3.11.9/include/python3.11 -Icython cfdUtils.c -o ./cfdUtils.o
clang -g -target arm64-apple-darwin  -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I../include -I/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/include -I. -DHAVE_PYTHON -I/Users/jenkins/util/ESP/Python/ESP_Python-3.11.9/include/python3.11 -Icython miscUtils.c -o ./miscUtils.o
clang -g -target arm64-apple-darwin  -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I../include -I/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/include -I. -DHAVE_PYTHON -I/Users/jenkins/util/ESP/Python/ESP_Python-3.11.9/include/python3.11 -Icython feaUtils.c -o ./feaUtils.o
clang -g -target arm64-apple-darwin  -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I../include -I/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/include -I. -DHAVE_PYTHON -I/Users/jenkins/util/ESP/Python/ESP_Python-3.11.9/include/python3.11 -Icython vlmUtils.c -o ./vlmUtils.o
clang -g -target arm64-apple-darwin  -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I../include -I/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/include -I. -DHAVE_PYTHON -I/Users/jenkins/util/ESP/Python/ESP_Python-3.11.9/include/python3.11 -Icython nastranUtils.c -o ./nastranUtils.o
clang -g -target arm64-apple-darwin  -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I../include -I/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/include -I. -DHAVE_PYTHON -I/Users/jenkins/util/ESP/Python/ESP_Python-3.11.9/include/python3.11 -Icython tecplotUtils.c -o ./tecplotUtils.o
clang -g -target arm64-apple-darwin  -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I../include -I/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/include -I. -DHAVE_PYTHON -I/Users/jenkins/util/ESP/Python/ESP_Python-3.11.9/include/python3.11 -Icython arrayUtils.c -o ./arrayUtils.o
clang -g -target arm64-apple-darwin  -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I../include -I/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/include -I. -DHAVE_PYTHON -I/Users/jenkins/util/ESP/Python/ESP_Python-3.11.9/include/python3.11 -Icython deprecateUtils.c -o ./deprecateUtils.o
clang -g -target arm64-apple-darwin  -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I../include -I/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/include -I. -DHAVE_PYTHON -I/Users/jenkins/util/ESP/Python/ESP_Python-3.11.9/include/python3.11 -Icython cardUtils.c -o ./cardUtils.o
clang -g -target arm64-apple-darwin  -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I../include -I/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/include -I. -DHAVE_PYTHON -I/Users/jenkins/util/ESP/Python/ESP_Python-3.11.9/include/python3.11 -Icython nastranCards.c -o ./nastranCards.o
clang -g -target arm64-apple-darwin  -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I../include -I/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/include -I. -DHAVE_PYTHON -I/Users/jenkins/util/ESP/Python/ESP_Python-3.11.9/include/python3.11 -Icython jsonUtils.c -o ./jsonUtils.o
clang -g -target arm64-apple-darwin  -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I../include -I/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/include -I. -DHAVE_PYTHON -I/Users/jenkins/util/ESP/Python/ESP_Python-3.11.9/include/python3.11 -Icython cython/nastranOP2Reader.c -o ./nastranOP2Reader.o
clang++ -g -target arm64-apple-darwin  -c -O -fPIC -DOCC_CONVERT_SIGNALS -DNDEBUG -DNo_Exception -D_OCC64 -Wall -Wno-write-strings -Wno-dangling-else -Wno-unused-result -std=c++11 -ffp-model=strict -DREVISION=7.8 -I../include -I/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/include -I. vlmSpanSpace.cpp -o ./vlmSpanSpace.o
touch /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib/libutils.a
rm /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib/libutils.a
(cd .; ar -rs /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib/libutils.a attrUtils.o meshUtils.o cfdUtils.o miscUtils.o feaUtils.o vlmUtils.o nastranUtils.o tecplotUtils.o arrayUtils.o deprecateUtils.o cardUtils.o nastranCards.o jsonUtils.o nastranOP2Reader.o vlmSpanSpace.o )
ar: creating archive /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib/libutils.a
mkdir -p /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/include/aim/utils
cp -p -f arrayUtils.h /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/include/aim/utils/arrayUtils.h
cp -p -f attrTypes.h /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/include/aim/utils/attrTypes.h
cp -p -f attrUtils.h /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/include/aim/utils/attrUtils.h
cp -p -f cardTypes.h /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/include/aim/utils/cardTypes.h
cp -p -f cardUtils.h /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/include/aim/utils/cardUtils.h
cp -p -f cfdTypes.h /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/include/aim/utils/cfdTypes.h
cp -p -f cfdUtils.h /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/include/aim/utils/cfdUtils.h
cp -p -f deprecateUtils.h /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/include/aim/utils/deprecateUtils.h
cp -p -f feaTypes.h /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/include/aim/utils/feaTypes.h
cp -p -f feaUtils.h /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/include/aim/utils/feaUtils.h
cp -p -f jsonUtils.h /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/include/aim/utils/jsonUtils.h
cp -p -f meshTypes.h /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/include/aim/utils/meshTypes.h
cp -p -f meshUtils.h /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/include/aim/utils/meshUtils.h
cp -p -f miscTypes.h /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/include/aim/utils/miscTypes.h
cp -p -f miscUtils.h /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/include/aim/utils/miscUtils.h
cp -p -f nastranCards.h /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/include/aim/utils/nastranCards.h
cp -p -f nastranUtils.h /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/include/aim/utils/nastranUtils.h
cp -p -f tecplotUtils.h /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/include/aim/utils/tecplotUtils.h
cp -p -f vlmSpanSpace.h /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/include/aim/utils/vlmSpanSpace.h
cp -p -f vlmTypes.h /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/include/aim/utils/vlmTypes.h
cp -p -f vlmUtils.h /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/include/aim/utils/vlmUtils.h
/Library/Developer/CommandLineTools/usr/bin/make -C abaqus 
clang -g -target arm64-apple-darwin  -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/include -I../utils \
		abaqusAIM.c -o ./abaqusAIM.o
clang -g -target arm64-apple-darwin  -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -DHAVE_PYTHON -I/Users/jenkins/util/ESP/Python/ESP_Python-3.11.9/include/python3.11 -Icython -I/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/include -I../utils \
		abaqusUtils.c -o ./abaqusUtils.o
clang -g -target arm64-apple-darwin  -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/include -I../utils \
		-I/Users/jenkins/util/ESP/Python/ESP_Python-3.11.9/include/python3.11 cython/abaqusFILReader.c -o ./abaqusFILReader.o
echo "Building Abaqus with Python"
Building Abaqus with Python
clang -g -target arm64-apple-darwin  -bundle -o /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib/abaqusAIM.so ./abaqusAIM.o ./abaqusUtils.o ./abaqusFILReader.o \
		-L/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib -lutils -laimUtil -locsm -legads -ludunits2 -L/Users/jenkins/util/ESP/Python/ESP_Python-3.11.9/lib -lpython3.11 -lm -ldl -Wl,-rpath /Users/jenkins/util/ESP/Python/ESP_Python-3.11.9/lib
/Library/Developer/CommandLineTools/usr/bin/make -C aflr2 
Not compiling aflr2AIM: AFLR must be set -- Please fix the environment....
/Library/Developer/CommandLineTools/usr/bin/make -C aflr3 
Not compiling aflr3AIM: AFLR must be set -- Please fix the environment....
/Library/Developer/CommandLineTools/usr/bin/make -C aflr4 
Not compiling aflr4AIM: AFLR must be set -- Please fix the environment....
/Library/Developer/CommandLineTools/usr/bin/make -C astros 
clang -g -target arm64-apple-darwin  -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/include -I../utils astrosAIM.c \
		-o ./astrosAIM.o
clang -g -target arm64-apple-darwin  -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/include -I../utils astrosUtils.c \
		-o ./astrosUtils.o
clang -g -target arm64-apple-darwin  -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/include -I../utils astrosCards.c \
        -o ./astrosCards.o
clang -g -target arm64-apple-darwin  -bundle -o /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib/astrosAIM.so ./astrosAIM.o  ./astrosUtils.o ./astrosCards.o \
		-L/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib -lutils -laimUtil -locsm -legads -ludunits2 -ldl -lm -L/Users/jenkins/util/ESP/Python/ESP_Python-3.11.9/lib -lpython3.11
/Library/Developer/CommandLineTools/usr/bin/make -C avl 
clang -g -target arm64-apple-darwin  -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/include -I../utils avlAIM.c -o ./avlAIM.o
clang -g -target arm64-apple-darwin  -c -O -Wall -Wno-dangling-else -Wno-unused-result -Wno-unused-function -Iavlmrf avlmrf/avlRead_BODY.c -o avlRead_BODY.o
clang -g -target arm64-apple-darwin  -c -O -Wall -Wno-dangling-else -Wno-unused-result -Wno-unused-function -Iavlmrf avlmrf/avlRead_CNC.c -o avlRead_CNC.o
clang -g -target arm64-apple-darwin  -c -O -Wall -Wno-dangling-else -Wno-unused-result -Wno-unused-function -Iavlmrf avlmrf/avlRead_CPOML.c -o avlRead_CPOML.o
clang -g -target arm64-apple-darwin  -c -O -Wall -Wno-dangling-else -Wno-unused-result -Wno-unused-function -Iavlmrf avlmrf/avlRead_DERMATB.c -o avlRead_DERMATB.o
clang -g -target arm64-apple-darwin  -c -O -Wall -Wno-dangling-else -Wno-unused-result -Wno-unused-function -Iavlmrf avlmrf/avlRead_DERMATM.c -o avlRead_DERMATM.o
clang -g -target arm64-apple-darwin  -c -O -Wall -Wno-dangling-else -Wno-unused-result -Wno-unused-function -Iavlmrf avlmrf/avlRead_DERMATS.c -o avlRead_DERMATS.o
clang -g -target arm64-apple-darwin  -c -O -Wall -Wno-dangling-else -Wno-unused-result -Wno-unused-function -Iavlmrf avlmrf/avlRead_ELE.c -o avlRead_ELE.o
clang -g -target arm64-apple-darwin  -c -O -Wall -Wno-dangling-else -Wno-unused-result -Wno-unused-function -Iavlmrf avlmrf/avlRead_HINGE.c -o avlRead_HINGE.o
clang -g -target arm64-apple-darwin  -c -O -Wall -Wno-dangling-else -Wno-unused-result -Wno-unused-function -Iavlmrf avlmrf/avlRead_STRP.c -o avlRead_STRP.o
clang -g -target arm64-apple-darwin  -c -O -Wall -Wno-dangling-else -Wno-unused-result -Wno-unused-function -Iavlmrf avlmrf/avlRead_SURF.c -o avlRead_SURF.o
clang -g -target arm64-apple-darwin  -c -O -Wall -Wno-dangling-else -Wno-unused-result -Wno-unused-function -Iavlmrf avlmrf/avlRead_TOT.c -o avlRead_TOT.o
clang -g -target arm64-apple-darwin  -c -O -Wall -Wno-dangling-else -Wno-unused-result -Wno-unused-function -Iavlmrf avlmrf/avlRead_VM.c -o avlRead_VM.o
touch /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib/avlAIM.so
rm /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib/avlAIM.so
clang -g -target arm64-apple-darwin  -bundle -o /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib/avlAIM.so ./avlAIM.o ./avlRead_BODY.o ./avlRead_CNC.o ./avlRead_CPOML.o ./avlRead_DERMATB.o ./avlRead_DERMATM.o ./avlRead_DERMATS.o ./avlRead_ELE.o ./avlRead_HINGE.o ./avlRead_STRP.o ./avlRead_SURF.o ./avlRead_TOT.o ./avlRead_VM.o \
		-L/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib -laimUtil -lutils -locsm -legads -ludunits2 -ldl \
		-lc++ -rpath /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.8.0/./lib -lm
/Library/Developer/CommandLineTools/usr/bin/make -C awave 
clang -g -target arm64-apple-darwin  -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/include -I../utils awaveAIM.c \
		-o ./awaveAIM.o
clang -g -target arm64-apple-darwin  -bundle -o /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib/awaveAIM.so ./awaveAIM.o \
		-L/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib -lutils -laimUtil -locsm -legads -ludunits2 -ldl -lm
/Library/Developer/CommandLineTools/usr/bin/make -C cart3d 
clang -g -target arm64-apple-darwin  -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -DCAPS_MESHUTILS -I/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/include -I../utils -I/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/include/libCart3D -I./xddm \
		cart3dAIM.c -o ./cart3dAIM.o
clang -g -target arm64-apple-darwin  -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/include -I/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/include/c3dio \
		-I/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/include/libCart3D -I./xddm \
		writeTrix.c -o ./writeTrix.o
clang -g -target arm64-apple-darwin  -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/include -I/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/include/c3dio \
		-I/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/include/libCart3D \
		surfTrix.c -o ./surfTrix.o
clang -g -target arm64-apple-darwin  -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -pedantic -I./xddm -I. \
		`xml2-config --cflags` ./xddm/xddm.c \
		 -o ./xddm.o
clang -g -target arm64-apple-darwin  -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/include bodyTess.c -o ./bodyTess.o
clang -g -target arm64-apple-darwin  -bundle -o /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib/cart3dAIM.so ./cart3dAIM.o \
		./writeTrix.o ./surfTrix.o ./xddm.o ./bodyTess.o -L/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib -lutils \
		-laimUtil -locsm -legads -ludunits2 -L/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/include/ \
		-lc3dio -lCart3D -ldl -L/Library/Developer/CommandLineTools/SDKs/MacOSX.sdk/usr/lib -lxml2 -lz  -licucore  -Wl,-no_compact_unwind -lm
clang -g -target arm64-apple-darwin  -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/include cart3dTest.c \
		-o ./cart3dTest.o
clang -g -target arm64-apple-darwin  -o /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/bin/cart3dTest ./cart3dTest.o \
		-L/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib -lcaps -locsm -legads -rpath /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.8.0/./lib -lm -ldl
clang -g -target arm64-apple-darwin  -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/include -I./xddm \
		-I. `xml2-config --cflags` ESPxddm.c -o ./ESPxddm.o
clang -g -target arm64-apple-darwin  -o /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/bin/ESPxddm ./ESPxddm.o ./writeTrix.o \
		./surfTrix.o ./xddm.o ./bodyTess.o -L/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib -locsm -legads \
		-L/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/include/ -lc3dio -lCart3D \
		-lpthread -ldl -Wl,-rpath,/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib -Wl,-rpath,@loader_path/ -Wl,-rpath,/Users/jenkins/util/ESP/OpenCASCADE-7.8.0/./lib -L/Library/Developer/CommandLineTools/SDKs/MacOSX.sdk/usr/lib -lxml2 -lz  -licucore  -Wl,-no_compact_unwind -lm
/Library/Developer/CommandLineTools/usr/bin/make -C cbaero 
clang -g -target arm64-apple-darwin  -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I. -I/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/include -I../utils -I../meshWriter/fastWriter cbaeroAIM.c -o cbaeroAIM.o
clang -g -target arm64-apple-darwin  -bundle cbaeroAIM.o -o /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib/cbaeroAIM.so -L/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib -lutils -laimUtil -locsm -legads -ludunits2 -lm -ldl
/Library/Developer/CommandLineTools/usr/bin/make -C cgt 
clang -g -target arm64-apple-darwin  -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/include egads2cgt.c \
		-o ./egads2cgt.o
clang -g -target arm64-apple-darwin  -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/include aflr4egads.c \
		-o ./aflr4egads.o
clang++ -g -target arm64-apple-darwin  -o /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/bin/egads2cgt ./egads2cgt.o ./aflr4egads.o \
		-L/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib -legads -lcaps -locsm -rpath /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.8.0/./lib -lm -ldl
/Library/Developer/CommandLineTools/usr/bin/make -C custom 
make[2]: Nothing to be done for `default'.
/Library/Developer/CommandLineTools/usr/bin/make -C delaundo 
clang -g -target arm64-apple-darwin  -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/include -I../utils delaundoAIM.c \
		-o ./delaundoAIM.o
touch /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib/delaundoAIM.so
rm /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib/delaundoAIM.so
clang -g -target arm64-apple-darwin  -bundle -o /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib/delaundoAIM.so ./delaundoAIM.o \
		-L/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib -lutils -laimUtil -locsm -legads -ludunits2 -ldl \
		-rpath /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.8.0/./lib -lm
/Library/Developer/CommandLineTools/usr/bin/make -C egadsTess 
clang -g -target arm64-apple-darwin  -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/include -I../utils egadsTessAIM.c \
		-o ./egadsTessAIM.o
touch /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib/egadsTessAIM.so
rm /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib/egadsTessAIM.so
clang -g -target arm64-apple-darwin  -bundle -o /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib/egadsTessAIM.so ./egadsTessAIM.o \
		-L/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib -lutils -laimUtil -locsm -legads -ludunits2 -ldl \
		-rpath /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.8.0/./lib -lm
/Library/Developer/CommandLineTools/usr/bin/make -C friction 
clang -g -target arm64-apple-darwin  -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -Wno-format -I/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/include -I../utils frictionAIM.c \
		-o ./frictionAIM.o
clang -g -target arm64-apple-darwin  -bundle -o /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib/frictionAIM.so ./frictionAIM.o \
		-L/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib -lutils -laimUtil -locsm -legads -ludunits2 -ldl -lm
gfortran -g  -c -O -frecursive -fcray-pointer friction_eja_mod.f -o ./friction.o
gfortran -g  -o /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/bin/friction ./friction.o -static-libgfortran -static-libgcc -Wl,-w
/Library/Developer/CommandLineTools/usr/bin/make -C fun3d 
clang -g -target arm64-apple-darwin  -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -DHAVE_PYTHON -DCYTHON_PEP489_MULTI_PHASE_INIT=0 \
		-I/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/include -I../utils -I../meshWriter/ugridWriter \
		-I/Users/jenkins/util/ESP/Python/ESP_Python-3.11.9/include/python3.11 -Icython fun3dAIM.c -o ./fun3dAIM.o
clang -g -target arm64-apple-darwin  -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/include -I../utils -I../meshWriter/ugridWriter \
		fun3dUtils.c -o ./fun3dUtils.o
clang -g -target arm64-apple-darwin  -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -DCYTHON_PEP489_MULTI_PHASE_INIT=0 \
		-I/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/include -I../utils \
		-I/Users/jenkins/util/ESP/Python/ESP_Python-3.11.9/include/python3.11 cython/fun3dNamelist.c -o ./fun3dNamelist.o
Building FUN3D with Python
clang -g -target arm64-apple-darwin  -bundle -o /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib/fun3dAIM.so ./fun3dAIM.o ./fun3dUtils.o \
		./fun3dNamelist.o -L/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib -lutils -laimUtil -locsm \
		-legads -ludunits2 -ldl -L/Users/jenkins/util/ESP/Python/ESP_Python-3.11.9/lib -lpython3.11 -lm -Wl,-rpath /Users/jenkins/util/ESP/Python/ESP_Python-3.11.9/lib
/Library/Developer/CommandLineTools/usr/bin/make -C hsm 
clang -g -target arm64-apple-darwin  -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/include -I../utils hsmAIM.c \
		-o src/hsmAIM.o
clang -g -target arm64-apple-darwin  -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/include -I../utils hsmUtils.c \
		-o src/hsmUtils.o
clang -g -target arm64-apple-darwin  -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/include -I../utils hsmAdj.c \
		-o src/hsmAdj.o
clang++ -g -target arm64-apple-darwin  -c -O -fPIC -DOCC_CONVERT_SIGNALS -DNDEBUG -DNo_Exception -D_OCC64 -Wall -Wno-write-strings -Wno-dangling-else -Wno-unused-result -std=c++11 -ffp-model=strict -Wno-comment rcm/rcm.cpp -DREVISION=7.8 \
		-o src/rcm.o
clang++ -g -target arm64-apple-darwin  -c -O -fPIC -DOCC_CONVERT_SIGNALS -DNDEBUG -DNo_Exception -D_OCC64 -Wall -Wno-write-strings -Wno-dangling-else -Wno-unused-result -std=c++11 -ffp-model=strict rcm/genrcmi.cpp -DREVISION=7.8 \
		-o src/genrcmi.o
/Library/Developer/CommandLineTools/usr/bin/make -C src atanc.o
gfortran -g  -c -O -frecursive -fcray-pointer -fdefault-real-8 -fbounds-check -ffpe-trap=invalid,zero  atanc.f -o ./atanc.o
/Library/Developer/CommandLineTools/usr/bin/make -C src bmdump.o
gfortran -g  -c -O -frecursive -fcray-pointer -fdefault-real-8 -fbounds-check -ffpe-trap=invalid,zero  bmdump.f -o ./bmdump.o
/Library/Developer/CommandLineTools/usr/bin/make -C src cross.o
gfortran -g  -c -O -frecursive -fcray-pointer -fdefault-real-8 -fbounds-check -ffpe-trap=invalid,zero  cross.f -o ./cross.o
/Library/Developer/CommandLineTools/usr/bin/make -C src hsmabd.o
gfortran -g  -c -O -frecursive -fcray-pointer -fdefault-real-8 -fbounds-check -ffpe-trap=invalid,zero  hsmabd.f -o ./hsmabd.o
/Library/Developer/CommandLineTools/usr/bin/make -C src hsmbb2.o
gfortran -g  -c -O -frecursive -fcray-pointer -fdefault-real-8 -fbounds-check -ffpe-trap=invalid,zero  hsmbb2.f -o ./hsmbb2.o
/Library/Developer/CommandLineTools/usr/bin/make -C src hsmbc.o
gfortran -g  -c -O -frecursive -fcray-pointer -fdefault-real-8 -fbounds-check -ffpe-trap=invalid,zero  hsmbc.f -o ./hsmbc.o
/Library/Developer/CommandLineTools/usr/bin/make -C src hsmdep.o
gfortran -g  -c -O -frecursive -fcray-pointer -fdefault-real-8 -fbounds-check -ffpe-trap=invalid,zero  hsmdep.f -o ./hsmdep.o
/Library/Developer/CommandLineTools/usr/bin/make -C src hsmeqn.o
gfortran -g  -c -O -frecursive -fcray-pointer -fdefault-real-8 -fbounds-check -ffpe-trap=invalid,zero  hsmeqn.f -o ./hsmeqn.o
/Library/Developer/CommandLineTools/usr/bin/make -C src hsmgeo.o
gfortran -g  -c -O -frecursive -fcray-pointer -fdefault-real-8 -fbounds-check -ffpe-trap=invalid,zero  hsmgeo.f -o ./hsmgeo.o
/Library/Developer/CommandLineTools/usr/bin/make -C src hsmglr.o
gfortran -g  -c -O -frecursive -fcray-pointer -fdefault-real-8 -fbounds-check -ffpe-trap=invalid,zero  hsmglr.f -o ./hsmglr.o
/Library/Developer/CommandLineTools/usr/bin/make -C src hsmout.o
gfortran -g  -c -O -frecursive -fcray-pointer -fdefault-real-8 -fbounds-check -ffpe-trap=invalid,zero  hsmout.f -o ./hsmout.o
/Library/Developer/CommandLineTools/usr/bin/make -C src hsmprj.o
gfortran -g  -c -O -frecursive -fcray-pointer -fdefault-real-8 -fbounds-check -ffpe-trap=invalid,zero  hsmprj.f -o ./hsmprj.o
/Library/Developer/CommandLineTools/usr/bin/make -C src hsmre1.o
gfortran -g  -c -O -frecursive -fcray-pointer -fdefault-real-8 -fbounds-check -ffpe-trap=invalid,zero  hsmre1.f -o ./hsmre1.o
/Library/Developer/CommandLineTools/usr/bin/make -C src hsmren.o
gfortran -g  -c -O -frecursive -fcray-pointer -fdefault-real-8 -fbounds-check -ffpe-trap=invalid,zero  hsmren.f -o ./hsmren.o
/Library/Developer/CommandLineTools/usr/bin/make -C src hsmrfm.o
gfortran -g  -c -O -frecursive -fcray-pointer -fdefault-real-8 -fbounds-check -ffpe-trap=invalid,zero  hsmrfm.f -o ./hsmrfm.o
/Library/Developer/CommandLineTools/usr/bin/make -C src hsmrun.o
gfortran -g  -c -O -frecursive -fcray-pointer -fdefault-real-8 -fbounds-check -ffpe-trap=invalid,zero -fno-recursive hsmrun.f -o ./hsmrun.o
/Library/Developer/CommandLineTools/usr/bin/make -C src hsmsol.o
gfortran -g  -c -O -frecursive -fcray-pointer -fdefault-real-8 -fbounds-check -ffpe-trap=invalid,zero  hsmsol.f -o ./hsmsol.o
/Library/Developer/CommandLineTools/usr/bin/make -C src ludcmp.o
gfortran -g  -c -O -frecursive -fcray-pointer -fdefault-real-8 -fbounds-check -ffpe-trap=invalid,zero  ludcmp.f -o ./ludcmp.o
/Library/Developer/CommandLineTools/usr/bin/make -C src sbsolve.o
gfortran -g  -c -O -frecursive -fcray-pointer -fdefault-real-8 -fbounds-check -ffpe-trap=invalid,zero  sbsolve.f -o ./sbsolve.o
/Library/Developer/CommandLineTools/usr/bin/make -C src /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib/libhsm.a
touch /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib/libhsm.a
rm /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib/libhsm.a
(cd .; ar -rs /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib/libhsm.a hsmsol.o hsmdep.o hsmout.o hsmgeo.o hsmabd.o hsmeqn.o hsmbc.o hsmprj.o hsmren.o hsmre1.o hsmrfm.o hsmbb2.o hsmglr.o ludcmp.o sbsolve.o atanc.o bmdump.o cross.o )
ar: creating archive /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib/libhsm.a
touch /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib/hsmAIM.so
rm /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib/hsmAIM.so
gfortran -g  -bundle -o /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib/hsmAIM.so \
		src/hsmAIM.o src/hsmUtils.o src/hsmAdj.o \
		src/rcm.o src/genrcmi.o \
		 -L/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib -lutils -laimUtil -locsm \
		-legads -ludunits2 -lhsm -ldl -Wl,-rpath,/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib -Wl,-rpath,@loader_path/ -Wl,-rpath,/Users/jenkins/util/ESP/OpenCASCADE-7.8.0/./lib -lc++ -static-libgfortran -static-libgcc -Wl,-w
/Library/Developer/CommandLineTools/usr/bin/make -C interference 
clang -g -target arm64-apple-darwin  -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/include interferenceAIM.c \
		-o ./interferenceAIM.o
clang -g -target arm64-apple-darwin  -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/include -I. cloudFns.c \
		-o ./cloudFns.o
touch /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib/interferenceAIM.so
rm /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib/interferenceAIM.so
clang -g -target arm64-apple-darwin  -bundle -o /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib/interferenceAIM.so \
		./interferenceAIM.o ./cloudFns.o -L/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib \
		-laimUtil -locsm -legads -ludunits2 -ldl -lc++ -rpath /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.8.0/./lib -lm
/Library/Developer/CommandLineTools/usr/bin/make -C masstran 
clang++ -g -target arm64-apple-darwin  -c -O -fPIC -DOCC_CONVERT_SIGNALS -DNDEBUG -DNo_Exception -D_OCC64 -Wall -Wno-write-strings -Wno-dangling-else -Wno-unused-result -std=c++11 -ffp-model=strict -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/include -I../utils masstranAIM.cpp \
		-o ./masstranAIM.o
clang++ -g -target arm64-apple-darwin  -bundle -o /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib/masstranAIM.so ./masstranAIM.o \
		-L/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib -lutils -laimUtil -locsm -legads -ludunits2 -ldl -lm
/Library/Developer/CommandLineTools/usr/bin/make -C meshWriter 
/Library/Developer/CommandLineTools/usr/bin/make -C bstlWriter 
clang -g -target arm64-apple-darwin  -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I../include -I/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/include bstlWriter.c \
		-o ./bstlWriter.o
clang -g -target arm64-apple-darwin  -bundle -o /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib/bstlWriter.so ./bstlWriter.o \
		-L/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib -laimUtil -legads -locsm -ludunits2 -ldl -rpath /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.8.0/./lib -lm
/Library/Developer/CommandLineTools/usr/bin/make -C bvtkWriter 
clang -g -target arm64-apple-darwin  -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I../include -I/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/include bvtkWriter.c \
		-o ./bvtkWriter.o
clang -g -target arm64-apple-darwin  -bundle -o /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib/bvtkWriter.so ./bvtkWriter.o \
		-L/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib -laimUtil -legads -locsm -ludunits2 -ldl -rpath /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.8.0/./lib -lm
/Library/Developer/CommandLineTools/usr/bin/make -C exodusWriter 
clang++ -g -target arm64-apple-darwin  -c -O -Wall -Wno-dangling-else -Wno-unused-result -std=c++11 -DREVISION=7.8  -I../include -I/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/include -I/Users/jenkins/util/sandialabs/seacas/include -I/opt/homebrew/include exodusWriter.cpp \
		-o ./exodusWriter.o
clang++ -g -target arm64-apple-darwin  -bundle -std=c++11 -o /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib/exodusWriter.so ./exodusWriter.o \
		-L/Users/jenkins/util/sandialabs/seacas/lib -lexodus -Wl,-rpath /Users/jenkins/util/sandialabs/seacas/lib  -L/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib -laimUtil -legads -locsm -ludunits2 -ldl -rpath /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.8.0/./lib -lm
/Library/Developer/CommandLineTools/usr/bin/make -C fastWriter 
clang -g -target arm64-apple-darwin  -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I../include -I/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/include fastWriter.c \
		-o ./fastWriter.o
clang -g -target arm64-apple-darwin  -bundle -o /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib/fastWriter.so ./fastWriter.o \
		-L/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib -laimUtil -legads -locsm -ludunits2 -ldl -rpath /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.8.0/./lib -lm
/Library/Developer/CommandLineTools/usr/bin/make -C libmeshbWriter 
clang -g -target arm64-apple-darwin  -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I../include -I/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/include libmeshbWriter.c \
		-o ./libmeshbWriter.o
clang -g -target arm64-apple-darwin  -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8  -IlibMeshb/sources -I../include -I/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/include libMeshb/sources/libmeshb7.c \
		-o ./libmeshb7.o
clang -g -target arm64-apple-darwin  -bundle -o /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib/libmeshbWriter.so ./libmeshbWriter.o ./libmeshb7.o \
		-L/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib -laimUtil -legads -locsm -ludunits2 -ldl -rpath /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.8.0/./lib -lm
/Library/Developer/CommandLineTools/usr/bin/make -C stlWriter 
clang -g -target arm64-apple-darwin  -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I../include -I/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/include stlWriter.c \
		-o ./stlWriter.o
clang -g -target arm64-apple-darwin  -bundle -o /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib/stlWriter.so ./stlWriter.o \
		-L/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib -laimUtil -legads -locsm -ludunits2 -ldl -rpath /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.8.0/./lib -lm
/Library/Developer/CommandLineTools/usr/bin/make -C su2Writer 
clang -g -target arm64-apple-darwin  -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I../include -I/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/include su2Writer.c \
		-o ./su2Writer.o
clang -g -target arm64-apple-darwin  -bundle -o /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib/su2Writer.so ./su2Writer.o \
		-L/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib -laimUtil -legads -locsm -ludunits2 -ldl -rpath /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.8.0/./lib -lm
/Library/Developer/CommandLineTools/usr/bin/make -C tecplotWriter 
clang -g -target arm64-apple-darwin  -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I../include -I/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/include tecplotWriter.c \
		-o ./tecplotWriter.o
clang -g -target arm64-apple-darwin  -bundle -o /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib/tecplotWriter.so ./tecplotWriter.o \
		-L/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib -laimUtil -legads -locsm -ludunits2 -ldl -rpath /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.8.0/./lib -lm
/Library/Developer/CommandLineTools/usr/bin/make -C ugridWriter 
clang -g -target arm64-apple-darwin  -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I../include -I/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/include ugridWriter.c \
		-o ./ugridWriter.o
clang -g -target arm64-apple-darwin  -bundle -o /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib/ugridWriter.so ./ugridWriter.o \
		-L/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib -laimUtil -legads -locsm -ludunits2 -ldl -rpath /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.8.0/./lib -lm
/Library/Developer/CommandLineTools/usr/bin/make -C vtkWriter 
clang -g -target arm64-apple-darwin  -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I../include -I/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/include vtkWriter.c \
		-o ./vtkWriter.o
clang -g -target arm64-apple-darwin  -bundle -o /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib/vtkWriter.so ./vtkWriter.o \
		-L/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib -laimUtil -legads -locsm -ludunits2 -ldl -rpath /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.8.0/./lib -lm
/Library/Developer/CommandLineTools/usr/bin/make -C mses 
clang -g -target arm64-apple-darwin  -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/include -I../utils msesAIM.c -o msesAIM.o
clang -g -target arm64-apple-darwin  -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/include -I../utils msesUtils.c -o msesUtils.o
clang -g -target arm64-apple-darwin  -bundle -o /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib/msesAIM.so ./msesAIM.o ./msesUtils.o \
		-L/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib -lutils -laimUtil -locsm -legads -ludunits2 -ldl -lm
/Library/Developer/CommandLineTools/usr/bin/make -C mystran 
clang -g -target arm64-apple-darwin  -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/include -I../utils mystranAIM.c \
		-o ./mystranAIM.o
clang -g -target arm64-apple-darwin  -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/include -I../utils mystranUtils.c \
		-o ./mystranUtils.o
clang -g -target arm64-apple-darwin  -bundle -o /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib/mystranAIM.so ./mystranAIM.o ./mystranUtils.o \
		-L/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib -lutils -laimUtil -locsm -legads -ludunits2 -ldl -lm -L/Users/jenkins/util/ESP/Python/ESP_Python-3.11.9/lib -lpython3.11
/Library/Developer/CommandLineTools/usr/bin/make -C nastran 
clang -g -target arm64-apple-darwin  -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/include -I../utils nastranAIM.c \
		-o ./nastranAIM.o
clang -g -target arm64-apple-darwin  -bundle -o /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib/nastranAIM.so ./nastranAIM.o \
		-L/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib -lutils -laimUtil -locsm -legads -ludunits2 -ldl -lm -L/Users/jenkins/util/ESP/Python/ESP_Python-3.11.9/lib -lpython3.11
/Library/Developer/CommandLineTools/usr/bin/make -C plato 
clang -g -target arm64-apple-darwin  -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/include -I../meshWriter/exodusWriter -I../utils  -I/Users/jenkins/util/sandialabs/seacas/include -I/opt/homebrew/include platoAIM.c \
		-o ./platoAIM.o
clang -g -target arm64-apple-darwin  -bundle -o /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib/platoAIM.so ./platoAIM.o -L/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib \
		-L/Users/jenkins/util/sandialabs/seacas/lib -lexodus -Wl,-rpath /Users/jenkins/util/sandialabs/seacas/lib  \
		-laimUtil -locsm -legads -ludunits2 -ldl -lm
/Library/Developer/CommandLineTools/usr/bin/make -C pointwise 
clang -g -target arm64-apple-darwin  -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/include -I../utils pointwiseAIM.c \
		-o ./pointwiseAIM.o
clang -g -target arm64-apple-darwin  -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/include -I../utils hashElement.c \
		-o ./hashElement.o
touch /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib/pointwiseAIM.so
rm /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib/pointwiseAIM.so
clang -g -target arm64-apple-darwin  -bundle -o /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib/pointwiseAIM.so ./pointwiseAIM.o ./hashElement.o \
		-L/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib -lutils -laimUtil -locsm -legads -ludunits2 -ldl \
		-rpath /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.8.0/./lib -lm -lpthread
/Library/Developer/CommandLineTools/usr/bin/make -C refine 
clang -g -target arm64-apple-darwin  -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/include -I../utils -I../meshWriter/libmeshbWriter refineAIM.c \
		-o ./refineAIM.o
clang -g -target arm64-apple-darwin  -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 \
		-I../meshWriter/libmeshbWriter/libMeshb/sources \
		../meshWriter/libmeshbWriter/libMeshb/sources/libmeshb7.c \
		-o ./libmeshb7.o
touch /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib/refineAIM.so
rm /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib/refineAIM.so
clang -g -target arm64-apple-darwin  -bundle -o /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib/refineAIM.so ./refineAIM.o ./libmeshb7.o \
		-L/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib -lutils -laimUtil -locsm -legads -ludunits2 -ldl \
		-rpath /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.8.0/./lib -lm
/Library/Developer/CommandLineTools/usr/bin/make -C sierraSD 
clang -g -target arm64-apple-darwin  -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/include -I../meshWriter/exodusWriter -I../utils  -I/Users/jenkins/util/sandialabs/seacas/include -I/opt/homebrew/include sierraSDAIM.c \
		-o ./sierraSDAIM.o
clang -g -target arm64-apple-darwin  -bundle -o /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib/sierraSDAIM.so ./sierraSDAIM.o -L/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib \
		-L/Users/jenkins/util/sandialabs/seacas/lib -lexodus -Wl,-rpath /Users/jenkins/util/sandialabs/seacas/lib  \
		-lutils -laimUtil -locsm -legads -ludunits2 -ldl -lm
/Library/Developer/CommandLineTools/usr/bin/make -C sierraSM 
clang -g -target arm64-apple-darwin  -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/include -I../meshWriter/exodusWriter -I../utils  -I/Users/jenkins/util/sandialabs/seacas/include -I/opt/homebrew/include sierraSMAIM.c \
		-o ./sierraSMAIM.o
clang -g -target arm64-apple-darwin  -bundle -o /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib/sierraSMAIM.so ./sierraSMAIM.o -L/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib \
		-L/Users/jenkins/util/sandialabs/seacas/lib -lexodus -Wl,-rpath /Users/jenkins/util/sandialabs/seacas/lib  \
		-lutils -laimUtil -locsm -legads -ludunits2 -ldl -lm
/Library/Developer/CommandLineTools/usr/bin/make -C skeleton 
clang -g -target arm64-apple-darwin  -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/include -I../utils skeletonAIM.c \
		-o ./skeletonAIM.o
clang -g -target arm64-apple-darwin  -bundle -o /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib/skeletonAIM.so ./skeletonAIM.o \
		-L/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib -lutils -laimUtil -locsm -legads -ludunits2 -ldl -lm
/Library/Developer/CommandLineTools/usr/bin/make -C spinnaker 
clang -g -target arm64-apple-darwin  -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/include \
		-I../meshWriter/exodusWriter \
		-I../meshWriter/libmeshbWriter \
		-I../utils -I/Users/jenkins/util/sandialabs/seacas/include \
		-I/opt/homebrew/include \
		spinnakerAIM.c \
		-o ./spinnakerAIM.o
clang -g -target arm64-apple-darwin  -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 \
		-I../meshWriter/libmeshbWriter/libMeshb/sources \
		../meshWriter/libmeshbWriter/libMeshb/sources/libmeshb7.c \
		-o ./libmeshb7.o
clang -g -target arm64-apple-darwin  -bundle -o /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib/spinnakerAIM.so ./spinnakerAIM.o ./libmeshb7.o -L/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib \
		-L/Users/jenkins/util/sandialabs/seacas/lib -lexodus -Wl,-rpath /Users/jenkins/util/sandialabs/seacas/lib  \
		-laimUtil -locsm -legads -ludunits2 -ldl -lm
/Library/Developer/CommandLineTools/usr/bin/make -C su2 
clang -g -target arm64-apple-darwin  -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/include -I../meshWriter/su2Writer -I../utils su2AIM.c \
		-o ./su2AIM.o
clang -g -target arm64-apple-darwin  -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/include -I../utils su2Utils.c \
		-o ./su2Utils.o
clang -g -target arm64-apple-darwin  -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/include -I../utils su2_4_Cardinal.c \
		-o ./su2_4_Cardinal.o
clang -g -target arm64-apple-darwin  -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/include -I../utils su2_5_Raven.c \
		-o ./su2_5_Raven.o
clang -g -target arm64-apple-darwin  -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/include -I../utils su2_6_Falcon.c \
		-o ./su2_6_Falcon.o
clang -g -target arm64-apple-darwin  -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/include -I../utils su2_7_Blackbird.c \
		-o ./su2_7_Blackbird.o
clang -g -target arm64-apple-darwin  -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/include -I../utils su2_801_Harrier.c \
		-o ./su2_801_Harrier.o
clang -g -target arm64-apple-darwin  -bundle -o /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib/su2AIM.so ./su2AIM.o ./su2Utils.o ./su2_4_Cardinal.o ./su2_5_Raven.o ./su2_6_Falcon.o ./su2_7_Blackbird.o ./su2_801_Harrier.o \
		-L/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib -lutils -laimUtil -locsm -legads -ludunits2 -ldl -lm
/Library/Developer/CommandLineTools/usr/bin/make -C tacs 
clang -g -target arm64-apple-darwin  -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/include -I../utils tacsAIM.c \
		-o ./tacsAIM.o
clang -g -target arm64-apple-darwin  -bundle -o /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib/tacsAIM.so ./tacsAIM.o \
		-L/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib -lutils -laimUtil -locsm -legads -ludunits2 -ldl -lm -L/Users/jenkins/util/ESP/Python/ESP_Python-3.11.9/lib -lpython3.11
/Library/Developer/CommandLineTools/usr/bin/make -C tetgen 
clang++ -g -target arm64-apple-darwin  -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/include -I../utils tetgenAIM.cpp \
		-o ./tetgenAIM.o
clang++ -g -target arm64-apple-darwin  -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/include -I/Users/jenkins/util/tetgen/tetgen1.6.0 -I../utils \
		-DTETLIBRARY tetgen_Interface.cpp -o ./tetgen_Interface.o
clang++ -g -target arm64-apple-darwin  -c -O -Wall -Wno-dangling-else -Wno-unused-result -DTETLIBRARY -w /Users/jenkins/util/tetgen/tetgen1.6.0/tetgen.cxx -o ./tetgen.o
clang++ -g -target arm64-apple-darwin  -c -O -Wall -Wno-dangling-else -Wno-unused-result -O0 -w /Users/jenkins/util/tetgen/tetgen1.6.0/predicates.cxx -o ./predicates.o
clang++ -g -target arm64-apple-darwin  -bundle -o /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib/tetgenAIM.so ./tetgenAIM.o \
		./tetgen_Interface.o ./tetgen.o \
		./predicates.o -L/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib -lutils -laimUtil -locsm \
		-legads -ludunits2 -ldl -rpath /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.8.0/./lib -lm
/Library/Developer/CommandLineTools/usr/bin/make -C tsfoil 
clang -g -target arm64-apple-darwin  -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/include -I../utils \
		tsfoilAIM.c -o ./tsfoilAIM.o
clang -g -target arm64-apple-darwin  -bundle -o /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib/tsfoilAIM.so ./tsfoilAIM.o \
		-L/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib -lutils -laimUtil -locsm -legads -ludunits2 -ldl -lm
/Library/Developer/CommandLineTools/usr/bin/make -C unitTest 
make[2]: Nothing to be done for `all'.
/Library/Developer/CommandLineTools/usr/bin/make -C xfoil 
clang -g -target arm64-apple-darwin  -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/include -I../utils \
		xfoilAIM.c -o ./xfoilAIM.o
clang -g -target arm64-apple-darwin  -bundle -o /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib/xfoilAIM.so ./xfoilAIM.o \
		-L/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib -lutils -laimUtil -locsm -legads -ludunits2 -ldl -lm
/Library/Developer/CommandLineTools/usr/bin/make -C zaero 
clang -g -target arm64-apple-darwin  -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/include -I../utils zaeroAIM.c -o zaeroAIM.o
clang -g -target arm64-apple-darwin  -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/include -I../utils zaeroUtils.c -o zaeroUtils.o
clang -g -target arm64-apple-darwin  -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/include -I../utils zaeroLinearFlutter.c -o zaeroLinearFlutter.o
clang -g -target arm64-apple-darwin  -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/include -I../utils zaeroTrim.c -o zaeroTrim.o
clang -g -target arm64-apple-darwin  -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/include -I../utils zaeroTypes.c -o zaeroTypes.o
clang -g -target arm64-apple-darwin  -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/include -I../utils zaeroCards.c -o zaeroCards.o
clang -g -target arm64-apple-darwin  -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/include -I../utils zaeroGeneral.c -o zaeroGeneral.o
clang -g -target arm64-apple-darwin  -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/include -I../utils zaeroGraphical.c -o zaeroGraphical.o
clang -g -target arm64-apple-darwin  -bundle  -o /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib/zaeroAIM.so ./zaeroAIM.o ./zaeroUtils.o ./zaeroLinearFlutter.o ./zaeroTrim.o ./zaeroTypes.o ./zaeroCards.o ./zaeroGeneral.o ./zaeroGraphical.o -L/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib -lutils -laimUtil -locsm -legads -ludunits2 -lm -ldl
(cd OpenCSM; make -f serveESP.make)
clang -g -target arm64-apple-darwin  -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/include -I. timCapsMode.c -o ./timCapsMode.o
touch /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib/capsMode.so
rm /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib/capsMode.so
clang++ -g -target arm64-apple-darwin  -bundle -o /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib/capsMode.so ./timCapsMode.o -L/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib -lcaps -locsm -lwsserver -legads -ldl -lm
clang -g -target arm64-apple-darwin  -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/include -I. timFlowchart.c -o ./timFlowchart.o
touch /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib/flowchart.so
rm /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib/flowchart.so
clang++ -g -target arm64-apple-darwin  -bundle -o /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib/flowchart.so ./timFlowchart.o -L/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib -lcaps -locsm -lwsserver -legads -ldl -lm
clang -g -target arm64-apple-darwin  -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/include -I. timViewer.c -o ./timViewer.o
touch /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib/viewer.so
rm /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib/viewer.so
clang++ -g -target arm64-apple-darwin  -bundle -o /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib/viewer.so ./timViewer.o -L/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib -lcaps -locsm -lwsserver -legads -ldl -lm
clang -g -target arm64-apple-darwin  -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/include -I. -I/Users/jenkins/util/ESP/Python/ESP_Python-3.11.9/include/python3.11 timPyscript.c -o ./timPyscript.o
touch /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib/pyscript.so
rm /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib/pyscript.so
clang++ -g -target arm64-apple-darwin  -bundle -o /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib/pyscript.so ./timPyscript.o -L/Users/jenkins/util/ESP/Python/ESP_Python-3.11.9/lib -lpython3.11 -L/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib -lcaps -locsm -lwsserver -legads -ldl -rpath /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.8.0/./lib -Wl,-rpath /Users/jenkins/util/ESP/Python/ESP_Python-3.11.9/lib
 
 *** Build Completed! ***
+ export CSMDATA=/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/data
+ CSMDATA=/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/data
+ cd /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/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_Beta/7.8/DARWIN_ARM64/Verification.sh
+ bash -ex /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/Verification.sh
+ expectSuccess 01 /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/data/basic/expressions
+ ./serveESP -batch -verify -outLevel 0 /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/data/basic/expressions
WARNING:: cannot open "/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/data/basic/verify_7.8.0/expressions.vfy", so verification is being skipped
ERROR:: problem evaluating argument 2 (slice(e3,0,999)) for Branch 152 (set)
ERROR:: problem evaluating argument 2 (slice(e3,14,999)) for Branch 158 (set)
ERROR:: problem evaluating argument 2 (slice(e3,4,-1)) for Branch 164 (set)

==> serveESP completed successfully with no verification data

real	0m0.468s
user	0m0.188s
sys	0m0.011s
+ set +x

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

+ expectSuccess 02 /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/data/basic/demo2
+ ./serveESP -batch -verify -outLevel 0 /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/data/basic/demo2
WARNING:: cannot open "/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/data/basic/verify_7.8.0/demo2.vfy", so verification is being skipped

==> serveESP completed successfully with no verification data

real	0m0.375s
user	0m0.390s
sys	0m0.044s
+ set +x

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

+ expectSuccess 03 /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/data/legacy/tutorial1_whole
+ ./serveESP -batch -verify -outLevel 0 /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/data/legacy/tutorial1_whole
WARNING:: cannot open "/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/data/legacy/verify_7.8.0/tutorial1_whole.vfy", so verification is being skipped

==> serveESP completed successfully with no verification data

real	0m2.218s
user	0m2.879s
sys	0m0.321s
+ set +x

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

+ expectSuccess 04 /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/data/basic/design2
+ ./serveESP -batch -verify -outLevel 0 /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/data/basic/design2
WARNING:: cannot open "/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/data/basic/verify_7.8.0/design2.vfy", so verification is being skipped

==> serveESP completed successfully with no verification data

real	0m0.501s
user	0m0.514s
sys	0m0.039s
+ set +x

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

+ expectSuccess 05 /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/data/basic/design3
+ ./serveESP -batch -verify -outLevel 0 /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/data/basic/design3
WARNING:: cannot open "/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/data/basic/verify_7.8.0/design3.vfy", so verification is being skipped

==> serveESP completed successfully with no verification data

real	0m0.594s
user	0m0.660s
sys	0m0.023s
+ set +x

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

+ expectSuccess 06 /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/data/legacy/tutorial2
+ ./serveESP -batch -verify -outLevel 0 /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/data/legacy/tutorial2
WARNING:: cannot open "/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/data/legacy/verify_7.8.0/tutorial2.vfy", so verification is being skipped

==> serveESP completed successfully with no verification data

real	0m0.534s
user	0m0.642s
sys	0m0.024s
+ set +x

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

+ expectSuccess 07 /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/data/legacy/tutorial3
+ ./serveESP -batch -verify -outLevel 0 /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/data/legacy/tutorial3
WARNING:: cannot open "/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/data/legacy/verify_7.8.0/tutorial3.vfy", so verification is being skipped

==> serveESP completed successfully with no verification data

real	0m3.101s
user	0m4.487s
sys	0m0.301s
+ set +x

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

+ expectSuccess 08 /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/data/CAPS/myPlane
+ ./serveESP -batch -verify -outLevel 0 /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/data/CAPS/myPlane
WARNING:: cannot open "/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/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	0m24.924s
user	0m36.412s
sys	0m1.142s
+ set +x

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

+ expectSuccess 09 /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/data/bottle
+ ./serveESP -batch -verify -outLevel 0 /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/data/bottle
WARNING:: cannot open "/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/data/verify_7.8.0/bottle.vfy", so verification is being skipped

==> serveESP completed successfully with no verification data

real	0m0.574s
user	0m0.602s
sys	0m0.019s
+ set +x

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

+ expectSuccess 10 /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/data/basic/wingMultiModel
+ ./serveESP -batch -verify -outLevel 0 /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/data/basic/wingMultiModel
WARNING:: cannot open "/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/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	0m33.951s
user	0m54.807s
sys	0m12.748s
+ set +x

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

+ expectSuccess 11 /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/data/basic/bullet
+ ./serveESP -batch -verify -outLevel 0 /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/data/basic/bullet
WARNING:: cannot open "/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/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	0m0.436s
user	0m0.356s
sys	0m0.021s
+ set +x

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

+ expectSuccess 12 /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/data/basic/connect5
+ ./serveESP -batch -verify -outLevel 0 /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/data/basic/connect5
WARNING:: cannot open "/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/data/basic/verify_7.8.0/connect5.vfy", so verification is being skipped

==> serveESP completed successfully with no verification data

real	0m0.603s
user	0m0.798s
sys	0m0.012s
+ set +x

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

+ expectSuccess 13 /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/data/basic/group2
+ ./serveESP -batch -verify -outLevel 0 /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/data/basic/group2
WARNING:: cannot open "/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/data/basic/verify_7.8.0/group2.vfy", so verification is being skipped

==> serveESP completed successfully with no verification data

real	0m0.248s
user	0m0.266s
sys	0m0.010s
+ set +x

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

+ expectSuccess 14 /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/data/basic/csm3
+ ./serveESP -batch -verify -outLevel 0 /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/data/basic/csm3
WARNING:: cannot open "/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/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	0m0.471s
user	0m0.494s
sys	0m0.018s
+ set +x

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

+ cd /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/pyESP/testEGADS
+ make test
python --version
Python 3.11.9
python -u -m unittest discover
....................................................   PCurve Map: 48 (alloc 48)!
   Surface Map: 12 (alloc 24)!
   Curve Map: 28 (alloc 28)!
 Writing PCurves...
 Writing Curves...
 Writing Surfaces...
 Writing 16 Nodes...
 Writing 28 Edges...
 Writing 12 Loops...
 Writing 12 Faces...
 Writing 1 Shells...
 EGADS Info: 0 Objects, 0 Reference in Use (of 972) at Close!
...................
----------------------------------------------------------------------
Ran 71 tests in 1.899s

OK
+ cd /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/pyESP/testOCSM
+ source /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/JenkinsESP/test_pyOCSM.sh
++ set -x
++ python -u test_pyOCSM.py -skipHelp

real	0m5.403s
user	0m7.469s
sys	0m0.143s
++ set +x
=================================================
test_pyOCSM.py passed (as expected)
=================================================
+ cd /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/pyESP/testCAPS
+ make test
python --version
Python 3.11.9
python -u -m unittest discover
..
Mapping Csys attributes ................
	Number of unique Csys attributes = 2
	Name = leftWingSkin, index = 1
	Name = riteWingSkin, index = 2

Getting FEA coordinate systems.......
	Number of coordinate systems - 2
	Coordinate system name - leftWingSkin
	Coordinate system name - riteWingSkin
Mapping capsConstraint attributes ................
	Number of unique capsConstraint attributes = 0
Mapping capsLoad attributes ................
	Number of unique capsLoad attributes = 0
Mapping capsBound attributes ................
	Number of unique capsBound attributes = 1
	Name = Upper_Left, index = 1
Mapping capsConnect attributes ................
	Number of unique capsConnect attributes = 0
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 2
	Name = Wing1, index = 1
	Name = Wing2, index = 2
Setting FEA Data
	Mesh for body = 0
	Number of nodal coordinates = 143
	Number of elements = 282
	Elemental Nodes = 0
	Elemental Rods  = 0
	Elemental Tria3 = 282
	Elemental Quad4 = 0
Setting FEA Data
	Mesh for body = 1
	Number of nodal coordinates = 155
	Number of elements = 306
	Elemental Nodes = 0
	Elemental Rods  = 0
	Elemental Tria3 = 306
	Elemental Quad4 = 0
Combining multiple FEA meshes!
	Combined Number of nodal coordinates = 298
	Combined Number of elements = 588
	Combined Elemental Nodes = 0
	Combined Elemental Rods  = 0
	Combined Elemental Tria3 = 588
	Combined Elemental Quad4 = 0

Getting FEA materials.......
	Number of materials - 2
	Material name - madeupium
	Material name - unobtainium
	Done getting FEA materials

Getting FEA properties.......
	Number of properties - 2
	Property name - Wing1
	Property name - Wing2
	Done getting FEA properties
Updating mesh element types based on properties input
..
. EGADS Info: 0 Objects, 0 Reference in Use (of 0) at Close!
..Writing D3 Javascript library -  d3.v3.min.js
........... EGADS Info: 0 Objects, 0 Reference in Use (of 0) at Close!
. EGADS Info: 0 Objects, 0 Reference in Use (of 0) at Close!
. EGADS Info: 0 Objects, 0 Reference in Use (of 0) at Close!
 EGADS Info: 0 Objects, 0 Reference in Use (of 0) at Close!
.No analysis directory provided - defaulting to altName

Mapping Csys attributes ................
	Number of unique Csys attributes = 2
	Name = leftWingSkin, index = 1
	Name = riteWingSkin, index = 2

Getting FEA coordinate systems.......
	Number of coordinate systems - 2
	Coordinate system name - leftWingSkin
	Coordinate system name - riteWingSkin
Mapping capsConstraint attributes ................
	Number of unique capsConstraint attributes = 0
Mapping capsLoad attributes ................
	Number of unique capsLoad attributes = 0
Mapping capsBound attributes ................
	Number of unique capsBound attributes = 1
	Name = Upper_Left, index = 1
Mapping capsConnect attributes ................
	Number of unique capsConnect attributes = 0
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 2
	Name = Wing1, index = 1
	Name = Wing2, index = 2
Setting FEA Data
	Mesh for body = 0
	Number of nodal coordinates = 209
	Number of elements = 414
	Elemental Nodes = 0
	Elemental Rods  = 0
	Elemental Tria3 = 414
	Elemental Quad4 = 0
Setting FEA Data
	Mesh for body = 1
	Number of nodal coordinates = 186
	Number of elements = 368
	Elemental Nodes = 0
	Elemental Rods  = 0
	Elemental Tria3 = 368
	Elemental Quad4 = 0
Combining multiple FEA meshes!
	Combined Number of nodal coordinates = 395
	Combined Number of elements = 782
	Combined Elemental Nodes = 0
	Combined Elemental Rods  = 0
	Combined Elemental Tria3 = 782
	Combined Elemental Quad4 = 0

Getting FEA materials.......
	Number of materials - 2
	Material name - madeupium
	Material name - unobtainium
	Done getting FEA materials

Getting FEA properties.......
	Number of properties - 2
	Property name - Wing1
	Property name - Wing2
	Done getting FEA properties
Updating mesh element types based on properties input
.
.
..
























.
..

...--> Opening DESPMTR file "unitGeom.param"
    updating CFGPMTR series                          [ 1, 1] =  8412.000000
    updating CFGPMTR series2                         [ 1, 1] =    20.000000
    updating CFGPMTR VIEW:CFD                        [ 1, 1] =     1.000000
    updating CFGPMTR nrow                            [ 1, 1] =     3.000000
    updating CFGPMTR ncol                            [ 1, 1] =     2.000000
    updating DESPMTR area                            [ 1, 1] =    40.000000
    updating DESPMTR aspect                          [ 1, 1] =     5.000000
    updating DESPMTR taper                           [ 1, 1] =     0.500000
    updating DESPMTR twist                           [ 1, 1] =    15.000000
    updating DESPMTR wing:lesweep                    [ 1, 1] =    30.000000
    updating DESPMTR wing:dihedral                   [ 1, 1] =     1.000000
    updating DESPMTR wing:chord:root                 [ 1, 1] =     1.560000
    updating DESPMTR htail                           [ 1, 1] =     1.000000
    updating DESPMTR htail:chord                     [ 1, 1] =     2.000000
    updating DESPMTR vtail:chord                     [ 1, 1] =     3.000000
    updating DESPMTR vtail                           [ 1, 1] =     4.000000
    updating DESPMTR sphereR                         [ 1, 1] =    80.000000
    updating DESPMTR v@1:d_name                      [ 1, 1] =     1.000000
    updating DESPMTR despMat                         [ 1, 1] =    11.000000
    updating DESPMTR despMat                         [ 1, 2] =    12.000000
    updating DESPMTR despMat                         [ 2, 1] =    13.000000
    updating DESPMTR despMat                         [ 2, 2] =    14.000000
    updating DESPMTR despMat                         [ 3, 1] =    15.000000
    updating DESPMTR despMat                         [ 3, 2] =    16.000000
    updating DESPMTR despCol                         [ 1, 1] =    11.000000
    updating DESPMTR despCol                         [ 2, 1] =    13.000000
    updating DESPMTR despCol                         [ 3, 1] =    15.000000
    updating DESPMTR despRow                         [ 1, 1] =    11.000000
    updating DESPMTR despRow                         [ 1, 2] =    12.000000
    updating DESPMTR despRow                         [ 1, 3] =    13.000000
ERROR:: DESPMTR file "unitGeom.param" not found
 CAPS Error: ocsmSaveDespmtrs = -201 (caps_readParameters)!
 EGADS Info: 0 Objects, 0 Reference in Use (of 0) at Close!
.
.
 EGADS Error: No Attribute -> __numRemaining__ (EG_attributeDel)!
 EGADS Error: No Attribute -> __numRemaining__ (EG_attributeDel)!
 EGADS Error: No Attribute -> _body (EG_attributeDel)!
 EGADS Error: No Attribute -> _nface (EG_attributeDel)!
 EGADS Error: No Attribute -> __trace__ (EG_attributeDel)!
 EGADS Error: No Attribute -> _body (EG_attributeDel)!
 EGADS Error: No Attribute -> _nface (EG_attributeDel)!
 EGADS Error: No Attribute -> __trace__ (EG_attributeDel)!
 EGADS Error: No Attribute -> _body (EG_attributeDel)!
 EGADS Error: No Attribute -> _nface (EG_attributeDel)!
 EGADS Error: No Attribute -> __trace__ (EG_attributeDel)!
 EGADS Error: No Attribute -> _body (EG_attributeDel)!
 EGADS Error: No Attribute -> _nface (EG_attributeDel)!
 EGADS Error: No Attribute -> __trace__ (EG_attributeDel)!
. EGADS Info: 0 Objects, 0 Reference in Use (of 0) at Close!
..
 EGADS Info: 0 Objects, 0 Reference in Use (of 0) at Close!


 CAPS Info: Hit last success -- going live!

 CAPS Info: Hit last success -- going live!

 CAPS Info: Hit last success -- going live!

 CAPS Info: Hit last success -- going live!

 CAPS Info: Hit last success -- going live!


 CAPS Info: Hit last success -- going live!

 CAPS Info: Hit last success -- going live!

 CAPS Info: Hit last success -- going live!

 CAPS Info: Hit last success -- going live!

 CAPS Info: Hit last success -- going live!

 CAPS Info: Hit last success -- going live!

 CAPS Info: Hit last success -- going live!

 CAPS Info: Hit last success -- going live!

 CAPS Info: Hit last success -- going live!

 CAPS Info: Hit last success -- going live!

 CAPS Info: Hit last success -- going live!

 CAPS Info: Hit last success -- going live!

 CAPS Info: Hit last success -- going live!

 CAPS Info: Hit last success -- going live!

.
 EGADS Info: 0 Objects, 0 Reference in Use (of 0) at Close!


 CAPS Info: Hit last success -- going live!

 CAPS Info: Hit last success -- going live!

 CAPS Info: Hit last success -- going live!

 CAPS Info: Hit last success -- going live!

 CAPS Info: Hit last success -- going live!

 CAPS Info: Hit last success -- going live!

 CAPS Info: Hit last success -- going live!

 CAPS Info: Hit last success -- going live!

 CAPS Info: Hit last success -- going live!

 CAPS Info: Hit last success -- going live!


 CAPS Info: Hit last success -- going live!

 CAPS Info: Hit last success -- going live!

.
 EGADS Info: 0 Objects, 0 Reference in Use (of 0) at Close!


 CAPS Info: Hit last success -- going live!

 CAPS Info: Hit last success -- going live!

 CAPS Info: Hit last success -- going live!

 CAPS Info: Hit last success -- going live!

 CAPS Info: Hit last success -- going live!

 CAPS Info: Hit last success -- going live!

 CAPS Info: Hit last success -- going live!


 CAPS Info: Hit last success -- going live!

 CAPS Info: Hit last success -- going live!

 CAPS Info: Hit last success -- going live!

 CAPS Info: Hit last success -- going live!

 CAPS Info: Hit last success -- going live!

..Linked Parameter Beta to analysis su2 input Beta
Linked Parameter Alpha to analysis su2 input Alpha
No linkable data found for Altitude
No linkable data found for Strings
No linkable data found for Strings2
Linked Parameter Beta to analysis su2 input Beta
Linked Parameter Alpha to analysis su2 input Alpha
............ EGADS Info: 0 Objects, 0 Reference in Use (of 0) at Close!


. EGADS Info: 0 Objects, 0 Reference in Use (of 0) at Close!
. EGADS Info: 0 Objects, 0 Reference in Use (of 0) at Close!
.
. EGADS Info: 0 Objects, 0 Reference in Use (of 0) at Close!
 EGADS Info: 0 Objects, 0 Reference in Use (of 0) at Close!
 EGADS Info: 0 Objects, 0 Reference in Use (of 0) at Close!
. EGADS Info: 0 Objects, 0 Reference in Use (of 0) at Close!
. EGADS Info: 0 Objects, 0 Reference in Use (of 0) at Close!
 EGADS Info: 0 Objects, 0 Reference in Use (of 0) at Close!
 EGADS Info: 0 Objects, 0 Reference in Use (of 0) at Close!
 EGADS Info: 0 Objects, 0 Reference in Use (of 0) at Close!
. EGADS Info: 0 Objects, 0 Reference in Use (of 0) at Close!
.


 CAPS Info: Hit last success -- going live!

... EGADS Info: 0 Objects, 0 Reference in Use (of 0) at Close!
. EGADS Info: 0 Objects, 0 Reference in Use (of 0) at Close!
. EGADS Info: 0 Objects, 0 Reference in Use (of 0) at Close!
.
. EGADS Info: 0 Objects, 0 Reference in Use (of 0) at Close!
.
. EGADS Info: 0 Objects, 0 Reference in Use (of 0) at Close!
. EGADS Info: 0 Objects, 0 Reference in Use (of 0) at Close!
. EGADS Info: 0 Objects, 0 Reference in Use (of 0) at Close!
.
. EGADS Info: 0 Objects, 0 Reference in Use (of 0) at Close!
. EGADS Info: 0 Objects, 0 Reference in Use (of 0) at Close!
. EGADS Info: 0 Objects, 0 Reference in Use (of 0) at Close!
.

. EGADS Info: 0 Objects, 0 Reference in Use (of 0) at Close!
. EGADS Info: 0 Objects, 0 Reference in Use (of 0) at Close!
. EGADS Info: 0 Objects, 0 Reference in Use (of 0) at Close!
.
 EGADS Error: No Attribute -> __numRemaining__ (EG_attributeDel)!
 EGADS Error: No Attribute -> _body (EG_attributeDel)!
 EGADS Error: No Attribute -> _nface (EG_attributeDel)!
 EGADS Error: No Attribute -> __trace__ (EG_attributeDel)!
 EGADS Error: No Attribute -> _body (EG_attributeDel)!
 EGADS Error: No Attribute -> _nface (EG_attributeDel)!
 EGADS Error: No Attribute -> __trace__ (EG_attributeDel)!
 EGADS Error: No Attribute -> _body (EG_attributeDel)!
 EGADS Error: No Attribute -> _nface (EG_attributeDel)!
 EGADS Error: No Attribute -> __trace__ (EG_attributeDel)!
 EGADS Error: No Attribute -> _body (EG_attributeDel)!
 EGADS Error: No Attribute -> _nface (EG_attributeDel)!
 EGADS Error: No Attribute -> __trace__ (EG_attributeDel)!
 EGADS Error: No Attribute -> __numRemaining__ (EG_attributeDel)!
. EGADS Info: 0 Objects, 0 Reference in Use (of 0) at Close!
.--> Opening DESPMTR file "unitGeom.param"
    updating CFGPMTR series                          [ 1, 1] =  8412.000000
    updating CFGPMTR series2                         [ 1, 1] =    20.000000
    updating CFGPMTR VIEW:CFD                        [ 1, 1] =     1.000000
    updating CFGPMTR nrow                            [ 1, 1] =     3.000000
    updating CFGPMTR ncol                            [ 1, 1] =     2.000000
    updating DESPMTR area                            [ 1, 1] =    40.000000
    updating DESPMTR aspect                          [ 1, 1] =     5.000000
    updating DESPMTR taper                           [ 1, 1] =     0.500000
    updating DESPMTR twist                           [ 1, 1] =    15.000000
    updating DESPMTR wing:lesweep                    [ 1, 1] =    30.000000
    updating DESPMTR wing:dihedral                   [ 1, 1] =     1.000000
    updating DESPMTR wing:chord:root                 [ 1, 1] =     1.560000
    updating DESPMTR htail                           [ 1, 1] =     1.000000
    updating DESPMTR htail:chord                     [ 1, 1] =     2.000000
    updating DESPMTR vtail:chord                     [ 1, 1] =     3.000000
    updating DESPMTR vtail                           [ 1, 1] =     4.000000
    updating DESPMTR sphereR                         [ 1, 1] =    80.000000
    updating DESPMTR v@1:d_name                      [ 1, 1] =     1.000000
    updating DESPMTR despMat                         [ 1, 1] =    11.000000
    updating DESPMTR despMat                         [ 1, 2] =    12.000000
    updating DESPMTR despMat                         [ 2, 1] =    13.000000
    updating DESPMTR despMat                         [ 2, 2] =    14.000000
    updating DESPMTR despMat                         [ 3, 1] =    15.000000
    updating DESPMTR despMat                         [ 3, 2] =    16.000000
    updating DESPMTR despCol                         [ 1, 1] =    11.000000
    updating DESPMTR despCol                         [ 2, 1] =    13.000000
    updating DESPMTR despCol                         [ 3, 1] =    15.000000
    updating DESPMTR despRow                         [ 1, 1] =    11.000000
    updating DESPMTR despRow                         [ 1, 2] =    12.000000
    updating DESPMTR despRow                         [ 1, 3] =    13.000000
ERROR:: DESPMTR file "unitGeom.param" not found
 CAPS Error: ocsmSaveDespmtrs = -201 (caps_readParameters)!
 EGADS Info: 0 Objects, 0 Reference in Use (of 0) at Close!
. EGADS Info: 0 Objects, 0 Reference in Use (of 0) at Close!
. EGADS Info: 0 Objects, 0 Reference in Use (of 0) at Close!
................ EGADS Info: 0 Objects, 0 Reference in Use (of 0) at Close!

----------------------------------------------------------------------
Ran 100 tests in 17.085s

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_Beta/7.8/DARWIN_ARM64/EngSketchPad/src/CAPS/aim/unitTest/pyCAPS/
+ make test
python --version
Python 3.11.9
python -u -m unittest discover --verbose
test_journal (test_aflr2.TestAFLR2.test_journal) ... 
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 5
	Name = 2DSlice, index = 1
	Name = TunnelWall, index = 2
	Name = OutFlow, index = 3
	Name = InFlow, index = 4
	Name = Airfoil, index = 5
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 4
	Name = TunnelWall, index = 1
	Name = OutFlow, index = 2
	Name = InFlow, index = 3
	Name = Airfoil, index = 4
Getting 2D mesh for body 1 (of 1)
 
AFLR2    : ---------------------------------------
AFLR2    : AFLR2 LIBRARY
AFLR2    : ADVANCING-FRONT/LOCAL-RECONNECTION
AFLR2    : TRIA/QUAD GRID GENERATOR
AFLR2    : Version Number 9.17.15
AFLR2    : Version Date   04/23/24 @ 12:51AM
AFLR2    : Compile OS     Darwin 23.4.0 arm64
AFLR2    : Compile Date   04/23/24 @ 12:51AM
AFLR2    : Copyright 1994-2021, D.L. Marcum
AFLR2    : ---------------------------------------
 
AFLR2 IC : INPUT DATA CHECK
 
AFLR2 IC : Nodes, Faces      =      2244         0
 
AFLR2    : CPU Time          =     0.000   seconds
 
AFLR2 EG : EDGE GRID RE-GENERATION
 
AFLR2 EG : Nodes, Edges      =      2244      2244
 
AFLR2    : CPU Time          =     0.000   seconds
 
AFLR2 IG : INITIAL GRID GENERATION
 
AFLR2 IG : Nodes, Faces      =         0         2
AFLR2 IG : Nodes, Faces      =       450       902
AFLR2 IG : Nodes, Faces      =       900      1802
AFLR2 IG : Nodes, Faces      =      1145      2292
AFLR2 IG : Nodes, Faces      =      1260      2522
AFLR2 IG : Nodes, Faces      =      1350      2702
AFLR2 IG : Nodes, Faces      =      1360      2722
AFLR2 IG : Nodes, Faces      =      1460      2922
AFLR2 IG : Nodes, Faces      =      1560      3122
AFLR2 IG : Nodes, Faces      =      1660      3322
AFLR2 IG : Nodes, Faces      =      1760      3522
AFLR2 IG : Nodes, Faces      =      1800      3602
AFLR2 IG : Nodes, Faces      =      1860      3722
AFLR2 IG : Nodes, Faces      =      1960      3922
AFLR2 IG : Nodes, Faces      =      2060      4122
AFLR2 IG : Nodes, Faces      =      2085      4172
AFLR2 IG : Nodes, Faces      =      2244      4490
AFLR2 IG : Nodes, Faces      =      2248      4490
AFLR2 IG : Nodes, Faces      =      2244      2244
 
AFLR2    : CPU Time          =     0.028   seconds
 
AFLR2 GG : FIELD GRID GENERATION
 
AFLR2 GG : Nodes, Faces      =      2244      2244
AFLR2 GG : Nodes, Faces      =      4285      6326
AFLR2 GG : Nodes, Faces      =      6135     10026
AFLR2 GG : Nodes, Faces      =      7878     13512
AFLR2 GG : Nodes, Faces      =      9485     16726
AFLR2 GG : Nodes, Faces      =     10981     19718
AFLR2 GG : Nodes, Faces      =     12372     22500
AFLR2 GG : Nodes, Faces      =     13686     25128
AFLR2 GG : Nodes, Faces      =     14908     27572
AFLR2 GG : Nodes, Faces      =     16063     29882
AFLR2 GG : Nodes, Faces      =     17170     32096
AFLR2 GG : Nodes, Faces      =     18222     34200
AFLR2 GG : Nodes, Faces      =     19208     36172
AFLR2 GG : Nodes, Faces      =     20165     38086
AFLR2 GG : Nodes, Faces      =     21087     39930
AFLR2 GG : Nodes, Faces      =     21975     41706
AFLR2 GG : Nodes, Faces      =     22803     43362
AFLR2 GG : Nodes, Faces      =     23582     44920
AFLR2 GG : Nodes, Faces      =     24330     46416
AFLR2 GG : Nodes, Faces      =     25041     47838
AFLR2 GG : Nodes, Faces      =     25723     49202
AFLR2 GG : Nodes, Faces      =     26365     50486
AFLR2 GG : Nodes, Faces      =     26993     51742
AFLR2 GG : Nodes, Faces      =     27556     52868
AFLR2 GG : Nodes, Faces      =     28054     53864
AFLR2 GG : Nodes, Faces      =     28487     54730
AFLR2 GG : Nodes, Faces      =     28847     55450
AFLR2 GG : Nodes, Faces      =     29118     55992
AFLR2 GG : Nodes, Faces      =     29355     56466
AFLR2 GG : Nodes, Faces      =     29553     56862
AFLR2 GG : Nodes, Faces      =     29735     57226
AFLR2 GG : Nodes, Faces      =     29878     57512
AFLR2 GG : Nodes, Faces      =     29969     57694
AFLR2 GG : Nodes, Faces      =     30009     57774
AFLR2 GG : Nodes, Faces      =     30018     57792
AFLR2 GG : Nodes, Faces      =     30019     57794
 
AFLR2    : CPU Time          =     0.061   seconds
 
AFLR2 QI : QUALITY IMPROVEMENT
 
AFLR2 QI : Nodes, Faces      =     30019     57794
 
AFLR2    : CPU Time          =     0.003   seconds
 
AFLR2    : DONE

Writing AFLR3 file ....
Finished writing AFLR3 file

Number of nodes = 30019
Number of elements = 60038
Number of tris = 57794
Number of quad = 0
Getting 2D mesh for body 1 (of 1)
 
AFLR2 IC : INPUT DATA CHECK
 
AFLR2 IC : Nodes, Faces      =      2224         0
 
AFLR2    : CPU Time          =     0.000   seconds
 
AFLR2 EG : EDGE GRID RE-GENERATION
 
AFLR2 EG : Nodes, Edges      =      2224      2224
 
AFLR2    : CPU Time          =     0.000   seconds
 
AFLR2 IG : INITIAL GRID GENERATION
 
AFLR2 IG : Nodes, Faces      =         0         2
AFLR2 IG : Nodes, Faces      =       446       894
AFLR2 IG : Nodes, Faces      =       892      1786
AFLR2 IG : Nodes, Faces      =       918      1838
AFLR2 IG : Nodes, Faces      =      1033      2068
AFLR2 IG : Nodes, Faces      =      1133      2268
AFLR2 IG : Nodes, Faces      =      1233      2468
AFLR2 IG : Nodes, Faces      =      1333      2668
AFLR2 IG : Nodes, Faces      =      1338      2678
AFLR2 IG : Nodes, Faces      =      1433      2868
AFLR2 IG : Nodes, Faces      =      1533      3068
AFLR2 IG : Nodes, Faces      =      1633      3268
AFLR2 IG : Nodes, Faces      =      1733      3468
AFLR2 IG : Nodes, Faces      =      1784      3570
AFLR2 IG : Nodes, Faces      =      1833      3668
AFLR2 IG : Nodes, Faces      =      1858      3718
AFLR2 IG : Nodes, Faces      =      2224      4450
AFLR2 IG : Nodes, Faces      =      2228      4450
AFLR2 IG : Nodes, Faces      =      2224      2224
 
AFLR2    : CPU Time          =     0.014   seconds
 
AFLR2 GG : FIELD GRID GENERATION
 
AFLR2 GG : Nodes, Faces      =      2224      2224
AFLR2 GG : Nodes, Faces      =      4120      6016
AFLR2 GG : Nodes, Faces      =      5820      9416
AFLR2 GG : Nodes, Faces      =      7322     12420
AFLR2 GG : Nodes, Faces      =      8613     15002
AFLR2 GG : Nodes, Faces      =      9793     17362
AFLR2 GG : Nodes, Faces      =     10847     19470
AFLR2 GG : Nodes, Faces      =     11828     21432
AFLR2 GG : Nodes, Faces      =     12749     23274
AFLR2 GG : Nodes, Faces      =     13580     24936
AFLR2 GG : Nodes, Faces      =     14355     26486
AFLR2 GG : Nodes, Faces      =     15088     27952
AFLR2 GG : Nodes, Faces      =     15774     29324
AFLR2 GG : Nodes, Faces      =     16420     30616
AFLR2 GG : Nodes, Faces      =     17013     31802
AFLR2 GG : Nodes, Faces      =     17571     32918
AFLR2 GG : Nodes, Faces      =     18089     33954
AFLR2 GG : Nodes, Faces      =     18573     34922
AFLR2 GG : Nodes, Faces      =     19005     35786
AFLR2 GG : Nodes, Faces      =     19413     36602
AFLR2 GG : Nodes, Faces      =     19779     37334
AFLR2 GG : Nodes, Faces      =     20116     38008
AFLR2 GG : Nodes, Faces      =     20443     38662
AFLR2 GG : Nodes, Faces      =     20756     39288
AFLR2 GG : Nodes, Faces      =     21054     39884
AFLR2 GG : Nodes, Faces      =     21344     40464
AFLR2 GG : Nodes, Faces      =     21621     41018
AFLR2 GG : Nodes, Faces      =     21885     41546
AFLR2 GG : Nodes, Faces      =     22137     42050
AFLR2 GG : Nodes, Faces      =     22387     42550
AFLR2 GG : Nodes, Faces      =     22603     42982
AFLR2 GG : Nodes, Faces      =     22772     43320
AFLR2 GG : Nodes, Faces      =     22912     43600
AFLR2 GG : Nodes, Faces      =     23039     43854
AFLR2 GG : Nodes, Faces      =     23142     44060
AFLR2 GG : Nodes, Faces      =     23205     44186
AFLR2 GG : Nodes, Faces      =     23240     44256
AFLR2 GG : Nodes, Faces      =     23257     44290
AFLR2 GG : Nodes, Faces      =     23269     44314
AFLR2 GG : Nodes, Faces      =     23273     44322
 
AFLR2    : CPU Time          =     0.045   seconds
 
AFLR2 QI : QUALITY IMPROVEMENT
 
AFLR2 QI : Nodes, Faces      =     23273     44322
 
AFLR2    : CPU Time          =     0.003   seconds
 
AFLR2    : DONE

Writing AFLR3 file ....
Finished writing AFLR3 file

Number of nodes = 23273
Number of elements = 46546
Number of tris = 44322
Number of quad = 0
 EGADS Info: 0 Objects, 0 Reference in Use (of 0) at Close!


 CAPS Info: Hit last success -- going live!

 CAPS Info: Hit last success -- going live!

 CAPS Info: Hit last success -- going live!

 CAPS Info: Hit last success -- going live!

 CAPS Info: Hit last success -- going live!

Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 5
	Name = 2DSlice, index = 1
	Name = TunnelWall, index = 2
	Name = OutFlow, index = 3
	Name = InFlow, index = 4
	Name = Airfoil, index = 5
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 4
	Name = TunnelWall, index = 1
	Name = OutFlow, index = 2
	Name = InFlow, index = 3
	Name = Airfoil, index = 4
Getting 2D mesh for body 1 (of 1)
 
AFLR2    : ---------------------------------------
AFLR2    : AFLR2 LIBRARY
AFLR2    : ADVANCING-FRONT/LOCAL-RECONNECTION
AFLR2    : TRIA/QUAD GRID GENERATOR
AFLR2    : Version Number 9.17.15
AFLR2    : Version Date   04/23/24 @ 12:51AM
AFLR2    : Compile OS     Darwin 23.4.0 arm64
AFLR2    : Compile Date   04/23/24 @ 12:51AM
AFLR2    : Copyright 1994-2021, D.L. Marcum
AFLR2    : ---------------------------------------
 
AFLR2 IC : INPUT DATA CHECK
 
AFLR2 IC : Nodes, Faces      =      2244         0
 
AFLR2    : CPU Time          =     0.000   seconds
 
AFLR2 EG : EDGE GRID RE-GENERATION
 
AFLR2 EG : Nodes, Edges      =      2244      2244
 
AFLR2    : CPU Time          =     0.000   seconds
 
AFLR2 IG : INITIAL GRID GENERATION
 
AFLR2 IG : Nodes, Faces      =         0         2
AFLR2 IG : Nodes, Faces      =       450       902
AFLR2 IG : Nodes, Faces      =       900      1802
AFLR2 IG : Nodes, Faces      =      1145      2292
AFLR2 IG : Nodes, Faces      =      1260      2522
AFLR2 IG : Nodes, Faces      =      1350      2702
AFLR2 IG : Nodes, Faces      =      1360      2722
AFLR2 IG : Nodes, Faces      =      1460      2922
AFLR2 IG : Nodes, Faces      =      1560      3122
AFLR2 IG : Nodes, Faces      =      1660      3322
AFLR2 IG : Nodes, Faces      =      1760      3522
AFLR2 IG : Nodes, Faces      =      1800      3602
AFLR2 IG : Nodes, Faces      =      1860      3722
AFLR2 IG : Nodes, Faces      =      1960      3922
AFLR2 IG : Nodes, Faces      =      2060      4122
AFLR2 IG : Nodes, Faces      =      2085      4172
AFLR2 IG : Nodes, Faces      =      2244      4490
AFLR2 IG : Nodes, Faces      =      2248      4490
AFLR2 IG : Nodes, Faces      =      2244      2244
 
AFLR2    : CPU Time          =     0.024   seconds
 
AFLR2 GG : FIELD GRID GENERATION
 
AFLR2 GG : Nodes, Faces      =      2244      2244
AFLR2 GG : Nodes, Faces      =      4285      6326
AFLR2 GG : Nodes, Faces      =      6135     10026
AFLR2 GG : Nodes, Faces      =      7878     13512
AFLR2 GG : Nodes, Faces      =      9485     16726
AFLR2 GG : Nodes, Faces      =     10981     19718
AFLR2 GG : Nodes, Faces      =     12372     22500
AFLR2 GG : Nodes, Faces      =     13686     25128
AFLR2 GG : Nodes, Faces      =     14908     27572
AFLR2 GG : Nodes, Faces      =     16063     29882
AFLR2 GG : Nodes, Faces      =     17170     32096
AFLR2 GG : Nodes, Faces      =     18222     34200
AFLR2 GG : Nodes, Faces      =     19208     36172
AFLR2 GG : Nodes, Faces      =     20165     38086
AFLR2 GG : Nodes, Faces      =     21087     39930
AFLR2 GG : Nodes, Faces      =     21975     41706
AFLR2 GG : Nodes, Faces      =     22803     43362
AFLR2 GG : Nodes, Faces      =     23582     44920
AFLR2 GG : Nodes, Faces      =     24330     46416
AFLR2 GG : Nodes, Faces      =     25041     47838
AFLR2 GG : Nodes, Faces      =     25723     49202
AFLR2 GG : Nodes, Faces      =     26365     50486
AFLR2 GG : Nodes, Faces      =     26993     51742
AFLR2 GG : Nodes, Faces      =     27556     52868
AFLR2 GG : Nodes, Faces      =     28054     53864
AFLR2 GG : Nodes, Faces      =     28487     54730
AFLR2 GG : Nodes, Faces      =     28847     55450
AFLR2 GG : Nodes, Faces      =     29118     55992
AFLR2 GG : Nodes, Faces      =     29355     56466
AFLR2 GG : Nodes, Faces      =     29553     56862
AFLR2 GG : Nodes, Faces      =     29735     57226
AFLR2 GG : Nodes, Faces      =     29878     57512
AFLR2 GG : Nodes, Faces      =     29969     57694
AFLR2 GG : Nodes, Faces      =     30009     57774
AFLR2 GG : Nodes, Faces      =     30018     57792
AFLR2 GG : Nodes, Faces      =     30019     57794
 
AFLR2    : CPU Time          =     0.057   seconds
 
AFLR2 QI : QUALITY IMPROVEMENT
 
AFLR2 QI : Nodes, Faces      =     30019     57794
 
AFLR2    : CPU Time          =     0.011   seconds
 
AFLR2    : DONE

Writing AFLR3 file ....
Finished writing AFLR3 file

Number of nodes = 30019
Number of elements = 60038
Number of tris = 57794
Number of quad = 0

 CAPS Info: Hit last success -- going live!
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 5
	Name = 2DSlice, index = 1
	Name = TunnelWall, index = 2
	Name = OutFlow, index = 3
	Name = InFlow, index = 4
	Name = Airfoil, index = 5
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 4
	Name = TunnelWall, index = 1
	Name = OutFlow, index = 2
	Name = InFlow, index = 3
	Name = Airfoil, index = 4

 CAPS Info: Hit last success -- going live!
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 5
	Name = 2DSlice, index = 1
	Name = TunnelWall, index = 2
	Name = OutFlow, index = 3
	Name = InFlow, index = 4
	Name = Airfoil, index = 5
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 4
	Name = TunnelWall, index = 1
	Name = OutFlow, index = 2
	Name = InFlow, index = 3
	Name = Airfoil, index = 4

 CAPS Info: Hit last success -- going live!

 CAPS Info: Hit last success -- going live!

 CAPS Info: Hit last success -- going live!
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 5
	Name = 2DSlice, index = 1
	Name = TunnelWall, index = 2
	Name = OutFlow, index = 3
	Name = InFlow, index = 4
	Name = Airfoil, index = 5
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 4
	Name = TunnelWall, index = 1
	Name = OutFlow, index = 2
	Name = InFlow, index = 3
	Name = Airfoil, index = 4
Getting 2D mesh for body 1 (of 1)
 
AFLR2    : ---------------------------------------
AFLR2    : AFLR2 LIBRARY
AFLR2    : ADVANCING-FRONT/LOCAL-RECONNECTION
AFLR2    : TRIA/QUAD GRID GENERATOR
AFLR2    : Version Number 9.17.15
AFLR2    : Version Date   04/23/24 @ 12:51AM
AFLR2    : Compile OS     Darwin 23.4.0 arm64
AFLR2    : Compile Date   04/23/24 @ 12:51AM
AFLR2    : Copyright 1994-2021, D.L. Marcum
AFLR2    : ---------------------------------------
 
AFLR2 IC : INPUT DATA CHECK
 
AFLR2 IC : Nodes, Faces      =      2224         0
 
AFLR2    : CPU Time          =     0.000   seconds
 
AFLR2 EG : EDGE GRID RE-GENERATION
 
AFLR2 EG : Nodes, Edges      =      2224      2224
 
AFLR2    : CPU Time          =     0.000   seconds
 
AFLR2 IG : INITIAL GRID GENERATION
 
AFLR2 IG : Nodes, Faces      =         0         2
AFLR2 IG : Nodes, Faces      =       446       894
AFLR2 IG : Nodes, Faces      =       892      1786
AFLR2 IG : Nodes, Faces      =       918      1838
AFLR2 IG : Nodes, Faces      =      1033      2068
AFLR2 IG : Nodes, Faces      =      1133      2268
AFLR2 IG : Nodes, Faces      =      1233      2468
AFLR2 IG : Nodes, Faces      =      1333      2668
AFLR2 IG : Nodes, Faces      =      1338      2678
AFLR2 IG : Nodes, Faces      =      1433      2868
AFLR2 IG : Nodes, Faces      =      1533      3068
AFLR2 IG : Nodes, Faces      =      1633      3268
AFLR2 IG : Nodes, Faces      =      1733      3468
AFLR2 IG : Nodes, Faces      =      1784      3570
AFLR2 IG : Nodes, Faces      =      1833      3668
AFLR2 IG : Nodes, Faces      =      1858      3718
AFLR2 IG : Nodes, Faces      =      2224      4450
AFLR2 IG : Nodes, Faces      =      2228      4450
AFLR2 IG : Nodes, Faces      =      2224      2224
 
AFLR2    : CPU Time          =     0.041   seconds
 
AFLR2 GG : FIELD GRID GENERATION
 
AFLR2 GG : Nodes, Faces      =      2224      2224
AFLR2 GG : Nodes, Faces      =      4120      6016
AFLR2 GG : Nodes, Faces      =      5820      9416
AFLR2 GG : Nodes, Faces      =      7322     12420
AFLR2 GG : Nodes, Faces      =      8613     15002
AFLR2 GG : Nodes, Faces      =      9793     17362
AFLR2 GG : Nodes, Faces      =     10847     19470
AFLR2 GG : Nodes, Faces      =     11828     21432
AFLR2 GG : Nodes, Faces      =     12749     23274
AFLR2 GG : Nodes, Faces      =     13580     24936
AFLR2 GG : Nodes, Faces      =     14355     26486
AFLR2 GG : Nodes, Faces      =     15088     27952
AFLR2 GG : Nodes, Faces      =     15774     29324
AFLR2 GG : Nodes, Faces      =     16420     30616
AFLR2 GG : Nodes, Faces      =     17013     31802
AFLR2 GG : Nodes, Faces      =     17571     32918
AFLR2 GG : Nodes, Faces      =     18089     33954
AFLR2 GG : Nodes, Faces      =     18573     34922
AFLR2 GG : Nodes, Faces      =     19005     35786
AFLR2 GG : Nodes, Faces      =     19413     36602
AFLR2 GG : Nodes, Faces      =     19779     37334
AFLR2 GG : Nodes, Faces      =     20116     38008
AFLR2 GG : Nodes, Faces      =     20443     38662
AFLR2 GG : Nodes, Faces      =     20756     39288
AFLR2 GG : Nodes, Faces      =     21054     39884
AFLR2 GG : Nodes, Faces      =     21344     40464
AFLR2 GG : Nodes, Faces      =     21621     41018
AFLR2 GG : Nodes, Faces      =     21885     41546
AFLR2 GG : Nodes, Faces      =     22137     42050
AFLR2 GG : Nodes, Faces      =     22387     42550
AFLR2 GG : Nodes, Faces      =     22603     42982
AFLR2 GG : Nodes, Faces      =     22772     43320
AFLR2 GG : Nodes, Faces      =     22912     43600
AFLR2 GG : Nodes, Faces      =     23039     43854
AFLR2 GG : Nodes, Faces      =     23142     44060
AFLR2 GG : Nodes, Faces      =     23205     44186
AFLR2 GG : Nodes, Faces      =     23240     44256
AFLR2 GG : Nodes, Faces      =     23257     44290
AFLR2 GG : Nodes, Faces      =     23269     44314
AFLR2 GG : Nodes, Faces      =     23273     44322
 
AFLR2    : CPU Time          =     0.053   seconds
 
AFLR2 QI : QUALITY IMPROVEMENT
 
AFLR2 QI : Nodes, Faces      =     23273     44322
 
AFLR2    : CPU Time          =     0.008   seconds
 
AFLR2    : DONE

Writing AFLR3 file ....
Finished writing AFLR3 file

Number of nodes = 23273
Number of elements = 46546
Number of tris = 44322
Number of quad = 0

 CAPS Info: Hit last success -- going live!
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 5
	Name = 2DSlice, index = 1
	Name = TunnelWall, index = 2
	Name = OutFlow, index = 3
	Name = InFlow, index = 4
	Name = Airfoil, index = 5
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 4
	Name = TunnelWall, index = 1
	Name = OutFlow, index = 2
	Name = InFlow, index = 3
	Name = Airfoil, index = 4

ok
test_phase (test_aflr2.TestAFLR2.test_phase) ... 
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 5
	Name = 2DSlice, index = 1
	Name = TunnelWall, index = 2
	Name = OutFlow, index = 3
	Name = InFlow, index = 4
	Name = Airfoil, index = 5
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 4
	Name = TunnelWall, index = 1
	Name = OutFlow, index = 2
	Name = InFlow, index = 3
	Name = Airfoil, index = 4
Getting 2D mesh for body 1 (of 1)
 
AFLR2    : ---------------------------------------
AFLR2    : AFLR2 LIBRARY
AFLR2    : ADVANCING-FRONT/LOCAL-RECONNECTION
AFLR2    : TRIA/QUAD GRID GENERATOR
AFLR2    : Version Number 9.17.15
AFLR2    : Version Date   04/23/24 @ 12:51AM
AFLR2    : Compile OS     Darwin 23.4.0 arm64
AFLR2    : Compile Date   04/23/24 @ 12:51AM
AFLR2    : Copyright 1994-2021, D.L. Marcum
AFLR2    : ---------------------------------------
 
AFLR2 IC : INPUT DATA CHECK
 
AFLR2 IC : Nodes, Faces      =      2244         0
 
AFLR2    : CPU Time          =     0.000   seconds
 
AFLR2 EG : EDGE GRID RE-GENERATION
 
AFLR2 EG : Nodes, Edges      =      2244      2244
 
AFLR2    : CPU Time          =     0.000   seconds
 
AFLR2 IG : INITIAL GRID GENERATION
 
AFLR2 IG : Nodes, Faces      =         0         2
AFLR2 IG : Nodes, Faces      =       450       902
AFLR2 IG : Nodes, Faces      =       900      1802
AFLR2 IG : Nodes, Faces      =      1145      2292
AFLR2 IG : Nodes, Faces      =      1260      2522
AFLR2 IG : Nodes, Faces      =      1350      2702
AFLR2 IG : Nodes, Faces      =      1360      2722
AFLR2 IG : Nodes, Faces      =      1460      2922
AFLR2 IG : Nodes, Faces      =      1560      3122
AFLR2 IG : Nodes, Faces      =      1660      3322
AFLR2 IG : Nodes, Faces      =      1760      3522
AFLR2 IG : Nodes, Faces      =      1800      3602
AFLR2 IG : Nodes, Faces      =      1860      3722
AFLR2 IG : Nodes, Faces      =      1960      3922
AFLR2 IG : Nodes, Faces      =      2060      4122
AFLR2 IG : Nodes, Faces      =      2085      4172
AFLR2 IG : Nodes, Faces      =      2244      4490
AFLR2 IG : Nodes, Faces      =      2248      4490
AFLR2 IG : Nodes, Faces      =      2244      2244
 
AFLR2    : CPU Time          =     0.022   seconds
 
AFLR2 GG : FIELD GRID GENERATION
 
AFLR2 GG : Nodes, Faces      =      2244      2244
AFLR2 GG : Nodes, Faces      =      4285      6326
AFLR2 GG : Nodes, Faces      =      6135     10026
AFLR2 GG : Nodes, Faces      =      7878     13512
AFLR2 GG : Nodes, Faces      =      9485     16726
AFLR2 GG : Nodes, Faces      =     10981     19718
AFLR2 GG : Nodes, Faces      =     12372     22500
AFLR2 GG : Nodes, Faces      =     13686     25128
AFLR2 GG : Nodes, Faces      =     14908     27572
AFLR2 GG : Nodes, Faces      =     16063     29882
AFLR2 GG : Nodes, Faces      =     17170     32096
AFLR2 GG : Nodes, Faces      =     18222     34200
AFLR2 GG : Nodes, Faces      =     19208     36172
AFLR2 GG : Nodes, Faces      =     20165     38086
AFLR2 GG : Nodes, Faces      =     21087     39930
AFLR2 GG : Nodes, Faces      =     21975     41706
AFLR2 GG : Nodes, Faces      =     22803     43362
AFLR2 GG : Nodes, Faces      =     23582     44920
AFLR2 GG : Nodes, Faces      =     24330     46416
AFLR2 GG : Nodes, Faces      =     25041     47838
AFLR2 GG : Nodes, Faces      =     25723     49202
AFLR2 GG : Nodes, Faces      =     26365     50486
AFLR2 GG : Nodes, Faces      =     26993     51742
AFLR2 GG : Nodes, Faces      =     27556     52868
AFLR2 GG : Nodes, Faces      =     28054     53864
AFLR2 GG : Nodes, Faces      =     28487     54730
AFLR2 GG : Nodes, Faces      =     28847     55450
AFLR2 GG : Nodes, Faces      =     29118     55992
AFLR2 GG : Nodes, Faces      =     29355     56466
AFLR2 GG : Nodes, Faces      =     29553     56862
AFLR2 GG : Nodes, Faces      =     29735     57226
AFLR2 GG : Nodes, Faces      =     29878     57512
AFLR2 GG : Nodes, Faces      =     29969     57694
AFLR2 GG : Nodes, Faces      =     30009     57774
AFLR2 GG : Nodes, Faces      =     30018     57792
AFLR2 GG : Nodes, Faces      =     30019     57794
 
AFLR2    : CPU Time          =     0.055   seconds
 
AFLR2 QI : QUALITY IMPROVEMENT
 
AFLR2 QI : Nodes, Faces      =     30019     57794
 
AFLR2    : CPU Time          =     0.003   seconds
 
AFLR2    : DONE

Writing AFLR3 file ....
Finished writing AFLR3 file

Number of nodes = 30019
Number of elements = 60038
Number of tris = 57794
Number of quad = 0

Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 5
	Name = 2DSlice, index = 1
	Name = TunnelWall, index = 2
	Name = OutFlow, index = 3
	Name = InFlow, index = 4
	Name = Airfoil, index = 5
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 4
	Name = TunnelWall, index = 1
	Name = OutFlow, index = 2
	Name = InFlow, index = 3
	Name = Airfoil, index = 4
Getting 2D mesh for body 1 (of 1)
 
AFLR2    : ---------------------------------------
AFLR2    : AFLR2 LIBRARY
AFLR2    : ADVANCING-FRONT/LOCAL-RECONNECTION
AFLR2    : TRIA/QUAD GRID GENERATOR
AFLR2    : Version Number 9.17.15
AFLR2    : Version Date   04/23/24 @ 12:51AM
AFLR2    : Compile OS     Darwin 23.4.0 arm64
AFLR2    : Compile Date   04/23/24 @ 12:51AM
AFLR2    : Copyright 1994-2021, D.L. Marcum
AFLR2    : ---------------------------------------
 
AFLR2 IC : INPUT DATA CHECK
 
AFLR2 IC : Nodes, Faces      =        48         0
 
AFLR2    : CPU Time          =     0.000   seconds
 
AFLR2 EG : EDGE GRID RE-GENERATION
 
AFLR2 EG : Nodes, Edges      =        48        48
 
AFLR2    : CPU Time          =     0.000   seconds
 
AFLR2 IG : INITIAL GRID GENERATION
 
AFLR2 IG : Nodes, Faces      =         0         2
AFLR2 IG : Nodes, Faces      =        10        22
AFLR2 IG : Nodes, Faces      =        20        42
AFLR2 IG : Nodes, Faces      =        30        62
AFLR2 IG : Nodes, Faces      =        40        82
AFLR2 IG : Nodes, Faces      =        45        92
AFLR2 IG : Nodes, Faces      =        46        94
AFLR2 IG : Nodes, Faces      =        48        98
AFLR2 IG : Nodes, Faces      =        52        98
AFLR2 IG : Nodes, Faces      =        48        48
 
AFLR2    : CPU Time          =     0.000   seconds
 
AFLR2 GG : FIELD GRID GENERATION
 
AFLR2 GG : Nodes, Faces      =        48        48
AFLR2 GG : Nodes, Faces      =        88       128
AFLR2 GG : Nodes, Faces      =       109       170
AFLR2 GG : Nodes, Faces      =       124       200
AFLR2 GG : Nodes, Faces      =       136       224
AFLR2 GG : Nodes, Faces      =       148       248
AFLR2 GG : Nodes, Faces      =       160       272
AFLR2 GG : Nodes, Faces      =       172       296
AFLR2 GG : Nodes, Faces      =       182       316
AFLR2 GG : Nodes, Faces      =       188       328
AFLR2 GG : Nodes, Faces      =       190       332
 
AFLR2    : CPU Time          =     0.000   seconds
 
AFLR2 QI : QUALITY IMPROVEMENT
 
AFLR2 QI : Nodes, Faces      =       190       332
 
AFLR2    : CPU Time          =     0.000   seconds
 
AFLR2    : DONE

Writing AFLR3 file ....
Finished writing AFLR3 file

Number of nodes = 190
Number of elements = 380
Number of tris = 332
Number of quad = 0
ok
test_reenter (test_aflr2.TestAFLR2.test_reenter) ... 
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 5
	Name = 2DSlice, index = 1
	Name = TunnelWall, index = 2
	Name = OutFlow, index = 3
	Name = InFlow, index = 4
	Name = Airfoil, index = 5
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 4
	Name = TunnelWall, index = 1
	Name = OutFlow, index = 2
	Name = InFlow, index = 3
	Name = Airfoil, index = 4

Getting mesh sizing parameters
	Mesh sizing name - 2DSlice
	Mesh sizing name - Airfoil
	Mesh sizing name - InFlow
	Mesh sizing name - OutFlow
	Mesh sizing name - TunnelWall
	Done getting mesh sizing parameters
Getting 2D mesh for body 1 (of 1)
 
AFLR2    : ---------------------------------------
AFLR2    : AFLR2 LIBRARY
AFLR2    : ADVANCING-FRONT/LOCAL-RECONNECTION
AFLR2    : TRIA/QUAD GRID GENERATOR
AFLR2    : Version Number 9.17.15
AFLR2    : Version Date   04/23/24 @ 12:51AM
AFLR2    : Compile OS     Darwin 23.4.0 arm64
AFLR2    : Compile Date   04/23/24 @ 12:51AM
AFLR2    : Copyright 1994-2021, D.L. Marcum
AFLR2    : ---------------------------------------
 
AFLR2 IC : INPUT DATA CHECK
 
AFLR2 IC : Nodes, Faces      =       344         0
 
AFLR2    : CPU Time          =     0.000   seconds
 
AFLR2 EG : EDGE GRID RE-GENERATION
 
AFLR2 EG : Nodes, Edges      =       344       344
 
AFLR2    : CPU Time          =     0.000   seconds
 
AFLR2 IG : INITIAL GRID GENERATION
 
AFLR2 IG : Nodes, Faces      =         0         2
AFLR2 IG : Nodes, Faces      =        70       142
AFLR2 IG : Nodes, Faces      =       140       282
AFLR2 IG : Nodes, Faces      =       210       422
AFLR2 IG : Nodes, Faces      =       280       562
AFLR2 IG : Nodes, Faces      =       339       680
AFLR2 IG : Nodes, Faces      =       340       682
AFLR2 IG : Nodes, Faces      =       344       690
AFLR2 IG : Nodes, Faces      =       348       690
AFLR2 IG : Nodes, Faces      =       344       344
 
AFLR2    : CPU Time          =     0.000   seconds
 
AFLR2 GG : FIELD GRID GENERATION
 
AFLR2 GG : Nodes, Faces      =       344       344
AFLR2 GG : Nodes, Faces      =       679      1014
AFLR2 GG : Nodes, Faces      =      1006      1668
AFLR2 GG : Nodes, Faces      =      1321      2298
AFLR2 GG : Nodes, Faces      =      1604      2864
AFLR2 GG : Nodes, Faces      =      1886      3428
AFLR2 GG : Nodes, Faces      =      2155      3966
AFLR2 GG : Nodes, Faces      =      2409      4474
AFLR2 GG : Nodes, Faces      =      2649      4954
AFLR2 GG : Nodes, Faces      =      2867      5390
AFLR2 GG : Nodes, Faces      =      3063      5782
AFLR2 GG : Nodes, Faces      =      3243      6142
AFLR2 GG : Nodes, Faces      =      3400      6456
AFLR2 GG : Nodes, Faces      =      3540      6736
AFLR2 GG : Nodes, Faces      =      3665      6986
AFLR2 GG : Nodes, Faces      =      3786      7228
AFLR2 GG : Nodes, Faces      =      3900      7456
AFLR2 GG : Nodes, Faces      =      4010      7676
AFLR2 GG : Nodes, Faces      =      4114      7884
AFLR2 GG : Nodes, Faces      =      4209      8074
AFLR2 GG : Nodes, Faces      =      4292      8240
AFLR2 GG : Nodes, Faces      =      4368      8392
AFLR2 GG : Nodes, Faces      =      4439      8534
AFLR2 GG : Nodes, Faces      =      4503      8662
AFLR2 GG : Nodes, Faces      =      4560      8776
AFLR2 GG : Nodes, Faces      =      4611      8878
AFLR2 GG : Nodes, Faces      =      4650      8956
AFLR2 GG : Nodes, Faces      =      4677      9010
AFLR2 GG : Nodes, Faces      =      4695      9046
AFLR2 GG : Nodes, Faces      =      4705      9066
 
AFLR2    : CPU Time          =     0.005   seconds
 
AFLR2 QI : QUALITY IMPROVEMENT
 
AFLR2 QI : Nodes, Faces      =      4705      9066
 
AFLR2    : CPU Time          =     0.001   seconds
 
AFLR2    : DONE

Writing AFLR3 file ....
Finished writing AFLR3 file

Number of nodes = 4705
Number of elements = 9410
Number of tris = 9066
Number of quad = 0

Writing Binary VTK file ....
Finished writing Binary VTK file


Writing vtk file ....

Writing vtk general file ....
Finished writing vtk file

libMeshb expects 2D meshes in the x-y plane... attempting to rotate mesh!Swapping z and y coordinates!
Writing FAST file ....
Finished writing FAST file


Writing SU2 file ....
SU2 expects 2D meshes in the x-y plane... attempting to rotate mesh!
Swapping z and y coordinates!
Finished writing SU2 file


Writing exodus file ....
Exodus expects 2D meshes in the x-y plane... attempting to rotate mesh!
Swapping z and y coordinates!
	Block: 'Block1_tri', blk_id 1, num_entries 9066
	Sideset: 'Airfoil', set_id 1, num_entries 198
	Sideset: 'InFlow', set_id 2, num_entries 24
	Sideset: 'OutFlow', set_id 3, num_entries 24
	Sideset: 'TunnelWall', set_id 4, num_entries 98
Finished writing Exodus file


Writing Binary STL file ....
Finished writing Binary STL file


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


Writing Tecplot file ....
Finished writing Tecplot file


Getting mesh sizing parameters
	Mesh sizing name - 2DSlice
	Mesh sizing name - Airfoil
	Mesh sizing name - InFlow
	Mesh sizing name - OutFlow
	Mesh sizing name - TunnelWall
	Done getting mesh sizing parameters
Getting 2D mesh for body 1 (of 1)
 
AFLR2 IC : INPUT DATA CHECK
 
AFLR2 IC : Nodes, Faces      =       344         0
 
AFLR2    : CPU Time          =     0.000   seconds
 
AFLR2 EG : EDGE GRID RE-GENERATION
 
AFLR2 EG : Nodes, Edges      =       344       344
 
AFLR2    : CPU Time          =     0.000   seconds
 
AFLR2 IG : INITIAL GRID GENERATION
 
AFLR2 IG : Nodes, Faces      =         0         2
AFLR2 IG : Nodes, Faces      =        70       142
AFLR2 IG : Nodes, Faces      =       140       282
AFLR2 IG : Nodes, Faces      =       210       422
AFLR2 IG : Nodes, Faces      =       280       562
AFLR2 IG : Nodes, Faces      =       339       680
AFLR2 IG : Nodes, Faces      =       340       682
AFLR2 IG : Nodes, Faces      =       344       690
AFLR2 IG : Nodes, Faces      =       348       690
AFLR2 IG : Nodes, Faces      =       344       344
 
AFLR2    : CPU Time          =     0.000   seconds
 
AFLR2 GG : FIELD GRID GENERATION
 
AFLR2 GGp: Nodes, Faces      =       344       344
AFLR2 GGp: Nodes, Faces      =       682      1020
AFLR2 GGp: Nodes, Faces      =      1010      1676
AFLR2 GGp: Nodes, Faces      =      1316      2288
AFLR2 GGp: Nodes, Faces      =      1592      2840
AFLR2 GGp: Nodes, Faces      =      1855      3366
AFLR2 GGp: Nodes, Faces      =      2106      3868
AFLR2 GGp: Nodes, Faces      =      2341      4338
AFLR2 GGp: Nodes, Faces      =      2551      4758
AFLR2 GGp: Nodes, Faces      =      2741      5138
AFLR2 GGp: Nodes, Faces      =      2917      5490
AFLR2 GGp: Nodes, Faces      =      3082      5820
AFLR2 GGp: Nodes, Faces      =      3240      6136
AFLR2 GGp: Nodes, Faces      =      3379      6414
AFLR2 GGp: Nodes, Faces      =      3513      6682
AFLR2 GGp: Nodes, Faces      =      3642      6940
AFLR2 GGp: Nodes, Faces      =      3748      7152
AFLR2 GGp: Nodes, Faces      =      3846      7348
AFLR2 GGp: Nodes, Faces      =      3931      7518
AFLR2 GGp: Nodes, Faces      =      3999      7654
AFLR2 GGp: Nodes, Faces      =      4044      7744
AFLR2 GGp: Nodes, Faces      =      4058      7772
 
AFLR2    : CPU Time          =     0.014   seconds
 
AFLR2 QI : QUALITY IMPROVEMENT
 
AFLR2 QI : Nodes, Faces      =      4058      7772
AFLR2 QI : Nodes, Faces      =      4057       364
AFLR2 QI : Nodes, Faces      =      4057      3703
AFLR2 QI : Nodes, Faces      =      4057      7770
AFLR2 QI : Nodes, Faces      =      4056       344
AFLR2 QI : Nodes, Faces      =      4056      3712
AFLR2 QI : Nodes, Faces      =      4056      7768
AFLR2 QI : Nodes, Faces      =      4055       348
AFLR2 QI : Nodes, Faces      =      4055      3709
AFLR2 QI : Nodes, Faces      =      4055      7766
AFLR2 QI : Nodes, Faces      =      4055       392
AFLR2 QI : Nodes, Faces      =      4055      3687
AFLR2 QI : Nodes, Faces      =      4055      7766
AFLR2 QI : Nodes, Faces      =      4055       386
AFLR2 QI : Nodes, Faces      =      4055      3690
AFLR2 QI : Nodes, Faces      =      4055       386
AFLR2 QI : Nodes, Faces      =      4055      3690
 
AFLR2    : CPU Time          =     0.009   seconds
 
AFLR2    : DONE

Writing AFLR3 file ....
Finished writing AFLR3 file

Number of nodes = 4055
Number of elements = 4420
Number of tris = 386
Number of quad = 3690

Writing Binary VTK file ....
Finished writing Binary VTK file


Writing vtk file ....

Writing vtk general file ....
Finished writing vtk file

libMeshb expects 2D meshes in the x-y plane... attempting to rotate mesh!Swapping z and y coordinates!
Writing SU2 file ....
SU2 expects 2D meshes in the x-y plane... attempting to rotate mesh!
Swapping z and y coordinates!
Finished writing SU2 file


Writing exodus file ....
Exodus expects 2D meshes in the x-y plane... attempting to rotate mesh!
Swapping z and y coordinates!
	Block: 'Block1_tri', blk_id 1, num_entries 386
	Block: 'Block2_quad', blk_id 2, num_entries 3690
	Sideset: 'Airfoil', set_id 1, num_entries 198
	Sideset: 'InFlow', set_id 2, num_entries 24
	Sideset: 'OutFlow', set_id 3, num_entries 24
	Sideset: 'TunnelWall', set_id 4, num_entries 98
Finished writing Exodus file


Writing Binary STL file ....
Finished writing Binary STL file


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


Writing Tecplot file ....
Finished writing Tecplot file

ok
test_setInput (test_aflr2.TestAFLR2.test_setInput) ... 
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 5
	Name = 2DSlice, index = 1
	Name = TunnelWall, index = 2
	Name = OutFlow, index = 3
	Name = InFlow, index = 4
	Name = Airfoil, index = 5
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 4
	Name = TunnelWall, index = 1
	Name = OutFlow, index = 2
	Name = InFlow, index = 3
	Name = Airfoil, index = 4

Getting mesh sizing parameters
	Mesh sizing name - 2DSlice
	Mesh sizing name - Airfoil
	Mesh sizing name - InFlow
	Mesh sizing name - OutFlow
	Mesh sizing name - TunnelWall
	Done getting mesh sizing parameters
Getting 2D mesh for body 1 (of 1)
 
AFLR2    : ---------------------------------------
AFLR2    : AFLR2 LIBRARY
AFLR2    : ADVANCING-FRONT/LOCAL-RECONNECTION
AFLR2    : TRIA/QUAD GRID GENERATOR
AFLR2    : Version Number 9.17.15
AFLR2    : Version Date   04/23/24 @ 12:51AM
AFLR2    : Compile OS     Darwin 23.4.0 arm64
AFLR2    : Compile Date   04/23/24 @ 12:51AM
AFLR2    : Copyright 1994-2021, D.L. Marcum
AFLR2    : ---------------------------------------
 
AFLR2 IC : INPUT DATA CHECK
 
AFLR2 IC : Nodes, Faces      =       344         0
 
AFLR2    : CPU Time          =     0.000   seconds
 
AFLR2 EG : EDGE GRID RE-GENERATION
 
AFLR2 EG : Nodes, Edges      =       344       344
 
AFLR2    : CPU Time          =     0.000   seconds
 
AFLR2 IG : INITIAL GRID GENERATION
 
AFLR2 IG : Nodes, Faces      =         0         2
AFLR2 IG : Nodes, Faces      =        70       142
AFLR2 IG : Nodes, Faces      =       140       282
AFLR2 IG : Nodes, Faces      =       210       422
AFLR2 IG : Nodes, Faces      =       280       562
AFLR2 IG : Nodes, Faces      =       339       680
AFLR2 IG : Nodes, Faces      =       340       682
AFLR2 IG : Nodes, Faces      =       344       690
AFLR2 IG : Nodes, Faces      =       348       690
AFLR2 IG : Nodes, Faces      =       344       344
 
AFLR2    : CPU Time          =     0.000   seconds
 
AFLR2 GG : FIELD GRID GENERATION
 
AFLR2 GGp: Nodes, Faces      =       344       344
AFLR2 GGp: Nodes, Faces      =       682      1020
AFLR2 GGp: Nodes, Faces      =      1010      1676
AFLR2 GGp: Nodes, Faces      =      1316      2288
AFLR2 GGp: Nodes, Faces      =      1592      2840
AFLR2 GGp: Nodes, Faces      =      1855      3366
AFLR2 GGp: Nodes, Faces      =      2106      3868
AFLR2 GGp: Nodes, Faces      =      2341      4338
AFLR2 GGp: Nodes, Faces      =      2551      4758
AFLR2 GGp: Nodes, Faces      =      2741      5138
AFLR2 GGp: Nodes, Faces      =      2917      5490
AFLR2 GGp: Nodes, Faces      =      3082      5820
AFLR2 GGp: Nodes, Faces      =      3240      6136
AFLR2 GGp: Nodes, Faces      =      3379      6414
AFLR2 GGp: Nodes, Faces      =      3513      6682
AFLR2 GGp: Nodes, Faces      =      3642      6940
AFLR2 GGp: Nodes, Faces      =      3748      7152
AFLR2 GGp: Nodes, Faces      =      3846      7348
AFLR2 GGp: Nodes, Faces      =      3931      7518
AFLR2 GGp: Nodes, Faces      =      3999      7654
AFLR2 GGp: Nodes, Faces      =      4044      7744
AFLR2 GGp: Nodes, Faces      =      4058      7772
 
AFLR2    : CPU Time          =     0.006   seconds
 
AFLR2 QI : QUALITY IMPROVEMENT
 
AFLR2 QI : Nodes, Faces      =      4058      7772
AFLR2 QI : Nodes, Faces      =      4057       364
AFLR2 QI : Nodes, Faces      =      4057      3703
AFLR2 QI : Nodes, Faces      =      4057      7770
AFLR2 QI : Nodes, Faces      =      4056       344
AFLR2 QI : Nodes, Faces      =      4056      3712
AFLR2 QI : Nodes, Faces      =      4056      7768
AFLR2 QI : Nodes, Faces      =      4055       348
AFLR2 QI : Nodes, Faces      =      4055      3709
AFLR2 QI : Nodes, Faces      =      4055      7766
AFLR2 QI : Nodes, Faces      =      4055       392
AFLR2 QI : Nodes, Faces      =      4055      3687
AFLR2 QI : Nodes, Faces      =      4055      7766
AFLR2 QI : Nodes, Faces      =      4055       386
AFLR2 QI : Nodes, Faces      =      4055      3690
AFLR2 QI : Nodes, Faces      =      4055       386
AFLR2 QI : Nodes, Faces      =      4055      3690
 
AFLR2    : CPU Time          =     0.003   seconds
 
AFLR2    : DONE

Writing AFLR3 file ....
Finished writing AFLR3 file

Number of nodes = 4055
Number of elements = 4420
Number of tris = 386
Number of quad = 3690

Writing Tecplot file ....
Finished writing Tecplot file

ok
test_Multiple_Mesh (test_aflr3.TestAFLR3.test_Multiple_Mesh) ... ERROR:: BAD STATUS = -276 from matsol (called from solveSketchOrig:61976)

Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 7
	Name = box, index = 1
	Name = cylinder, index = 2
	Name = cone, index = 3
	Name = torus, index = 4
	Name = sphere, index = 5
	Name = boxhole, index = 6
	Name = bullet, index = 7
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 1
	Name = box, index = 1
AFLR4    : Proximity BG Surface Grid Generation Skipped
AFLR4    : No Modifications Required
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 1
	Name = box, index = 1
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 7
	Name = box, index = 1
	Name = cylinder, index = 2
	Name = cone, index = 3
	Name = torus, index = 4
	Name = sphere, index = 5
	Name = boxhole, index = 6
	Name = bullet, index = 7
Getting volume mesh for body 1 (of 7)
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = box, index = 1
 
AFLR2    : ---------------------------------------
AFLR2    : AFLR2 LIBRARY
AFLR2    : ADVANCING-FRONT/LOCAL-RECONNECTION
AFLR2    : TRIA/QUAD GRID GENERATOR
AFLR2    : Version Number 9.17.15
AFLR2    : Version Date   04/23/24 @ 12:51AM
AFLR2    : Compile OS     Darwin 23.4.0 arm64
AFLR2    : Compile Date   04/23/24 @ 12:51AM
AFLR2    : Copyright 1994-2021, D.L. Marcum
AFLR2    : ---------------------------------------
 
AFLR4    : ---------------------------------------
AFLR4    : AFLR4 LIBRARY
AFLR4    : ADVANCING-FRONT/LOCAL-RECONNECTION
AFLR4    : TRIA/QUAD SURFACE GRID GENERATOR
AFLR4    : Version Number 11.5.14
AFLR4    : Version Date   04/18/24 @ 12:45PM
AFLR4    : Compile OS     Darwin 23.4.0 arm64
AFLR4    : Compile Date   04/18/24 @ 03:04PM
AFLR4    : Copyright 1994-2021, D.L. Marcum
AFLR4    : ---------------------------------------

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

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------
Volume mesh for body 1 (of 7):
	Number of nodes          = 1198
	Number of elements       = 6307
	Number of triangles      = 1332
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 4975
	Number of pyramids       = 0
	Number of prisms         = 0
	Number of hexahedrals    = 0
Getting volume mesh for body 2 (of 7)
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = cylinder, index = 1

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

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------
Volume mesh for body 2 (of 7):
	Number of nodes          = 6226
	Number of elements       = 34532
	Number of triangles      = 4438
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 30094
	Number of pyramids       = 0
	Number of prisms         = 0
	Number of hexahedrals    = 0
Getting volume mesh for body 3 (of 7)
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = cone, index = 1

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

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------
Volume mesh for body 3 (of 7):
	Number of nodes          = 13688
	Number of elements       = 76798
	Number of triangles      = 8142
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 68656
	Number of pyramids       = 0
	Number of prisms         = 0
	Number of hexahedrals    = 0
Getting volume mesh for body 4 (of 7)
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = torus, index = 1

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

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------
Volume mesh for body 4 (of 7):
	Number of nodes          = 41861
	Number of elements       = 237846
	Number of triangles      = 19888
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 217958
	Number of pyramids       = 0
	Number of prisms         = 0
	Number of hexahedrals    = 0
Getting volume mesh for body 5 (of 7)
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = sphere, index = 1

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

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------
Volume mesh for body 5 (of 7):
	Number of nodes          = 4339
	Number of elements       = 24073
	Number of triangles      = 3010
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 21063
	Number of pyramids       = 0
	Number of prisms         = 0
	Number of hexahedrals    = 0
Getting volume mesh for body 6 (of 7)
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = boxhole, index = 1

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

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------
Volume mesh for body 6 (of 7):
	Number of nodes          = 11025
	Number of elements       = 60915
	Number of triangles      = 8632
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 52283
	Number of pyramids       = 0
	Number of prisms         = 0
	Number of hexahedrals    = 0
Getting volume mesh for body 7 (of 7)
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = bullet, index = 1

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

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------
Volume mesh for body 7 (of 7):
	Number of nodes          = 10398
	Number of elements       = 58234
	Number of triangles      = 6366
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 51868
	Number of pyramids       = 0
	Number of prisms         = 0
	Number of hexahedrals    = 0

Writing Tecplot file ....
Finished writing Tecplot file


Writing Tecplot file ....
Finished writing Tecplot file


Writing Tecplot file ....
Finished writing Tecplot file


Writing Tecplot file ....
Finished writing Tecplot file


Writing Tecplot file ....
Finished writing Tecplot file


Writing Tecplot file ....
Finished writing Tecplot file


Writing Tecplot file ....
Finished writing Tecplot file

AFLR4    : Proximity BG Surface Grid Generation Skipped
AFLR4    : No Modifications Required
Getting volume mesh for body 1 (of 7)

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

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

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

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

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

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

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

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

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

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

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

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

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

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------
Volume mesh:
	Number of nodes          = 88735
	Number of elements       = 498705
	Number of triangles      = 51808
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 446897
	Number of pyramids       = 0
	Number of prisms         = 0
	Number of hexahedrals    = 0

Writing Tecplot file ....
Finished writing Tecplot file

ok
test_all (test_aflr3.TestAFLR3.test_all) ... ERROR:: BAD STATUS = -276 from matsol (called from solveSketchOrig:61976)

Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 8
	Name = box, index = 1
	Name = cylinder, index = 2
	Name = cone, index = 3
	Name = torus, index = 4
	Name = sphere, index = 5
	Name = boxhole, index = 6
	Name = bullet, index = 7
	Name = farfield, index = 8
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 1
	Name = box, index = 1
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 1
	Name = box, index = 1
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 8
	Name = box, index = 1
	Name = cylinder, index = 2
	Name = cone, index = 3
	Name = torus, index = 4
	Name = sphere, index = 5
	Name = boxhole, index = 6
	Name = bullet, index = 7
	Name = farfield, index = 8
Getting volume mesh
 
AFLR2    : ---------------------------------------
AFLR2    : AFLR2 LIBRARY
AFLR2    : ADVANCING-FRONT/LOCAL-RECONNECTION
AFLR2    : TRIA/QUAD GRID GENERATOR
AFLR2    : Version Number 9.17.15
AFLR2    : Version Date   04/23/24 @ 12:51AM
AFLR2    : Compile OS     Darwin 23.4.0 arm64
AFLR2    : Compile Date   04/23/24 @ 12:51AM
AFLR2    : Copyright 1994-2021, D.L. Marcum
AFLR2    : ---------------------------------------
 
AFLR4    : ---------------------------------------
AFLR4    : AFLR4 LIBRARY
AFLR4    : ADVANCING-FRONT/LOCAL-RECONNECTION
AFLR4    : TRIA/QUAD SURFACE GRID GENERATOR
AFLR4    : Version Number 11.5.14
AFLR4    : Version Date   04/18/24 @ 12:45PM
AFLR4    : Compile OS     Darwin 23.4.0 arm64
AFLR4    : Compile Date   04/18/24 @ 03:04PM
AFLR4    : Copyright 1994-2021, D.L. Marcum
AFLR4    : ---------------------------------------

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

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

Writing Tecplot file ....
Finished writing Tecplot file

ok
test_box (test_aflr3.TestAFLR3.test_box) ... Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 2
	Name = box, index = 1
	Name = farfield, index = 2
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 1
	Name = box, index = 1
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 1
	Name = box, index = 1
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 2
	Name = box, index = 1
	Name = farfield, index = 2
Getting volume mesh

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

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------
Volume mesh:
	Number of nodes          = 2585
	Number of elements       = 13784
	Number of triangles      = 2758
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 11026
	Number of pyramids       = 0
	Number of prisms         = 0
	Number of hexahedrals    = 0

Writing Tecplot file ....
Finished writing Tecplot file

ok
test_boxhole (test_aflr3.TestAFLR3.test_boxhole) ... Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 2
	Name = boxhole, index = 1
	Name = farfield, index = 2
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 0
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 0
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 2
	Name = boxhole, index = 1
	Name = farfield, index = 2
Getting volume mesh

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

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------
Volume mesh:
	Number of nodes          = 3615
	Number of elements       = 19589
	Number of triangles      = 3392
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 16197
	Number of pyramids       = 0
	Number of prisms         = 0
	Number of hexahedrals    = 0

Writing Tecplot file ....
Finished writing Tecplot file

ok
test_bullet (test_aflr3.TestAFLR3.test_bullet) ... Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 2
	Name = bullet, index = 1
	Name = farfield, index = 2
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 0
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 0
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 2
	Name = bullet, index = 1
	Name = farfield, index = 2
Getting volume mesh

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

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------
Volume mesh:
	Number of nodes          = 5438
	Number of elements       = 30214
	Number of triangles      = 3654
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 26560
	Number of pyramids       = 0
	Number of prisms         = 0
	Number of hexahedrals    = 0

Writing Tecplot file ....
Finished writing Tecplot file

ok
test_cone (test_aflr3.TestAFLR3.test_cone) ... Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 2
	Name = cone, index = 1
	Name = farfield, index = 2
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 0
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 0
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 2
	Name = cone, index = 1
	Name = farfield, index = 2
Getting volume mesh

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

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------
Volume mesh:
	Number of nodes          = 4697
	Number of elements       = 26013
	Number of triangles      = 3324
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 22689
	Number of pyramids       = 0
	Number of prisms         = 0
	Number of hexahedrals    = 0

Writing Tecplot file ....
Finished writing Tecplot file

ok
test_cylinder (test_aflr3.TestAFLR3.test_cylinder) ... Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 2
	Name = cylinder, index = 1
	Name = farfield, index = 2
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 0
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 0
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 2
	Name = cylinder, index = 1
	Name = farfield, index = 2
Getting volume mesh

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

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------
Volume mesh:
	Number of nodes          = 5467
	Number of elements       = 30346
	Number of triangles      = 3754
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 26592
	Number of pyramids       = 0
	Number of prisms         = 0
	Number of hexahedrals    = 0

Writing Tecplot file ....
Finished writing Tecplot file

ok
test_faceMatch (test_aflr3.TestAFLR3.test_faceMatch) ... 
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = wall, index = 1
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 0
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 0
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = wall, index = 1
Getting volume mesh

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

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------
Volume mesh:
	Number of nodes          = 2273
	Number of elements       = 12220
	Number of triangles      = 2222
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 9998
	Number of pyramids       = 0
	Number of prisms         = 0
	Number of hexahedrals    = 0

Writing Tecplot file ....
Finished writing Tecplot file

Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 0
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 0
Getting volume mesh for body 1 (of 2)

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

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

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

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------
Volume mesh:
	Number of nodes          = 2405
	Number of elements       = 12664
	Number of triangles      = 2666
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 9998
	Number of pyramids       = 0
	Number of prisms         = 0
	Number of hexahedrals    = 0

Writing Tecplot file ....
Finished writing Tecplot file

Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 0
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 0
Getting volume mesh for body 1 (of 2)
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = wall, index = 1

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

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------
Volume mesh for body 1 (of 2):
	Number of nodes          = 1212
	Number of elements       = 6382
	Number of triangles      = 1334
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 5048
	Number of pyramids       = 0
	Number of prisms         = 0
	Number of hexahedrals    = 0
Getting volume mesh for body 2 (of 2)
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = wall, index = 1

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

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------
Volume mesh for body 2 (of 2):
	Number of nodes          = 1193
	Number of elements       = 6282
	Number of triangles      = 1332
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 4950
	Number of pyramids       = 0
	Number of prisms         = 0
	Number of hexahedrals    = 0

Writing Tecplot file ....
Finished writing Tecplot file


Writing Tecplot file ....
Finished writing Tecplot file

Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = wall, index = 1
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 0
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 0
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = wall, index = 1
Getting volume mesh

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

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------
Volume mesh:
	Number of nodes          = 3357
	Number of elements       = 18188
	Number of triangles      = 3110
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 15078
	Number of pyramids       = 0
	Number of prisms         = 0
	Number of hexahedrals    = 0

Writing Tecplot file ....
Finished writing Tecplot file

Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 0
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 0
Getting volume mesh for body 1 (of 3)

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

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

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

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

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

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------
Volume mesh:
	Number of nodes          = 3622
	Number of elements       = 19080
	Number of triangles      = 4002
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 15078
	Number of pyramids       = 0
	Number of prisms         = 0
	Number of hexahedrals    = 0

Writing Tecplot file ....
Finished writing Tecplot file

Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 0
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 0
Getting volume mesh for body 1 (of 3)
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = wall, index = 1

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

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------
Volume mesh for body 1 (of 3):
	Number of nodes          = 1212
	Number of elements       = 6382
	Number of triangles      = 1334
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 5048
	Number of pyramids       = 0
	Number of prisms         = 0
	Number of hexahedrals    = 0
Getting volume mesh for body 2 (of 3)
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = wall, index = 1

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

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------
Volume mesh for body 2 (of 3):
	Number of nodes          = 1193
	Number of elements       = 6282
	Number of triangles      = 1332
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 4950
	Number of pyramids       = 0
	Number of prisms         = 0
	Number of hexahedrals    = 0
Getting volume mesh for body 3 (of 3)
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = wall, index = 1

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

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------
Volume mesh for body 3 (of 3):
	Number of nodes          = 1217
	Number of elements       = 6416
	Number of triangles      = 1336
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 5080
	Number of pyramids       = 0
	Number of prisms         = 0
	Number of hexahedrals    = 0

Writing Tecplot file ....
Finished writing Tecplot file


Writing Tecplot file ....
Finished writing Tecplot file


Writing Tecplot file ....
Finished writing Tecplot file

Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = wall, index = 1
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 0
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 0
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = wall, index = 1
Getting volume mesh

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

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------
Volume mesh:
	Number of nodes          = 4425
	Number of elements       = 24045
	Number of triangles      = 4000
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 20045
	Number of pyramids       = 0
	Number of prisms         = 0
	Number of hexahedrals    = 0

Writing Tecplot file ....
Finished writing Tecplot file

Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 0
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 0
Getting volume mesh for body 1 (of 4)

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

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

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

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

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

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

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

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------
Volume mesh:
	Number of nodes          = 4822
	Number of elements       = 25381
	Number of triangles      = 5336
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 20045
	Number of pyramids       = 0
	Number of prisms         = 0
	Number of hexahedrals    = 0

Writing Tecplot file ....
Finished writing Tecplot file

Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 0
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 0
Getting volume mesh for body 1 (of 4)
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = wall, index = 1

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

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------
Volume mesh for body 1 (of 4):
	Number of nodes          = 1212
	Number of elements       = 6382
	Number of triangles      = 1334
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 5048
	Number of pyramids       = 0
	Number of prisms         = 0
	Number of hexahedrals    = 0
Getting volume mesh for body 2 (of 4)
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = wall, index = 1

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

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------
Volume mesh for body 2 (of 4):
	Number of nodes          = 1193
	Number of elements       = 6282
	Number of triangles      = 1332
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 4950
	Number of pyramids       = 0
	Number of prisms         = 0
	Number of hexahedrals    = 0
Getting volume mesh for body 3 (of 4)
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = wall, index = 1

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

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------
Volume mesh for body 3 (of 4):
	Number of nodes          = 1217
	Number of elements       = 6416
	Number of triangles      = 1336
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 5080
	Number of pyramids       = 0
	Number of prisms         = 0
	Number of hexahedrals    = 0
Getting volume mesh for body 4 (of 4)
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = wall, index = 1

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

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------
Volume mesh for body 4 (of 4):
	Number of nodes          = 1200
	Number of elements       = 6301
	Number of triangles      = 1334
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 4967
	Number of pyramids       = 0
	Number of prisms         = 0
	Number of hexahedrals    = 0

Writing Tecplot file ....
Finished writing Tecplot file


Writing Tecplot file ....
Finished writing Tecplot file


Writing Tecplot file ....
Finished writing Tecplot file


Writing Tecplot file ....
Finished writing Tecplot file

Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = wall, index = 1
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 0
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 0
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = wall, index = 1
Getting volume mesh

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

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------
Volume mesh:
	Number of nodes          = 5483
	Number of elements       = 29853
	Number of triangles      = 4890
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 24963
	Number of pyramids       = 0
	Number of prisms         = 0
	Number of hexahedrals    = 0

Writing Tecplot file ....
Finished writing Tecplot file

Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 0
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 0
Getting volume mesh for body 1 (of 5)

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

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

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

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

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

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

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

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

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

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------
Volume mesh:
	Number of nodes          = 6012
	Number of elements       = 31633
	Number of triangles      = 6670
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 24963
	Number of pyramids       = 0
	Number of prisms         = 0
	Number of hexahedrals    = 0

Writing Tecplot file ....
Finished writing Tecplot file

Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 0
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 0
Getting volume mesh for body 1 (of 5)
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = wall, index = 1

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

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------
Volume mesh for body 1 (of 5):
	Number of nodes          = 1212
	Number of elements       = 6382
	Number of triangles      = 1334
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 5048
	Number of pyramids       = 0
	Number of prisms         = 0
	Number of hexahedrals    = 0
Getting volume mesh for body 2 (of 5)
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = wall, index = 1

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

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------
Volume mesh for body 2 (of 5):
	Number of nodes          = 1193
	Number of elements       = 6282
	Number of triangles      = 1332
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 4950
	Number of pyramids       = 0
	Number of prisms         = 0
	Number of hexahedrals    = 0
Getting volume mesh for body 3 (of 5)
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = wall, index = 1

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

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------
Volume mesh for body 3 (of 5):
	Number of nodes          = 1217
	Number of elements       = 6416
	Number of triangles      = 1336
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 5080
	Number of pyramids       = 0
	Number of prisms         = 0
	Number of hexahedrals    = 0
Getting volume mesh for body 4 (of 5)
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = wall, index = 1

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

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------
Volume mesh for body 4 (of 5):
	Number of nodes          = 1200
	Number of elements       = 6301
	Number of triangles      = 1334
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 4967
	Number of pyramids       = 0
	Number of prisms         = 0
	Number of hexahedrals    = 0
Getting volume mesh for body 5 (of 5)
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = wall, index = 1

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

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------
Volume mesh for body 5 (of 5):
	Number of nodes          = 1190
	Number of elements       = 6252
	Number of triangles      = 1334
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 4918
	Number of pyramids       = 0
	Number of prisms         = 0
	Number of hexahedrals    = 0

Writing Tecplot file ....
Finished writing Tecplot file


Writing Tecplot file ....
Finished writing Tecplot file


Writing Tecplot file ....
Finished writing Tecplot file


Writing Tecplot file ....
Finished writing Tecplot file


Writing Tecplot file ....
Finished writing Tecplot file

Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = wall, index = 1
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 0
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 0
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = wall, index = 1
Getting volume mesh

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

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------
Volume mesh:
	Number of nodes          = 6555
	Number of elements       = 35742
	Number of triangles      = 5780
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 29962
	Number of pyramids       = 0
	Number of prisms         = 0
	Number of hexahedrals    = 0

Writing Tecplot file ....
Finished writing Tecplot file

Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 0
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 0
Getting volume mesh for body 1 (of 6)

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

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

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

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

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

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

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

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

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

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

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

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------
Volume mesh:
	Number of nodes          = 7216
	Number of elements       = 37966
	Number of triangles      = 8004
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 29962
	Number of pyramids       = 0
	Number of prisms         = 0
	Number of hexahedrals    = 0

Writing Tecplot file ....
Finished writing Tecplot file

Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 0
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 0
Getting volume mesh for body 1 (of 6)
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = wall, index = 1

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

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------
Volume mesh for body 1 (of 6):
	Number of nodes          = 1212
	Number of elements       = 6382
	Number of triangles      = 1334
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 5048
	Number of pyramids       = 0
	Number of prisms         = 0
	Number of hexahedrals    = 0
Getting volume mesh for body 2 (of 6)
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = wall, index = 1

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

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------
Volume mesh for body 2 (of 6):
	Number of nodes          = 1193
	Number of elements       = 6282
	Number of triangles      = 1332
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 4950
	Number of pyramids       = 0
	Number of prisms         = 0
	Number of hexahedrals    = 0
Getting volume mesh for body 3 (of 6)
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = wall, index = 1

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

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------
Volume mesh for body 3 (of 6):
	Number of nodes          = 1217
	Number of elements       = 6416
	Number of triangles      = 1336
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 5080
	Number of pyramids       = 0
	Number of prisms         = 0
	Number of hexahedrals    = 0
Getting volume mesh for body 4 (of 6)
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = wall, index = 1

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

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------
Volume mesh for body 4 (of 6):
	Number of nodes          = 1200
	Number of elements       = 6301
	Number of triangles      = 1334
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 4967
	Number of pyramids       = 0
	Number of prisms         = 0
	Number of hexahedrals    = 0
Getting volume mesh for body 5 (of 6)
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = wall, index = 1

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

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------
Volume mesh for body 5 (of 6):
	Number of nodes          = 1190
	Number of elements       = 6252
	Number of triangles      = 1334
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 4918
	Number of pyramids       = 0
	Number of prisms         = 0
	Number of hexahedrals    = 0
Getting volume mesh for body 6 (of 6)
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = wall, index = 1

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

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------
Volume mesh for body 6 (of 6):
	Number of nodes          = 1204
	Number of elements       = 6333
	Number of triangles      = 1334
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 4999
	Number of pyramids       = 0
	Number of prisms         = 0
	Number of hexahedrals    = 0

Writing Tecplot file ....
Finished writing Tecplot file


Writing Tecplot file ....
Finished writing Tecplot file


Writing Tecplot file ....
Finished writing Tecplot file


Writing Tecplot file ....
Finished writing Tecplot file


Writing Tecplot file ....
Finished writing Tecplot file


Writing Tecplot file ....
Finished writing Tecplot file

Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = wall, index = 1
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 0
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 0
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = wall, index = 1
Getting volume mesh

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

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------
Volume mesh:
	Number of nodes          = 7634
	Number of elements       = 41677
	Number of triangles      = 6670
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 35007
	Number of pyramids       = 0
	Number of prisms         = 0
	Number of hexahedrals    = 0

Writing Tecplot file ....
Finished writing Tecplot file

Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 0
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 0
Getting volume mesh for body 1 (of 7)

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

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

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

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

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

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

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

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

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

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

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

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

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

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------
Volume mesh:
	Number of nodes          = 8427
	Number of elements       = 44345
	Number of triangles      = 9338
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 35007
	Number of pyramids       = 0
	Number of prisms         = 0
	Number of hexahedrals    = 0

Writing Tecplot file ....
Finished writing Tecplot file

Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 0
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 0
Getting volume mesh for body 1 (of 7)
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = wall, index = 1

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

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------
Volume mesh for body 1 (of 7):
	Number of nodes          = 1212
	Number of elements       = 6382
	Number of triangles      = 1334
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 5048
	Number of pyramids       = 0
	Number of prisms         = 0
	Number of hexahedrals    = 0
Getting volume mesh for body 2 (of 7)
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = wall, index = 1

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

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------
Volume mesh for body 2 (of 7):
	Number of nodes          = 1193
	Number of elements       = 6282
	Number of triangles      = 1332
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 4950
	Number of pyramids       = 0
	Number of prisms         = 0
	Number of hexahedrals    = 0
Getting volume mesh for body 3 (of 7)
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = wall, index = 1

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

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------
Volume mesh for body 3 (of 7):
	Number of nodes          = 1217
	Number of elements       = 6416
	Number of triangles      = 1336
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 5080
	Number of pyramids       = 0
	Number of prisms         = 0
	Number of hexahedrals    = 0
Getting volume mesh for body 4 (of 7)
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = wall, index = 1

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

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------
Volume mesh for body 4 (of 7):
	Number of nodes          = 1200
	Number of elements       = 6301
	Number of triangles      = 1334
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 4967
	Number of pyramids       = 0
	Number of prisms         = 0
	Number of hexahedrals    = 0
Getting volume mesh for body 5 (of 7)
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = wall, index = 1

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

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------
Volume mesh for body 5 (of 7):
	Number of nodes          = 1190
	Number of elements       = 6252
	Number of triangles      = 1334
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 4918
	Number of pyramids       = 0
	Number of prisms         = 0
	Number of hexahedrals    = 0
Getting volume mesh for body 6 (of 7)
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = wall, index = 1

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

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------
Volume mesh for body 6 (of 7):
	Number of nodes          = 1204
	Number of elements       = 6333
	Number of triangles      = 1334
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 4999
	Number of pyramids       = 0
	Number of prisms         = 0
	Number of hexahedrals    = 0
Getting volume mesh for body 7 (of 7)
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = wall, index = 1

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

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------
Volume mesh for body 7 (of 7):
	Number of nodes          = 1211
	Number of elements       = 6379
	Number of triangles      = 1334
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 5045
	Number of pyramids       = 0
	Number of prisms         = 0
	Number of hexahedrals    = 0

Writing Tecplot file ....
Finished writing Tecplot file


Writing Tecplot file ....
Finished writing Tecplot file


Writing Tecplot file ....
Finished writing Tecplot file


Writing Tecplot file ....
Finished writing Tecplot file


Writing Tecplot file ....
Finished writing Tecplot file


Writing Tecplot file ....
Finished writing Tecplot file


Writing Tecplot file ....
Finished writing Tecplot file

Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = wall, index = 1
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 0
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 0
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = wall, index = 1
Getting volume mesh

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

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------
Volume mesh:
	Number of nodes          = 19879
	Number of elements       = 110275
	Number of triangles      = 15558
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 94717
	Number of pyramids       = 0
	Number of prisms         = 0
	Number of hexahedrals    = 0

Writing Tecplot file ....
Finished writing Tecplot file

Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 0
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 0
Getting volume mesh for body 1 (of 19)

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------
Volume mesh:
	Number of nodes          = 22822
	Number of elements       = 120055
	Number of triangles      = 25338
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 94717
	Number of pyramids       = 0
	Number of prisms         = 0
	Number of hexahedrals    = 0

Writing Tecplot file ....
Finished writing Tecplot file

Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 0
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 0
Getting volume mesh for body 1 (of 19)
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = wall, index = 1

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

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------
Volume mesh for body 1 (of 19):
	Number of nodes          = 1212
	Number of elements       = 6382
	Number of triangles      = 1334
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 5048
	Number of pyramids       = 0
	Number of prisms         = 0
	Number of hexahedrals    = 0
Getting volume mesh for body 2 (of 19)
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = wall, index = 1

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

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------
Volume mesh for body 2 (of 19):
	Number of nodes          = 1193
	Number of elements       = 6282
	Number of triangles      = 1332
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 4950
	Number of pyramids       = 0
	Number of prisms         = 0
	Number of hexahedrals    = 0
Getting volume mesh for body 3 (of 19)
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = wall, index = 1

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

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------
Volume mesh for body 3 (of 19):
	Number of nodes          = 1217
	Number of elements       = 6416
	Number of triangles      = 1336
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 5080
	Number of pyramids       = 0
	Number of prisms         = 0
	Number of hexahedrals    = 0
Getting volume mesh for body 4 (of 19)
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = wall, index = 1

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

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------
Volume mesh for body 4 (of 19):
	Number of nodes          = 1200
	Number of elements       = 6301
	Number of triangles      = 1334
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 4967
	Number of pyramids       = 0
	Number of prisms         = 0
	Number of hexahedrals    = 0
Getting volume mesh for body 5 (of 19)
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = wall, index = 1

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

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------
Volume mesh for body 5 (of 19):
	Number of nodes          = 1190
	Number of elements       = 6252
	Number of triangles      = 1334
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 4918
	Number of pyramids       = 0
	Number of prisms         = 0
	Number of hexahedrals    = 0
Getting volume mesh for body 6 (of 19)
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = wall, index = 1

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

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------
Volume mesh for body 6 (of 19):
	Number of nodes          = 1204
	Number of elements       = 6333
	Number of triangles      = 1334
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 4999
	Number of pyramids       = 0
	Number of prisms         = 0
	Number of hexahedrals    = 0
Getting volume mesh for body 7 (of 19)
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = wall, index = 1

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

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------
Volume mesh for body 7 (of 19):
	Number of nodes          = 1211
	Number of elements       = 6379
	Number of triangles      = 1334
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 5045
	Number of pyramids       = 0
	Number of prisms         = 0
	Number of hexahedrals    = 0
Getting volume mesh for body 8 (of 19)
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = wall, index = 1

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

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------
Volume mesh for body 8 (of 19):
	Number of nodes          = 1220
	Number of elements       = 6413
	Number of triangles      = 1336
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 5077
	Number of pyramids       = 0
	Number of prisms         = 0
	Number of hexahedrals    = 0
Getting volume mesh for body 9 (of 19)
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = wall, index = 1

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

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------
Volume mesh for body 9 (of 19):
	Number of nodes          = 1214
	Number of elements       = 6396
	Number of triangles      = 1336
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 5060
	Number of pyramids       = 0
	Number of prisms         = 0
	Number of hexahedrals    = 0
Getting volume mesh for body 10 (of 19)
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = wall, index = 1

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

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------
Volume mesh for body 10 (of 19):
	Number of nodes          = 1192
	Number of elements       = 6262
	Number of triangles      = 1332
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 4930
	Number of pyramids       = 0
	Number of prisms         = 0
	Number of hexahedrals    = 0
Getting volume mesh for body 11 (of 19)
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = wall, index = 1

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

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------
Volume mesh for body 11 (of 19):
	Number of nodes          = 1201
	Number of elements       = 6326
	Number of triangles      = 1332
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 4994
	Number of pyramids       = 0
	Number of prisms         = 0
	Number of hexahedrals    = 0
Getting volume mesh for body 12 (of 19)
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = wall, index = 1

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

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------
Volume mesh for body 12 (of 19):
	Number of nodes          = 1206
	Number of elements       = 6356
	Number of triangles      = 1334
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 5022
	Number of pyramids       = 0
	Number of prisms         = 0
	Number of hexahedrals    = 0
Getting volume mesh for body 13 (of 19)
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = wall, index = 1

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

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------
Volume mesh for body 13 (of 19):
	Number of nodes          = 1187
	Number of elements       = 6236
	Number of triangles      = 1332
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 4904
	Number of pyramids       = 0
	Number of prisms         = 0
	Number of hexahedrals    = 0
Getting volume mesh for body 14 (of 19)
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = wall, index = 1

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

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------
Volume mesh for body 14 (of 19):
	Number of nodes          = 1197
	Number of elements       = 6293
	Number of triangles      = 1334
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 4959
	Number of pyramids       = 0
	Number of prisms         = 0
	Number of hexahedrals    = 0
Getting volume mesh for body 15 (of 19)
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = wall, index = 1

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

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------
Volume mesh for body 15 (of 19):
	Number of nodes          = 1180
	Number of elements       = 6202
	Number of triangles      = 1332
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 4870
	Number of pyramids       = 0
	Number of prisms         = 0
	Number of hexahedrals    = 0
Getting volume mesh for body 16 (of 19)
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = wall, index = 1

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

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------
Volume mesh for body 16 (of 19):
	Number of nodes          = 1197
	Number of elements       = 6289
	Number of triangles      = 1332
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 4957
	Number of pyramids       = 0
	Number of prisms         = 0
	Number of hexahedrals    = 0
Getting volume mesh for body 17 (of 19)
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = wall, index = 1

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

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------
Volume mesh for body 17 (of 19):
	Number of nodes          = 1208
	Number of elements       = 6351
	Number of triangles      = 1334
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 5017
	Number of pyramids       = 0
	Number of prisms         = 0
	Number of hexahedrals    = 0
Getting volume mesh for body 18 (of 19)
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = wall, index = 1

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

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------
Volume mesh for body 18 (of 19):
	Number of nodes          = 1193
	Number of elements       = 6277
	Number of triangles      = 1332
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 4945
	Number of pyramids       = 0
	Number of prisms         = 0
	Number of hexahedrals    = 0
Getting volume mesh for body 19 (of 19)
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = wall, index = 1

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

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------
Volume mesh for body 19 (of 19):
	Number of nodes          = 1200
	Number of elements       = 6309
	Number of triangles      = 1334
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 4975
	Number of pyramids       = 0
	Number of prisms         = 0
	Number of hexahedrals    = 0

Writing Tecplot file ....
Finished writing Tecplot file


Writing Tecplot file ....
Finished writing Tecplot file


Writing Tecplot file ....
Finished writing Tecplot file


Writing Tecplot file ....
Finished writing Tecplot file


Writing Tecplot file ....
Finished writing Tecplot file


Writing Tecplot file ....
Finished writing Tecplot file


Writing Tecplot file ....
Finished writing Tecplot file


Writing Tecplot file ....
Finished writing Tecplot file


Writing Tecplot file ....
Finished writing Tecplot file


Writing Tecplot file ....
Finished writing Tecplot file


Writing Tecplot file ....
Finished writing Tecplot file


Writing Tecplot file ....
Finished writing Tecplot file


Writing Tecplot file ....
Finished writing Tecplot file


Writing Tecplot file ....
Finished writing Tecplot file


Writing Tecplot file ....
Finished writing Tecplot file


Writing Tecplot file ....
Finished writing Tecplot file


Writing Tecplot file ....
Finished writing Tecplot file


Writing Tecplot file ....
Finished writing Tecplot file


Writing Tecplot file ....
Finished writing Tecplot file

ok
test_faceMatch_MultiDomain (test_aflr3.TestAFLR3.test_faceMatch_MultiDomain) ... ../csmData/MultiDomain/example1.csm

Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = dummy_att, index = 1
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 0
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 0
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = dummy_att, index = 1
Getting volume mesh

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

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------
Volume mesh:
	Number of nodes          = 8499
	Number of elements       = 47040
	Number of triangles      = 6258
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 40782
	Number of pyramids       = 0
	Number of prisms         = 0
	Number of hexahedrals    = 0

Writing Tecplot file ....
Finished writing Tecplot file

Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 0
Getting volume mesh for body 1 (of 2)

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

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

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

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------
Volume mesh:
	Number of nodes          = 8631
	Number of elements       = 47484
	Number of triangles      = 6702
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 40782
	Number of pyramids       = 0
	Number of prisms         = 0
	Number of hexahedrals    = 0

Writing Tecplot file ....
Finished writing Tecplot file

Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 0
Getting volume mesh for body 1 (of 2)
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = dummy_att, index = 1

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

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------
Volume mesh for body 1 (of 2):
	Number of nodes          = 7444
	Number of elements       = 41254
	Number of triangles      = 5370
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 35884
	Number of pyramids       = 0
	Number of prisms         = 0
	Number of hexahedrals    = 0
Getting volume mesh for body 2 (of 2)
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = dummy_att, index = 1

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

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------
Volume mesh for body 2 (of 2):
	Number of nodes          = 1187
	Number of elements       = 6230
	Number of triangles      = 1332
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 4898
	Number of pyramids       = 0
	Number of prisms         = 0
	Number of hexahedrals    = 0

Writing Tecplot file ....
Finished writing Tecplot file


Writing Tecplot file ....
Finished writing Tecplot file

../csmData/MultiDomain/example2.csm

Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = dummy_att, index = 1
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 0
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 0
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = dummy_att, index = 1
Getting volume mesh

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

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------
Volume mesh:
	Number of nodes          = 9625
	Number of elements       = 53328
	Number of triangles      = 7146
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 46182
	Number of pyramids       = 0
	Number of prisms         = 0
	Number of hexahedrals    = 0

Writing Tecplot file ....
Finished writing Tecplot file

Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 0
Getting volume mesh for body 1 (of 3)

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

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

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

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

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

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------
Volume mesh:
	Number of nodes          = 9899
	Number of elements       = 54216
	Number of triangles      = 8034
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 46182
	Number of pyramids       = 0
	Number of prisms         = 0
	Number of hexahedrals    = 0

Writing Tecplot file ....
Finished writing Tecplot file

Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 0
Getting volume mesh for body 1 (of 3)
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = dummy_att, index = 1

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

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------
Volume mesh for body 1 (of 3):
	Number of nodes          = 7485
	Number of elements       = 41497
	Number of triangles      = 5370
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 36127
	Number of pyramids       = 0
	Number of prisms         = 0
	Number of hexahedrals    = 0
Getting volume mesh for body 2 (of 3)
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = dummy_att, index = 1

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

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------
Volume mesh for body 2 (of 3):
	Number of nodes          = 1212
	Number of elements       = 6385
	Number of triangles      = 1332
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 5053
	Number of pyramids       = 0
	Number of prisms         = 0
	Number of hexahedrals    = 0
Getting volume mesh for body 3 (of 3)
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = dummy_att, index = 1

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

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------
Volume mesh for body 3 (of 3):
	Number of nodes          = 1202
	Number of elements       = 6334
	Number of triangles      = 1332
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 5002
	Number of pyramids       = 0
	Number of prisms         = 0
	Number of hexahedrals    = 0

Writing Tecplot file ....
Finished writing Tecplot file


Writing Tecplot file ....
Finished writing Tecplot file


Writing Tecplot file ....
Finished writing Tecplot file

../csmData/MultiDomain/example3.csm

Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = dummy_att, index = 1
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 0
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 0
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = dummy_att, index = 1
Getting volume mesh

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

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------
Volume mesh:
	Number of nodes          = 9302
	Number of elements       = 51451
	Number of triangles      = 6968
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 44483
	Number of pyramids       = 0
	Number of prisms         = 0
	Number of hexahedrals    = 0

Writing Tecplot file ....
Finished writing Tecplot file

Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 0
Getting volume mesh for body 1 (of 3)

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

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

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

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

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

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------
Volume mesh:
	Number of nodes          = 9522
	Number of elements       = 52179
	Number of triangles      = 7696
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 44483
	Number of pyramids       = 0
	Number of prisms         = 0
	Number of hexahedrals    = 0

Writing Tecplot file ....
Finished writing Tecplot file

Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 0
Getting volume mesh for body 1 (of 3)
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = dummy_att, index = 1

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

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------
Volume mesh for body 1 (of 3):
	Number of nodes          = 7466
	Number of elements       = 41416
	Number of triangles      = 5368
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 36048
	Number of pyramids       = 0
	Number of prisms         = 0
	Number of hexahedrals    = 0
Getting volume mesh for body 2 (of 3)
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = dummy_att, index = 1

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

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------
Volume mesh for body 2 (of 3):
	Number of nodes          = 1187
	Number of elements       = 6230
	Number of triangles      = 1332
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 4898
	Number of pyramids       = 0
	Number of prisms         = 0
	Number of hexahedrals    = 0
Getting volume mesh for body 3 (of 3)
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = dummy_att, index = 1

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

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------
Volume mesh for body 3 (of 3):
	Number of nodes          = 869
	Number of elements       = 4533
	Number of triangles      = 996
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 3537
	Number of pyramids       = 0
	Number of prisms         = 0
	Number of hexahedrals    = 0

Writing Tecplot file ....
Finished writing Tecplot file


Writing Tecplot file ....
Finished writing Tecplot file


Writing Tecplot file ....
Finished writing Tecplot file

../csmData/MultiDomain/example4.csm

Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = dummy_att, index = 1
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 0
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 0
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = dummy_att, index = 1
Getting volume mesh

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

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------
Volume mesh:
	Number of nodes          = 8956
	Number of elements       = 49469
	Number of triangles      = 6784
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 42685
	Number of pyramids       = 0
	Number of prisms         = 0
	Number of hexahedrals    = 0

Writing Tecplot file ....
Finished writing Tecplot file

Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 0
Getting volume mesh for body 1 (of 3)

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

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

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

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

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

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------
Volume mesh:
	Number of nodes          = 9139
	Number of elements       = 50065
	Number of triangles      = 7380
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 42685
	Number of pyramids       = 0
	Number of prisms         = 0
	Number of hexahedrals    = 0

Writing Tecplot file ....
Finished writing Tecplot file

Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 0
Getting volume mesh for body 1 (of 3)
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = dummy_att, index = 1

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

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------
Volume mesh for body 1 (of 3):
	Number of nodes          = 7430
	Number of elements       = 41197
	Number of triangles      = 5360
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 35837
	Number of pyramids       = 0
	Number of prisms         = 0
	Number of hexahedrals    = 0
Getting volume mesh for body 2 (of 3)
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = dummy_att, index = 1

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

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------
Volume mesh for body 2 (of 3):
	Number of nodes          = 1187
	Number of elements       = 6230
	Number of triangles      = 1332
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 4898
	Number of pyramids       = 0
	Number of prisms         = 0
	Number of hexahedrals    = 0
Getting volume mesh for body 3 (of 3)
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = dummy_att, index = 1

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

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------
Volume mesh for body 3 (of 3):
	Number of nodes          = 522
	Number of elements       = 2638
	Number of triangles      = 688
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 1950
	Number of pyramids       = 0
	Number of prisms         = 0
	Number of hexahedrals    = 0

Writing Tecplot file ....
Finished writing Tecplot file


Writing Tecplot file ....
Finished writing Tecplot file


Writing Tecplot file ....
Finished writing Tecplot file

../csmData/MultiDomain/example6.csm

Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = dummy_att, index = 1
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 0
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 0
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = dummy_att, index = 1
Getting volume mesh

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

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------
Volume mesh:
	Number of nodes          = 8638
	Number of elements       = 47663
	Number of triangles      = 6598
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 41065
	Number of pyramids       = 0
	Number of prisms         = 0
	Number of hexahedrals    = 0

Writing Tecplot file ....
Finished writing Tecplot file

Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 0
Getting volume mesh for body 1 (of 3)

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

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

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

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

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

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------
Volume mesh:
	Number of nodes          = 8777
	Number of elements       = 48099
	Number of triangles      = 7034
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 41065
	Number of pyramids       = 0
	Number of prisms         = 0
	Number of hexahedrals    = 0

Writing Tecplot file ....
Finished writing Tecplot file

Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 0
Getting volume mesh for body 1 (of 3)
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = dummy_att, index = 1

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

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------
Volume mesh for body 1 (of 3):
	Number of nodes          = 7402
	Number of elements       = 41032
	Number of triangles      = 5352
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 35680
	Number of pyramids       = 0
	Number of prisms         = 0
	Number of hexahedrals    = 0
Getting volume mesh for body 2 (of 3)
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = dummy_att, index = 1

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

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------
Volume mesh for body 2 (of 3):
	Number of nodes          = 848
	Number of elements       = 4402
	Number of triangles      = 994
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 3408
	Number of pyramids       = 0
	Number of prisms         = 0
	Number of hexahedrals    = 0
Getting volume mesh for body 3 (of 3)
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = dummy_att, index = 1

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

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------
Volume mesh for body 3 (of 3):
	Number of nodes          = 527
	Number of elements       = 2665
	Number of triangles      = 688
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 1977
	Number of pyramids       = 0
	Number of prisms         = 0
	Number of hexahedrals    = 0

Writing Tecplot file ....
Finished writing Tecplot file


Writing Tecplot file ....
Finished writing Tecplot file


Writing Tecplot file ....
Finished writing Tecplot file

../csmData/MultiDomain/example7.csm

Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = dummy_att, index = 1
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 0
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 0
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = dummy_att, index = 1
Getting volume mesh

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

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------
Volume mesh:
	Number of nodes          = 9771
	Number of elements       = 54406
	Number of triangles      = 6748
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 47658
	Number of pyramids       = 0
	Number of prisms         = 0
	Number of hexahedrals    = 0

Writing Tecplot file ....
Finished writing Tecplot file

Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 0
Getting volume mesh for body 1 (of 3)

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

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

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

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

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

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------
Volume mesh:
	Number of nodes          = 10261
	Number of elements       = 56170
	Number of triangles      = 8512
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 47658
	Number of pyramids       = 0
	Number of prisms         = 0
	Number of hexahedrals    = 0

Writing Tecplot file ....
Finished writing Tecplot file

Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 0
Getting volume mesh for body 1 (of 3)
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = dummy_att, index = 1

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

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------
Volume mesh for body 1 (of 3):
	Number of nodes          = 7355
	Number of elements       = 40784
	Number of triangles      = 5334
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 35450
	Number of pyramids       = 0
	Number of prisms         = 0
	Number of hexahedrals    = 0
Getting volume mesh for body 2 (of 3)
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = dummy_att, index = 1

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

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------
Volume mesh for body 2 (of 3):
	Number of nodes          = 2663
	Number of elements       = 14238
	Number of triangles      = 2794
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 11444
	Number of pyramids       = 0
	Number of prisms         = 0
	Number of hexahedrals    = 0
Getting volume mesh for body 3 (of 3)
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = dummy_att, index = 1

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

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------
Volume mesh for body 3 (of 3):
	Number of nodes          = 243
	Number of elements       = 1148
	Number of triangles      = 384
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 764
	Number of pyramids       = 0
	Number of prisms         = 0
	Number of hexahedrals    = 0

Writing Tecplot file ....
Finished writing Tecplot file


Writing Tecplot file ....
Finished writing Tecplot file


Writing Tecplot file ....
Finished writing Tecplot file

../csmData/MultiDomain/example8.csm

Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = dummy_att, index = 1
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 0
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 0
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = dummy_att, index = 1
Getting volume mesh

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

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

Writing Tecplot file ....
Finished writing Tecplot file

Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 0
Getting volume mesh for body 1 (of 3)

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

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

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

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

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

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

Writing Tecplot file ....
Finished writing Tecplot file

Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 0
Getting volume mesh for body 1 (of 3)
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = dummy_att, index = 1

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

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------
Volume mesh for body 1 (of 3):
	Number of nodes          = 1170
	Number of elements       = 6155
	Number of triangles      = 1308
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 4847
	Number of pyramids       = 0
	Number of prisms         = 0
	Number of hexahedrals    = 0
Getting volume mesh for body 2 (of 3)
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = dummy_att, index = 1

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

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------
Volume mesh for body 2 (of 3):
	Number of nodes          = 360
	Number of elements       = 1630
	Number of triangles      = 718
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 912
	Number of pyramids       = 0
	Number of prisms         = 0
	Number of hexahedrals    = 0
Getting volume mesh for body 3 (of 3)
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = dummy_att, index = 1

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

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------
Volume mesh for body 3 (of 3):
	Number of nodes          = 44
	Number of elements       = 160
	Number of triangles      = 84
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 76
	Number of pyramids       = 0
	Number of prisms         = 0
	Number of hexahedrals    = 0

Writing Tecplot file ....
Finished writing Tecplot file


Writing Tecplot file ....
Finished writing Tecplot file


Writing Tecplot file ....
Finished writing Tecplot file

../csmData/MultiDomain/example9.csm

Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = dummy_att, index = 1
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 0
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 0
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = dummy_att, index = 1
Getting volume mesh

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

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------
Volume mesh:
	Number of nodes          = 5096
	Number of elements       = 27903
	Number of triangles      = 4076
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 23827
	Number of pyramids       = 0
	Number of prisms         = 0
	Number of hexahedrals    = 0

Writing Tecplot file ....
Finished writing Tecplot file

Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 0
Getting volume mesh for body 1 (of 2)

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

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

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

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------
Volume mesh:
	Number of nodes          = 5242
	Number of elements       = 28455
	Number of triangles      = 4628
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 23827
	Number of pyramids       = 0
	Number of prisms         = 0
	Number of hexahedrals    = 0

Writing Tecplot file ....
Finished writing Tecplot file

Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 0
Getting volume mesh for body 1 (of 2)
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = dummy_att, index = 1

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

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------
Volume mesh for body 1 (of 2):
	Number of nodes          = 4905
	Number of elements       = 26939
	Number of triangles      = 4044
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 22895
	Number of pyramids       = 0
	Number of prisms         = 0
	Number of hexahedrals    = 0
Getting volume mesh for body 2 (of 2)
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = dummy_att, index = 1

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

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------
Volume mesh for body 2 (of 2):
	Number of nodes          = 337
	Number of elements       = 1516
	Number of triangles      = 584
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 932
	Number of pyramids       = 0
	Number of prisms         = 0
	Number of hexahedrals    = 0

Writing Tecplot file ....
Finished writing Tecplot file


Writing Tecplot file ....
Finished writing Tecplot file

../csmData/MultiDomain/multi_prim.csm

Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = dummy_att, index = 1
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 0
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 0
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = dummy_att, index = 1
Getting volume mesh

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

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------
Volume mesh:
	Number of nodes          = 33115
	Number of elements       = 191815
	Number of triangles      = 8476
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 183339
	Number of pyramids       = 0
	Number of prisms         = 0
	Number of hexahedrals    = 0

Writing Tecplot file ....
Finished writing Tecplot file

Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 0
Getting volume mesh for body 1 (of 5)

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

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

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

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

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

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

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

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

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

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------
Volume mesh:
	Number of nodes          = 36459
	Number of elements       = 205159
	Number of triangles      = 21820
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 183339
	Number of pyramids       = 0
	Number of prisms         = 0
	Number of hexahedrals    = 0

Writing Tecplot file ....
Finished writing Tecplot file

Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 0
Getting volume mesh for body 1 (of 5)
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = dummy_att, index = 1

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

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------
Volume mesh for body 1 (of 5):
	Number of nodes          = 28820
	Number of elements       = 163772
	Number of triangles      = 15148
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 148624
	Number of pyramids       = 0
	Number of prisms         = 0
	Number of hexahedrals    = 0
Getting volume mesh for body 2 (of 5)
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = dummy_att, index = 1

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

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------
Volume mesh for body 2 (of 5):
	Number of nodes          = 1416
	Number of elements       = 7524
	Number of triangles      = 1456
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 6068
	Number of pyramids       = 0
	Number of prisms         = 0
	Number of hexahedrals    = 0
Getting volume mesh for body 3 (of 5)
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = dummy_att, index = 1

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

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------
Volume mesh for body 3 (of 5):
	Number of nodes          = 4240
	Number of elements       = 23511
	Number of triangles      = 2950
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 20561
	Number of pyramids       = 0
	Number of prisms         = 0
	Number of hexahedrals    = 0
Getting volume mesh for body 4 (of 5)
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = dummy_att, index = 1

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

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------
Volume mesh for body 4 (of 5):
	Number of nodes          = 720
	Number of elements       = 3724
	Number of triangles      = 842
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 2882
	Number of pyramids       = 0
	Number of prisms         = 0
	Number of hexahedrals    = 0
Getting volume mesh for body 5 (of 5)
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = dummy_att, index = 1

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

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------
Volume mesh for body 5 (of 5):
	Number of nodes          = 1263
	Number of elements       = 6628
	Number of triangles      = 1424
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 5204
	Number of pyramids       = 0
	Number of prisms         = 0
	Number of hexahedrals    = 0

Writing Tecplot file ....
Finished writing Tecplot file


Writing Tecplot file ....
Finished writing Tecplot file


Writing Tecplot file ....
Finished writing Tecplot file


Writing Tecplot file ....
Finished writing Tecplot file


Writing Tecplot file ....
Finished writing Tecplot file

../csmData/MultiDomain/cyl_seam.csm

Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = dummy_att, index = 1
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 0
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 0
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = dummy_att, index = 1
Getting volume mesh

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

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------
Volume mesh:
	Number of nodes          = 16667
	Number of elements       = 94472
	Number of triangles      = 8798
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 85674
	Number of pyramids       = 0
	Number of prisms         = 0
	Number of hexahedrals    = 0

Writing Tecplot file ....
Finished writing Tecplot file

Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 0
Getting volume mesh for body 1 (of 2)

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

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

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

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------
Volume mesh:
	Number of nodes          = 18591
	Number of elements       = 101848
	Number of triangles      = 16174
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 85674
	Number of pyramids       = 0
	Number of prisms         = 0
	Number of hexahedrals    = 0

Writing Tecplot file ....
Finished writing Tecplot file

Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 0
Getting volume mesh for body 1 (of 2)
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = dummy_att, index = 1

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

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------
Volume mesh for body 1 (of 2):
	Number of nodes          = 12023
	Number of elements       = 67478
	Number of triangles      = 7138
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 60340
	Number of pyramids       = 0
	Number of prisms         = 0
	Number of hexahedrals    = 0
Getting volume mesh for body 2 (of 2)
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = dummy_att, index = 1

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

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------
Volume mesh for body 2 (of 2):
	Number of nodes          = 6568
	Number of elements       = 34370
	Number of triangles      = 9036
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 25334
	Number of pyramids       = 0
	Number of prisms         = 0
	Number of hexahedrals    = 0

Writing Tecplot file ....
Finished writing Tecplot file


Writing Tecplot file ....
Finished writing Tecplot file

ok
test_journal (test_aflr3.TestAFLR3.test_journal) ... 
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 2
	Name = Farfield, index = 1
	Name = Wing1, index = 2
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 3
	Name = Farfield, index = 1
	Name = Wing1, index = 2
	Name = trailingEdge, index = 3
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 3
	Name = Farfield, index = 1
	Name = Wing1, index = 2
	Name = trailingEdge, index = 3
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 2
	Name = Farfield, index = 1
	Name = Wing1, index = 2
Getting volume mesh

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

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

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

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------
Volume mesh:
	Number of nodes          = 2494
	Number of elements       = 10977
	Number of triangles      = 4552
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 6425
	Number of pyramids       = 0
	Number of prisms         = 0
	Number of hexahedrals    = 0
 EGADS Info: 0 Objects, 0 Reference in Use (of 0) at Close!


 CAPS Info: Hit last success -- going live!

 CAPS Info: Hit last success -- going live!

 CAPS Info: Hit last success -- going live!

 CAPS Info: Hit last success -- going live!

 CAPS Info: Hit last success -- going live!


 CAPS Info: Hit last success -- going live!

Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 2
	Name = Farfield, index = 1
	Name = Wing1, index = 2
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 3
	Name = Farfield, index = 1
	Name = Wing1, index = 2
	Name = trailingEdge, index = 3
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 3
	Name = Farfield, index = 1
	Name = Wing1, index = 2
	Name = trailingEdge, index = 3
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 2
	Name = Farfield, index = 1
	Name = Wing1, index = 2
Getting volume mesh

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

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

 CAPS Info: Hit last success -- going live!
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 2
	Name = Farfield, index = 1
	Name = Wing1, index = 2
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 3
	Name = Farfield, index = 1
	Name = Wing1, index = 2
	Name = trailingEdge, index = 3
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 3
	Name = Farfield, index = 1
	Name = Wing1, index = 2
	Name = trailingEdge, index = 3
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 2
	Name = Farfield, index = 1
	Name = Wing1, index = 2

 CAPS Info: Hit last success -- going live!
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 2
	Name = Farfield, index = 1
	Name = Wing1, index = 2
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 3
	Name = Farfield, index = 1
	Name = Wing1, index = 2
	Name = trailingEdge, index = 3
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 3
	Name = Farfield, index = 1
	Name = Wing1, index = 2
	Name = trailingEdge, index = 3
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 2
	Name = Farfield, index = 1
	Name = Wing1, index = 2

 CAPS Info: Hit last success -- going live!

 CAPS Info: Hit last success -- going live!
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 2
	Name = Farfield, index = 1
	Name = Wing1, index = 2
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 3
	Name = Farfield, index = 1
	Name = Wing1, index = 2
	Name = trailingEdge, index = 3
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 3
	Name = Farfield, index = 1
	Name = Wing1, index = 2
	Name = trailingEdge, index = 3
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 2
	Name = Farfield, index = 1
	Name = Wing1, index = 2
Getting volume mesh

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

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

 CAPS Info: Hit last success -- going live!
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 2
	Name = Farfield, index = 1
	Name = Wing1, index = 2
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 3
	Name = Farfield, index = 1
	Name = Wing1, index = 2
	Name = trailingEdge, index = 3
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 3
	Name = Farfield, index = 1
	Name = Wing1, index = 2
	Name = trailingEdge, index = 3
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 2
	Name = Farfield, index = 1
	Name = Wing1, index = 2

ok
test_phase (test_aflr3.TestAFLR3.test_phase) ... 
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 2
	Name = Farfield, index = 1
	Name = Wing1, index = 2
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 3
	Name = Farfield, index = 1
	Name = Wing1, index = 2
	Name = trailingEdge, index = 3
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 3
	Name = Farfield, index = 1
	Name = Wing1, index = 2
	Name = trailingEdge, index = 3
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 2
	Name = Farfield, index = 1
	Name = Wing1, index = 2
Getting volume mesh

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

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

Writing Tecplot file ....
Finished writing Tecplot file


Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 2
	Name = Farfield, index = 1
	Name = Wing1, index = 2
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 3
	Name = Farfield, index = 1
	Name = Wing1, index = 2
	Name = trailingEdge, index = 3
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 3
	Name = Farfield, index = 1
	Name = Wing1, index = 2
	Name = trailingEdge, index = 3
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 2
	Name = Farfield, index = 1
	Name = Wing1, index = 2
Getting volume mesh

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

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

Writing Tecplot file ....
Finished writing Tecplot file

ok
test_reenter (test_aflr3.TestAFLR3.test_reenter) ... 
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 2
	Name = Farfield, index = 1
	Name = Wing1, index = 2
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 3
	Name = Farfield, index = 1
	Name = Wing1, index = 2
	Name = trailingEdge, index = 3
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 3
	Name = Farfield, index = 1
	Name = Wing1, index = 2
	Name = trailingEdge, index = 3
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 2
	Name = Farfield, index = 1
	Name = Wing1, index = 2
Getting volume mesh

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

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

Writing Binary VTK file ....
Finished writing Binary VTK file


Writing vtk file ....

Writing vtk general file ....
Finished writing vtk file


Writing FAST file ....
Finished writing FAST file


Writing SU2 file ....
Finished writing SU2 file


Writing exodus file ....
	Block: 'Block1_tet', blk_id 1, num_entries 6952
	Sideset: 'Farfield', set_id 1, num_entries 12
	Sideset: 'Wing1', set_id 2, num_entries 5440
Finished writing Exodus file


Writing Binary STL file ....
Finished writing Binary STL file


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


Writing Tecplot file ....
Finished writing Tecplot file

Getting volume mesh

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

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

Writing Binary VTK file ....
Finished writing Binary VTK file


Writing vtk file ....

Writing vtk general file ....
Finished writing vtk file


Writing FAST file ....
Finished writing FAST file


Writing SU2 file ....
Finished writing SU2 file


Writing exodus file ....
	Block: 'Block1_tet', blk_id 1, num_entries 6425
	Sideset: 'Farfield', set_id 1, num_entries 12
	Sideset: 'Wing1', set_id 2, num_entries 4540
Finished writing Exodus file


Writing Binary STL file ....
Finished writing Binary STL file


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


Writing Tecplot file ....
Finished writing Tecplot file

ok
test_setInput (test_aflr3.TestAFLR3.test_setInput) ...  EGADS Info: 0 Objects, 0 Reference in Use (of 0) at Close!
ok
test_sphere (test_aflr3.TestAFLR3.test_sphere) ... Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 2
	Name = sphere, index = 1
	Name = farfield, index = 2
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 0
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 0
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 2
	Name = sphere, index = 1
	Name = farfield, index = 2
Getting volume mesh

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

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------
Volume mesh:
	Number of nodes          = 4972
	Number of elements       = 27531
	Number of triangles      = 3460
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 24071
	Number of pyramids       = 0
	Number of prisms         = 0
	Number of hexahedrals    = 0

Writing Tecplot file ....
Finished writing Tecplot file

ok
test_torus (test_aflr3.TestAFLR3.test_torus) ... Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 2
	Name = torus, index = 1
	Name = farfield, index = 2
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 0
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 0
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 2
	Name = torus, index = 1
	Name = farfield, index = 2
Getting volume mesh

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

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------
Volume mesh:
	Number of nodes          = 6395
	Number of elements       = 35692
	Number of triangles      = 4048
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 31644
	Number of pyramids       = 0
	Number of prisms         = 0
	Number of hexahedrals    = 0

Writing Tecplot file ....
Finished writing Tecplot file

ok
test_transp (test_aflr3.TestAFLR3.test_transp) ... 
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 4
	Name = Wing1, index = 1
	Name = Wing2, index = 2
	Name = Wake, index = 3
	Name = Farfield, index = 4
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 4
	Name = Wing1, index = 1
	Name = Wing2, index = 2
	Name = Wake, index = 3
	Name = Farfield, index = 4
AFLR4    : Proximity BG Surface Grid Generation Skipped
AFLR4    : No Modifications Required

Writing Tecplot file ....
Finished writing Tecplot file

Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 4
	Name = Wing1, index = 1
	Name = Wing2, index = 2
	Name = Wake, index = 3
	Name = Farfield, index = 4
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 4
	Name = Wing1, index = 1
	Name = Wing2, index = 2
	Name = Wake, index = 3
	Name = Farfield, index = 4

Getting mesh sizing parameters
	Mesh sizing name - Wake
	Done getting mesh sizing parameters
Getting volume mesh

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

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

Writing Tecplot file ....
Finished writing Tecplot file


Getting mesh sizing parameters
	Mesh sizing name - Wake
	Done getting mesh sizing parameters
Getting volume mesh

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

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

Writing Tecplot file ....
Finished writing Tecplot file


Getting mesh sizing parameters
	Mesh sizing name - Wake
	Done getting mesh sizing parameters
Getting volume mesh

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

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

Writing Tecplot file ....
Finished writing Tecplot file

ok
test_MultiBody_quad (test_aflr4.TestAFLR4.test_MultiBody_quad) ... 
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 4
	Name = Wing1, index = 1
	Name = Wing2, index = 2
	Name = Wake, index = 3
	Name = Farfield, index = 4
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 4
	Name = Wing1, index = 1
	Name = Wing2, index = 2
	Name = Wake, index = 3
	Name = Farfield, index = 4
AFLR4    : Proximity BG Surface Grid Generation Skipped
AFLR4    : No Modifications Required
ok
test_SingleBody_output (test_aflr4.TestAFLR4.test_SingleBody_output) ... 
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 2
	Name = Farfield, index = 1
	Name = Wing1, index = 2
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 3
	Name = Farfield, index = 1
	Name = Wing1, index = 2
	Name = trailingEdge, index = 3

Getting mesh sizing parameters
	Mesh sizing name - trailingEdge
	Done getting mesh sizing parameters
ok
test_all (test_aflr4.TestAFLR4.test_all) ... ERROR:: BAD STATUS = -276 from matsol (called from solveSketchOrig:61976)

Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 8
	Name = box, index = 1
	Name = cylinder, index = 2
	Name = cone, index = 3
	Name = torus, index = 4
	Name = sphere, index = 5
	Name = boxhole, index = 6
	Name = bullet, index = 7
	Name = farfield, index = 8
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 1
	Name = box, index = 1
ok
test_box (test_aflr4.TestAFLR4.test_box) ... Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 2
	Name = box, index = 1
	Name = farfield, index = 2
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 1
	Name = box, index = 1
ok
test_boxhole (test_aflr4.TestAFLR4.test_boxhole) ... Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 2
	Name = boxhole, index = 1
	Name = farfield, index = 2
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 0
ok
test_bullet (test_aflr4.TestAFLR4.test_bullet) ... Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 2
	Name = bullet, index = 1
	Name = farfield, index = 2
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 0
ok
test_cone (test_aflr4.TestAFLR4.test_cone) ... Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 2
	Name = cone, index = 1
	Name = farfield, index = 2
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 0
ok
test_cylinder (test_aflr4.TestAFLR4.test_cylinder) ... Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 2
	Name = cylinder, index = 1
	Name = farfield, index = 2
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 0
ok
test_faceMatch (test_aflr4.TestAFLR4.test_faceMatch) ... 
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = wall, index = 1
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 0
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 0
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 0
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = wall, index = 1
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 0
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 0
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 0
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = wall, index = 1
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 0
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 0
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 0
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = wall, index = 1
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 0
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 0
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 0
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = wall, index = 1
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 0
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 0
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 0
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = wall, index = 1
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 0
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 0
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 0
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = wall, index = 1
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 0
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 0
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 0
ok
test_faceMatch_MultiDomain (test_aflr4.TestAFLR4.test_faceMatch_MultiDomain) ... ../csmData/MultiDomain/example1.csm

Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = dummy_att, index = 1
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 0

Writing Tecplot file ....
Finished writing Tecplot file

Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 0

Writing Tecplot file ....
Finished writing Tecplot file

Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 0

Writing Tecplot file ....
Finished writing Tecplot file


Writing Tecplot file ....
Finished writing Tecplot file

../csmData/MultiDomain/example2.csm

Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = dummy_att, index = 1
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 0

Writing Tecplot file ....
Finished writing Tecplot file

Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 0

Writing Tecplot file ....
Finished writing Tecplot file

Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 0

Writing Tecplot file ....
Finished writing Tecplot file


Writing Tecplot file ....
Finished writing Tecplot file


Writing Tecplot file ....
Finished writing Tecplot file

../csmData/MultiDomain/example3.csm

Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = dummy_att, index = 1
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 0

Writing Tecplot file ....
Finished writing Tecplot file

Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 0

Writing Tecplot file ....
Finished writing Tecplot file

Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 0

Writing Tecplot file ....
Finished writing Tecplot file


Writing Tecplot file ....
Finished writing Tecplot file


Writing Tecplot file ....
Finished writing Tecplot file

../csmData/MultiDomain/example4.csm

Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = dummy_att, index = 1
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 0

Writing Tecplot file ....
Finished writing Tecplot file

Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 0

Writing Tecplot file ....
Finished writing Tecplot file

Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 0

Writing Tecplot file ....
Finished writing Tecplot file


Writing Tecplot file ....
Finished writing Tecplot file


Writing Tecplot file ....
Finished writing Tecplot file

../csmData/MultiDomain/example6.csm

Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = dummy_att, index = 1
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 0

Writing Tecplot file ....
Finished writing Tecplot file

Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 0

Writing Tecplot file ....
Finished writing Tecplot file

Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 0

Writing Tecplot file ....
Finished writing Tecplot file


Writing Tecplot file ....
Finished writing Tecplot file


Writing Tecplot file ....
Finished writing Tecplot file

../csmData/MultiDomain/example7.csm

Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = dummy_att, index = 1
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 0

Writing Tecplot file ....
Finished writing Tecplot file

Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 0

Writing Tecplot file ....
Finished writing Tecplot file

Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 0

Writing Tecplot file ....
Finished writing Tecplot file


Writing Tecplot file ....
Finished writing Tecplot file


Writing Tecplot file ....
Finished writing Tecplot file

../csmData/MultiDomain/example8.csm

Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = dummy_att, index = 1
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 0

Writing Tecplot file ....
Finished writing Tecplot file

Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 0

Writing Tecplot file ....
Finished writing Tecplot file

Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 0

Writing Tecplot file ....
Finished writing Tecplot file


Writing Tecplot file ....
Finished writing Tecplot file


Writing Tecplot file ....
Finished writing Tecplot file

../csmData/MultiDomain/example9.csm

Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = dummy_att, index = 1
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 0

Writing Tecplot file ....
Finished writing Tecplot file

Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 0

Writing Tecplot file ....
Finished writing Tecplot file

Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 0

Writing Tecplot file ....
Finished writing Tecplot file


Writing Tecplot file ....
Finished writing Tecplot file

../csmData/MultiDomain/multi_prim.csm

Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = dummy_att, index = 1
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 0

Writing Tecplot file ....
Finished writing Tecplot file

Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 0

Writing Tecplot file ....
Finished writing Tecplot file

Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 0

Writing Tecplot file ....
Finished writing Tecplot file


Writing Tecplot file ....
Finished writing Tecplot file


Writing Tecplot file ....
Finished writing Tecplot file


Writing Tecplot file ....
Finished writing Tecplot file


Writing Tecplot file ....
Finished writing Tecplot file

../csmData/MultiDomain/cyl_seam.csm

Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = dummy_att, index = 1
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 0

Writing Tecplot file ....
Finished writing Tecplot file

Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 0

Writing Tecplot file ....
Finished writing Tecplot file

Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 0

Writing Tecplot file ....
Finished writing Tecplot file


Writing Tecplot file ....
Finished writing Tecplot file

ok
test_invalid_Mesh_Lenght_Scale (test_aflr4.TestAFLR4.test_invalid_Mesh_Lenght_Scale) ... 
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 2
	Name = Farfield, index = 1
	Name = Wing1, index = 2
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 3
	Name = Farfield, index = 1
	Name = Wing1, index = 2
	Name = trailingEdge, index = 3
ok
test_journal (test_aflr4.TestAFLR4.test_journal) ... ERROR:: BAD STATUS = -276 from matsol (called from solveSketchOrig:61976)

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:61976)

ERROR:: BAD STATUS = -276 from matsol (called from solveSketchOrig:61976)

 CAPS Info: Hit last success -- going live!
ERROR:: BAD STATUS = -276 from matsol (called from solveSketchOrig:61976)

 CAPS Info: Hit last success -- going live!
ERROR:: BAD STATUS = -276 from matsol (called from solveSketchOrig:61976)

 CAPS Info: Hit last success -- going live!
ERROR:: BAD STATUS = -276 from matsol (called from solveSketchOrig:61976)

 CAPS Info: Hit last success -- going live!
ERROR:: BAD STATUS = -276 from matsol (called from solveSketchOrig:61976)

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:61976)

 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:61976)

 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:61976)

 CAPS Info: Hit last success -- going live!
ERROR:: BAD STATUS = -276 from matsol (called from solveSketchOrig:61976)

 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:61976)

 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:61976)

ok
test_phase (test_aflr4.TestAFLR4.test_phase) ... ERROR:: BAD STATUS = -276 from matsol (called from solveSketchOrig:61976)

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:61976)

Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 2
	Name = box, index = 1
	Name = farfield, index = 2
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 1
	Name = box, index = 1
ok
test_reenter (test_aflr4.TestAFLR4.test_reenter) ... 
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 2
	Name = Farfield, index = 1
	Name = Wing1, index = 2
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 3
	Name = Farfield, index = 1
	Name = Wing1, index = 2
	Name = trailingEdge, index = 3

Writing Binary VTK file ....
Finished writing Binary VTK file


Writing vtk file ....

Writing vtk surface file ....

capsGroups found:
  1: Farfield
  2: Wing1
Finished writing vtk file


Writing FAST file ....
Finished writing FAST file


Writing SU2 file ....
Finished writing SU2 file


Writing exodus file ....
	Block: 'Farfield_tri', blk_id 1, num_entries 1332
	Block: 'Wing1_tri', blk_id 2, num_entries 73442
	Sideset: 'Farfield', set_id 1, num_entries 1332
	Sideset: 'Wing1', set_id 2, num_entries 73442
Finished writing Exodus file


Writing Binary STL file ....
Finished writing Binary STL file


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


Writing Tecplot file ....
Finished writing Tecplot file


Writing ugrid file ....
Finished writing ugrid file


Writing Binary VTK file ....
Finished writing Binary VTK file


Writing vtk file ....

Writing vtk surface file ....

capsGroups found:
  1: Farfield
  2: Wing1
Finished writing vtk file


Writing FAST file ....
Finished writing FAST file


Writing SU2 file ....
Finished writing SU2 file


Writing exodus file ....
	Block: 'Farfield_tri', blk_id 1, num_entries 300
	Block: 'Wing1_tri', blk_id 2, num_entries 32990
	Sideset: 'Farfield', set_id 1, num_entries 300
	Sideset: 'Wing1', set_id 2, num_entries 32990
Finished writing Exodus file


Writing Binary STL file ....
Finished writing Binary STL file


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


Writing Tecplot file ....
Finished writing Tecplot file


Writing ugrid file ....
Finished writing ugrid file

ok
test_setInput (test_aflr4.TestAFLR4.test_setInput) ...  EGADS Info: 0 Objects, 0 Reference in Use (of 0) at Close!
ok
test_sphere (test_aflr4.TestAFLR4.test_sphere) ... Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 2
	Name = sphere, index = 1
	Name = farfield, index = 2
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 0
ok
test_torus (test_aflr4.TestAFLR4.test_torus) ... Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 2
	Name = torus, index = 1
	Name = farfield, index = 2
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 0
ok
test_Aeroelastic (test_astros.TestAstros.test_Aeroelastic) ... 
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 2
	Name = Rib_Root, index = 1
	Name = Skin, index = 2
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 0
Getting surface mesh for body 1 (of 2)
Getting surface mesh for body 2 (of 2)
Body 1 (of 2)
Number of nodes    = 1
Number of elements = 0
Number of triangle elements      = 0
Number of quadrilateral elements = 0
Body 2 (of 2)
Number of nodes    = 46
Number of elements = 44
Number of triangle elements      = 0
Number of quadrilateral elements = 44
----------------------------
Total number of nodes    = 47
Total number of elements = 44
Mapping Csys attributes ................
	Number of unique Csys attributes = 0

Getting FEA coordinate systems.......
	Number of coordinate systems - 0
	No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
	Number of unique capsConstraint attributes = 1
	Name = Rib_Root_Point, index = 1
Mapping capsLoad attributes ................
	Number of unique capsLoad attributes = 0
Mapping capsBound attributes ................
	Number of unique capsBound attributes = 1
	Name = Skin_Top, index = 1
Mapping capsConnect attributes ................
	Number of unique capsConnect attributes = 1
	Name = Rib_Root, index = 1
Mapping capsResponse attributes ................
	Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
	Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 3
	Name = Rib_Root, index = 1
	Name = Skin, index = 2
	Name = Wing, index = 3
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 3
	Name = Rib_Root, index = 1
	Name = Skin, index = 2
	Name = Wing, index = 3
Setting FEA Data
	Mesh for body = 0
	Number of nodal coordinates = 1
	Number of elements = 1
	Elemental Nodes = 1
	Elemental Rods  = 0
	Elemental Tria3 = 0
	Elemental Quad4 = 0
Setting FEA Data
	Mesh for body = 1
	Number of nodal coordinates = 46
	Number of elements = 44
	Elemental Nodes = 0
	Elemental Rods  = 0
	Elemental Tria3 = 0
	Elemental Quad4 = 44
Combining multiple FEA meshes!
	Combined Number of nodal coordinates = 47
	Combined Number of elements = 45
	Combined Elemental Nodes = 1
	Combined Elemental Rods  = 0
	Combined Elemental Tria3 = 0
	Combined Elemental Quad4 = 44
Getting vortex lattice surface data
	VLM surface name - Skin_Top
	Done getting vortex lattice surface data

Getting FEA vortex lattice mesh
	Surface 1: Number of points found for aero-spline = 3
	Surface 2: Number of points found for aero-spline = 6
	(Re-)Combining all aerodynamic surfaces into a 'Wing', 'Canard', and/or  'Fin' single surfaces !
Aero_Reference value is NULL - No aero reference parameters set

Getting FEA materials.......
	Number of materials - 1
	Material name - Unobtainium
	No "materialType" specified for Material tuple Unobtainium, defaulting to "Isotropic"
	Done getting FEA materials

Getting FEA properties.......
	Number of properties - 2
	Property name - Rib_Root
	No "material" specified for Property tuple Rib_Root, defaulting to an index of 1
	Property name - Skin
	No "material" specified for Property tuple Skin, defaulting to an index of 1
	Done getting FEA properties
Updating mesh element types based on properties input

Getting FEA constraints.......
	Number of constraints - 1
	Constraint name - ribConstraint
	No "constraintType" specified for Constraint tuple ribConstraint, defaulting to "ZeroDisplacement"
	Done getting FEA constraints

Getting FEA supports.......
	Number of supports - 1
	Support name - ribSupport
	Done getting FEA supports

Getting FEA connections.......
	Number of connection tuples - 1
	Connection name - Rib_Root
	No "groupName" specified for Connection tuple Rib_Root!
	Looking for automatic connections from the use of capsConnectLink for Rib_Root
	8 automatic connections were made for capsConnect Rib_Root (node id 1)
	Done getting FEA connections
Load tuple is NULL - No loads applied
Optimization Control tuple is NULL - Default optimization control is used

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

Getting FEA analyses.......
	Number of analyses - 1
	Analysis name - Trim1
	Done getting FEA analyses

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

Writing subElement types (if any) - appending mesh file
Writing connection cards - appending mesh file

Writing Astros instruction file....
	Writing aeros card
	Writing analysis cards
	Writing constraint cards--each subcase individually
	Writing support cards
	Writing material cards
	Writing property cards
	Writing aeroelastic cards


Running Astros......
Note: The following floating-point exceptions are signalling: IEEE_UNDERFLOW_FLAG
Done running Astros!
ok
test_Plate (test_astros.TestAstros.test_Plate) ... 
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = plate, index = 1
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 0
	Face 1 TFI quading disabled with attribute .qParams
Getting surface mesh for body 1 (of 1)
Body 1 (of 1)
Number of nodes    = 25
Number of elements = 16
Number of triangle elements      = 0
Number of quadrilateral elements = 16
----------------------------
Total number of nodes    = 25
Total number of elements = 16
Mapping Csys attributes ................
	Number of unique Csys attributes = 0

Getting FEA coordinate systems.......
	Number of coordinate systems - 0
	No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
	Number of unique capsConstraint attributes = 1
	Name = plateEdge, index = 1
Mapping capsLoad attributes ................
	Number of unique capsLoad attributes = 1
	Name = plate, index = 1
Mapping capsBound attributes ................
	Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
	Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
	Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
	Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
	Mesh for body = 0
	Number of nodal coordinates = 25
	Number of elements = 16
	Elemental Nodes = 0
	Elemental Rods  = 0
	Elemental Tria3 = 0
	Elemental Quad4 = 16
Aero_Reference value is NULL - No aero reference parameters set

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

Getting FEA properties.......
	Number of properties - 1
	Property name - plate
	Done getting FEA properties
Updating mesh element types based on properties input

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

Getting FEA loads.......
	Number of loads - 1
	Load name - appliedPressure
	Done getting FEA loads
Optimization Control tuple is NULL - Default optimization control is used

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

Getting FEA analyses.......
	Number of analyses - 1
	Analysis name - Default
	Done getting FEA analyses

Writing Astros grid and connectivity file ....
Finished writing Astros grid file

Writing subElement types (if any) - appending mesh file

Writing Astros instruction file....
	Writing analysis cards
	Writing load ADD cards
	Writing constraint cards--each subcase individually
	Writing load cards
	Writing material cards
	Writing property cards
Note: The following floating-point exceptions are signalling: IEEE_UNDERFLOW_FLAG
Aero_Reference value is NULL - No aero reference parameters set

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

Getting FEA properties.......
	Number of properties - 1
	Property name - plate
	Done getting FEA properties
Updating mesh element types based on properties input

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

Getting FEA loads.......
	Number of loads - 1
	Load name - appliedPressure
	Done getting FEA loads
Optimization Control tuple is NULL - Default optimization control is used

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

Getting FEA analyses.......
	Number of analyses - 1
	Analysis name - Default
	Done getting FEA analyses

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

Writing subElement types (if any) - appending mesh file

Writing Astros instruction file....
	Writing analysis cards
	Writing load ADD cards
	Writing constraint cards--each subcase individually
	Writing load cards
	Writing material cards
	Writing property cards
Note: The following floating-point exceptions are signalling: IEEE_UNDERFLOW_FLAG
Aero_Reference value is NULL - No aero reference parameters set

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

Getting FEA properties.......
	Number of properties - 1
	Property name - plate
	Done getting FEA properties
Updating mesh element types based on properties input

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

Getting FEA loads.......
	Number of loads - 1
	Load name - appliedPressure
	Done getting FEA loads
Optimization Control tuple is NULL - Default optimization control is used

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

Getting FEA analyses.......
	Number of analyses - 1
	Analysis name - Default
	Done getting FEA analyses

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

Writing subElement types (if any) - appending mesh file

Writing Astros instruction file....
	Writing analysis cards
	Writing load ADD cards
	Writing constraint cards--each subcase individually
	Writing load cards
	Writing material cards
	Writing property cards
Note: The following floating-point exceptions are signalling: IEEE_UNDERFLOW_FLAG
ok
test_MassProp_Units (test_avl.TestAVL.test_MassProp_Units) ... 
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 5
	Name = Wing, index = 1
	Name = hTail, index = 2
	Name = vTail, index = 3
	Name = VTail1, index = 4
	Name = VTail2, index = 5
Getting vortex lattice surface data
	VLM surface name - Wing
	Done getting vortex lattice surface data
Warning: Control RightAileron not found in controls tuple! Only defaults will be used.
Warning: Control RightAileron not found in controls tuple! Only defaults will be used.
Warning: Control LeftAileron not found in controls tuple! Only defaults will be used.
Warning: Control LeftAileron not found in controls tuple! Only defaults will be used.
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 5
	Name = Wing, index = 1
	Name = hTail, index = 2
	Name = vTail, index = 3
	Name = VTail1, index = 4
	Name = VTail2, index = 5
Getting vortex lattice surface data
	VLM surface name - Wing
	Done getting vortex lattice surface data
Warning: Control RightAileron not found in controls tuple! Only defaults will be used.
Warning: Control RightAileron not found in controls tuple! Only defaults will be used.
Warning: Control LeftAileron not found in controls tuple! Only defaults will be used.
Warning: Control LeftAileron not found in controls tuple! Only defaults will be used.
Writing surface - Wing (ID = 0)
	Section 1 of 4 (ID = 3)
	  Control surface 1 of 1 
	Section 2 of 4 (ID = 2)
	  Control surface 1 of 1 
	Section 3 of 4 (ID = 1)
	  Control surface 1 of 1 
	Section 4 of 4 (ID = 0)
	  Control surface 1 of 1 
Writing mass properties file: caps.mass
Parsing MassProp
Note: The following floating-point exceptions are signalling: IEEE_DIVIDE_BY_ZERO
Warning: Control RightAileron not found in controls tuple! Only defaults will be used.
Warning: Control RightAileron not found in controls tuple! Only defaults will be used.
Warning: Control LeftAileron not found in controls tuple! Only defaults will be used.
Warning: Control LeftAileron not found in controls tuple! Only defaults will be used.
Writing mass properties file: caps.mass
Parsing MassProp
Note: The following floating-point exceptions are signalling: IEEE_DIVIDE_BY_ZERO
Warning: Control RightAileron not found in controls tuple! Only defaults will be used.
Warning: Control RightAileron not found in controls tuple! Only defaults will be used.
Warning: Control LeftAileron not found in controls tuple! Only defaults will be used.
Warning: Control LeftAileron not found in controls tuple! Only defaults will be used.
Writing mass properties file: caps.mass
Parsing MassProp
Warning: Control RightAileron not found in controls tuple! Only defaults will be used.
Warning: Control RightAileron not found in controls tuple! Only defaults will be used.
Warning: Control LeftAileron not found in controls tuple! Only defaults will be used.
Warning: Control LeftAileron not found in controls tuple! Only defaults will be used.
Writing mass properties file: caps.mass
Parsing MassProp
Warning: Control RightAileron not found in controls tuple! Only defaults will be used.
Warning: Control RightAileron not found in controls tuple! Only defaults will be used.
Warning: Control LeftAileron not found in controls tuple! Only defaults will be used.
Warning: Control LeftAileron not found in controls tuple! Only defaults will be used.
Writing mass properties file: caps.mass
Parsing MassProp
Warning: Control RightAileron not found in controls tuple! Only defaults will be used.
Warning: Control RightAileron not found in controls tuple! Only defaults will be used.
Warning: Control LeftAileron not found in controls tuple! Only defaults will be used.
Warning: Control LeftAileron not found in controls tuple! Only defaults will be used.
Writing mass properties file: caps.mass
Parsing MassProp
Warning: Control RightAileron not found in controls tuple! Only defaults will be used.
Warning: Control RightAileron not found in controls tuple! Only defaults will be used.
Warning: Control LeftAileron not found in controls tuple! Only defaults will be used.
Warning: Control LeftAileron not found in controls tuple! Only defaults will be used.
Writing mass properties file: caps.mass
Parsing MassProp
Warning: Control RightAileron not found in controls tuple! Only defaults will be used.
Warning: Control RightAileron not found in controls tuple! Only defaults will be used.
Warning: Control LeftAileron not found in controls tuple! Only defaults will be used.
Warning: Control LeftAileron not found in controls tuple! Only defaults will be used.
Writing mass properties file: caps.mass
Parsing MassProp
Warning: Control RightAileron not found in controls tuple! Only defaults will be used.
Warning: Control RightAileron not found in controls tuple! Only defaults will be used.
Warning: Control LeftAileron not found in controls tuple! Only defaults will be used.
Warning: Control LeftAileron not found in controls tuple! Only defaults will be used.
Writing mass properties file: caps.mass
Parsing MassProp
ok
test_MassProp_noUnits (test_avl.TestAVL.test_MassProp_noUnits) ... Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 5
	Name = Wing, index = 1
	Name = hTail, index = 2
	Name = vTail, index = 3
	Name = VTail1, index = 4
	Name = VTail2, index = 5
Getting vortex lattice surface data
	VLM surface name - Wing
	Done getting vortex lattice surface data
Warning: Control RightAileron not found in controls tuple! Only defaults will be used.
Warning: Control RightAileron not found in controls tuple! Only defaults will be used.
Warning: Control LeftAileron not found in controls tuple! Only defaults will be used.
Warning: Control LeftAileron not found in controls tuple! Only defaults will be used.
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 5
	Name = Wing, index = 1
	Name = hTail, index = 2
	Name = vTail, index = 3
	Name = VTail1, index = 4
	Name = VTail2, index = 5
Getting vortex lattice surface data
	VLM surface name - Wing
	Done getting vortex lattice surface data
Warning: Control RightAileron not found in controls tuple! Only defaults will be used.
Warning: Control RightAileron not found in controls tuple! Only defaults will be used.
Warning: Control LeftAileron not found in controls tuple! Only defaults will be used.
Warning: Control LeftAileron not found in controls tuple! Only defaults will be used.
Writing surface - Wing (ID = 0)
	Section 1 of 4 (ID = 3)
	  Control surface 1 of 1 
	Section 2 of 4 (ID = 2)
	  Control surface 1 of 1 
	Section 3 of 4 (ID = 1)
	  Control surface 1 of 1 
	Section 4 of 4 (ID = 0)
	  Control surface 1 of 1 
Writing mass properties file: caps.mass
Parsing MassProp
Note: The following floating-point exceptions are signalling: IEEE_DIVIDE_BY_ZERO
Warning: Control RightAileron not found in controls tuple! Only defaults will be used.
Warning: Control RightAileron not found in controls tuple! Only defaults will be used.
Warning: Control LeftAileron not found in controls tuple! Only defaults will be used.
Warning: Control LeftAileron not found in controls tuple! Only defaults will be used.
Writing mass properties file: caps.mass
Parsing MassProp
Note: The following floating-point exceptions are signalling: IEEE_DIVIDE_BY_ZERO
Warning: Control RightAileron not found in controls tuple! Only defaults will be used.
Warning: Control RightAileron not found in controls tuple! Only defaults will be used.
Warning: Control LeftAileron not found in controls tuple! Only defaults will be used.
Warning: Control LeftAileron not found in controls tuple! Only defaults will be used.
Writing mass properties file: caps.mass
Parsing MassProp
Warning: Control RightAileron not found in controls tuple! Only defaults will be used.
Warning: Control RightAileron not found in controls tuple! Only defaults will be used.
Warning: Control LeftAileron not found in controls tuple! Only defaults will be used.
Warning: Control LeftAileron not found in controls tuple! Only defaults will be used.
Writing mass properties file: caps.mass
Parsing MassProp
Warning: Control RightAileron not found in controls tuple! Only defaults will be used.
Warning: Control RightAileron not found in controls tuple! Only defaults will be used.
Warning: Control LeftAileron not found in controls tuple! Only defaults will be used.
Warning: Control LeftAileron not found in controls tuple! Only defaults will be used.
Writing mass properties file: caps.mass
Parsing MassProp
Warning: Control RightAileron not found in controls tuple! Only defaults will be used.
Warning: Control RightAileron not found in controls tuple! Only defaults will be used.
Warning: Control LeftAileron not found in controls tuple! Only defaults will be used.
Warning: Control LeftAileron not found in controls tuple! Only defaults will be used.
Writing mass properties file: caps.mass
Parsing MassProp
ok
test_alpha_custom_increment (test_avl.TestAVL.test_alpha_custom_increment) ... Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 5
	Name = Wing, index = 1
	Name = hTail, index = 2
	Name = vTail, index = 3
	Name = VTail1, index = 4
	Name = VTail2, index = 5
Getting vortex lattice surface data
	VLM surface name - Wing
	Done getting vortex lattice surface data
Warning: Control RightAileron not found in controls tuple! Only defaults will be used.
Warning: Control RightAileron not found in controls tuple! Only defaults will be used.
Warning: Control LeftAileron not found in controls tuple! Only defaults will be used.
Warning: Control LeftAileron not found in controls tuple! Only defaults will be used.
Writing surface - Wing (ID = 0)
	Section 1 of 4 (ID = 3)
	  Control surface 1 of 1 
	Section 2 of 4 (ID = 2)
	  Control surface 1 of 1 
	Section 3 of 4 (ID = 1)
	  Control surface 1 of 1 
	Section 4 of 4 (ID = 0)
	  Control surface 1 of 1 
Warning: Control RightAileron not found in controls tuple! Only defaults will be used.
Warning: Control RightAileron not found in controls tuple! Only defaults will be used.
Warning: Control LeftAileron not found in controls tuple! Only defaults will be used.
Warning: Control LeftAileron not found in controls tuple! Only defaults will be used.
Warning: Control RightAileron not found in controls tuple! Only defaults will be used.
Warning: Control RightAileron not found in controls tuple! Only defaults will be used.
Warning: Control LeftAileron not found in controls tuple! Only defaults will be used.
Warning: Control LeftAileron not found in controls tuple! Only defaults will be used.
ok
test_geom_change (test_avl.TestAVL.test_geom_change) ... Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 5
	Name = Wing, index = 1
	Name = hTail, index = 2
	Name = vTail, index = 3
	Name = VTail1, index = 4
	Name = VTail2, index = 5
Getting vortex lattice surface data
	VLM surface name - Wing
	Done getting vortex lattice surface data
Warning: Control RightAileron not found in controls tuple! Only defaults will be used.
Warning: Control RightAileron not found in controls tuple! Only defaults will be used.
Warning: Control LeftAileron not found in controls tuple! Only defaults will be used.
Warning: Control LeftAileron not found in controls tuple! Only defaults will be used.
Writing surface - Wing (ID = 0)
	Section 1 of 4 (ID = 3)
	  Control surface 1 of 1 
	Section 2 of 4 (ID = 2)
	  Control surface 1 of 1 
	Section 3 of 4 (ID = 1)
	  Control surface 1 of 1 
	Section 4 of 4 (ID = 0)
	  Control surface 1 of 1 

Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 5
	Name = Wing, index = 1
	Name = hTail, index = 2
	Name = vTail, index = 3
	Name = VTail1, index = 4
	Name = VTail2, index = 5
Getting vortex lattice surface data
	VLM surface name - Wing
	Done getting vortex lattice surface data
Warning: Control RightAileron not found in controls tuple! Only defaults will be used.
Warning: Control RightAileron not found in controls tuple! Only defaults will be used.
Warning: Control LeftAileron not found in controls tuple! Only defaults will be used.
Warning: Control LeftAileron not found in controls tuple! Only defaults will be used.
Writing surface - Wing (ID = 0)
	Section 1 of 4 (ID = 3)
	  Control surface 1 of 1 
	Section 2 of 4 (ID = 2)
	  Control surface 1 of 1 
	Section 3 of 4 (ID = 1)
	  Control surface 1 of 1 
	Section 4 of 4 (ID = 0)
	  Control surface 1 of 1 
ok
test_numSpan (test_avl.TestAVL.test_numSpan) ... 
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 5
	Name = Wing, index = 1
	Name = hTail, index = 2
	Name = vTail, index = 3
	Name = VTail1, index = 4
	Name = VTail2, index = 5
Getting vortex lattice surface data
	VLM surface name - Wing
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 5
	Name = Wing, index = 1
	Name = hTail, index = 2
	Name = vTail, index = 3
	Name = VTail1, index = 4
	Name = VTail2, index = 5
Getting vortex lattice surface data
	VLM surface name - Wing
ok
test_phase (test_avl.TestAVL.test_phase) ... 
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 5
	Name = Wing, index = 1
	Name = hTail, index = 2
	Name = vTail, index = 3
	Name = VTail1, index = 4
	Name = VTail2, index = 5
Getting vortex lattice surface data
	VLM surface name - Wing
	Done getting vortex lattice surface data
Warning: Control RightAileron not found in controls tuple! Only defaults will be used.
Warning: Control RightAileron not found in controls tuple! Only defaults will be used.
Warning: Control LeftAileron not found in controls tuple! Only defaults will be used.
Warning: Control LeftAileron not found in controls tuple! Only defaults will be used.
Writing surface - Wing (ID = 0)
	Section 1 of 4 (ID = 3)
	  Control surface 1 of 1 
	Section 2 of 4 (ID = 2)
	  Control surface 1 of 1 
	Section 3 of 4 (ID = 1)
	  Control surface 1 of 1 
	Section 4 of 4 (ID = 0)
	  Control surface 1 of 1 

Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 5
	Name = Wing, index = 1
	Name = hTail, index = 2
	Name = vTail, index = 3
	Name = VTail1, index = 4
	Name = VTail2, index = 5
Getting vortex lattice surface data
	VLM surface name - Wing
	Done getting vortex lattice surface data
Warning: Control RightAileron not found in controls tuple! Only defaults will be used.
Warning: Control RightAileron not found in controls tuple! Only defaults will be used.
Warning: Control LeftAileron not found in controls tuple! Only defaults will be used.
Warning: Control LeftAileron not found in controls tuple! Only defaults will be used.
Warning: Control RightAileron not found in controls tuple! Only defaults will be used.
Warning: Control RightAileron not found in controls tuple! Only defaults will be used.
Warning: Control LeftAileron not found in controls tuple! Only defaults will be used.
Warning: Control LeftAileron not found in controls tuple! Only defaults will be used.
ok
test_wing_Vtail (test_avl.TestAVL.test_wing_Vtail) ... Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 5
	Name = Wing, index = 1
	Name = hTail, index = 2
	Name = vTail, index = 3
	Name = VTail1, index = 4
	Name = VTail2, index = 5
Getting vortex lattice surface data
	VLM surface name - VTail1
	No "groupName" variable provided or no matches found, going to use tuple name
	VLM surface name - VTail2
	No "groupName" variable provided or no matches found, going to use tuple name
	VLM surface name - Wing
	Done getting vortex lattice surface data
Warning: Control RightAileron not found in controls tuple! Only defaults will be used.
Warning: Control RightAileron not found in controls tuple! Only defaults will be used.
Warning: Control LeftAileron not found in controls tuple! Only defaults will be used.
Warning: Control LeftAileron not found in controls tuple! Only defaults will be used.
Writing surface - VTail1 (ID = 0)
	Section 1 of 2 (ID = 1)
	Section 2 of 2 (ID = 0)
Writing surface - VTail2 (ID = 1)
	Section 1 of 2 (ID = 0)
	Section 2 of 2 (ID = 1)
Writing surface - Wing (ID = 2)
	Section 1 of 4 (ID = 3)
	  Control surface 1 of 1 
	Section 2 of 4 (ID = 2)
	  Control surface 1 of 1 
	Section 3 of 4 (ID = 1)
	  Control surface 1 of 1 
	Section 4 of 4 (ID = 0)
	  Control surface 1 of 1 
ok
test_wing_tail (test_avl.TestAVL.test_wing_tail) ... Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 5
	Name = Wing, index = 1
	Name = hTail, index = 2
	Name = vTail, index = 3
	Name = VTail1, index = 4
	Name = VTail2, index = 5
Getting vortex lattice surface data
	VLM surface name - Wing
	VLM surface name - hTail
	VLM surface name - vTail
	No "groupName" variable provided or no matches found, going to use tuple name
	Done getting vortex lattice surface data
Warning: Control RightAileron not found in controls tuple! Only defaults will be used.
Warning: Control RightAileron not found in controls tuple! Only defaults will be used.
Warning: Control LeftAileron not found in controls tuple! Only defaults will be used.
Warning: Control LeftAileron not found in controls tuple! Only defaults will be used.
Warning: Control Elevator not found in controls tuple! Only defaults will be used.
Warning: Control Elevator not found in controls tuple! Only defaults will be used.
Warning: Control Elevator not found in controls tuple! Only defaults will be used.
Warning: Control Rudder not found in controls tuple! Only defaults will be used.
Warning: Control Rudder not found in controls tuple! Only defaults will be used.
Writing surface - Wing (ID = 0)
	Section 1 of 4 (ID = 3)
	  Control surface 1 of 1 
	Section 2 of 4 (ID = 2)
	  Control surface 1 of 1 
	Section 3 of 4 (ID = 1)
	  Control surface 1 of 1 
	Section 4 of 4 (ID = 0)
	  Control surface 1 of 1 
Writing surface - hTail (ID = 1)
	Section 1 of 3 (ID = 2)
	  Control surface 1 of 1 
	Section 2 of 3 (ID = 1)
	  Control surface 1 of 1 
	Section 3 of 3 (ID = 0)
	  Control surface 1 of 1 
Writing surface - vTail (ID = 2)
	Section 1 of 2 (ID = 0)
	  Control surface 1 of 1 
	Section 2 of 2 (ID = 1)
	  Control surface 1 of 1 
ok
test_wing_tail_control (test_avl.TestAVL.test_wing_tail_control) ... Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 5
	Name = Wing, index = 1
	Name = hTail, index = 2
	Name = vTail, index = 3
	Name = VTail1, index = 4
	Name = VTail2, index = 5
Getting vortex lattice control surface data
	VLM control surface name - Elevator
	VLM control surface name - LeftAileron
	VLM control surface name - RightAileron
	VLM control surface name - Rudder
	Done getting vortex lattice control surface data
Getting vortex lattice surface data
	VLM surface name - Wing
	VLM surface name - hTail
	VLM surface name - vTail
	No "groupName" variable provided or no matches found, going to use tuple name
	Done getting vortex lattice surface data
Writing surface - Wing (ID = 0)
	Section 1 of 4 (ID = 3)
	  Control surface 1 of 1 
	Section 2 of 4 (ID = 2)
	  Control surface 1 of 1 
	Section 3 of 4 (ID = 1)
	  Control surface 1 of 1 
	Section 4 of 4 (ID = 0)
	  Control surface 1 of 1 
Writing surface - hTail (ID = 1)
	Section 1 of 3 (ID = 2)
	  Control surface 1 of 1 
	Section 2 of 3 (ID = 1)
	  Control surface 1 of 1 
	Section 3 of 3 (ID = 0)
	  Control surface 1 of 1 
Writing surface - vTail (ID = 2)
	Section 1 of 2 (ID = 0)
	  Control surface 1 of 1 
	Section 2 of 2 (ID = 1)
	  Control surface 1 of 1 
ok
test_TargetCL (test_cart3d.TestCart3D.test_TargetCL) ... 
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = Wing1, index = 1
 Body size = 15.356535
 Tessellating body 1 with  MaxEdge = 0.383913  Sag = 0.015357  Angle = 15.000000
 Executing: autoInputs -r 28.284271 -nDiv 9 -maxR 7  -mesh2d > autoInputs.out
 Executing: ./aero.csh > aero.out
ok
test_outputs (test_cart3d.TestCart3D.test_outputs) ... ok
test_reenter (test_cart3d.TestCart3D.test_reenter) ... Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = Wing1, index = 1
Getting CFD functional.......
	Number of design variables - 1
	Objective name - Drag
	Done getting CFD functional
 Body size = 15.356535
 Tessellating body 1 with  MaxEdge = 0.383913  Sag = 0.015357  Angle = 15.000000
 Executing: autoInputs -r 80.000000 -nDiv 5 -maxR 7  > autoInputs.out
 Executing: ./aero.csh > aero.out
 Executing: ./aero.csh > aero.out
 Body size = 15.356535
 Tessellating body 1 with  MaxEdge = 0.307131  Sag = 0.015357  Angle = 15.000000
 Executing: autoInputs -r 80.000000 -nDiv 5 -maxR 7  > autoInputs.out
 Executing: ./aero.csh > aero.out
ok
test_sensitivity_AnalysisIn (test_cart3d.TestCart3D.test_sensitivity_AnalysisIn) ... Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = Wing1, index = 1

Getting CFD design variables.......
	Number of design variables - 1
	Design Variable name - Mach
	Done getting CFD design variables
Getting CFD functional.......
	Number of design variables - 3
	Objective name - C_A
	Objective name - C_N
	Objective name - C_Y
	Done getting CFD functional
 Body size = 15.356535
 Tessellating body 1 with  MaxEdge = 0.383913  Sag = 0.015357  Angle = 15.000000
 Executing: autoInputs -r 80.000000 -nDiv 5 -maxR 7  > autoInputs.out
 o Evaluating Cart3D functionals and/or gradients
   ATTENTION: using static geometry ../inputs/Components.i.tri
   (00:24:44) Running aero.csh on 2 core(s) in M0.5A1B0_DP1
   (00:24:47) aero.csh done
 o case M0.5A1B0_DP1, averaging data over 1 cycle(s)
 o Evaluating Cart3D functionals and/or gradients
   ATTENTION: using static geometry ../inputs/Components.i.tri
   (00:24:48) Running aero.csh on 2 core(s) in M0.5A1B0_DP1
   (00:24:54) 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
   (00:24:54) Linearizing cut-cells
   (00:24:54) ... done
   o Number of simultaneous xsensit jobs:  1
   (00:24:54) Computing gradients
   (00:25:02) ... 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
   (00:25:04) Running aero.csh on 2 core(s) in M0.5A1B0_DP1
   (00:25:06) 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
   (00:25:07) Running aero.csh on 2 core(s) in M0.5A1B0_DP1
   (00:25:10) 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
   (00:25:11) Running aero.csh on 2 core(s) in M0.5A1B0_DP1
   (00:25:17) 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
   (00:25:17) Linearizing cut-cells
   (00:25:17) ... done
   o Number of simultaneous xsensit jobs:  1
   (00:25:17) Computing gradients
   (00:25:25) ... 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
   (00:25:26) Running aero.csh on 2 core(s) in M0.5A1B0_DP1
   (00:25:29) 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
   (00:25:31) Running aero.csh on 2 core(s) in M0.5A1B0_DP1
   (00:25:34) 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
   (00:25:35) Running aero.csh on 2 core(s) in M0.5A1B0_DP1
   (00:25:38) 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
   (00:25:39) Linearizing cut-cells
   (00:25:39) ... done
   o Number of simultaneous xsensit jobs:  1
   (00:25:39) Computing gradients
   (00:25:43) ... 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
   (00:25:44) Running aero.csh on 2 core(s) in M0.5A1B0_DP1
   (00:25:47) 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
   (00:25:49) Running aero.csh on 2 core(s) in M0.5A1B0_DP1
   (00:25:51) 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
   (00:25:53) Running aero.csh on 2 core(s) in M0.5A1B0_DP1
   (00:25:56) 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
   (00:25:56) Linearizing cut-cells
   (00:25:56) ... done
   o Number of simultaneous xsensit jobs:  1
   (00:25:56) Computing gradients
   (00:26:00) ... 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
   (00:26:02) Running aero.csh on 2 core(s) in M0.5A1B0_DP1
   (00:26:04) aero.csh done
 o case M0.5A1B0_DP1, averaging data over 1 cycle(s)
Getting CFD functional.......
	Number of design variables - 1
	Objective name - C_n
	Done getting CFD functional
 o Evaluating Cart3D functionals and/or gradients
   ATTENTION: using static geometry ../inputs/Components.i.tri
   (00:26:06) Running aero.csh on 2 core(s) in M0.5A1B0_DP1
   (00:26:08) 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
   (00:26:09) Running aero.csh on 2 core(s) in M0.5A1B0_DP1
   (00:26:12) 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
   (00:26:12) Linearizing cut-cells
   (00:26:12) ... done
   o Number of simultaneous xsensit jobs:  1
   (00:26:12) Computing gradients
   (00:26:16) ... 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
   (00:26:18) Running aero.csh on 2 core(s) in M0.5A1B0_DP1
   (00:26:20) 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
   (00:26:21) Running aero.csh on 2 core(s) in M0.5A1B0_DP1
   (00:26:24) aero.csh done
 o case M0.5A1B0_DP1, averaging data over 1 cycle(s)
 o Evaluating Cart3D functionals and/or gradients
   ATTENTION: using static geometry ../inputs/Components.i.tri
   (00:26:25) Running aero.csh on 2 core(s) in M0.5A1B0_DP1
   (00:26:28) 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
   (00:26:28) Linearizing cut-cells
   (00:26:28) ... done
   o Number of simultaneous xsensit jobs:  1
   (00:26:28) Computing gradients
   (00:26:32) ... 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
   (00:26:34) Running aero.csh on 2 core(s) in M0.5A1B0_DP1
   (00:26:36) aero.csh done
 o case M0.5A1B0_DP1, averaging data over 1 cycle(s)
Getting CFD functional.......
	Number of design variables - 1
	Objective name - C_M_y
	Done getting CFD functional
 o Evaluating Cart3D functionals and/or gradients
   ATTENTION: using static geometry ../inputs/Components.i.tri
   (00:26:37) Running aero.csh on 2 core(s) in M0.5A1B0_DP1
   (00:26:40) 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
   (00:26:41) Running aero.csh on 2 core(s) in M0.5A1B0_DP1
   (00:26:44) 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
   (00:26:44) Linearizing cut-cells
   (00:26:44) ... done
   o Number of simultaneous xsensit jobs:  1
   (00:26:44) Computing gradients
   (00:26:48) ... 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
   (00:26:50) Running aero.csh on 2 core(s) in M0.5A1B0_DP1
   (00:26:52) 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_z
	Done getting CFD functional
 o Evaluating Cart3D functionals and/or gradients
   ATTENTION: using static geometry ../inputs/Components.i.tri
   (00:26:53) Running aero.csh on 2 core(s) in M0.5A1B0_DP1
   (00:26:56) 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
   (00:26:57) Running aero.csh on 2 core(s) in M0.5A1B0_DP1
   (00:26:59) 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
   (00:26:59) Linearizing cut-cells
   (00:26:59) ... done
   o Number of simultaneous xsensit jobs:  1
   (00:27:00) Computing gradients
   (00:27:04) ... 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
   (00:27:05) Running aero.csh on 2 core(s) in M0.5A1B0_DP1
   (00:27:07) 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
   (00:27:10) Running aero.csh on 2 core(s) in M0.5A1B0_DP1
   (00:27:13) aero.csh done
 o case M0.5A1B0_DP1, averaging data over 1 cycle(s)

 o Evaluating Cart3D functionals and/or gradients
   ATTENTION: using static geometry ../inputs/Components.i.tri
   (00:27:14) Running aero.csh on 2 core(s) in M0.5A1B0_DP1
   (00:27:19) 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
   (00:27:20) Linearizing cut-cells
   (00:27:22) ... done
   o Number of simultaneous xsensit jobs:  2
   (00:27:22) Computing gradients
              Adjusted OMP_NUM_THREADS to 1 for xsensit
   (00:27:30) ... 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
   (00:27:31) Running aero.csh on 2 core(s) in M0.5A1B0_DP1
   (00:27:34) aero.csh done
 o case M0.5A1B0_DP1, averaging data over 1 cycle(s)
ok
test_Output (test_cbaero.TestCBAERO.test_Output) ... 
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = Wing1, index = 1
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 2
	Name = Wing1, index = 1
	Name = trailingEdge, index = 2

Writing FAST file ....
Finished writing FAST file

Writing CBAero input file - cbaero_CAPS.cbaero
Writing CBAero tagged regions - TaggedRegions
Writing CBAero setup file - cbaero_CAPS.stp
ok
test_inputs (test_cbaero.TestCBAERO.test_inputs) ... Writing CBAero input file - cbaero_CAPS.cbaero
Writing CBAero tagged regions - TaggedRegions
Writing CBAero setup file - cbaero_CAPS.stp
ok
test_MultiBody (test_egadsTess.TestEGADS.test_MultiBody) ... 
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 4
	Name = Wing1, index = 1
	Name = Wing2, index = 2
	Name = Wake, index = 3
	Name = Farfield, index = 4
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 4
	Name = Wing1, index = 1
	Name = Wing2, index = 2
	Name = Wake, index = 3
	Name = Farfield, index = 4

Getting mesh sizing parameters
	Mesh sizing name - Farfield
	Done getting mesh sizing parameters
ok
test_SingleBody_AnalysisOutVal (test_egadsTess.TestEGADS.test_SingleBody_AnalysisOutVal) ... 
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 2
	Name = Farfield, index = 1
	Name = Wing1, index = 2
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 3
	Name = Farfield, index = 1
	Name = Wing1, index = 2
	Name = trailingEdge, index = 3

Getting mesh sizing parameters
	Mesh sizing name - Farfield
	Done getting mesh sizing parameters
ok
test_all (test_egadsTess.TestEGADS.test_all) ... ERROR:: BAD STATUS = -276 from matsol (called from solveSketchOrig:61976)

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!
 17181B000 EGADS Info: Face #5 -> Edge #17 (9) Internally in Loop 7 4, sen = -1!
 17181B000 EGADS Info: Face #5 -> Edge #17 (9) Internally in Loop 4 7, sen = 1!
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 9
	Name = box, index = 1
	Name = cylinder, index = 2
	Name = cone, index = 3
	Name = torus, index = 4
	Name = sphere, index = 5
	Name = boxhole, index = 6
	Name = bullet, index = 7
	Name = nodeBody, index = 8
	Name = farfield, index = 9
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 1
	Name = box, index = 1
 17181B000 EGADS Info: Face #3 -> Edge #9 (9) Internally in Loop 4 7, sen = -1!
 17181B000 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!
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
 17181B000 EGADS Info: Face #3 -> Edge #9 (9) Internally in Loop 4 7, sen = -1!
 17181B000 EGADS Info: Face #3 -> Edge #9 (9) Internally in Loop 7 4, sen = 1!
 1E2491C40 EGADS Info: Face #5 -> Edge #17 (9) Internally in Loop 7 4, sen = -1!
 1E2491C40 EGADS Info: Face #5 -> Edge #17 (9) Internally in Loop 4 7, sen = 1!
ok
test_box (test_egadsTess.TestEGADS.test_box) ... Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 2
	Name = box, index = 1
	Name = farfield, index = 2
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 1
	Name = box, index = 1
ok
test_boxhole (test_egadsTess.TestEGADS.test_boxhole) ... Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 2
	Name = boxhole, index = 1
	Name = farfield, index = 2
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 0
 1E2491C40 EGADS Info: Face #3 -> Edge #9 (9) Internally in Loop 4 7, sen = -1!
 1E2491C40 EGADS Info: Face #3 -> Edge #9 (9) Internally in Loop 7 4, sen = 1!
 17181B000 EGADS Info: Face #5 -> Edge #17 (9) Internally in Loop 7 4, sen = -1!
 17181B000 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:61976)

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:61976)

ERROR:: BAD STATUS = -276 from matsol (called from solveSketchOrig:61976)

 CAPS Info: Hit last success -- going live!
ERROR:: BAD STATUS = -276 from matsol (called from solveSketchOrig:61976)

 CAPS Info: Hit last success -- going live!
ERROR:: BAD STATUS = -276 from matsol (called from solveSketchOrig:61976)

 CAPS Info: Hit last success -- going live!
ERROR:: BAD STATUS = -276 from matsol (called from solveSketchOrig:61976)

 CAPS Info: Hit last success -- going live!
ERROR:: BAD STATUS = -276 from matsol (called from solveSketchOrig:61976)

 CAPS Info: Hit last success -- going live!
ERROR:: BAD STATUS = -276 from matsol (called from solveSketchOrig:61976)

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:61976)

 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:61976)

 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:61976)

 CAPS Info: Hit last success -- going live!
ERROR:: BAD STATUS = -276 from matsol (called from solveSketchOrig:61976)

 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:61976)

 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:61976)

 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:61976)

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:61976)

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:61976)

Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 2
	Name = box, index = 1
	Name = farfield, index = 2
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 1
	Name = box, index = 1

Getting mesh sizing parameters
	Mesh sizing name - box
	Done getting mesh sizing parameters
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 2
	Name = box, index = 1
	Name = farfield, index = 2
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 1
	Name = box, index = 1

Getting mesh sizing parameters
	Mesh sizing name - box
	Done getting mesh sizing parameters
ok
test_reenter (test_egadsTess.TestEGADS.test_reenter) ... 
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 2
	Name = Farfield, index = 1
	Name = Wing1, index = 2
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 3
	Name = Farfield, index = 1
	Name = Wing1, index = 2
	Name = trailingEdge, index = 3

Getting mesh sizing parameters
	Mesh sizing name - Farfield
	Done getting mesh sizing parameters

Writing Binary VTK file ....
Finished writing Binary VTK file


Writing vtk file ....

Writing vtk surface file ....

capsGroups found:
  1: Farfield
  2: Wing1
Finished writing vtk file


Writing FAST file ....
Finished writing FAST file


Writing SU2 file ....
Finished writing SU2 file


Writing exodus file ....
	Block: 'Farfield_tri', blk_id 1, num_entries 48
	Block: 'Wing1_tri', blk_id 2, num_entries 19110
	Sideset: 'Farfield', set_id 1, num_entries 48
	Sideset: 'Wing1', set_id 2, num_entries 19110
Finished writing Exodus file


Writing Binary STL file ....
Finished writing Binary STL file


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


Writing Tecplot file ....
Finished writing Tecplot file


Writing ugrid file ....
Finished writing ugrid file

Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 2
	Name = Farfield, index = 1
	Name = Wing1, index = 2
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 3
	Name = Farfield, index = 1
	Name = Wing1, index = 2
	Name = trailingEdge, index = 3

Getting mesh sizing parameters
	Mesh sizing name - Farfield
	Done getting mesh sizing parameters

Writing Binary VTK file ....
Finished writing Binary VTK file


Writing vtk file ....

Writing vtk surface file ....

capsGroups found:
  1: Farfield
  2: Wing1
Finished writing vtk file


Writing FAST file ....
Finished writing FAST file


Writing SU2 file ....
Finished writing SU2 file


Writing exodus file ....
	Block: 'Farfield_tri', blk_id 1, num_entries 12
	Block: 'Wing1_tri', blk_id 2, num_entries 14282
	Sideset: 'Farfield', set_id 1, num_entries 12
	Sideset: 'Wing1', set_id 2, num_entries 14282
Finished writing Exodus file


Writing Binary STL file ....
Finished writing Binary STL file


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


Writing Tecplot file ....
Finished writing Tecplot file


Writing ugrid file ....
Finished writing ugrid file

ok
test_setInput (test_egadsTess.TestEGADS.test_setInput) ...  EGADS Info: 0 Objects, 0 Reference in Use (of 0) at Close!
ok
test_sphere (test_egadsTess.TestEGADS.test_sphere) ... Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 2
	Name = sphere, index = 1
	Name = farfield, index = 2
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 0
ok
test_torus (test_egadsTess.TestEGADS.test_torus) ... Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 2
	Name = torus, index = 1
	Name = farfield, index = 2
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 0
ok
test_Design_SensFile (test_fun3d.TestFUN3D.test_Design_SensFile) ... 
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 3
	Name = Wing1, index = 1
	Name = Wing2, index = 2
	Name = Farfield, index = 3
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 3
	Name = Wing1, index = 1
	Name = Wing2, index = 2
	Name = Farfield, index = 3

Getting mesh sizing parameters
	Mesh sizing name - Farfield
	Done getting mesh sizing parameters
Getting surface mesh for body 1 (of 3)
Getting surface mesh for body 2 (of 3)
Getting surface mesh for body 3 (of 3)
Body 1 (of 3)
Number of nodes    = 7800
Number of elements = 15596
Number of triangle elements      = 15596
Number of quadrilateral elements = 0
Body 2 (of 3)
Number of nodes    = 5906
Number of elements = 11808
Number of triangle elements      = 11808
Number of quadrilateral elements = 0
Body 3 (of 3)
Number of nodes    = 542
Number of elements = 1080
Number of triangle elements      = 1080
Number of quadrilateral elements = 0
----------------------------
Total number of nodes    = 14248
Total number of elements = 28484
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 3
	Name = Wing1, index = 1
	Name = Wing2, index = 2
	Name = Farfield, index = 3
Number of surface: nodes - 14248, elements - 28484
Getting volume mesh

Generating volume mesh using TetGen.....

Tetgen input string = pYq1.500/0.000T1.00e-16A
Delaunizing vertices...
Delaunay seconds:  0.113577
Creating surface mesh ...
Surface mesh seconds:  0.015469
Recovering boundaries...
Boundary recovery seconds:  0.12527
Removing exterior tetrahedra ...
Spreading region attributes.
Exterior tets removal seconds:  0.030088
Recovering Delaunayness...
Delaunay recovery seconds:  0.057712
Refining mesh...
  18992 insertions, added 13405 points, 688228 tetrahedra in queue.
  6324 insertions, added 2619 points, 589108 tetrahedra in queue.
  8430 insertions, added 2014 points, 124223 tetrahedra in queue.
Refinement seconds:  2.06175
Smoothing vertices...
Mesh smoothing seconds:  1.80891
Improving mesh...
Mesh improvement seconds:  0.040675

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

Output seconds:  0.006546
Total running seconds:  4.26035

Statistics:

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

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

Done meshing using TetGen!
Getting CFD boundary conditions
	Boundary condition name - Farfield
	Boundary condition name - Wing1
	Boundary condition name - Wing2
	Done getting CFD boundary conditions

Getting CFD design variables.......
	Number of design variables - 5
	Design Variable name - Mach
Warning: No initial value set for Mach
	Design Variable name - area
	Design Variable name - aspect
	Design Variable name - taper
	Design Variable name - twist
	Done getting CFD design variables
Python library was linked, but will not be used!
Creating FUN3D directory tree

Writing MAPBC file ....
Finished writing MAPBC file

Warning: The fun3d.nml file will be overwritten!
Writing fun3d.nml
Info: No recognized data transfer names found.








ok
test_Design_Sensitivity (test_fun3d.TestFUN3D.test_Design_Sensitivity) ... Getting CFD boundary conditions
	Boundary condition name - Farfield
	Boundary condition name - Wing1
	Boundary condition name - Wing2
	Done getting CFD boundary conditions

Getting CFD design variables.......
	Number of design variables - 6
	Design Variable name - Alpha
	Design Variable name - Beta
Warning: No initial value set for Beta
	Design Variable name - area
	Design Variable name - aspect
	Design Variable name - taper
	Design Variable name - twist
	Done getting CFD design variables
Getting CFD functional.......
	Number of design variables - 2
	Objective name - Composite
	Objective name - Lift^2
	Done getting CFD functional
Python library was linked, but will not be used!
Creating FUN3D directory tree
Writing rubber.data 

Writing MAPBC file ....
Finished writing MAPBC file

Warning: The fun3d.nml file will be overwritten!
Writing fun3d.nml
Info: No recognized data transfer names found.
Reading rubber.data 
Creating FUN3D directory tree
DesignVariable = Alpha
DesignVariable = Beta
DesignVariable = area
DesignVariable = aspect
DesignVariable = taper
DesignVariable = twist








Writing sensitivity file for body 1, File - Rubberize/model.tec.1.sd1
Writing sensitivity file for body 2, File - Rubberize/model.tec.2.sd1
Writing sensitivity file for body 3, File - Rubberize/model.tec.3.sd1
Writing rubber.data 

Writing MAPBC file ....
Finished writing MAPBC file


Using Python to write FUN3D namelist (fun3d.nml)
	Overwrite_NML is set to 'True' - a new namelist will be created
	Creating namelist
	Done writing nml file with Python
Info: No recognized data transfer names found.
Reading rubber.data 

Getting CFD design variables.......
	Number of design variables - 1
	Design Variable name - Alpha
	Done getting CFD design variables
Getting CFD functional.......
	Number of design variables - 2
	Objective name - Composite
	Objective name - Lift^2
	Done getting CFD functional
Creating FUN3D directory tree
DesignVariable = Alpha
Writing rubber.data 

Writing MAPBC file ....
Finished writing MAPBC file


Using Python to write FUN3D namelist (fun3d.nml)
	Overwrite_NML is set to 'True' - a new namelist will be created
	Creating namelist
	Done writing nml file with Python
Info: No recognized data transfer names found.
Reading rubber.data 
ok
test_Mesh_Morph_Sensitivity (test_fun3d.TestFUN3D.test_Mesh_Morph_Sensitivity) ... Getting CFD boundary conditions
	Boundary condition name - Farfield
	Boundary condition name - Wing1
	Boundary condition name - Wing2
	Done getting CFD boundary conditions

Getting CFD design variables.......
	Number of design variables - 6
	Design Variable name - Alpha
	Design Variable name - Beta
Warning: No initial value set for Beta
	Design Variable name - area
	Design Variable name - aspect
	Design Variable name - taper
	Design Variable name - twist
	Done getting CFD design variables
Getting CFD functional.......
	Number of design variables - 2
	Objective name - Composite
	Objective name - Lift^2
	Done getting CFD functional
Python library was linked, but will not be used!
Creating FUN3D directory tree
DesignVariable = Alpha
DesignVariable = Beta
DesignVariable = area
DesignVariable = aspect
DesignVariable = taper
DesignVariable = twist








Writing sensitivity file for body 1, File - Rubberize/model.tec.1.sd1
Writing sensitivity file for body 2, File - Rubberize/model.tec.2.sd1
Writing sensitivity file for body 3, File - Rubberize/model.tec.3.sd1
Writing rubber.data 
Writing surface file for 1 (of 3) in body 1 File - Flow/fun3d_CAPS_body1.dat
Writing surface file for 1 (of 3) in body 1 File - Flow/fun3d_CAPS_body1.dat
Writing surface file for 1 (of 3) in body 1 File - Flow/fun3d_CAPS_body1.dat

Writing MAPBC file ....
Finished writing MAPBC file

Warning: The fun3d.nml file will be overwritten!
Writing fun3d.nml
Info: No recognized data transfer names found.
Reading rubber.data 

Projecting tessellation 1 (of 3) on to new body
Projecting tessellation 2 (of 3) on to new body
Projecting tessellation 3 (of 3) on to new body
Python library was linked, but will not be used!
Creating FUN3D directory tree
DesignVariable = Alpha
DesignVariable = Beta
DesignVariable = area
DesignVariable = aspect
DesignVariable = taper
DesignVariable = twist








Writing sensitivity file for body 1, File - Rubberize/model.tec.1.sd1
Writing sensitivity file for body 2, File - Rubberize/model.tec.2.sd1
Writing sensitivity file for body 3, File - Rubberize/model.tec.3.sd1
Writing surface file for 1 (of 3) in body 1 File - Flow/fun3d_CAPS_body1.dat
Writing surface file for 1 (of 3) in body 1 File - Flow/fun3d_CAPS_body1.dat
Writing surface file for 1 (of 3) in body 1 File - Flow/fun3d_CAPS_body1.dat

Writing MAPBC file ....
Finished writing MAPBC file

Warning: The fun3d.nml file will be overwritten!
Writing fun3d.nml
Info: No recognized data transfer names found.
Reading rubber.data 

Projecting tessellation 1 (of 3) on to new body
Projecting tessellation 2 (of 3) on to new body
Projecting tessellation 3 (of 3) on to new body
Python library was linked, but will not be used!
Creating FUN3D directory tree
DesignVariable = Alpha
DesignVariable = Beta
DesignVariable = area
DesignVariable = aspect
DesignVariable = taper
DesignVariable = twist








Writing sensitivity file for body 1, File - Rubberize/model.tec.1.sd1
Writing sensitivity file for body 2, File - Rubberize/model.tec.2.sd1
Writing sensitivity file for body 3, File - Rubberize/model.tec.3.sd1
Writing surface file for 1 (of 3) in body 1 File - Flow/fun3d_CAPS_body1.dat
Writing surface file for 1 (of 3) in body 1 File - Flow/fun3d_CAPS_body1.dat
Writing surface file for 1 (of 3) in body 1 File - Flow/fun3d_CAPS_body1.dat

Writing MAPBC file ....
Finished writing MAPBC file

Warning: The fun3d.nml file will be overwritten!
Writing fun3d.nml
Info: No recognized data transfer names found.
Reading rubber.data 
ok
test_cythonNML (test_fun3d.TestFUN3D.test_cythonNML) ... Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 3
	Name = Wing1, index = 1
	Name = Wing2, index = 2
	Name = Farfield, index = 3
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 3
	Name = Wing1, index = 1
	Name = Wing2, index = 2
	Name = Farfield, index = 3

Getting mesh sizing parameters
	Mesh sizing name - Farfield
	Done getting mesh sizing parameters
Getting surface mesh for body 1 (of 3)
Getting surface mesh for body 2 (of 3)
Getting surface mesh for body 3 (of 3)
Body 1 (of 3)
Number of nodes    = 7800
Number of elements = 15596
Number of triangle elements      = 15596
Number of quadrilateral elements = 0
Body 2 (of 3)
Number of nodes    = 5906
Number of elements = 11808
Number of triangle elements      = 11808
Number of quadrilateral elements = 0
Body 3 (of 3)
Number of nodes    = 542
Number of elements = 1080
Number of triangle elements      = 1080
Number of quadrilateral elements = 0
----------------------------
Total number of nodes    = 14248
Total number of elements = 28484
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 3
	Name = Wing1, index = 1
	Name = Wing2, index = 2
	Name = Farfield, index = 3
Number of surface: nodes - 14248, elements - 28484
Getting volume mesh

Generating volume mesh using TetGen.....

Tetgen input string = pYq1.500/0.000T1.00e-16A
Delaunizing vertices...
Delaunay seconds:  0.147865
Creating surface mesh ...
Surface mesh seconds:  0.014424
Recovering boundaries...
Boundary recovery seconds:  0.132412
Removing exterior tetrahedra ...
Spreading region attributes.
Exterior tets removal seconds:  0.026383
Recovering Delaunayness...
Delaunay recovery seconds:  0.04932
Refining mesh...
  18992 insertions, added 13405 points, 688228 tetrahedra in queue.
  6324 insertions, added 2619 points, 589108 tetrahedra in queue.
  8430 insertions, added 2014 points, 124223 tetrahedra in queue.
Refinement seconds:  1.99747
Smoothing vertices...
Mesh smoothing seconds:  1.8306
Improving mesh...
Mesh improvement seconds:  0.052351

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

Output seconds:  0.00595
Total running seconds:  4.25707

Statistics:

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

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

Done meshing using TetGen!
Getting CFD boundary conditions
	Boundary condition name - Farfield
	Boundary condition name - Wing1
	Boundary condition name - Wing2
	Done getting CFD boundary conditions

Writing MAPBC file ....
Finished writing MAPBC file


Using Python to write FUN3D namelist (fun3d.nml)

	Reading /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/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_Beta/7.8/DARWIN_ARM64/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_Beta/7.8/DARWIN_ARM64/EngSketchPad/src/CAPS/aim/unitTest/pyCAPS/workDir_fun3dTest/Scratch/fun3dAIM6/fun3d.nml .....
	Appending namelist
	Done writing nml file with Python
Info: No recognized data transfer names found.
ok
test_invalidBoundary (test_fun3d.TestFUN3D.test_invalidBoundary) ... Getting CFD boundary conditions
	Boundary condition name - Wing1
ok
test_invalidBoundaryName (test_fun3d.TestFUN3D.test_invalidBoundaryName) ... Getting CFD boundary conditions
	Boundary condition name - Farfield
	Boundary condition name - Wing1
	Boundary condition name - X
ok
test_journal (test_fun3d.TestFUN3D.test_journal) ... 
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 3
	Name = Wing1, index = 1
	Name = Wing2, index = 2
	Name = Farfield, index = 3
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 3
	Name = Wing1, index = 1
	Name = Wing2, index = 2
	Name = Farfield, index = 3

Getting mesh sizing parameters
	Mesh sizing name - Farfield
	Done getting mesh sizing parameters
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 3
	Name = Wing1, index = 1
	Name = Wing2, index = 2
	Name = Farfield, index = 3
Number of surface: nodes - 5097, elements - 10182
Getting volume mesh

Generating volume mesh using TetGen.....

Tetgen input string = pYq1.500/0.000QT1.00e-16A
Done meshing using TetGen!
Getting CFD boundary conditions
	Boundary condition name - Farfield
	Boundary condition name - Wing1
	Boundary condition name - Wing2
	Done getting CFD boundary conditions

Getting CFD design variables.......
	Number of design variables - 4
	Design Variable name - area
	Design Variable name - aspect
	Design Variable name - taper
	Design Variable name - twist
	Done getting CFD design variables
Python library was linked, but will not be used!
Creating FUN3D directory tree

Writing MAPBC file ....
Finished writing MAPBC file

Warning: The fun3d.nml file will be overwritten!
Writing fun3d.nml
Info: No recognized data transfer names found.








 EGADS Info: 0 Objects, 0 Reference in Use (of 0) at Close!


 CAPS Info: Hit last success -- going live!

 CAPS Info: Hit last success -- going live!

 CAPS Info: Hit last success -- going live!

 CAPS Info: Hit last success -- going live!

 CAPS Info: Hit last success -- going live!

 CAPS Info: Hit last success -- going live!

 CAPS Info: Hit last success -- going live!


 CAPS Info: Hit last success -- going live!


 CAPS Info: Hit last success -- going live!

 CAPS Info: Hit last success -- going live!

 CAPS Info: Hit last success -- going live!

 CAPS Info: Hit last success -- going live!

 CAPS Info: Hit last success -- going live!

 CAPS Info: Hit last success -- going live!

Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 3
	Name = Wing1, index = 1
	Name = Wing2, index = 2
	Name = Farfield, index = 3
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 3
	Name = Wing1, index = 1
	Name = Wing2, index = 2
	Name = Farfield, index = 3

Getting mesh sizing parameters
	Mesh sizing name - Farfield
	Done getting mesh sizing parameters
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 3
	Name = Wing1, index = 1
	Name = Wing2, index = 2
	Name = Farfield, index = 3
Number of surface: nodes - 5097, elements - 10182
Getting volume mesh

Generating volume mesh using TetGen.....

Tetgen input string = pYq1.500/0.000QT1.00e-16A
Done meshing using TetGen!
Getting CFD boundary conditions
	Boundary condition name - Farfield
	Boundary condition name - Wing1
	Boundary condition name - Wing2
	Done getting CFD boundary conditions

Getting CFD design variables.......
	Number of design variables - 4
	Design Variable name - area
	Design Variable name - aspect
	Design Variable name - taper
	Design Variable name - twist
	Done getting CFD design variables
Python library was linked, but will not be used!
Creating FUN3D directory tree

Writing MAPBC file ....
Finished writing MAPBC file

Warning: The fun3d.nml file will be overwritten!
Writing fun3d.nml
Info: No recognized data transfer names found.

 CAPS Info: Hit last success -- going live!
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 3
	Name = Wing1, index = 1
	Name = Wing2, index = 2
	Name = Farfield, index = 3
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 3
	Name = Wing1, index = 1
	Name = Wing2, index = 2
	Name = Farfield, index = 3

Getting mesh sizing parameters
	Mesh sizing name - Farfield
	Done getting mesh sizing parameters

 CAPS Info: Hit last success -- going live!
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 3
	Name = Wing1, index = 1
	Name = Wing2, index = 2
	Name = Farfield, index = 3
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 3
	Name = Wing1, index = 1
	Name = Wing2, index = 2
	Name = Farfield, index = 3

Getting mesh sizing parameters
	Mesh sizing name - Farfield
	Done getting mesh sizing parameters
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 3
	Name = Wing1, index = 1
	Name = Wing2, index = 2
	Name = Farfield, index = 3
Getting CFD boundary conditions
	Boundary condition name - Farfield
	Boundary condition name - Wing1
	Boundary condition name - Wing2
	Done getting CFD boundary conditions

Getting CFD design variables.......
	Number of design variables - 4
	Design Variable name - area
	Design Variable name - aspect
	Design Variable name - taper
	Design Variable name - twist
	Done getting CFD design variables









 CAPS Info: Hit last success -- going live!

 CAPS Info: Hit last success -- going live!

 CAPS Info: Hit last success -- going live!

 CAPS Info: Hit last success -- going live!

 CAPS Info: Hit last success -- going live!

 CAPS Info: Hit last success -- going live!

ok
test_moving_body (test_fun3d.TestFUN3D.test_moving_body) ... Getting CFD boundary conditions
	Boundary condition name - Farfield
	Boundary condition name - Wing1
	Boundary condition name - Wing2
	Done getting CFD boundary conditions
Python library was linked, but will not be used!

Writing MAPBC file ....
Finished writing MAPBC file

Warning: The fun3d.nml file will be overwritten!
Writing fun3d.nml
Info: No recognized data transfer names found.
Writing moving_body.input
ok
test_overwriteNML (test_fun3d.TestFUN3D.test_overwriteNML) ... Getting CFD boundary conditions
	Boundary condition name - Farfield
	Boundary condition name - Wing1
	Boundary condition name - Wing2
	Done getting CFD boundary conditions
Python library was linked, but will not be used!

Writing MAPBC file ....
Finished writing MAPBC file

Since Python was not linked and/or being used, the "Overwrite_NML" input needs to be set to "True" to give permission to create a new fun3d.nml. fun3d.nml will NOT be updated!!
Info: No recognized data transfer names found.
ok
test_phase (test_fun3d.TestFUN3D.test_phase) ... 
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 3
	Name = Wing1, index = 1
	Name = Wing2, index = 2
	Name = Farfield, index = 3
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 3
	Name = Wing1, index = 1
	Name = Wing2, index = 2
	Name = Farfield, index = 3

Getting mesh sizing parameters
	Mesh sizing name - Farfield
	Done getting mesh sizing parameters
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 3
	Name = Wing1, index = 1
	Name = Wing2, index = 2
	Name = Farfield, index = 3
Number of surface: nodes - 14248, elements - 28484
Getting volume mesh

Generating volume mesh using TetGen.....

Tetgen input string = pYq1.500/0.000QT1.00e-16A
Done meshing using TetGen!
Getting CFD boundary conditions
	Boundary condition name - Farfield
	Boundary condition name - Wing1
	Boundary condition name - Wing2
	Done getting CFD boundary conditions
Python library was linked, but will not be used!

Writing MAPBC file ....
Finished writing MAPBC file

Since Python was not linked and/or being used, the "Overwrite_NML" input needs to be set to "True" to give permission to create a new fun3d.nml. fun3d.nml will NOT be updated!!
Info: No recognized data transfer names found.

Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 3
	Name = Wing1, index = 1
	Name = Wing2, index = 2
	Name = Farfield, index = 3
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 3
	Name = Wing1, index = 1
	Name = Wing2, index = 2
	Name = Farfield, index = 3

Getting mesh sizing parameters
	Mesh sizing name - Farfield
	Done getting mesh sizing parameters
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 3
	Name = Wing1, index = 1
	Name = Wing2, index = 2
	Name = Farfield, index = 3
Getting CFD boundary conditions
	Boundary condition name - Farfield
	Boundary condition name - Wing1
	Boundary condition name - Wing2
	Done getting CFD boundary conditions
Python library was linked, but will not be used!

Writing MAPBC file ....
Finished writing MAPBC file

Since Python was not linked and/or being used, the "Overwrite_NML" input needs to be set to "True" to give permission to create a new fun3d.nml. fun3d.nml will NOT be updated!!
Info: No recognized data transfer names found.
ok
test_reenter (test_fun3d.TestFUN3D.test_reenter) ... Getting CFD boundary conditions
	Boundary condition name - Farfield
	Boundary condition name - Wing1
	Boundary condition name - Wing2
	Done getting CFD boundary conditions
Python library was linked, but will not be used!

Writing MAPBC file ....
Finished writing MAPBC file

Warning: The fun3d.nml file will be overwritten!
Writing fun3d.nml
Info: No recognized data transfer names found.
Getting CFD boundary conditions
	Boundary condition name - Farfield
	Boundary condition name - Wing1
	Boundary condition name - Wing2
	Done getting CFD boundary conditions
Python library was linked, but will not be used!

Writing MAPBC file ....
Finished writing MAPBC file

Warning: The fun3d.nml file will be overwritten!
Writing fun3d.nml
Info: No recognized data transfer names found.
ok
test_symmetry (test_fun3d.TestFUN3D.test_symmetry) ... Getting CFD boundary conditions
	Boundary condition name - Farfield
	Boundary condition name - Wing1
	Boundary condition name - Wing2
	Done getting CFD boundary conditions
Python library was linked, but will not be used!

Writing MAPBC file ....
Finished writing MAPBC file

Since Python was not linked and/or being used, the "Overwrite_NML" input needs to be set to "True" to give permission to create a new fun3d.nml. fun3d.nml will NOT be updated!!
Info: No recognized data transfer names found.
ok
test_box1 (test_masstran.TestMasstran.test_box1) ... 
Mapping Csys attributes ................
	Number of unique Csys attributes = 0

Getting FEA coordinate systems.......
	Number of coordinate systems - 0
	No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
	Number of unique capsConstraint attributes = 0
Mapping capsLoad attributes ................
	Number of unique capsLoad attributes = 0
Mapping capsBound attributes ................
	Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
	Number of unique capsConnect attributes = 0
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = box1, index = 1
Setting FEA Data
	Mesh for body = 0
	Number of nodal coordinates = 2402
	Number of elements = 2400
	Elemental Nodes = 0
	Elemental Rods  = 0
	Elemental Tria3 = 0
	Elemental Quad4 = 2400

Getting FEA materials.......
	Number of materials - 2
	Material name - madeupium
	Material name - unobtainium
	Done getting FEA materials

Getting FEA properties.......
	Number of properties - 1
	Property name - box1
	Done getting FEA properties
Updating mesh element types based on properties input
Updating mesh element types based on properties input

Getting FEA design variables.......
	Number of design variables          - 7
	Design_Variable name - H
	Design_Variable name - L
	Design_Variable name - W
	Design_Variable name - m0
	Design_Variable name - m1
	Design_Variable name - x0
	Design_Variable name - x1
	Design_Variable_Relation name - rho_madeupium
	Name madeupium not found in attribute map!!!!
	Design_Variable_Relation name - rho_unobtainium
	Name unobtainium not found in attribute map!!!!
	Design_Variable_Relation name - thick_box1
	Number of design variable relations - 3
	Done getting FEA design variables



===> L

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

Getting FEA coordinate systems.......
	Number of coordinate systems - 0
	No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
	Number of unique capsConstraint attributes = 0
Mapping capsLoad attributes ................
	Number of unique capsLoad attributes = 0
Mapping capsBound attributes ................
	Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
	Number of unique capsConnect attributes = 0
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = box1, index = 1
Setting FEA Data
	Mesh for body = 0
	Number of nodal coordinates = 2402
	Number of elements = 2400
	Elemental Nodes = 0
	Elemental Rods  = 0
	Elemental Tria3 = 0
	Elemental Quad4 = 2400
Updating mesh element types based on properties input

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

Getting FEA coordinate systems.......
	Number of coordinate systems - 0
	No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
	Number of unique capsConstraint attributes = 0
Mapping capsLoad attributes ................
	Number of unique capsLoad attributes = 0
Mapping capsBound attributes ................
	Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
	Number of unique capsConnect attributes = 0
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = box1, index = 1
Setting FEA Data
	Mesh for body = 0
	Number of nodal coordinates = 2402
	Number of elements = 2400
	Elemental Nodes = 0
	Elemental Rods  = 0
	Elemental Tria3 = 0
	Elemental Quad4 = 2400
Updating mesh element types based on properties input
===> W

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

Getting FEA coordinate systems.......
	Number of coordinate systems - 0
	No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
	Number of unique capsConstraint attributes = 0
Mapping capsLoad attributes ................
	Number of unique capsLoad attributes = 0
Mapping capsBound attributes ................
	Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
	Number of unique capsConnect attributes = 0
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = box1, index = 1
Setting FEA Data
	Mesh for body = 0
	Number of nodal coordinates = 2402
	Number of elements = 2400
	Elemental Nodes = 0
	Elemental Rods  = 0
	Elemental Tria3 = 0
	Elemental Quad4 = 2400
Updating mesh element types based on properties input

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

Getting FEA coordinate systems.......
	Number of coordinate systems - 0
	No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
	Number of unique capsConstraint attributes = 0
Mapping capsLoad attributes ................
	Number of unique capsLoad attributes = 0
Mapping capsBound attributes ................
	Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
	Number of unique capsConnect attributes = 0
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = box1, index = 1
Setting FEA Data
	Mesh for body = 0
	Number of nodal coordinates = 2402
	Number of elements = 2400
	Elemental Nodes = 0
	Elemental Rods  = 0
	Elemental Tria3 = 0
	Elemental Quad4 = 2400
Updating mesh element types based on properties input
===> H

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

Getting FEA coordinate systems.......
	Number of coordinate systems - 0
	No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
	Number of unique capsConstraint attributes = 0
Mapping capsLoad attributes ................
	Number of unique capsLoad attributes = 0
Mapping capsBound attributes ................
	Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
	Number of unique capsConnect attributes = 0
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = box1, index = 1
Setting FEA Data
	Mesh for body = 0
	Number of nodal coordinates = 2402
	Number of elements = 2400
	Elemental Nodes = 0
	Elemental Rods  = 0
	Elemental Tria3 = 0
	Elemental Quad4 = 2400
Updating mesh element types based on properties input

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

Getting FEA coordinate systems.......
	Number of coordinate systems - 0
	No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
	Number of unique capsConstraint attributes = 0
Mapping capsLoad attributes ................
	Number of unique capsLoad attributes = 0
Mapping capsBound attributes ................
	Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
	Number of unique capsConnect attributes = 0
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = box1, index = 1
Setting FEA Data
	Mesh for body = 0
	Number of nodal coordinates = 2402
	Number of elements = 2400
	Elemental Nodes = 0
	Elemental Rods  = 0
	Elemental Tria3 = 0
	Elemental Quad4 = 2400
Updating mesh element types based on properties input
===> x0

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

Getting FEA coordinate systems.......
	Number of coordinate systems - 0
	No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
	Number of unique capsConstraint attributes = 0
Mapping capsLoad attributes ................
	Number of unique capsLoad attributes = 0
Mapping capsBound attributes ................
	Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
	Number of unique capsConnect attributes = 0
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = box1, index = 1
Setting FEA Data
	Mesh for body = 0
	Number of nodal coordinates = 2402
	Number of elements = 2400
	Elemental Nodes = 0
	Elemental Rods  = 0
	Elemental Tria3 = 0
	Elemental Quad4 = 2400
Updating mesh element types based on properties input

Getting FEA design variables.......
	Number of design variables          - 4
	Design_Variable name - m0
	Design_Variable name - m1
	Design_Variable name - x0
	Design_Variable name - x1
	Design_Variable_Relation name - rho_madeupium
	Name madeupium not found in attribute map!!!!
	Design_Variable_Relation name - rho_unobtainium
	Name unobtainium not found in attribute map!!!!
	Design_Variable_Relation name - thick_box1
	Number of design variable relations - 3
	Done getting FEA design variables
Updating mesh element types based on properties input

Getting FEA design variables.......
	Number of design variables          - 4
	Design_Variable name - m0
	Design_Variable name - m1
	Design_Variable name - x0
	Design_Variable name - x1
	Design_Variable_Relation name - rho_madeupium
	Name madeupium not found in attribute map!!!!
	Design_Variable_Relation name - rho_unobtainium
	Name unobtainium not found in attribute map!!!!
	Design_Variable_Relation name - thick_box1
	Number of design variable relations - 3
	Done getting FEA design variables
===> x1
Updating mesh element types based on properties input

Getting FEA design variables.......
	Number of design variables          - 4
	Design_Variable name - m0
	Design_Variable name - m1
	Design_Variable name - x0
	Design_Variable name - x1
	Design_Variable_Relation name - rho_madeupium
	Name madeupium not found in attribute map!!!!
	Design_Variable_Relation name - rho_unobtainium
	Name unobtainium not found in attribute map!!!!
	Design_Variable_Relation name - thick_box1
	Number of design variable relations - 3
	Done getting FEA design variables
Updating mesh element types based on properties input

Getting FEA design variables.......
	Number of design variables          - 4
	Design_Variable name - m0
	Design_Variable name - m1
	Design_Variable name - x0
	Design_Variable name - x1
	Design_Variable_Relation name - rho_madeupium
	Name madeupium not found in attribute map!!!!
	Design_Variable_Relation name - rho_unobtainium
	Name unobtainium not found in attribute map!!!!
	Design_Variable_Relation name - thick_box1
	Number of design variable relations - 3
	Done getting FEA design variables
===> m0
Updating mesh element types based on properties input

Getting FEA design variables.......
	Number of design variables          - 4
	Design_Variable name - m0
	Design_Variable name - m1
	Design_Variable name - x0
	Design_Variable name - x1
	Design_Variable_Relation name - rho_madeupium
	Name madeupium not found in attribute map!!!!
	Design_Variable_Relation name - rho_unobtainium
	Name unobtainium not found in attribute map!!!!
	Design_Variable_Relation name - thick_box1
	Number of design variable relations - 3
	Done getting FEA design variables
Updating mesh element types based on properties input

Getting FEA design variables.......
	Number of design variables          - 4
	Design_Variable name - m0
	Design_Variable name - m1
	Design_Variable name - x0
	Design_Variable name - x1
	Design_Variable_Relation name - rho_madeupium
	Name madeupium not found in attribute map!!!!
	Design_Variable_Relation name - rho_unobtainium
	Name unobtainium not found in attribute map!!!!
	Design_Variable_Relation name - thick_box1
	Number of design variable relations - 3
	Done getting FEA design variables
===> m1
Updating mesh element types based on properties input

Getting FEA design variables.......
	Number of design variables          - 4
	Design_Variable name - m0
	Design_Variable name - m1
	Design_Variable name - x0
	Design_Variable name - x1
	Design_Variable_Relation name - rho_madeupium
	Name madeupium not found in attribute map!!!!
	Design_Variable_Relation name - rho_unobtainium
	Name unobtainium not found in attribute map!!!!
	Design_Variable_Relation name - thick_box1
	Number of design variable relations - 3
	Done getting FEA design variables
Updating mesh element types based on properties input

Getting FEA design variables.......
	Number of design variables          - 4
	Design_Variable name - m0
	Design_Variable name - m1
	Design_Variable name - x0
	Design_Variable name - x1
	Design_Variable_Relation name - rho_madeupium
	Name madeupium not found in attribute map!!!!
	Design_Variable_Relation name - rho_unobtainium
	Name unobtainium not found in attribute map!!!!
	Design_Variable_Relation name - thick_box1
	Number of design variable relations - 3
	Done getting FEA design variables
ok
test_box2 (test_masstran.TestMasstran.test_box2) ... 
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = box1, index = 1
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 0
Mapping Csys attributes ................
	Number of unique Csys attributes = 0

Getting FEA coordinate systems.......
	Number of coordinate systems - 0
	No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
	Number of unique capsConstraint attributes = 0
Mapping capsLoad attributes ................
	Number of unique capsLoad attributes = 0
Mapping capsBound attributes ................
	Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
	Number of unique capsConnect attributes = 0
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = box1, index = 1
Setting FEA Data
	Mesh for body = 0
	Number of nodal coordinates = 1692
	Number of elements = 3380
	Elemental Nodes = 0
	Elemental Rods  = 0
	Elemental Tria3 = 3380
	Elemental Quad4 = 0

Getting FEA properties.......
	Number of properties - 1
	Property name - box1
	Done getting FEA properties
Updating mesh element types based on properties input
Updating mesh element types based on properties input

Getting FEA design variables.......
	Number of design variables          - 7
	Design_Variable name - H
	Design_Variable name - L
	Design_Variable name - W
	Design_Variable name - m0
	Design_Variable name - m1
	Design_Variable name - x0
	Design_Variable name - x1
	Design_Variable_Relation name - rho_madeupium
	Name madeupium not found in attribute map!!!!
	Design_Variable_Relation name - rho_unobtainium
	Name unobtainium not found in attribute map!!!!
	Design_Variable_Relation name - thick_box1
	Number of design variable relations - 3
	Done getting FEA design variables



===> L

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

Getting FEA coordinate systems.......
	Number of coordinate systems - 0
	No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
	Number of unique capsConstraint attributes = 0
Mapping capsLoad attributes ................
	Number of unique capsLoad attributes = 0
Mapping capsBound attributes ................
	Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
	Number of unique capsConnect attributes = 0
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = box1, index = 1
Projecting tessellation 1 (of 1) on to new body
Setting FEA Data
	Mesh for body = 0
	Number of nodal coordinates = 1692
	Number of elements = 3380
	Elemental Nodes = 0
	Elemental Rods  = 0
	Elemental Tria3 = 3380
	Elemental Quad4 = 0
Updating mesh element types based on properties input

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

Getting FEA coordinate systems.......
	Number of coordinate systems - 0
	No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
	Number of unique capsConstraint attributes = 0
Mapping capsLoad attributes ................
	Number of unique capsLoad attributes = 0
Mapping capsBound attributes ................
	Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
	Number of unique capsConnect attributes = 0
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = box1, index = 1
Projecting tessellation 1 (of 1) on to new body
Setting FEA Data
	Mesh for body = 0
	Number of nodal coordinates = 1692
	Number of elements = 3380
	Elemental Nodes = 0
	Elemental Rods  = 0
	Elemental Tria3 = 3380
	Elemental Quad4 = 0
Updating mesh element types based on properties input
===> W

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

Getting FEA coordinate systems.......
	Number of coordinate systems - 0
	No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
	Number of unique capsConstraint attributes = 0
Mapping capsLoad attributes ................
	Number of unique capsLoad attributes = 0
Mapping capsBound attributes ................
	Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
	Number of unique capsConnect attributes = 0
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = box1, index = 1
Projecting tessellation 1 (of 1) on to new body
Setting FEA Data
	Mesh for body = 0
	Number of nodal coordinates = 1692
	Number of elements = 3380
	Elemental Nodes = 0
	Elemental Rods  = 0
	Elemental Tria3 = 3380
	Elemental Quad4 = 0
Updating mesh element types based on properties input

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

Getting FEA coordinate systems.......
	Number of coordinate systems - 0
	No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
	Number of unique capsConstraint attributes = 0
Mapping capsLoad attributes ................
	Number of unique capsLoad attributes = 0
Mapping capsBound attributes ................
	Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
	Number of unique capsConnect attributes = 0
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = box1, index = 1
Projecting tessellation 1 (of 1) on to new body
Setting FEA Data
	Mesh for body = 0
	Number of nodal coordinates = 1692
	Number of elements = 3380
	Elemental Nodes = 0
	Elemental Rods  = 0
	Elemental Tria3 = 3380
	Elemental Quad4 = 0
Updating mesh element types based on properties input
===> H

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

Getting FEA coordinate systems.......
	Number of coordinate systems - 0
	No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
	Number of unique capsConstraint attributes = 0
Mapping capsLoad attributes ................
	Number of unique capsLoad attributes = 0
Mapping capsBound attributes ................
	Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
	Number of unique capsConnect attributes = 0
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = box1, index = 1
Projecting tessellation 1 (of 1) on to new body
Setting FEA Data
	Mesh for body = 0
	Number of nodal coordinates = 1692
	Number of elements = 3380
	Elemental Nodes = 0
	Elemental Rods  = 0
	Elemental Tria3 = 3380
	Elemental Quad4 = 0
Updating mesh element types based on properties input

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

Getting FEA coordinate systems.......
	Number of coordinate systems - 0
	No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
	Number of unique capsConstraint attributes = 0
Mapping capsLoad attributes ................
	Number of unique capsLoad attributes = 0
Mapping capsBound attributes ................
	Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
	Number of unique capsConnect attributes = 0
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = box1, index = 1
Projecting tessellation 1 (of 1) on to new body
Setting FEA Data
	Mesh for body = 0
	Number of nodal coordinates = 1692
	Number of elements = 3380
	Elemental Nodes = 0
	Elemental Rods  = 0
	Elemental Tria3 = 3380
	Elemental Quad4 = 0
Updating mesh element types based on properties input
===> x0

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

Getting FEA coordinate systems.......
	Number of coordinate systems - 0
	No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
	Number of unique capsConstraint attributes = 0
Mapping capsLoad attributes ................
	Number of unique capsLoad attributes = 0
Mapping capsBound attributes ................
	Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
	Number of unique capsConnect attributes = 0
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = box1, index = 1
Projecting tessellation 1 (of 1) on to new body
Setting FEA Data
	Mesh for body = 0
	Number of nodal coordinates = 1692
	Number of elements = 3380
	Elemental Nodes = 0
	Elemental Rods  = 0
	Elemental Tria3 = 3380
	Elemental Quad4 = 0
Updating mesh element types based on properties input

Getting FEA design variables.......
	Number of design variables          - 4
	Design_Variable name - m0
	Design_Variable name - m1
	Design_Variable name - x0
	Design_Variable name - x1
	Design_Variable_Relation name - rho_madeupium
	Name madeupium not found in attribute map!!!!
	Design_Variable_Relation name - rho_unobtainium
	Name unobtainium not found in attribute map!!!!
	Design_Variable_Relation name - thick_box1
	Number of design variable relations - 3
	Done getting FEA design variables
Updating mesh element types based on properties input

Getting FEA design variables.......
	Number of design variables          - 4
	Design_Variable name - m0
	Design_Variable name - m1
	Design_Variable name - x0
	Design_Variable name - x1
	Design_Variable_Relation name - rho_madeupium
	Name madeupium not found in attribute map!!!!
	Design_Variable_Relation name - rho_unobtainium
	Name unobtainium not found in attribute map!!!!
	Design_Variable_Relation name - thick_box1
	Number of design variable relations - 3
	Done getting FEA design variables
===> x1
Updating mesh element types based on properties input

Getting FEA design variables.......
	Number of design variables          - 4
	Design_Variable name - m0
	Design_Variable name - m1
	Design_Variable name - x0
	Design_Variable name - x1
	Design_Variable_Relation name - rho_madeupium
	Name madeupium not found in attribute map!!!!
	Design_Variable_Relation name - rho_unobtainium
	Name unobtainium not found in attribute map!!!!
	Design_Variable_Relation name - thick_box1
	Number of design variable relations - 3
	Done getting FEA design variables
Updating mesh element types based on properties input

Getting FEA design variables.......
	Number of design variables          - 4
	Design_Variable name - m0
	Design_Variable name - m1
	Design_Variable name - x0
	Design_Variable name - x1
	Design_Variable_Relation name - rho_madeupium
	Name madeupium not found in attribute map!!!!
	Design_Variable_Relation name - rho_unobtainium
	Name unobtainium not found in attribute map!!!!
	Design_Variable_Relation name - thick_box1
	Number of design variable relations - 3
	Done getting FEA design variables
===> m0
Updating mesh element types based on properties input

Getting FEA design variables.......
	Number of design variables          - 4
	Design_Variable name - m0
	Design_Variable name - m1
	Design_Variable name - x0
	Design_Variable name - x1
	Design_Variable_Relation name - rho_madeupium
	Name madeupium not found in attribute map!!!!
	Design_Variable_Relation name - rho_unobtainium
	Name unobtainium not found in attribute map!!!!
	Design_Variable_Relation name - thick_box1
	Number of design variable relations - 3
	Done getting FEA design variables
Updating mesh element types based on properties input

Getting FEA design variables.......
	Number of design variables          - 4
	Design_Variable name - m0
	Design_Variable name - m1
	Design_Variable name - x0
	Design_Variable name - x1
	Design_Variable_Relation name - rho_madeupium
	Name madeupium not found in attribute map!!!!
	Design_Variable_Relation name - rho_unobtainium
	Name unobtainium not found in attribute map!!!!
	Design_Variable_Relation name - thick_box1
	Number of design variable relations - 3
	Done getting FEA design variables
===> m1
Updating mesh element types based on properties input

Getting FEA design variables.......
	Number of design variables          - 4
	Design_Variable name - m0
	Design_Variable name - m1
	Design_Variable name - x0
	Design_Variable name - x1
	Design_Variable_Relation name - rho_madeupium
	Name madeupium not found in attribute map!!!!
	Design_Variable_Relation name - rho_unobtainium
	Name unobtainium not found in attribute map!!!!
	Design_Variable_Relation name - thick_box1
	Number of design variable relations - 3
	Done getting FEA design variables
Updating mesh element types based on properties input

Getting FEA design variables.......
	Number of design variables          - 4
	Design_Variable name - m0
	Design_Variable name - m1
	Design_Variable name - x0
	Design_Variable name - x1
	Design_Variable_Relation name - rho_madeupium
	Name madeupium not found in attribute map!!!!
	Design_Variable_Relation name - rho_unobtainium
	Name unobtainium not found in attribute map!!!!
	Design_Variable_Relation name - thick_box1
	Number of design variable relations - 3
	Done getting FEA design variables
ok
test_box3 (test_masstran.TestMasstran.test_box3) ... 
Mapping Csys attributes ................
	Number of unique Csys attributes = 0

Getting FEA coordinate systems.......
	Number of coordinate systems - 0
	No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
	Number of unique capsConstraint attributes = 0
Mapping capsLoad attributes ................
	Number of unique capsLoad attributes = 0
Mapping capsBound attributes ................
	Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
	Number of unique capsConnect attributes = 0
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 2
	Name = box1, index = 1
	Name = box2, index = 2
Setting FEA Data
	Mesh for body = 0
	Number of nodal coordinates = 2402
	Number of elements = 2400
	Elemental Nodes = 0
	Elemental Rods  = 0
	Elemental Tria3 = 0
	Elemental Quad4 = 2400

Getting FEA properties.......
	Number of properties - 2
	Property name - box1
	Property name - box2
	Done getting FEA properties
Updating mesh element types based on properties input
Updating mesh element types based on properties input

Getting FEA design variables.......
	Number of design variables          - 7
	Design_Variable name - H
	Design_Variable name - L
	Design_Variable name - W
	Design_Variable name - m0
	Design_Variable name - m1
	Design_Variable name - x0
	Design_Variable name - x1
	Design_Variable_Relation name - rho_madeupium
	Name madeupium not found in attribute map!!!!
	Design_Variable_Relation name - rho_unobtainium
	Name unobtainium not found in attribute map!!!!
	Design_Variable_Relation name - thick_box1
	Design_Variable_Relation name - thick_box2
	Number of design variable relations - 4
	Done getting FEA design variables



===> L

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

Getting FEA coordinate systems.......
	Number of coordinate systems - 0
	No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
	Number of unique capsConstraint attributes = 0
Mapping capsLoad attributes ................
	Number of unique capsLoad attributes = 0
Mapping capsBound attributes ................
	Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
	Number of unique capsConnect attributes = 0
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 2
	Name = box1, index = 1
	Name = box2, index = 2
Setting FEA Data
	Mesh for body = 0
	Number of nodal coordinates = 2402
	Number of elements = 2400
	Elemental Nodes = 0
	Elemental Rods  = 0
	Elemental Tria3 = 0
	Elemental Quad4 = 2400
Updating mesh element types based on properties input

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

Getting FEA coordinate systems.......
	Number of coordinate systems - 0
	No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
	Number of unique capsConstraint attributes = 0
Mapping capsLoad attributes ................
	Number of unique capsLoad attributes = 0
Mapping capsBound attributes ................
	Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
	Number of unique capsConnect attributes = 0
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 2
	Name = box1, index = 1
	Name = box2, index = 2
Setting FEA Data
	Mesh for body = 0
	Number of nodal coordinates = 2402
	Number of elements = 2400
	Elemental Nodes = 0
	Elemental Rods  = 0
	Elemental Tria3 = 0
	Elemental Quad4 = 2400
Updating mesh element types based on properties input
===> W

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

Getting FEA coordinate systems.......
	Number of coordinate systems - 0
	No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
	Number of unique capsConstraint attributes = 0
Mapping capsLoad attributes ................
	Number of unique capsLoad attributes = 0
Mapping capsBound attributes ................
	Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
	Number of unique capsConnect attributes = 0
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 2
	Name = box1, index = 1
	Name = box2, index = 2
Setting FEA Data
	Mesh for body = 0
	Number of nodal coordinates = 2402
	Number of elements = 2400
	Elemental Nodes = 0
	Elemental Rods  = 0
	Elemental Tria3 = 0
	Elemental Quad4 = 2400
Updating mesh element types based on properties input

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

Getting FEA coordinate systems.......
	Number of coordinate systems - 0
	No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
	Number of unique capsConstraint attributes = 0
Mapping capsLoad attributes ................
	Number of unique capsLoad attributes = 0
Mapping capsBound attributes ................
	Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
	Number of unique capsConnect attributes = 0
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 2
	Name = box1, index = 1
	Name = box2, index = 2
Setting FEA Data
	Mesh for body = 0
	Number of nodal coordinates = 2402
	Number of elements = 2400
	Elemental Nodes = 0
	Elemental Rods  = 0
	Elemental Tria3 = 0
	Elemental Quad4 = 2400
Updating mesh element types based on properties input
===> H

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

Getting FEA coordinate systems.......
	Number of coordinate systems - 0
	No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
	Number of unique capsConstraint attributes = 0
Mapping capsLoad attributes ................
	Number of unique capsLoad attributes = 0
Mapping capsBound attributes ................
	Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
	Number of unique capsConnect attributes = 0
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 2
	Name = box1, index = 1
	Name = box2, index = 2
Setting FEA Data
	Mesh for body = 0
	Number of nodal coordinates = 2402
	Number of elements = 2400
	Elemental Nodes = 0
	Elemental Rods  = 0
	Elemental Tria3 = 0
	Elemental Quad4 = 2400
Updating mesh element types based on properties input

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

Getting FEA coordinate systems.......
	Number of coordinate systems - 0
	No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
	Number of unique capsConstraint attributes = 0
Mapping capsLoad attributes ................
	Number of unique capsLoad attributes = 0
Mapping capsBound attributes ................
	Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
	Number of unique capsConnect attributes = 0
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 2
	Name = box1, index = 1
	Name = box2, index = 2
Setting FEA Data
	Mesh for body = 0
	Number of nodal coordinates = 2402
	Number of elements = 2400
	Elemental Nodes = 0
	Elemental Rods  = 0
	Elemental Tria3 = 0
	Elemental Quad4 = 2400
Updating mesh element types based on properties input
===> x0

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

Getting FEA coordinate systems.......
	Number of coordinate systems - 0
	No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
	Number of unique capsConstraint attributes = 0
Mapping capsLoad attributes ................
	Number of unique capsLoad attributes = 0
Mapping capsBound attributes ................
	Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
	Number of unique capsConnect attributes = 0
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 2
	Name = box1, index = 1
	Name = box2, index = 2
Setting FEA Data
	Mesh for body = 0
	Number of nodal coordinates = 2402
	Number of elements = 2400
	Elemental Nodes = 0
	Elemental Rods  = 0
	Elemental Tria3 = 0
	Elemental Quad4 = 2400
Updating mesh element types based on properties input

Getting FEA design variables.......
	Number of design variables          - 4
	Design_Variable name - m0
	Design_Variable name - m1
	Design_Variable name - x0
	Design_Variable name - x1
	Design_Variable_Relation name - rho_madeupium
	Name madeupium not found in attribute map!!!!
	Design_Variable_Relation name - rho_unobtainium
	Name unobtainium not found in attribute map!!!!
	Design_Variable_Relation name - thick_box1
	Design_Variable_Relation name - thick_box2
	Number of design variable relations - 4
	Done getting FEA design variables
Updating mesh element types based on properties input

Getting FEA design variables.......
	Number of design variables          - 4
	Design_Variable name - m0
	Design_Variable name - m1
	Design_Variable name - x0
	Design_Variable name - x1
	Design_Variable_Relation name - rho_madeupium
	Name madeupium not found in attribute map!!!!
	Design_Variable_Relation name - rho_unobtainium
	Name unobtainium not found in attribute map!!!!
	Design_Variable_Relation name - thick_box1
	Design_Variable_Relation name - thick_box2
	Number of design variable relations - 4
	Done getting FEA design variables
===> x1
Updating mesh element types based on properties input

Getting FEA design variables.......
	Number of design variables          - 4
	Design_Variable name - m0
	Design_Variable name - m1
	Design_Variable name - x0
	Design_Variable name - x1
	Design_Variable_Relation name - rho_madeupium
	Name madeupium not found in attribute map!!!!
	Design_Variable_Relation name - rho_unobtainium
	Name unobtainium not found in attribute map!!!!
	Design_Variable_Relation name - thick_box1
	Design_Variable_Relation name - thick_box2
	Number of design variable relations - 4
	Done getting FEA design variables
Updating mesh element types based on properties input

Getting FEA design variables.......
	Number of design variables          - 4
	Design_Variable name - m0
	Design_Variable name - m1
	Design_Variable name - x0
	Design_Variable name - x1
	Design_Variable_Relation name - rho_madeupium
	Name madeupium not found in attribute map!!!!
	Design_Variable_Relation name - rho_unobtainium
	Name unobtainium not found in attribute map!!!!
	Design_Variable_Relation name - thick_box1
	Design_Variable_Relation name - thick_box2
	Number of design variable relations - 4
	Done getting FEA design variables
===> m0
Updating mesh element types based on properties input

Getting FEA design variables.......
	Number of design variables          - 4
	Design_Variable name - m0
	Design_Variable name - m1
	Design_Variable name - x0
	Design_Variable name - x1
	Design_Variable_Relation name - rho_madeupium
	Name madeupium not found in attribute map!!!!
	Design_Variable_Relation name - rho_unobtainium
	Name unobtainium not found in attribute map!!!!
	Design_Variable_Relation name - thick_box1
	Design_Variable_Relation name - thick_box2
	Number of design variable relations - 4
	Done getting FEA design variables
Updating mesh element types based on properties input

Getting FEA design variables.......
	Number of design variables          - 4
	Design_Variable name - m0
	Design_Variable name - m1
	Design_Variable name - x0
	Design_Variable name - x1
	Design_Variable_Relation name - rho_madeupium
	Name madeupium not found in attribute map!!!!
	Design_Variable_Relation name - rho_unobtainium
	Name unobtainium not found in attribute map!!!!
	Design_Variable_Relation name - thick_box1
	Design_Variable_Relation name - thick_box2
	Number of design variable relations - 4
	Done getting FEA design variables
===> m1
Updating mesh element types based on properties input

Getting FEA design variables.......
	Number of design variables          - 4
	Design_Variable name - m0
	Design_Variable name - m1
	Design_Variable name - x0
	Design_Variable name - x1
	Design_Variable_Relation name - rho_madeupium
	Name madeupium not found in attribute map!!!!
	Design_Variable_Relation name - rho_unobtainium
	Name unobtainium not found in attribute map!!!!
	Design_Variable_Relation name - thick_box1
	Design_Variable_Relation name - thick_box2
	Number of design variable relations - 4
	Done getting FEA design variables
Updating mesh element types based on properties input

Getting FEA design variables.......
	Number of design variables          - 4
	Design_Variable name - m0
	Design_Variable name - m1
	Design_Variable name - x0
	Design_Variable name - x1
	Design_Variable_Relation name - rho_madeupium
	Name madeupium not found in attribute map!!!!
	Design_Variable_Relation name - rho_unobtainium
	Name unobtainium not found in attribute map!!!!
	Design_Variable_Relation name - thick_box1
	Design_Variable_Relation name - thick_box2
	Number of design variable relations - 4
	Done getting FEA design variables
ok
test_journal (test_masstran.TestMasstran.test_journal) ... 
Mapping Csys attributes ................
	Number of unique Csys attributes = 0

Getting FEA coordinate systems.......
	Number of coordinate systems - 0
	No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
	Number of unique capsConstraint attributes = 0
Mapping capsLoad attributes ................
	Number of unique capsLoad attributes = 0
Mapping capsBound attributes ................
	Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
	Number of unique capsConnect attributes = 0
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 2
	Name = box1, index = 1
	Name = point, index = 2
Setting FEA Data
	Mesh for body = 0
	Number of nodal coordinates = 2168
	Number of elements = 4332
	Elemental Nodes = 0
	Elemental Rods  = 0
	Elemental Tria3 = 4332
	Elemental Quad4 = 0
Setting FEA Data
	Mesh for body = 1
	Number of nodal coordinates = 4048
	Number of elements = 8092
	Elemental Nodes = 0
	Elemental Rods  = 0
	Elemental Tria3 = 8092
	Elemental Quad4 = 0
Setting FEA Data
	Mesh for body = 2
	Number of nodal coordinates = 1
	Number of elements = 1
	Elemental Nodes = 1
	Elemental Rods  = 0
	Elemental Tria3 = 0
	Elemental Quad4 = 0
Combining multiple FEA meshes!
	Combined Number of nodal coordinates = 6217
	Combined Number of elements = 12425
	Combined Elemental Nodes = 1
	Combined Elemental Rods  = 0
	Combined Elemental Tria3 = 12424
	Combined Elemental Quad4 = 0

Getting FEA materials.......
	Number of materials - 2
	Material name - madeupium
	Material name - unobtainium
	Done getting FEA materials

Getting FEA properties.......
	Number of properties - 2
	Property name - box1
	Property name - point
	Done getting FEA properties
Updating mesh element types based on properties input

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

Getting FEA coordinate systems.......
	Number of coordinate systems - 0
	No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
	Number of unique capsConstraint attributes = 0
Mapping capsLoad attributes ................
	Number of unique capsLoad attributes = 0
Mapping capsBound attributes ................
	Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
	Number of unique capsConnect attributes = 0
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 2
	Name = box1, index = 1
	Name = point, index = 2
Setting FEA Data
	Mesh for body = 0
	Number of nodal coordinates = 2168
	Number of elements = 4332
	Elemental Nodes = 0
	Elemental Rods  = 0
	Elemental Tria3 = 4332
	Elemental Quad4 = 0
Setting FEA Data
	Mesh for body = 1
	Number of nodal coordinates = 3908
	Number of elements = 7812
	Elemental Nodes = 0
	Elemental Rods  = 0
	Elemental Tria3 = 7812
	Elemental Quad4 = 0
Setting FEA Data
	Mesh for body = 2
	Number of nodal coordinates = 1
	Number of elements = 1
	Elemental Nodes = 1
	Elemental Rods  = 0
	Elemental Tria3 = 0
	Elemental Quad4 = 0
Combining multiple FEA meshes!
	Combined Number of nodal coordinates = 6077
	Combined Number of elements = 12145
	Combined Elemental Nodes = 1
	Combined Elemental Rods  = 0
	Combined Elemental Tria3 = 12144
	Combined Elemental Quad4 = 0
Updating mesh element types based on properties input
 EGADS Info: 0 Objects, 0 Reference in Use (of 0) at Close!


 CAPS Info: Hit last success -- going live!

 CAPS Info: Hit last success -- going live!

 CAPS Info: Hit last success -- going live!

 CAPS Info: Hit last success -- going live!

 CAPS Info: Hit last success -- going live!

 CAPS Info: Hit last success -- going live!

 CAPS Info: Hit last success -- going live!

 CAPS Info: Hit last success -- going live!

 CAPS Info: Hit last success -- going live!

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

Getting FEA coordinate systems.......
	Number of coordinate systems - 0
	No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
	Number of unique capsConstraint attributes = 0
Mapping capsLoad attributes ................
	Number of unique capsLoad attributes = 0
Mapping capsBound attributes ................
	Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
	Number of unique capsConnect attributes = 0
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 2
	Name = box1, index = 1
	Name = point, index = 2
Setting FEA Data
	Mesh for body = 0
	Number of nodal coordinates = 2168
	Number of elements = 4332
	Elemental Nodes = 0
	Elemental Rods  = 0
	Elemental Tria3 = 4332
	Elemental Quad4 = 0
Setting FEA Data
	Mesh for body = 1
	Number of nodal coordinates = 4048
	Number of elements = 8092
	Elemental Nodes = 0
	Elemental Rods  = 0
	Elemental Tria3 = 8092
	Elemental Quad4 = 0
Setting FEA Data
	Mesh for body = 2
	Number of nodal coordinates = 1
	Number of elements = 1
	Elemental Nodes = 1
	Elemental Rods  = 0
	Elemental Tria3 = 0
	Elemental Quad4 = 0
Combining multiple FEA meshes!
	Combined Number of nodal coordinates = 6217
	Combined Number of elements = 12425
	Combined Elemental Nodes = 1
	Combined Elemental Rods  = 0
	Combined Elemental Tria3 = 12424
	Combined Elemental Quad4 = 0

Getting FEA materials.......
	Number of materials - 2
	Material name - madeupium
	Material name - unobtainium
	Done getting FEA materials

Getting FEA properties.......
	Number of properties - 2
	Property name - box1
	Property name - point
	Done getting FEA properties
Updating mesh element types based on properties input

 CAPS Info: Hit last success -- going live!
Mapping Csys attributes ................
	Number of unique Csys attributes = 0

Getting FEA coordinate systems.......
	Number of coordinate systems - 0
	No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
	Number of unique capsConstraint attributes = 0
Mapping capsLoad attributes ................
	Number of unique capsLoad attributes = 0
Mapping capsBound attributes ................
	Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
	Number of unique capsConnect attributes = 0
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 2
	Name = box1, index = 1
	Name = point, index = 2
Setting FEA Data
	Mesh for body = 0
	Number of nodal coordinates = 2168
	Number of elements = 4332
	Elemental Nodes = 0
	Elemental Rods  = 0
	Elemental Tria3 = 4332
	Elemental Quad4 = 0
Setting FEA Data
	Mesh for body = 1
	Number of nodal coordinates = 4048
	Number of elements = 8092
	Elemental Nodes = 0
	Elemental Rods  = 0
	Elemental Tria3 = 8092
	Elemental Quad4 = 0
Setting FEA Data
	Mesh for body = 2
	Number of nodal coordinates = 1
	Number of elements = 1
	Elemental Nodes = 1
	Elemental Rods  = 0
	Elemental Tria3 = 0
	Elemental Quad4 = 0
Combining multiple FEA meshes!
	Combined Number of nodal coordinates = 6217
	Combined Number of elements = 12425
	Combined Elemental Nodes = 1
	Combined Elemental Rods  = 0
	Combined Elemental Tria3 = 12424
	Combined Elemental Quad4 = 0

Getting FEA materials.......
	Number of materials - 2
	Material name - madeupium
	Material name - unobtainium
	Done getting FEA materials

Getting FEA properties.......
	Number of properties - 2
	Property name - box1
	Property name - point
	Done getting FEA properties
Updating mesh element types based on properties input

 CAPS Info: Hit last success -- going live!

 CAPS Info: Hit last success -- going live!

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

Getting FEA coordinate systems.......
	Number of coordinate systems - 0
	No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
	Number of unique capsConstraint attributes = 0
Mapping capsLoad attributes ................
	Number of unique capsLoad attributes = 0
Mapping capsBound attributes ................
	Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
	Number of unique capsConnect attributes = 0
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 2
	Name = box1, index = 1
	Name = point, index = 2
Setting FEA Data
	Mesh for body = 0
	Number of nodal coordinates = 2168
	Number of elements = 4332
	Elemental Nodes = 0
	Elemental Rods  = 0
	Elemental Tria3 = 4332
	Elemental Quad4 = 0
Setting FEA Data
	Mesh for body = 1
	Number of nodal coordinates = 3908
	Number of elements = 7812
	Elemental Nodes = 0
	Elemental Rods  = 0
	Elemental Tria3 = 7812
	Elemental Quad4 = 0
Setting FEA Data
	Mesh for body = 2
	Number of nodal coordinates = 1
	Number of elements = 1
	Elemental Nodes = 1
	Elemental Rods  = 0
	Elemental Tria3 = 0
	Elemental Quad4 = 0
Combining multiple FEA meshes!
	Combined Number of nodal coordinates = 6077
	Combined Number of elements = 12145
	Combined Elemental Nodes = 1
	Combined Elemental Rods  = 0
	Combined Elemental Tria3 = 12144
	Combined Elemental Quad4 = 0

Getting FEA materials.......
	Number of materials - 2
	Material name - madeupium
	Material name - unobtainium
	Done getting FEA materials

Getting FEA properties.......
	Number of properties - 2
	Property name - box1
	Property name - point
	Done getting FEA properties
Updating mesh element types based on properties input

 CAPS Info: Hit last success -- going live!
Mapping Csys attributes ................
	Number of unique Csys attributes = 0

Getting FEA coordinate systems.......
	Number of coordinate systems - 0
	No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
	Number of unique capsConstraint attributes = 0
Mapping capsLoad attributes ................
	Number of unique capsLoad attributes = 0
Mapping capsBound attributes ................
	Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
	Number of unique capsConnect attributes = 0
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 2
	Name = box1, index = 1
	Name = point, index = 2
Setting FEA Data
	Mesh for body = 0
	Number of nodal coordinates = 2168
	Number of elements = 4332
	Elemental Nodes = 0
	Elemental Rods  = 0
	Elemental Tria3 = 4332
	Elemental Quad4 = 0
Setting FEA Data
	Mesh for body = 1
	Number of nodal coordinates = 3908
	Number of elements = 7812
	Elemental Nodes = 0
	Elemental Rods  = 0
	Elemental Tria3 = 7812
	Elemental Quad4 = 0
Setting FEA Data
	Mesh for body = 2
	Number of nodal coordinates = 1
	Number of elements = 1
	Elemental Nodes = 1
	Elemental Rods  = 0
	Elemental Tria3 = 0
	Elemental Quad4 = 0
Combining multiple FEA meshes!
	Combined Number of nodal coordinates = 6077
	Combined Number of elements = 12145
	Combined Elemental Nodes = 1
	Combined Elemental Rods  = 0
	Combined Elemental Tria3 = 12144
	Combined Elemental Quad4 = 0

Getting FEA materials.......
	Number of materials - 2
	Material name - madeupium
	Material name - unobtainium
	Done getting FEA materials

Getting FEA properties.......
	Number of properties - 2
	Property name - box1
	Property name - point
	Done getting FEA properties
Updating mesh element types based on properties input

ok
test_plate (test_masstran.TestMasstran.test_plate) ... 
Mapping Csys attributes ................
	Number of unique Csys attributes = 0

Getting FEA coordinate systems.......
	Number of coordinate systems - 0
	No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
	Number of unique capsConstraint attributes = 0
Mapping capsLoad attributes ................
	Number of unique capsLoad attributes = 0
Mapping capsBound attributes ................
	Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
	Number of unique capsConnect attributes = 0
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = box1, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
	Mesh for body = 0
	Number of nodal coordinates = 441
	Number of elements = 400
	Elemental Nodes = 0
	Elemental Rods  = 0
	Elemental Tria3 = 0
	Elemental Quad4 = 400

Getting FEA properties.......
	Number of properties - 1
	Property name - box1
	Done getting FEA properties
Updating mesh element types based on properties input
Updating mesh element types based on properties input

Getting FEA design variables.......
	Number of design variables          - 7
	Design_Variable name - H
	Design_Variable name - L
	Design_Variable name - W
	Design_Variable name - m0
	Design_Variable name - m1
	Design_Variable name - x0
	Design_Variable name - x1
	Design_Variable_Relation name - rho_madeupium
	Name madeupium not found in attribute map!!!!
	Design_Variable_Relation name - rho_unobtainium
	Name unobtainium not found in attribute map!!!!
	Design_Variable_Relation name - thick_box1
	Number of design variable relations - 3
	Done getting FEA design variables



===> L

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

Getting FEA coordinate systems.......
	Number of coordinate systems - 0
	No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
	Number of unique capsConstraint attributes = 0
Mapping capsLoad attributes ................
	Number of unique capsLoad attributes = 0
Mapping capsBound attributes ................
	Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
	Number of unique capsConnect attributes = 0
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = box1, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
	Mesh for body = 0
	Number of nodal coordinates = 441
	Number of elements = 400
	Elemental Nodes = 0
	Elemental Rods  = 0
	Elemental Tria3 = 0
	Elemental Quad4 = 400
Updating mesh element types based on properties input

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

Getting FEA coordinate systems.......
	Number of coordinate systems - 0
	No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
	Number of unique capsConstraint attributes = 0
Mapping capsLoad attributes ................
	Number of unique capsLoad attributes = 0
Mapping capsBound attributes ................
	Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
	Number of unique capsConnect attributes = 0
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = box1, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
	Mesh for body = 0
	Number of nodal coordinates = 441
	Number of elements = 400
	Elemental Nodes = 0
	Elemental Rods  = 0
	Elemental Tria3 = 0
	Elemental Quad4 = 400
Updating mesh element types based on properties input
===> W

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

Getting FEA coordinate systems.......
	Number of coordinate systems - 0
	No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
	Number of unique capsConstraint attributes = 0
Mapping capsLoad attributes ................
	Number of unique capsLoad attributes = 0
Mapping capsBound attributes ................
	Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
	Number of unique capsConnect attributes = 0
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = box1, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
	Mesh for body = 0
	Number of nodal coordinates = 441
	Number of elements = 400
	Elemental Nodes = 0
	Elemental Rods  = 0
	Elemental Tria3 = 0
	Elemental Quad4 = 400
Updating mesh element types based on properties input

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

Getting FEA coordinate systems.......
	Number of coordinate systems - 0
	No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
	Number of unique capsConstraint attributes = 0
Mapping capsLoad attributes ................
	Number of unique capsLoad attributes = 0
Mapping capsBound attributes ................
	Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
	Number of unique capsConnect attributes = 0
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = box1, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
	Mesh for body = 0
	Number of nodal coordinates = 441
	Number of elements = 400
	Elemental Nodes = 0
	Elemental Rods  = 0
	Elemental Tria3 = 0
	Elemental Quad4 = 400
Updating mesh element types based on properties input
===> H

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

Getting FEA coordinate systems.......
	Number of coordinate systems - 0
	No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
	Number of unique capsConstraint attributes = 0
Mapping capsLoad attributes ................
	Number of unique capsLoad attributes = 0
Mapping capsBound attributes ................
	Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
	Number of unique capsConnect attributes = 0
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = box1, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
	Mesh for body = 0
	Number of nodal coordinates = 441
	Number of elements = 400
	Elemental Nodes = 0
	Elemental Rods  = 0
	Elemental Tria3 = 0
	Elemental Quad4 = 400
Updating mesh element types based on properties input

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

Getting FEA coordinate systems.......
	Number of coordinate systems - 0
	No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
	Number of unique capsConstraint attributes = 0
Mapping capsLoad attributes ................
	Number of unique capsLoad attributes = 0
Mapping capsBound attributes ................
	Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
	Number of unique capsConnect attributes = 0
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = box1, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
	Mesh for body = 0
	Number of nodal coordinates = 441
	Number of elements = 400
	Elemental Nodes = 0
	Elemental Rods  = 0
	Elemental Tria3 = 0
	Elemental Quad4 = 400
Updating mesh element types based on properties input
===> x0

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

Getting FEA coordinate systems.......
	Number of coordinate systems - 0
	No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
	Number of unique capsConstraint attributes = 0
Mapping capsLoad attributes ................
	Number of unique capsLoad attributes = 0
Mapping capsBound attributes ................
	Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
	Number of unique capsConnect attributes = 0
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = box1, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
	Mesh for body = 0
	Number of nodal coordinates = 441
	Number of elements = 400
	Elemental Nodes = 0
	Elemental Rods  = 0
	Elemental Tria3 = 0
	Elemental Quad4 = 400
Updating mesh element types based on properties input

Getting FEA design variables.......
	Number of design variables          - 4
	Design_Variable name - m0
	Design_Variable name - m1
	Design_Variable name - x0
	Design_Variable name - x1
	Design_Variable_Relation name - rho_madeupium
	Name madeupium not found in attribute map!!!!
	Design_Variable_Relation name - rho_unobtainium
	Name unobtainium not found in attribute map!!!!
	Design_Variable_Relation name - thick_box1
	Number of design variable relations - 3
	Done getting FEA design variables
Updating mesh element types based on properties input

Getting FEA design variables.......
	Number of design variables          - 4
	Design_Variable name - m0
	Design_Variable name - m1
	Design_Variable name - x0
	Design_Variable name - x1
	Design_Variable_Relation name - rho_madeupium
	Name madeupium not found in attribute map!!!!
	Design_Variable_Relation name - rho_unobtainium
	Name unobtainium not found in attribute map!!!!
	Design_Variable_Relation name - thick_box1
	Number of design variable relations - 3
	Done getting FEA design variables
===> x1
Updating mesh element types based on properties input

Getting FEA design variables.......
	Number of design variables          - 4
	Design_Variable name - m0
	Design_Variable name - m1
	Design_Variable name - x0
	Design_Variable name - x1
	Design_Variable_Relation name - rho_madeupium
	Name madeupium not found in attribute map!!!!
	Design_Variable_Relation name - rho_unobtainium
	Name unobtainium not found in attribute map!!!!
	Design_Variable_Relation name - thick_box1
	Number of design variable relations - 3
	Done getting FEA design variables
Updating mesh element types based on properties input

Getting FEA design variables.......
	Number of design variables          - 4
	Design_Variable name - m0
	Design_Variable name - m1
	Design_Variable name - x0
	Design_Variable name - x1
	Design_Variable_Relation name - rho_madeupium
	Name madeupium not found in attribute map!!!!
	Design_Variable_Relation name - rho_unobtainium
	Name unobtainium not found in attribute map!!!!
	Design_Variable_Relation name - thick_box1
	Number of design variable relations - 3
	Done getting FEA design variables
===> m0
Updating mesh element types based on properties input

Getting FEA design variables.......
	Number of design variables          - 4
	Design_Variable name - m0
	Design_Variable name - m1
	Design_Variable name - x0
	Design_Variable name - x1
	Design_Variable_Relation name - rho_madeupium
	Name madeupium not found in attribute map!!!!
	Design_Variable_Relation name - rho_unobtainium
	Name unobtainium not found in attribute map!!!!
	Design_Variable_Relation name - thick_box1
	Number of design variable relations - 3
	Done getting FEA design variables
Updating mesh element types based on properties input

Getting FEA design variables.......
	Number of design variables          - 4
	Design_Variable name - m0
	Design_Variable name - m1
	Design_Variable name - x0
	Design_Variable name - x1
	Design_Variable_Relation name - rho_madeupium
	Name madeupium not found in attribute map!!!!
	Design_Variable_Relation name - rho_unobtainium
	Name unobtainium not found in attribute map!!!!
	Design_Variable_Relation name - thick_box1
	Number of design variable relations - 3
	Done getting FEA design variables
===> m1
Updating mesh element types based on properties input

Getting FEA design variables.......
	Number of design variables          - 4
	Design_Variable name - m0
	Design_Variable name - m1
	Design_Variable name - x0
	Design_Variable name - x1
	Design_Variable_Relation name - rho_madeupium
	Name madeupium not found in attribute map!!!!
	Design_Variable_Relation name - rho_unobtainium
	Name unobtainium not found in attribute map!!!!
	Design_Variable_Relation name - thick_box1
	Number of design variable relations - 3
	Done getting FEA design variables
Updating mesh element types based on properties input

Getting FEA design variables.......
	Number of design variables          - 4
	Design_Variable name - m0
	Design_Variable name - m1
	Design_Variable name - x0
	Design_Variable name - x1
	Design_Variable_Relation name - rho_madeupium
	Name madeupium not found in attribute map!!!!
	Design_Variable_Relation name - rho_unobtainium
	Name unobtainium not found in attribute map!!!!
	Design_Variable_Relation name - thick_box1
	Number of design variable relations - 3
	Done getting FEA design variables
ok
test_plate_point (test_masstran.TestMasstran.test_plate_point) ... 
Mapping Csys attributes ................
	Number of unique Csys attributes = 0

Getting FEA coordinate systems.......
	Number of coordinate systems - 0
	No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
	Number of unique capsConstraint attributes = 0
Mapping capsLoad attributes ................
	Number of unique capsLoad attributes = 0
Mapping capsBound attributes ................
	Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
	Number of unique capsConnect attributes = 0
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 2
	Name = box1, index = 1
	Name = point, index = 2
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
	Mesh for body = 0
	Number of nodal coordinates = 441
	Number of elements = 400
	Elemental Nodes = 0
	Elemental Rods  = 0
	Elemental Tria3 = 0
	Elemental Quad4 = 400
Setting FEA Data
	Mesh for body = 1
	Number of nodal coordinates = 1
	Number of elements = 1
	Elemental Nodes = 1
	Elemental Rods  = 0
	Elemental Tria3 = 0
	Elemental Quad4 = 0
Combining multiple FEA meshes!
	Combined Number of nodal coordinates = 442
	Combined Number of elements = 401
	Combined Elemental Nodes = 1
	Combined Elemental Rods  = 0
	Combined Elemental Tria3 = 0
	Combined Elemental Quad4 = 400

Getting FEA properties.......
	Number of properties - 2
	Property name - box1
	Property name - point
	Done getting FEA properties
Updating mesh element types based on properties input
Updating mesh element types based on properties input

Getting FEA design variables.......
	Number of design variables          - 7
	Design_Variable name - H
	Design_Variable name - L
	Design_Variable name - W
	Design_Variable name - m0
	Design_Variable name - m1
	Design_Variable name - x0
	Design_Variable name - x1
	Design_Variable_Relation name - mass_point
	Design_Variable_Relation name - rho_madeupium
	Name madeupium not found in attribute map!!!!
	Design_Variable_Relation name - rho_unobtainium
	Name unobtainium not found in attribute map!!!!
	Design_Variable_Relation name - thick_box1
	Number of design variable relations - 4
	Done getting FEA design variables



===> L

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

Getting FEA coordinate systems.......
	Number of coordinate systems - 0
	No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
	Number of unique capsConstraint attributes = 0
Mapping capsLoad attributes ................
	Number of unique capsLoad attributes = 0
Mapping capsBound attributes ................
	Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
	Number of unique capsConnect attributes = 0
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 2
	Name = box1, index = 1
	Name = point, index = 2
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
	Mesh for body = 0
	Number of nodal coordinates = 441
	Number of elements = 400
	Elemental Nodes = 0
	Elemental Rods  = 0
	Elemental Tria3 = 0
	Elemental Quad4 = 400
Setting FEA Data
	Mesh for body = 1
	Number of nodal coordinates = 1
	Number of elements = 1
	Elemental Nodes = 1
	Elemental Rods  = 0
	Elemental Tria3 = 0
	Elemental Quad4 = 0
Combining multiple FEA meshes!
	Combined Number of nodal coordinates = 442
	Combined Number of elements = 401
	Combined Elemental Nodes = 1
	Combined Elemental Rods  = 0
	Combined Elemental Tria3 = 0
	Combined Elemental Quad4 = 400
Updating mesh element types based on properties input

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

Getting FEA coordinate systems.......
	Number of coordinate systems - 0
	No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
	Number of unique capsConstraint attributes = 0
Mapping capsLoad attributes ................
	Number of unique capsLoad attributes = 0
Mapping capsBound attributes ................
	Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
	Number of unique capsConnect attributes = 0
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 2
	Name = box1, index = 1
	Name = point, index = 2
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
	Mesh for body = 0
	Number of nodal coordinates = 441
	Number of elements = 400
	Elemental Nodes = 0
	Elemental Rods  = 0
	Elemental Tria3 = 0
	Elemental Quad4 = 400
Setting FEA Data
	Mesh for body = 1
	Number of nodal coordinates = 1
	Number of elements = 1
	Elemental Nodes = 1
	Elemental Rods  = 0
	Elemental Tria3 = 0
	Elemental Quad4 = 0
Combining multiple FEA meshes!
	Combined Number of nodal coordinates = 442
	Combined Number of elements = 401
	Combined Elemental Nodes = 1
	Combined Elemental Rods  = 0
	Combined Elemental Tria3 = 0
	Combined Elemental Quad4 = 400
Updating mesh element types based on properties input
===> W

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

Getting FEA coordinate systems.......
	Number of coordinate systems - 0
	No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
	Number of unique capsConstraint attributes = 0
Mapping capsLoad attributes ................
	Number of unique capsLoad attributes = 0
Mapping capsBound attributes ................
	Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
	Number of unique capsConnect attributes = 0
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 2
	Name = box1, index = 1
	Name = point, index = 2
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
	Mesh for body = 0
	Number of nodal coordinates = 441
	Number of elements = 400
	Elemental Nodes = 0
	Elemental Rods  = 0
	Elemental Tria3 = 0
	Elemental Quad4 = 400
Setting FEA Data
	Mesh for body = 1
	Number of nodal coordinates = 1
	Number of elements = 1
	Elemental Nodes = 1
	Elemental Rods  = 0
	Elemental Tria3 = 0
	Elemental Quad4 = 0
Combining multiple FEA meshes!
	Combined Number of nodal coordinates = 442
	Combined Number of elements = 401
	Combined Elemental Nodes = 1
	Combined Elemental Rods  = 0
	Combined Elemental Tria3 = 0
	Combined Elemental Quad4 = 400
Updating mesh element types based on properties input

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

Getting FEA coordinate systems.......
	Number of coordinate systems - 0
	No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
	Number of unique capsConstraint attributes = 0
Mapping capsLoad attributes ................
	Number of unique capsLoad attributes = 0
Mapping capsBound attributes ................
	Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
	Number of unique capsConnect attributes = 0
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 2
	Name = box1, index = 1
	Name = point, index = 2
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
	Mesh for body = 0
	Number of nodal coordinates = 441
	Number of elements = 400
	Elemental Nodes = 0
	Elemental Rods  = 0
	Elemental Tria3 = 0
	Elemental Quad4 = 400
Setting FEA Data
	Mesh for body = 1
	Number of nodal coordinates = 1
	Number of elements = 1
	Elemental Nodes = 1
	Elemental Rods  = 0
	Elemental Tria3 = 0
	Elemental Quad4 = 0
Combining multiple FEA meshes!
	Combined Number of nodal coordinates = 442
	Combined Number of elements = 401
	Combined Elemental Nodes = 1
	Combined Elemental Rods  = 0
	Combined Elemental Tria3 = 0
	Combined Elemental Quad4 = 400
Updating mesh element types based on properties input
===> H

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

Getting FEA coordinate systems.......
	Number of coordinate systems - 0
	No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
	Number of unique capsConstraint attributes = 0
Mapping capsLoad attributes ................
	Number of unique capsLoad attributes = 0
Mapping capsBound attributes ................
	Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
	Number of unique capsConnect attributes = 0
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 2
	Name = box1, index = 1
	Name = point, index = 2
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
	Mesh for body = 0
	Number of nodal coordinates = 441
	Number of elements = 400
	Elemental Nodes = 0
	Elemental Rods  = 0
	Elemental Tria3 = 0
	Elemental Quad4 = 400
Setting FEA Data
	Mesh for body = 1
	Number of nodal coordinates = 1
	Number of elements = 1
	Elemental Nodes = 1
	Elemental Rods  = 0
	Elemental Tria3 = 0
	Elemental Quad4 = 0
Combining multiple FEA meshes!
	Combined Number of nodal coordinates = 442
	Combined Number of elements = 401
	Combined Elemental Nodes = 1
	Combined Elemental Rods  = 0
	Combined Elemental Tria3 = 0
	Combined Elemental Quad4 = 400
Updating mesh element types based on properties input

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

Getting FEA coordinate systems.......
	Number of coordinate systems - 0
	No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
	Number of unique capsConstraint attributes = 0
Mapping capsLoad attributes ................
	Number of unique capsLoad attributes = 0
Mapping capsBound attributes ................
	Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
	Number of unique capsConnect attributes = 0
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 2
	Name = box1, index = 1
	Name = point, index = 2
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
	Mesh for body = 0
	Number of nodal coordinates = 441
	Number of elements = 400
	Elemental Nodes = 0
	Elemental Rods  = 0
	Elemental Tria3 = 0
	Elemental Quad4 = 400
Setting FEA Data
	Mesh for body = 1
	Number of nodal coordinates = 1
	Number of elements = 1
	Elemental Nodes = 1
	Elemental Rods  = 0
	Elemental Tria3 = 0
	Elemental Quad4 = 0
Combining multiple FEA meshes!
	Combined Number of nodal coordinates = 442
	Combined Number of elements = 401
	Combined Elemental Nodes = 1
	Combined Elemental Rods  = 0
	Combined Elemental Tria3 = 0
	Combined Elemental Quad4 = 400
Updating mesh element types based on properties input
===> x0

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

Getting FEA coordinate systems.......
	Number of coordinate systems - 0
	No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
	Number of unique capsConstraint attributes = 0
Mapping capsLoad attributes ................
	Number of unique capsLoad attributes = 0
Mapping capsBound attributes ................
	Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
	Number of unique capsConnect attributes = 0
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 2
	Name = box1, index = 1
	Name = point, index = 2
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
	Mesh for body = 0
	Number of nodal coordinates = 441
	Number of elements = 400
	Elemental Nodes = 0
	Elemental Rods  = 0
	Elemental Tria3 = 0
	Elemental Quad4 = 400
Setting FEA Data
	Mesh for body = 1
	Number of nodal coordinates = 1
	Number of elements = 1
	Elemental Nodes = 1
	Elemental Rods  = 0
	Elemental Tria3 = 0
	Elemental Quad4 = 0
Combining multiple FEA meshes!
	Combined Number of nodal coordinates = 442
	Combined Number of elements = 401
	Combined Elemental Nodes = 1
	Combined Elemental Rods  = 0
	Combined Elemental Tria3 = 0
	Combined Elemental Quad4 = 400
Updating mesh element types based on properties input

Getting FEA design variables.......
	Number of design variables          - 4
	Design_Variable name - m0
	Design_Variable name - m1
	Design_Variable name - x0
	Design_Variable name - x1
	Design_Variable_Relation name - mass_point
	Design_Variable_Relation name - rho_madeupium
	Name madeupium not found in attribute map!!!!
	Design_Variable_Relation name - rho_unobtainium
	Name unobtainium not found in attribute map!!!!
	Design_Variable_Relation name - thick_box1
	Number of design variable relations - 4
	Done getting FEA design variables
Updating mesh element types based on properties input

Getting FEA design variables.......
	Number of design variables          - 4
	Design_Variable name - m0
	Design_Variable name - m1
	Design_Variable name - x0
	Design_Variable name - x1
	Design_Variable_Relation name - mass_point
	Design_Variable_Relation name - rho_madeupium
	Name madeupium not found in attribute map!!!!
	Design_Variable_Relation name - rho_unobtainium
	Name unobtainium not found in attribute map!!!!
	Design_Variable_Relation name - thick_box1
	Number of design variable relations - 4
	Done getting FEA design variables
===> x1
Updating mesh element types based on properties input

Getting FEA design variables.......
	Number of design variables          - 4
	Design_Variable name - m0
	Design_Variable name - m1
	Design_Variable name - x0
	Design_Variable name - x1
	Design_Variable_Relation name - mass_point
	Design_Variable_Relation name - rho_madeupium
	Name madeupium not found in attribute map!!!!
	Design_Variable_Relation name - rho_unobtainium
	Name unobtainium not found in attribute map!!!!
	Design_Variable_Relation name - thick_box1
	Number of design variable relations - 4
	Done getting FEA design variables
Updating mesh element types based on properties input

Getting FEA design variables.......
	Number of design variables          - 4
	Design_Variable name - m0
	Design_Variable name - m1
	Design_Variable name - x0
	Design_Variable name - x1
	Design_Variable_Relation name - mass_point
	Design_Variable_Relation name - rho_madeupium
	Name madeupium not found in attribute map!!!!
	Design_Variable_Relation name - rho_unobtainium
	Name unobtainium not found in attribute map!!!!
	Design_Variable_Relation name - thick_box1
	Number of design variable relations - 4
	Done getting FEA design variables
===> m0
Updating mesh element types based on properties input

Getting FEA design variables.......
	Number of design variables          - 4
	Design_Variable name - m0
	Design_Variable name - m1
	Design_Variable name - x0
	Design_Variable name - x1
	Design_Variable_Relation name - mass_point
	Design_Variable_Relation name - rho_madeupium
	Name madeupium not found in attribute map!!!!
	Design_Variable_Relation name - rho_unobtainium
	Name unobtainium not found in attribute map!!!!
	Design_Variable_Relation name - thick_box1
	Number of design variable relations - 4
	Done getting FEA design variables
Updating mesh element types based on properties input

Getting FEA design variables.......
	Number of design variables          - 4
	Design_Variable name - m0
	Design_Variable name - m1
	Design_Variable name - x0
	Design_Variable name - x1
	Design_Variable_Relation name - mass_point
	Design_Variable_Relation name - rho_madeupium
	Name madeupium not found in attribute map!!!!
	Design_Variable_Relation name - rho_unobtainium
	Name unobtainium not found in attribute map!!!!
	Design_Variable_Relation name - thick_box1
	Number of design variable relations - 4
	Done getting FEA design variables
===> m1
Updating mesh element types based on properties input

Getting FEA design variables.......
	Number of design variables          - 4
	Design_Variable name - m0
	Design_Variable name - m1
	Design_Variable name - x0
	Design_Variable name - x1
	Design_Variable_Relation name - mass_point
	Design_Variable_Relation name - rho_madeupium
	Name madeupium not found in attribute map!!!!
	Design_Variable_Relation name - rho_unobtainium
	Name unobtainium not found in attribute map!!!!
	Design_Variable_Relation name - thick_box1
	Number of design variable relations - 4
	Done getting FEA design variables
Updating mesh element types based on properties input

Getting FEA design variables.......
	Number of design variables          - 4
	Design_Variable name - m0
	Design_Variable name - m1
	Design_Variable name - x0
	Design_Variable name - x1
	Design_Variable_Relation name - mass_point
	Design_Variable_Relation name - rho_madeupium
	Name madeupium not found in attribute map!!!!
	Design_Variable_Relation name - rho_unobtainium
	Name unobtainium not found in attribute map!!!!
	Design_Variable_Relation name - thick_box1
	Number of design variable relations - 4
	Done getting FEA design variables
ok
test_Cheby_Modes (test_mses.TestMSES_Kulfan.test_Cheby_Modes) ... 

Getting CFD design variables.......
	Number of design variables - 4
	Design Variable name - alowervar
	Design Variable name - auppervar
	Design Variable name - classvar
	Design Variable name - ztailvar
	Done getting CFD design variables


 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05


 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05


 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05


 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05


 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05


 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05


 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05


 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05


 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05


 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05


 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05


 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
ok
test_Cheby_Modes_Symmetric (test_mses.TestMSES_Kulfan.test_Cheby_Modes_Symmetric) ... 

Getting CFD design variables.......
	Number of design variables - 1
	Design Variable name - avar
	Done getting CFD design variables


 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05


 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05


 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05


 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
ok
test_allInputs (test_mses.TestMSES_Kulfan.test_allInputs) ... ok
test_execute (test_mses.TestMSES_Kulfan.test_execute) ... ok
test_sensitivity_AnalysisIn (test_mses.TestMSES_Kulfan.test_sensitivity_AnalysisIn) ... ok
test_Cheby_Modes_Symmetric (test_mses.TestMSES_NACA.test_Cheby_Modes_Symmetric) ... 

Getting CFD design variables.......
	Number of design variables - 1
	Design Variable name - thick
	Done getting CFD design variables

ok
test_geom_sensitivity_CL (test_mses.TestMSES_NACA.test_geom_sensitivity_CL) ... 
Getting CFD design variables.......
	Number of design variables - 2
	Design Variable name - camber
	Design Variable name - thick
	Done getting CFD design variables






ok
test_journal (test_mses.TestMSES_NACA.test_journal) ... 

Getting CFD design variables.......
	Number of design variables - 1
	Design Variable name - thick
	Done getting CFD design variables

 EGADS Info: 0 Objects, 0 Reference in Use (of 0) at Close!


 CAPS Info: Hit last success -- going live!

 CAPS Info: Hit last success -- going live!

 CAPS Info: Hit last success -- going live!

 CAPS Info: Hit last success -- going live!

 CAPS Info: Hit last success -- going live!

 CAPS Info: Hit last success -- going live!


Getting CFD design variables.......
	Number of design variables - 1
	Design Variable name - thick
	Done getting CFD design variables


 CAPS Info: Hit last success -- going live!

Getting CFD design variables.......
	Number of design variables - 1
	Design Variable name - thick
	Done getting CFD design variables


 CAPS Info: Hit last success -- going live!

 CAPS Info: Hit last success -- going live!

Getting CFD design variables.......
	Number of design variables - 1
	Design Variable name - thick
	Done getting CFD design variables


 CAPS Info: Hit last success -- going live!

Getting CFD design variables.......
	Number of design variables - 1
	Design Variable name - thick
	Done getting CFD design variables


ok
test_MultiBody (test_pointwise.TestPointwise.test_MultiBody) ... skipped 'No pointwise executable'
test_SingleBody (test_pointwise.TestPointwise.test_SingleBody) ... skipped 'No pointwise executable'
test_all (test_pointwise.TestPointwise.test_all) ... skipped 'No pointwise executable'
test_box (test_pointwise.TestPointwise.test_box) ... skipped 'No pointwise executable'
test_bullet (test_pointwise.TestPointwise.test_bullet) ... skipped 'No pointwise executable'
test_cone (test_pointwise.TestPointwise.test_cone) ... skipped 'No pointwise executable'
test_cylinder (test_pointwise.TestPointwise.test_cylinder) ... skipped 'No pointwise executable'
test_executeError (test_pointwise.TestPointwise.test_executeError) ... skipped 'No pointwise executable'
test_reenter (test_pointwise.TestPointwise.test_reenter) ... skipped 'No pointwise executable'
test_sphere (test_pointwise.TestPointwise.test_sphere) ... skipped 'No pointwise executable'
 EGADS Info: 0 Objects, 0 Reference in Use (of 0) at Close!
test_Area_Mesh (test_refine.TestREFINE.test_Area_Mesh) ... 
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 5
	Name = 2DSlice, index = 1
	Name = TunnelWall, index = 2
	Name = OutFlow, index = 3
	Name = InFlow, index = 4
	Name = Airfoil, index = 5
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 4
	Name = TunnelWall, index = 1
	Name = OutFlow, index = 2
	Name = InFlow, index = 3
	Name = Airfoil, index = 4
Getting 2D mesh for body 1 (of 1)
 
AFLR2    : ---------------------------------------
AFLR2    : AFLR2 LIBRARY
AFLR2    : ADVANCING-FRONT/LOCAL-RECONNECTION
AFLR2    : TRIA/QUAD GRID GENERATOR
AFLR2    : Version Number 9.17.15
AFLR2    : Version Date   04/23/24 @ 12:51AM
AFLR2    : Compile OS     Darwin 23.4.0 arm64
AFLR2    : Compile Date   04/23/24 @ 12:51AM
AFLR2    : Copyright 1994-2021, D.L. Marcum
AFLR2    : ---------------------------------------
 
AFLR2 IC : INPUT DATA CHECK
 
AFLR2 IC : Nodes, Faces      =        54         0
 
AFLR2    : CPU Time          =     0.000   seconds
 
AFLR2 EG : EDGE GRID RE-GENERATION
 
AFLR2 EG : Nodes, Edges      =        54        54
 
AFLR2    : CPU Time          =     0.000   seconds
 
AFLR2 IG : INITIAL GRID GENERATION
 
AFLR2 IG : Nodes, Faces      =         0         2
AFLR2 IG : Nodes, Faces      =        12        26
AFLR2 IG : Nodes, Faces      =        24        50
AFLR2 IG : Nodes, Faces      =        36        74
AFLR2 IG : Nodes, Faces      =        48        98
AFLR2 IG : Nodes, Faces      =        52       106
AFLR2 IG : Nodes, Faces      =        53       108
AFLR2 IG : Nodes, Faces      =        54       110
AFLR2 IG : Nodes, Faces      =        58       110
AFLR2 IG : Nodes, Faces      =        54        54
 
AFLR2    : CPU Time          =     0.000   seconds
 
AFLR2 GG : FIELD GRID GENERATION
 
AFLR2 GG : Nodes, Faces      =        54        54
AFLR2 GG : Nodes, Faces      =       100       146
AFLR2 GG : Nodes, Faces      =       122       190
AFLR2 GG : Nodes, Faces      =       138       222
AFLR2 GG : Nodes, Faces      =       153       252
AFLR2 GG : Nodes, Faces      =       168       282
AFLR2 GG : Nodes, Faces      =       180       306
AFLR2 GG : Nodes, Faces      =       192       330
AFLR2 GG : Nodes, Faces      =       201       348
AFLR2 GG : Nodes, Faces      =       210       366
AFLR2 GG : Nodes, Faces      =       216       378
AFLR2 GG : Nodes, Faces      =       221       388
AFLR2 GG : Nodes, Faces      =       224       394
AFLR2 GG : Nodes, Faces      =       225       396
 
AFLR2    : CPU Time          =     0.000   seconds
 
AFLR2 QI : QUALITY IMPROVEMENT
 
AFLR2 QI : Nodes, Faces      =       225       396
 
AFLR2    : CPU Time          =     0.000   seconds
 
AFLR2    : DONE

Writing AFLR3 file ....
Finished writing AFLR3 file

Number of nodes = 225
Number of elements = 450
Number of tris = 396
Number of quad = 0

Writing Binary VTK file ....
Finished writing Binary VTK file


Writing vtk file ....

Writing vtk general file ....
Finished writing vtk file


Writing FAST file ....
Finished writing FAST file


Writing SU2 file ....
Finished writing SU2 file


Writing exodus file ....
	Block: 'Block1_tri', blk_id 1, num_entries 396
	Sideset: 'Airfoil', set_id 1, num_entries 18
	Sideset: 'InFlow', set_id 2, num_entries 9
	Sideset: 'OutFlow', set_id 3, num_entries 9
	Sideset: 'TunnelWall', set_id 4, num_entries 18
Finished writing Exodus file


Writing Tecplot file ....
Finished writing Tecplot file


Writing ugrid file ....
Finished writing ugrid file


Writing Binary VTK file ....
Finished writing Binary VTK file


Writing vtk file ....

Writing vtk general file ....
Finished writing vtk file


Writing FAST file ....
Finished writing FAST file


Writing SU2 file ....
Finished writing SU2 file


Writing exodus file ....
	Block: 'Block1_tri', blk_id 1, num_entries 719
	Sideset: 'Airfoil', set_id 1, num_entries 17
	Sideset: 'InFlow', set_id 2, num_entries 4
	Sideset: 'OutFlow', set_id 3, num_entries 18
	Sideset: 'TunnelWall', set_id 4, num_entries 22
Finished writing Exodus file


Writing Tecplot file ....
Finished writing Tecplot file


Writing ugrid file ....
Finished writing ugrid file


Writing Binary VTK file ....
Finished writing Binary VTK file


Writing vtk file ....

Writing vtk general file ....
Finished writing vtk file


Writing FAST file ....
Finished writing FAST file


Writing SU2 file ....
Finished writing SU2 file


Writing exodus file ....
	Block: 'Block1_tri', blk_id 1, num_entries 1200
	Sideset: 'Airfoil', set_id 1, num_entries 20
	Sideset: 'InFlow', set_id 2, num_entries 4
	Sideset: 'OutFlow', set_id 3, num_entries 36
	Sideset: 'TunnelWall', set_id 4, num_entries 40
Finished writing Exodus file


Writing Tecplot file ....
Finished writing Tecplot file


Writing ugrid file ....
Finished writing ugrid file

ok
test_all (test_refine.TestREFINE.test_all) ... 
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 4
	Name = farfield, index = 1
	Name = box, index = 2
	Name = sphere, index = 3
	Name = boxhole, index = 4
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 1
	Name = box, index = 1
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 1
	Name = box, index = 1
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 4
	Name = farfield, index = 1
	Name = box, index = 2
	Name = sphere, index = 3
	Name = boxhole, index = 4
Getting volume mesh
 
AFLR2    : ---------------------------------------
AFLR2    : AFLR2 LIBRARY
AFLR2    : ADVANCING-FRONT/LOCAL-RECONNECTION
AFLR2    : TRIA/QUAD GRID GENERATOR
AFLR2    : Version Number 9.17.15
AFLR2    : Version Date   04/23/24 @ 12:51AM
AFLR2    : Compile OS     Darwin 23.4.0 arm64
AFLR2    : Compile Date   04/23/24 @ 12:51AM
AFLR2    : Copyright 1994-2021, D.L. Marcum
AFLR2    : ---------------------------------------
 
AFLR4    : ---------------------------------------
AFLR4    : AFLR4 LIBRARY
AFLR4    : ADVANCING-FRONT/LOCAL-RECONNECTION
AFLR4    : TRIA/QUAD SURFACE GRID GENERATOR
AFLR4    : Version Number 11.5.14
AFLR4    : Version Date   04/18/24 @ 12:45PM
AFLR4    : Compile OS     Darwin 23.4.0 arm64
AFLR4    : Compile Date   04/18/24 @ 03:04PM
AFLR4    : Copyright 1994-2021, D.L. Marcum
AFLR4    : ---------------------------------------

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

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------
Volume mesh:
	Number of nodes          = 1579
	Number of elements       = 8634
	Number of triangles      = 1240
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 7394
	Number of pyramids       = 0
	Number of prisms         = 0
	Number of hexahedrals    = 0
ok
test_box_volume (test_refine.TestREFINE.test_box_volume) ... 
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 2
	Name = farfield, index = 1
	Name = box, index = 2
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 1
	Name = box, index = 1
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 1
	Name = box, index = 1
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 2
	Name = farfield, index = 1
	Name = box, index = 2
Getting volume mesh

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

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------
Volume mesh:
	Number of nodes          = 2600
	Number of elements       = 13872
	Number of triangles      = 2758
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 11114
	Number of pyramids       = 0
	Number of prisms         = 0
	Number of hexahedrals    = 0
ok
test_boxhole (test_refine.TestREFINE.test_boxhole) ... 
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 2
	Name = farfield, index = 1
	Name = boxhole, index = 2
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 0
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 0
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 2
	Name = farfield, index = 1
	Name = boxhole, index = 2
Getting volume mesh

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

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------
Volume mesh:
	Number of nodes          = 1039
	Number of elements       = 5509
	Number of triangles      = 998
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 4511
	Number of pyramids       = 0
	Number of prisms         = 0
	Number of hexahedrals    = 0
ok
test_cfdSingleBody (test_refine.TestREFINE.test_cfdSingleBody) ... 
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 2
	Name = Farfield, index = 1
	Name = Wing1, index = 2
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 3
	Name = Farfield, index = 1
	Name = Wing1, index = 2
	Name = trailingEdge, index = 3
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 3
	Name = Farfield, index = 1
	Name = Wing1, index = 2
	Name = trailingEdge, index = 3
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 2
	Name = Farfield, index = 1
	Name = Wing1, index = 2
Getting volume mesh

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

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

Writing Binary VTK file ....
Finished writing Binary VTK file


Writing vtk file ....

Writing vtk general file ....
Finished writing vtk file


Writing FAST file ....
Finished writing FAST file


Writing SU2 file ....
Finished writing SU2 file


Writing exodus file ....
	Block: 'Block1_tet', blk_id 1, num_entries 86036
	Sideset: 'Farfield', set_id 1, num_entries 36
	Sideset: 'Wing1', set_id 2, num_entries 4596
Finished writing Exodus file


Writing Tecplot file ....
Finished writing Tecplot file


Writing ugrid file ....
Finished writing ugrid file

Getting CFD boundary conditions
	Boundary condition name - Farfield
	Boundary condition name - Wing1
	Done getting CFD boundary conditions
Writing boundary flags
 - bcProps.surfaceProp[0].surfaceType = 3
 - bcProps.surfaceProp[1].surfaceType = 1
Done boundary flags
Warning: The su2 cfg file will be overwritten!
Write SU2 configuration file for version "Harrier (8.0.1)"

Writing Binary VTK file ....
Finished writing Binary VTK file


Writing vtk file ....

Writing vtk general file ....
Finished writing vtk file


Writing FAST file ....
Finished writing FAST file


Writing SU2 file ....
Finished writing SU2 file


Writing exodus file ....
	Block: 'Block1_tet', blk_id 1, num_entries 98795
	Sideset: 'Farfield', set_id 1, num_entries 144
	Sideset: 'Wing1', set_id 2, num_entries 4086
Finished writing Exodus file


Writing Tecplot file ....
Finished writing Tecplot file


Writing ugrid file ....
Finished writing ugrid file

Getting CFD boundary conditions
	Boundary condition name - Farfield
	Boundary condition name - Wing1
	Done getting CFD boundary conditions
Writing boundary flags
 - bcProps.surfaceProp[0].surfaceType = 3
 - bcProps.surfaceProp[1].surfaceType = 1
Done boundary flags
Warning: The su2 cfg file will be overwritten!
Write SU2 configuration file for version "Harrier (8.0.1)"

Writing Binary VTK file ....
Finished writing Binary VTK file


Writing vtk file ....

Writing vtk general file ....
Finished writing vtk file


Writing FAST file ....
Finished writing FAST file


Writing SU2 file ....
Finished writing SU2 file


Writing exodus file ....
	Block: 'Block1_tet', blk_id 1, num_entries 163296
	Sideset: 'Farfield', set_id 1, num_entries 576
	Sideset: 'Wing1', set_id 2, num_entries 5666
Finished writing Exodus file


Writing Tecplot file ....
Finished writing Tecplot file


Writing ugrid file ....
Finished writing ugrid file

Getting CFD boundary conditions
	Boundary condition name - Farfield
	Boundary condition name - Wing1
	Done getting CFD boundary conditions
Writing boundary flags
 - bcProps.surfaceProp[0].surfaceType = 3
 - bcProps.surfaceProp[1].surfaceType = 1
Done boundary flags
Warning: The su2 cfg file will be overwritten!
Write SU2 configuration file for version "Harrier (8.0.1)"
ok
test_fun3d (test_refine.TestREFINE.test_fun3d) ... 
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 4
	Name = farfield, index = 1
	Name = box, index = 2
	Name = sphere, index = 3
	Name = boxhole, index = 4
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 1
	Name = box, index = 1
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 1
	Name = box, index = 1
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 4
	Name = farfield, index = 1
	Name = box, index = 2
	Name = sphere, index = 3
	Name = boxhole, index = 4
Getting volume mesh

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

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------
Volume mesh:
	Number of nodes          = 1579
	Number of elements       = 8634
	Number of triangles      = 1240
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 7394
	Number of pyramids       = 0
	Number of prisms         = 0
	Number of hexahedrals    = 0
ok
test_inputs (test_refine.TestREFINE.test_inputs) ... ok
test_phase (test_refine.TestREFINE.test_phase) ... 
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 2
	Name = farfield, index = 1
	Name = box, index = 2
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 1
	Name = box, index = 1
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 1
	Name = box, index = 1
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 2
	Name = farfield, index = 1
	Name = box, index = 2
Getting volume mesh

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

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------
Volume mesh:
	Number of nodes          = 432
	Number of elements       = 2132
	Number of triangles      = 644
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 1488
	Number of pyramids       = 0
	Number of prisms         = 0
	Number of hexahedrals    = 0

Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 2
	Name = farfield, index = 1
	Name = box, index = 2
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 1
	Name = box, index = 1
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 1
	Name = box, index = 1
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 2
	Name = farfield, index = 1
	Name = box, index = 2
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 2
	Name = farfield, index = 1
	Name = box, index = 2
ok
test_sphere (test_refine.TestREFINE.test_sphere) ... 
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 2
	Name = farfield, index = 1
	Name = sphere, index = 2
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 0
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 0
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 2
	Name = farfield, index = 1
	Name = sphere, index = 2
Getting volume mesh

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

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------
Volume mesh:
	Number of nodes          = 935
	Number of elements       = 5010
	Number of triangles      = 758
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 4252
	Number of pyramids       = 0
	Number of prisms         = 0
	Number of hexahedrals    = 0
ok
test_inputs (test_su2.TestSU2.test_inputs) ... 
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 3
	Name = Wing1, index = 1
	Name = Wing2, index = 2
	Name = Farfield, index = 3
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 3
	Name = Wing1, index = 1
	Name = Wing2, index = 2
	Name = Farfield, index = 3
AFLR4    : Proximity BG Surface Grid Generation Skipped
AFLR4    : No Modifications Required
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 3
	Name = Wing1, index = 1
	Name = Wing2, index = 2
	Name = Farfield, index = 3
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 3
	Name = Wing1, index = 1
	Name = Wing2, index = 2
	Name = Farfield, index = 3
Getting volume mesh
 
UG PARAM : SETTING INPUT PARAMETERS FROM ARGUMENT VECTOR
 
UG PARAM : mrecm                       = 3         
UG PARAM : mrecqm                      = 3         
UG PARAM : mpfrmt                      = 0         
 
AFLR2    : ---------------------------------------
AFLR2    : AFLR2 LIBRARY
AFLR2    : ADVANCING-FRONT/LOCAL-RECONNECTION
AFLR2    : TRIA/QUAD GRID GENERATOR
AFLR2    : Version Number 9.17.15
AFLR2    : Version Date   04/23/24 @ 12:51AM
AFLR2    : Compile OS     Darwin 23.4.0 arm64
AFLR2    : Compile Date   04/23/24 @ 12:51AM
AFLR2    : Copyright 1994-2021, D.L. Marcum
AFLR2    : ---------------------------------------
 
AFLR4    : ---------------------------------------
AFLR4    : AFLR4 LIBRARY
AFLR4    : ADVANCING-FRONT/LOCAL-RECONNECTION
AFLR4    : TRIA/QUAD SURFACE GRID GENERATOR
AFLR4    : Version Number 11.5.14
AFLR4    : Version Date   04/18/24 @ 12:45PM
AFLR4    : Compile OS     Darwin 23.4.0 arm64
AFLR4    : Compile Date   04/18/24 @ 03:04PM
AFLR4    : Copyright 1994-2021, D.L. Marcum
AFLR4    : ---------------------------------------

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

EGADS    : EGADS CAD Geometry Setup

EGADS    : Model has 3 Active Bodies

EGADS    : Body 0 is a SolidBody
EGADS    : Body 0 has 1 Shells
EGADS    : Body 0 has 8 Faces
EGADS    : Body 0 has 15 Edges
EGADS    : Body 0 has 8 Loops
EGADS    : Body 0 has 9 Nodes
EGADS    : Body 1 is a SolidBody
EGADS    : Body 1 has 1 Shells
EGADS    : Body 1 has 8 Faces
EGADS    : Body 1 has 15 Edges
EGADS    : Body 1 has 8 Loops
EGADS    : Body 1 has 9 Nodes
EGADS    : Body 2 is a SolidBody
EGADS    : Body 2 has 1 Shells
EGADS    : Body 2 has 2 Faces
EGADS    : Body 2 has 6 Edges
EGADS    : Body 2 has 2 Loops
EGADS    : Body 2 has 2 Nodes

EGADS    : Check Grid BCs

EGADS    : Grid BCs are OK

EGADS    : Face Neighbor-Faces Information

EGADS    : QC  = Face Quad Combination Flag
EGADS    : IER = Face Isolated Edge Refinement Flag
EGADS    : ER  = Face Edge Refinement Factor
EGADS    :       Not applicable for Faces with a FarField Grid BC.
EGADS    : SF  = Face Scale Factor
EGADS    :       Not applicable for Faces with a FarField Grid BC.

EGADS    :   Face          Body    QC   IER       ER    Scale   Neighbor
EGADS    :     ID  Active    ID  Flag  Flag   Weight   Factor   Faces
EGADS    :      1     Yes     0     0     1        1        1   2 3 4 5
EGADS    :      2     Yes     0     0     1        1        1   1 3 4 6
EGADS    :      3     Yes     0     0     1        1        1   1 2 4 7
EGADS    :      4     Yes     0     0     1        1        1   1 2 3
EGADS    :      5     Yes     0     0     1        1        1   1 6 7 8
EGADS    :      6     Yes     0     0     1        1        1   2 5 7 8
EGADS    :      7     Yes     0     0     1        1        1   3 5 6 8
EGADS    :      8     Yes     0     0     1        1        1   5 6 7
EGADS    :      9     Yes     1     0     1        0       10   10 11 12 13
EGADS    :     10     Yes     1     0     1        0       10   9 11 12 14
EGADS    :     11     Yes     1     0     1        0       10   9 10 12 15
EGADS    :     12     Yes     1     0     1        0       10   9 10 11
EGADS    :     13     Yes     1     0     1        0       10   9 14 15 16
EGADS    :     14     Yes     1     0     1        0       10   10 13 15 16
EGADS    :     15     Yes     1     0     1        0       10   11 13 14 16
EGADS    :     16     Yes     1     0     1        0       10   13 14 15
EGADS    :     17     Yes     2     0     1       NA       NA   18
EGADS    :     18     Yes     2     0     1       NA       NA   17

EGADS    : Face Edges Information

EGADS    :   Face   Edges
EGADS    :      1   1 4 -3 -2
EGADS    :      2   3 7 -6 -5
EGADS    :      3   6 9 -1 -8
EGADS    :      4   -4 -9 -7
EGADS    :      5   -10 2 11 -12
EGADS    :      6   -11 5 13 -14
EGADS    :      7   -13 8 10 -15
EGADS    :      8   12 14 15
EGADS    :      9   16 19 -18 -17
EGADS    :     10   18 22 -21 -20
EGADS    :     11   21 24 -16 -23
EGADS    :     12   -19 -24 -22
EGADS    :     13   -25 17 26 -27
EGADS    :     14   -26 20 28 -29
EGADS    :     15   -28 23 25 -30
EGADS    :     16   27 29 30
EGADS    :     17   -31 -32 33 34
EGADS    :     18   -35 -34 36 32

EGADS    : Face Loops Information

EGADS    :   Face   Loops
EGADS    :      1   1
EGADS    :      2   2
EGADS    :      3   3
EGADS    :      4   4
EGADS    :      5   5
EGADS    :      6   6
EGADS    :      7   7
EGADS    :      8   8
EGADS    :      9   9
EGADS    :     10   10
EGADS    :     11   11
EGADS    :     12   12
EGADS    :     13   13
EGADS    :     14   14
EGADS    :     15   15
EGADS    :     16   16
EGADS    :     17   17
EGADS    :     18   18

EGADS    : Loop Edges Information

EGADS    :   Loop  Active   Edges
EGADS    :      1     Yes   1 4 -3 -2
EGADS    :      2     Yes   3 7 -6 -5
EGADS    :      3     Yes   6 9 -1 -8
EGADS    :      4     Yes   -4 -9 -7
EGADS    :      5     Yes   -10 2 11 -12
EGADS    :      6     Yes   -11 5 13 -14
EGADS    :      7     Yes   -13 8 10 -15
EGADS    :      8     Yes   12 14 15
EGADS    :      9     Yes   16 19 -18 -17
EGADS    :     10     Yes   18 22 -21 -20
EGADS    :     11     Yes   21 24 -16 -23
EGADS    :     12     Yes   -19 -24 -22
EGADS    :     13     Yes   -25 17 26 -27
EGADS    :     14     Yes   -26 20 28 -29
EGADS    :     15     Yes   -28 23 25 -30
EGADS    :     16     Yes   27 29 30
EGADS    :     17     Yes   -31 -32 33 34
EGADS    :     18     Yes   -35 -34 36 32

EGADS    : Edge Node, Scale Factor, and Neighbor-Faces Information

EGADS    : ESF = Edge Scale Factor
EGADS    :       Not applicable for DEGENERATE Edges or Edges with a FarField
EGADS    :       Grid BC Neighbor Face.

EGADS    :                                             Neighbor
EGADS    :   Edge  Body  Active Node1 Node2      ESF   Faces
EGADS    :      1     0     Yes     1     2        1   1 3
EGADS    :      2     0     Yes     1     3        1   1 5
EGADS    :      3     0     Yes     3     4        1   1 2
EGADS    :      4     0     Yes     2     4        1   1 4
EGADS    :      5     0     Yes     3     5        1   2 6
EGADS    :      6     0     Yes     5     6        1   2 3
EGADS    :      7     0     Yes     4     6        1   2 4
EGADS    :      8     0     Yes     5     1        1   3 7
EGADS    :      9     0     Yes     6     2        1   3 4
EGADS    :     10     0     Yes     1     7        1   5 7
EGADS    :     11     0     Yes     3     8        1   5 6
EGADS    :     12     0     Yes     7     8        1   5 8
EGADS    :     13     0     Yes     5     9        1   6 7
EGADS    :     14     0     Yes     8     9        1   6 8
EGADS    :     15     0     Yes     9     7        1   7 8
EGADS    :     16     1     Yes    10    11        1   9 11
EGADS    :     17     1     Yes    10    12        1   9 13
EGADS    :     18     1     Yes    12    13        1   9 10
EGADS    :     19     1     Yes    11    13        1   9 12
EGADS    :     20     1     Yes    12    14        1   10 14
EGADS    :     21     1     Yes    14    15        1   10 11
EGADS    :     22     1     Yes    13    15        1   10 12
EGADS    :     23     1     Yes    14    10        1   11 15
EGADS    :     24     1     Yes    15    11        1   11 12
EGADS    :     25     1     Yes    10    16        1   13 15
EGADS    :     26     1     Yes    12    17        1   13 14
EGADS    :     27     1     Yes    16    17        1   13 16
EGADS    :     28     1     Yes    14    18        1   14 15
EGADS    :     29     1     Yes    17    18        1   14 16
EGADS    :     30     1     Yes    18    16        1   15 16
EGADS    :     31     2   DEGEN    19    19        -   17
EGADS    :     32     2     Yes    20    19       NA   17 18
EGADS    :     33     2   DEGEN    20    20        -   17
EGADS    :     34     2     Yes    20    19       NA   17 18
EGADS    :     35     2   DEGEN    19    19        -   18
EGADS    :     36     2   DEGEN    20    20        -   18

EGADS    : Node Information

EGADS    :   Node  Active      Coordinates
EGADS    :      1     Yes       3.77246052                0    0.00459131419
EGADS    :      2     Yes       5.90487498       7.07106781                0
EGADS    :      3     Yes                0                0                0
EGADS    :      4     Yes        4.0824829       7.07106781      0.123425948
EGADS    :      5     Yes       3.77001182                0                0
EGADS    :      6     Yes       5.90282524       7.07106781                0
EGADS    :      7     Yes       5.90487498                0                0
EGADS    :      8     Yes        4.0824829                0      0.123425948
EGADS    :      9     Yes       5.90282524                0                0
EGADS    :     10     Yes       11.5089842                0    0.00183652568
EGADS    :     11     Yes         12.36195       2.82842712                0
EGADS    :     12     Yes               10                0                0
EGADS    :     13     Yes       11.6329932       2.82842712     0.0493703791
EGADS    :     14     Yes       11.5080047                0                0
EGADS    :     15     Yes       12.3611301       2.82842712                0
EGADS    :     16     Yes         12.36195                0                0
EGADS    :     17     Yes       11.6329932                0     0.0493703791
EGADS    :     18     Yes       12.3611301                0                0
EGADS    :     19     Yes                0                0               80
EGADS    :     20     Yes                0                0                0

EGADS    : Face and Edge Match Information

EGADS    : No Face Matches Found

AFLR4    : Surface Mesh Spacing Setup

AFLR4    : Max Bounding Box Length     = 160
AFLR4    : Min Bounding Box Length     = 160
AFLR4    : Max Ref Bounding Box Length = 14.1421
AFLR4    : Min Ref Bounding Box Length = 0.890888
AFLR4    : Reference Length            = 0.890888
AFLR4    : BL Thickness                = 0
AFLR4    : FarField Spacing            = 15.6122
AFLR4    : Abs Min Surf Spacing        = 0.00222722
AFLR4    : Min Surf Spacing            = 0.00445444
AFLR4    : Max Surf Spacing            = 0.0890888
AFLR4    : Global Scale Factor         = 1

AFLR4    : Geometry Definition Information

AFLR4    : Definition              Definition   Composite             Grid BC
AFLR4    :         ID                    Type          ID                Type
AFLR4    :          0     glue-only composite           -                   -
AFLR4    :          1            CAD geometry           0                 STD
AFLR4    :          2            CAD geometry           0                 STD
AFLR4    :          3            CAD geometry           0                 STD
AFLR4    :          4            CAD geometry           0                 STD
AFLR4    :          5            CAD geometry           0                 STD
AFLR4    :          6            CAD geometry           0                 STD
AFLR4    :          7            CAD geometry           0                 STD
AFLR4    :          8            CAD geometry           0                 STD
AFLR4    :          9            CAD geometry           0                 STD
AFLR4    :         10            CAD geometry           0                 STD
AFLR4    :         11            CAD geometry           0                 STD
AFLR4    :         12            CAD geometry           0                 STD
AFLR4    :         13            CAD geometry           0                 STD
AFLR4    :         14            CAD geometry           0                 STD
AFLR4    :         15            CAD geometry           0                 STD
AFLR4    :         16            CAD geometry           0                 STD
AFLR4    :         17            CAD geometry           0            FARFIELD
AFLR4    :         18            CAD geometry           0            FARFIELD

AFLR4    : Case has 2 Proximity Checking Components

AFLR4    : Component 1 includes Definitions 1 2 3 4 5 6 7 8
AFLR4    : Component 2 includes Definitions 9 10 11 12 13 14 15 16

AFLR4    : Define CAD surface definition 1
AFLR4    : Define CAD surface definition 2
AFLR4    : Define CAD surface definition 3
AFLR4    : Define CAD surface definition 4
AFLR4    : Define CAD surface definition 5
AFLR4    : Define CAD surface definition 6
AFLR4    : Define CAD surface definition 7
AFLR4    : Define CAD surface definition 8
AFLR4    : Define CAD surface definition 9
AFLR4    : Define CAD surface definition 10
AFLR4    : Define CAD surface definition 11
AFLR4    : Define CAD surface definition 12
AFLR4    : Define CAD surface definition 13
AFLR4    : Define CAD surface definition 14
AFLR4    : Define CAD surface definition 15
AFLR4    : Define CAD surface definition 16
AFLR4    : Define CAD surface definition 17
AFLR4    : Define CAD surface definition 18
 
AFLR43   : INPUT SURFACE MESH FROM TESS
 
AFLR43   : Quad Surface Faces=         0
AFLR43   : Tria Surface Faces=     12428
AFLR43   : Nodes             =      6220
 
 
UG PARAM : SETTING INPUT PARAMETERS FROM ARGUMENT VECTOR
 
UG PARAM : mrecm                       = 3         
UG PARAM : mrecqm                      = 3         
UG PARAM : mpfrmt                      = 0         
 
AFLR3    : ---------------------------------------
AFLR3    : AFLR3 LIBRARY
AFLR3    : ADVANCING-FRONT/LOCAL-RECONNECTION
AFLR3    : TETRAHEDRAL GRID GENERATOR
AFLR3    : Version Number 16.32.50
AFLR3    : Version Date   10/31/23 @ 06:31PM
AFLR3    : Compile OS     Darwin 23.3.0 arm64
AFLR3    : Compile Date   02/08/24 @ 04:22PM
AFLR3    : Copyright 1994-2021, D.L. Marcum
AFLR3    : ---------------------------------------
 
AFLR3 IC : INPUT SURFACE GRID CHECK
 
AFLR3 IC : Nodes, Elements   =      6220         0

UG3      : Boundary Conditions

UG3      :  B-Face ID            Boundary Condition
UG3      :          1                         Solid
UG3      :          2                         Solid
UG3      :          3                         Solid
UG3      :          4                         Solid
UG3      :          5                         Solid
UG3      :          6                         Solid
UG3      :          7                         Solid
UG3      :          8                         Solid
UG3      :          9                         Solid
UG3      :         10                         Solid
UG3      :         11                         Solid
UG3      :         12                         Solid
UG3      :         13                         Solid
UG3      :         14                         Solid
UG3      :         15                         Solid
UG3      :         16                         Solid
UG3      :         17                      FarField
UG3      :         18                      FarField
 
AFLR3    : CPU Time          =     0.014   seconds
 
AFLR3 IG : INITIAL VOLUME GRID GENERATION
 
AFLR3 IG : Nodes, Elements   =      6220         0
AFLR3 IG : Nodes, Elements   =         8        10
AFLR3 IG : Nodes, Elements   =      1246      7333
AFLR3 IG : Nodes, Elements   =      2492     16261
AFLR3 IG : Nodes, Elements   =      3738     25026
AFLR3 IG : Nodes, Elements   =      4984     34312
AFLR3 IG : Nodes, Elements   =      6227     43517
AFLR3 IG : Nodes, Elements   =      6227     43439
AFLR3 IG : Nodes, Elements   =      6227     43476
AFLR3 IG : Nodes, Elements   =      6227     43444
AFLR3 IG : Nodes, Elements   =      6220     26114
AFLR3 IG : Nodes, Elements   =      6220     26132
AFLR3 IG : Nodes, Elements   =      6220     21569
AFLR3 IG : Nodes, Elements   =      6220     19193
 
AFLR3    : CPU Time          =     0.132   seconds
 
AFLR3 GG : ISOTROPIC VOLUME GRID GENERATION
 
AFLR3 GG : Nodes, Elements   =      6220     19193
AFLR3 GG : Nodes, Elements   =      9101     28053
AFLR3 GG : Nodes, Elements   =      9101     39640
AFLR3 GG : Nodes, Elements   =      9101     36690
AFLR3 GG : Nodes, Elements   =      9101     35155
AFLR3 GG : Nodes, Elements   =     11687     43216
AFLR3 GG : Nodes, Elements   =     11687     54497
AFLR3 GG : Nodes, Elements   =     11687     51170
AFLR3 GG : Nodes, Elements   =     11687     50185
AFLR3 GG : Nodes, Elements   =     14519     58970
AFLR3 GG : Nodes, Elements   =     14519     71103
AFLR3 GG : Nodes, Elements   =     14519     67722
AFLR3 GG : Nodes, Elements   =     14519     66894
AFLR3 GG : Nodes, Elements   =     17597     76360
AFLR3 GG : Nodes, Elements   =     17597     89686
AFLR3 GG : Nodes, Elements   =     17597     86040
AFLR3 GG : Nodes, Elements   =     17597     85134
AFLR3 GG : Nodes, Elements   =     20802     94942
AFLR3 GG : Nodes, Elements   =     20802    108532
AFLR3 GG : Nodes, Elements   =     20802    104847
AFLR3 GG : Nodes, Elements   =     20802    104019
AFLR3 GG : Nodes, Elements   =     24174    114290
AFLR3 GG : Nodes, Elements   =     24174    128631
AFLR3 GG : Nodes, Elements   =     24174    124801
AFLR3 GG : Nodes, Elements   =     24174    123982
AFLR3 GG : Nodes, Elements   =     27742    134809
AFLR3 GG : Nodes, Elements   =     27742    150037
AFLR3 GG : Nodes, Elements   =     27742    145948
AFLR3 GG : Nodes, Elements   =     27742    145081
AFLR3 GG : Nodes, Elements   =     31383    156143
AFLR3 GG : Nodes, Elements   =     31383    171588
AFLR3 GG : Nodes, Elements   =     31383    167421
AFLR3 GG : Nodes, Elements   =     31383    166536
AFLR3 GG : Nodes, Elements   =     35115    177837
AFLR3 GG : Nodes, Elements   =     35115    193748
AFLR3 GG : Nodes, Elements   =     35115    189548
AFLR3 GG : Nodes, Elements   =     35115    188723
AFLR3 GG : Nodes, Elements   =     38948    200319
AFLR3 GG : Nodes, Elements   =     38948    216342
AFLR3 GG : Nodes, Elements   =     38948    212298
AFLR3 GG : Nodes, Elements   =     38948    211481
AFLR3 GG : Nodes, Elements   =     42740    222940
AFLR3 GG : Nodes, Elements   =     42740    239184
AFLR3 GG : Nodes, Elements   =     42740    234883
AFLR3 GG : Nodes, Elements   =     42740    234060
AFLR3 GG : Nodes, Elements   =     46416    245151
AFLR3 GG : Nodes, Elements   =     46416    260680
AFLR3 GG : Nodes, Elements   =     46416    256642
AFLR3 GG : Nodes, Elements   =     46416    255866
AFLR3 GG : Nodes, Elements   =     50035    266777
AFLR3 GG : Nodes, Elements   =     50035    281993
AFLR3 GG : Nodes, Elements   =     50035    278055
AFLR3 GG : Nodes, Elements   =     50035    277383
AFLR3 GG : Nodes, Elements   =     53591    288088
AFLR3 GG : Nodes, Elements   =     53591    303095
AFLR3 GG : Nodes, Elements   =     53591    299307
AFLR3 GG : Nodes, Elements   =     53591    298569
AFLR3 GG : Nodes, Elements   =     57005    308827
AFLR3 GG : Nodes, Elements   =     57005    323244
AFLR3 GG : Nodes, Elements   =     57005    319601
AFLR3 GG : Nodes, Elements   =     57005    318957
AFLR3 GG : Nodes, Elements   =     60293    328832
AFLR3 GG : Nodes, Elements   =     60293    342689
AFLR3 GG : Nodes, Elements   =     60293    339197
AFLR3 GG : Nodes, Elements   =     60293    338647
AFLR3 GG : Nodes, Elements   =     63359    347851
AFLR3 GG : Nodes, Elements   =     63359    360783
AFLR3 GG : Nodes, Elements   =     63359    357437
AFLR3 GG : Nodes, Elements   =     63359    356932
AFLR3 GG : Nodes, Elements   =     66259    365641
AFLR3 GG : Nodes, Elements   =     66259    377775
AFLR3 GG : Nodes, Elements   =     66259    374741
AFLR3 GG : Nodes, Elements   =     66259    374315
AFLR3 GG : Nodes, Elements   =     68879    382177
AFLR3 GG : Nodes, Elements   =     68879    393099
AFLR3 GG : Nodes, Elements   =     68879    390371
AFLR3 GG : Nodes, Elements   =     68879    390020
AFLR3 GG : Nodes, Elements   =     71152    396844
AFLR3 GG : Nodes, Elements   =     71152    406357
AFLR3 GG : Nodes, Elements   =     71152    403836
AFLR3 GG : Nodes, Elements   =     71152    403561
AFLR3 GG : Nodes, Elements   =     73068    409315
AFLR3 GG : Nodes, Elements   =     73068    417362
AFLR3 GG : Nodes, Elements   =     73068    415318
AFLR3 GG : Nodes, Elements   =     73068    415069
AFLR3 GG : Nodes, Elements   =     74529    419454
AFLR3 GG : Nodes, Elements   =     74529    425587
AFLR3 GG : Nodes, Elements   =     74529    423928
AFLR3 GG : Nodes, Elements   =     74529    423776
AFLR3 GG : Nodes, Elements   =     75631    427084
AFLR3 GG : Nodes, Elements   =     75631    431714
AFLR3 GG : Nodes, Elements   =     75631    430512
AFLR3 GG : Nodes, Elements   =     75631    430423
AFLR3 GG : Nodes, Elements   =     76419    432787
AFLR3 GG : Nodes, Elements   =     76419    436211
AFLR3 GG : Nodes, Elements   =     76419    435175
AFLR3 GG : Nodes, Elements   =     76419    435106
AFLR3 GG : Nodes, Elements   =     76934    436651
AFLR3 GG : Nodes, Elements   =     76934    438851
AFLR3 GG : Nodes, Elements   =     76934    438238
AFLR3 GG : Nodes, Elements   =     76934    438198
AFLR3 GG : Nodes, Elements   =     77241    439119
AFLR3 GG : Nodes, Elements   =     77241    440474
AFLR3 GG : Nodes, Elements   =     77241    440052
AFLR3 GG : Nodes, Elements   =     77241    440022
AFLR3 GG : Nodes, Elements   =     77416    440547
AFLR3 GG : Nodes, Elements   =     77416    441274
AFLR3 GG : Nodes, Elements   =     77416    441066
AFLR3 GG : Nodes, Elements   =     77416    441056
AFLR3 GG : Nodes, Elements   =     77509    441335
AFLR3 GG : Nodes, Elements   =     77509    441739
AFLR3 GG : Nodes, Elements   =     77509    441625
AFLR3 GG : Nodes, Elements   =     77509    441612
AFLR3 GG : Nodes, Elements   =     77549    441732
AFLR3 GG : Nodes, Elements   =     77549    441904
AFLR3 GG : Nodes, Elements   =     77549    441849
AFLR3 GG : Nodes, Elements   =     77549    441848
AFLR3 GG : Nodes, Elements   =     77559    441878
AFLR3 GG : Nodes, Elements   =     77559    441913
AFLR3 GG : Nodes, Elements   =     77559    441902
AFLR3 GG : Nodes, Elements   =     77564    441917
AFLR3 GG : Nodes, Elements   =     77564    441932
AFLR3 GG : Nodes, Elements   =     77564    441928
AFLR3 GG : Nodes, Elements   =     77565    441931
AFLR3 GG : Nodes, Elements   =     77565    441938
AFLR3 GG : Nodes, Elements   =     77565    441933
AFLR3 GG : Nodes, Elements   =     77595    442023
AFLR3 GG : Nodes, Elements   =     77595    442128
AFLR3 GG : Nodes, Elements   =     77595    442098
AFLR3 GG : Nodes, Elements   =     77595    442094
AFLR3 GG : Nodes, Elements   =     77599    442106
AFLR3 GG : Nodes, Elements   =     77599    442119
AFLR3 GG : Nodes, Elements   =     77599    442116
AFLR3 GG : Nodes, Elements   =     77599    442115
AFLR3 GG : Nodes, Elements   =     77600    442118
AFLR3 GG : Nodes, Elements   =     77600    442125
AFLR3 GG : Nodes, Elements   =     77600    442121
 
AFLR3    : CPU Time          =     5.500   seconds
 
AFLR3 QI : QUALITY IMPROVEMENT
 
AFLR3 QI : Nodes, Elements   =     77600    442121
AFLR3 QI : Nodes, Elements   =     76105    433678
AFLR3 QI : Nodes, Elements   =     75842    432198
AFLR3 QI : Nodes, Elements   =     75829    432123
AFLR3 QI : Nodes, Elements   =     75827    432113
AFLR3 QI : Nodes, Elements   =     75826    432107
AFLR3 QI : Nodes, Elements   =     75826    436049
AFLR3 QI : Nodes, Elements   =     75826    431912
AFLR3 QI : Nodes, Elements   =     75826    431430
AFLR3 QI : Nodes, Elements   =     75826    431831
AFLR3 QI : Nodes, Elements   =     75826    431146
AFLR3 QI : Nodes, Elements   =     75826    430921
AFLR3 QI : Nodes, Elements   =     75826    431306
AFLR3 QI : Nodes, Elements   =     75826    430921
AFLR3 QI : Nodes, Elements   =     75826    430900
AFLR3 QI : Nodes, Elements   =     75826    431192
AFLR3 QI : Nodes, Elements   =     75826    430885
AFLR3 QI : Nodes, Elements   =     75826    430832
AFLR3 QI : Nodes, Elements   =     75826    431117
AFLR3 QI : Nodes, Elements   =     75826    430836
AFLR3 QI : Nodes, Elements   =     75826    430821
AFLR3 QI : Nodes, Elements   =     75831    430843
AFLR3 QI : Nodes, Elements   =     75831    431136
AFLR3 QI : Nodes, Elements   =     75831    430863
AFLR3 QI : Nodes, Elements   =     75831    430845
AFLR3 QI : Nodes, Elements   =     75831    431106
AFLR3 QI : Nodes, Elements   =     75831    430850
AFLR3 QI : Nodes, Elements   =     75831    430821
 
AFLR3    : CPU Time          =     1.711   seconds
 
AFLR3 QRG: QUALITY GRID RE-GENERATION
 
AFLR3 QRG: Nodes, Elements   =     75831    430821
AFLR3 QRG: Nodes, Elements   =     75839    430867
AFLR3 QRG: Nodes, Elements   =     75842    430887
AFLR3 QRG: Nodes, Elements   =     75841    430884
AFLR3 QRG: Nodes, Elements   =     75841    430883
AFLR3 QRG: Nodes, Elements   =     75848    430923
AFLR3 QRG: Nodes, Elements   =     75847    430916
 
AFLR3    : CPU Time          =     0.070   seconds
 
AFLR3    : DONE

UG3      : DIHEDRAL ANGLE CHECK

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

UG3      : VOL CHECK

UG3      : Total-Volume      =  2.12e+06

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

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

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

OVERALL  : CPU Time          =     7.813   seconds

UG3      : DIHEDRAL ANGLE CHECK

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

UG3      : VOL CHECK

UG3      : Total-Volume      =  2.12e+06

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

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

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

UG3      : CPU Time          =     0.000   seconds

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

EGADS    : CREATE EGADS TESS FROM AFLR3 DATA

EGADS    : CREATING TESSELLATION FOR BODY 0 EDGE 1
EGADS    : CREATING TESSELLATION FOR BODY 0 EDGE 2
EGADS    : CREATING TESSELLATION FOR BODY 0 EDGE 3
EGADS    : CREATING TESSELLATION FOR BODY 0 EDGE 4
EGADS    : CREATING TESSELLATION FOR BODY 0 EDGE 5
EGADS    : CREATING TESSELLATION FOR BODY 0 EDGE 6
EGADS    : CREATING TESSELLATION FOR BODY 0 EDGE 7
EGADS    : CREATING TESSELLATION FOR BODY 0 EDGE 8
EGADS    : CREATING TESSELLATION FOR BODY 0 EDGE 9
EGADS    : CREATING TESSELLATION FOR BODY 0 EDGE 10
EGADS    : CREATING TESSELLATION FOR BODY 0 EDGE 11
EGADS    : CREATING TESSELLATION FOR BODY 0 EDGE 12
EGADS    : CREATING TESSELLATION FOR BODY 0 EDGE 13
EGADS    : CREATING TESSELLATION FOR BODY 0 EDGE 14
EGADS    : CREATING TESSELLATION FOR BODY 0 EDGE 15

EGADS    : CREATING TESSELLATION FOR BODY 0 FACE 1
EGADS    : CREATING TESSELLATION FOR BODY 0 FACE 2
EGADS    : CREATING TESSELLATION FOR BODY 0 FACE 3
EGADS    : CREATING TESSELLATION FOR BODY 0 FACE 4
EGADS    : CREATING TESSELLATION FOR BODY 0 FACE 5
EGADS    : CREATING TESSELLATION FOR BODY 0 FACE 6
EGADS    : CREATING TESSELLATION FOR BODY 0 FACE 7
EGADS    : CREATING TESSELLATION FOR BODY 0 FACE 8

EGADS    : CREATING TESSELLATION FOR BODY 1 EDGE 16
EGADS    : CREATING TESSELLATION FOR BODY 1 EDGE 17
EGADS    : CREATING TESSELLATION FOR BODY 1 EDGE 18
EGADS    : CREATING TESSELLATION FOR BODY 1 EDGE 19
EGADS    : CREATING TESSELLATION FOR BODY 1 EDGE 20
EGADS    : CREATING TESSELLATION FOR BODY 1 EDGE 21
EGADS    : CREATING TESSELLATION FOR BODY 1 EDGE 22
EGADS    : CREATING TESSELLATION FOR BODY 1 EDGE 23
EGADS    : CREATING TESSELLATION FOR BODY 1 EDGE 24
EGADS    : CREATING TESSELLATION FOR BODY 1 EDGE 25
EGADS    : CREATING TESSELLATION FOR BODY 1 EDGE 26
EGADS    : CREATING TESSELLATION FOR BODY 1 EDGE 27
EGADS    : CREATING TESSELLATION FOR BODY 1 EDGE 28
EGADS    : CREATING TESSELLATION FOR BODY 1 EDGE 29
EGADS    : CREATING TESSELLATION FOR BODY 1 EDGE 30

EGADS    : CREATING TESSELLATION FOR BODY 1 FACE 9
EGADS    : CREATING TESSELLATION FOR BODY 1 FACE 10
EGADS    : CREATING TESSELLATION FOR BODY 1 FACE 11
EGADS    : CREATING TESSELLATION FOR BODY 1 FACE 12
EGADS    : CREATING TESSELLATION FOR BODY 1 FACE 13
EGADS    : CREATING TESSELLATION FOR BODY 1 FACE 14
EGADS    : CREATING TESSELLATION FOR BODY 1 FACE 15
EGADS    : CREATING TESSELLATION FOR BODY 1 FACE 16

EGADS    : CREATING TESSELLATION FOR BODY 2 EDGE 32
EGADS    : CREATING TESSELLATION FOR BODY 2 EDGE 34

EGADS    : CREATING TESSELLATION FOR BODY 2 FACE 17
EGADS    : CREATING TESSELLATION FOR BODY 2 FACE 18

EGADS    : EGADS TESS CREATED

EGADS    : CHECK TESS FACE NODE MAP

EGADS    : CHECKING NODE MAP FOR BODY 0 FACE 1
EGADS    : CHECKING NODE MAP FOR BODY 0 FACE 2
EGADS    : CHECKING NODE MAP FOR BODY 0 FACE 3
EGADS    : CHECKING NODE MAP FOR BODY 0 FACE 4
EGADS    : CHECKING NODE MAP FOR BODY 0 FACE 5
EGADS    : CHECKING NODE MAP FOR BODY 0 FACE 6
EGADS    : CHECKING NODE MAP FOR BODY 0 FACE 7
EGADS    : CHECKING NODE MAP FOR BODY 0 FACE 8
EGADS    : CHECKING NODE MAP FOR BODY 1 FACE 9
EGADS    : CHECKING NODE MAP FOR BODY 1 FACE 10
EGADS    : CHECKING NODE MAP FOR BODY 1 FACE 11
EGADS    : CHECKING NODE MAP FOR BODY 1 FACE 12
EGADS    : CHECKING NODE MAP FOR BODY 1 FACE 13
EGADS    : CHECKING NODE MAP FOR BODY 1 FACE 14
EGADS    : CHECKING NODE MAP FOR BODY 1 FACE 15
EGADS    : CHECKING NODE MAP FOR BODY 1 FACE 16
EGADS    : CHECKING NODE MAP FOR BODY 2 FACE 17
EGADS    : CHECKING NODE MAP FOR BODY 2 FACE 18
Volume mesh:
	Number of nodes          = 75847
	Number of elements       = 443344
	Number of triangles      = 12428
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 430916
	Number of pyramids       = 0
	Number of prisms         = 0
	Number of hexahedrals    = 0

Writing SU2 file ....
Finished writing SU2 file

Getting CFD boundary conditions
	Boundary condition name - Farfield
	Boundary condition name - Wing1
	Boundary condition name - Wing2
	Done getting CFD boundary conditions
Writing boundary flags
 - bcProps.surfaceProp[0].surfaceType = 3
 - bcProps.surfaceProp[1].surfaceType = 1
 - bcProps.surfaceProp[2].surfaceType = 1
Done boundary flags
Warning: The su2 cfg file will be overwritten!
Write SU2 configuration file for version "Cardinal"
Getting CFD boundary conditions
	Boundary condition name - Farfield
	Boundary condition name - Wing1
	Boundary condition name - Wing2
	Done getting CFD boundary conditions
Writing boundary flags
 - bcProps.surfaceProp[0].surfaceType = 3
 - bcProps.surfaceProp[1].surfaceType = 1
 - bcProps.surfaceProp[2].surfaceType = 1
Done boundary flags
Warning: The su2 cfg file will be overwritten!
Write SU2 configuration file for version "Raven"
Getting CFD boundary conditions
	Boundary condition name - Farfield
	Boundary condition name - Wing1
	Boundary condition name - Wing2
	Done getting CFD boundary conditions
Writing boundary flags
 - bcProps.surfaceProp[0].surfaceType = 3
 - bcProps.surfaceProp[1].surfaceType = 1
 - bcProps.surfaceProp[2].surfaceType = 1
Done boundary flags
Warning: The su2 cfg file will be overwritten!
Write SU2 configuration file for version "Falcon"
Getting CFD boundary conditions
	Boundary condition name - Farfield
	Boundary condition name - Wing1
	Boundary condition name - Wing2
	Done getting CFD boundary conditions
Writing boundary flags
 - bcProps.surfaceProp[0].surfaceType = 3
 - bcProps.surfaceProp[1].surfaceType = 1
 - bcProps.surfaceProp[2].surfaceType = 1
Done boundary flags
Warning: The su2 cfg file will be overwritten!
Write SU2 configuration file for version "BlackBird (7.5.1) "
ok
test_invalidBoundary (test_su2.TestSU2.test_invalidBoundary) ... Getting CFD boundary conditions
	Boundary condition name - Wing1
ok
test_invalidBoundaryName (test_su2.TestSU2.test_invalidBoundaryName) ... Getting CFD boundary conditions
	Boundary condition name - Farfield
	Boundary condition name - Wing1
	Boundary condition name - X
ok
test_journal (test_su2.TestSU2.test_journal) ... 
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 3
	Name = Wing1, index = 1
	Name = Wing2, index = 2
	Name = Farfield, index = 3
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 3
	Name = Wing1, index = 1
	Name = Wing2, index = 2
	Name = Farfield, index = 3
AFLR4    : Proximity BG Surface Grid Generation Skipped
AFLR4    : No Modifications Required
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 3
	Name = Wing1, index = 1
	Name = Wing2, index = 2
	Name = Farfield, index = 3
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 3
	Name = Wing1, index = 1
	Name = Wing2, index = 2
	Name = Farfield, index = 3
Getting volume mesh

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

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

Writing SU2 file ....
Finished writing SU2 file

Getting CFD boundary conditions
	Boundary condition name - Farfield
	Boundary condition name - Wing1
	Boundary condition name - Wing2
	Done getting CFD boundary conditions
Warning: The su2 cfg file will be overwritten!
Write SU2 configuration file for version "Harrier (8.0.1)"
Running SU2 1
Getting CFD boundary conditions
	Boundary condition name - Farfield
	Boundary condition name - Wing1
	Boundary condition name - Wing2
	Done getting CFD boundary conditions
Writing boundary flags
 - bcProps.surfaceProp[0].surfaceType = 3
 - bcProps.surfaceProp[1].surfaceType = 2
 - bcProps.surfaceProp[2].surfaceType = 1
Done boundary flags
Warning: The su2 cfg file will be overwritten!
Write SU2 configuration file for version "Harrier (8.0.1)"
Running SU2 2
 EGADS Info: 0 Objects, 0 Reference in Use (of 0) at Close!


 CAPS Info: Hit last success -- going live!

 CAPS Info: Hit last success -- going live!

 CAPS Info: Hit last success -- going live!

 CAPS Info: Hit last success -- going live!

 CAPS Info: Hit last success -- going live!

 CAPS Info: Hit last success -- going live!

 CAPS Info: Hit last success -- going live!

 CAPS Info: Hit last success -- going live!


 CAPS Info: Hit last success -- going live!


 CAPS Info: Hit last success -- going live!

 CAPS Info: Hit last success -- going live!

Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 3
	Name = Wing1, index = 1
	Name = Wing2, index = 2
	Name = Farfield, index = 3
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 3
	Name = Wing1, index = 1
	Name = Wing2, index = 2
	Name = Farfield, index = 3
AFLR4    : Proximity BG Surface Grid Generation Skipped
AFLR4    : No Modifications Required
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 3
	Name = Wing1, index = 1
	Name = Wing2, index = 2
	Name = Farfield, index = 3
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 3
	Name = Wing1, index = 1
	Name = Wing2, index = 2
	Name = Farfield, index = 3
Getting volume mesh

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

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

Writing SU2 file ....
Finished writing SU2 file

Getting CFD boundary conditions
	Boundary condition name - Farfield
	Boundary condition name - Wing1
	Boundary condition name - Wing2
	Done getting CFD boundary conditions
Warning: The su2 cfg file will be overwritten!
Write SU2 configuration file for version "Harrier (8.0.1)"

 CAPS Info: Hit last success -- going live!
Running SU2 1

 CAPS Info: Hit last success -- going live!
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 3
	Name = Wing1, index = 1
	Name = Wing2, index = 2
	Name = Farfield, index = 3
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 3
	Name = Wing1, index = 1
	Name = Wing2, index = 2
	Name = Farfield, index = 3
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 3
	Name = Wing1, index = 1
	Name = Wing2, index = 2
	Name = Farfield, index = 3
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 3
	Name = Wing1, index = 1
	Name = Wing2, index = 2
	Name = Farfield, index = 3
Getting CFD boundary conditions
	Boundary condition name - Farfield
	Boundary condition name - Wing1
	Boundary condition name - Wing2
	Done getting CFD boundary conditions

 CAPS Info: Hit last success -- going live!

 CAPS Info: Hit last success -- going live!
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 3
	Name = Wing1, index = 1
	Name = Wing2, index = 2
	Name = Farfield, index = 3
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 3
	Name = Wing1, index = 1
	Name = Wing2, index = 2
	Name = Farfield, index = 3
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 3
	Name = Wing1, index = 1
	Name = Wing2, index = 2
	Name = Farfield, index = 3
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 3
	Name = Wing1, index = 1
	Name = Wing2, index = 2
	Name = Farfield, index = 3
Getting CFD boundary conditions
	Boundary condition name - Farfield
	Boundary condition name - Wing1
	Boundary condition name - Wing2
	Done getting CFD boundary conditions
Writing boundary flags
 - bcProps.surfaceProp[0].surfaceType = 3
 - bcProps.surfaceProp[1].surfaceType = 2
 - bcProps.surfaceProp[2].surfaceType = 1
Done boundary flags
Warning: The su2 cfg file will be overwritten!
Write SU2 configuration file for version "Harrier (8.0.1)"

 CAPS Info: Hit last success -- going live!
Running SU2 2

 CAPS Info: Hit last success -- going live!
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 3
	Name = Wing1, index = 1
	Name = Wing2, index = 2
	Name = Farfield, index = 3
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 3
	Name = Wing1, index = 1
	Name = Wing2, index = 2
	Name = Farfield, index = 3
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 3
	Name = Wing1, index = 1
	Name = Wing2, index = 2
	Name = Farfield, index = 3
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 3
	Name = Wing1, index = 1
	Name = Wing2, index = 2
	Name = Farfield, index = 3
Getting CFD boundary conditions
	Boundary condition name - Farfield
	Boundary condition name - Wing1
	Boundary condition name - Wing2
	Done getting CFD boundary conditions

ok
test_phase (test_su2.TestSU2.test_phase) ... 
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 3
	Name = Wing1, index = 1
	Name = Wing2, index = 2
	Name = Farfield, index = 3
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 3
	Name = Wing1, index = 1
	Name = Wing2, index = 2
	Name = Farfield, index = 3
AFLR4    : Proximity BG Surface Grid Generation Skipped
AFLR4    : No Modifications Required
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 3
	Name = Wing1, index = 1
	Name = Wing2, index = 2
	Name = Farfield, index = 3
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 3
	Name = Wing1, index = 1
	Name = Wing2, index = 2
	Name = Farfield, index = 3
Getting volume mesh

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

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

Writing SU2 file ....
Finished writing SU2 file

Getting CFD boundary conditions
	Boundary condition name - Farfield
	Boundary condition name - Wing1
	Boundary condition name - Wing2
	Done getting CFD boundary conditions
Warning: The su2 cfg file will be overwritten!
Write SU2 configuration file for version "Harrier (8.0.1)"

Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 3
	Name = Wing1, index = 1
	Name = Wing2, index = 2
	Name = Farfield, index = 3
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 3
	Name = Wing1, index = 1
	Name = Wing2, index = 2
	Name = Farfield, index = 3
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 3
	Name = Wing1, index = 1
	Name = Wing2, index = 2
	Name = Farfield, index = 3
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 3
	Name = Wing1, index = 1
	Name = Wing2, index = 2
	Name = Farfield, index = 3
Getting CFD boundary conditions
	Boundary condition name - Farfield
	Boundary condition name - Wing1
	Boundary condition name - Wing2
	Done getting CFD boundary conditions
Writing boundary flags
 - bcProps.surfaceProp[0].surfaceType = 3
 - bcProps.surfaceProp[1].surfaceType = 1
 - bcProps.surfaceProp[2].surfaceType = 1
Done boundary flags
Warning: The su2 cfg file will be overwritten!
Write SU2 configuration file for version "Harrier (8.0.1)"
ok
test_reenter (test_su2.TestSU2.test_reenter) ... Getting CFD boundary conditions
	Boundary condition name - Farfield
	Boundary condition name - Wing1
	Boundary condition name - Wing2
	Done getting CFD boundary conditions
Writing boundary flags
 - bcProps.surfaceProp[0].surfaceType = 3
 - bcProps.surfaceProp[1].surfaceType = 1
 - bcProps.surfaceProp[2].surfaceType = 1
Done boundary flags
Warning: The su2 cfg file will be overwritten!
Write SU2 configuration file for version "BlackBird (7.5.1) "
Getting CFD boundary conditions
	Boundary condition name - Farfield
	Boundary condition name - Wing1
	Boundary condition name - Wing2
	Done getting CFD boundary conditions
Writing boundary flags
 - bcProps.surfaceProp[0].surfaceType = 3
 - bcProps.surfaceProp[1].surfaceType = 2
 - bcProps.surfaceProp[2].surfaceType = 1
Done boundary flags
Warning: The su2 cfg file will be overwritten!
Write SU2 configuration file for version "BlackBird (7.5.1) "
ok
test_units (test_su2.TestSU2.test_units) ... Getting CFD boundary conditions
	Boundary condition name - Farfield
	Boundary condition name - Wing1
	Boundary condition name - Wing2
	Done getting CFD boundary conditions
Warning: The su2 cfg file will be overwritten!
Write SU2 configuration file for version "Harrier (8.0.1)"
ok
test_PlateSensFile (test_tacs.TestTACS.test_PlateSensFile) ... 
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = plate, index = 1
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 0
	Face 1 TFI quading disabled with attribute .qParams
Getting surface mesh for body 1 (of 1)
Body 1 (of 1)
Number of nodes    = 25
Number of elements = 16
Number of triangle elements      = 0
Number of quadrilateral elements = 16
----------------------------
Total number of nodes    = 25
Total number of elements = 16

Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = plate, index = 1
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 0
	Face 1 TFI quading disabled with attribute .qParams
Getting surface mesh for body 1 (of 1)
Body 1 (of 1)
Number of nodes    = 25
Number of elements = 16
Number of triangle elements      = 0
Number of quadrilateral elements = 16
----------------------------
Total number of nodes    = 25
Total number of elements = 16
Mapping Csys attributes ................
	Number of unique Csys attributes = 0

Getting FEA coordinate systems.......
	Number of coordinate systems - 0
	No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
	Number of unique capsConstraint attributes = 1
	Name = plateEdge, index = 1
Mapping capsLoad attributes ................
	Number of unique capsLoad attributes = 1
	Name = plate, index = 1
Mapping capsBound attributes ................
	Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
	Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
	Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
	Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
	Mesh for body = 0
	Number of nodal coordinates = 25
	Number of elements = 16
	Elemental Nodes = 0
	Elemental Rods  = 0
	Elemental Tria3 = 0
	Elemental Quad4 = 16

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

Getting FEA properties.......
	Number of properties - 1
	Property name - plate
	Done getting FEA properties
Updating mesh element types based on properties input

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

Getting FEA loads.......
	Number of loads - 1
	Load name - appliedPressure
	Done getting FEA loads

Getting FEA design variables.......
	Number of design variables          - 2
	Design_Variable name - plateLength
	Design_Variable name - thick1
	Design_Variable_Relation name - thick1
	Number of design variable relations - 1
	Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL

Getting FEA analyses.......
	Number of analyses - 1
	Analysis name - Default
	Done getting FEA analyses

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

Writing subElement types (if any) - appending mesh file

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

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

Getting FEA coordinate systems.......
	Number of coordinate systems - 0
	No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
	Number of unique capsConstraint attributes = 1
	Name = plateEdge, index = 1
Mapping capsLoad attributes ................
	Number of unique capsLoad attributes = 1
	Name = plate, index = 1
Mapping capsBound attributes ................
	Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
	Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
	Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
	Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
	Mesh for body = 0
	Number of nodal coordinates = 25
	Number of elements = 16
	Elemental Nodes = 0
	Elemental Rods  = 0
	Elemental Tria3 = 0
	Elemental Quad4 = 16

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

Getting FEA properties.......
	Number of properties - 1
	Property name - plate
	Done getting FEA properties
Updating mesh element types based on properties input

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

Getting FEA loads.......
	Number of loads - 1
	Load name - appliedPressure
	Done getting FEA loads

Getting FEA design variables.......
	Number of design variables          - 2
	Design_Variable name - plateLength
	Design_Variable name - thick1
	Design_Variable_Relation name - thick1
	Number of design variable relations - 1
	Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL

Getting FEA analyses.......
	Number of analyses - 1
	Analysis name - Default
	Done getting FEA analyses

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

Writing subElement types (if any) - appending mesh file

Writing TACS instruction file....
	Writing analysis cards
	Writing load ADD cards
	Writing constraint ADD cards
	Writing load cards
	Writing constraint cards
	Writing material cards
	Writing property cards
	Writing design variable cards
	Writing design variable relation cards
Mapping Csys attributes ................
	Number of unique Csys attributes = 0

Getting FEA coordinate systems.......
	Number of coordinate systems - 0
	No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
	Number of unique capsConstraint attributes = 1
	Name = plateEdge, index = 1
Mapping capsLoad attributes ................
	Number of unique capsLoad attributes = 1
	Name = plate, index = 1
Mapping capsBound attributes ................
	Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
	Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
	Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
	Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
	Mesh for body = 0
	Number of nodal coordinates = 25
	Number of elements = 16
	Elemental Nodes = 0
	Elemental Rods  = 0
	Elemental Tria3 = 0
	Elemental Quad4 = 16

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

Getting FEA properties.......
	Number of properties - 1
	Property name - plate
	Done getting FEA properties
Updating mesh element types based on properties input

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

Getting FEA loads.......
	Number of loads - 1
	Load name - appliedPressure
	Done getting FEA loads

Getting FEA design variables.......
	Number of design variables          - 2
	Design_Variable name - plateLength
	Design_Variable name - thick1
	Design_Variable_Relation name - thick1
	Number of design variable relations - 1
	Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL

Getting FEA analyses.......
	Number of analyses - 1
	Analysis name - Default
	Done getting FEA analyses

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

Writing subElement types (if any) - appending mesh file

Writing TACS instruction file....
	Writing analysis cards
	Writing load ADD cards
	Writing constraint ADD cards
	Writing load cards
	Writing constraint cards
	Writing material cards
	Writing property cards
	Writing design variable cards
	Writing design variable relation cards
Mapping Csys attributes ................
	Number of unique Csys attributes = 0

Getting FEA coordinate systems.......
	Number of coordinate systems - 0
	No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
	Number of unique capsConstraint attributes = 1
	Name = plateEdge, index = 1
Mapping capsLoad attributes ................
	Number of unique capsLoad attributes = 1
	Name = plate, index = 1
Mapping capsBound attributes ................
	Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
	Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
	Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
	Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
	Mesh for body = 0
	Number of nodal coordinates = 25
	Number of elements = 16
	Elemental Nodes = 0
	Elemental Rods  = 0
	Elemental Tria3 = 0
	Elemental Quad4 = 16

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

Getting FEA properties.......
	Number of properties - 1
	Property name - plate
	Done getting FEA properties
Updating mesh element types based on properties input

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

Getting FEA loads.......
	Number of loads - 1
	Load name - appliedPressure
	Done getting FEA loads

Getting FEA design variables.......
	Number of design variables          - 2
	Design_Variable name - plateLength
	Design_Variable name - thick1
	Design_Variable_Relation name - thick1
	Number of design variable relations - 1
	Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL

Getting FEA analyses.......
	Number of analyses - 1
	Analysis name - Default
	Done getting FEA analyses

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

Writing subElement types (if any) - appending mesh file

Writing TACS instruction file....
	Writing analysis cards
	Writing load ADD cards
	Writing constraint ADD cards
	Writing load cards
	Writing constraint cards
	Writing material cards
	Writing property cards
	Writing design variable cards
	Writing design variable relation cards
Mapping Csys attributes ................
	Number of unique Csys attributes = 0

Getting FEA coordinate systems.......
	Number of coordinate systems - 0
	No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
	Number of unique capsConstraint attributes = 1
	Name = plateEdge, index = 1
Mapping capsLoad attributes ................
	Number of unique capsLoad attributes = 1
	Name = plate, index = 1
Mapping capsBound attributes ................
	Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
	Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
	Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
	Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
	Mesh for body = 0
	Number of nodal coordinates = 25
	Number of elements = 16
	Elemental Nodes = 0
	Elemental Rods  = 0
	Elemental Tria3 = 0
	Elemental Quad4 = 16

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

Getting FEA properties.......
	Number of properties - 1
	Property name - plate
	Done getting FEA properties
Updating mesh element types based on properties input

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

Getting FEA loads.......
	Number of loads - 1
	Load name - appliedPressure
	Done getting FEA loads

Getting FEA design variables.......
	Number of design variables          - 2
	Design_Variable name - plateLength
	Design_Variable name - thick1
	Design_Variable_Relation name - thick1
	Number of design variable relations - 1
	Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL

Getting FEA analyses.......
	Number of analyses - 1
	Analysis name - Default
	Done getting FEA analyses

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

Writing subElement types (if any) - appending mesh file

Writing TACS instruction file....
	Writing analysis cards
	Writing load ADD cards
	Writing constraint ADD cards
	Writing load cards
	Writing constraint cards
	Writing material cards
	Writing property cards
	Writing design variable cards
	Writing design variable relation cards
Mapping Csys attributes ................
	Number of unique Csys attributes = 0

Getting FEA coordinate systems.......
	Number of coordinate systems - 0
	No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
	Number of unique capsConstraint attributes = 1
	Name = plateEdge, index = 1
Mapping capsLoad attributes ................
	Number of unique capsLoad attributes = 1
	Name = plate, index = 1
Mapping capsBound attributes ................
	Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
	Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
	Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
	Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
	Mesh for body = 0
	Number of nodal coordinates = 25
	Number of elements = 16
	Elemental Nodes = 0
	Elemental Rods  = 0
	Elemental Tria3 = 0
	Elemental Quad4 = 16

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

Getting FEA properties.......
	Number of properties - 1
	Property name - plate
	Done getting FEA properties
Updating mesh element types based on properties input

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

Getting FEA loads.......
	Number of loads - 1
	Load name - appliedPressure
	Done getting FEA loads

Getting FEA design variables.......
	Number of design variables          - 2
	Design_Variable name - plateLength
	Design_Variable name - thick1
	Design_Variable_Relation name - thick1
	Number of design variable relations - 1
	Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL

Getting FEA analyses.......
	Number of analyses - 1
	Analysis name - Default
	Done getting FEA analyses

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

Writing subElement types (if any) - appending mesh file

Writing TACS instruction file....
	Writing analysis cards
	Writing load ADD cards
	Writing constraint ADD cards
	Writing load cards
	Writing constraint cards
	Writing material cards
	Writing property cards
	Writing design variable cards
	Writing design variable relation cards
Mapping Csys attributes ................
	Number of unique Csys attributes = 0

Getting FEA coordinate systems.......
	Number of coordinate systems - 0
	No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
	Number of unique capsConstraint attributes = 1
	Name = plateEdge, index = 1
Mapping capsLoad attributes ................
	Number of unique capsLoad attributes = 1
	Name = plate, index = 1
Mapping capsBound attributes ................
	Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
	Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
	Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
	Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
	Mesh for body = 0
	Number of nodal coordinates = 25
	Number of elements = 16
	Elemental Nodes = 0
	Elemental Rods  = 0
	Elemental Tria3 = 0
	Elemental Quad4 = 16

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

Getting FEA properties.......
	Number of properties - 1
	Property name - plate
	Done getting FEA properties
Updating mesh element types based on properties input

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

Getting FEA loads.......
	Number of loads - 1
	Load name - appliedPressure
	Done getting FEA loads

Getting FEA design variables.......
	Number of design variables          - 2
	Design_Variable name - plateLength
	Design_Variable name - thick1
	Design_Variable_Relation name - thick1
	Number of design variable relations - 1
	Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL

Getting FEA analyses.......
	Number of analyses - 1
	Analysis name - Default
	Done getting FEA analyses

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

Writing subElement types (if any) - appending mesh file

Writing TACS instruction file....
	Writing analysis cards
	Writing load ADD cards
	Writing constraint ADD cards
	Writing load cards
	Writing constraint cards
	Writing material cards
	Writing property cards
	Writing design variable cards
	Writing design variable relation cards
Mapping Csys attributes ................
	Number of unique Csys attributes = 0

Getting FEA coordinate systems.......
	Number of coordinate systems - 0
	No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
	Number of unique capsConstraint attributes = 1
	Name = plateEdge, index = 1
Mapping capsLoad attributes ................
	Number of unique capsLoad attributes = 1
	Name = plate, index = 1
Mapping capsBound attributes ................
	Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
	Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
	Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
	Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
	Mesh for body = 0
	Number of nodal coordinates = 25
	Number of elements = 16
	Elemental Nodes = 0
	Elemental Rods  = 0
	Elemental Tria3 = 0
	Elemental Quad4 = 16

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

Getting FEA properties.......
	Number of properties - 1
	Property name - plate
	Done getting FEA properties
Updating mesh element types based on properties input

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

Getting FEA loads.......
	Number of loads - 1
	Load name - appliedPressure
	Done getting FEA loads

Getting FEA design variables.......
	Number of design variables          - 2
	Design_Variable name - plateLength
	Design_Variable name - thick1
	Design_Variable_Relation name - thick1
	Number of design variable relations - 1
	Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL

Getting FEA analyses.......
	Number of analyses - 1
	Analysis name - Default
	Done getting FEA analyses

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

Writing subElement types (if any) - appending mesh file

Writing TACS instruction file....
	Writing analysis cards
	Writing load ADD cards
	Writing constraint ADD cards
	Writing load cards
	Writing constraint cards
	Writing material cards
	Writing property cards
	Writing design variable cards
	Writing design variable relation cards
Mapping Csys attributes ................
	Number of unique Csys attributes = 0

Getting FEA coordinate systems.......
	Number of coordinate systems - 0
	No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
	Number of unique capsConstraint attributes = 1
	Name = plateEdge, index = 1
Mapping capsLoad attributes ................
	Number of unique capsLoad attributes = 1
	Name = plate, index = 1
Mapping capsBound attributes ................
	Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
	Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
	Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
	Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
	Mesh for body = 0
	Number of nodal coordinates = 25
	Number of elements = 16
	Elemental Nodes = 0
	Elemental Rods  = 0
	Elemental Tria3 = 0
	Elemental Quad4 = 16

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

Getting FEA properties.......
	Number of properties - 1
	Property name - plate
	Done getting FEA properties
Updating mesh element types based on properties input

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

Getting FEA loads.......
	Number of loads - 1
	Load name - appliedPressure
	Done getting FEA loads

Getting FEA design variables.......
	Number of design variables          - 2
	Design_Variable name - plateLength
	Design_Variable name - thick1
	Design_Variable_Relation name - thick1
	Number of design variable relations - 1
	Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL

Getting FEA analyses.......
	Number of analyses - 1
	Analysis name - Default
	Done getting FEA analyses

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

Writing subElement types (if any) - appending mesh file

Writing TACS instruction file....
	Writing analysis cards
	Writing load ADD cards
	Writing constraint ADD cards
	Writing load cards
	Writing constraint cards
	Writing material cards
	Writing property cards
	Writing design variable cards
	Writing design variable relation cards
Mapping Csys attributes ................
	Number of unique Csys attributes = 0

Getting FEA coordinate systems.......
	Number of coordinate systems - 0
	No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
	Number of unique capsConstraint attributes = 1
	Name = plateEdge, index = 1
Mapping capsLoad attributes ................
	Number of unique capsLoad attributes = 1
	Name = plate, index = 1
Mapping capsBound attributes ................
	Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
	Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
	Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
	Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
	Mesh for body = 0
	Number of nodal coordinates = 25
	Number of elements = 16
	Elemental Nodes = 0
	Elemental Rods  = 0
	Elemental Tria3 = 0
	Elemental Quad4 = 16

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

Getting FEA properties.......
	Number of properties - 1
	Property name - plate
	Done getting FEA properties
Updating mesh element types based on properties input

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

Getting FEA loads.......
	Number of loads - 1
	Load name - appliedPressure
	Done getting FEA loads

Getting FEA design variables.......
	Number of design variables          - 2
	Design_Variable name - plateLength
	Design_Variable name - thick1
	Design_Variable_Relation name - thick1
	Number of design variable relations - 1
	Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL

Getting FEA analyses.......
	Number of analyses - 1
	Analysis name - Default
	Done getting FEA analyses

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

Writing subElement types (if any) - appending mesh file

Writing TACS instruction file....
	Writing analysis cards
	Writing load ADD cards
	Writing constraint ADD cards
	Writing load cards
	Writing constraint cards
	Writing material cards
	Writing property cards
	Writing design variable cards
	Writing design variable relation cards
Mapping Csys attributes ................
	Number of unique Csys attributes = 0

Getting FEA coordinate systems.......
	Number of coordinate systems - 0
	No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
	Number of unique capsConstraint attributes = 1
	Name = plateEdge, index = 1
Mapping capsLoad attributes ................
	Number of unique capsLoad attributes = 1
	Name = plate, index = 1
Mapping capsBound attributes ................
	Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
	Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
	Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
	Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
	Mesh for body = 0
	Number of nodal coordinates = 25
	Number of elements = 16
	Elemental Nodes = 0
	Elemental Rods  = 0
	Elemental Tria3 = 0
	Elemental Quad4 = 16

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

Getting FEA properties.......
	Number of properties - 1
	Property name - plate
	Done getting FEA properties
Updating mesh element types based on properties input

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

Getting FEA loads.......
	Number of loads - 1
	Load name - appliedPressure
	Done getting FEA loads

Getting FEA design variables.......
	Number of design variables          - 2
	Design_Variable name - plateLength
	Design_Variable name - thick1
	Design_Variable_Relation name - thick1
	Number of design variable relations - 1
	Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL

Getting FEA analyses.......
	Number of analyses - 1
	Analysis name - Default
	Done getting FEA analyses

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

Writing subElement types (if any) - appending mesh file

Writing TACS instruction file....
	Writing analysis cards
	Writing load ADD cards
	Writing constraint ADD cards
	Writing load cards
	Writing constraint cards
	Writing material cards
	Writing property cards
	Writing design variable cards
	Writing design variable relation cards
Mapping Csys attributes ................
	Number of unique Csys attributes = 0

Getting FEA coordinate systems.......
	Number of coordinate systems - 0
	No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
	Number of unique capsConstraint attributes = 1
	Name = plateEdge, index = 1
Mapping capsLoad attributes ................
	Number of unique capsLoad attributes = 1
	Name = plate, index = 1
Mapping capsBound attributes ................
	Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
	Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
	Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
	Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
	Mesh for body = 0
	Number of nodal coordinates = 25
	Number of elements = 16
	Elemental Nodes = 0
	Elemental Rods  = 0
	Elemental Tria3 = 0
	Elemental Quad4 = 16

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

Getting FEA properties.......
	Number of properties - 1
	Property name - plate
	Done getting FEA properties
Updating mesh element types based on properties input

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

Getting FEA loads.......
	Number of loads - 1
	Load name - appliedPressure
	Done getting FEA loads

Getting FEA design variables.......
	Number of design variables          - 2
	Design_Variable name - plateLength
	Design_Variable name - thick1
	Design_Variable_Relation name - thick1
	Number of design variable relations - 1
	Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL

Getting FEA analyses.......
	Number of analyses - 1
	Analysis name - Default
	Done getting FEA analyses

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

Writing subElement types (if any) - appending mesh file

Writing TACS instruction file....
	Writing analysis cards
	Writing load ADD cards
	Writing constraint ADD cards
	Writing load cards
	Writing constraint cards
	Writing material cards
	Writing property cards
	Writing design variable cards
	Writing design variable relation cards
Mapping Csys attributes ................
	Number of unique Csys attributes = 0

Getting FEA coordinate systems.......
	Number of coordinate systems - 0
	No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
	Number of unique capsConstraint attributes = 1
	Name = plateEdge, index = 1
Mapping capsLoad attributes ................
	Number of unique capsLoad attributes = 1
	Name = plate, index = 1
Mapping capsBound attributes ................
	Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
	Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
	Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
	Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
	Mesh for body = 0
	Number of nodal coordinates = 25
	Number of elements = 16
	Elemental Nodes = 0
	Elemental Rods  = 0
	Elemental Tria3 = 0
	Elemental Quad4 = 16

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

Getting FEA properties.......
	Number of properties - 1
	Property name - plate
	Done getting FEA properties
Updating mesh element types based on properties input

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

Getting FEA loads.......
	Number of loads - 1
	Load name - appliedPressure
	Done getting FEA loads

Getting FEA design variables.......
	Number of design variables          - 2
	Design_Variable name - plateLength
	Design_Variable name - thick1
	Design_Variable_Relation name - thick1
	Number of design variable relations - 1
	Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL

Getting FEA analyses.......
	Number of analyses - 1
	Analysis name - Default
	Done getting FEA analyses

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

Writing subElement types (if any) - appending mesh file

Writing TACS instruction file....
	Writing analysis cards
	Writing load ADD cards
	Writing constraint ADD cards
	Writing load cards
	Writing constraint cards
	Writing material cards
	Writing property cards
	Writing design variable cards
	Writing design variable relation cards
Mapping Csys attributes ................
	Number of unique Csys attributes = 0

Getting FEA coordinate systems.......
	Number of coordinate systems - 0
	No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
	Number of unique capsConstraint attributes = 1
	Name = plateEdge, index = 1
Mapping capsLoad attributes ................
	Number of unique capsLoad attributes = 1
	Name = plate, index = 1
Mapping capsBound attributes ................
	Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
	Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
	Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
	Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
	Mesh for body = 0
	Number of nodal coordinates = 25
	Number of elements = 16
	Elemental Nodes = 0
	Elemental Rods  = 0
	Elemental Tria3 = 0
	Elemental Quad4 = 16

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

Getting FEA properties.......
	Number of properties - 1
	Property name - plate
	Done getting FEA properties
Updating mesh element types based on properties input

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

Getting FEA loads.......
	Number of loads - 1
	Load name - appliedPressure
	Done getting FEA loads

Getting FEA design variables.......
	Number of design variables          - 2
	Design_Variable name - plateLength
	Design_Variable name - thick1
	Design_Variable_Relation name - thick1
	Number of design variable relations - 1
	Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL

Getting FEA analyses.......
	Number of analyses - 1
	Analysis name - Default
	Done getting FEA analyses

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

Writing subElement types (if any) - appending mesh file

Writing TACS instruction file....
	Writing analysis cards
	Writing load ADD cards
	Writing constraint ADD cards
	Writing load cards
	Writing constraint cards
	Writing material cards
	Writing property cards
	Writing design variable cards
	Writing design variable relation cards
Mapping Csys attributes ................
	Number of unique Csys attributes = 0

Getting FEA coordinate systems.......
	Number of coordinate systems - 0
	No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
	Number of unique capsConstraint attributes = 1
	Name = plateEdge, index = 1
Mapping capsLoad attributes ................
	Number of unique capsLoad attributes = 1
	Name = plate, index = 1
Mapping capsBound attributes ................
	Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
	Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
	Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
	Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
	Mesh for body = 0
	Number of nodal coordinates = 25
	Number of elements = 16
	Elemental Nodes = 0
	Elemental Rods  = 0
	Elemental Tria3 = 0
	Elemental Quad4 = 16

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

Getting FEA properties.......
	Number of properties - 1
	Property name - plate
	Done getting FEA properties
Updating mesh element types based on properties input

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

Getting FEA loads.......
	Number of loads - 1
	Load name - appliedPressure
	Done getting FEA loads

Getting FEA design variables.......
	Number of design variables          - 2
	Design_Variable name - plateLength
	Design_Variable name - thick1
	Design_Variable_Relation name - thick1
	Number of design variable relations - 1
	Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL

Getting FEA analyses.......
	Number of analyses - 1
	Analysis name - Default
	Done getting FEA analyses

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

Writing subElement types (if any) - appending mesh file

Writing TACS instruction file....
	Writing analysis cards
	Writing load ADD cards
	Writing constraint ADD cards
	Writing load cards
	Writing constraint cards
	Writing material cards
	Writing property cards
	Writing design variable cards
	Writing design variable relation cards
Mapping Csys attributes ................
	Number of unique Csys attributes = 0

Getting FEA coordinate systems.......
	Number of coordinate systems - 0
	No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
	Number of unique capsConstraint attributes = 1
	Name = plateEdge, index = 1
Mapping capsLoad attributes ................
	Number of unique capsLoad attributes = 1
	Name = plate, index = 1
Mapping capsBound attributes ................
	Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
	Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
	Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
	Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
	Mesh for body = 0
	Number of nodal coordinates = 25
	Number of elements = 16
	Elemental Nodes = 0
	Elemental Rods  = 0
	Elemental Tria3 = 0
	Elemental Quad4 = 16

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

Getting FEA properties.......
	Number of properties - 1
	Property name - plate
	Done getting FEA properties
Updating mesh element types based on properties input

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

Getting FEA loads.......
	Number of loads - 1
	Load name - appliedPressure
	Done getting FEA loads

Getting FEA design variables.......
	Number of design variables          - 2
	Design_Variable name - plateLength
	Design_Variable name - thick1
	Design_Variable_Relation name - thick1
	Number of design variable relations - 1
	Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL

Getting FEA analyses.......
	Number of analyses - 1
	Analysis name - Default
	Done getting FEA analyses

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

Writing subElement types (if any) - appending mesh file

Writing TACS instruction file....
	Writing analysis cards
	Writing load ADD cards
	Writing constraint ADD cards
	Writing load cards
	Writing constraint cards
	Writing material cards
	Writing property cards
	Writing design variable cards
	Writing design variable relation cards
Mapping Csys attributes ................
	Number of unique Csys attributes = 0

Getting FEA coordinate systems.......
	Number of coordinate systems - 0
	No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
	Number of unique capsConstraint attributes = 1
	Name = plateEdge, index = 1
Mapping capsLoad attributes ................
	Number of unique capsLoad attributes = 1
	Name = plate, index = 1
Mapping capsBound attributes ................
	Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
	Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
	Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
	Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
	Mesh for body = 0
	Number of nodal coordinates = 25
	Number of elements = 16
	Elemental Nodes = 0
	Elemental Rods  = 0
	Elemental Tria3 = 0
	Elemental Quad4 = 16

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

Getting FEA properties.......
	Number of properties - 1
	Property name - plate
	Done getting FEA properties
Updating mesh element types based on properties input

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

Getting FEA loads.......
	Number of loads - 1
	Load name - appliedPressure
	Done getting FEA loads

Getting FEA design variables.......
	Number of design variables          - 2
	Design_Variable name - plateLength
	Design_Variable name - thick1
	Design_Variable_Relation name - thick1
	Number of design variable relations - 1
	Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL

Getting FEA analyses.......
	Number of analyses - 1
	Analysis name - Default
	Done getting FEA analyses

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

Writing subElement types (if any) - appending mesh file

Writing TACS instruction file....
	Writing analysis cards
	Writing load ADD cards
	Writing constraint ADD cards
	Writing load cards
	Writing constraint cards
	Writing material cards
	Writing property cards
	Writing design variable cards
	Writing design variable relation cards
Mapping Csys attributes ................
	Number of unique Csys attributes = 0

Getting FEA coordinate systems.......
	Number of coordinate systems - 0
	No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
	Number of unique capsConstraint attributes = 1
	Name = plateEdge, index = 1
Mapping capsLoad attributes ................
	Number of unique capsLoad attributes = 1
	Name = plate, index = 1
Mapping capsBound attributes ................
	Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
	Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
	Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
	Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
	Mesh for body = 0
	Number of nodal coordinates = 25
	Number of elements = 16
	Elemental Nodes = 0
	Elemental Rods  = 0
	Elemental Tria3 = 0
	Elemental Quad4 = 16

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

Getting FEA properties.......
	Number of properties - 1
	Property name - plate
	Done getting FEA properties
Updating mesh element types based on properties input

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

Getting FEA loads.......
	Number of loads - 1
	Load name - appliedPressure
	Done getting FEA loads

Getting FEA design variables.......
	Number of design variables          - 2
	Design_Variable name - plateLength
	Design_Variable name - thick1
	Design_Variable_Relation name - thick1
	Number of design variable relations - 1
	Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL

Getting FEA analyses.......
	Number of analyses - 1
	Analysis name - Default
	Done getting FEA analyses

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

Writing subElement types (if any) - appending mesh file

Writing TACS instruction file....
	Writing analysis cards
	Writing load ADD cards
	Writing constraint ADD cards
	Writing load cards
	Writing constraint cards
	Writing material cards
	Writing property cards
	Writing design variable cards
	Writing design variable relation cards
Mapping Csys attributes ................
	Number of unique Csys attributes = 0

Getting FEA coordinate systems.......
	Number of coordinate systems - 0
	No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
	Number of unique capsConstraint attributes = 1
	Name = plateEdge, index = 1
Mapping capsLoad attributes ................
	Number of unique capsLoad attributes = 1
	Name = plate, index = 1
Mapping capsBound attributes ................
	Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
	Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
	Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
	Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
	Mesh for body = 0
	Number of nodal coordinates = 25
	Number of elements = 16
	Elemental Nodes = 0
	Elemental Rods  = 0
	Elemental Tria3 = 0
	Elemental Quad4 = 16

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

Getting FEA properties.......
	Number of properties - 1
	Property name - plate
	Done getting FEA properties
Updating mesh element types based on properties input

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

Getting FEA loads.......
	Number of loads - 1
	Load name - appliedPressure
	Done getting FEA loads

Getting FEA design variables.......
	Number of design variables          - 2
	Design_Variable name - plateLength
	Design_Variable name - thick1
	Design_Variable_Relation name - thick1
	Number of design variable relations - 1
	Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL

Getting FEA analyses.......
	Number of analyses - 1
	Analysis name - Default
	Done getting FEA analyses

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

Writing subElement types (if any) - appending mesh file

Writing TACS instruction file....
	Writing analysis cards
	Writing load ADD cards
	Writing constraint ADD cards
	Writing load cards
	Writing constraint cards
	Writing material cards
	Writing property cards
	Writing design variable cards
	Writing design variable relation cards
Mapping Csys attributes ................
	Number of unique Csys attributes = 0

Getting FEA coordinate systems.......
	Number of coordinate systems - 0
	No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
	Number of unique capsConstraint attributes = 1
	Name = plateEdge, index = 1
Mapping capsLoad attributes ................
	Number of unique capsLoad attributes = 1
	Name = plate, index = 1
Mapping capsBound attributes ................
	Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
	Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
	Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
	Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
	Mesh for body = 0
	Number of nodal coordinates = 25
	Number of elements = 16
	Elemental Nodes = 0
	Elemental Rods  = 0
	Elemental Tria3 = 0
	Elemental Quad4 = 16

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

Getting FEA properties.......
	Number of properties - 1
	Property name - plate
	Done getting FEA properties
Updating mesh element types based on properties input

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

Getting FEA loads.......
	Number of loads - 1
	Load name - appliedPressure
	Done getting FEA loads

Getting FEA design variables.......
	Number of design variables          - 2
	Design_Variable name - plateLength
	Design_Variable name - thick1
	Design_Variable_Relation name - thick1
	Number of design variable relations - 1
	Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL

Getting FEA analyses.......
	Number of analyses - 1
	Analysis name - Default
	Done getting FEA analyses

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

Writing subElement types (if any) - appending mesh file

Writing TACS instruction file....
	Writing analysis cards
	Writing load ADD cards
	Writing constraint ADD cards
	Writing load cards
	Writing constraint cards
	Writing material cards
	Writing property cards
	Writing design variable cards
	Writing design variable relation cards
Mapping Csys attributes ................
	Number of unique Csys attributes = 0

Getting FEA coordinate systems.......
	Number of coordinate systems - 0
	No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
	Number of unique capsConstraint attributes = 1
	Name = plateEdge, index = 1
Mapping capsLoad attributes ................
	Number of unique capsLoad attributes = 1
	Name = plate, index = 1
Mapping capsBound attributes ................
	Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
	Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
	Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
	Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
	Mesh for body = 0
	Number of nodal coordinates = 25
	Number of elements = 16
	Elemental Nodes = 0
	Elemental Rods  = 0
	Elemental Tria3 = 0
	Elemental Quad4 = 16

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

Getting FEA properties.......
	Number of properties - 1
	Property name - plate
	Done getting FEA properties
Updating mesh element types based on properties input

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

Getting FEA loads.......
	Number of loads - 1
	Load name - appliedPressure
	Done getting FEA loads

Getting FEA design variables.......
	Number of design variables          - 2
	Design_Variable name - plateLength
	Design_Variable name - thick1
	Design_Variable_Relation name - thick1
	Number of design variable relations - 1
	Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL

Getting FEA analyses.......
	Number of analyses - 1
	Analysis name - Default
	Done getting FEA analyses

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

Writing subElement types (if any) - appending mesh file

Writing TACS instruction file....
	Writing analysis cards
	Writing load ADD cards
	Writing constraint ADD cards
	Writing load cards
	Writing constraint cards
	Writing material cards
	Writing property cards
	Writing design variable cards
	Writing design variable relation cards
Mapping Csys attributes ................
	Number of unique Csys attributes = 0

Getting FEA coordinate systems.......
	Number of coordinate systems - 0
	No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
	Number of unique capsConstraint attributes = 1
	Name = plateEdge, index = 1
Mapping capsLoad attributes ................
	Number of unique capsLoad attributes = 1
	Name = plate, index = 1
Mapping capsBound attributes ................
	Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
	Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
	Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
	Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
	Mesh for body = 0
	Number of nodal coordinates = 25
	Number of elements = 16
	Elemental Nodes = 0
	Elemental Rods  = 0
	Elemental Tria3 = 0
	Elemental Quad4 = 16

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

Getting FEA properties.......
	Number of properties - 1
	Property name - plate
	Done getting FEA properties
Updating mesh element types based on properties input

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

Getting FEA loads.......
	Number of loads - 1
	Load name - appliedPressure
	Done getting FEA loads

Getting FEA design variables.......
	Number of design variables          - 2
	Design_Variable name - plateLength
	Design_Variable name - thick1
	Design_Variable_Relation name - thick1
	Number of design variable relations - 1
	Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL

Getting FEA analyses.......
	Number of analyses - 1
	Analysis name - Default
	Done getting FEA analyses

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

Writing subElement types (if any) - appending mesh file

Writing TACS instruction file....
	Writing analysis cards
	Writing load ADD cards
	Writing constraint ADD cards
	Writing load cards
	Writing constraint cards
	Writing material cards
	Writing property cards
	Writing design variable cards
	Writing design variable relation cards
Mapping Csys attributes ................
	Number of unique Csys attributes = 0

Getting FEA coordinate systems.......
	Number of coordinate systems - 0
	No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
	Number of unique capsConstraint attributes = 1
	Name = plateEdge, index = 1
Mapping capsLoad attributes ................
	Number of unique capsLoad attributes = 1
	Name = plate, index = 1
Mapping capsBound attributes ................
	Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
	Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
	Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
	Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
	Mesh for body = 0
	Number of nodal coordinates = 25
	Number of elements = 16
	Elemental Nodes = 0
	Elemental Rods  = 0
	Elemental Tria3 = 0
	Elemental Quad4 = 16

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

Getting FEA properties.......
	Number of properties - 1
	Property name - plate
	Done getting FEA properties
Updating mesh element types based on properties input

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

Getting FEA loads.......
	Number of loads - 1
	Load name - appliedPressure
	Done getting FEA loads

Getting FEA design variables.......
	Number of design variables          - 2
	Design_Variable name - plateLength
	Design_Variable name - thick1
	Design_Variable_Relation name - thick1
	Number of design variable relations - 1
	Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL

Getting FEA analyses.......
	Number of analyses - 1
	Analysis name - Default
	Done getting FEA analyses

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

Writing subElement types (if any) - appending mesh file

Writing TACS instruction file....
	Writing analysis cards
	Writing load ADD cards
	Writing constraint ADD cards
	Writing load cards
	Writing constraint cards
	Writing material cards
	Writing property cards
	Writing design variable cards
	Writing design variable relation cards
Mapping Csys attributes ................
	Number of unique Csys attributes = 0

Getting FEA coordinate systems.......
	Number of coordinate systems - 0
	No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
	Number of unique capsConstraint attributes = 1
	Name = plateEdge, index = 1
Mapping capsLoad attributes ................
	Number of unique capsLoad attributes = 1
	Name = plate, index = 1
Mapping capsBound attributes ................
	Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
	Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
	Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
	Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
	Mesh for body = 0
	Number of nodal coordinates = 25
	Number of elements = 16
	Elemental Nodes = 0
	Elemental Rods  = 0
	Elemental Tria3 = 0
	Elemental Quad4 = 16

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

Getting FEA properties.......
	Number of properties - 1
	Property name - plate
	Done getting FEA properties
Updating mesh element types based on properties input

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

Getting FEA loads.......
	Number of loads - 1
	Load name - appliedPressure
	Done getting FEA loads

Getting FEA design variables.......
	Number of design variables          - 2
	Design_Variable name - plateLength
	Design_Variable name - thick1
	Design_Variable_Relation name - thick1
	Number of design variable relations - 1
	Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL

Getting FEA analyses.......
	Number of analyses - 1
	Analysis name - Default
	Done getting FEA analyses

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

Writing subElement types (if any) - appending mesh file

Writing TACS instruction file....
	Writing analysis cards
	Writing load ADD cards
	Writing constraint ADD cards
	Writing load cards
	Writing constraint cards
	Writing material cards
	Writing property cards
	Writing design variable cards
	Writing design variable relation cards
Mapping Csys attributes ................
	Number of unique Csys attributes = 0

Getting FEA coordinate systems.......
	Number of coordinate systems - 0
	No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
	Number of unique capsConstraint attributes = 1
	Name = plateEdge, index = 1
Mapping capsLoad attributes ................
	Number of unique capsLoad attributes = 1
	Name = plate, index = 1
Mapping capsBound attributes ................
	Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
	Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
	Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
	Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
	Mesh for body = 0
	Number of nodal coordinates = 25
	Number of elements = 16
	Elemental Nodes = 0
	Elemental Rods  = 0
	Elemental Tria3 = 0
	Elemental Quad4 = 16

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

Getting FEA properties.......
	Number of properties - 1
	Property name - plate
	Done getting FEA properties
Updating mesh element types based on properties input

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

Getting FEA loads.......
	Number of loads - 1
	Load name - appliedPressure
	Done getting FEA loads

Getting FEA design variables.......
	Number of design variables          - 2
	Design_Variable name - plateLength
	Design_Variable name - thick1
	Design_Variable_Relation name - thick1
	Number of design variable relations - 1
	Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL

Getting FEA analyses.......
	Number of analyses - 1
	Analysis name - Default
	Done getting FEA analyses

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

Writing subElement types (if any) - appending mesh file

Writing TACS instruction file....
	Writing analysis cards
	Writing load ADD cards
	Writing constraint ADD cards
	Writing load cards
	Writing constraint cards
	Writing material cards
	Writing property cards
	Writing design variable cards
	Writing design variable relation cards
Mapping Csys attributes ................
	Number of unique Csys attributes = 0

Getting FEA coordinate systems.......
	Number of coordinate systems - 0
	No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
	Number of unique capsConstraint attributes = 1
	Name = plateEdge, index = 1
Mapping capsLoad attributes ................
	Number of unique capsLoad attributes = 1
	Name = plate, index = 1
Mapping capsBound attributes ................
	Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
	Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
	Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
	Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = plate, index = 1
Projecting tessellation 1 (of 1) on to new body
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
	Mesh for body = 0
	Number of nodal coordinates = 25
	Number of elements = 16
	Elemental Nodes = 0
	Elemental Rods  = 0
	Elemental Tria3 = 0
	Elemental Quad4 = 16

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

Getting FEA properties.......
	Number of properties - 1
	Property name - plate
	Done getting FEA properties
Updating mesh element types based on properties input

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

Getting FEA loads.......
	Number of loads - 1
	Load name - appliedPressure
	Done getting FEA loads

Getting FEA design variables.......
	Number of design variables          - 1
	Design_Variable name - plateWidth
	Number of design variable relations - 0
	Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL

Getting FEA analyses.......
	Number of analyses - 1
	Analysis name - Default
	Done getting FEA analyses

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

Writing subElement types (if any) - appending mesh file

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

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

Getting FEA coordinate systems.......
	Number of coordinate systems - 0
	No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
	Number of unique capsConstraint attributes = 1
	Name = plateEdge, index = 1
Mapping capsLoad attributes ................
	Number of unique capsLoad attributes = 1
	Name = plate, index = 1
Mapping capsBound attributes ................
	Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
	Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
	Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
	Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
	Mesh for body = 0
	Number of nodal coordinates = 25
	Number of elements = 16
	Elemental Nodes = 0
	Elemental Rods  = 0
	Elemental Tria3 = 0
	Elemental Quad4 = 16

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

Getting FEA properties.......
	Number of properties - 1
	Property name - plate
	Done getting FEA properties
Updating mesh element types based on properties input

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

Getting FEA loads.......
	Number of loads - 1
	Load name - appliedPressure
	Done getting FEA loads

Getting FEA design variables.......
	Number of design variables          - 1
	Design_Variable name - plateWidth
	Number of design variable relations - 0
	Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL

Getting FEA analyses.......
	Number of analyses - 1
	Analysis name - Default
	Done getting FEA analyses

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

Writing subElement types (if any) - appending mesh file

Writing TACS instruction file....
	Writing analysis cards
	Writing load ADD cards
	Writing constraint ADD cards
	Writing load cards
	Writing constraint cards
	Writing material cards
	Writing property cards
	Writing design variable cards
Mapping Csys attributes ................
	Number of unique Csys attributes = 0

Getting FEA coordinate systems.......
	Number of coordinate systems - 0
	No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
	Number of unique capsConstraint attributes = 1
	Name = plateEdge, index = 1
Mapping capsLoad attributes ................
	Number of unique capsLoad attributes = 1
	Name = plate, index = 1
Mapping capsBound attributes ................
	Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
	Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
	Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
	Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
	Mesh for body = 0
	Number of nodal coordinates = 25
	Number of elements = 16
	Elemental Nodes = 0
	Elemental Rods  = 0
	Elemental Tria3 = 0
	Elemental Quad4 = 16

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

Getting FEA properties.......
	Number of properties - 1
	Property name - plate
	Done getting FEA properties
Updating mesh element types based on properties input

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

Getting FEA loads.......
	Number of loads - 1
	Load name - appliedPressure
	Done getting FEA loads

Getting FEA design variables.......
	Number of design variables          - 1
	Design_Variable name - plateWidth
	Number of design variable relations - 0
	Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL

Getting FEA analyses.......
	Number of analyses - 1
	Analysis name - Default
	Done getting FEA analyses

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

Writing subElement types (if any) - appending mesh file

Writing TACS instruction file....
	Writing analysis cards
	Writing load ADD cards
	Writing constraint ADD cards
	Writing load cards
	Writing constraint cards
	Writing material cards
	Writing property cards
	Writing design variable cards
Mapping Csys attributes ................
	Number of unique Csys attributes = 0

Getting FEA coordinate systems.......
	Number of coordinate systems - 0
	No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
	Number of unique capsConstraint attributes = 1
	Name = plateEdge, index = 1
Mapping capsLoad attributes ................
	Number of unique capsLoad attributes = 1
	Name = plate, index = 1
Mapping capsBound attributes ................
	Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
	Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
	Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
	Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
	Mesh for body = 0
	Number of nodal coordinates = 25
	Number of elements = 16
	Elemental Nodes = 0
	Elemental Rods  = 0
	Elemental Tria3 = 0
	Elemental Quad4 = 16

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

Getting FEA properties.......
	Number of properties - 1
	Property name - plate
	Done getting FEA properties
Updating mesh element types based on properties input

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

Getting FEA loads.......
	Number of loads - 1
	Load name - appliedPressure
	Done getting FEA loads

Getting FEA design variables.......
	Number of design variables          - 1
	Design_Variable name - plateWidth
	Number of design variable relations - 0
	Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL

Getting FEA analyses.......
	Number of analyses - 1
	Analysis name - Default
	Done getting FEA analyses

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

Writing subElement types (if any) - appending mesh file

Writing TACS instruction file....
	Writing analysis cards
	Writing load ADD cards
	Writing constraint ADD cards
	Writing load cards
	Writing constraint cards
	Writing material cards
	Writing property cards
	Writing design variable cards
Mapping Csys attributes ................
	Number of unique Csys attributes = 0

Getting FEA coordinate systems.......
	Number of coordinate systems - 0
	No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
	Number of unique capsConstraint attributes = 1
	Name = plateEdge, index = 1
Mapping capsLoad attributes ................
	Number of unique capsLoad attributes = 1
	Name = plate, index = 1
Mapping capsBound attributes ................
	Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
	Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
	Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
	Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
	Mesh for body = 0
	Number of nodal coordinates = 25
	Number of elements = 16
	Elemental Nodes = 0
	Elemental Rods  = 0
	Elemental Tria3 = 0
	Elemental Quad4 = 16

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

Getting FEA properties.......
	Number of properties - 1
	Property name - plate
	Done getting FEA properties
Updating mesh element types based on properties input

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

Getting FEA loads.......
	Number of loads - 1
	Load name - appliedPressure
	Done getting FEA loads

Getting FEA design variables.......
	Number of design variables          - 1
	Design_Variable name - plateWidth
	Number of design variable relations - 0
	Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL

Getting FEA analyses.......
	Number of analyses - 1
	Analysis name - Default
	Done getting FEA analyses

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

Writing subElement types (if any) - appending mesh file

Writing TACS instruction file....
	Writing analysis cards
	Writing load ADD cards
	Writing constraint ADD cards
	Writing load cards
	Writing constraint cards
	Writing material cards
	Writing property cards
	Writing design variable cards
Mapping Csys attributes ................
	Number of unique Csys attributes = 0

Getting FEA coordinate systems.......
	Number of coordinate systems - 0
	No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
	Number of unique capsConstraint attributes = 1
	Name = plateEdge, index = 1
Mapping capsLoad attributes ................
	Number of unique capsLoad attributes = 1
	Name = plate, index = 1
Mapping capsBound attributes ................
	Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
	Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
	Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
	Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
	Mesh for body = 0
	Number of nodal coordinates = 25
	Number of elements = 16
	Elemental Nodes = 0
	Elemental Rods  = 0
	Elemental Tria3 = 0
	Elemental Quad4 = 16

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

Getting FEA properties.......
	Number of properties - 1
	Property name - plate
	Done getting FEA properties
Updating mesh element types based on properties input

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

Getting FEA loads.......
	Number of loads - 1
	Load name - appliedPressure
	Done getting FEA loads

Getting FEA design variables.......
	Number of design variables          - 1
	Design_Variable name - plateWidth
	Number of design variable relations - 0
	Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL

Getting FEA analyses.......
	Number of analyses - 1
	Analysis name - Default
	Done getting FEA analyses

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

Writing subElement types (if any) - appending mesh file

Writing TACS instruction file....
	Writing analysis cards
	Writing load ADD cards
	Writing constraint ADD cards
	Writing load cards
	Writing constraint cards
	Writing material cards
	Writing property cards
	Writing design variable cards
Mapping Csys attributes ................
	Number of unique Csys attributes = 0

Getting FEA coordinate systems.......
	Number of coordinate systems - 0
	No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
	Number of unique capsConstraint attributes = 1
	Name = plateEdge, index = 1
Mapping capsLoad attributes ................
	Number of unique capsLoad attributes = 1
	Name = plate, index = 1
Mapping capsBound attributes ................
	Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
	Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
	Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
	Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
	Mesh for body = 0
	Number of nodal coordinates = 25
	Number of elements = 16
	Elemental Nodes = 0
	Elemental Rods  = 0
	Elemental Tria3 = 0
	Elemental Quad4 = 16

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

Getting FEA properties.......
	Number of properties - 1
	Property name - plate
	Done getting FEA properties
Updating mesh element types based on properties input

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

Getting FEA loads.......
	Number of loads - 1
	Load name - appliedPressure
	Done getting FEA loads

Getting FEA design variables.......
	Number of design variables          - 1
	Design_Variable name - plateWidth
	Number of design variable relations - 0
	Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL

Getting FEA analyses.......
	Number of analyses - 1
	Analysis name - Default
	Done getting FEA analyses

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

Writing subElement types (if any) - appending mesh file

Writing TACS instruction file....
	Writing analysis cards
	Writing load ADD cards
	Writing constraint ADD cards
	Writing load cards
	Writing constraint cards
	Writing material cards
	Writing property cards
	Writing design variable cards
Mapping Csys attributes ................
	Number of unique Csys attributes = 0

Getting FEA coordinate systems.......
	Number of coordinate systems - 0
	No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
	Number of unique capsConstraint attributes = 1
	Name = plateEdge, index = 1
Mapping capsLoad attributes ................
	Number of unique capsLoad attributes = 1
	Name = plate, index = 1
Mapping capsBound attributes ................
	Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
	Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
	Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
	Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
	Mesh for body = 0
	Number of nodal coordinates = 25
	Number of elements = 16
	Elemental Nodes = 0
	Elemental Rods  = 0
	Elemental Tria3 = 0
	Elemental Quad4 = 16

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

Getting FEA properties.......
	Number of properties - 1
	Property name - plate
	Done getting FEA properties
Updating mesh element types based on properties input

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

Getting FEA loads.......
	Number of loads - 1
	Load name - appliedPressure
	Done getting FEA loads

Getting FEA design variables.......
	Number of design variables          - 1
	Design_Variable name - plateWidth
	Number of design variable relations - 0
	Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL

Getting FEA analyses.......
	Number of analyses - 1
	Analysis name - Default
	Done getting FEA analyses

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

Writing subElement types (if any) - appending mesh file

Writing TACS instruction file....
	Writing analysis cards
	Writing load ADD cards
	Writing constraint ADD cards
	Writing load cards
	Writing constraint cards
	Writing material cards
	Writing property cards
	Writing design variable cards
Mapping Csys attributes ................
	Number of unique Csys attributes = 0

Getting FEA coordinate systems.......
	Number of coordinate systems - 0
	No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
	Number of unique capsConstraint attributes = 1
	Name = plateEdge, index = 1
Mapping capsLoad attributes ................
	Number of unique capsLoad attributes = 1
	Name = plate, index = 1
Mapping capsBound attributes ................
	Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
	Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
	Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
	Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
	Mesh for body = 0
	Number of nodal coordinates = 25
	Number of elements = 16
	Elemental Nodes = 0
	Elemental Rods  = 0
	Elemental Tria3 = 0
	Elemental Quad4 = 16

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

Getting FEA properties.......
	Number of properties - 1
	Property name - plate
	Done getting FEA properties
Updating mesh element types based on properties input

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

Getting FEA loads.......
	Number of loads - 1
	Load name - appliedPressure
	Done getting FEA loads

Getting FEA design variables.......
	Number of design variables          - 1
	Design_Variable name - plateWidth
	Number of design variable relations - 0
	Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL

Getting FEA analyses.......
	Number of analyses - 1
	Analysis name - Default
	Done getting FEA analyses

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

Writing subElement types (if any) - appending mesh file

Writing TACS instruction file....
	Writing analysis cards
	Writing load ADD cards
	Writing constraint ADD cards
	Writing load cards
	Writing constraint cards
	Writing material cards
	Writing property cards
	Writing design variable cards
Mapping Csys attributes ................
	Number of unique Csys attributes = 0

Getting FEA coordinate systems.......
	Number of coordinate systems - 0
	No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
	Number of unique capsConstraint attributes = 1
	Name = plateEdge, index = 1
Mapping capsLoad attributes ................
	Number of unique capsLoad attributes = 1
	Name = plate, index = 1
Mapping capsBound attributes ................
	Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
	Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
	Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
	Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
	Mesh for body = 0
	Number of nodal coordinates = 25
	Number of elements = 16
	Elemental Nodes = 0
	Elemental Rods  = 0
	Elemental Tria3 = 0
	Elemental Quad4 = 16

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

Getting FEA properties.......
	Number of properties - 1
	Property name - plate
	Done getting FEA properties
Updating mesh element types based on properties input

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

Getting FEA loads.......
	Number of loads - 1
	Load name - appliedPressure
	Done getting FEA loads

Getting FEA design variables.......
	Number of design variables          - 1
	Design_Variable name - plateWidth
	Number of design variable relations - 0
	Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL

Getting FEA analyses.......
	Number of analyses - 1
	Analysis name - Default
	Done getting FEA analyses

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

Writing subElement types (if any) - appending mesh file

Writing TACS instruction file....
	Writing analysis cards
	Writing load ADD cards
	Writing constraint ADD cards
	Writing load cards
	Writing constraint cards
	Writing material cards
	Writing property cards
	Writing design variable cards
Mapping Csys attributes ................
	Number of unique Csys attributes = 0

Getting FEA coordinate systems.......
	Number of coordinate systems - 0
	No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
	Number of unique capsConstraint attributes = 1
	Name = plateEdge, index = 1
Mapping capsLoad attributes ................
	Number of unique capsLoad attributes = 1
	Name = plate, index = 1
Mapping capsBound attributes ................
	Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
	Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
	Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
	Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
	Mesh for body = 0
	Number of nodal coordinates = 25
	Number of elements = 16
	Elemental Nodes = 0
	Elemental Rods  = 0
	Elemental Tria3 = 0
	Elemental Quad4 = 16

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

Getting FEA properties.......
	Number of properties - 1
	Property name - plate
	Done getting FEA properties
Updating mesh element types based on properties input

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

Getting FEA loads.......
	Number of loads - 1
	Load name - appliedPressure
	Done getting FEA loads

Getting FEA design variables.......
	Number of design variables          - 1
	Design_Variable name - plateWidth
	Number of design variable relations - 0
	Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL

Getting FEA analyses.......
	Number of analyses - 1
	Analysis name - Default
	Done getting FEA analyses

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

Writing subElement types (if any) - appending mesh file

Writing TACS instruction file....
	Writing analysis cards
	Writing load ADD cards
	Writing constraint ADD cards
	Writing load cards
	Writing constraint cards
	Writing material cards
	Writing property cards
	Writing design variable cards
Mapping Csys attributes ................
	Number of unique Csys attributes = 0

Getting FEA coordinate systems.......
	Number of coordinate systems - 0
	No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
	Number of unique capsConstraint attributes = 1
	Name = plateEdge, index = 1
Mapping capsLoad attributes ................
	Number of unique capsLoad attributes = 1
	Name = plate, index = 1
Mapping capsBound attributes ................
	Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
	Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
	Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
	Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
	Mesh for body = 0
	Number of nodal coordinates = 25
	Number of elements = 16
	Elemental Nodes = 0
	Elemental Rods  = 0
	Elemental Tria3 = 0
	Elemental Quad4 = 16

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

Getting FEA properties.......
	Number of properties - 1
	Property name - plate
	Done getting FEA properties
Updating mesh element types based on properties input

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

Getting FEA loads.......
	Number of loads - 1
	Load name - appliedPressure
	Done getting FEA loads

Getting FEA design variables.......
	Number of design variables          - 1
	Design_Variable name - plateWidth
	Number of design variable relations - 0
	Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL

Getting FEA analyses.......
	Number of analyses - 1
	Analysis name - Default
	Done getting FEA analyses

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

Writing subElement types (if any) - appending mesh file

Writing TACS instruction file....
	Writing analysis cards
	Writing load ADD cards
	Writing constraint ADD cards
	Writing load cards
	Writing constraint cards
	Writing material cards
	Writing property cards
	Writing design variable cards
Mapping Csys attributes ................
	Number of unique Csys attributes = 0

Getting FEA coordinate systems.......
	Number of coordinate systems - 0
	No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
	Number of unique capsConstraint attributes = 1
	Name = plateEdge, index = 1
Mapping capsLoad attributes ................
	Number of unique capsLoad attributes = 1
	Name = plate, index = 1
Mapping capsBound attributes ................
	Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
	Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
	Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
	Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
	Mesh for body = 0
	Number of nodal coordinates = 25
	Number of elements = 16
	Elemental Nodes = 0
	Elemental Rods  = 0
	Elemental Tria3 = 0
	Elemental Quad4 = 16

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

Getting FEA properties.......
	Number of properties - 1
	Property name - plate
	Done getting FEA properties
Updating mesh element types based on properties input

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

Getting FEA loads.......
	Number of loads - 1
	Load name - appliedPressure
	Done getting FEA loads

Getting FEA design variables.......
	Number of design variables          - 1
	Design_Variable name - plateWidth
	Number of design variable relations - 0
	Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL

Getting FEA analyses.......
	Number of analyses - 1
	Analysis name - Default
	Done getting FEA analyses

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

Writing subElement types (if any) - appending mesh file

Writing TACS instruction file....
	Writing analysis cards
	Writing load ADD cards
	Writing constraint ADD cards
	Writing load cards
	Writing constraint cards
	Writing material cards
	Writing property cards
	Writing design variable cards
Mapping Csys attributes ................
	Number of unique Csys attributes = 0

Getting FEA coordinate systems.......
	Number of coordinate systems - 0
	No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
	Number of unique capsConstraint attributes = 1
	Name = plateEdge, index = 1
Mapping capsLoad attributes ................
	Number of unique capsLoad attributes = 1
	Name = plate, index = 1
Mapping capsBound attributes ................
	Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
	Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
	Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
	Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
	Mesh for body = 0
	Number of nodal coordinates = 25
	Number of elements = 16
	Elemental Nodes = 0
	Elemental Rods  = 0
	Elemental Tria3 = 0
	Elemental Quad4 = 16

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

Getting FEA properties.......
	Number of properties - 1
	Property name - plate
	Done getting FEA properties
Updating mesh element types based on properties input

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

Getting FEA loads.......
	Number of loads - 1
	Load name - appliedPressure
	Done getting FEA loads

Getting FEA design variables.......
	Number of design variables          - 1
	Design_Variable name - plateWidth
	Number of design variable relations - 0
	Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL

Getting FEA analyses.......
	Number of analyses - 1
	Analysis name - Default
	Done getting FEA analyses

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

Writing subElement types (if any) - appending mesh file

Writing TACS instruction file....
	Writing analysis cards
	Writing load ADD cards
	Writing constraint ADD cards
	Writing load cards
	Writing constraint cards
	Writing material cards
	Writing property cards
	Writing design variable cards
Mapping Csys attributes ................
	Number of unique Csys attributes = 0

Getting FEA coordinate systems.......
	Number of coordinate systems - 0
	No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
	Number of unique capsConstraint attributes = 1
	Name = plateEdge, index = 1
Mapping capsLoad attributes ................
	Number of unique capsLoad attributes = 1
	Name = plate, index = 1
Mapping capsBound attributes ................
	Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
	Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
	Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
	Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
	Mesh for body = 0
	Number of nodal coordinates = 25
	Number of elements = 16
	Elemental Nodes = 0
	Elemental Rods  = 0
	Elemental Tria3 = 0
	Elemental Quad4 = 16

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

Getting FEA properties.......
	Number of properties - 1
	Property name - plate
	Done getting FEA properties
Updating mesh element types based on properties input

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

Getting FEA loads.......
	Number of loads - 1
	Load name - appliedPressure
	Done getting FEA loads

Getting FEA design variables.......
	Number of design variables          - 1
	Design_Variable name - plateWidth
	Number of design variable relations - 0
	Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL

Getting FEA analyses.......
	Number of analyses - 1
	Analysis name - Default
	Done getting FEA analyses

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

Writing subElement types (if any) - appending mesh file

Writing TACS instruction file....
	Writing analysis cards
	Writing load ADD cards
	Writing constraint ADD cards
	Writing load cards
	Writing constraint cards
	Writing material cards
	Writing property cards
	Writing design variable cards
Mapping Csys attributes ................
	Number of unique Csys attributes = 0

Getting FEA coordinate systems.......
	Number of coordinate systems - 0
	No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
	Number of unique capsConstraint attributes = 1
	Name = plateEdge, index = 1
Mapping capsLoad attributes ................
	Number of unique capsLoad attributes = 1
	Name = plate, index = 1
Mapping capsBound attributes ................
	Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
	Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
	Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
	Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
	Mesh for body = 0
	Number of nodal coordinates = 25
	Number of elements = 16
	Elemental Nodes = 0
	Elemental Rods  = 0
	Elemental Tria3 = 0
	Elemental Quad4 = 16

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

Getting FEA properties.......
	Number of properties - 1
	Property name - plate
	Done getting FEA properties
Updating mesh element types based on properties input

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

Getting FEA loads.......
	Number of loads - 1
	Load name - appliedPressure
	Done getting FEA loads

Getting FEA design variables.......
	Number of design variables          - 1
	Design_Variable name - plateWidth
	Number of design variable relations - 0
	Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL

Getting FEA analyses.......
	Number of analyses - 1
	Analysis name - Default
	Done getting FEA analyses

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

Writing subElement types (if any) - appending mesh file

Writing TACS instruction file....
	Writing analysis cards
	Writing load ADD cards
	Writing constraint ADD cards
	Writing load cards
	Writing constraint cards
	Writing material cards
	Writing property cards
	Writing design variable cards
Mapping Csys attributes ................
	Number of unique Csys attributes = 0

Getting FEA coordinate systems.......
	Number of coordinate systems - 0
	No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
	Number of unique capsConstraint attributes = 1
	Name = plateEdge, index = 1
Mapping capsLoad attributes ................
	Number of unique capsLoad attributes = 1
	Name = plate, index = 1
Mapping capsBound attributes ................
	Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
	Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
	Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
	Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
	Mesh for body = 0
	Number of nodal coordinates = 25
	Number of elements = 16
	Elemental Nodes = 0
	Elemental Rods  = 0
	Elemental Tria3 = 0
	Elemental Quad4 = 16

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

Getting FEA properties.......
	Number of properties - 1
	Property name - plate
	Done getting FEA properties
Updating mesh element types based on properties input

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

Getting FEA loads.......
	Number of loads - 1
	Load name - appliedPressure
	Done getting FEA loads

Getting FEA design variables.......
	Number of design variables          - 1
	Design_Variable name - plateWidth
	Number of design variable relations - 0
	Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL

Getting FEA analyses.......
	Number of analyses - 1
	Analysis name - Default
	Done getting FEA analyses

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

Writing subElement types (if any) - appending mesh file

Writing TACS instruction file....
	Writing analysis cards
	Writing load ADD cards
	Writing constraint ADD cards
	Writing load cards
	Writing constraint cards
	Writing material cards
	Writing property cards
	Writing design variable cards
Mapping Csys attributes ................
	Number of unique Csys attributes = 0

Getting FEA coordinate systems.......
	Number of coordinate systems - 0
	No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
	Number of unique capsConstraint attributes = 1
	Name = plateEdge, index = 1
Mapping capsLoad attributes ................
	Number of unique capsLoad attributes = 1
	Name = plate, index = 1
Mapping capsBound attributes ................
	Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
	Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
	Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
	Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
	Mesh for body = 0
	Number of nodal coordinates = 25
	Number of elements = 16
	Elemental Nodes = 0
	Elemental Rods  = 0
	Elemental Tria3 = 0
	Elemental Quad4 = 16

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

Getting FEA properties.......
	Number of properties - 1
	Property name - plate
	Done getting FEA properties
Updating mesh element types based on properties input

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

Getting FEA loads.......
	Number of loads - 1
	Load name - appliedPressure
	Done getting FEA loads

Getting FEA design variables.......
	Number of design variables          - 1
	Design_Variable name - plateWidth
	Number of design variable relations - 0
	Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL

Getting FEA analyses.......
	Number of analyses - 1
	Analysis name - Default
	Done getting FEA analyses

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

Writing subElement types (if any) - appending mesh file

Writing TACS instruction file....
	Writing analysis cards
	Writing load ADD cards
	Writing constraint ADD cards
	Writing load cards
	Writing constraint cards
	Writing material cards
	Writing property cards
	Writing design variable cards
Mapping Csys attributes ................
	Number of unique Csys attributes = 0

Getting FEA coordinate systems.......
	Number of coordinate systems - 0
	No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
	Number of unique capsConstraint attributes = 1
	Name = plateEdge, index = 1
Mapping capsLoad attributes ................
	Number of unique capsLoad attributes = 1
	Name = plate, index = 1
Mapping capsBound attributes ................
	Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
	Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
	Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
	Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
	Mesh for body = 0
	Number of nodal coordinates = 25
	Number of elements = 16
	Elemental Nodes = 0
	Elemental Rods  = 0
	Elemental Tria3 = 0
	Elemental Quad4 = 16

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

Getting FEA properties.......
	Number of properties - 1
	Property name - plate
	Done getting FEA properties
Updating mesh element types based on properties input

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

Getting FEA loads.......
	Number of loads - 1
	Load name - appliedPressure
	Done getting FEA loads

Getting FEA design variables.......
	Number of design variables          - 1
	Design_Variable name - plateWidth
	Number of design variable relations - 0
	Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL

Getting FEA analyses.......
	Number of analyses - 1
	Analysis name - Default
	Done getting FEA analyses

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

Writing subElement types (if any) - appending mesh file

Writing TACS instruction file....
	Writing analysis cards
	Writing load ADD cards
	Writing constraint ADD cards
	Writing load cards
	Writing constraint cards
	Writing material cards
	Writing property cards
	Writing design variable cards
Mapping Csys attributes ................
	Number of unique Csys attributes = 0

Getting FEA coordinate systems.......
	Number of coordinate systems - 0
	No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
	Number of unique capsConstraint attributes = 1
	Name = plateEdge, index = 1
Mapping capsLoad attributes ................
	Number of unique capsLoad attributes = 1
	Name = plate, index = 1
Mapping capsBound attributes ................
	Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
	Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
	Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
	Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
	Mesh for body = 0
	Number of nodal coordinates = 25
	Number of elements = 16
	Elemental Nodes = 0
	Elemental Rods  = 0
	Elemental Tria3 = 0
	Elemental Quad4 = 16

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

Getting FEA properties.......
	Number of properties - 1
	Property name - plate
	Done getting FEA properties
Updating mesh element types based on properties input

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

Getting FEA loads.......
	Number of loads - 1
	Load name - appliedPressure
	Done getting FEA loads

Getting FEA design variables.......
	Number of design variables          - 1
	Design_Variable name - plateWidth
	Number of design variable relations - 0
	Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL

Getting FEA analyses.......
	Number of analyses - 1
	Analysis name - Default
	Done getting FEA analyses

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

Writing subElement types (if any) - appending mesh file

Writing TACS instruction file....
	Writing analysis cards
	Writing load ADD cards
	Writing constraint ADD cards
	Writing load cards
	Writing constraint cards
	Writing material cards
	Writing property cards
	Writing design variable cards
Mapping Csys attributes ................
	Number of unique Csys attributes = 0

Getting FEA coordinate systems.......
	Number of coordinate systems - 0
	No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
	Number of unique capsConstraint attributes = 1
	Name = plateEdge, index = 1
Mapping capsLoad attributes ................
	Number of unique capsLoad attributes = 1
	Name = plate, index = 1
Mapping capsBound attributes ................
	Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
	Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
	Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
	Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
	Mesh for body = 0
	Number of nodal coordinates = 25
	Number of elements = 16
	Elemental Nodes = 0
	Elemental Rods  = 0
	Elemental Tria3 = 0
	Elemental Quad4 = 16

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

Getting FEA properties.......
	Number of properties - 1
	Property name - plate
	Done getting FEA properties
Updating mesh element types based on properties input

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

Getting FEA loads.......
	Number of loads - 1
	Load name - appliedPressure
	Done getting FEA loads

Getting FEA design variables.......
	Number of design variables          - 1
	Design_Variable name - plateWidth
	Number of design variable relations - 0
	Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL

Getting FEA analyses.......
	Number of analyses - 1
	Analysis name - Default
	Done getting FEA analyses

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

Writing subElement types (if any) - appending mesh file

Writing TACS instruction file....
	Writing analysis cards
	Writing load ADD cards
	Writing constraint ADD cards
	Writing load cards
	Writing constraint cards
	Writing material cards
	Writing property cards
	Writing design variable cards
Mapping Csys attributes ................
	Number of unique Csys attributes = 0

Getting FEA coordinate systems.......
	Number of coordinate systems - 0
	No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
	Number of unique capsConstraint attributes = 1
	Name = plateEdge, index = 1
Mapping capsLoad attributes ................
	Number of unique capsLoad attributes = 1
	Name = plate, index = 1
Mapping capsBound attributes ................
	Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
	Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
	Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
	Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
	Mesh for body = 0
	Number of nodal coordinates = 25
	Number of elements = 16
	Elemental Nodes = 0
	Elemental Rods  = 0
	Elemental Tria3 = 0
	Elemental Quad4 = 16

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

Getting FEA properties.......
	Number of properties - 1
	Property name - plate
	Done getting FEA properties
Updating mesh element types based on properties input

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

Getting FEA loads.......
	Number of loads - 1
	Load name - appliedPressure
	Done getting FEA loads

Getting FEA design variables.......
	Number of design variables          - 1
	Design_Variable name - plateWidth
	Number of design variable relations - 0
	Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL

Getting FEA analyses.......
	Number of analyses - 1
	Analysis name - Default
	Done getting FEA analyses

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

Writing subElement types (if any) - appending mesh file

Writing TACS instruction file....
	Writing analysis cards
	Writing load ADD cards
	Writing constraint ADD cards
	Writing load cards
	Writing constraint cards
	Writing material cards
	Writing property cards
	Writing design variable cards
Mapping Csys attributes ................
	Number of unique Csys attributes = 0

Getting FEA coordinate systems.......
	Number of coordinate systems - 0
	No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
	Number of unique capsConstraint attributes = 1
	Name = plateEdge, index = 1
Mapping capsLoad attributes ................
	Number of unique capsLoad attributes = 1
	Name = plate, index = 1
Mapping capsBound attributes ................
	Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
	Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
	Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
	Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
	Mesh for body = 0
	Number of nodal coordinates = 25
	Number of elements = 16
	Elemental Nodes = 0
	Elemental Rods  = 0
	Elemental Tria3 = 0
	Elemental Quad4 = 16

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

Getting FEA properties.......
	Number of properties - 1
	Property name - plate
	Done getting FEA properties
Updating mesh element types based on properties input

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

Getting FEA loads.......
	Number of loads - 1
	Load name - appliedPressure
	Done getting FEA loads

Getting FEA design variables.......
	Number of design variables          - 1
	Design_Variable name - plateWidth
	Number of design variable relations - 0
	Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL

Getting FEA analyses.......
	Number of analyses - 1
	Analysis name - Default
	Done getting FEA analyses

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

Writing subElement types (if any) - appending mesh file

Writing TACS instruction file....
	Writing analysis cards
	Writing load ADD cards
	Writing constraint ADD cards
	Writing load cards
	Writing constraint cards
	Writing material cards
	Writing property cards
	Writing design variable cards
Mapping Csys attributes ................
	Number of unique Csys attributes = 0

Getting FEA coordinate systems.......
	Number of coordinate systems - 0
	No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
	Number of unique capsConstraint attributes = 1
	Name = plateEdge, index = 1
Mapping capsLoad attributes ................
	Number of unique capsLoad attributes = 1
	Name = plate, index = 1
Mapping capsBound attributes ................
	Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
	Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
	Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
	Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
	Mesh for body = 0
	Number of nodal coordinates = 25
	Number of elements = 16
	Elemental Nodes = 0
	Elemental Rods  = 0
	Elemental Tria3 = 0
	Elemental Quad4 = 16

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

Getting FEA properties.......
	Number of properties - 1
	Property name - plate
	Done getting FEA properties
Updating mesh element types based on properties input

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

Getting FEA loads.......
	Number of loads - 1
	Load name - appliedPressure
	Done getting FEA loads

Getting FEA design variables.......
	Number of design variables          - 1
	Design_Variable name - plateWidth
	Number of design variable relations - 0
	Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL

Getting FEA analyses.......
	Number of analyses - 1
	Analysis name - Default
	Done getting FEA analyses

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

Writing subElement types (if any) - appending mesh file

Writing TACS instruction file....
	Writing analysis cards
	Writing load ADD cards
	Writing constraint ADD cards
	Writing load cards
	Writing constraint cards
	Writing material cards
	Writing property cards
	Writing design variable cards
Mapping Csys attributes ................
	Number of unique Csys attributes = 0

Getting FEA coordinate systems.......
	Number of coordinate systems - 0
	No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
	Number of unique capsConstraint attributes = 1
	Name = plateEdge, index = 1
Mapping capsLoad attributes ................
	Number of unique capsLoad attributes = 1
	Name = plate, index = 1
Mapping capsBound attributes ................
	Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
	Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
	Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
	Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
	Mesh for body = 0
	Number of nodal coordinates = 25
	Number of elements = 16
	Elemental Nodes = 0
	Elemental Rods  = 0
	Elemental Tria3 = 0
	Elemental Quad4 = 16

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

Getting FEA properties.......
	Number of properties - 1
	Property name - plate
	Done getting FEA properties
Updating mesh element types based on properties input

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

Getting FEA loads.......
	Number of loads - 1
	Load name - appliedPressure
	Done getting FEA loads

Getting FEA design variables.......
	Number of design variables          - 1
	Design_Variable name - plateWidth
	Number of design variable relations - 0
	Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL

Getting FEA analyses.......
	Number of analyses - 1
	Analysis name - Default
	Done getting FEA analyses

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

Writing subElement types (if any) - appending mesh file

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

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

Getting FEA coordinate systems.......
	Number of coordinate systems - 0
	No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
	Number of unique capsConstraint attributes = 1
	Name = plateEdge, index = 1
Mapping capsLoad attributes ................
	Number of unique capsLoad attributes = 1
	Name = plate, index = 1
Mapping capsBound attributes ................
	Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
	Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
	Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
	Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = plate, index = 1
Projecting tessellation 1 (of 1) on to new body
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
	Mesh for body = 0
	Number of nodal coordinates = 25
	Number of elements = 16
	Elemental Nodes = 0
	Elemental Rods  = 0
	Elemental Tria3 = 0
	Elemental Quad4 = 16

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

Getting FEA properties.......
	Number of properties - 1
	Property name - plate
	Done getting FEA properties
Updating mesh element types based on properties input

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

Getting FEA loads.......
	Number of loads - 1
	Load name - appliedPressure
	Done getting FEA loads

Getting FEA design variables.......
	Number of design variables          - 1
	Design_Variable name - plateWidth
	Number of design variable relations - 0
	Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL

Getting FEA analyses.......
	Number of analyses - 1
	Analysis name - Default
	Done getting FEA analyses

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

Writing subElement types (if any) - appending mesh file

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

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

Getting FEA coordinate systems.......
	Number of coordinate systems - 0
	No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
	Number of unique capsConstraint attributes = 1
	Name = plateEdge, index = 1
Mapping capsLoad attributes ................
	Number of unique capsLoad attributes = 1
	Name = plate, index = 1
Mapping capsBound attributes ................
	Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
	Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
	Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
	Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
	Mesh for body = 0
	Number of nodal coordinates = 25
	Number of elements = 16
	Elemental Nodes = 0
	Elemental Rods  = 0
	Elemental Tria3 = 0
	Elemental Quad4 = 16

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

Getting FEA properties.......
	Number of properties - 1
	Property name - plate
	Done getting FEA properties
Updating mesh element types based on properties input

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

Getting FEA loads.......
	Number of loads - 1
	Load name - appliedPressure
	Done getting FEA loads

Getting FEA design variables.......
	Number of design variables          - 1
	Design_Variable name - plateWidth
	Number of design variable relations - 0
	Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL

Getting FEA analyses.......
	Number of analyses - 1
	Analysis name - Default
	Done getting FEA analyses

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

Writing subElement types (if any) - appending mesh file

Writing TACS instruction file....
	Writing analysis cards
	Writing load ADD cards
	Writing constraint ADD cards
	Writing load cards
	Writing constraint cards
	Writing material cards
	Writing property cards
	Writing design variable cards
Mapping Csys attributes ................
	Number of unique Csys attributes = 0

Getting FEA coordinate systems.......
	Number of coordinate systems - 0
	No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
	Number of unique capsConstraint attributes = 1
	Name = plateEdge, index = 1
Mapping capsLoad attributes ................
	Number of unique capsLoad attributes = 1
	Name = plate, index = 1
Mapping capsBound attributes ................
	Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
	Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
	Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
	Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
	Mesh for body = 0
	Number of nodal coordinates = 25
	Number of elements = 16
	Elemental Nodes = 0
	Elemental Rods  = 0
	Elemental Tria3 = 0
	Elemental Quad4 = 16

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

Getting FEA properties.......
	Number of properties - 1
	Property name - plate
	Done getting FEA properties
Updating mesh element types based on properties input

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

Getting FEA loads.......
	Number of loads - 1
	Load name - appliedPressure
	Done getting FEA loads

Getting FEA design variables.......
	Number of design variables          - 1
	Design_Variable name - plateWidth
	Number of design variable relations - 0
	Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL

Getting FEA analyses.......
	Number of analyses - 1
	Analysis name - Default
	Done getting FEA analyses

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

Writing subElement types (if any) - appending mesh file

Writing TACS instruction file....
	Writing analysis cards
	Writing load ADD cards
	Writing constraint ADD cards
	Writing load cards
	Writing constraint cards
	Writing material cards
	Writing property cards
	Writing design variable cards
Mapping Csys attributes ................
	Number of unique Csys attributes = 0

Getting FEA coordinate systems.......
	Number of coordinate systems - 0
	No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
	Number of unique capsConstraint attributes = 1
	Name = plateEdge, index = 1
Mapping capsLoad attributes ................
	Number of unique capsLoad attributes = 1
	Name = plate, index = 1
Mapping capsBound attributes ................
	Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
	Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
	Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
	Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
	Mesh for body = 0
	Number of nodal coordinates = 25
	Number of elements = 16
	Elemental Nodes = 0
	Elemental Rods  = 0
	Elemental Tria3 = 0
	Elemental Quad4 = 16

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

Getting FEA properties.......
	Number of properties - 1
	Property name - plate
	Done getting FEA properties
Updating mesh element types based on properties input

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

Getting FEA loads.......
	Number of loads - 1
	Load name - appliedPressure
	Done getting FEA loads

Getting FEA design variables.......
	Number of design variables          - 1
	Design_Variable name - plateWidth
	Number of design variable relations - 0
	Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL

Getting FEA analyses.......
	Number of analyses - 1
	Analysis name - Default
	Done getting FEA analyses

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

Writing subElement types (if any) - appending mesh file

Writing TACS instruction file....
	Writing analysis cards
	Writing load ADD cards
	Writing constraint ADD cards
	Writing load cards
	Writing constraint cards
	Writing material cards
	Writing property cards
	Writing design variable cards
Mapping Csys attributes ................
	Number of unique Csys attributes = 0

Getting FEA coordinate systems.......
	Number of coordinate systems - 0
	No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
	Number of unique capsConstraint attributes = 1
	Name = plateEdge, index = 1
Mapping capsLoad attributes ................
	Number of unique capsLoad attributes = 1
	Name = plate, index = 1
Mapping capsBound attributes ................
	Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
	Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
	Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
	Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
	Mesh for body = 0
	Number of nodal coordinates = 25
	Number of elements = 16
	Elemental Nodes = 0
	Elemental Rods  = 0
	Elemental Tria3 = 0
	Elemental Quad4 = 16

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

Getting FEA properties.......
	Number of properties - 1
	Property name - plate
	Done getting FEA properties
Updating mesh element types based on properties input

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

Getting FEA loads.......
	Number of loads - 1
	Load name - appliedPressure
	Done getting FEA loads

Getting FEA design variables.......
	Number of design variables          - 1
	Design_Variable name - plateWidth
	Number of design variable relations - 0
	Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL

Getting FEA analyses.......
	Number of analyses - 1
	Analysis name - Default
	Done getting FEA analyses

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

Writing subElement types (if any) - appending mesh file

Writing TACS instruction file....
	Writing analysis cards
	Writing load ADD cards
	Writing constraint ADD cards
	Writing load cards
	Writing constraint cards
	Writing material cards
	Writing property cards
	Writing design variable cards
Mapping Csys attributes ................
	Number of unique Csys attributes = 0

Getting FEA coordinate systems.......
	Number of coordinate systems - 0
	No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
	Number of unique capsConstraint attributes = 1
	Name = plateEdge, index = 1
Mapping capsLoad attributes ................
	Number of unique capsLoad attributes = 1
	Name = plate, index = 1
Mapping capsBound attributes ................
	Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
	Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
	Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
	Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
	Mesh for body = 0
	Number of nodal coordinates = 25
	Number of elements = 16
	Elemental Nodes = 0
	Elemental Rods  = 0
	Elemental Tria3 = 0
	Elemental Quad4 = 16

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

Getting FEA properties.......
	Number of properties - 1
	Property name - plate
	Done getting FEA properties
Updating mesh element types based on properties input

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

Getting FEA loads.......
	Number of loads - 1
	Load name - appliedPressure
	Done getting FEA loads

Getting FEA design variables.......
	Number of design variables          - 1
	Design_Variable name - plateWidth
	Number of design variable relations - 0
	Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL

Getting FEA analyses.......
	Number of analyses - 1
	Analysis name - Default
	Done getting FEA analyses

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

Writing subElement types (if any) - appending mesh file

Writing TACS instruction file....
	Writing analysis cards
	Writing load ADD cards
	Writing constraint ADD cards
	Writing load cards
	Writing constraint cards
	Writing material cards
	Writing property cards
	Writing design variable cards
Mapping Csys attributes ................
	Number of unique Csys attributes = 0

Getting FEA coordinate systems.......
	Number of coordinate systems - 0
	No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
	Number of unique capsConstraint attributes = 1
	Name = plateEdge, index = 1
Mapping capsLoad attributes ................
	Number of unique capsLoad attributes = 1
	Name = plate, index = 1
Mapping capsBound attributes ................
	Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
	Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
	Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
	Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
	Mesh for body = 0
	Number of nodal coordinates = 25
	Number of elements = 16
	Elemental Nodes = 0
	Elemental Rods  = 0
	Elemental Tria3 = 0
	Elemental Quad4 = 16

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

Getting FEA properties.......
	Number of properties - 1
	Property name - plate
	Done getting FEA properties
Updating mesh element types based on properties input

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

Getting FEA loads.......
	Number of loads - 1
	Load name - appliedPressure
	Done getting FEA loads

Getting FEA design variables.......
	Number of design variables          - 1
	Design_Variable name - plateWidth
	Number of design variable relations - 0
	Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL

Getting FEA analyses.......
	Number of analyses - 1
	Analysis name - Default
	Done getting FEA analyses

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

Writing subElement types (if any) - appending mesh file

Writing TACS instruction file....
	Writing analysis cards
	Writing load ADD cards
	Writing constraint ADD cards
	Writing load cards
	Writing constraint cards
	Writing material cards
	Writing property cards
	Writing design variable cards
Mapping Csys attributes ................
	Number of unique Csys attributes = 0

Getting FEA coordinate systems.......
	Number of coordinate systems - 0
	No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
	Number of unique capsConstraint attributes = 1
	Name = plateEdge, index = 1
Mapping capsLoad attributes ................
	Number of unique capsLoad attributes = 1
	Name = plate, index = 1
Mapping capsBound attributes ................
	Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
	Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
	Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
	Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
	Mesh for body = 0
	Number of nodal coordinates = 25
	Number of elements = 16
	Elemental Nodes = 0
	Elemental Rods  = 0
	Elemental Tria3 = 0
	Elemental Quad4 = 16

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

Getting FEA properties.......
	Number of properties - 1
	Property name - plate
	Done getting FEA properties
Updating mesh element types based on properties input

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

Getting FEA loads.......
	Number of loads - 1
	Load name - appliedPressure
	Done getting FEA loads

Getting FEA design variables.......
	Number of design variables          - 1
	Design_Variable name - plateWidth
	Number of design variable relations - 0
	Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL

Getting FEA analyses.......
	Number of analyses - 1
	Analysis name - Default
	Done getting FEA analyses

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

Writing subElement types (if any) - appending mesh file

Writing TACS instruction file....
	Writing analysis cards
	Writing load ADD cards
	Writing constraint ADD cards
	Writing load cards
	Writing constraint cards
	Writing material cards
	Writing property cards
	Writing design variable cards
Mapping Csys attributes ................
	Number of unique Csys attributes = 0

Getting FEA coordinate systems.......
	Number of coordinate systems - 0
	No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
	Number of unique capsConstraint attributes = 1
	Name = plateEdge, index = 1
Mapping capsLoad attributes ................
	Number of unique capsLoad attributes = 1
	Name = plate, index = 1
Mapping capsBound attributes ................
	Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
	Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
	Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
	Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
	Mesh for body = 0
	Number of nodal coordinates = 25
	Number of elements = 16
	Elemental Nodes = 0
	Elemental Rods  = 0
	Elemental Tria3 = 0
	Elemental Quad4 = 16

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

Getting FEA properties.......
	Number of properties - 1
	Property name - plate
	Done getting FEA properties
Updating mesh element types based on properties input

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

Getting FEA loads.......
	Number of loads - 1
	Load name - appliedPressure
	Done getting FEA loads

Getting FEA design variables.......
	Number of design variables          - 1
	Design_Variable name - plateWidth
	Number of design variable relations - 0
	Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL

Getting FEA analyses.......
	Number of analyses - 1
	Analysis name - Default
	Done getting FEA analyses

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

Writing subElement types (if any) - appending mesh file

Writing TACS instruction file....
	Writing analysis cards
	Writing load ADD cards
	Writing constraint ADD cards
	Writing load cards
	Writing constraint cards
	Writing material cards
	Writing property cards
	Writing design variable cards
Mapping Csys attributes ................
	Number of unique Csys attributes = 0

Getting FEA coordinate systems.......
	Number of coordinate systems - 0
	No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
	Number of unique capsConstraint attributes = 1
	Name = plateEdge, index = 1
Mapping capsLoad attributes ................
	Number of unique capsLoad attributes = 1
	Name = plate, index = 1
Mapping capsBound attributes ................
	Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
	Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
	Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
	Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
	Mesh for body = 0
	Number of nodal coordinates = 25
	Number of elements = 16
	Elemental Nodes = 0
	Elemental Rods  = 0
	Elemental Tria3 = 0
	Elemental Quad4 = 16

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

Getting FEA properties.......
	Number of properties - 1
	Property name - plate
	Done getting FEA properties
Updating mesh element types based on properties input

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

Getting FEA loads.......
	Number of loads - 1
	Load name - appliedPressure
	Done getting FEA loads

Getting FEA design variables.......
	Number of design variables          - 1
	Design_Variable name - plateWidth
	Number of design variable relations - 0
	Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL

Getting FEA analyses.......
	Number of analyses - 1
	Analysis name - Default
	Done getting FEA analyses

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

Writing subElement types (if any) - appending mesh file

Writing TACS instruction file....
	Writing analysis cards
	Writing load ADD cards
	Writing constraint ADD cards
	Writing load cards
	Writing constraint cards
	Writing material cards
	Writing property cards
	Writing design variable cards
Mapping Csys attributes ................
	Number of unique Csys attributes = 0

Getting FEA coordinate systems.......
	Number of coordinate systems - 0
	No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
	Number of unique capsConstraint attributes = 1
	Name = plateEdge, index = 1
Mapping capsLoad attributes ................
	Number of unique capsLoad attributes = 1
	Name = plate, index = 1
Mapping capsBound attributes ................
	Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
	Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
	Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
	Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
	Mesh for body = 0
	Number of nodal coordinates = 25
	Number of elements = 16
	Elemental Nodes = 0
	Elemental Rods  = 0
	Elemental Tria3 = 0
	Elemental Quad4 = 16

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

Getting FEA properties.......
	Number of properties - 1
	Property name - plate
	Done getting FEA properties
Updating mesh element types based on properties input

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

Getting FEA loads.......
	Number of loads - 1
	Load name - appliedPressure
	Done getting FEA loads

Getting FEA design variables.......
	Number of design variables          - 1
	Design_Variable name - plateWidth
	Number of design variable relations - 0
	Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL

Getting FEA analyses.......
	Number of analyses - 1
	Analysis name - Default
	Done getting FEA analyses

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

Writing subElement types (if any) - appending mesh file

Writing TACS instruction file....
	Writing analysis cards
	Writing load ADD cards
	Writing constraint ADD cards
	Writing load cards
	Writing constraint cards
	Writing material cards
	Writing property cards
	Writing design variable cards
Mapping Csys attributes ................
	Number of unique Csys attributes = 0

Getting FEA coordinate systems.......
	Number of coordinate systems - 0
	No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
	Number of unique capsConstraint attributes = 1
	Name = plateEdge, index = 1
Mapping capsLoad attributes ................
	Number of unique capsLoad attributes = 1
	Name = plate, index = 1
Mapping capsBound attributes ................
	Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
	Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
	Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
	Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
	Mesh for body = 0
	Number of nodal coordinates = 25
	Number of elements = 16
	Elemental Nodes = 0
	Elemental Rods  = 0
	Elemental Tria3 = 0
	Elemental Quad4 = 16

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

Getting FEA properties.......
	Number of properties - 1
	Property name - plate
	Done getting FEA properties
Updating mesh element types based on properties input

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

Getting FEA loads.......
	Number of loads - 1
	Load name - appliedPressure
	Done getting FEA loads

Getting FEA design variables.......
	Number of design variables          - 1
	Design_Variable name - plateWidth
	Number of design variable relations - 0
	Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL

Getting FEA analyses.......
	Number of analyses - 1
	Analysis name - Default
	Done getting FEA analyses

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

Writing subElement types (if any) - appending mesh file

Writing TACS instruction file....
	Writing analysis cards
	Writing load ADD cards
	Writing constraint ADD cards
	Writing load cards
	Writing constraint cards
	Writing material cards
	Writing property cards
	Writing design variable cards
Mapping Csys attributes ................
	Number of unique Csys attributes = 0

Getting FEA coordinate systems.......
	Number of coordinate systems - 0
	No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
	Number of unique capsConstraint attributes = 1
	Name = plateEdge, index = 1
Mapping capsLoad attributes ................
	Number of unique capsLoad attributes = 1
	Name = plate, index = 1
Mapping capsBound attributes ................
	Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
	Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
	Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
	Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
	Mesh for body = 0
	Number of nodal coordinates = 25
	Number of elements = 16
	Elemental Nodes = 0
	Elemental Rods  = 0
	Elemental Tria3 = 0
	Elemental Quad4 = 16

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

Getting FEA properties.......
	Number of properties - 1
	Property name - plate
	Done getting FEA properties
Updating mesh element types based on properties input

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

Getting FEA loads.......
	Number of loads - 1
	Load name - appliedPressure
	Done getting FEA loads

Getting FEA design variables.......
	Number of design variables          - 1
	Design_Variable name - plateWidth
	Number of design variable relations - 0
	Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL

Getting FEA analyses.......
	Number of analyses - 1
	Analysis name - Default
	Done getting FEA analyses

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

Writing subElement types (if any) - appending mesh file

Writing TACS instruction file....
	Writing analysis cards
	Writing load ADD cards
	Writing constraint ADD cards
	Writing load cards
	Writing constraint cards
	Writing material cards
	Writing property cards
	Writing design variable cards
Mapping Csys attributes ................
	Number of unique Csys attributes = 0

Getting FEA coordinate systems.......
	Number of coordinate systems - 0
	No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
	Number of unique capsConstraint attributes = 1
	Name = plateEdge, index = 1
Mapping capsLoad attributes ................
	Number of unique capsLoad attributes = 1
	Name = plate, index = 1
Mapping capsBound attributes ................
	Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
	Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
	Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
	Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
	Mesh for body = 0
	Number of nodal coordinates = 25
	Number of elements = 16
	Elemental Nodes = 0
	Elemental Rods  = 0
	Elemental Tria3 = 0
	Elemental Quad4 = 16

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

Getting FEA properties.......
	Number of properties - 1
	Property name - plate
	Done getting FEA properties
Updating mesh element types based on properties input

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

Getting FEA loads.......
	Number of loads - 1
	Load name - appliedPressure
	Done getting FEA loads

Getting FEA design variables.......
	Number of design variables          - 1
	Design_Variable name - plateWidth
	Number of design variable relations - 0
	Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL

Getting FEA analyses.......
	Number of analyses - 1
	Analysis name - Default
	Done getting FEA analyses

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

Writing subElement types (if any) - appending mesh file

Writing TACS instruction file....
	Writing analysis cards
	Writing load ADD cards
	Writing constraint ADD cards
	Writing load cards
	Writing constraint cards
	Writing material cards
	Writing property cards
	Writing design variable cards
Mapping Csys attributes ................
	Number of unique Csys attributes = 0

Getting FEA coordinate systems.......
	Number of coordinate systems - 0
	No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
	Number of unique capsConstraint attributes = 1
	Name = plateEdge, index = 1
Mapping capsLoad attributes ................
	Number of unique capsLoad attributes = 1
	Name = plate, index = 1
Mapping capsBound attributes ................
	Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
	Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
	Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
	Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
	Mesh for body = 0
	Number of nodal coordinates = 25
	Number of elements = 16
	Elemental Nodes = 0
	Elemental Rods  = 0
	Elemental Tria3 = 0
	Elemental Quad4 = 16

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

Getting FEA properties.......
	Number of properties - 1
	Property name - plate
	Done getting FEA properties
Updating mesh element types based on properties input

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

Getting FEA loads.......
	Number of loads - 1
	Load name - appliedPressure
	Done getting FEA loads

Getting FEA design variables.......
	Number of design variables          - 1
	Design_Variable name - plateWidth
	Number of design variable relations - 0
	Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL

Getting FEA analyses.......
	Number of analyses - 1
	Analysis name - Default
	Done getting FEA analyses

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

Writing subElement types (if any) - appending mesh file

Writing TACS instruction file....
	Writing analysis cards
	Writing load ADD cards
	Writing constraint ADD cards
	Writing load cards
	Writing constraint cards
	Writing material cards
	Writing property cards
	Writing design variable cards
Mapping Csys attributes ................
	Number of unique Csys attributes = 0

Getting FEA coordinate systems.......
	Number of coordinate systems - 0
	No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
	Number of unique capsConstraint attributes = 1
	Name = plateEdge, index = 1
Mapping capsLoad attributes ................
	Number of unique capsLoad attributes = 1
	Name = plate, index = 1
Mapping capsBound attributes ................
	Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
	Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
	Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
	Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
	Mesh for body = 0
	Number of nodal coordinates = 25
	Number of elements = 16
	Elemental Nodes = 0
	Elemental Rods  = 0
	Elemental Tria3 = 0
	Elemental Quad4 = 16

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

Getting FEA properties.......
	Number of properties - 1
	Property name - plate
	Done getting FEA properties
Updating mesh element types based on properties input

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

Getting FEA loads.......
	Number of loads - 1
	Load name - appliedPressure
	Done getting FEA loads

Getting FEA design variables.......
	Number of design variables          - 1
	Design_Variable name - plateWidth
	Number of design variable relations - 0
	Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL

Getting FEA analyses.......
	Number of analyses - 1
	Analysis name - Default
	Done getting FEA analyses

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

Writing subElement types (if any) - appending mesh file

Writing TACS instruction file....
	Writing analysis cards
	Writing load ADD cards
	Writing constraint ADD cards
	Writing load cards
	Writing constraint cards
	Writing material cards
	Writing property cards
	Writing design variable cards
Mapping Csys attributes ................
	Number of unique Csys attributes = 0

Getting FEA coordinate systems.......
	Number of coordinate systems - 0
	No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
	Number of unique capsConstraint attributes = 1
	Name = plateEdge, index = 1
Mapping capsLoad attributes ................
	Number of unique capsLoad attributes = 1
	Name = plate, index = 1
Mapping capsBound attributes ................
	Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
	Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
	Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
	Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
	Mesh for body = 0
	Number of nodal coordinates = 25
	Number of elements = 16
	Elemental Nodes = 0
	Elemental Rods  = 0
	Elemental Tria3 = 0
	Elemental Quad4 = 16

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

Getting FEA properties.......
	Number of properties - 1
	Property name - plate
	Done getting FEA properties
Updating mesh element types based on properties input

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

Getting FEA loads.......
	Number of loads - 1
	Load name - appliedPressure
	Done getting FEA loads

Getting FEA design variables.......
	Number of design variables          - 1
	Design_Variable name - plateWidth
	Number of design variable relations - 0
	Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL

Getting FEA analyses.......
	Number of analyses - 1
	Analysis name - Default
	Done getting FEA analyses

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

Writing subElement types (if any) - appending mesh file

Writing TACS instruction file....
	Writing analysis cards
	Writing load ADD cards
	Writing constraint ADD cards
	Writing load cards
	Writing constraint cards
	Writing material cards
	Writing property cards
	Writing design variable cards
Mapping Csys attributes ................
	Number of unique Csys attributes = 0

Getting FEA coordinate systems.......
	Number of coordinate systems - 0
	No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
	Number of unique capsConstraint attributes = 1
	Name = plateEdge, index = 1
Mapping capsLoad attributes ................
	Number of unique capsLoad attributes = 1
	Name = plate, index = 1
Mapping capsBound attributes ................
	Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
	Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
	Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
	Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
	Mesh for body = 0
	Number of nodal coordinates = 25
	Number of elements = 16
	Elemental Nodes = 0
	Elemental Rods  = 0
	Elemental Tria3 = 0
	Elemental Quad4 = 16

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

Getting FEA properties.......
	Number of properties - 1
	Property name - plate
	Done getting FEA properties
Updating mesh element types based on properties input

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

Getting FEA loads.......
	Number of loads - 1
	Load name - appliedPressure
	Done getting FEA loads

Getting FEA design variables.......
	Number of design variables          - 1
	Design_Variable name - plateWidth
	Number of design variable relations - 0
	Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL

Getting FEA analyses.......
	Number of analyses - 1
	Analysis name - Default
	Done getting FEA analyses

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

Writing subElement types (if any) - appending mesh file

Writing TACS instruction file....
	Writing analysis cards
	Writing load ADD cards
	Writing constraint ADD cards
	Writing load cards
	Writing constraint cards
	Writing material cards
	Writing property cards
	Writing design variable cards
Mapping Csys attributes ................
	Number of unique Csys attributes = 0

Getting FEA coordinate systems.......
	Number of coordinate systems - 0
	No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
	Number of unique capsConstraint attributes = 1
	Name = plateEdge, index = 1
Mapping capsLoad attributes ................
	Number of unique capsLoad attributes = 1
	Name = plate, index = 1
Mapping capsBound attributes ................
	Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
	Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
	Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
	Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
	Mesh for body = 0
	Number of nodal coordinates = 25
	Number of elements = 16
	Elemental Nodes = 0
	Elemental Rods  = 0
	Elemental Tria3 = 0
	Elemental Quad4 = 16

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

Getting FEA properties.......
	Number of properties - 1
	Property name - plate
	Done getting FEA properties
Updating mesh element types based on properties input

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

Getting FEA loads.......
	Number of loads - 1
	Load name - appliedPressure
	Done getting FEA loads

Getting FEA design variables.......
	Number of design variables          - 1
	Design_Variable name - plateWidth
	Number of design variable relations - 0
	Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL

Getting FEA analyses.......
	Number of analyses - 1
	Analysis name - Default
	Done getting FEA analyses

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

Writing subElement types (if any) - appending mesh file

Writing TACS instruction file....
	Writing analysis cards
	Writing load ADD cards
	Writing constraint ADD cards
	Writing load cards
	Writing constraint cards
	Writing material cards
	Writing property cards
	Writing design variable cards
Mapping Csys attributes ................
	Number of unique Csys attributes = 0

Getting FEA coordinate systems.......
	Number of coordinate systems - 0
	No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
	Number of unique capsConstraint attributes = 1
	Name = plateEdge, index = 1
Mapping capsLoad attributes ................
	Number of unique capsLoad attributes = 1
	Name = plate, index = 1
Mapping capsBound attributes ................
	Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
	Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
	Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
	Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
	Mesh for body = 0
	Number of nodal coordinates = 25
	Number of elements = 16
	Elemental Nodes = 0
	Elemental Rods  = 0
	Elemental Tria3 = 0
	Elemental Quad4 = 16

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

Getting FEA properties.......
	Number of properties - 1
	Property name - plate
	Done getting FEA properties
Updating mesh element types based on properties input

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

Getting FEA loads.......
	Number of loads - 1
	Load name - appliedPressure
	Done getting FEA loads

Getting FEA design variables.......
	Number of design variables          - 1
	Design_Variable name - plateWidth
	Number of design variable relations - 0
	Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL

Getting FEA analyses.......
	Number of analyses - 1
	Analysis name - Default
	Done getting FEA analyses

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

Writing subElement types (if any) - appending mesh file

Writing TACS instruction file....
	Writing analysis cards
	Writing load ADD cards
	Writing constraint ADD cards
	Writing load cards
	Writing constraint cards
	Writing material cards
	Writing property cards
	Writing design variable cards
Mapping Csys attributes ................
	Number of unique Csys attributes = 0

Getting FEA coordinate systems.......
	Number of coordinate systems - 0
	No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
	Number of unique capsConstraint attributes = 1
	Name = plateEdge, index = 1
Mapping capsLoad attributes ................
	Number of unique capsLoad attributes = 1
	Name = plate, index = 1
Mapping capsBound attributes ................
	Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
	Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
	Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
	Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
	Mesh for body = 0
	Number of nodal coordinates = 25
	Number of elements = 16
	Elemental Nodes = 0
	Elemental Rods  = 0
	Elemental Tria3 = 0
	Elemental Quad4 = 16

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

Getting FEA properties.......
	Number of properties - 1
	Property name - plate
	Done getting FEA properties
Updating mesh element types based on properties input

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

Getting FEA loads.......
	Number of loads - 1
	Load name - appliedPressure
	Done getting FEA loads

Getting FEA design variables.......
	Number of design variables          - 1
	Design_Variable name - plateWidth
	Number of design variable relations - 0
	Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL

Getting FEA analyses.......
	Number of analyses - 1
	Analysis name - Default
	Done getting FEA analyses

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

Writing subElement types (if any) - appending mesh file

Writing TACS instruction file....
	Writing analysis cards
	Writing load ADD cards
	Writing constraint ADD cards
	Writing load cards
	Writing constraint cards
	Writing material cards
	Writing property cards
	Writing design variable cards
Mapping Csys attributes ................
	Number of unique Csys attributes = 0

Getting FEA coordinate systems.......
	Number of coordinate systems - 0
	No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
	Number of unique capsConstraint attributes = 1
	Name = plateEdge, index = 1
Mapping capsLoad attributes ................
	Number of unique capsLoad attributes = 1
	Name = plate, index = 1
Mapping capsBound attributes ................
	Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
	Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
	Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
	Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
	Mesh for body = 0
	Number of nodal coordinates = 25
	Number of elements = 16
	Elemental Nodes = 0
	Elemental Rods  = 0
	Elemental Tria3 = 0
	Elemental Quad4 = 16

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

Getting FEA properties.......
	Number of properties - 1
	Property name - plate
	Done getting FEA properties
Updating mesh element types based on properties input

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

Getting FEA loads.......
	Number of loads - 1
	Load name - appliedPressure
	Done getting FEA loads

Getting FEA design variables.......
	Number of design variables          - 1
	Design_Variable name - plateWidth
	Number of design variable relations - 0
	Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL

Getting FEA analyses.......
	Number of analyses - 1
	Analysis name - Default
	Done getting FEA analyses

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

Writing subElement types (if any) - appending mesh file

Writing TACS instruction file....
	Writing analysis cards
	Writing load ADD cards
	Writing constraint ADD cards
	Writing load cards
	Writing constraint cards
	Writing material cards
	Writing property cards
	Writing design variable cards
Mapping Csys attributes ................
	Number of unique Csys attributes = 0

Getting FEA coordinate systems.......
	Number of coordinate systems - 0
	No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
	Number of unique capsConstraint attributes = 1
	Name = plateEdge, index = 1
Mapping capsLoad attributes ................
	Number of unique capsLoad attributes = 1
	Name = plate, index = 1
Mapping capsBound attributes ................
	Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
	Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
	Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
	Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
	Mesh for body = 0
	Number of nodal coordinates = 25
	Number of elements = 16
	Elemental Nodes = 0
	Elemental Rods  = 0
	Elemental Tria3 = 0
	Elemental Quad4 = 16

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

Getting FEA properties.......
	Number of properties - 1
	Property name - plate
	Done getting FEA properties
Updating mesh element types based on properties input

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

Getting FEA loads.......
	Number of loads - 1
	Load name - appliedPressure
	Done getting FEA loads

Getting FEA design variables.......
	Number of design variables          - 1
	Design_Variable name - plateWidth
	Number of design variable relations - 0
	Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL

Getting FEA analyses.......
	Number of analyses - 1
	Analysis name - Default
	Done getting FEA analyses

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

Writing subElement types (if any) - appending mesh file

Writing TACS instruction file....
	Writing analysis cards
	Writing load ADD cards
	Writing constraint ADD cards
	Writing load cards
	Writing constraint cards
	Writing material cards
	Writing property cards
	Writing design variable cards
Mapping Csys attributes ................
	Number of unique Csys attributes = 0

Getting FEA coordinate systems.......
	Number of coordinate systems - 0
	No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
	Number of unique capsConstraint attributes = 1
	Name = plateEdge, index = 1
Mapping capsLoad attributes ................
	Number of unique capsLoad attributes = 1
	Name = plate, index = 1
Mapping capsBound attributes ................
	Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
	Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
	Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
	Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
	Mesh for body = 0
	Number of nodal coordinates = 25
	Number of elements = 16
	Elemental Nodes = 0
	Elemental Rods  = 0
	Elemental Tria3 = 0
	Elemental Quad4 = 16

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

Getting FEA properties.......
	Number of properties - 1
	Property name - plate
	Done getting FEA properties
Updating mesh element types based on properties input

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

Getting FEA loads.......
	Number of loads - 1
	Load name - appliedPressure
	Done getting FEA loads

Getting FEA design variables.......
	Number of design variables          - 1
	Design_Variable name - plateWidth
	Number of design variable relations - 0
	Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL

Getting FEA analyses.......
	Number of analyses - 1
	Analysis name - Default
	Done getting FEA analyses

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

Writing subElement types (if any) - appending mesh file

Writing TACS instruction file....
	Writing analysis cards
	Writing load ADD cards
	Writing constraint ADD cards
	Writing load cards
	Writing constraint cards
	Writing material cards
	Writing property cards
	Writing design variable cards
Mapping Csys attributes ................
	Number of unique Csys attributes = 0

Getting FEA coordinate systems.......
	Number of coordinate systems - 0
	No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
	Number of unique capsConstraint attributes = 1
	Name = plateEdge, index = 1
Mapping capsLoad attributes ................
	Number of unique capsLoad attributes = 1
	Name = plate, index = 1
Mapping capsBound attributes ................
	Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
	Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
	Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
	Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
	Mesh for body = 0
	Number of nodal coordinates = 25
	Number of elements = 16
	Elemental Nodes = 0
	Elemental Rods  = 0
	Elemental Tria3 = 0
	Elemental Quad4 = 16

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

Getting FEA properties.......
	Number of properties - 1
	Property name - plate
	Done getting FEA properties
Updating mesh element types based on properties input

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

Getting FEA loads.......
	Number of loads - 1
	Load name - appliedPressure
	Done getting FEA loads

Getting FEA design variables.......
	Number of design variables          - 1
	Design_Variable name - plateWidth
	Number of design variable relations - 0
	Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL

Getting FEA analyses.......
	Number of analyses - 1
	Analysis name - Default
	Done getting FEA analyses

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

Writing subElement types (if any) - appending mesh file

Writing TACS instruction file....
	Writing analysis cards
	Writing load ADD cards
	Writing constraint ADD cards
	Writing load cards
	Writing constraint cards
	Writing material cards
	Writing property cards
	Writing design variable cards
Mapping Csys attributes ................
	Number of unique Csys attributes = 0

Getting FEA coordinate systems.......
	Number of coordinate systems - 0
	No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
	Number of unique capsConstraint attributes = 1
	Name = plateEdge, index = 1
Mapping capsLoad attributes ................
	Number of unique capsLoad attributes = 1
	Name = plate, index = 1
Mapping capsBound attributes ................
	Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
	Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
	Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
	Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
	Mesh for body = 0
	Number of nodal coordinates = 25
	Number of elements = 16
	Elemental Nodes = 0
	Elemental Rods  = 0
	Elemental Tria3 = 0
	Elemental Quad4 = 16

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

Getting FEA properties.......
	Number of properties - 1
	Property name - plate
	Done getting FEA properties
Updating mesh element types based on properties input

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

Getting FEA loads.......
	Number of loads - 1
	Load name - appliedPressure
	Done getting FEA loads

Getting FEA design variables.......
	Number of design variables          - 1
	Design_Variable name - thick1
	Design_Variable_Relation name - thick1
	Number of design variable relations - 1
	Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL

Getting FEA analyses.......
	Number of analyses - 1
	Analysis name - Default
	Done getting FEA analyses

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

Writing subElement types (if any) - appending mesh file

Writing TACS instruction file....
	Writing analysis cards
	Writing load ADD cards
	Writing constraint ADD cards
	Writing load cards
	Writing constraint cards
	Writing material cards
	Writing property cards
	Writing design variable cards
	Writing design variable relation cards
Mapping Csys attributes ................
	Number of unique Csys attributes = 0

Getting FEA coordinate systems.......
	Number of coordinate systems - 0
	No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
	Number of unique capsConstraint attributes = 1
	Name = plateEdge, index = 1
Mapping capsLoad attributes ................
	Number of unique capsLoad attributes = 1
	Name = plate, index = 1
Mapping capsBound attributes ................
	Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
	Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
	Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
	Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
	Mesh for body = 0
	Number of nodal coordinates = 25
	Number of elements = 16
	Elemental Nodes = 0
	Elemental Rods  = 0
	Elemental Tria3 = 0
	Elemental Quad4 = 16

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

Getting FEA properties.......
	Number of properties - 1
	Property name - plate
	Done getting FEA properties
Updating mesh element types based on properties input

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

Getting FEA loads.......
	Number of loads - 1
	Load name - appliedPressure
	Done getting FEA loads

Getting FEA design variables.......
	Number of design variables          - 1
	Design_Variable name - thick1
	Design_Variable_Relation name - thick1
	Number of design variable relations - 1
	Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL

Getting FEA analyses.......
	Number of analyses - 1
	Analysis name - Default
	Done getting FEA analyses

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

Writing subElement types (if any) - appending mesh file

Writing TACS instruction file....
	Writing analysis cards
	Writing load ADD cards
	Writing constraint ADD cards
	Writing load cards
	Writing constraint cards
	Writing material cards
	Writing property cards
	Writing design variable cards
	Writing design variable relation cards
Mapping Csys attributes ................
	Number of unique Csys attributes = 0

Getting FEA coordinate systems.......
	Number of coordinate systems - 0
	No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
	Number of unique capsConstraint attributes = 1
	Name = plateEdge, index = 1
Mapping capsLoad attributes ................
	Number of unique capsLoad attributes = 1
	Name = plate, index = 1
Mapping capsBound attributes ................
	Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
	Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
	Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
	Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
	Mesh for body = 0
	Number of nodal coordinates = 25
	Number of elements = 16
	Elemental Nodes = 0
	Elemental Rods  = 0
	Elemental Tria3 = 0
	Elemental Quad4 = 16

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

Getting FEA properties.......
	Number of properties - 1
	Property name - plate
	Done getting FEA properties
Updating mesh element types based on properties input

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

Getting FEA loads.......
	Number of loads - 1
	Load name - appliedPressure
	Done getting FEA loads

Getting FEA design variables.......
	Number of design variables          - 1
	Design_Variable name - thick1
	Design_Variable_Relation name - thick1
	Number of design variable relations - 1
	Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL

Getting FEA analyses.......
	Number of analyses - 1
	Analysis name - Default
	Done getting FEA analyses

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

Writing subElement types (if any) - appending mesh file

Writing TACS instruction file....
	Writing analysis cards
	Writing load ADD cards
	Writing constraint ADD cards
	Writing load cards
	Writing constraint cards
	Writing material cards
	Writing property cards
	Writing design variable cards
	Writing design variable relation cards
Mapping Csys attributes ................
	Number of unique Csys attributes = 0

Getting FEA coordinate systems.......
	Number of coordinate systems - 0
	No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
	Number of unique capsConstraint attributes = 1
	Name = plateEdge, index = 1
Mapping capsLoad attributes ................
	Number of unique capsLoad attributes = 1
	Name = plate, index = 1
Mapping capsBound attributes ................
	Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
	Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
	Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
	Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
	Mesh for body = 0
	Number of nodal coordinates = 25
	Number of elements = 16
	Elemental Nodes = 0
	Elemental Rods  = 0
	Elemental Tria3 = 0
	Elemental Quad4 = 16

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

Getting FEA properties.......
	Number of properties - 1
	Property name - plate
	Done getting FEA properties
Updating mesh element types based on properties input

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

Getting FEA loads.......
	Number of loads - 1
	Load name - appliedPressure
	Done getting FEA loads

Getting FEA design variables.......
	Number of design variables          - 1
	Design_Variable name - thick1
	Design_Variable_Relation name - thick1
	Number of design variable relations - 1
	Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL

Getting FEA analyses.......
	Number of analyses - 1
	Analysis name - Default
	Done getting FEA analyses

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

Writing subElement types (if any) - appending mesh file

Writing TACS instruction file....
	Writing analysis cards
	Writing load ADD cards
	Writing constraint ADD cards
	Writing load cards
	Writing constraint cards
	Writing material cards
	Writing property cards
	Writing design variable cards
	Writing design variable relation cards
Mapping Csys attributes ................
	Number of unique Csys attributes = 0

Getting FEA coordinate systems.......
	Number of coordinate systems - 0
	No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
	Number of unique capsConstraint attributes = 1
	Name = plateEdge, index = 1
Mapping capsLoad attributes ................
	Number of unique capsLoad attributes = 1
	Name = plate, index = 1
Mapping capsBound attributes ................
	Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
	Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
	Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
	Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
	Mesh for body = 0
	Number of nodal coordinates = 25
	Number of elements = 16
	Elemental Nodes = 0
	Elemental Rods  = 0
	Elemental Tria3 = 0
	Elemental Quad4 = 16

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

Getting FEA properties.......
	Number of properties - 1
	Property name - plate
	Done getting FEA properties
Updating mesh element types based on properties input

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

Getting FEA loads.......
	Number of loads - 1
	Load name - appliedPressure
	Done getting FEA loads

Getting FEA design variables.......
	Number of design variables          - 1
	Design_Variable name - thick1
	Design_Variable_Relation name - thick1
	Number of design variable relations - 1
	Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL

Getting FEA analyses.......
	Number of analyses - 1
	Analysis name - Default
	Done getting FEA analyses

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

Writing subElement types (if any) - appending mesh file

Writing TACS instruction file....
	Writing analysis cards
	Writing load ADD cards
	Writing constraint ADD cards
	Writing load cards
	Writing constraint cards
	Writing material cards
	Writing property cards
	Writing design variable cards
	Writing design variable relation cards
Mapping Csys attributes ................
	Number of unique Csys attributes = 0

Getting FEA coordinate systems.......
	Number of coordinate systems - 0
	No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
	Number of unique capsConstraint attributes = 1
	Name = plateEdge, index = 1
Mapping capsLoad attributes ................
	Number of unique capsLoad attributes = 1
	Name = plate, index = 1
Mapping capsBound attributes ................
	Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
	Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
	Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
	Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
	Mesh for body = 0
	Number of nodal coordinates = 25
	Number of elements = 16
	Elemental Nodes = 0
	Elemental Rods  = 0
	Elemental Tria3 = 0
	Elemental Quad4 = 16

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

Getting FEA properties.......
	Number of properties - 1
	Property name - plate
	Done getting FEA properties
Updating mesh element types based on properties input

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

Getting FEA loads.......
	Number of loads - 1
	Load name - appliedPressure
	Done getting FEA loads

Getting FEA design variables.......
	Number of design variables          - 1
	Design_Variable name - thick1
	Design_Variable_Relation name - thick1
	Number of design variable relations - 1
	Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL

Getting FEA analyses.......
	Number of analyses - 1
	Analysis name - Default
	Done getting FEA analyses

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

Writing subElement types (if any) - appending mesh file

Writing TACS instruction file....
	Writing analysis cards
	Writing load ADD cards
	Writing constraint ADD cards
	Writing load cards
	Writing constraint cards
	Writing material cards
	Writing property cards
	Writing design variable cards
	Writing design variable relation cards
Mapping Csys attributes ................
	Number of unique Csys attributes = 0

Getting FEA coordinate systems.......
	Number of coordinate systems - 0
	No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
	Number of unique capsConstraint attributes = 1
	Name = plateEdge, index = 1
Mapping capsLoad attributes ................
	Number of unique capsLoad attributes = 1
	Name = plate, index = 1
Mapping capsBound attributes ................
	Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
	Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
	Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
	Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
	Mesh for body = 0
	Number of nodal coordinates = 25
	Number of elements = 16
	Elemental Nodes = 0
	Elemental Rods  = 0
	Elemental Tria3 = 0
	Elemental Quad4 = 16

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

Getting FEA properties.......
	Number of properties - 1
	Property name - plate
	Done getting FEA properties
Updating mesh element types based on properties input

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

Getting FEA loads.......
	Number of loads - 1
	Load name - appliedPressure
	Done getting FEA loads

Getting FEA design variables.......
	Number of design variables          - 1
	Design_Variable name - thick1
	Design_Variable_Relation name - thick1
	Number of design variable relations - 1
	Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL

Getting FEA analyses.......
	Number of analyses - 1
	Analysis name - Default
	Done getting FEA analyses

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

Writing subElement types (if any) - appending mesh file

Writing TACS instruction file....
	Writing analysis cards
	Writing load ADD cards
	Writing constraint ADD cards
	Writing load cards
	Writing constraint cards
	Writing material cards
	Writing property cards
	Writing design variable cards
	Writing design variable relation cards
Mapping Csys attributes ................
	Number of unique Csys attributes = 0

Getting FEA coordinate systems.......
	Number of coordinate systems - 0
	No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
	Number of unique capsConstraint attributes = 1
	Name = plateEdge, index = 1
Mapping capsLoad attributes ................
	Number of unique capsLoad attributes = 1
	Name = plate, index = 1
Mapping capsBound attributes ................
	Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
	Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
	Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
	Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
	Mesh for body = 0
	Number of nodal coordinates = 25
	Number of elements = 16
	Elemental Nodes = 0
	Elemental Rods  = 0
	Elemental Tria3 = 0
	Elemental Quad4 = 16

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

Getting FEA properties.......
	Number of properties - 1
	Property name - plate
	Done getting FEA properties
Updating mesh element types based on properties input

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

Getting FEA loads.......
	Number of loads - 1
	Load name - appliedPressure
	Done getting FEA loads

Getting FEA design variables.......
	Number of design variables          - 1
	Design_Variable name - thick1
	Design_Variable_Relation name - thick1
	Number of design variable relations - 1
	Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL

Getting FEA analyses.......
	Number of analyses - 1
	Analysis name - Default
	Done getting FEA analyses

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

Writing subElement types (if any) - appending mesh file

Writing TACS instruction file....
	Writing analysis cards
	Writing load ADD cards
	Writing constraint ADD cards
	Writing load cards
	Writing constraint cards
	Writing material cards
	Writing property cards
	Writing design variable cards
	Writing design variable relation cards
Mapping Csys attributes ................
	Number of unique Csys attributes = 0

Getting FEA coordinate systems.......
	Number of coordinate systems - 0
	No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
	Number of unique capsConstraint attributes = 1
	Name = plateEdge, index = 1
Mapping capsLoad attributes ................
	Number of unique capsLoad attributes = 1
	Name = plate, index = 1
Mapping capsBound attributes ................
	Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
	Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
	Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
	Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
	Mesh for body = 0
	Number of nodal coordinates = 25
	Number of elements = 16
	Elemental Nodes = 0
	Elemental Rods  = 0
	Elemental Tria3 = 0
	Elemental Quad4 = 16

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

Getting FEA properties.......
	Number of properties - 1
	Property name - plate
	Done getting FEA properties
Updating mesh element types based on properties input

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

Getting FEA loads.......
	Number of loads - 1
	Load name - appliedPressure
	Done getting FEA loads

Getting FEA design variables.......
	Number of design variables          - 1
	Design_Variable name - thick1
	Design_Variable_Relation name - thick1
	Number of design variable relations - 1
	Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL

Getting FEA analyses.......
	Number of analyses - 1
	Analysis name - Default
	Done getting FEA analyses

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

Writing subElement types (if any) - appending mesh file

Writing TACS instruction file....
	Writing analysis cards
	Writing load ADD cards
	Writing constraint ADD cards
	Writing load cards
	Writing constraint cards
	Writing material cards
	Writing property cards
	Writing design variable cards
	Writing design variable relation cards
Mapping Csys attributes ................
	Number of unique Csys attributes = 0

Getting FEA coordinate systems.......
	Number of coordinate systems - 0
	No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
	Number of unique capsConstraint attributes = 1
	Name = plateEdge, index = 1
Mapping capsLoad attributes ................
	Number of unique capsLoad attributes = 1
	Name = plate, index = 1
Mapping capsBound attributes ................
	Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
	Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
	Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
	Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
	Mesh for body = 0
	Number of nodal coordinates = 25
	Number of elements = 16
	Elemental Nodes = 0
	Elemental Rods  = 0
	Elemental Tria3 = 0
	Elemental Quad4 = 16

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

Getting FEA properties.......
	Number of properties - 1
	Property name - plate
	Done getting FEA properties
Updating mesh element types based on properties input

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

Getting FEA loads.......
	Number of loads - 1
	Load name - appliedPressure
	Done getting FEA loads

Getting FEA design variables.......
	Number of design variables          - 1
	Design_Variable name - thick1
	Design_Variable_Relation name - thick1
	Number of design variable relations - 1
	Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL

Getting FEA analyses.......
	Number of analyses - 1
	Analysis name - Default
	Done getting FEA analyses

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

Writing subElement types (if any) - appending mesh file

Writing TACS instruction file....
	Writing analysis cards
	Writing load ADD cards
	Writing constraint ADD cards
	Writing load cards
	Writing constraint cards
	Writing material cards
	Writing property cards
	Writing design variable cards
	Writing design variable relation cards
Mapping Csys attributes ................
	Number of unique Csys attributes = 0

Getting FEA coordinate systems.......
	Number of coordinate systems - 0
	No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
	Number of unique capsConstraint attributes = 1
	Name = plateEdge, index = 1
Mapping capsLoad attributes ................
	Number of unique capsLoad attributes = 1
	Name = plate, index = 1
Mapping capsBound attributes ................
	Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
	Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
	Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
	Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
	Mesh for body = 0
	Number of nodal coordinates = 25
	Number of elements = 16
	Elemental Nodes = 0
	Elemental Rods  = 0
	Elemental Tria3 = 0
	Elemental Quad4 = 16

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

Getting FEA properties.......
	Number of properties - 1
	Property name - plate
	Done getting FEA properties
Updating mesh element types based on properties input

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

Getting FEA loads.......
	Number of loads - 1
	Load name - appliedPressure
	Done getting FEA loads

Getting FEA design variables.......
	Number of design variables          - 1
	Design_Variable name - thick1
	Design_Variable_Relation name - thick1
	Number of design variable relations - 1
	Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL

Getting FEA analyses.......
	Number of analyses - 1
	Analysis name - Default
	Done getting FEA analyses

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

Writing subElement types (if any) - appending mesh file

Writing TACS instruction file....
	Writing analysis cards
	Writing load ADD cards
	Writing constraint ADD cards
	Writing load cards
	Writing constraint cards
	Writing material cards
	Writing property cards
	Writing design variable cards
	Writing design variable relation cards
Mapping Csys attributes ................
	Number of unique Csys attributes = 0

Getting FEA coordinate systems.......
	Number of coordinate systems - 0
	No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
	Number of unique capsConstraint attributes = 1
	Name = plateEdge, index = 1
Mapping capsLoad attributes ................
	Number of unique capsLoad attributes = 1
	Name = plate, index = 1
Mapping capsBound attributes ................
	Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
	Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
	Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
	Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
	Mesh for body = 0
	Number of nodal coordinates = 25
	Number of elements = 16
	Elemental Nodes = 0
	Elemental Rods  = 0
	Elemental Tria3 = 0
	Elemental Quad4 = 16

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

Getting FEA properties.......
	Number of properties - 1
	Property name - plate
	Done getting FEA properties
Updating mesh element types based on properties input

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

Getting FEA loads.......
	Number of loads - 1
	Load name - appliedPressure
	Done getting FEA loads

Getting FEA design variables.......
	Number of design variables          - 1
	Design_Variable name - thick1
	Design_Variable_Relation name - thick1
	Number of design variable relations - 1
	Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL

Getting FEA analyses.......
	Number of analyses - 1
	Analysis name - Default
	Done getting FEA analyses

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

Writing subElement types (if any) - appending mesh file

Writing TACS instruction file....
	Writing analysis cards
	Writing load ADD cards
	Writing constraint ADD cards
	Writing load cards
	Writing constraint cards
	Writing material cards
	Writing property cards
	Writing design variable cards
	Writing design variable relation cards
Mapping Csys attributes ................
	Number of unique Csys attributes = 0

Getting FEA coordinate systems.......
	Number of coordinate systems - 0
	No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
	Number of unique capsConstraint attributes = 1
	Name = plateEdge, index = 1
Mapping capsLoad attributes ................
	Number of unique capsLoad attributes = 1
	Name = plate, index = 1
Mapping capsBound attributes ................
	Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
	Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
	Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
	Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
	Mesh for body = 0
	Number of nodal coordinates = 25
	Number of elements = 16
	Elemental Nodes = 0
	Elemental Rods  = 0
	Elemental Tria3 = 0
	Elemental Quad4 = 16

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

Getting FEA properties.......
	Number of properties - 1
	Property name - plate
	Done getting FEA properties
Updating mesh element types based on properties input

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

Getting FEA loads.......
	Number of loads - 1
	Load name - appliedPressure
	Done getting FEA loads

Getting FEA design variables.......
	Number of design variables          - 1
	Design_Variable name - thick1
	Design_Variable_Relation name - thick1
	Number of design variable relations - 1
	Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL

Getting FEA analyses.......
	Number of analyses - 1
	Analysis name - Default
	Done getting FEA analyses

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

Writing subElement types (if any) - appending mesh file

Writing TACS instruction file....
	Writing analysis cards
	Writing load ADD cards
	Writing constraint ADD cards
	Writing load cards
	Writing constraint cards
	Writing material cards
	Writing property cards
	Writing design variable cards
	Writing design variable relation cards
Mapping Csys attributes ................
	Number of unique Csys attributes = 0

Getting FEA coordinate systems.......
	Number of coordinate systems - 0
	No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
	Number of unique capsConstraint attributes = 1
	Name = plateEdge, index = 1
Mapping capsLoad attributes ................
	Number of unique capsLoad attributes = 1
	Name = plate, index = 1
Mapping capsBound attributes ................
	Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
	Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
	Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
	Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
	Mesh for body = 0
	Number of nodal coordinates = 25
	Number of elements = 16
	Elemental Nodes = 0
	Elemental Rods  = 0
	Elemental Tria3 = 0
	Elemental Quad4 = 16

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

Getting FEA properties.......
	Number of properties - 1
	Property name - plate
	Done getting FEA properties
Updating mesh element types based on properties input

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

Getting FEA loads.......
	Number of loads - 1
	Load name - appliedPressure
	Done getting FEA loads

Getting FEA design variables.......
	Number of design variables          - 1
	Design_Variable name - thick1
	Design_Variable_Relation name - thick1
	Number of design variable relations - 1
	Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL

Getting FEA analyses.......
	Number of analyses - 1
	Analysis name - Default
	Done getting FEA analyses

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

Writing subElement types (if any) - appending mesh file

Writing TACS instruction file....
	Writing analysis cards
	Writing load ADD cards
	Writing constraint ADD cards
	Writing load cards
	Writing constraint cards
	Writing material cards
	Writing property cards
	Writing design variable cards
	Writing design variable relation cards
Mapping Csys attributes ................
	Number of unique Csys attributes = 0

Getting FEA coordinate systems.......
	Number of coordinate systems - 0
	No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
	Number of unique capsConstraint attributes = 1
	Name = plateEdge, index = 1
Mapping capsLoad attributes ................
	Number of unique capsLoad attributes = 1
	Name = plate, index = 1
Mapping capsBound attributes ................
	Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
	Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
	Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
	Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
	Mesh for body = 0
	Number of nodal coordinates = 25
	Number of elements = 16
	Elemental Nodes = 0
	Elemental Rods  = 0
	Elemental Tria3 = 0
	Elemental Quad4 = 16

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

Getting FEA properties.......
	Number of properties - 1
	Property name - plate
	Done getting FEA properties
Updating mesh element types based on properties input

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

Getting FEA loads.......
	Number of loads - 1
	Load name - appliedPressure
	Done getting FEA loads

Getting FEA design variables.......
	Number of design variables          - 1
	Design_Variable name - thick1
	Design_Variable_Relation name - thick1
	Number of design variable relations - 1
	Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL

Getting FEA analyses.......
	Number of analyses - 1
	Analysis name - Default
	Done getting FEA analyses

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

Writing subElement types (if any) - appending mesh file

Writing TACS instruction file....
	Writing analysis cards
	Writing load ADD cards
	Writing constraint ADD cards
	Writing load cards
	Writing constraint cards
	Writing material cards
	Writing property cards
	Writing design variable cards
	Writing design variable relation cards
Mapping Csys attributes ................
	Number of unique Csys attributes = 0

Getting FEA coordinate systems.......
	Number of coordinate systems - 0
	No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
	Number of unique capsConstraint attributes = 1
	Name = plateEdge, index = 1
Mapping capsLoad attributes ................
	Number of unique capsLoad attributes = 1
	Name = plate, index = 1
Mapping capsBound attributes ................
	Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
	Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
	Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
	Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
	Mesh for body = 0
	Number of nodal coordinates = 25
	Number of elements = 16
	Elemental Nodes = 0
	Elemental Rods  = 0
	Elemental Tria3 = 0
	Elemental Quad4 = 16

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

Getting FEA properties.......
	Number of properties - 1
	Property name - plate
	Done getting FEA properties
Updating mesh element types based on properties input

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

Getting FEA loads.......
	Number of loads - 1
	Load name - appliedPressure
	Done getting FEA loads

Getting FEA design variables.......
	Number of design variables          - 1
	Design_Variable name - thick1
	Design_Variable_Relation name - thick1
	Number of design variable relations - 1
	Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL

Getting FEA analyses.......
	Number of analyses - 1
	Analysis name - Default
	Done getting FEA analyses

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

Writing subElement types (if any) - appending mesh file

Writing TACS instruction file....
	Writing analysis cards
	Writing load ADD cards
	Writing constraint ADD cards
	Writing load cards
	Writing constraint cards
	Writing material cards
	Writing property cards
	Writing design variable cards
	Writing design variable relation cards
Mapping Csys attributes ................
	Number of unique Csys attributes = 0

Getting FEA coordinate systems.......
	Number of coordinate systems - 0
	No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
	Number of unique capsConstraint attributes = 1
	Name = plateEdge, index = 1
Mapping capsLoad attributes ................
	Number of unique capsLoad attributes = 1
	Name = plate, index = 1
Mapping capsBound attributes ................
	Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
	Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
	Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
	Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
	Mesh for body = 0
	Number of nodal coordinates = 25
	Number of elements = 16
	Elemental Nodes = 0
	Elemental Rods  = 0
	Elemental Tria3 = 0
	Elemental Quad4 = 16

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

Getting FEA properties.......
	Number of properties - 1
	Property name - plate
	Done getting FEA properties
Updating mesh element types based on properties input

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

Getting FEA loads.......
	Number of loads - 1
	Load name - appliedPressure
	Done getting FEA loads

Getting FEA design variables.......
	Number of design variables          - 1
	Design_Variable name - thick1
	Design_Variable_Relation name - thick1
	Number of design variable relations - 1
	Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL

Getting FEA analyses.......
	Number of analyses - 1
	Analysis name - Default
	Done getting FEA analyses

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

Writing subElement types (if any) - appending mesh file

Writing TACS instruction file....
	Writing analysis cards
	Writing load ADD cards
	Writing constraint ADD cards
	Writing load cards
	Writing constraint cards
	Writing material cards
	Writing property cards
	Writing design variable cards
	Writing design variable relation cards
Mapping Csys attributes ................
	Number of unique Csys attributes = 0

Getting FEA coordinate systems.......
	Number of coordinate systems - 0
	No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
	Number of unique capsConstraint attributes = 1
	Name = plateEdge, index = 1
Mapping capsLoad attributes ................
	Number of unique capsLoad attributes = 1
	Name = plate, index = 1
Mapping capsBound attributes ................
	Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
	Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
	Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
	Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
	Mesh for body = 0
	Number of nodal coordinates = 25
	Number of elements = 16
	Elemental Nodes = 0
	Elemental Rods  = 0
	Elemental Tria3 = 0
	Elemental Quad4 = 16

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

Getting FEA properties.......
	Number of properties - 1
	Property name - plate
	Done getting FEA properties
Updating mesh element types based on properties input

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

Getting FEA loads.......
	Number of loads - 1
	Load name - appliedPressure
	Done getting FEA loads

Getting FEA design variables.......
	Number of design variables          - 1
	Design_Variable name - thick1
	Design_Variable_Relation name - thick1
	Number of design variable relations - 1
	Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL

Getting FEA analyses.......
	Number of analyses - 1
	Analysis name - Default
	Done getting FEA analyses

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

Writing subElement types (if any) - appending mesh file

Writing TACS instruction file....
	Writing analysis cards
	Writing load ADD cards
	Writing constraint ADD cards
	Writing load cards
	Writing constraint cards
	Writing material cards
	Writing property cards
	Writing design variable cards
	Writing design variable relation cards
Mapping Csys attributes ................
	Number of unique Csys attributes = 0

Getting FEA coordinate systems.......
	Number of coordinate systems - 0
	No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
	Number of unique capsConstraint attributes = 1
	Name = plateEdge, index = 1
Mapping capsLoad attributes ................
	Number of unique capsLoad attributes = 1
	Name = plate, index = 1
Mapping capsBound attributes ................
	Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
	Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
	Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
	Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
	Mesh for body = 0
	Number of nodal coordinates = 25
	Number of elements = 16
	Elemental Nodes = 0
	Elemental Rods  = 0
	Elemental Tria3 = 0
	Elemental Quad4 = 16

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

Getting FEA properties.......
	Number of properties - 1
	Property name - plate
	Done getting FEA properties
Updating mesh element types based on properties input

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

Getting FEA loads.......
	Number of loads - 1
	Load name - appliedPressure
	Done getting FEA loads

Getting FEA design variables.......
	Number of design variables          - 1
	Design_Variable name - thick1
	Design_Variable_Relation name - thick1
	Number of design variable relations - 1
	Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL

Getting FEA analyses.......
	Number of analyses - 1
	Analysis name - Default
	Done getting FEA analyses

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

Writing subElement types (if any) - appending mesh file

Writing TACS instruction file....
	Writing analysis cards
	Writing load ADD cards
	Writing constraint ADD cards
	Writing load cards
	Writing constraint cards
	Writing material cards
	Writing property cards
	Writing design variable cards
	Writing design variable relation cards
Mapping Csys attributes ................
	Number of unique Csys attributes = 0

Getting FEA coordinate systems.......
	Number of coordinate systems - 0
	No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
	Number of unique capsConstraint attributes = 1
	Name = plateEdge, index = 1
Mapping capsLoad attributes ................
	Number of unique capsLoad attributes = 1
	Name = plate, index = 1
Mapping capsBound attributes ................
	Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
	Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
	Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
	Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
	Mesh for body = 0
	Number of nodal coordinates = 25
	Number of elements = 16
	Elemental Nodes = 0
	Elemental Rods  = 0
	Elemental Tria3 = 0
	Elemental Quad4 = 16

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

Getting FEA properties.......
	Number of properties - 1
	Property name - plate
	Done getting FEA properties
Updating mesh element types based on properties input

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

Getting FEA loads.......
	Number of loads - 1
	Load name - appliedPressure
	Done getting FEA loads

Getting FEA design variables.......
	Number of design variables          - 1
	Design_Variable name - thick1
	Design_Variable_Relation name - thick1
	Number of design variable relations - 1
	Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL

Getting FEA analyses.......
	Number of analyses - 1
	Analysis name - Default
	Done getting FEA analyses

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

Writing subElement types (if any) - appending mesh file

Writing TACS instruction file....
	Writing analysis cards
	Writing load ADD cards
	Writing constraint ADD cards
	Writing load cards
	Writing constraint cards
	Writing material cards
	Writing property cards
	Writing design variable cards
	Writing design variable relation cards
Mapping Csys attributes ................
	Number of unique Csys attributes = 0

Getting FEA coordinate systems.......
	Number of coordinate systems - 0
	No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
	Number of unique capsConstraint attributes = 1
	Name = plateEdge, index = 1
Mapping capsLoad attributes ................
	Number of unique capsLoad attributes = 1
	Name = plate, index = 1
Mapping capsBound attributes ................
	Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
	Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
	Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
	Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
	Mesh for body = 0
	Number of nodal coordinates = 25
	Number of elements = 16
	Elemental Nodes = 0
	Elemental Rods  = 0
	Elemental Tria3 = 0
	Elemental Quad4 = 16

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

Getting FEA properties.......
	Number of properties - 1
	Property name - plate
	Done getting FEA properties
Updating mesh element types based on properties input

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

Getting FEA loads.......
	Number of loads - 1
	Load name - appliedPressure
	Done getting FEA loads

Getting FEA design variables.......
	Number of design variables          - 1
	Design_Variable name - thick1
	Design_Variable_Relation name - thick1
	Number of design variable relations - 1
	Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL

Getting FEA analyses.......
	Number of analyses - 1
	Analysis name - Default
	Done getting FEA analyses

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

Writing subElement types (if any) - appending mesh file

Writing TACS instruction file....
	Writing analysis cards
	Writing load ADD cards
	Writing constraint ADD cards
	Writing load cards
	Writing constraint cards
	Writing material cards
	Writing property cards
	Writing design variable cards
	Writing design variable relation cards
Mapping Csys attributes ................
	Number of unique Csys attributes = 0

Getting FEA coordinate systems.......
	Number of coordinate systems - 0
	No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
	Number of unique capsConstraint attributes = 1
	Name = plateEdge, index = 1
Mapping capsLoad attributes ................
	Number of unique capsLoad attributes = 1
	Name = plate, index = 1
Mapping capsBound attributes ................
	Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
	Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
	Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
	Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
	Mesh for body = 0
	Number of nodal coordinates = 25
	Number of elements = 16
	Elemental Nodes = 0
	Elemental Rods  = 0
	Elemental Tria3 = 0
	Elemental Quad4 = 16

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

Getting FEA properties.......
	Number of properties - 1
	Property name - plate
	Done getting FEA properties
Updating mesh element types based on properties input

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

Getting FEA loads.......
	Number of loads - 1
	Load name - appliedPressure
	Done getting FEA loads

Getting FEA design variables.......
	Number of design variables          - 1
	Design_Variable name - thick1
	Design_Variable_Relation name - thick1
	Number of design variable relations - 1
	Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL

Getting FEA analyses.......
	Number of analyses - 1
	Analysis name - Default
	Done getting FEA analyses

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

Writing subElement types (if any) - appending mesh file

Writing TACS instruction file....
	Writing analysis cards
	Writing load ADD cards
	Writing constraint ADD cards
	Writing load cards
	Writing constraint cards
	Writing material cards
	Writing property cards
	Writing design variable cards
	Writing design variable relation cards
Mapping Csys attributes ................
	Number of unique Csys attributes = 0

Getting FEA coordinate systems.......
	Number of coordinate systems - 0
	No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
	Number of unique capsConstraint attributes = 1
	Name = plateEdge, index = 1
Mapping capsLoad attributes ................
	Number of unique capsLoad attributes = 1
	Name = plate, index = 1
Mapping capsBound attributes ................
	Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
	Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
	Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
	Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
	Mesh for body = 0
	Number of nodal coordinates = 25
	Number of elements = 16
	Elemental Nodes = 0
	Elemental Rods  = 0
	Elemental Tria3 = 0
	Elemental Quad4 = 16

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

Getting FEA properties.......
	Number of properties - 1
	Property name - plate
	Done getting FEA properties
Updating mesh element types based on properties input

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

Getting FEA loads.......
	Number of loads - 1
	Load name - appliedPressure
	Done getting FEA loads

Getting FEA design variables.......
	Number of design variables          - 1
	Design_Variable name - thick1
	Design_Variable_Relation name - thick1
	Number of design variable relations - 1
	Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL

Getting FEA analyses.......
	Number of analyses - 1
	Analysis name - Default
	Done getting FEA analyses

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

Writing subElement types (if any) - appending mesh file

Writing TACS instruction file....
	Writing analysis cards
	Writing load ADD cards
	Writing constraint ADD cards
	Writing load cards
	Writing constraint cards
	Writing material cards
	Writing property cards
	Writing design variable cards
	Writing design variable relation cards
Mapping Csys attributes ................
	Number of unique Csys attributes = 0

Getting FEA coordinate systems.......
	Number of coordinate systems - 0
	No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
	Number of unique capsConstraint attributes = 1
	Name = plateEdge, index = 1
Mapping capsLoad attributes ................
	Number of unique capsLoad attributes = 1
	Name = plate, index = 1
Mapping capsBound attributes ................
	Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
	Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
	Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
	Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
	Mesh for body = 0
	Number of nodal coordinates = 25
	Number of elements = 16
	Elemental Nodes = 0
	Elemental Rods  = 0
	Elemental Tria3 = 0
	Elemental Quad4 = 16

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

Getting FEA properties.......
	Number of properties - 1
	Property name - plate
	Done getting FEA properties
Updating mesh element types based on properties input

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

Getting FEA loads.......
	Number of loads - 1
	Load name - appliedPressure
	Done getting FEA loads

Getting FEA design variables.......
	Number of design variables          - 1
	Design_Variable name - thick1
	Design_Variable_Relation name - thick1
	Number of design variable relations - 1
	Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL

Getting FEA analyses.......
	Number of analyses - 1
	Analysis name - Default
	Done getting FEA analyses

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

Writing subElement types (if any) - appending mesh file

Writing TACS instruction file....
	Writing analysis cards
	Writing load ADD cards
	Writing constraint ADD cards
	Writing load cards
	Writing constraint cards
	Writing material cards
	Writing property cards
	Writing design variable cards
	Writing design variable relation cards
Mapping Csys attributes ................
	Number of unique Csys attributes = 0

Getting FEA coordinate systems.......
	Number of coordinate systems - 0
	No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
	Number of unique capsConstraint attributes = 1
	Name = plateEdge, index = 1
Mapping capsLoad attributes ................
	Number of unique capsLoad attributes = 1
	Name = plate, index = 1
Mapping capsBound attributes ................
	Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
	Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
	Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
	Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
	Mesh for body = 0
	Number of nodal coordinates = 25
	Number of elements = 16
	Elemental Nodes = 0
	Elemental Rods  = 0
	Elemental Tria3 = 0
	Elemental Quad4 = 16

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

Getting FEA properties.......
	Number of properties - 1
	Property name - plate
	Done getting FEA properties
Updating mesh element types based on properties input

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

Getting FEA loads.......
	Number of loads - 1
	Load name - appliedPressure
	Done getting FEA loads

Getting FEA design variables.......
	Number of design variables          - 1
	Design_Variable name - thick1
	Design_Variable_Relation name - thick1
	Number of design variable relations - 1
	Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL

Getting FEA analyses.......
	Number of analyses - 1
	Analysis name - Default
	Done getting FEA analyses

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

Writing subElement types (if any) - appending mesh file

Writing TACS instruction file....
	Writing analysis cards
	Writing load ADD cards
	Writing constraint ADD cards
	Writing load cards
	Writing constraint cards
	Writing material cards
	Writing property cards
	Writing design variable cards
	Writing design variable relation cards
ok
test_Multiple_Mesh (test_tetgen.TestTETGEN.test_Multiple_Mesh) ... ERROR:: BAD STATUS = -276 from matsol (called from solveSketchOrig:61976)

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!
 1E2491C40 EGADS Info: Face #3 -> Edge #9 (9) Internally in Loop 7 4, sen = 1!
 17181B000 EGADS Info: Face #5 -> Edge #17 (9) Internally in Loop 7 4, sen = -1!
 17181B000 EGADS Info: Face #5 -> Edge #17 (9) Internally in Loop 4 7, sen = 1!
Getting surface mesh for body 7 (of 7)
Body 1 (of 7)
Number of nodes    = 98
Number of elements = 192
Number of triangle elements      = 192
Number of quadrilateral elements = 0
Body 2 (of 7)
Number of nodes    = 298
Number of elements = 592
Number of triangle elements      = 592
Number of quadrilateral elements = 0
Body 3 (of 7)
Number of nodes    = 488
Number of elements = 972
Number of triangle elements      = 972
Number of quadrilateral elements = 0
Body 4 (of 7)
Number of nodes    = 2048
Number of elements = 4096
Number of triangle elements      = 4096
Number of quadrilateral elements = 0
Body 5 (of 7)
Number of nodes    = 152
Number of elements = 300
Number of triangle elements      = 300
Number of quadrilateral elements = 0
Body 6 (of 7)
Number of nodes    = 624
Number of elements = 1248
Number of triangle elements      = 1248
Number of quadrilateral elements = 0
Body 7 (of 7)
Number of nodes    = 489
Number of elements = 974
Number of triangle elements      = 974
Number of quadrilateral elements = 0
----------------------------
Total number of nodes    = 4197
Total number of elements = 8374
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 7
	Name = box, index = 1
	Name = cylinder, index = 2
	Name = cone, index = 3
	Name = torus, index = 4
	Name = sphere, index = 5
	Name = boxhole, index = 6
	Name = bullet, index = 7
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Body 1 number of surface: nodes - 98, elements - 192
Body 2 number of surface: nodes - 298, elements - 592
Body 3 number of surface: nodes - 488, elements - 972
Body 4 number of surface: nodes - 2048, elements - 4096
Body 5 number of surface: nodes - 152, elements - 300
Body 6 number of surface: nodes - 624, elements - 1248
Body 7 number of surface: nodes - 489, elements - 974
Getting volume mesh for body 1 (of 7)
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = box, index = 1

Generating volume mesh using TetGen.....

Tetgen input string = pYq1.500/0.000QT1.00e-16A
Done meshing using TetGen!
Getting volume mesh for body 2 (of 7)
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = cylinder, index = 1

Generating volume mesh using TetGen.....

Tetgen input string = pYq1.500/0.000QT1.00e-16A
Done meshing using TetGen!
Getting volume mesh for body 3 (of 7)
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = cone, index = 1

Generating volume mesh using TetGen.....

Tetgen input string = pYq1.500/0.000QT1.00e-16A
Done meshing using TetGen!
Getting volume mesh for body 4 (of 7)
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = torus, index = 1

Generating volume mesh using TetGen.....

Tetgen input string = pYq1.500/0.000QT1.00e-16A
Done meshing using TetGen!
Getting volume mesh for body 5 (of 7)
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = sphere, index = 1

Generating volume mesh using TetGen.....

Tetgen input string = pYq1.500/0.000QT1.00e-16A
Done meshing using TetGen!
Getting volume mesh for body 6 (of 7)
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = boxhole, index = 1

Generating volume mesh using TetGen.....

Tetgen input string = pYq1.500/0.000QT1.00e-16A
Done meshing using TetGen!
Getting volume mesh for body 7 (of 7)
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = bullet, index = 1

Generating volume mesh using TetGen.....

Tetgen input string = pYq1.500/0.000QT1.00e-16A
Done meshing using TetGen!
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 7
	Name = box, index = 1
	Name = cylinder, index = 2
	Name = cone, index = 3
	Name = torus, index = 4
	Name = sphere, index = 5
	Name = boxhole, index = 6
	Name = bullet, index = 7
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Body 1 number of surface: nodes - 98, elements - 192
Body 2 number of surface: nodes - 298, elements - 592
Body 3 number of surface: nodes - 488, elements - 972
Body 4 number of surface: nodes - 2048, elements - 4096
Body 5 number of surface: nodes - 152, elements - 300
Body 6 number of surface: nodes - 624, elements - 1248
Body 7 number of surface: nodes - 489, elements - 974
Getting volume mesh

Generating volume mesh using TetGen.....

Tetgen input string = pYq1.500/0.000QT1.00e-16A

Generating volume mesh using TetGen.....

Tetgen input string = pYq1.500/0.000QT1.00e-16A

Generating volume mesh using TetGen.....

Tetgen input string = pYq1.500/0.000QT1.00e-16A

Generating volume mesh using TetGen.....

Tetgen input string = pYq1.500/0.000QT1.00e-16A

Generating volume mesh using TetGen.....

Tetgen input string = pYq1.500/0.000QT1.00e-16A

Generating volume mesh using TetGen.....

Tetgen input string = pYq1.500/0.000QT1.00e-16A

Generating volume mesh using TetGen.....

Tetgen input string = pYq1.500/0.000QT1.00e-16A
Done meshing using TetGen!
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 7
	Name = box, index = 1
	Name = cylinder, index = 2
	Name = cone, index = 3
	Name = torus, index = 4
	Name = sphere, index = 5
	Name = boxhole, index = 6
	Name = bullet, index = 7
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Number of surface: nodes - 4197, elements - 8374
Getting volume mesh

Generating volume mesh using TetGen.....

Tetgen input string = pYq1.500/0.000QT1.00e-16A
Done meshing using TetGen!
ok
test_faceMatch_MultiDomain (test_tetgen.TestTETGEN.test_faceMatch_MultiDomain) ... ../csmData/MultiDomain/example1.csm

Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = dummy_att, index = 1
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 0
Getting surface mesh for body 1 (of 2)
Getting surface mesh for body 2 (of 2)
Body 1 (of 2)
Number of nodes    = 374
Number of elements = 744
Number of triangle elements      = 744
Number of quadrilateral elements = 0
Body 2 (of 2)
Number of nodes    = 98
Number of elements = 192
Number of triangle elements      = 192
Number of quadrilateral elements = 0
----------------------------
Total number of nodes    = 472
Total number of elements = 936
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = dummy_att, index = 1
Body 1 number of surface: nodes - 374, elements - 744
Body 2 number of surface: nodes - 98, elements - 192
Getting volume mesh

Generating volume mesh using TetGen.....

Tetgen input string = pYq1.500/0.000QT1.00e-16A

Generating volume mesh using TetGen.....

Tetgen input string = pYq1.500/0.000QT1.00e-16A
Done meshing using TetGen!
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = dummy_att, index = 1
Body 1 number of surface: nodes - 374, elements - 744
Body 2 number of surface: nodes - 98, elements - 192
Getting volume mesh for body 1 (of 2)
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = dummy_att, index = 1

Generating volume mesh using TetGen.....

Tetgen input string = pYq1.500/0.000QT1.00e-16A
Done meshing using TetGen!
Getting volume mesh for body 2 (of 2)
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = dummy_att, index = 1

Generating volume mesh using TetGen.....

Tetgen input string = pYq1.500/0.000QT1.00e-16A
Done meshing using TetGen!
../csmData/MultiDomain/example2.csm

Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = dummy_att, index = 1
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 0
Getting surface mesh for body 1 (of 3)
Getting surface mesh for body 2 (of 3)
Getting surface mesh for body 3 (of 3)
Body 1 (of 3)
Number of nodes    = 386
Number of elements = 768
Number of triangle elements      = 768
Number of quadrilateral elements = 0
Body 2 (of 3)
Number of nodes    = 98
Number of elements = 192
Number of triangle elements      = 192
Number of quadrilateral elements = 0
Body 3 (of 3)
Number of nodes    = 98
Number of elements = 192
Number of triangle elements      = 192
Number of quadrilateral elements = 0
----------------------------
Total number of nodes    = 582
Total number of elements = 1152
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = dummy_att, index = 1
Body 1 number of surface: nodes - 386, elements - 768
Body 2 number of surface: nodes - 98, elements - 192
Body 3 number of surface: nodes - 98, elements - 192
Getting volume mesh

Generating volume mesh using TetGen.....

Tetgen input string = pYq1.500/0.000QT1.00e-16A

Generating volume mesh using TetGen.....

Tetgen input string = pYq1.500/0.000QT1.00e-16A

Generating volume mesh using TetGen.....

Tetgen input string = pYq1.500/0.000QT1.00e-16A
Done meshing using TetGen!
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = dummy_att, index = 1
Body 1 number of surface: nodes - 386, elements - 768
Body 2 number of surface: nodes - 98, elements - 192
Body 3 number of surface: nodes - 98, elements - 192
Getting volume mesh for body 1 (of 3)
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = dummy_att, index = 1

Generating volume mesh using TetGen.....

Tetgen input string = pYq1.500/0.000QT1.00e-16A
Done meshing using TetGen!
Getting volume mesh for body 2 (of 3)
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = dummy_att, index = 1

Generating volume mesh using TetGen.....

Tetgen input string = pYq1.500/0.000QT1.00e-16A
Done meshing using TetGen!
Getting volume mesh for body 3 (of 3)
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = dummy_att, index = 1

Generating volume mesh using TetGen.....

Tetgen input string = pYq1.500/0.000QT1.00e-16A
Done meshing using TetGen!
../csmData/MultiDomain/example3.csm

Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = dummy_att, index = 1
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 0
Getting surface mesh for body 1 (of 3)
Getting surface mesh for body 2 (of 3)
Getting surface mesh for body 3 (of 3)
Body 1 (of 3)
Number of nodes    = 351
Number of elements = 698
Number of triangle elements      = 698
Number of quadrilateral elements = 0
Body 2 (of 3)
Number of nodes    = 98
Number of elements = 192
Number of triangle elements      = 192
Number of quadrilateral elements = 0
Body 3 (of 3)
Number of nodes    = 42
Number of elements = 80
Number of triangle elements      = 80
Number of quadrilateral elements = 0
----------------------------
Total number of nodes    = 491
Total number of elements = 970
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = dummy_att, index = 1
Body 1 number of surface: nodes - 351, elements - 698
Body 2 number of surface: nodes - 98, elements - 192
Body 3 number of surface: nodes - 42, elements - 80
Getting volume mesh

Generating volume mesh using TetGen.....

Tetgen input string = pYq1.500/0.000QT1.00e-16A

Generating volume mesh using TetGen.....

Tetgen input string = pYq1.500/0.000QT1.00e-16A

Generating volume mesh using TetGen.....

Tetgen input string = pYq1.500/0.000QT1.00e-16A
Done meshing using TetGen!
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = dummy_att, index = 1
Body 1 number of surface: nodes - 351, elements - 698
Body 2 number of surface: nodes - 98, elements - 192
Body 3 number of surface: nodes - 42, elements - 80
Getting volume mesh for body 1 (of 3)
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = dummy_att, index = 1

Generating volume mesh using TetGen.....

Tetgen input string = pYq1.500/0.000QT1.00e-16A
Done meshing using TetGen!
Getting volume mesh for body 2 (of 3)
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = dummy_att, index = 1

Generating volume mesh using TetGen.....

Tetgen input string = pYq1.500/0.000QT1.00e-16A
Done meshing using TetGen!
Getting volume mesh for body 3 (of 3)
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = dummy_att, index = 1

Generating volume mesh using TetGen.....

Tetgen input string = pYq1.500/0.000QT1.00e-16A
Done meshing using TetGen!
../csmData/MultiDomain/example4.csm

Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = dummy_att, index = 1
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 0
Getting surface mesh for body 1 (of 3)
Getting surface mesh for body 2 (of 3)
Getting surface mesh for body 3 (of 3)
Body 1 (of 3)
Number of nodes    = 376
Number of elements = 748
Number of triangle elements      = 748
Number of quadrilateral elements = 0
Body 2 (of 3)
Number of nodes    = 98
Number of elements = 192
Number of triangle elements      = 192
Number of quadrilateral elements = 0
Body 3 (of 3)
Number of nodes    = 42
Number of elements = 80
Number of triangle elements      = 80
Number of quadrilateral elements = 0
----------------------------
Total number of nodes    = 516
Total number of elements = 1020
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = dummy_att, index = 1
Body 1 number of surface: nodes - 376, elements - 748
Body 2 number of surface: nodes - 98, elements - 192
Body 3 number of surface: nodes - 42, elements - 80
Getting volume mesh

Generating volume mesh using TetGen.....

Tetgen input string = pYq1.500/0.000QT1.00e-16A

Generating volume mesh using TetGen.....

Tetgen input string = pYq1.500/0.000QT1.00e-16A

Generating volume mesh using TetGen.....

Tetgen input string = pYq1.500/0.000QT1.00e-16A
Done meshing using TetGen!
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = dummy_att, index = 1
Body 1 number of surface: nodes - 376, elements - 748
Body 2 number of surface: nodes - 98, elements - 192
Body 3 number of surface: nodes - 42, elements - 80
Getting volume mesh for body 1 (of 3)
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = dummy_att, index = 1

Generating volume mesh using TetGen.....

Tetgen input string = pYq1.500/0.000QT1.00e-16A
Done meshing using TetGen!
Getting volume mesh for body 2 (of 3)
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = dummy_att, index = 1

Generating volume mesh using TetGen.....

Tetgen input string = pYq1.500/0.000QT1.00e-16A
Done meshing using TetGen!
Getting volume mesh for body 3 (of 3)
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = dummy_att, index = 1

Generating volume mesh using TetGen.....

Tetgen input string = pYq1.500/0.000QT1.00e-16A
Done meshing using TetGen!
../csmData/MultiDomain/example6.csm

Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = dummy_att, index = 1
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 0
Getting surface mesh for body 1 (of 3)
Getting surface mesh for body 2 (of 3)
Getting surface mesh for body 3 (of 3)
Body 1 (of 3)
Number of nodes    = 370
Number of elements = 736
Number of triangle elements      = 736
Number of quadrilateral elements = 0
Body 2 (of 3)
Number of nodes    = 42
Number of elements = 80
Number of triangle elements      = 80
Number of quadrilateral elements = 0
Body 3 (of 3)
Number of nodes    = 42
Number of elements = 80
Number of triangle elements      = 80
Number of quadrilateral elements = 0
----------------------------
Total number of nodes    = 454
Total number of elements = 896
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = dummy_att, index = 1
Body 1 number of surface: nodes - 370, elements - 736
Body 2 number of surface: nodes - 42, elements - 80
Body 3 number of surface: nodes - 42, elements - 80
Getting volume mesh

Generating volume mesh using TetGen.....

Tetgen input string = pYq1.500/0.000QT1.00e-16A

Generating volume mesh using TetGen.....

Tetgen input string = pYq1.500/0.000QT1.00e-16A

Generating volume mesh using TetGen.....

Tetgen input string = pYq1.500/0.000QT1.00e-16A
Done meshing using TetGen!
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = dummy_att, index = 1
Body 1 number of surface: nodes - 370, elements - 736
Body 2 number of surface: nodes - 42, elements - 80
Body 3 number of surface: nodes - 42, elements - 80
Getting volume mesh for body 1 (of 3)
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = dummy_att, index = 1

Generating volume mesh using TetGen.....

Tetgen input string = pYq1.500/0.000QT1.00e-16A
Done meshing using TetGen!
Getting volume mesh for body 2 (of 3)
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = dummy_att, index = 1

Generating volume mesh using TetGen.....

Tetgen input string = pYq1.500/0.000QT1.00e-16A
Done meshing using TetGen!
Getting volume mesh for body 3 (of 3)
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = dummy_att, index = 1

Generating volume mesh using TetGen.....

Tetgen input string = pYq1.500/0.000QT1.00e-16A
Done meshing using TetGen!
../csmData/MultiDomain/example7.csm

Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = dummy_att, index = 1
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 0
Getting surface mesh for body 1 (of 3)
Getting surface mesh for body 2 (of 3)
Getting surface mesh for body 3 (of 3)
Body 1 (of 3)
Number of nodes    = 370
Number of elements = 736
Number of triangle elements      = 736
Number of quadrilateral elements = 0
Body 2 (of 3)
Number of nodes    = 126
Number of elements = 252
Number of triangle elements      = 252
Number of quadrilateral elements = 0
Body 3 (of 3)
Number of nodes    = 20
Number of elements = 36
Number of triangle elements      = 36
Number of quadrilateral elements = 0
----------------------------
Total number of nodes    = 516
Total number of elements = 1024
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = dummy_att, index = 1
Body 1 number of surface: nodes - 370, elements - 736
Body 2 number of surface: nodes - 126, elements - 252
Body 3 number of surface: nodes - 20, elements - 36
Getting volume mesh

Generating volume mesh using TetGen.....

Tetgen input string = pYq1.500/0.000QT1.00e-16A

Generating volume mesh using TetGen.....

Tetgen input string = pYq1.500/0.000QT1.00e-16A

Generating volume mesh using TetGen.....

Tetgen input string = pYq1.500/0.000QT1.00e-16A
Done meshing using TetGen!
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = dummy_att, index = 1
Body 1 number of surface: nodes - 370, elements - 736
Body 2 number of surface: nodes - 126, elements - 252
Body 3 number of surface: nodes - 20, elements - 36
Getting volume mesh for body 1 (of 3)
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = dummy_att, index = 1

Generating volume mesh using TetGen.....

Tetgen input string = pYq1.500/0.000QT1.00e-16A
Done meshing using TetGen!
Getting volume mesh for body 2 (of 3)
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = dummy_att, index = 1

Generating volume mesh using TetGen.....

Tetgen input string = pYq1.500/0.000QT1.00e-16A
Done meshing using TetGen!
Getting volume mesh for body 3 (of 3)
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = dummy_att, index = 1

Generating volume mesh using TetGen.....

Tetgen input string = pYq1.500/0.000QT1.00e-16A
Done meshing using TetGen!
../csmData/MultiDomain/example8.csm

Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = dummy_att, index = 1
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 0
Getting surface mesh for body 1 (of 3)
Getting surface mesh for body 2 (of 3)
Getting surface mesh for body 3 (of 3)
Body 1 (of 3)
Number of nodes    = 109
Number of elements = 214
Number of triangle elements      = 214
Number of quadrilateral elements = 0
Body 2 (of 3)
Number of nodes    = 48
Number of elements = 96
Number of triangle elements      = 96
Number of quadrilateral elements = 0
Body 3 (of 3)
Number of nodes    = 12
Number of elements = 20
Number of triangle elements      = 20
Number of quadrilateral elements = 0
----------------------------
Total number of nodes    = 169
Total number of elements = 330
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = dummy_att, index = 1
Body 1 number of surface: nodes - 109, elements - 214
Body 2 number of surface: nodes - 48, elements - 96
Body 3 number of surface: nodes - 12, elements - 20
Getting volume mesh

Generating volume mesh using TetGen.....

Tetgen input string = pYq1.500/0.000QT1.00e-16A

Generating volume mesh using TetGen.....

Tetgen input string = pYq1.500/0.000QT1.00e-16A

Generating volume mesh using TetGen.....

Tetgen input string = pYq1.500/0.000QT1.00e-16A
Done meshing using TetGen!
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = dummy_att, index = 1
Body 1 number of surface: nodes - 109, elements - 214
Body 2 number of surface: nodes - 48, elements - 96
Body 3 number of surface: nodes - 12, elements - 20
Getting volume mesh for body 1 (of 3)
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = dummy_att, index = 1

Generating volume mesh using TetGen.....

Tetgen input string = pYq1.500/0.000QT1.00e-16A
Done meshing using TetGen!
Getting volume mesh for body 2 (of 3)
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = dummy_att, index = 1

Generating volume mesh using TetGen.....

Tetgen input string = pYq1.500/0.000QT1.00e-16A
Done meshing using TetGen!
Getting volume mesh for body 3 (of 3)
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = dummy_att, index = 1

Generating volume mesh using TetGen.....

Tetgen input string = pYq1.500/0.000QT1.00e-16A
Done meshing using TetGen!
../csmData/MultiDomain/example9.csm

Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = dummy_att, index = 1
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 0
Getting surface mesh for body 1 (of 2)
Getting surface mesh for body 2 (of 2)
Body 1 (of 2)
Number of nodes    = 536
Number of elements = 1072
Number of triangle elements      = 1072
Number of quadrilateral elements = 0
Body 2 (of 2)
Number of nodes    = 544
Number of elements = 1084
Number of triangle elements      = 1084
Number of quadrilateral elements = 0
----------------------------
Total number of nodes    = 1080
Total number of elements = 2156
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = dummy_att, index = 1
Body 1 number of surface: nodes - 536, elements - 1072
Body 2 number of surface: nodes - 544, elements - 1084
Getting volume mesh

Generating volume mesh using TetGen.....

Tetgen input string = pYq1.500/0.000QT1.00e-16A

Generating volume mesh using TetGen.....

Tetgen input string = pYq1.500/0.000QT1.00e-16A
Done meshing using TetGen!
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = dummy_att, index = 1
Body 1 number of surface: nodes - 536, elements - 1072
Body 2 number of surface: nodes - 544, elements - 1084
Getting volume mesh for body 1 (of 2)
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = dummy_att, index = 1

Generating volume mesh using TetGen.....

Tetgen input string = pYq1.500/0.000QT1.00e-16A
Done meshing using TetGen!
Getting volume mesh for body 2 (of 2)
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = dummy_att, index = 1

Generating volume mesh using TetGen.....

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

Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = dummy_att, index = 1
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 0
Getting surface mesh for body 1 (of 5)
Getting surface mesh for body 2 (of 5)
Getting surface mesh for body 3 (of 5)
Getting surface mesh for body 4 (of 5)
Getting surface mesh for body 5 (of 5)
Body 1 (of 5)
Number of nodes    = 1351
Number of elements = 2682
Number of triangle elements      = 2682
Number of quadrilateral elements = 0
Body 2 (of 5)
Number of nodes    = 288
Number of elements = 572
Number of triangle elements      = 572
Number of quadrilateral elements = 0
Body 3 (of 5)
Number of nodes    = 173
Number of elements = 342
Number of triangle elements      = 342
Number of quadrilateral elements = 0
Body 4 (of 5)
Number of nodes    = 26
Number of elements = 48
Number of triangle elements      = 48
Number of quadrilateral elements = 0
Body 5 (of 5)
Number of nodes    = 482
Number of elements = 960
Number of triangle elements      = 960
Number of quadrilateral elements = 0
----------------------------
Total number of nodes    = 2320
Total number of elements = 4604
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = dummy_att, index = 1
Body 1 number of surface: nodes - 1351, elements - 2682
Body 2 number of surface: nodes - 288, elements - 572
Body 3 number of surface: nodes - 173, elements - 342
Body 4 number of surface: nodes - 26, elements - 48
Body 5 number of surface: nodes - 482, elements - 960
Getting volume mesh

Generating volume mesh using TetGen.....

Tetgen input string = pYq1.500/0.000QT1.00e-16A

Generating volume mesh using TetGen.....

Tetgen input string = pYq1.500/0.000QT1.00e-16A

Generating volume mesh using TetGen.....

Tetgen input string = pYq1.500/0.000QT1.00e-16A

Generating volume mesh using TetGen.....

Tetgen input string = pYq1.500/0.000QT1.00e-16A

Generating volume mesh using TetGen.....

Tetgen input string = pYq1.500/0.000QT1.00e-16A
Done meshing using TetGen!
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = dummy_att, index = 1
Body 1 number of surface: nodes - 1351, elements - 2682
Body 2 number of surface: nodes - 288, elements - 572
Body 3 number of surface: nodes - 173, elements - 342
Body 4 number of surface: nodes - 26, elements - 48
Body 5 number of surface: nodes - 482, elements - 960
Getting volume mesh for body 1 (of 5)
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = dummy_att, index = 1

Generating volume mesh using TetGen.....

Tetgen input string = pYq1.500/0.000QT1.00e-16A
Done meshing using TetGen!
Getting volume mesh for body 2 (of 5)
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = dummy_att, index = 1

Generating volume mesh using TetGen.....

Tetgen input string = pYq1.500/0.000QT1.00e-16A
Done meshing using TetGen!
Getting volume mesh for body 3 (of 5)
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = dummy_att, index = 1

Generating volume mesh using TetGen.....

Tetgen input string = pYq1.500/0.000QT1.00e-16A
Done meshing using TetGen!
Getting volume mesh for body 4 (of 5)
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = dummy_att, index = 1

Generating volume mesh using TetGen.....

Tetgen input string = pYq1.500/0.000QT1.00e-16A
Done meshing using TetGen!
Getting volume mesh for body 5 (of 5)
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = dummy_att, index = 1

Generating volume mesh using TetGen.....

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

Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = dummy_att, index = 1
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 0
Getting surface mesh for body 1 (of 2)
Getting surface mesh for body 2 (of 2)
Body 1 (of 2)
Number of nodes    = 443
Number of elements = 882
Number of triangle elements      = 882
Number of quadrilateral elements = 0
Body 2 (of 2)
Number of nodes    = 522
Number of elements = 1044
Number of triangle elements      = 1044
Number of quadrilateral elements = 0
----------------------------
Total number of nodes    = 965
Total number of elements = 1926
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = dummy_att, index = 1
Body 1 number of surface: nodes - 443, elements - 882
Body 2 number of surface: nodes - 522, elements - 1044
Getting volume mesh

Generating volume mesh using TetGen.....

Tetgen input string = pYq1.500/0.000QT1.00e-16A

Generating volume mesh using TetGen.....

Tetgen input string = pYq1.500/0.000QT1.00e-16A
Done meshing using TetGen!
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = dummy_att, index = 1
Body 1 number of surface: nodes - 443, elements - 882
Body 2 number of surface: nodes - 522, elements - 1044
Getting volume mesh for body 1 (of 2)
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = dummy_att, index = 1

Generating volume mesh using TetGen.....

Tetgen input string = pYq1.500/0.000QT1.00e-16A
Done meshing using TetGen!
Getting volume mesh for body 2 (of 2)
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = dummy_att, index = 1

Generating volume mesh using TetGen.....

Tetgen input string = pYq1.500/0.000QT1.00e-16A
Done meshing using TetGen!
ok
test_journal (test_tetgen.TestTETGEN.test_journal) ... 
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 2
	Name = Farfield, index = 1
	Name = Wing1, index = 2
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 3
	Name = Farfield, index = 1
	Name = Wing1, index = 2
	Name = trailingEdge, index = 3

Getting mesh sizing parameters
	Mesh sizing name - Farfield
	Done getting mesh sizing parameters
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 2
	Name = Farfield, index = 1
	Name = Wing1, index = 2
Number of surface: nodes - 9583, elements - 19158
Getting volume mesh

Generating volume mesh using TetGen.....

Tetgen input string = pYq1.500/0.000QT1.00e-16A
Done meshing using TetGen!
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 2
	Name = Farfield, index = 1
	Name = Wing1, index = 2
Number of surface: nodes - 9583, elements - 19158
Getting volume mesh

Generating volume mesh using TetGen.....

Tetgen input string = pYq2.000/0.000QT1.00e-16A
Done meshing using TetGen!
 EGADS Info: 0 Objects, 0 Reference in Use (of 0) at Close!


 CAPS Info: Hit last success -- going live!

 CAPS Info: Hit last success -- going live!

 CAPS Info: Hit last success -- going live!

 CAPS Info: Hit last success -- going live!

 CAPS Info: Hit last success -- going live!

 CAPS Info: Hit last success -- going live!


 CAPS Info: Hit last success -- going live!

Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 2
	Name = Farfield, index = 1
	Name = Wing1, index = 2
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 3
	Name = Farfield, index = 1
	Name = Wing1, index = 2
	Name = trailingEdge, index = 3

Getting mesh sizing parameters
	Mesh sizing name - Farfield
	Done getting mesh sizing parameters
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 2
	Name = Farfield, index = 1
	Name = Wing1, index = 2
Number of surface: nodes - 9583, elements - 19158
Getting volume mesh

Generating volume mesh using TetGen.....

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

 CAPS Info: Hit last success -- going live!
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 2
	Name = Farfield, index = 1
	Name = Wing1, index = 2
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 3
	Name = Farfield, index = 1
	Name = Wing1, index = 2
	Name = trailingEdge, index = 3

Getting mesh sizing parameters
	Mesh sizing name - Farfield
	Done getting mesh sizing parameters
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 2
	Name = Farfield, index = 1
	Name = Wing1, index = 2

 CAPS Info: Hit last success -- going live!
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 2
	Name = Farfield, index = 1
	Name = Wing1, index = 2
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 3
	Name = Farfield, index = 1
	Name = Wing1, index = 2
	Name = trailingEdge, index = 3

Getting mesh sizing parameters
	Mesh sizing name - Farfield
	Done getting mesh sizing parameters
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 2
	Name = Farfield, index = 1
	Name = Wing1, index = 2

 CAPS Info: Hit last success -- going live!

 CAPS Info: Hit last success -- going live!
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 2
	Name = Farfield, index = 1
	Name = Wing1, index = 2
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 3
	Name = Farfield, index = 1
	Name = Wing1, index = 2
	Name = trailingEdge, index = 3

Getting mesh sizing parameters
	Mesh sizing name - Farfield
	Done getting mesh sizing parameters
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 2
	Name = Farfield, index = 1
	Name = Wing1, index = 2
Number of surface: nodes - 9583, elements - 19158
Getting volume mesh

Generating volume mesh using TetGen.....

Tetgen input string = pYq2.000/0.000QT1.00e-16A
Done meshing using TetGen!

 CAPS Info: Hit last success -- going live!
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 2
	Name = Farfield, index = 1
	Name = Wing1, index = 2
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 3
	Name = Farfield, index = 1
	Name = Wing1, index = 2
	Name = trailingEdge, index = 3

Getting mesh sizing parameters
	Mesh sizing name - Farfield
	Done getting mesh sizing parameters
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 2
	Name = Farfield, index = 1
	Name = Wing1, index = 2

ok
test_phase (test_tetgen.TestTETGEN.test_phase) ... 
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 2
	Name = Farfield, index = 1
	Name = Wing1, index = 2
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 3
	Name = Farfield, index = 1
	Name = Wing1, index = 2
	Name = trailingEdge, index = 3

Getting mesh sizing parameters
	Mesh sizing name - Farfield
	Done getting mesh sizing parameters
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 2
	Name = Farfield, index = 1
	Name = Wing1, index = 2
Number of surface: nodes - 9583, elements - 19158
Getting volume mesh

Generating volume mesh using TetGen.....

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

Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 2
	Name = Farfield, index = 1
	Name = Wing1, index = 2
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 3
	Name = Farfield, index = 1
	Name = Wing1, index = 2
	Name = trailingEdge, index = 3

Getting mesh sizing parameters
	Mesh sizing name - Farfield
	Done getting mesh sizing parameters
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 2
	Name = Farfield, index = 1
	Name = Wing1, index = 2
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 2
	Name = Farfield, index = 1
	Name = Wing1, index = 2
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 3
	Name = Farfield, index = 1
	Name = Wing1, index = 2
	Name = trailingEdge, index = 3

Getting mesh sizing parameters
	Mesh sizing name - Farfield
	Done getting mesh sizing parameters
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 2
	Name = Farfield, index = 1
	Name = Wing1, index = 2
Number of surface: nodes - 7151, elements - 14294
Getting volume mesh

Generating volume mesh using TetGen.....

Tetgen input string = pYq1.500/0.000QT1.00e-16A
Done meshing using TetGen!
ok
test_reenter (test_tetgen.TestTETGEN.test_reenter) ... 
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 2
	Name = Farfield, index = 1
	Name = Wing1, index = 2
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 3
	Name = Farfield, index = 1
	Name = Wing1, index = 2
	Name = trailingEdge, index = 3

Getting mesh sizing parameters
	Mesh sizing name - Farfield
	Done getting mesh sizing parameters
Getting surface mesh for body 1 (of 1)
Body 1 (of 1)
Number of nodes    = 9583
Number of elements = 19158
Number of triangle elements      = 19158
Number of quadrilateral elements = 0
----------------------------
Total number of nodes    = 9583
Total number of elements = 19158
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 2
	Name = Farfield, index = 1
	Name = Wing1, index = 2
Number of surface: nodes - 9583, elements - 19158
Getting volume mesh

Generating volume mesh using TetGen.....

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

Writing Binary VTK file ....
Finished writing Binary VTK file


Writing vtk file ....

Writing vtk general file ....
Finished writing vtk file


Writing FAST file ....
Finished writing FAST file


Writing SU2 file ....
Finished writing SU2 file


Writing exodus file ....
	Block: 'Block1_tet', blk_id 1, num_entries 104182
	Sideset: 'Farfield', set_id 1, num_entries 48
	Sideset: 'Wing1', set_id 2, num_entries 19110
Finished writing Exodus file


Writing Binary STL file ....
Finished writing Binary STL file


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


Writing Tecplot file ....
Finished writing Tecplot file

Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 2
	Name = Farfield, index = 1
	Name = Wing1, index = 2
Number of surface: nodes - 9583, elements - 19158
Getting volume mesh

Generating volume mesh using TetGen.....

Tetgen input string = pYq2.000/0.000QT1.00e-16A
Done meshing using TetGen!

Writing Binary VTK file ....
Finished writing Binary VTK file


Writing vtk file ....

Writing vtk general file ....
Finished writing vtk file


Writing FAST file ....
Finished writing FAST file


Writing SU2 file ....
Finished writing SU2 file


Writing exodus file ....
	Block: 'Block1_tet', blk_id 1, num_entries 69273
	Sideset: 'Farfield', set_id 1, num_entries 48
	Sideset: 'Wing1', set_id 2, num_entries 19110
Finished writing Exodus file


Writing Binary STL file ....
Finished writing Binary STL file


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


Writing Tecplot file ....
Finished writing Tecplot file

ok
test_setInput (test_tetgen.TestTETGEN.test_setInput) ...  EGADS Info: 0 Objects, 0 Reference in Use (of 0) at Close!
ok
test_Cl (test_xfoil.Testxfoil_Kulfan.test_Cl) ... 
ok
test_alpha_custom_increment (test_xfoil.Testxfoil_Kulfan.test_alpha_custom_increment) ... ok
test_CL_uniform_increment (test_xfoil.Testxfoil_NACA.test_CL_uniform_increment) ... 
ok
test_Cl (test_xfoil.Testxfoil_NACA.test_Cl) ... ok
test_alpha_custom_increment (test_xfoil.Testxfoil_NACA.test_alpha_custom_increment) ... ok
test_alpha_uniform_inrement (test_xfoil.Testxfoil_NACA.test_alpha_uniform_inrement) ... ok
test_append (test_xfoil.Testxfoil_NACA.test_append) ... ok
test_normalize (test_xfoil.Testxfoil_NACA.test_normalize) ... 
ok
test_phase (test_xfoil.Testxfoil_NACA.test_phase) ... 

ok
test_Output (test_zaero.TestZAERO.test_Output) ... ok
test_inputs (test_zaero.TestZAERO.test_inputs) ... 
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 6
	Name = Ribs, index = 1
	Name = Skin, index = 2
	Name = Spar1, index = 3
	Name = Rib_Root, index = 4
	Name = Spar2, index = 5
	Name = Rib_Root_Point, index = 6
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 2
	Name = LeadingEdge, index = 1
	Name = TrailingEdge, index = 2
Getting surface mesh for body 1 (of 2)
Getting surface mesh for body 2 (of 2)
Body 1 (of 2)
Number of nodes    = 1220
Number of elements = 2680
Number of triangle elements      = 2680
Number of quadrilateral elements = 0
Body 2 (of 2)
Number of nodes    = 1
Number of elements = 0
Number of triangle elements      = 0
Number of quadrilateral elements = 0
----------------------------
Total number of nodes    = 1221
Total number of elements = 2680
Mapping Csys attributes ................
	Number of unique Csys attributes = 0

Getting FEA coordinate systems.......
	Number of coordinate systems - 0
	No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
	Number of unique capsConstraint attributes = 1
	Name = Rib_Root_Point, index = 1
Mapping capsLoad attributes ................
	Number of unique capsLoad attributes = 0
Mapping capsBound attributes ................
	Number of unique capsBound attributes = 1
	Name = Skin_Top, index = 1
Mapping capsConnect attributes ................
	Number of unique capsConnect attributes = 1
	Name = Rib_Root, index = 1
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 6
	Name = Ribs, index = 1
	Name = Skin, index = 2
	Name = Spar1, index = 3
	Name = Rib_Root, index = 4
	Name = Spar2, index = 5
	Name = Rib_Root_Point, index = 6
Setting FEA Data
	Mesh for body = 0
	Number of nodal coordinates = 1220
	Number of elements = 2680
	Elemental Nodes = 0
	Elemental Rods  = 0
	Elemental Tria3 = 2680
	Elemental Quad4 = 0
Setting FEA Data
	Mesh for body = 1
	Number of nodal coordinates = 1
	Number of elements = 1
	Elemental Nodes = 1
	Elemental Rods  = 0
	Elemental Tria3 = 0
	Elemental Quad4 = 0
Combining multiple FEA meshes!
	Combined Number of nodal coordinates = 1221
	Combined Number of elements = 2681
	Combined Elemental Nodes = 1
	Combined Elemental Rods  = 0
	Combined Elemental Tria3 = 2680
	Combined Elemental Quad4 = 0

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

Getting FEA properties.......
	Number of properties - 6
	Property name - Rib_Root
	Property name - Rib_Root_Point
	Property name - Ribs
	Property name - Skin
	Property name - Spar1
	Property name - Spar2
	Done getting FEA properties
Updating mesh element types based on properties input

'Smart_Restart' is ON
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = Wing, index = 1
Getting vortex lattice surface data
	VLM surface name - WingSurface
	Done getting vortex lattice surface data
Getting vortex lattice control surface data
	VLM control surface name - CntrlLE
	VLM control surface name - CntrlTE
	Done getting vortex lattice control surface data

Getting FEA vortex lattice mesh

Getting ZAERO UAIC Configurations.......
	Number of UAIC Configurations - 2

	UAIC Configuration: climb, id = 1
	- Mach Number : 0.200000
	- Reduced Freq: [0.020000, ... , 0.250000]

	UAIC Configuration: cruise, id = 2
	- Mach Number : 0.700000
	- Reduced Freq: [0.040000, ... , 0.350000]

Getting ZAERO Analysis Subcases.......
	Number of Analysis Subcases - 2

	Analysis Subcase: FlutterCruise, id = 1
	- Discipline : flutter
	- UAIC       : cruise

	Analysis Subcase: Trim, id = 2
	- Discipline : Trim
	- UAIC       : climb

Getting ZAERO Trim Variables.......
	Number of Trim Variables - 2

	Trim Variable: ANGLEA
	- Label : ALPHA
	- Value : free

	Trim Variable: URDD3
	- Label : NZ
	- Value : 1.0

	Updating StaticAeroelastic subcase: Trim
	- vectorToCG -> [0.345898, 1.652951, -0.041403]
	- weight -> 476456.149985
	- weightMomentOfInertia -> [304902.643270, 98963.803823, 69822.813293, 6179.981375, 19723.152208, 370546.335525]
ok

----------------------------------------------------------------------
Ran 143 tests in 761.759s

OK (skipped=10)
+ cd /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/CAPSexamples/
+ make test TYPE=MINIMAL
(make -C cCAPS -f aeroelastic_SU2.make)
make[1]: `aeroelasticSimple_Iterative_SU2_and_MystranTest' is up to date.
(make -C cCAPS -f avlTest.make)
make[1]: `avlTest' is up to date.
(make -C cCAPS -f awaveTest.make)
make[1]: `awaveTest' is up to date.
(make -C cCAPS -f frictionTest.make)
make[1]: `frictionTest' is up to date.
(make -C cCAPS -f fun3d.make)
make[1]: Nothing to be done for `fun3d'.
(make -C cCAPS -f hsm.make)
make[1]: `hsm' is up to date.
(make -C cCAPS -f interferenceTest.make)
make[1]: `interferenceTest' is up to date.
(make -C cCAPS -f msesTest.make)
make[1]: `msesTest' is up to date.
(make -C cCAPS -f mystran.make)
make[1]: `mystranTest' is up to date.
(make -C cCAPS -f pointwiseTest.make)
make[1]: `pointwiseTest' is up to date.
(cd ./regressionTest; ./execute_CTestRegression.sh MINIMAL)
Running.... MINIMAL c-Tests

All tests pass!


=================================================
=================================================
(cd ./regressionTest; ./execute_PyTestRegression.sh MINIMAL)

=================================================
Using python : /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/ESP_venv/bin/python
=================================================

Running.... MINIMAL PyTests

=================================================
+ echo 'avl_PyTest.py test;'
+ tee -a /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
avl_PyTest.py test;
+ python -u avl_PyTest.py -outLevel=0
+ tee -a /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
Loading AIM

Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = Wing, index = 1
Getting vortex lattice surface data
	VLM surface name - Wing
	Done getting vortex lattice surface data
Writing surface - Wing (ID = 0)
	Section 1 of 3 (ID = 0)
	Section 2 of 3 (ID = 1)
	Section 3 of 3 (ID = 2)
CXtot   0.0006119078685800925
CYtot   -6.292592518559147e-15
CZtot   -0.3012861394881712
Cltot   -4.783069014642483e-14
Cmtot   -0.1945055953448147
Cntot   -2.338890054396671e-15
Cl'tot  -4.786422456048383e-14
Cn'tot  -1.50377318550154e-15
CLtot   0.3012509314146395
CDtot   0.00464635348821979
CDvis   0.0
CLff    0.3009503023516151
CYff    -7.7198870803959e-15
CDind   0.00464635348821979
CDff    0.004968969500894849
e       0.9669902146155998
StripForces 
Wing  cl =  [0.02994790451338, 0.08555545178909, 0.1329003532584, 0.1733025192691, 0.2100182422829, 0.2453427152542, 0.279274699636, 0.3101221284185, 0.3355632628219, 0.3531618776071, 0.3603457261529, 0.3542128805661, 0.3542128805657, 0.3603457261529, 0.3531618776083, 0.3355632628247, 0.3101221284231, 0.2792746996423, 0.2453427152618, 0.2100182422917, 0.1733025192796, 0.132900353272, 0.08555545180763, 0.0299479045407]
Wing  cd =  [-0.004234137763148, -0.004494543653181, -0.003752887372721, -0.002739626801633, -0.001762021024329, -0.0007386538946456, 0.0005114598078319, 0.00211914728609, 0.00414518990896, 0.006609094404164, 0.009540018987574, 0.01315518814705, 0.01315518814715, 0.00954001898777, 0.006609094404422, 0.004145189909247, 0.002119147286374, 0.0005114598080921, -0.0007386538944123, -0.001762021024098, -0.002739626801367, -0.003752887372442, -0.004494543653152, -0.00423413776453]

real	0m0.825s
user	0m0.720s
sys	0m0.245s
+ status=0
+ set +x

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


=================================================
+ echo 'xfoil_PyTest.py test;'
+ tee -a /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
xfoil_PyTest.py test;
+ python -u xfoil_PyTest.py -outLevel=0 -noPlotData
+ tee -a /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/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	0m3.808s
user	0m3.303s
sys	0m0.132s
+ status=0
+ set +x

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


=================================================
+ echo 'mses_PyTest.py test;'
+ tee -a /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
mses_PyTest.py test;
+ python -u mses_PyTest.py -outLevel=0 -noPlotData
+ tee -a /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt

Cl =  0.3783791085548177
Cd =  0.007775858417209677
Cm =  0.005262636995835036

real	0m3.671s
user	0m3.130s
sys	0m0.157s
+ status=0
+ set +x

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


=================================================
+ echo 'friction_PyTest.py test;'
+ tee -a /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
friction_PyTest.py test;
+ python -u friction_PyTest.py -outLevel=0
+ tee -a /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/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	0m0.633s
user	0m0.659s
sys	0m0.129s
+ status=0
+ set +x

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


=================================================
+ echo 'tsfoil_PyTest.py test;'
+ tee -a /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
tsfoil_PyTest.py test;
+ python -u tsfoil_PyTest.py -outLevel=0
+ tee -a /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/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	0m0.522s
user	0m0.641s
sys	0m0.103s
+ status=0
+ set +x

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


=================================================
+ echo 'delaundo_PyTest.py test;'
+ tee -a /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
delaundo_PyTest.py test;
+ python -u delaundo_PyTest.py -outLevel=0
+ tee -a /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt

Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 6
	Name = 2DSlice, index = 1
	Name = TunnelWall, index = 2
	Name = OutFlow, index = 3
	Name = InFlow, index = 4
	Name = Airfoil, index = 5
	Name = AirfoilTE, index = 6
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 6
	Name = 2DSlice, index = 1
	Name = TunnelWall, index = 2
	Name = OutFlow, index = 3
	Name = InFlow, index = 4
	Name = Airfoil, index = 5
	Name = AirfoilTE, index = 6

Getting mesh sizing parameters
	Mesh sizing name - Airfoil
	Mesh sizing name - AirfoilTE
	Mesh sizing name - InFlow
	Mesh sizing name - OutFlow
	Mesh sizing name - TunnelWall
	Done getting mesh sizing parameters
Getting edge discretization for body 1
	Delaundo expects 2D meshes in the x-y plane... attempting to rotate mesh through node swapping!
	Swapping z and y coordinates!
Writing delaundo control file - delaundo.ctr
	Writing out *.pts file
Reading delaundo mesh file - delaundo_CAPS.mesh
	Swapping y and z coordinates!

Writing Tecplot file ....
Tecplot expects 2D meshes in the x-y plane... attempting to rotate mesh!
Swapping z and y coordinates!
Finished writing Tecplot file


Writing ugrid file ....
Finished writing ugrid file


real	0m0.720s
user	0m0.843s
sys	0m0.343s
+ status=0
+ set +x

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


=================================================
+ echo 'egadsTess_PyTest.py test;'
+ tee -a /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
egadsTess_PyTest.py test;
+ python -u egadsTess_PyTest.py -outLevel=0
+ tee -a /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt

Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 7
	Name = Ribs, index = 1
	Name = Skin, index = 2
	Name = Spar1, index = 3
	Name = Rib_Root, index = 4
	Name = Spar2, index = 5
	Name = Rib_Root_Point, index = 6
	Name = Wing, index = 7
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 2
	Name = LeadingEdge, index = 1
	Name = TrailingEdge, index = 2

Getting mesh sizing parameters
	Mesh sizing name - LeadingEdge
	Done getting mesh sizing parameters
Getting surface mesh for body 1 (of 4)
Getting surface mesh for body 2 (of 4)
Getting surface mesh for body 3 (of 4)
Getting surface mesh for body 4 (of 4)
Body 1 (of 4)
Number of nodes    = 3793
Number of elements = 4001
Number of triangle elements      = 0
Number of quadrilateral elements = 4001
Body 2 (of 4)
Number of nodes    = 1
Number of elements = 0
Number of triangle elements      = 0
Number of quadrilateral elements = 0
Body 3 (of 4)
Number of nodes    = 76
Number of elements = 55
Number of triangle elements      = 0
Number of quadrilateral elements = 55
Body 4 (of 4)
Number of nodes    = 100
Number of elements = 73
Number of triangle elements      = 0
Number of quadrilateral elements = 73
----------------------------
Total number of nodes    = 3970
Total number of elements = 4129

Writing Tecplot file ....
Finished writing Tecplot file


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


Writing ugrid file ....
Finished writing ugrid file


real	0m6.422s
user	0m12.509s
sys	0m5.004s
+ status=0
+ set +x

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


=================================================
+ echo 'aflr2_PyTest.py test;'
+ tee -a /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
aflr2_PyTest.py test;
+ python -u aflr2_PyTest.py -outLevel=0
+ tee -a /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt

Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 5
	Name = 2DSlice, index = 1
	Name = TunnelWall, index = 2
	Name = OutFlow, index = 3
	Name = InFlow, index = 4
	Name = Airfoil, index = 5
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 4
	Name = TunnelWall, index = 1
	Name = OutFlow, index = 2
	Name = InFlow, index = 3
	Name = Airfoil, index = 4

Getting mesh sizing parameters
	Mesh sizing name - 2DSlice
	Mesh sizing name - Airfoil
	Mesh sizing name - InFlow
	Mesh sizing name - OutFlow
	Mesh sizing name - TunnelWall
	Done getting mesh sizing parameters
Getting 2D mesh for body 1 (of 1)
 
AFLR2    : ---------------------------------------
AFLR2    : AFLR2 LIBRARY
AFLR2    : ADVANCING-FRONT/LOCAL-RECONNECTION
AFLR2    : TRIA/QUAD GRID GENERATOR
AFLR2    : Version Number 9.17.15
AFLR2    : Version Date   04/23/24 @ 12:51AM
AFLR2    : Compile OS     Darwin 23.4.0 arm64
AFLR2    : Compile Date   04/23/24 @ 12:51AM
AFLR2    : Copyright 1994-2021, D.L. Marcum
AFLR2    : ---------------------------------------
 
AFLR2 IC : INPUT DATA CHECK
 
AFLR2 IC : Nodes, Faces      =       344         0
 
AFLR2    : CPU Time          =     0.000   seconds
 
AFLR2 EG : EDGE GRID RE-GENERATION
 
AFLR2 EG : Nodes, Edges      =       344       344
 
AFLR2    : CPU Time          =     0.000   seconds
 
AFLR2 IG : INITIAL GRID GENERATION
 
AFLR2 IG : Nodes, Faces      =         0         2
AFLR2 IG : Nodes, Faces      =        70       142
AFLR2 IG : Nodes, Faces      =       140       282
AFLR2 IG : Nodes, Faces      =       210       422
AFLR2 IG : Nodes, Faces      =       280       562
AFLR2 IG : Nodes, Faces      =       316       634
AFLR2 IG : Nodes, Faces      =       344       690
AFLR2 IG : Nodes, Faces      =       348       690
AFLR2 IG : Nodes, Faces      =       344       344
 
AFLR2    : CPU Time          =     0.000   seconds
 
AFLR2 GG : FIELD GRID GENERATION
 
AFLR2 GGp: Nodes, Faces      =       344       344
AFLR2 GGp: Nodes, Faces      =       681      1018
AFLR2 GGp: Nodes, Faces      =      1013      1682
AFLR2 GGp: Nodes, Faces      =      1339      2334
AFLR2 GGp: Nodes, Faces      =      1652      2960
AFLR2 GGp: Nodes, Faces      =      1957      3570
AFLR2 GGp: Nodes, Faces      =      2252      4160
AFLR2 GGp: Nodes, Faces      =      2526      4708
AFLR2 GGp: Nodes, Faces      =      2809      5274
AFLR2 GGp: Nodes, Faces      =      3083      5822
AFLR2 GGp: Nodes, Faces      =      3327      6310
AFLR2 GGp: Nodes, Faces      =      3564      6784
AFLR2 GGp: Nodes, Faces      =      3788      7232
AFLR2 GGp: Nodes, Faces      =      3995      7646
AFLR2 GGp: Nodes, Faces      =      4194      8044
AFLR2 GGp: Nodes, Faces      =      4394      8444
AFLR2 GGp: Nodes, Faces      =      4585      8826
AFLR2 GGp: Nodes, Faces      =      4772      9200
AFLR2 GGp: Nodes, Faces      =      4943      9542
AFLR2 GGp: Nodes, Faces      =      5129      9914
AFLR2 GGp: Nodes, Faces      =      5293     10242
AFLR2 GGp: Nodes, Faces      =      5447     10550
AFLR2 GGp: Nodes, Faces      =      5594     10844
AFLR2 GGp: Nodes, Faces      =      5716     11088
AFLR2 GGp: Nodes, Faces      =      5830     11316
AFLR2 GGp: Nodes, Faces      =      5909     11474
AFLR2 GGp: Nodes, Faces      =      5964     11584
AFLR2 GGp: Nodes, Faces      =      6006     11668
AFLR2 GGp: Nodes, Faces      =      6025     11706
AFLR2 GGp: Nodes, Faces      =      6034     11724
 
AFLR2    : CPU Time          =     0.010   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          =     0.006   seconds
 
AFLR2    : DONE
EGADS Internal: Face 1, Side 4741 4722 complete [but 7915] (EG_makeConnect)!
EGADS Internal: Face 1, Side 4741 4912 complete [but 7916] (EG_makeConnect)!
EGADS Internal: Face 1, Side 5850 5858 complete [but 8742] (EG_makeConnect)!
EGADS Internal: Face 1, Side 5850 5851 complete [but 8742] (EG_makeConnect)!
EGADS Internal: Face 1, Side 5858 5851 complete [but 8791] (EG_makeConnect)!
EGADS Internal: Face 1, Side 4912 4722 complete [but 9417] (EG_makeConnect)!

Writing AFLR3 file ....
Finished writing AFLR3 file

Number of nodes = 6031
Number of elements = 6448
Number of tris = 488
Number of quad = 5616
EGADS Internal: Face 1, Side 4741 4722 complete [but 7915] (EG_makeConnect)!
EGADS Internal: Face 1, Side 4741 4912 complete [but 7916] (EG_makeConnect)!
EGADS Internal: Face 1, Side 5850 5858 complete [but 8742] (EG_makeConnect)!
EGADS Internal: Face 1, Side 5850 5851 complete [but 8742] (EG_makeConnect)!
EGADS Internal: Face 1, Side 5858 5851 complete [but 8791] (EG_makeConnect)!
EGADS Internal: Face 1, Side 4912 4722 complete [but 9417] (EG_makeConnect)!
EGADS Internal: Face 1, Side 4741 4722 complete [but 7915] (EG_makeConnect)!
EGADS Internal: Face 1, Side 4741 4912 complete [but 7916] (EG_makeConnect)!
EGADS Internal: Face 1, Side 5850 5858 complete [but 8742] (EG_makeConnect)!
EGADS Internal: Face 1, Side 5850 5851 complete [but 8742] (EG_makeConnect)!
EGADS Internal: Face 1, Side 5858 5851 complete [but 8791] (EG_makeConnect)!
EGADS Internal: Face 1, Side 4912 4722 complete [but 9417] (EG_makeConnect)!

Writing Tecplot file ....
Tecplot expects 2D meshes in the x-y plane... attempting to rotate mesh!
Swapping z and y coordinates!
Finished writing Tecplot file


real	0m0.806s
user	0m0.945s
sys	0m0.347s
+ status=0
+ set +x

=================================================
CAPS verification (using pyCAPS) case aflr2_PyTest.py passed (as expected)
=================================================


=================================================
+ echo 'aflr4_and_aflr3_PyTest.py test;'
+ tee -a /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/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_Beta/7.8/DARWIN_ARM64/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt

Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 4
	Name = Wing1, index = 1
	Name = Wing2, index = 2
	Name = Wake, index = 3
	Name = Farfield, index = 4
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 4
	Name = Wing1, index = 1
	Name = Wing2, index = 2
	Name = Wake, index = 3
	Name = Farfield, index = 4
AFLR4    : Proximity BG Surface Grid Generation Skipped
AFLR4    : No Modifications Required

Writing Tecplot file ....
Finished writing Tecplot file


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


Writing ugrid file ....
Finished writing ugrid file

Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 4
	Name = Wing1, index = 1
	Name = Wing2, index = 2
	Name = Wake, index = 3
	Name = Farfield, index = 4
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 4
	Name = Wing1, index = 1
	Name = Wing2, index = 2
	Name = Wake, index = 3
	Name = Farfield, index = 4

Getting mesh sizing parameters
	Mesh sizing name - Wing1
	Mesh sizing name - Wing2
	Done getting mesh sizing parameters
Getting volume mesh
 
AFLR2    : ---------------------------------------
AFLR2    : AFLR2 LIBRARY
AFLR2    : ADVANCING-FRONT/LOCAL-RECONNECTION
AFLR2    : TRIA/QUAD GRID GENERATOR
AFLR2    : Version Number 9.17.15
AFLR2    : Version Date   04/23/24 @ 12:51AM
AFLR2    : Compile OS     Darwin 23.4.0 arm64
AFLR2    : Compile Date   04/23/24 @ 12:51AM
AFLR2    : Copyright 1994-2021, D.L. Marcum
AFLR2    : ---------------------------------------
 
AFLR4    : ---------------------------------------
AFLR4    : AFLR4 LIBRARY
AFLR4    : ADVANCING-FRONT/LOCAL-RECONNECTION
AFLR4    : TRIA/QUAD SURFACE GRID GENERATOR
AFLR4    : Version Number 11.5.14
AFLR4    : Version Date   04/18/24 @ 12:45PM
AFLR4    : Compile OS     Darwin 23.4.0 arm64
AFLR4    : Compile Date   04/18/24 @ 03:04PM
AFLR4    : Copyright 1994-2021, D.L. Marcum
AFLR4    : ---------------------------------------

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

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------
Volume mesh:
	Number of nodes          = 150214
	Number of elements       = 450024
	Number of triangles      = 14380
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 214592
	Number of pyramids       = 425
	Number of prisms         = 220627
	Number of hexahedrals    = 0

Writing Tecplot file ....
Finished writing Tecplot file


real	0m14.287s
user	0m11.276s
sys	0m0.368s
+ status=0
+ set +x

=================================================
CAPS verification (using pyCAPS) case aflr4_and_aflr3_PyTest.py passed (as expected)
=================================================


=================================================
+ echo 'tetgen_PyTest.py test;'
+ tee -a /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
tetgen_PyTest.py test;
+ python -u tetgen_PyTest.py -outLevel=0
+ tee -a /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt

Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 3
	Name = Wing1, index = 1
	Name = Wing2, index = 2
	Name = Farfield, index = 3
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 3
	Name = Wing1, index = 1
	Name = Wing2, index = 2
	Name = Farfield, index = 3
Getting surface mesh for body 1 (of 3)
Getting surface mesh for body 2 (of 3)
Getting surface mesh for body 3 (of 3)
Body 1 (of 3)
Number of nodes    = 2236
Number of elements = 4468
Number of triangle elements      = 4468
Number of quadrilateral elements = 0
Body 2 (of 3)
Number of nodes    = 636
Number of elements = 1268
Number of triangle elements      = 1268
Number of quadrilateral elements = 0
Body 3 (of 3)
Number of nodes    = 258
Number of elements = 512
Number of triangle elements      = 512
Number of quadrilateral elements = 0
----------------------------
Total number of nodes    = 3130
Total number of elements = 6248

Writing Tecplot file ....
Finished writing Tecplot file

Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 3
	Name = Wing1, index = 1
	Name = Wing2, index = 2
	Name = Farfield, index = 3
Number of surface: nodes - 3130, elements - 6248
Getting volume mesh

Generating volume mesh using TetGen.....

Tetgen input string = pYq1.500/0.000T1.00e-16A
Delaunizing vertices...
Delaunay seconds:  0.030698
Creating surface mesh ...
Surface mesh seconds:  0.006452
Recovering boundaries...
Boundary recovery seconds:  0.080571
Removing exterior tetrahedra ...
Spreading region attributes.
Exterior tets removal seconds:  0.00354
Suppressing Steiner points ...
Steiner suppression seconds:  9e-06
Recovering Delaunayness...
Delaunay recovery seconds:  0.014129
Refining mesh...
  4177 insertions, added 2159 points, 136953 tetrahedra in queue.
  1390 insertions, added 372 points, 139199 tetrahedra in queue.
  1853 insertions, added 454 points, 136118 tetrahedra in queue.
  2470 insertions, added 521 points, 118263 tetrahedra in queue.
  3293 insertions, added 464 points, 66933 tetrahedra in queue.
  4389 insertions, added 406 points, 1337 tetrahedra in queue.
  5851 insertions, added 599 points, 33 tetrahedra in queue.
Refinement seconds:  0.758419
Smoothing vertices...
Mesh smoothing seconds:  0.450576
Improving mesh...
Mesh improvement seconds:  0.00858
Jettisoning redundant points.

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

Output seconds:  0.002192
Total running seconds:  1.35547

Statistics:

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

  Mesh points: 8156
  Mesh tetrahedra: 40155
  Mesh faces: 83435
  Mesh faces on exterior boundary: 6250
  Mesh faces on input facets: 6250
  Mesh edges on input segments: 9373
  Steiner points on input segments:  1
  Steiner points inside domain: 5025

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

Writing Tecplot file ....
Finished writing Tecplot file


real	0m3.120s
user	0m2.736s
sys	0m0.218s
+ status=0
+ set +x

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


=================================================
+ echo 'su2_and_AFLR2_PyTest.py test;'
+ tee -a /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/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_Beta/7.8/DARWIN_ARM64/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
Saving geometry

Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 5
	Name = 2DSlice, index = 1
	Name = TunnelWall, index = 2
	Name = OutFlow, index = 3
	Name = InFlow, index = 4
	Name = Airfoil, index = 5
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 4
	Name = TunnelWall, index = 1
	Name = OutFlow, index = 2
	Name = InFlow, index = 3
	Name = Airfoil, index = 4

Getting mesh sizing parameters
	Mesh sizing name - 2DSlice
	Mesh sizing name - Airfoil
	Mesh sizing name - InFlow
	Mesh sizing name - OutFlow
	Mesh sizing name - TunnelWall
	Done getting mesh sizing parameters
Getting 2D mesh for body 1 (of 1)
 
AFLR2    : ---------------------------------------
AFLR2    : AFLR2 LIBRARY
AFLR2    : ADVANCING-FRONT/LOCAL-RECONNECTION
AFLR2    : TRIA/QUAD GRID GENERATOR
AFLR2    : Version Number 9.17.15
AFLR2    : Version Date   04/23/24 @ 12:51AM
AFLR2    : Compile OS     Darwin 23.4.0 arm64
AFLR2    : Compile Date   04/23/24 @ 12:51AM
AFLR2    : Copyright 1994-2021, D.L. Marcum
AFLR2    : ---------------------------------------
 
AFLR2 IC : INPUT DATA CHECK
 
AFLR2 IC : Nodes, Faces      =       545         0
 
AFLR2    : CPU Time          =     0.000   seconds
 
AFLR2 EG : EDGE GRID RE-GENERATION
 
AFLR2 EG : Nodes, Edges      =       545       545
 
AFLR2    : CPU Time          =     0.000   seconds
 
AFLR2 IG : INITIAL GRID GENERATION
 
AFLR2 IG : Nodes, Faces      =         0         2
AFLR2 IG : Nodes, Faces      =       110       222
AFLR2 IG : Nodes, Faces      =       220       442
AFLR2 IG : Nodes, Faces      =       330       662
AFLR2 IG : Nodes, Faces      =       440       882
AFLR2 IG : Nodes, Faces      =       517      1036
AFLR2 IG : Nodes, Faces      =       545      1092
AFLR2 IG : Nodes, Faces      =       549      1092
AFLR2 IG : Nodes, Faces      =       545       545
 
AFLR2    : CPU Time          =     0.001   seconds
 
AFLR2 GG : FIELD GRID GENERATION
 
AFLR2 GGp: Nodes, Faces      =       545       545
AFLR2 GGp: Nodes, Faces      =      1083      1621
AFLR2 GGp: Nodes, Faces      =      1616      2687
AFLR2 GGp: Nodes, Faces      =      2144      3743
AFLR2 GGp: Nodes, Faces      =      2661      4777
AFLR2 GGp: Nodes, Faces      =      3171      5797
AFLR2 GGp: Nodes, Faces      =      3672      6799
AFLR2 GGp: Nodes, Faces      =      4158      7771
AFLR2 GGp: Nodes, Faces      =      4653      8761
AFLR2 GGp: Nodes, Faces      =      5142      9739
AFLR2 GGp: Nodes, Faces      =      5608     10671
AFLR2 GGp: Nodes, Faces      =      6055     11565
AFLR2 GGp: Nodes, Faces      =      6482     12419
AFLR2 GGp: Nodes, Faces      =      6880     13215
AFLR2 GGp: Nodes, Faces      =      7257     13969
AFLR2 GGp: Nodes, Faces      =      7614     14683
AFLR2 GGp: Nodes, Faces      =      7947     15349
AFLR2 GGp: Nodes, Faces      =      8276     16007
AFLR2 GGp: Nodes, Faces      =      8575     16605
AFLR2 GGp: Nodes, Faces      =      8869     17193
AFLR2 GGp: Nodes, Faces      =      9140     17735
AFLR2 GGp: Nodes, Faces      =      9401     18257
AFLR2 GGp: Nodes, Faces      =      9654     18763
AFLR2 GGp: Nodes, Faces      =      9887     19229
AFLR2 GGp: Nodes, Faces      =     10110     19675
AFLR2 GGp: Nodes, Faces      =     10315     20085
AFLR2 GGp: Nodes, Faces      =     10497     20449
AFLR2 GGp: Nodes, Faces      =     10656     20767
AFLR2 GGp: Nodes, Faces      =     10791     21037
AFLR2 GGp: Nodes, Faces      =     10919     21293
AFLR2 GGp: Nodes, Faces      =     11022     21499
AFLR2 GGp: Nodes, Faces      =     11092     21639
AFLR2 GGp: Nodes, Faces      =     11145     21745
AFLR2 GGp: Nodes, Faces      =     11156     21767
 
AFLR2    : CPU Time          =     0.035   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          =     0.018   seconds
 
AFLR2    : DONE
EGADS Internal: Face 1, Side 11077 11153 complete [but 18248] (EG_makeConnect)!
EGADS Internal: Face 1, Side 10985 11077 complete [but 18248] (EG_makeConnect)!
EGADS Internal: Face 1, Side 10985 11152 complete [but 18249] (EG_makeConnect)!
EGADS Internal: Face 1, Side 11152 11153 complete [but 19022] (EG_makeConnect)!

Writing AFLR3 file ....
Finished writing AFLR3 file

Number of nodes = 11153
Number of elements = 11885
Number of tris = 917
Number of quad = 10423
EGADS Internal: Face 1, Side 11077 11153 complete [but 18248] (EG_makeConnect)!
EGADS Internal: Face 1, Side 10985 11077 complete [but 18248] (EG_makeConnect)!
EGADS Internal: Face 1, Side 10985 11152 complete [but 18249] (EG_makeConnect)!
EGADS Internal: Face 1, Side 11152 11153 complete [but 19022] (EG_makeConnect)!
EGADS Internal: Face 1, Side 11077 11153 complete [but 18248] (EG_makeConnect)!
EGADS Internal: Face 1, Side 10985 11077 complete [but 18248] (EG_makeConnect)!
EGADS Internal: Face 1, Side 10985 11152 complete [but 18249] (EG_makeConnect)!
EGADS Internal: Face 1, Side 11152 11153 complete [but 19022] (EG_makeConnect)!

Writing Tecplot file ....
Tecplot expects 2D meshes in the x-y plane... attempting to rotate mesh!
Swapping z and y coordinates!
Finished writing Tecplot file


Writing SU2 file ....
SU2 expects 2D meshes in the x-y plane... attempting to rotate mesh!
Swapping z and y coordinates!
Finished writing SU2 file

Getting CFD boundary conditions
	Boundary condition name - Airfoil
	Boundary condition name - InFlow
	Boundary condition name - OutFlow
	Boundary condition name - TunnelWall
	Done getting CFD boundary conditions
Warning: The su2 cfg file will be overwritten!
Write SU2 configuration file for version "Harrier (8.0.1)"


Running SU2......

-------------------------------------------------------------------------
|    ___ _   _ ___                                                      |
|   / __| | | |_  )   Release 8.0.0 "Harrier"                           |
|   \__ \ |_| |/ /                                                      |
|   |___/\___//___|   Suite (Computational Fluid Dynamics Code)         |
|                                                                       |
-------------------------------------------------------------------------
| SU2 Project Website: https://su2code.github.io                        |
|                                                                       |
| The SU2 Project is maintained by the SU2 Foundation                   |
| (http://su2foundation.org)                                            |
-------------------------------------------------------------------------
| Copyright 2012-2023, SU2 Contributors                                 |
|                                                                       |
| SU2 is free software; you can redistribute it and/or                  |
| modify it under the terms of the GNU Lesser General Public            |
| License as published by the Free Software Foundation; either          |
| version 2.1 of the License, or (at your option) any later version.    |
|                                                                       |
| SU2 is distributed in the hope that it will be useful,                |
| but WITHOUT ANY WARRANTY; without even the implied warranty of        |
| MERCHANTABILITY or FITNESS FOR A PARTICULAR PURPOSE. See the GNU      |
| Lesser General Public License for more details.                       |
|                                                                       |
| You should have received a copy of the GNU Lesser General Public      |
| License along with SU2. If not, see <http://www.gnu.org/licenses/>.   |
-------------------------------------------------------------------------

Parsing config file for zone 0

----------------- Physical Case Definition ( Zone 0 ) -------------------
Compressible Euler equations.
Mach number: 0.4.
Angle of attack (AoA): 0 deg, and angle of sideslip (AoS): 0 deg.
No restart solution, use the values at infinity (freestream).
Dimensional simulation.
The reference area is 1 m^2.
The semi-span will be computed using the max y(3D) value.
The reference length is 1 m.
Reference origin for moment evaluation is (0, 0, 0).
Surface(s) where the force coefficients are evaluated: BC_5.

Surface(s) plotted in the output file: BC_5, BC_2.
Input mesh file name: ../aflr2/aflr2_CAPS.su2

--------------- Space Numerical Integration ( Zone 0 ) ------------------
Roe (with entropy fix = 0.001) solver for the flow inviscid terms.
Standard Roe without low-dissipation function.
Second order integration in space, with slope limiter.
Venkatakrishnan slope-limiting method, with constant: 0.05.
The reference element size is: 1. 
Gradient for upwind reconstruction: inverse-distance weighted Least-Squares.
Gradient for viscous and source terms: inverse-distance weighted Least-Squares.

--------------- Time Numerical Integration  ( Zone 0 ) ------------------
Local time stepping (steady state simulation).
Euler implicit method for the flow equations.
FGMRES is used for solving the linear system.
Using a ILU(0) preconditioning.
Convergence criteria of the linear solver: 1e-06.
Max number of linear iterations: 10.
V Multigrid Cycle, with 2 multigrid levels.
Damping factor for the residual restriction: 0.75.
Damping factor for the correction prolongation: 0.75.
No CFL adaptation.
+-------------------------------------------+
|  MG Level| Presmooth|PostSmooth|CorrectSmo|
+-------------------------------------------+
|         0|         1|         0|         0|
|         1|         2|         0|         0|
|         2|         3|         0|         0|
+-------------------------------------------+
Courant-Friedrichs-Lewy number:       10

------------------ Convergence Criteria  ( Zone 0 ) ---------------------
Maximum number of solver subiterations: 10.
Begin convergence monitoring at iteration 5.
Residual minimum value: 1e-14.
Cauchy series min. value: 1e-10.
Number of Cauchy elements: 100.
Begin windowed time average at iteration 0.

-------------------- Output Information ( Zone 0 ) ----------------------
File writing frequency: 
+------------------------------------+
|                     File| Frequency|
+------------------------------------+
|                  RESTART|       250|
|              SURFACE_CSV|       250|
|                  TECPLOT|       250|
|          SURFACE_TECPLOT|       250|
+------------------------------------+
Writing the convergence history file every 1 inner iterations.
Writing the screen convergence history every 1 inner iterations.
The tabular file format is CSV (.csv).
Convergence history file name: history.
Forces breakdown file name: forces_breakdown_pyCAPS_su2_aflr2.dat.
Surface file name: surface_flow_pyCAPS_su2_aflr2.
Volume file name: flow_pyCAPS_su2_aflr2.
Restart file name: restart_flow_pyCAPS_su2_aflr2.dat.

------------- Config File Boundary Information ( Zone 0 ) ---------------
+-----------------------------------------------------------------------+
|                        Marker Type|                        Marker Name|
+-----------------------------------------------------------------------+
|                         Euler wall|                               BC_5|
|                                   |                               BC_2|
+-----------------------------------------------------------------------+
|                     Inlet boundary|                               BC_4|
+-----------------------------------------------------------------------+
|                    Outlet boundary|                               BC_3|
+-----------------------------------------------------------------------+

-------------------- Output Preprocessing ( Zone 0 ) --------------------

WARNING: SURFACE_PRESSURE_DROP can only be computed for at least 2 surfaces (outlet, inlet, ...)

Screen output fields: TIME_ITER, OUTER_ITER, INNER_ITER, CUR_TIME, TIME_STEP, WALL_TIME, RMS_DENSITY, RMS_MOMENTUM-X, RMS_MOMENTUM-Y, RMS_ENERGY, EFFICIENCY
History output group(s): ITER, TIME_DOMAIN, WALL_TIME, RMS_RES, AERO_COEFF
Convergence field(s): RMS_DENSITY
Warning: No (valid) fields chosen for time convergence monitoring. Time convergence monitoring inactive.
Volume output fields: COORDINATES, SOLUTION, PRIMITIVE

------------------- Geometry Preprocessing ( Zone 0 ) -------------------
Two dimensional problem.
11153 grid points.
11340 volume elements.
4 surface markers.
98 boundary elements in index 0 (Marker = BC_2).
24 boundary elements in index 1 (Marker = BC_3).
24 boundary elements in index 2 (Marker = BC_4).
399 boundary elements in index 3 (Marker = BC_5).
917 triangles.
10423 quadrilaterals.
Setting point connectivity.
Renumbering points (Reverse Cuthill McKee Ordering).
Recomputing point connectivity.
Setting element connectivity.
Checking the numerical grid orientation.
There has been a re-orientation of 917 TRIANGLE volume elements.
There has been a re-orientation of 10423 QUADRILATERAL volume elements.
There has been a re-orientation of 73 LINE surface elements.
Identifying edges and vertices.
Setting the control volume structure.
Area of the computational grid: 999.878.
Searching for the closest normal neighbors to the surfaces.
Storing a mapping from global to local point index.
Compute the surface curvature.
Max K: 385.665. Mean K: 2.15881. Standard deviation K: 17.7215.
Checking for periodicity.
Computing mesh quality statistics for the dual control volumes.
+--------------------------------------------------------------+
|           Mesh Quality Metric|        Minimum|        Maximum|
+--------------------------------------------------------------+
|    Orthogonality Angle (deg.)|        49.3184|             90|
|     CV Face Area Aspect Ratio|        1.00035|        33.4982|
|           CV Sub-Volume Ratio|        1.00001|        7.89914|
+--------------------------------------------------------------+
Setting the multigrid structure.
+-------------------------------------------+
|  MG Level|       CVs|Aggl. Rate|       CFL|
+-------------------------------------------+
|         0|     11153|    1/1.00|        10|
|         1|      2702|    1/4.13|   7.38309|
|         2|       549|    1/4.92|   4.99198|
+-------------------------------------------+
Finding max control volume width.
Wetted area = 2.06265 m.
Area projection in the x-plane = 0.211192 m, y-plane = 0.997011 m.
Max. coordinate in the x-direction = 1 m, y-direction = 0.102037 m.
Min. coordinate in the x-direction = 0.000323229 m, y-direction = -0.108492 m.
Checking if Euler & Symmetry markers are straight/plane:
Boundary marker BC_5 is NOT a single straight.
Boundary marker BC_2 is NOT a single straight.
Computing wall distances.

-------------------- Solver Preprocessing ( Zone 0 ) --------------------
Inviscid flow: Computing density based on free-stream
temperature and pressure using the ideal gas law.
Force coefficients computed using free-stream values.

-- Models:
+------------------------------------------------------------------------------+
|          Viscosity Model|        Conductivity Model|              Fluid Model|
+------------------------------------------------------------------------------+
|                        -|                         -|             STANDARD_AIR|
+------------------------------------------------------------------------------+
-- Fluid properties:
+------------------------------------------------------------------------------+
|                  Name|    Dim. value|    Ref. value|      Unit|Non-dim. value|
+------------------------------------------------------------------------------+
|          Gas Constant|       287.058|             1|  N.m/kg.K|       287.058|
|      Spec. Heat Ratio|             -|             -|         -|           1.4|
+------------------------------------------------------------------------------+
-- Initial and free-stream conditions:
+------------------------------------------------------------------------------+
|                  Name|    Dim. value|    Ref. value|      Unit|Non-dim. value|
+------------------------------------------------------------------------------+
|       Static Pressure|        101325|             1|        Pa|        101325|
|               Density|       1.22498|             1|    kg/m^3|       1.22498|
|           Temperature|        288.15|             1|         K|        288.15|
|          Total Energy|        216054|             1|   m^2/s^2|        216054|
|            Velocity-X|       136.119|             1|       m/s|       136.119|
|            Velocity-Y|             0|             1|       m/s|             0|
|    Velocity Magnitude|       136.119|             1|       m/s|       136.119|
+------------------------------------------------------------------------------+
|           Mach Number|             -|             -|         -|           0.4|
+------------------------------------------------------------------------------+
Initialize Jacobian structure (Euler). MG level: 0.
Initialize Jacobian structure (Euler). MG level: 1.
Initialize Jacobian structure (Euler). MG level: 2.

------------------- Numerics Preprocessing ( Zone 0 ) -------------------

----------------- Integration Preprocessing ( Zone 0 ) ------------------

------------------- Iteration Preprocessing ( Zone 0 ) ------------------
Euler/Navier-Stokes/RANS fluid iteration.

------------------------------ Begin Solver -----------------------------

Simulation Run using the Single-zone Driver
WARNING: SU2 was not compiled for an AVX-capable architecture. Performance could be better,
         see https://su2code.github.io/docs_v7/Build-SU2-Linux-MacOS/#compiler-optimizations
WARNING: SU2 was not compiled for an AVX-capable architecture. Performance could be better,
         see https://su2code.github.io/docs_v7/Build-SU2-Linux-MacOS/#compiler-optimizations
WARNING: SU2 was not compiled for an AVX-capable architecture. Performance could be better,
         see https://su2code.github.io/docs_v7/Build-SU2-Linux-MacOS/#compiler-optimizations
+----------------------------------------------------------------------------------------------------------------------------------------------+
|   Time_Iter|  Outer_Iter|  Inner_Iter|    Cur_Time|   Time_Step|   Time(sec)|    rms[Rho]|   rms[RhoU]|   rms[RhoV]|   rms[RhoE]|        CEff|
+----------------------------------------------------------------------------------------------------------------------------------------------+
|           0|           0|           0|  0.0000e+00|  0.0000e+00|  1.1771e-01|    0.071067|    2.739763|    1.616077|    5.599701|    0.055267|
|           0|           0|           1|  0.0000e+00|  0.0000e+00|  1.1697e-01|   -0.447576|    2.193837|    1.571349|    5.070382|    0.046028|
|           0|           0|           2|  0.0000e+00|  0.0000e+00|  1.1153e-01|   -0.561159|    2.074597|    1.490746|    4.953698|    0.033910|
|           0|           0|           3|  0.0000e+00|  0.0000e+00|  1.0696e-01|   -0.723326|    1.921155|    1.390756|    4.790278|    0.049695|
|           0|           0|           4|  0.0000e+00|  0.0000e+00|  1.0313e-01|   -0.876572|    1.825653|    1.275093|    4.637161|    0.133976|
|           0|           0|           5|  0.0000e+00|  0.0000e+00|  1.0202e-01|   -1.029177|    1.759196|    1.156078|    4.482282|    0.368542|
|           0|           0|           6|  0.0000e+00|  0.0000e+00|  9.8707e-02|   -1.215334|    1.704909|    1.114966|    4.286060|    0.974759|
|           0|           0|           7|  0.0000e+00|  0.0000e+00|  9.9186e-02|   -1.329970|    1.644937|    1.145030|    4.116982|    2.716332|
|           0|           0|           8|  0.0000e+00|  0.0000e+00|  9.9078e-02|   -1.270672|    1.570739|    1.155400|    4.139480|   16.569216|
|           0|           0|           9|  0.0000e+00|  0.0000e+00|  9.7687e-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	0m2.894s
user	0m2.355s
sys	0m0.759s
+ status=0
+ set +x

=================================================
CAPS verification (using pyCAPS) case su2_and_AFLR2_PyTest.py passed (as expected)
=================================================

./execute_PyTestRegression.sh: line 198: ulimit: stack size: cannot modify limit: Operation not permitted

=================================================
+ tee -a /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
+ echo 'cart3d_PyTest.py test;'
cart3d_PyTest.py test;
+ python -u cart3d_PyTest.py -outLevel=0
+ tee -a /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/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  -0.0012129281
C_N  0.065395002
C_D  0.025961197
C_S  -0.0012129281
C_L  0.064528279
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	0m44.481s
user	0m30.898s
sys	0m1.465s
+ status=0
+ set +x

=================================================
CAPS verification (using pyCAPS) case cart3d_PyTest.py passed (as expected)
=================================================


=================================================
+ echo 'astros_ThreeBar_PyTest.py test;'
+ tee -a /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
astros_ThreeBar_PyTest.py test;
+ python -u astros_ThreeBar_PyTest.py -outLevel=0
+ tee -a /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/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	0m1.110s
user	0m0.770s
sys	0m0.210s
+ status=0
+ set +x

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


=================================================
+ echo 'astros_Flutter_15degree.py test;'
+ tee -a /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
astros_Flutter_15degree.py test;
+ python -u astros_Flutter_15degree.py -outLevel=0
+ tee -a /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/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	0m1.597s
user	0m0.914s
sys	0m0.274s
+ status=0
+ set +x

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


=================================================
+ echo 'masstran_PyTest.py test;'
+ tee -a /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
masstran_PyTest.py test;
+ python -u masstran_PyTest.py -outLevel=0
+ tee -a /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt

Getting results mass properties.....


Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = Ribs_and_Spars, index = 1
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 0
Getting surface mesh for body 1 (of 1)
Body 1 (of 1)
Number of nodes    = 1159
Number of elements = 798
Number of triangle elements      = 0
Number of quadrilateral elements = 798
----------------------------
Total number of nodes    = 1159
Total number of elements = 798
Mapping Csys attributes ................
	Number of unique Csys attributes = 0

Getting FEA coordinate systems.......
	Number of coordinate systems - 0
	No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
	Number of unique capsConstraint attributes = 1
	Name = Rib_Constraint, index = 1
Mapping capsLoad attributes ................
	Number of unique capsLoad attributes = 0
Mapping capsBound attributes ................
	Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
	Number of unique capsConnect attributes = 0
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = Ribs_and_Spars, index = 1
Setting FEA Data
	Mesh for body = 0
	Number of nodal coordinates = 1159
	Number of elements = 798
	Elemental Nodes = 0
	Elemental Rods  = 0
	Elemental Tria3 = 0
	Elemental Quad4 = 798

Getting FEA materials.......
	Number of materials - 2
	Material name - Madeupium
	Material name - Unobtainium
	No "materialType" specified for Material tuple Unobtainium, defaulting to "Isotropic"
	Done getting FEA materials

Getting FEA properties.......
	Number of properties - 1
	Property name - Ribs_and_Spars
	No "material" specified for Property tuple Ribs_and_Spars, defaulting to an index of 1
	Done getting FEA properties
Updating mesh element types based on properties input
Area      3.428666259749
Mass      5383.006027806
Centroid  [1.222256036872, 0.1634981473779, -4.647736192456e-11]
CG        [1.222256036872, 0.1634981473779, -4.647907951721e-11]
Ixx       22133.97306031
Iyy       23448.30046704
Izz       1389.213122564
Ixy       164.2055275655
Ixz       -7.485782319314e-06
Iyz       1.710545499156e-06
I         [22133.97306031, 23448.30046704, 1389.213122564, 164.2055275655, -7.485782319314e-06, 1.710545499156e-06]
II        [[22133.97306031, -164.2055275655, 7.485782319314e-06], [-164.2055275655, 23448.30046704, -1.710545499156e-06], [7.485782319314e-06, -1.710545499156e-06, 1389.213122564]]

real	0m5.598s
user	0m5.760s
sys	0m5.795s
+ status=0
+ set +x

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


=================================================
+ echo 'hsm_SingleLoadCase_PyTest.py test;'
+ tee -a /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
hsm_SingleLoadCase_PyTest.py test;
+ tee -a /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
+ python -u hsm_SingleLoadCase_PyTest.py -outLevel=0

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

Getting FEA coordinate systems.......
	Number of coordinate systems - 0
	No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
	Number of unique capsConstraint attributes = 1
	Name = plateEdge, index = 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	0m0.889s
user	0m0.676s
sys	0m0.073s
+ status=0
+ set +x

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


=================================================
+ echo '../corsairlite/qp.py test;'
+ tee -a /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
../corsairlite/qp.py test;
+ python -u ../corsairlite/qp.py -outLevel=0
+ tee -a /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/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	0m6.508s
user	0m1.394s
sys	0m0.146s
+ status=0
+ set +x

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


*************************************************
*************************************************

=================================================
Did not run examples for:

abaqus
awave
Mystran
=================================================

All tests pass!


=================================================
=================================================
+ cd /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64
+ mkdir -p /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/test/plugs
+ cd /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/test/plugs
+ sort -f
+ find /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/data/Plugs -name 'plugs0*.csm'
+ awk '{ n=split($0, a, ";"); for(i=1; i<=n; i+=2) print a[i] }' /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/JenkinsESP/data/plugs/plugsFailure.txt
+ cp /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/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 46336
-rw-r--r--  1 jenkins  staff   1.2M May  3 00:18 ASTRO.D01
-rw-r--r--  1 jenkins  staff   277K May  3 00:18 ASTRO.IDX
-rwxr-xr-x  1 jenkins  staff   130K May  3 00:19 ESPxddm
-rwxr-xr-x  1 jenkins  staff   212K May  3 00:18 Slugs
-rwxr-xr-x  1 jenkins  staff    86K May  3 00:18 TestFit
-rwxr-xr-x  1 jenkins  staff   1.6M May  3 00:18 avl
-rwxr-xr-x  1 jenkins  staff    35K May  3 00:19 cart3dTest
-rwxr-xr-x  1 jenkins  staff    34K May  3 00:17 egads2cart
-rwxr-xr-x  1 jenkins  staff    70K May  3 00:19 egads2cgt
-rwxr-xr-x  1 jenkins  staff   345K May  3 00:19 friction
-rwxr-xr-x  1 jenkins  staff    10M May  3 00:18 mastros.exe
-rwxr-xr-x  1 jenkins  staff   749K May  3 00:18 mses
-rwxr-xr-x  1 jenkins  staff   1.4M May  3 00:18 mset
-rwxr-xr-x  1 jenkins  staff    34K May  3 00:18 phaseUtil
-rw-r--r--  1 jenkins  staff   1.6K May  3 00:20 pod.egads
-rw-r--r--  1 jenkins  staff     0B May  3 00:20 port7681.jrnl
-rwxr-xr-x  1 jenkins  staff   1.2M May  3 00:18 pplot
-rwxr-xr-x  1 jenkins  staff   1.1M May  3 00:18 pxplot
-rwxr-xr-x  1 jenkins  staff    68K May  3 00:18 sensCSM
-rwxr-xr-x  1 jenkins  staff   192K May  3 00:18 serveCSM
-rwxr-xr-x  1 jenkins  staff   175K May  3 00:18 serveESP
-rwxr-xr-x  1 jenkins  staff    52K May  3 00:17 vCurvature
-rwxr-xr-x  1 jenkins  staff    51K May  3 00:17 vGeom
-rwxr-xr-x  1 jenkins  staff    36K May  3 00:17 vTess
-rwxr-xr-x  1 jenkins  staff   1.7M May  3 00:17 vTesstatic
-rw-r--r--  1 jenkins  staff   195K May  3 00:20 wingMultiModel.bdf
-rwxr-xr-x  1 jenkins  staff   1.7M May  3 00:18 xfoil
( 1 / 4 )
data/Plugs/plugs0a.csm;
++ /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/bin/serveCSM /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/data/Plugs/plugs0a.csm -outLevel 0 -plugs 25 -plot /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/data/Plugs/plugs0.cloud -batch -verify -jrnl /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/data/Plugs/buildFinal.jrnl
WARNING:: cannot open "/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/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_Beta/7.8/DARWIN_ARM64/EngSketchPad/data/Plugs/buildFinal.jrnl"



==> Closing input journal file

==> serveCSM completed successfully with no verification data

real	0m9.210s
user	0m6.056s
sys	0m0.370s
++ set +x
data/Plugs/plugs0a                  passed (as expected)
--------------------------------------------------------------------------------------------------
( 2 / 4 )
data/Plugs/plugs0b.csm;
++ /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/bin/serveCSM /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/data/Plugs/plugs0b.csm -outLevel 0 -plugs 25 -plot /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/data/Plugs/plugs0.cloud -batch -verify -jrnl /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/data/Plugs/buildFinal.jrnl
WARNING:: cannot open "/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/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_Beta/7.8/DARWIN_ARM64/EngSketchPad/data/Plugs/buildFinal.jrnl"



==> Closing input journal file

==> serveCSM completed successfully with no verification data

real	0m9.863s
user	0m6.939s
sys	0m0.075s
++ set +x
data/Plugs/plugs0b                  passed (as expected)
--------------------------------------------------------------------------------------------------
( 3 / 4 )
data/Plugs/plugs0c.csm;
++ /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/bin/serveCSM /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/data/Plugs/plugs0c.csm -outLevel 0 -plugs 25 -plot /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/data/Plugs/plugs0.cloud -batch -verify -jrnl /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/data/Plugs/buildFinal.jrnl
WARNING:: cannot open "/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/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_Beta/7.8/DARWIN_ARM64/EngSketchPad/data/Plugs/buildFinal.jrnl"



==> Closing input journal file

==> serveCSM completed successfully with no verification data

real	0m24.393s
user	0m28.733s
sys	0m0.172s
++ set +x
data/Plugs/plugs0c                  passed (as expected)
--------------------------------------------------------------------------------------------------
( 4 / 4 )
data/Plugs/plugs0d.csm;
++ /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/bin/serveCSM /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/data/Plugs/plugs0d.csm -outLevel 0 -plugs 25 -plot /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/data/Plugs/plugs0.cloud -batch -verify -jrnl /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/data/Plugs/buildFinal.jrnl
WARNING:: cannot open "/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/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_Beta/7.8/DARWIN_ARM64/EngSketchPad/data/Plugs/buildFinal.jrnl"



==> Closing input journal file

==> serveCSM completed successfully with no verification data

real	0m23.584s
user	0m28.635s
sys	0m0.176s
++ 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_Beta/7.8/DARWIN_ARM64')
[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_Beta/7.8/DARWIN_ARM64')
[Clang] -> found 0 issues (skipped 0 duplicates)
[Clang] Parsing console log (workspace: '/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64')
[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_Beta/7.8/DARWIN_ARM64')
[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_Beta/7.8/DARWIN_ARM64')
[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_Beta/7.8/DARWIN_ARM64')
[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_Beta/CASREV=7.8,ESP_ARCH=DARWIN_ARM64,buildnode=viggen #713'.
[Checks API] No suitable checks publisher found.
[WS-CLEANUP] Deleting project workspace...
[WS-CLEANUP] Deferred wipeout is used...
[WS-CLEANUP] done
Finished: SUCCESS